Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status Documentation only) Issue Number 10073743 AMOC TO AD 328 SUPPORT 328-100 With CN-100519 EASA Major Change Applicable to Model 328-100 - all EASA 2008-0107 08/07/2020 Active SERVICES GmbH Approval No 10073701 an alternativeSpring S/N Tab lever P/N 001A272A4020006 instead of P/N001A272A4020004 aslisted in AD Section "Required action(s) and Compliance Time(s): No (5)"has been certified.The new P/N is considered also as terminating action to above listed AD... 10076933 AMOC TO AD AEROCONSEIL A320-232 ADT 406 ELT INSTALLATION ON A320 0242-05-A-ATI-F01-R00 or None 2020-0103 15/07/2021 Active A320-214 FAMILY.Following the Airworthiness Directive later revisions approved/ A320-212 2020-0103 published on the EASAwebsite acceptedunder theEASA A320-211 dated on 07 May 2020 EASA, related to the system. A319-114 Emergency LocatorTransmitter (ELT) having Part Number PN 01N65900 installed onlybyAirbus in production or as per Service Bulletin has... 10074765 AMOC TO AD AEROLOGIC Gmbh 777F Fuel - Centre Wing Tank Fuel Quantity Flight Crew Operations Serial Number(s): 36001, 36002, US-2020-11-11 06/11/2020 Active Indicating System - Check / Manual Bulletin for Aerologic 36003, 36004, 36198, AFMRevisionAerologic GmbH submitted an GmbH ref. AGT-49dated July 36199,36200,36201, 37708, application toEASA for an AMOC to 16, 2019Flight Crew 37710, 66081, 66082, 66085, ADUS-2020-11-11.AD US-2020‐11‐11 Operations Manual Volume 1 66086, 66088, 66164, paragraphs (g)(1) through (6) define work ref. 23TR dated June 15, 66632,66814 instructionsto be accomplished by 2020Maintenance TIP ref. 777 performing a Refuelling Station Door Cycling MT 28-031 R2 dated May 29, (RSDC)A... 2020 10073510 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial AD 2006-22-09 16/06/2020 Active ICELANDIC to the accomplishment of theinitial and Continued Airworthiness (ICA) Number (S/N) 27602. repeat inspections for overlapped skin panels of V1Aerospace document as required byparagraph (g) mandated by Damage Tolerance Analysis Airworthiness Directive (AD) (DTA) D20-0350-001 Rev 2006-22-09applicable to Boeing model 00,dated 06 Apr 2020.V1 747-4F6 with S/N 27602.The subject Aerospace Repair Instructions aircraft was damaged... R20-00350-001 Rev.04, dated 20 Mar2020. 10073511 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial AD 2016-04-02 16/06/2020 Active ICELANDIC to the accomplishment of theinitial and Continued Airworthiness (ICA) Number (S/N) 27602. repeat inspections and modifications of of V1Aerospace document certain skin lapjoints as required by Damage Tolerance Analysis paragraph (g) mandated by Airworthiness (DTA) D20-0350-001 Rev Directive(AD) 2016-04-02 applicable to 00,dated 06 Apr 2020.V1 Boeing model 747-4F6 airplane with S/ Aerospace Repair Instructions N27602.The subject air... R20-00350-001 Rev.04, dated 20 Mar2020. 10073512 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial AD 2018-04-07 16/06/2020 Active ICELANDIC to the accomplishment of thestructural Continued Airworthiness (ICA) Number (S/N) 27602. inspections required by paragraph (i) of V1Aerospace document mandated byAirworthiness Directive (AD) Damage Tolerance Analysis 2018-04-07 applicable to Boeing (DTA) D20-0350-001 Rev model747-4F6 airplane with S/N 27602.The 00,dated 06 Apr 2020.V1 subject aircraft was damaged in an incident Aerospace Repair Instructions involving ground suppo... R20-00350-001 Rev.04, dated 20 Mar2020. 10074335 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial 2016-04-02 24/09/2020 Active ICELANDIC to the accomplishment of theinitial and Continued Airworthiness (ICA) Number (S/N) 25700 repeat inspections and modifications of of V1Aerospace document certain skin lapjoints as required by Damage Tolerance Analysis paragraph (g) mandated by Airworthiness (DTA) D20-0365-001 Rev Directive(AD) 2016-04-02 applicable to 01,dated 10 Jul 2020.V1 Boeing model 747-4H6 airplane with S/ Aerospace Repair Instructions N25700.The subject air... R20-00365-001 Rev.03, dated 09 Apr2020.

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 1 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074826 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial 2016-04-02 13/11/2020 Active ICELANDIC to the accomplishment of theinitial and Continued Airworthiness (ICA) Number (S/N) 27899. repeat inspections and modifications of of V1Aerospace document certain skin lapjoints as required by Damage Tolerance Analysis paragraph (g) mandated by Airworthiness (DTE) Directive(AD) 2016-04-02 applicable to documentD20-00786-001 Rev Boeing model 747-400 airplane with S/ 01, dated 29 October 2020V1 N27899.The subject air... Aerospace Repair Instructions R20-00786-001 Rev 01 dated 21 July2020. 10074832 AMOC TO AD AIR ATLANTA REV. 1 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial 2018-04-07 17/11/2020 Active ICELANDIC to the accomplishment of thestructural Continued Airworthiness (ICA) Number (S/N) 27899. inspections mandated by paragraph (i) of of V1Aerospace document AirworthinessDirective (AD) 2018-04-07 Damage Tolerance Evaluation applicable to Boeing model 747-400 (DTE) airplanewith S/N 27899.The subject aircraft documentD20-00786-001 Rev had a gouge and dent in the RH fuselage skin 01, dated 29 October 2020V1 at STA2040-20... Aerospace Repair Instructions R20-00786-001 Rev 01 dated 21 July2020. 10075383 AMOC TO AD AIR ATLANTA 747-400 Air Icelandic Atlanta has requested an AMOC V1 Aerospace Repair Boeing Model 747-400 with Serial FAA 2010-01-01 12/01/2021 Active ICELANDIC to the accomplishment of theinitial and R20-0745-001, Rev 08 - RH Number (S/N) 27899. repeat inspections mandated by paragraphs Main Entry Door N° 5Forward (g)(1) and (j) ofAirworthiness Directive (AD) Reveal Frame,dated July 2010-01-01, applicable to Boeing 20,2020.V1 Aerospace model747-400 series airplane with S/N Damage Tolerance Analysis 27899, for the repaired areas ofcracked RH (DTA) document and LH Main En... D20-00745-001 Rev00, dated 23 Oct 2020*******V1 Aerospace Repair R20-0762-001, Rev 08 - LH Main Entry Door N° 5Forward Reveal Frame,dated Ju... 10075386 AMOC TO AD AIR ATLANTA 747-400 Fuselage areas cracking inspections V1 Aerospace Repair Boeing Model 747-400 with Serial EASA ADOPTED FAA 13/01/2021 Active ICELANDIC (2013-17-08 The Boeing Company: Docket R20-0745-001, Rev 08 - RH Number (S/N) 27899 2013-17-08 No. FAA-2013-0097; DirectorateIdentifier Main Entry Door N° 5Forward 2011-NM-243-AD; Amendment 39-17572)Air Reveal Frame, dated July Icelandic Atlanta has requested an AMOC to 20,2020.V1 the accomplishment of theinitial and repeat AerospaceDamage Tolerance inspections mandated by paragraphs (o) Analysis (DTA) document ofAirworthiness Dire... D20-00745-001 Rev00, dated 23 Oct 2020V1 Aerospace Repair R20-0762-001, Rev 08- LH Main Entry Door N° 5Forward Reveal Frame, dated July 22... 10075388 AMOC TO AD AIR ATLANTA 747-400 Inspections to detect cracks of all structure V1 Aerospace Repair Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 13/01/2021 Active ICELANDIC identified inBoeingdocument D6-35022 R20-0745-001, Rev 08 - RH Number (S/N) 27899 2018-04-07 “Supplemental Structural Main Entry Door N° 5Forward InspectionDocument for Model747 Reveal Frame, dated July ,” Revision H, dated September 20,2020.V1 2013(2018-04-07 The Boeing Company: AerospaceDamage Tolerance Amendment 39-19202; Docket Analysis (DTA) document No.FAA-2016-9067; Product Identifier 2016- D20-00745-001 Rev00, dated NM-043-AD).Ai... 23 Oct 2020*******V1 Aerospace Repair R20-0762-001,Rev 08 - LH Main Entry Door N° 5Forward Reveal Frame, datedV... 10075555 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC V1 Aerospace Repair Boeing Model 747-400F with Serial EASA ADOPTED FAA 02/02/2021 Active ICELANDIC to the accomplishment of thecorrective Instructions R21-00939-001, Number (S/N) 27603. 2005-03-01 actions required by paragraph (e) Rev. 01 dated 05 Jan2021. ofAirworthiness Directive(AD) 2005-03-01 applicable to Boeingmodel 747-400F airplane with S/N27603.The subject aircraft features a repair of shim migration at theunderwing midspar f...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 2 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10075642 AMOC TO AD AIR ATLANTA 747-400 Inspections to detect cracks of all structure Section 5.0 Instructions for Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 16/02/2021 Active ICELANDIC identified inBoeingdocument D6-35022 Continued Airworthiness (ICA) Number (S/N) 27066 2018-04-07 “Supplemental Structural of V1Aerospace document InspectionDocument for Model747 Damage Tolerance Evaluation Airplanes,” Revision H, dated September (DTE) 2013(2018-04-07 The Boeing Company: documentD20-00822-001 Rev Amendment 39-19202; Docket 01, dated 31 Jan 2021V1 No.FAA-2016-9067; Product Identifier 2016- Aerospace Repair Instructions NM-043-AD).Ai... R20-00822-001 Rev 05 dated 19 Sep 2020. 10075643 AMOC TO AD AIR ATLANTA 747-400 Body Station 2598 Bulkhead Inner Chord and Section 5.0 Instructions for Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 16/02/2021 Active ICELANDIC Web Inspection(2014-04-03 The Boeing Continued Airworthiness (ICA) Number (S/N) 27066 2014-14-03 Company: Amendment 39-17898; Docket of V1Aerospace document No.FAA-2014-0432; Product Identifier 2014- Damage Tolerance Evaluation NM-099-AD).Air Atlanta Icelandic has (DTE) requested an AMOC to the accomplishment documentD20-00822-001 Rev of theinspections mandated by paragraph (i) 01, dated 31 Jan 2021V1 of Airworthiness Dire... Aerospace Repair Instructions R20-00822-001 Rev 05 dated 19 Sep 2020. 10075762 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial EASA ADOPTED FAA 02/03/2021 Active ICELANDIC to the accomplishment of thepost-inspection Continued Airworthiness (ICA) Number (S/N) 27898. 2001-11-06 repair requirements mandated byparagraph of V1Aerospace document (i) ofAirworthiness Directive (AD) 2001-11-06 Damage Tolerance Evaluation applicable to Boeing model747-400 airplane (DTE) with S/N 27898.During a C-check on the documentD20-00844-001 Rev subject aircraft, a post-repair inspection... 00, dated 08 Jan 2021V1 Aerospace Repair Instructions R20-00844-001 Rev 00 dated 03 Oct 2020. 10075795 AMOC TO AD AIR ATLANTA 747-400 Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 05/03/2021 Active ICELANDIC to the accomplishment of therepair and Continued Airworthiness (ICA) Number (S/N) 27898 2001-15-14 inspection requirements mandated by of V1Aerospace document paragraph (g) and (h)(2)of Airworthiness Damage Tolerance Evaluation Directive (AD) 2020-15-04 applicable to (DTE) Boeing model747-400 airplane with S/N documentD20-00844-001 Rev 27898.During a C-check on the subject 00, dated 08 Jan 2021V1 aircraft, a post-repairt... Aerospace Repair Instructions R20-00844-001 Rev 00 dated 03 Oct 2020. 10075832 AMOC TO AD AIR ATLANTA 747-400 Air Icelandic Atlanta has requested an AMOC V1 Aerospace Repair Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 11/03/2021 Active ICELANDIC to the Nose Wheel Well (NWW)post Instructions R21-00950-001 Number (S/N) 27899. 2016-06-07 inspection repair requirements mandated Rev.02 dated26 Jan 2021V1 byparagraph (h) ofAirworthiness Directive Aerospace static (AD) 2016-06-07 applicable to Boeing substantiation S1-00950-001 model747-400 series airplane with S/N Rev.00, dated 26 Jan2021. 27899.During an inspection of the Nose Wheel Well pressure panels... 10076272 AMOC TO AD AIR ATLANTA REV. 1 747-400 Air Icelandic Atlanta has requested an AMOC Engineering Instruction EGAT Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 22/04/2021 Active ICELANDIC to the accomplishment of theinitial and E2010A52B-1529 Rev 01 Number (S/N) 27899. 2010-01-01 repeat inspections mandated by paragraph dated 04Aug 2010V1 (g) ofAirworthiness Directive (AD) Aerospace Damage Tolerance 2010-01-01, applicable to Boeing Evaluation (DTE) document model747-400 series airplane with S/N D20-00913-001Rev 00, dated 27899, for the repaired areas ofcracked LH 11 Feb 2021 Main Entry Door (MED) N°4D... 10076278 AMOC TO AD AIR ATLANTA 747-400 Main Frame – Inspections based on Fatigue Engineering Instruction EGAT Boeing Model 747-400 with Serial FAA 2010-01-01 22/04/2021 Active ICELANDIC Test Results(2010-01-01 The Boeing E2010A52B-1533 Rev 02 Number (S/N) 27899 Company: Docket No. FAA-2009-0655; dated 04Aug 2010V1 DirectorateIdentifier 2008-NM-192-AD; Aerospace Damage Tolerance Amendment 39-16157)Air Icelandic Atlanta Evaluation (DTE) document has requested an AMOC to the D20-00914-001Rev 01, dated accomplishment of theinitial and repeat 11 Feb 2021 inspections mandated by paragraph (g) of...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 3 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10076283 AMOC TO AD AIR ATLANTA 747-400 Main Frame – Inspections based on Fatigue Engineering Instruction EGAT Boeing Model 747-400 with Serial FAA 2010-01-01 22/04/2021 Active ICELANDIC Test Results(2010-01-01 The Boeing E2010A52B-1531 Rev 01 Number (S/N) 27899 Company: Docket No. FAA-2009-0655; dated 04Aug 2010V1 DirectorateIdentifier 2008-NM-192-AD; Aerospace Damage Tolerance Amendment 39-16157)Air Icelandic Atlanta Evaluation (DTE) document has requested an AMOC to the D20-00915-001Rev 01, dated accomplishment of theinitial and repeat 19 Mar 2021 inspections mandated by paragraph (g) of... 10076284 AMOC TO AD AIR ATLANTA 747-400 Main Frame – Inspections based on Fatigue Engineering Instruction EGAT Boeing Model 747-400 with Serial FAA 2010-01-01 22/04/2021 Active ICELANDIC Test Results(2010-01-01 The Boeing E2010A52B-1532 Rev 02 Number (S/N) 27899 Company: Docket No. FAA-2009-0655; dated 04Aug 2010V1 DirectorateIdentifier 2008-NM-192-AD; Aerospace Damage Tolerance Amendment 39-16157)Air Icelandic Atlanta Evaluation (DTE) document has requested an AMOC to the D20-00916-001Rev 0, dated accomplishment of theinitial and repeat 10 Feb 2021 inspections mandated by paragraph (g) of... 10076285 AMOC TO AD AIR ATLANTA 747-400 Main Frame – Inspections based on Fatigue Engineering Instruction EGAT Boeing Model 747-400 with Serial FAA 2010-01-01 22/04/2021 Active ICELANDIC Test Results(2010-01-01 The Boeing E2011A52B-1896 Rev 01 Number (S/N) 27899 Company: Docket No. FAA-2009-0655; dated 09Oct 2011V1 DirectorateIdentifier 2008-NM-192-AD; Aerospace Damage Tolerance Amendment 39-16157)Air Icelandic Atlanta Evaluation (DTE) document has requested an AMOC to the D20-00917-001Rev 0, dated accomplishment of theinitial and repeat 11 Feb 2021 inspections mandated by paragraph (g) of... 10076286 AMOC TO AD AIR ATLANTA 747-400 Air Icelandic Atlanta has requested an AMOC Engineering Instruction EGAT Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 22/04/2021 Active ICELANDIC to the accomplishment of theinitial and E2011A52B-1885 Rev 01 Number (S/N) 27899. 2010-01- repeat inspections mandated by paragraph dated 07Oct 2011V1 (g) ofAirworthiness Directive (AD) Aerospace Damage Tolerance 2010-01-01, applicable to Boeing Evaluation (DTE) document model747-400 series airplane with S/N D20-00918-001Rev 0, dated 27899, for the repaired areas ofcracked RH 10 Feb 2021. Main Entry Door (MED) N°4C... 10076287 AMOC TO AD AIR ATLANTA 747-400 Air Icelandic Atlanta has requested an AMOC Engineering Instruction EGAT Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 22/04/2021 Active ICELANDIC to the accomplishment of theinitial and E2013A52B-444 Rev 01 dated Number (S/N) 27899. 2010-01-01 repeat inspections mandated by paragraph 15 Mar 2013V1 Aerospace (g) ofAirworthiness Directive (AD) Damage Tolerance Evaluation 2010-01-01, applicable to Boeing (DTE) document model747-400 series airplane with S/N D20-00920-001Rev 0, dated 27899, for the repaired areas ofcracked LH 11 Feb 2021. Main Entry Door (MED) N°5D... 10076301 AMOC TO AD AIR ATLANTA 747-400 BCF Main Frame – Inspections based on Fatigue V1 Aerospace Damage Boeing Model 747-400BCF with FAA 2010-01-01 26/04/2021 Active ICELANDIC Test Results(2010-01-01 The Boeing Tolerance Evaluation (DTE) Serial Number (S/N) 24801 Company: Docket No. FAA-2009-0655; document D20-00871-001Rev DirectorateIdentifier 2008-NM-192-AD; 0, dated 24 Jan 2021 Amendment 39-16157)Air Icelandic Atlanta has requested an AMOC to the accomplishment of theinitial and repeat inspections mandated by paragraph (g) of... 10076347 AMOC TO AD AIR ATLANTA 747-400F Body Station 2598 Bulkhead Inner Chord and A20WE Section 5.0 Instructions for Boeing Model 747-400F with Serial FAA 2014-14-03 28/04/2021 Active ICELANDIC Web Inspection(2014-04-03 The Boeing Continued Airworthiness (ICA) Number (S/N) 28263 Company: Amendment 39-17898; Docket of V1Aerospace document No.FAA-2014-0432; Product Identifier 2014- Damage Tolerance Evaluation NM-099-AD).Air Atlanta Icelandic has (DTE) requested an AMOC to the accomplishment documentD20-00872-001 Rev of theinspections mandated by paragraph (i) 00, dated 05 Feb 2021Haeco of Airworthiness Dire... Repair Scheme RSK-53-0042 Rev 00 dated 13 Jul 2018. 10076348 AMOC TO AD AIR ATLANTA 747-400F Inspections to detect cracks of all structure A20WE Section 5.0 Instructions for Boeing Model 747-400F with Serial FAA 2018-04-07 28/04/2021 Active ICELANDIC identified inBoeingdocument D6-35022 Continued Airworthiness (ICA) Number (S/N) 28263 “Supplemental Structural of V1Aerospace document InspectionDocument for Model747 Damage Tolerance Evaluation Airplanes,” Revision H, dated September (DTE) 2013(2018-04-07 The Boeing Company: documentD20-00872-001 Rev Amendment 39-19202; Docket 00, dated 05 Feb 2021Haeco No.FAA-2016-9067; Product Identifier 2016- Repair Scheme RSK-53-0042 NM-043-AD).Ai... Rev 00 dated 13 Jul 2018.

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 4 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10076361 AMOC TO AD AIR ATLANTA 747-400F Main Frame – Inspections based on Fatigue A20WE V1 Aerospace Damage Boeing Model 747-400F with Serial FAA 2010-01-01 29/04/2021 Active ICELANDIC Test Results(2010-01-01 The Boeing Tolerance Evaluation (DTE) Number (S/N) 28263 Company: Docket No. FAA-2009-0655; document D20-00888-001Rev DirectorateIdentifier 2008-NM-192-AD; 0, dated 23 Feb 2021 Amendment 39-16157)Air Icelandic Atlanta has requested an AMOC to the accomplishment of theinitial and repeat inspections mandated by paragraph (g) of... 10076394 AMOC TO AD AIR ATLANTA 747-400F Inspections to detect cracks of all structure A20WE Section 5.0 Instructions for Boeing Model 747-400F with Serial FAA 2018-04-07 04/05/2021 Active ICELANDIC identified inBoeingdocument D6-35022 Continued Airworthiness (ICA) Number (S/N) 26563 “Supplemental Structural of V1Aerospace document InspectionDocument for Model747 Damage Tolerance Evaluation Airplanes,” Revision H, dated September (DTE) 2013(2018-04-07 The Boeing Company: documentD20-00907-001 Rev Amendment 39-19202; Docket 02, dated 13 Apr 2021 No.FAA-2016-9067; Product Identifier 2016- NM-043-AD).Ai... 10076405 AMOC TO AD AIR ATLANTA 747-400F Air Atlanta Icelandic has requested an AMOC A20WE Section 5.0 Instructions for Boeing Model 747-400F with Serial EASA ADOPTED FAA AD 05/05/2021 Active ICELANDIC to the accomplishment of theinitial and Continued Airworthiness (ICA) Number (S/N) 26563. 2016-04-02 repeat inspections and modifications of of V1Aerospace document certain skin lapjoints as required by Damage Tolerance Evaluation paragraph (g) mandated by Airworthiness (DTE) Directive(AD) 2016-04-02 applicable to documentD20-00907-001 Rev Boeing model 747-400F airplane with S/ 02, dated 13 Apr 2021. N26563.During a C-che... 10076425 AMOC TO AD AIR ATLANTA 747-400 Air Icelandic Atlanta has requested an AMOC A20WE V1 Aerospace Damage Boeing Model 747-400 with Serial EASA ADOPTED FAA AD 10/05/2021 Active ICELANDIC to the Nose Wheel Well (NWW)inspections Tolerance Evaluation (DTE) Number (S/N) 27899. 2016-06-07 mandated by paragraph (g) of Airworthiness document D21-00950-001Rev Directive (AD)2016-06-07 applicable to 00, dated 30 Mar 2021V1 Boeing model 747-400 series airplane with S/ Aerospace Repair Instructions N27899.During an inspection of the NWW R21-00950-001 Rev.02 dated pressure panels as per AD 2016-06-07 26 Jan 2021. onBoeing model... 10076511 AMOC TO AD AIR ATLANTA 747-400F Air Atlanta Icelandic has requested an AMOC Section 5.0 Instructions for Boeing Model 747-400F with Serial EASA ADOPTED FAA AD 19/05/2021 Active ICELANDIC to the accomplishment of thestructural Continued Airworthiness (ICA) Number (S/N) 28263. 2018-04-07 inspections mandated by paragraph (i) of of V1Aerospace document AirworthinessDirective (AD) 2018-04-07 Damage Tolerance Evaluation applicable to Boeing model 747-400F (DTE) airplanefor the skin and structure repaired documentD20-00884-001 Rev area of cargo door at STA 1790 ofS/N 00, dated 11 Apr 2021. 28263.During service... 10076606 AMOC TO AD AIR ATLANTA 747-400F Main Frame – Inspections based on Fatigue V1 Aerospace Damage Boeing Model 747-400F with Serial FAA 2010-01-01 02/06/2021 Active ICELANDIC Test Results(2010-01-01 The Boeing Tolerance Evaluation (DTE) Number (S/N) 28263 Company: Docket No. FAA-2009-0655; document D20-00885-001Rev DirectorateIdentifier 2008-NM-192-AD; 0, dated 13 Apr 2021 Amendment 39-16157)Air Icelandic Atlanta has requested an AMOC to the accomplishment of theinitial and repeat inspections mandated by paragraph (g) of... 10077051 AMOC TO AD AIR ATLANTA 747-400F Inspections to detect cracks of all structure Section 5.0 Instructions for Boeing Model 747-400F with Serial FAA 2018-04-07 03/08/2021 Active ICELANDIC identified inBoeingdocument D6-35022 Continued Airworthiness (ICA) Number (S/N) 28263 “Supplemental Structural of V1Aerospace document InspectionDocument for Model747 Damage Tolerance Evaluation Airplanes,” Revision H, dated September (DTE) 2013(2018-04-07 The Boeing Company: documentD20-00887-001 Rev Amendment 39-19202; Docket 00, dated 05 Apr 2021Haeco No.FAA-2016-9067; Product Identifier 2016- Repair Scheme RSK-53-0042 NM-043-AD).Ai... Rev 00 date. 10077052 AMOC TO AD AIR ATLANTA 747-400 Inspections to detect cracks of all structure Section 5.0 Instructions for Boeing Model 747-400 with Serial FAA 2018-04-07 03/08/2021 Active ICELANDIC identified inBoeingdocument D6-35022 Continued Airworthiness (ICA) Number (S/N) 27602 “Supplemental Structural of V1Aerospace document InspectionDocument for Model747 Damage Tolerance Evaluation Airplanes,” Revision H, dated September (DTE) D21-00953-001 Rev00, 2013(2018-04-07 The Boeing Company: dated 25 May 2021.V1 Amendment 39-19202; Docket Aerospace Repair Instructions No.FAA-2016-9067; Product Identifier 2016- R21-00953-001 Rev.02, dated NM-043-AD).Ai... 30 Jan2021.

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 5 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10077056 AMOC TO AD AIR ATLANTA 747-400 Nose Wheel Well sidewall panel web V1 Aerospace Damage Boeing Model 747-400 with Serial FAA 2016-06-07 03/08/2021 Active ICELANDIC (2016-06-07 The Boeing Company: Tolerance Evaluation (DTE) Number (S/N) 27898 Amendment 39-18438; Docket document D21-01036-001Rev No.FAA-2014-0774; Directorate Identifier 00 dated 09 Jun 2021.V1 2013-NM-154-AD)Air Icelandic Atlanta has Aerospace Repair Instructions requested an AMOC to the Nose Wheel Well R21-01036-001 Rev.02 dated (NWW)inspections mandated by paragraph 13 May 2021. (g) of Airworthiness Directive (AD) 2016-06-07... 10076725 AMOC TO AD AIRBUS DEFENCE A330-200, A330-243 For the Serial Numbers listed in the A330-MRTT STC 10069541:0747 2020-0273 29/06/2021 Active AND SPACE S.A. Limitations and Conditionsparagraph of this 0892 0898 0951 0969 0980 0996 AMOC (A330-MRTT, aircrafts modified bythe 1036 1080 1183 1186 1235 1379 STCsincluded in the STC Approved Model List 12501478 1516 1667 1735 1762 (10069541) and for A330-FSTA,aircrafts 1787 1799 1808 1822 1848 1857 modified by STC2 10035945 and STC1 1883 1886 18911911 1916 1919 10034690), the AirbusDefence and Space 1942 1945 1960 19651968 1982 Service Bulletin A3... 1989 1998 2008 2011A330-FSTA STC1 10034690 and STC2 10035945:1033 1046 1248 1275 1312 1334 1363... 10072585 AMOC TO AD AIRBUS AS 332 L Partial removal of the de-icing system, as Applicability = Model: AS 332 L; Serial doc. This AMOC is valid for the 2018-0142R1 25/02/2020 Active accomplished on thehelicopter AS332L, S/N No.: 2113 ETG478/17 issue EAirbus AS 332 L, Serial Number 2113 in accordance with Airbus Helicoptersdoc. Technical 2113provided that this helicopter Helicoptersinstructions described below (see Agreement AS332-02-001C stays in a configuration of Associated Technical Documentation),is partialremoval of the de-icing adequate Alternative Method of Compliance system as defined above.Should to the AD 2018-0142R1 toprevent that the helicopterbe otherwise helicopter to suffer... modified, it will have tocomply with altogetherrequirement of the AD 2018-0142R1. 10076125 AMOC TO AD AIRBUS HELICOPTERS AS 332 L1 As Alternative Method of Compliance None Limited to Serial Numbers: 2332, 2020-0022R2 07/04/2021 Active AS 332 C, AS 332 L (AMOC) to the requirements of 2351, 2053, 2067, 2132, 2151, AD2020-0022R2, Paragraph (2):For Group 1 2218<(>,<)> 9002, 2001, 2347, helicopters:Within 300 FH or within 31 9007, 2155, 2221, 9004<(>,<)> August 2021,whichever occurs first after 21 9003, 2145, 2143, 2153 and 2341. February 2020 [the effective date of theoriginalissue of this AD], modify the helicopter by installing FFMPa... 10076393 AMOC TO AD AIRBUS HELICOPTERS EC120B ATA 32 – – Skid Tubes – EC120 B ETIFF n°2021-0027 2020-0247 04/05/2021 Active InspectionParagraph (5) of EASA AD 2020-0247 is replaced by the following:(5) Replacing each affected part on a helicopter under the conditions oftable 1 is an acceptable alternative method to comply with therequirements of paragraph (4) of this AD for that helic... 10076963 AMOC TO AD AIRBUS HELICOPTERS EC 225 LP As Alternative Method of Compliance Airbus Helicopters (AH) This AMOC is limited to the EC225 2019-0074 20/07/2021 Active (AMOC) to requirement (6) of EASA Emergency Alert Service LP helicopter S/Ns 2662, 2749, AD2019-0074 mandating the replacement of Bulletin (EASB) 2753,2759, 2767, 2792, 2927 and the MainRotor (M/R) rotatingswashplate Part ref.EC225-05A051 Revision 2, 2973. Number (P/N) 332A31-3074-00 or P/N dated 26 February 2019;AH 332A31-3074-01 beforeit exceeds 12 years document ref. ETMD since new (date of manufacture), accomplish 2021_0330 issue A, released thefollowing action:-,,i... on 20 July 2021;AH document ref. ETMD N°2018-0215 issue B, released on 29June 2018;or later approved revisions of these documents. 10077146 AMOC TO AD AIRBUS HELICOPTERS EC 225 LP ATA 25 – Equipment / Furnishings – Hoist – EASA Major Change Approval This AMOC is limited to the EC225 2015-0226R5 27/08/2021 Active Test / ReplacementAs Alternative Method of 10073295 dated 18 May LP helicopter S/Ns 2914 and 2986. Compliance (AMOC) to requirement (7), 2020;Airbus Helicopters ALS Table 4,of EASA AD 2015-0226R5, Interval NR 013 dated 08 March applicable to All Affected 2021;or later approved Helicopters,accomplish the following action:- revisions of these documents. atintervals of 36 months (with a margin of 4 months), or 2000o...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 6 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10077047 AMOC TO AD A400M-180 ATA 71 – Power Plant – Engine Vibration (D< None 2021-0077 02/08/2021 Active SOCIEDAD Isolation System – Inspection / (>&<)>S) All Operators LIMITADAAMSL ReplacementEASA AD 2021-0077 requests to Transmission (AOT)AOT- performrepetitive inspections of theforward A400M-71-0001 Revision 1 lower Engine VibrationIsolation Systems (EVIS). The objectiveof these inspectionsis to detect a premature EVIS housing bolt failurethat, if s... 10072500 AMOC TO AD AIRBUS S.A.S. A320-271N ATA – Aircraft Flight Manual Section Airbus Major Modification 2019-0189 11/02/2020 Active A320-251N, A320-253N Limitations – AmendmentThis AD mandates 163923Airbus Flight Airbus Aircraft Flight Manual (AFM) Operations Transmission Temporary Revision(TR) 773 issue 1, TR 774 999.0059/19 issue 1, TR 775 issue 1and TR 776 issue 1, asapplicable, introducing limitations within the Centre of Gravityenvelope to mitigate the reduced e... 10072604 AMOC TO AD AIRBUS S.A.S. A380-841 ATA 54 – Nacelles / Pylons – Inboard and RDAS ref. None 2020-0025 28/02/2020 Active Outboard Pylon Drain System –Inspection / 80662998/003/2019 ModificationAD 2020-0025 mandates repetitive inspections as per SB A380-54-8073until embodiment of the applicable Modification SBs (MSB) whichconstitute terminating action of the Inspection SB A380-54-8073.For Pylon 3... 10072605 AMOC TO AD AIRBUS S.A.S. REV. 1 A320-251N/-253N/-271N ATA – Aircraft Flight Manual Section Airbus Major Modification This AMOC Revision 1 approval AD-2019-0189 12/03/2020 Active Limitations – AmendmentThe AD 2019-0189 163923Airbus Flight supersedes:- the AMOC approval mandates Airbus Aircraft Flight Manual Operations Transmission 10072500, dated 11 February (AFM) TemporaryRevision (TR) 773 issue 1, 999.0059/19Airbus Flight 2020, and- the AMOC 10072605 TR 774 issue 1, TR 775 issue 1 and TR Operations Transmission Original issue, dated 28 February 776issue 1, as applicable, introducing 999.0012/20Airbus Service 2020. limitations within the Centre ofGravity Bulletin A320-27-1284 (at any envelope to mitigate theA... revision) 10073217 AMOC TO AD AIRBUS S.A.S. A320-214, A320-232 Background:EASA AD 2019-0279R1 was - Technical Note None 2019-0279R1 08/05/2020 Active issued to remove a potential unsafe AJEY-2020-0011/SD Rev A- conditiondue to insufficient clearance Airbus SB A320-26-1109 between the cargo fire Revision 1- MOD CJ0648: extinguishingpipes.MSNs 4170 and 5255 are Cargo Compartment Fire not impacted by the issue described in EASA Extinguishers Relocation- AD2019-0279R1 being modified according to EASA STC 10031840 (MSN EASA STC 10031840 (MSN 4170) &EASA 4170)- EASA STC 10050094 STCr... (MSN 5255)- TDDS26001: Technical Design Directive regarding ATA26 on A320- AIS SB 601903-25-000101-002 10073857 AMOC TO AD AIRBUS S.A.S. A321-213/-231/-232 EASA AD 2017-0237 was issued to detect an Technical Adaptation (TA) None 2017-0237 22/07/2020 Active A321-111/-112/-131/-211/-2 eventual engagement of theSecondary Load 80783356/007/2020 dated 12 Path (SLP) of the Trimmable Horizontal April 30th, 2020. A320-231/-232/-233 StabilizerActuator (THSA).Among the various A320-211/-212/-214/-215/-2 actions required by the EASA AD 2017-0237, 16 it has beenidentified that some tasks referred A319-131/-132/-133 through the mandated technicalpublications A319-111/-112/-113/-114/-1 h... 15 A318-111/-112/-121/-122 10073967 AMOC TO AD AIRBUS S.A.S. A321-251N/-253N/-271N ATA 34 – Navigation – Traffic Collision -Airbus SB A320-34-1760 None 2017-0091R2 05/08/2020 Active A321-231/-232 Avoidance System Processor –Modification dated September 09, 2019< A321-211/-212/-213 (Software Update) / ReplacementEASA (>,<)> forA320 CEOmodels- A321-111/-112/-131 AD2017-0091R2 was issued to address the Airbus SB A320-34-1761 A320-251N/-271N number of false TCASresolution advisories dated September 09, 2019, A320-231/-232/-233 (RA) by modifying the traffic for A320 NEO models.-Airbus A320-211/-212/-214/-215/-2 collisionavoidancesystem (TCAS) processor modification 166196 16 through an upgrade of the s... A319-131/-132/-133 A319-111/-112/-113/-114/-1 15 A318-111/-112/-1231/-122

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 7 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074245 AMOC TO AD AIRBUS S.A.S. A380-841/-842/-861 AD 2020-0129 requires to introduce the None 2020-0129 11/09/2020 Active additional work described in theAirbus SB A380-36-8026 Rev2, as Rev1 (already mandated through AD2018-0100) didn’t achieve the full intent of the desired modification.The Technical Adaptations ref 80445344/014/2018, 80445344/068/2019< (>,<)> 80599250/019/2019, 8... 10074434 AMOC TO AD AIRBUS S.A.S. A321-231/-232 EASA AD 2020-0103 was issued to address a - Airbus Service Bulletin 2020-0103 30/09/2020 Active A321-131/-211/-212/-213 lack of protection againstcurrent injection of A320-25-1BQN original issue, A320-214/-231/-232/-233 28 Volts DC or 115 Volts AC ona non- dated 05 December2019.- A319-111/-112/-115/-132/-1 rechargeableELT lithium battery, by the Airbus Technical Adaptation 33 introduction of a modification in 80724343/009/2020 issue 1, A318-112/-122 accordancewith the Airbus Service Bulletins dated 20 May2020 instructions.Since the issuance of the EASA AD 2020-0103... 10075670 AMOC TO AD AIRBUS S.A.S. A321-271N/-271NX/-272N/- The EASA AD 2020-0274 has been issued to Airbus Repair and Design All manufacturer serial numbers. 2020-0274 18/02/2021 Active 272NX reduce the risk ofbatteriesover-discharged Approval Form, ref : A321-253N/-251NX/-252NX/ and to keep them in a serviceable condition 0828936/042/2021 Issue -253NX despite longaircraft parking A,dated 17 February 2021. A321-213/-231/-232/-251N/- situation.Mandatory Airbus AOT A24N006-20 252N provides operators with instructions A321-111/-112/-131/-211/-2 andrecommendations for battery 12 preservation, through Off-Wing o... A320-253N/-271N/-272N/-2 73N A320-231/-232/-233/-251N/- 252N A320-211/-212/-214/-215/-2 16 A319-131/-132/-133/-151N/- 153N A319-111/-112/-113/-114/-1 15 A318-111/-112/-121/-122 10075831 AMOC TO AD AIRBUS S.A.S. REV. 1 A310-304 EASA AD 2015-0174, covering A300-600/ Airbus Service Bulletins There is no change in the 2015-0174 16/03/2021 Active A310 aircraft, mandates correctiveactions A310-22-2067 Rev 00 dated compliance time required in the requiring the installation and activation of 27 Nov. 2020 AD 2015-0174(i.e. compliance the Stop RudderInputs Warning (SRIW).In andA310-22-2068 Rev 00 time of 48 months after particular, EASA AD 2015-0174 requires to dated27 Nov. 2020, or later respectively SBs A310- 22-2063/ install the SRIW device, inaccordance with approved revision. A310-22-2064 first issue date the instructions of2 Airbus SBs A310-22-2063 (revision 00)). and A3... 10075844 AMOC TO AD AIRBUS S.A.S. A321-251N/-253N/-271N/-2 AD 2019-0069 require the modification of the Memo E25M20002933 dated Manufacturer serial numbers as 2019-0069 12/03/2021 Active 72N attachments oftheleft-hand and right-hand May 28, 2020SB25-1BKT listed in the applicable SBs, as A321-211/-212/-213/-231/-2 overhead stowage compartments (OHSC), Revision 03 dated December definedin the AD; 32 inaccordance with the instructions of the 16, 2020SB25-1BKM Revision A320-233/-251N/-271N SB25-1BGK on A320 family CEOaircraft or 03 dated January 11, A319-133, SB25-1BGL on A320 family NEO aircraft fitted 2021SB25-1BKS Revision 03 A320-214/-216/-232 with enhancedcabin modification 35812/ dated October 05, 2020. A319-111/-112/-115/-131/-1 K17239 to... 32 A318-112/-121/-122 10075996 AMOC TO AD AIRBUS S.A.S. ALL AIRBUS Design Organisation has introduced LISTED IN TABLE 1 & 2 30/03/2021 Active on February 2021 a Repair andDesign Approval Form (RDAF) document which merges and supersedes theformer Repair Design Approval Sheet (RDAS) and Technical Adaptation (TA)documents.As RDAS and TA acronyms were used in some past EASA AirworthinessDirectives, in...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 8 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10076331 AMOC TO AD AIRBUS S.A.S. A380-861 ATA 36 – Pneumatic – Pylon / Wing Interface None The aircraft whose pylons were 2020-0286 27/04/2021 Active A380-842 Bleed Duct and Fuel Pipe –InspectionAD modified in accordance with A380-841 2020-0286 requires to inspect the pylon theinstructions detailed in RDAFs bleed duct installationwithin 50 FC / 400 FH number80885156/005/2021, (whatever occurs first) after 04 August 2020 80885156/007/2021, (effective date of EASA AD 2020-0162<(>,<)> 80885156/008/2021,80885156/00 superseded by EASA AD2020-0286), and 9/2021, 80885156/010/2021, thereaf... 80885156/011/2021,80885156/01 2/2021, 80885156/013/2021, 80894228/004/2021,80894228/00 5/2021, 80894228/006/2... 10076777 AMOC TO AD AIRBUS S.A.S. A321-271N/-271NX/-272N EASA AD 2020-0103 was issued to address a - Airbus Service Bulletin 2020-0103 29/06/2021 Active A321-251N/-251NX/-253N/- lack of protection againstcurrent injection of A320-25-1BQN original issue, 253NX 28 Volts DC or 115 Volts AC ona non- dated 05 December2019.- A320-251N/271N rechargeableELT lithium battery, by the Airbus Service Bulletin A319-153N introduction of a modification in A320-25-1BQP original issue, accordancewith the Airbus Service Bulletins dated 05 December2019.- instructions.Since the issuance of the EASA Airbus Technical Adaptation AD 2020-0103... 80832689/007/2020 issue 2, dated 29October 2020. 10077198 AMOC TO AD AIRBUS S.A.S. A319-115 The AD 2016-0212 was published on 25 Alternative Method of None AD2016-0212 08/09/2021 Active October 2016 to address thepotential risk Compliance associated to the penetration through the 300022876/60079830Airbus cabin floor ofa vertical strut at Frame (FR) 65, modification 153724 followingan airframe ground contactabove implemented in the Service certified vertical speed/vertical Bulletins: AirbusSB acceleration.To address this potential unsafe A320-53-1262 Revision 01 conditio... dated 29 July 2016. Airbus SB A320-53-1333original issue dated 29 July 2016 and/or Airbus SB A320-53-1334 originalissue dated 29 July 2016.STC 10054... 10074379 AMOC TO AD APTOZ EHF. REV. 1 737-400 This AMOC provides an acceptable level of V1 Aerospace Repair This AMOC only applies to serial 2012-23-04 29/09/2020 Active safety to replacethe actionsidentified in the Instructions R20-00774-001 numbers 24436.This AMOC isvalid AD 2012-23-04 paragraph (p) for FCBS STA Rev 03.FAA AMOC approval until 23 July 2021. 727 Bulkhead- Webs, chords and stiffeners 790-20-10058. (53-021).AD 2012-23-04 was issued to detect and correct fatigue cracking of thebody station (BS) 727 frame outboard chord, and c... 10074380 AMOC TO AD APTOZ EHF. REV. 1 737-400 This AMOC provides an acceptable level of V1 Aerospace Repair This AMOC only applies to serial 2018-01-08 29/09/2020 Active safety to replacethe actionsidentified in the Instructions R20-00774-001 numbers 24436.This AMOC isvalid AD 2018-01-08.AD 2018-01-08 requires Rev 03.FAA AMOC approval until 23 July 2021. repetitive high frequency eddy current 790-20-10058. (HFEC) anddetailed inspections to detect cracks in the auxiliary chord radius;time- limited repetitive inspections; replacement of the o... 10074381 AMOC TO AD APTOZ EHF. REV. 1 737-400 This AMOC provides an acceptable level of V1 Aerospace Repair This AMOC only applies to serial 2016-11-04 29/09/2020 Active safety to replacethe actionsidentified in the Instructions R20-00776-001, number 24436.This AMOC is valid AD 2016-11-04 paragraph (o) for FCBS Rev 02.FAA AMOC approval until 23 July 2021 Fuselage LowerLobe Frames BS 188-520 790-20-10059. (737-CLB-FCBS 53-010).AD 2016-11-04 requires inspections, modification and corrective actionsfor cracking at a wirepenetration hole.The a... 10074400 AMOC TO AD APTOZ EHF. REV. 1 737-400 This AMOC provides an acceptable level of V1 Aerospace Repair This AMOC only applies to serial 2018-19-20 29/09/2020 Active safety to replacethe actionsidentified in the Instructions R20-00778-001, number 24436.This AMOC is valid AD 2018-19-20 paragraph (m)(1)for FCBS Rev 06.FAA AMOC approval until 23 July 2021. stub beam atLH side body station (STA) 790-20-10072. 616 .AD 2018-19-20 requires inspections and corrective actions for fatiguecracking of certain fuselage frames and stub beams and pos...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 9 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074996 AMOC TO AD APTOZ EHF. 737-400 Doors, Fuselage, Nacelles/Pylons, Stabilizers, V1 Aerospace LLC Accomplish inspections of the (FAA) AD 2017-20-14 27/11/2020 Active Wings - StructuralSignificant Items - D20-00454-001 Rev 01FAA repair area in accordance with Inspections / Maintenance or Inspection AMOC approval theinstructions of and within the ProgramRevisionAD 2017-20-14 was issued 790-20-11089a thresholds and intervalsas to provide supplemental inspections that identified indocument arerequired for timely detection of fatigue D20-00454-001 Rev 01. All other cracking for certain structuralsignificant areas must be inspected items (... asmandated by FAA AD 2017-20-14.All provisions of AD 2017-20-14 that are not specifically reference... 10074997 AMOC TO AD APTOZ EHF. 737-400 AD 2016-20-02 was issued to detect and V1 Aerospace LLC Accomplish inspections of the (FAA) AD 2016-20-02 27/11/2020 Active correct fatigue cracking of theaft pressure D20-00454-001 Rev 01FAA repair area in accordance with bulkhead web at the ''Y''-chord, which could AMOC approval theinstructions of and within the result inreduced structural integrity of the 790-20-11089a thresholds and intervalsas airplane and rapid decompression ofthe identified indocument fuselage.During a C-check (25 May 2011), D20-00454-001 Rev 01. All other corrosion damage has been detected onthe areas must be inspected aft pr... asmandated by FAA AD 2016-20-02.All provisions of AD 2016-20-02 that are not specifically reference... 10074998 AMOC TO AD APTOZ EHF. 737-400 AD 2012-18-13R1 was issued to detect and V1 Aerospace LLC Accomplish inspections of the (FAA) AD 2012-18-13R1 27/11/2020 Active correct fatigue cracks in theaft pressure D20-00454-001 Rev 01FAA repair area in accordance with bulkhead, which could result in rapid AMOC approval theinstructions of and within the decompression of thefuselage.During a C- 790-20-11089a thresholds and intervalsas check (25 May 2011), corrosion damage has identified indocument been detected onthe aft pressure bulkhead D20-00454-001 Rev 01. All other (APB) web, the APB y-chord frame and the areas must be inspected APBy-chord ang... asmandated by FAA AD 2012-18-13R1.All provisions of AD 2012-18-13R1 that are not specifically refer... 10075133 AMOC TO AD APTOZ EHF. REV. 1 737-400 2016-11-04 requires inspections, - V1 Aerospace LLC Damage - All provisions of AD 2016-11-04 AD 2016-11-04& AD 16/12/2020 Active modification and corrective actions Tolerance analysis and AD 2017-2014 that 2017-20-14 forcracking at a wire penetration hole. AD D20-00776-001 Rev 00, arenotspecifically referenced 2017-20-14 requires timelydetection of 12August 2020- FAA AMOC above remain fully applicable and fatigue cracking for certainstructural approval letter 790-20-12458, must becomplied with significant items.During a scheduled dated 22 September 2020 accordingly.- This approval is accomplishment of Boeing Alert Service applicable to -400 Bulletin (SB)737-53A1279, Rev 02,... aircraft, SN 24436. 10075541 AMOC TO AD APTOZ EHF. 737-400 Fuselage - Frame Outboard Chord / Auxiliary V1 Aerospace LLC Accomplish the actions identified (FAA) 2018-01-08 01/02/2021 Active Chord - InspectionAD 2018-01-08 requires D20-00774-001 Rev 00FAA in, and within the threshold performing HFEC inspection of the radius of AMOC approval 790-20-15085 asspecified in, section 5.0 – theoutboard chord and the auxiliary chord at Instructions for STA 727, S-18A in accordancewith Boeing SB ContinuedAirworthiness –of 737-53A1166.During inspection per Service document D20-00774-001 Rev Bulletin SB 737-53A1166 (Group 7 airplane... 00.All provisions of AD 2018-01-08 that are not specifically referencedabove remain fully applicable and must be complied with accordin... 10075542 AMOC TO AD APTOZ EHF. 737-400 Fuselage - Frame Body Station (BS) 727 and V1 Aerospace LLC Accomplish the actions identified (FAA) 2012‐23‐04 01/02/2021 Active Stringer 18A Outboard Chords- Inspection / D20-00774-001 Rev 00FAA in, and within the threshold RepairAD 2012‐23‐04 was issued todetect AMOC approval 790-20-15085 asspecified in, section 5.0 – and correct fatigue cracking of thebody Instructions for station (BS)727frame outboard chord, and ContinuedAirworthiness –of cracks in the radius of the auxiliary document D20-00774-001 Rev chord,which could result inreduced structural 00.All provisions of AD 2012-23-04 integri... that are not specifically referencedabove remain fully applicable and must be complied with accordin...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 10 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10075734 AMOC TO AD APTOZ EHF. 737-400 AD 2015-21-06 requires inspection of the · KF Aerospace All provisions of FAA AD (FAA) 2015-21-06 & 26/02/2021 Active lower skin at the lower row offasteners in the R24751.1-053-016-001, Rev 2015-21-06 and AD 2017-22-04 2017-22-04 lap joints of the fuselage, repair of any NC, dated 9 Oct 2020· KF that are notspecifically referenced crackingfound, and modification of the Aerospace above remain fully applicableand fuselage lap joints at certain locationsin R24751.1-053-017-001, Rev must becomplied with accordance with the Boeing Alert Service NC, dated 9 Oct 2020· V1 accordingly.Only applicable to Bulletin (SB) 737-53A1177,Revision 7.AD Aerospace D20-00850-001, Boeing 737-400 aeroplanes 2017-22... Rev. 01, dated 12 Dec modified per EASA STC10015732. 2020·V1 Aerospace D20-00851-001, Rev. 01, dated 12 Dec 2020· V1 Aerospace S20-00850-001, Rev. 00, dated 21 Oct 2020· V1 Aeros... 10077130 AMOC TO AD APTOZ EHF. 737-400 Forward Entry Doorway and Airstairs Cutout - -KF Aerospace All provisions of FAA AD (FAA) 2015-06-07 24/08/2021 Active InspectionAD 2015-06-07 was issued to R24573.1-053-008-001, Rev 2015-06-07 that are not detect and correct cracks in the lowercorners NC, dated 19 Jan 2021-V1 specifically referencedabove of the forward entry door skin cutout and the Aerospace D21-00972-001, remain fully applicable and must upper corners ofthe airstairs cutout, which Rev 00, dated 26 Apr 2021-V1 be complied with accordingly.Only could progress and result in an inability Aerospace S21-00972-001, applicable to Boeing 737-400 tomaintain cabin pressurization. Inspec... Rev 00, dated 29 Mar 2021- aeroplanes modified per EASA Boeing Special Attention SB STC10015732. 737-53-1083 Rev 5, dated 22 Jul 2014-FAA AMOC Approval Letter 790-21-7458, dated 26 May 2021 10077132 AMOC TO AD APTOZ EHF. 737-400 Fuselage - Skin Panels - InspectionAD -KF Aerospace All provisions of FAA AD (FAA) 2017-22-04 24/08/2021 Active 2017-22-04 was issuedto detect and correct R24573.1-053-008-001, Rev 2017-22-04 that are not disbonded skin panels,which could result in NC, dated 19 Jan 2021-V1 specifically referencedabove fuselage skin cracking, rapid decompression, Aerospace D21-00972-001, remain fully applicable and must andloss of structural integrity of the airplane. Rev 00, dated 26 Apr 2021- be complied with accordingly.Only Inspection to detect andcorrect disbonded Boeing Alert SB 737-53A1349 applicable to Boeing 737-400 skin panels are in accordance with Boe... Rev IR, dated 23 Aug 2016- aeroplanes modified per EASA Boeing Special Attention SB STC10015732. 737-53-1083 Rev 5, dated 22 Jul 2014-FAA AMOC Approval Letter 790-21-7458, dated 26 May 2021 10077133 AMOC TO AD APTOZ EHF. 737-400 Doors, Fuselage, Nacelles/Pylons, Stabilizers, -KF Aerospace All provisions of FAA AD (FAA) 2017-20-14 24/08/2021 Active Wings - StructuralSignificant Items - R24573.1-053-008-001, Rev 2017-20-14 that are not Inspections / Maintenance or Inspection NC, dated 19 Jan 2021-V1 specifically referencedabove ProgramRevisionAD 2017-20-14 mandates Aerospace D21-00972-001, remain fully applicable and must that supplemental inspections are required Rev 00, dated 26 Apr 2021- be complied with accordingly.Only fortimely detection of fatigue cracking for Boeing Supplemental applicable to Boeing 737-400 certain structural significantitems (SSIs) in Structural Inspection aeroplanes modified per EASA acco... Document (SSID), STC10015732. Models737-300/400/500 Airplanes, Report D6-82669, Rev Oct 2015-Boeing Special Attention SB 737-53-1083 Rev 5, dated 22 Jul 20... 10074059 AMOC TO AD ASL 737-300/-400/-700/-800 Lights – Tail Strobe Light Housing – FAA AMOC approval This AMOC only applies to the US 2014-13-07 18/08/2020 Active FRANCE S.A. InstallationThis AMOC provides an extension 783-20-410.Boeing non- following serial numbers: 25124, to the compliance time to paragraphs(f), (g), technical objectionin message 28898,29336, 24709, 25063, (h) and (i) of the AD 2014-13-07 until 15th of number EUE- 25595, 29080, 29081, 32414, March2021.AD 2014-13-07 requires to install EUE-20-0058-03B. 32418, 32427, 30882 and30883.All a new tail strobe light and newdisconnect provisions of AD 2014-13-07 that bracket, and changing wire bundles. Thi... are not specifically referencedabove remain fully applicable and must be complied with accordingly.

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 11 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10072504 AMOC TO AD ATR AVIONS DE ATR 72-212A ATA 32 – Landing Gear – Main Landing Gear ATR Airworthiness Operator No flight hours accumulated with 2019-0236 12/02/2020 Active TRANSPORT ATR 72-211, ATR 72-212 Bush – InspectionSeveral cases of Main Message (AOM) 2019/12 the bush P/N D61002 installed in REGIONALG.I.E ATR 72-201, ATR 72-202 Landing Gear (MLG) bush Part Number (P/N) Issue 2 orlater wrongposition.Conformity ATR 72-101, ATR 72-102 D61002inversion have been reported from restored per the advanced copy of in-service aircraft. Such inversioncould had the JIC 321100 RAI 10000provided been done during any MLG RAI (Removal And in attachment of the AOM Installation) and,if not detected, could result 2019/12 issue 02 or later in... 10076311 AMOC TO AD ATR AVIONS DE ATR 72-211/-212/-212A ATA 53 – Fuselage – Passenger Seat Tracks – Technical note ES-384/21 Serial Number(s):ATR 42-300, ATR 2020-0097R1 27/04/2021 Active TRANSPORT ATR 72-101/-102/-201/-202 Inspection /Repair /ReplacementSee Annex 1 Issue 02 dated 17 March 2021 42-320, ATR 42-400 and ATR42500 REGIONALG.I.E ATR 42-300/-320/-400/-500 for Definition and Content. aeroplanes, allmanufacturer serial numbers (MSN), except MSN 001 to 362 inclusive;andATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212and ATR 72-212A aeroplanes, all MSNAircraft equipped with Geven Classic, Presti... 10073988 AMOC TO AD AVIATION PARTNERS 757-200/-200PF/-300 Time Limits / Maintenance Checks - - APB document This approval is applicable to all US-2020-01-18 10/08/2020 Active BOEINGWINGLETS Airworthiness LimitationsInstructions - AP57.2-0604.2 (March 2020), Boeing model COMPANY, LLC Principal Structural Elements - Inspections / “Supplement to D622N001 757-200/300airplanesthat have Maintenanceor Inspection Program 757MPD for -200 STC ST01518SE / EASA STC RevisionAMOC to AD US-2020‐01‐18 for with winglets”- APB 10015659 winglets installed. airplanes with FAA STC ST01518SE / EASA document AP57.3-0604.2 STC10015659 installed.AD 2020-01-18 (March 2020), “Supplement requires that structural inspecti... to D622N001 757MPD for Boeing 757-300 with winglets” 10073165 AMOC TO AD BABCOCK MISSION CL-215-1A10 AMOC APPROVAL FOR REO 215-57-V006 REV TCCA AMOC No. AARDG EASA endorses the TCCA AMOC CF-2019-07 30/04/2020 Active CRITICAL C AND REO 215-57-V007REV DAMOC 2020/A34, submitted by letter No. AARDG 2020/A34, submitted SERVICESESPANA approval request to comply with inspections RDIMS 16463461 by letterRDIMS 16463461, issued SAU included on TCCA ADCF-2019-07, corrective for serial numbers 1034 (EC-HET) actions,part C, accomplished according and 1038(EC-HEU):Viking Air Ltd. inspections included on REO 215-57-V006rev (Viking) requested (Ref. 1) to Cand REO 215-57-v007 rev D. Inspection Transport Canada CivilAviation instructions receivedV... (TCCA) for an AMOC-equivalent letter documenting ourconcurrence with the use of th... 10072886 AMOC TO AD BLUEBIRD LTD 737-300, 737-400 Background:EASA AD 2011-24-12 requires SSID R-816, Revision S, dated AMOC agreement should cover 2011-24-12 26/03/2020 Active inspections as identified in the Boeing 11.09.2018 or later approved only the modified area<(>,<)> thus SB737-53A1301 to detect cracks on the steps revision. the ADstill applies to the of chemically milled fuselageskin, which has unmodified areas.Serial been modified by the STC EASA.IM.A.S.01754 Numbers:TF-BBJ MSN 24436, TF- (FAAST01827LA). As a result of the BBK MSN 26302, TF-BBL MSN mentioned STC the area to be inspectedhas 28887 and TF-BBM MSN25376 been modifie... 10073659 AMOC TO AD BLUE PANORAMA 737-800 B737-800 aircraft 785-20-8185: Change of 1. All provisions of AD 2016-04-06 US 2016-04-06 30/06/2020 Active AIRLINES S.p.A. MSN 30007, 30289 and 30567 aregranted an Compliance Time (CCT) that are not specifically extension of the FAA AD 2016-04-06 par. (g) Alternative Method referencedabove remain fully and (h)compliance time up to 31 December ofCompliance (AMOC) to applicable and must be complied 2020, instead of the originalcompliance date Federal Aviation with accordingly.2. This approval is 30 June 2020. Administration (FAA) applicable only to Boeing Model AirworthinessDirective (AD) 737-800 seriesaircraft, MSN 2016-04-06 letter, dated June 30007, 30289, and 30567.3. This 22, 2020,,Issue No. 1BPA- AMOC is not transferable with the BPA-20-0051-06B: FAA AD aircraft to ano... 2016-04-06 Compliance Time Extension. Emailfrom The Boeing Company t...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 12 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10072682 AMOC TO AD DASSAULT AVIATION REV. 1 MYSTÈRE FALCON 20 Engine - First Stage Low Pressure Turbine None If fitted with Honeywell (formerly 2009-0175 REV. 1 06/03/2020 Active (LPT1) Blades / Allied-Signal, Garrett AirResearch) VibrationMonitoringInstallation of new LPT1 TFE731-5AR-2C or TFE731-5BR-2C and LPT2 rotor assembly blade retainers turbofan engines. inaccordance with the accomplishment instructions of Honeywell ServiceBulletin TFE731-72-3737 rev. 2, dated 17th June 2019, constitutesterminating action forA... 10075518 AMOC TO AD DASSAULT AVIATION FALCON 7X The temporary AFM modification introduced DGT105608 AFM-CP0173-PUB Applicable to all serial numbers, 2021-0036-E 28/01/2021 Active by AFM-CP0173-PUBrequiresflight crews to for Falcon 7X including those that perform a repetitive check of flight deck aeroplanesDGT147681 AFM- haveembodiedM1000. oxygen masksbefore the first take-off of the CP0173-PUB for Falcon 8X day allowing for postponing thecompletion of aeroplanes. the actions required byEASA AD 2021-0036-E, sect.“Required Action(s) and Compliance... 10074582 AMOC TO AD E A D AEROSPACE REV. 1 A318/A319/A320/A321 AD 2020-0103 identifies an unsafe condition - EAD Aerospace Service Applicable MSNs are identified in 2020-0103 20/05/2021 Active AIRWORTHINESS in relation with Emergencylocator Bulletin ref. 01604-IST-A-SRB, the EAD Aerospace Transmitter (ELT) Part Number (P/N) rev C.- Modification Approval ServiceBulletinref. 01604-IST-A- 01N65900 installed on someAirbus Single- Sheet ref. 01604-EAS-A- SRB. Aisle aircraft. The AD mandates removing the MAS-01, RevB. unsafecondition through the addition of a protective diode in theinstallation.EAD Aerospace aircrafts... 10075128 AMOC TO AD E A D AEROSPACE A330/A340 IDENTIFIED IN AD 2020-0083 identifies an unsafe condition - EAD Aerospace Service Only applicable to aircraft MSNs 2020-0083 10/12/2020 Active AIRWORTHINESS THE AD in relation with Emergencylocator Bulletin ref. 01604-IST-A-SRB, identified in EAD Aerospace Transmitter (ELT)Part Number (P/N) rev A.- Modification Approval ServiceBulletin ref. 01604-IST-A- 01N65900 or 01N65902 installed on some Sheet ref. 01604-EAS-A- SRB, rev A. Airbusproducts. The AD mandates removing MAS-01, RevB. the unsafe condition through theaddition of a protective diode in the installation.The AD requirement appli... 10072178 AMOC TO AD EASYJET REV. 1 A319-111, A320-214 This AD mandates Airbus SB A320-71-1068 Airbus A320 IPC This AMOC applicability is limited 2016-0257 05/02/2021 Active COMPANY LIMITED A319-111 / A320-214 introducing lockable fan cowllatches on 25-13-01-29MDesign Change to aeroplanes on which either CFM56 engines fitted to Document EZE-1470M Issue Airbusmodification 157519 has aeroplanes andincludes stowing the keys of 03(The use of later approved been embodied in production or the fan cowl latches in the box at thebottom revisions of this document is Airbus SBA320-71-1068 has been of the coat stowage, as applicable to acceptable.) embodied in service<(>,<)> and aeroplane configuration.easyJet had initially which are in“config 004” (A320) or stowe... “config 006” (A319), as defined through this SB.This AMOC is limited to Seria... 10073569 AMOC TO AD EIRTECH AVIATION REV. 1 737-900/-900ER Equipment / Furnishings - Passenger Service MAC/1368 - Approval None US-2019-03-26 23/06/2020 Active SERVICES LIMITED 737-600/-700/-700C/-800 Units and Life Vest Panels -ModificationThis Certificate: Lanyard AMOC to US AD 2019-03-26 (1). is based on Replacement - Passenger an existing Minor Change(2) issued by Eirtech ServiceUnit and Life Vest Aviation Services (under their EASA Panel - 737 - Issue 1MDL/ privileges)for installation of PSU and Life Vest 1368-001 - Master Document Panel Lanyard Assemblies on 737-600, -... List: Lanyard Replacement - PassengerService Unit and Life Vest Panel - 737 - Issue 1AMS/1368-001 - Aircraft Manual Supplement: 737 Lanyard Replacement –Pass... 10072651 AMOC TO AD ELBE A330-323/-341/-342/-343 The AD and the associated Service Bulletins 398/AMOC/032 Rev. B : The AMOC is proposed to be 2018-0276R1 05/03/2020 Active FLUGZEUGWERKE A330-301/-302/-303/-321/-3 are partially not applicableto A330-300 and “Alternative Methods of applicable to A330-300 and GmbH 22 A330-200 airplanes which have undergone Compliance forAirworthiness A330-200 airplaneswhich have A330-201/-202/-203/-223/-2 the passenger tofreighter (P2F) conversion Directive (AD) 2018-0276R1” , undergone the passenger to 43 prescribed by the EASA STC Project dated 20 Dec. 2019. freighterconversion prescribed Number0010042837 (for A330–300 P2F) and bythe EASA STC Project Number EASA STC Project Number 0010048879(for 0010042837 (for A330–300 P2F) A330–200 P2F as... and EASA STCProject Number 0010048879(for A330–200 P2F).

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 13 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10072652 AMOC TO AD ELBE A330-323/-341/-342/-343 AD 2019-0059 mandates compliance with the 398/AMOC/038 Rev. B: The AMOC is proposed to be 2019-0059 30/03/2020 Active FLUGZEUGWERKE A330-301/-302/-303/-321/-3 instructions contained inAirbus A330 “Alternative Methods of applicable to A330-300 and GmbH 22 Airworthiness Limitations Section (ALS) Part 2 Compliance forAirworthiness A330-200 airplaneswhich have A330-201/-202/-203/-223/-2 Revision 03.EFW proposes that for A330-300 Directive (AD) undergone the passenger to 43 and A330-200 passenger 2019-0059”A330P2F/ALS Part freighterconversion prescribed aeroplanesconverted to freighter 2 Supplement Rev 06. bythe EASA STC 10063798.On top configuration as per STC 0010063798, of thesupplementary maintenance theimplementation of ALS Part 2 Supple... tasks specified in A330P2F/ALSPart 2 supplement Rev 06, the maintenance tasks specified in Air... 10073521 AMOC TO AD ELBE A330-323/-341/-342/-343 The EASA AD 2019-0047 requires to comply EASA STC The AMOC is only valid for the 2019-0047 24/06/2020 Active FLUGZEUGWERKE A330-301/-302/-303/-321/-3 with the ALS Part 4‘System 10063798.A330_ALS_Part4_S Airbus A330-200 and GmbH 22 Equipment Maintenance Requirements EMR_R07A330P2F_ALS_Part4 A330-300airplanemodels modified A330-201/-202/-203/-223/-2 (SEMR)’ at Revision 07.ST Engineering -SEMR-ENV SEMR in accordance with EASA STC 43 Aerospace Pax to Freighter(P2F) conversion Supplement ENV 10063798.Supersedure of the STC (EASAapproval 10063798), applicable R00_Apr_01_20A330P2F/ EASA AD 2019-0047, or the update tothe Airbus A330-200 /-300 aircraftmodels, ALS_Part4-SEMR-ENV at of Airbus A330 ALSPart 4 Revision includes through i... R00398/AED/ICA at Rev.E 07 as well as the update of the ST Aerospace STC ALSPart 4 Supplement may invalidate this AMO... 10073995 AMOC TO AD ELBE A321-211/-231 Fuselage – Frame 35.2A - InspectionThe EASA EASA STC 10071994Airbus SB The AMOC is only valid for the 2016-0106R1 04/08/2021 Active FLUGZEUGWERKE AD 2016-0106R1 requires repetitive special A320-53-1355 (including roto -200 aircraft models GmbH detailed (rototest)inspections (SDI) of the probe inspection, cold modifiedto A321P2F in accordance affected holes and, depending on workingand fastener with EASA STC 10071994. findings,accomplishment of a repair.With the installation)349/AMOC/007 Elbe Flugzzeugwerke GmbH (EFW)Pax to Rev. B Alternative Method of Freighter (P2F)conversion STC (EASA Compliance for approval 10071994... AirworthinessDirectives EASA AD 2016-0106R1 and FAA AD 2017-10-23 10073996 AMOC TO AD ELBE A321-211/-231 Fuselage – Central Vertical Strut at Frame 65 EASA STC 10071994349/AED/ The AMOC is only valid for the AD 2016-0212 04/08/2021 Active FLUGZEUGWERKE – ModificationThe EASA AD 2016-0212 STR039 Static Substantiation Airbus A321-200 airplane models GmbH requires a modification of the Central of Vertical Struts for 14P349/ modifiedin accordance with EASA VerticalStrut at Frame 65 in order it cannot AED/008 Document Master STC 10071994. penetrate through the cabin flooras a List for A321P2FAirbus SB consequence of an airframe ground contact A320-53-1262 or SB above certified verticalspeed/vertical A320-53-1334349/AMOC/012 acceleration.To... Rev. B Alternative Method of Compliance for AirworthinessDirectives EASA AD 2016-0212 and FAA AD 2017-25-06 10074009 AMOC TO AD ELBE A321-211/-231 Fuselage – Crossbeam Splicing at Frames 16 EASA STC 10071994AIRBUS SB The AMOC is only valid for the 2016-0139 04/08/2021 Active FLUGZEUGWERKE and 20 – InspectionThe EASA AD 2016-0139 A320-53-1286 Fuselage – Airbus A321-200 aircraft models GmbH repetitive special detailed inspections (SDI) Nose Forward Fuselage – modifiedto A321P2F in accordance ofthe two upper rows of fasteners of the Inspection atCrossbeam with EASA STC 10071994. crossbeam splicing at FR16 andFR20, on both Splicing FR16/20 LHS/ LH and RH sides, and, depending on RHSAIRBUS SB A320-53-1295 aeroplaneconfiguration, provides an optional Fuselage – Main Structure – termi... Introduce Bolt withCold Working and Moderate Interference on Crossbeam Splicing FR 16 andFR20349/ AED/STR050C Fatigue and Damage...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 14 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074010 AMOC TO AD ELBE A321-231 ATA 53 – Fuselage – Frame 35 / Slidebox EASA STC 10071994AIRBUS SB The AMOC is only valid for the 2016-0146R1 18/08/2020 Active FLUGZEUGWERKE Junction - InspectionThe EASA AD A320-53-1308 – Fuselage – Airbus A321-231 airplane models GmbH 2016-0146R1 mandates the accomplishment Forward Fuselage – Holes modifiedin accordance with EASA of an SDI at thelocations of FR 35 as specified InspectionFrames 35.1 LHS STC 10071994. in Table 2 of AD 2016-0146R1 and Under SlideboxAIRBUS SB inaccordance with the instructions of the A320-53-1309 – Fuselage – applicable Airbus SB as definedin Table 2 AD Forward Fuselage – Holes 2016-0146R1within t... InspectionFrames 35.1 RHS Under SlideboxAIRBUS SB A320-53-1310 – Fuselage – Forward Fuselage – Holes InspectionFrames 35.... 10074122 AMOC TO AD ELBE REV. 2 A321-211, A321-231 The EASA AD 2018-0233R1 mandates the EASA STC 10071994Airbus SB The AMOC is only valid for the 2018-0233R1 07/07/2021 Active FLUGZEUGWERKE accomplishment of the repetitiveinspections, A320-53-1257 Fuselage – Airbus A321-211, A321-231 GmbH via rototest, of open tack holes and rivet Inspection of Tack Holes at FR airplane modelsmodified in holes at thecargo floor support fittings 50 – FR63 between P33 – P 39 accordance with EASA STC between FR 50and FR 63, between Stringer (LH Only) in Cargo Floor 10071994. (STGR) 33 and STGR 39 (LH side only), in AreaAirbus SB A320-53-1261 accordance with theinstructions of the Fuselage – Rear Fuselage – inspection SB... Reinforce Frames inArea of P31 – P39 LHS Section 17Airbus SB A320-53-1360 Fuselage – Rear Fuselage – Reinforce... 10074583 AMOC TO AD ELBE A321-211, A321-231 EASA AD 2020-0036R1 mandates to apply EASA STC 10071994AIRBUS The AMOC is only valid for the 2020-0036R1 09/03/2021 Active FLUGZEUGWERKE Airbus ALS Part 2 Revision 08, andto update A318/A319/A320/A321 Airbus A321-211, A321-231 GmbH the operator Airworthiness Limitations airplane modelsmodified in Programme (AMP) within 12months, from Section (ALS) Part2 Revision accordance with EASA STC the effective date of theoriginal issue of this 07, dated 13 Jun 2018AIRBUS 10071994. AD [i.e.21 March 2020].As part of their A318/A319/A320/A321 passenger to freighter (P2F) conversion STC, Airworthiness Limitations referencedEA... Section (ALS) Part2 Revision 08, dated 11 Oct 2019EFW Airworthiness Limitation Section ALS Part 2 Airworthiness LimitationItems... 10074812 AMOC TO AD ELBE A321-231 In the frame of the A321 Passenger to - EASA STC 10071994- Airbus The AMOC is only valid for the 2020-0067 11/11/2020 Active FLUGZEUGWERKE A321-211 Freighter conversion (A321P2F),the A318/A319/A320/A321 ALS Airbus A321-211, A321-231 GmbH Passenger Cabin was replaced by a Main Part 3 Revision 7 dated 31 Jul airplane modelsmodified in Deck Cargo Compartment.Consequently the 2020.“/A319/ accordance with EASA STC passenger oxygen system wasdeleted and A320/A321 Airworthiness 10071994. the smokedetection system was replaced by Limitations Section (ALS) a newdedicated one.The AD mandates the Part3 – Certification accomplishment of all main... Maintenance Requirement (CMR)”- A320/A321 P2F ALS Part 3 Supplement Envelope (ENV) Revision 00 dated01 Aug 2019. “A320/A32... 10074978 AMOC TO AD ELBE A330-341/-342/-343 The EASA AD 97-154-049R1 was issued to EASA STC 10063798.SB The AMOC is only valid for the 97-154-049(B) 26/11/2020 Active FLUGZEUGWERKE A330-321/-322/-323 protect against presence ofmoisture inside A330-21-3053 R01SB Airbus A330-200 and GmbH A330-301/-302/-303 the rear electrical connectors for THOMSON A330-92-3017 R04SB A330-300airplanemodels modified A330-201/-202/-203/-223/-2 radioaltimeter transceivers which can cause A330-34-3044 R01Airbus in accordance with EASA STC 43 incorrect fluctuations of theradio height and MOD-44457Airbus 10063798, and are embodiedwith therefore reduce the reliability of these MOD-45022 Service Bulletin A330-21-3053, radioaltimeters.Mandatory embodiment of A330-92-3017 and A330-34-3044, the... andwhich are not embodied with Airbus Modifications 44457 and 45022.Supersedure of the EASA AD...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 15 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074281 AMOC TO AD EPI EUROPROP TP400-D6 Para (5) on page 3 of the referenced AD Rolls-Royce Technical Report None EASA_AD_2019_0161-01 16/09/2020 Active INTERNATIONAL mandates that, from30 September2020, EDNS01000901392 issue 02. GmbH installation of an engine on an aeroplaneis allowed, provided theengine is a Group 2 engine, or has been modified in accordance with theinstructions of the related ASB. This AMOC revises the compliance timeof 31 March 202... 10075459 AMOC TO AD HELI-HOLLAND AIR EC 175 B ATA 53 - Fuselage- Lower Fuselage Fuel Tank AH NTO no. ETJ 21-06029, None 2020-0004 25/01/2021 Active SERVICE BV Structure and EquipmentElectrical dated 22.01.2021 Connectors - Rework/ RelocationAs Alternative Method of Compliance (AMOC) to the requirements of AD2020-0004, Paragraph (1):Before exceeding 880 flight hours or within 18 months after theeffective date of this AD, whicheve... 10072276 AMOC TO AD ISRAEL AEROSPACE REV. 1 747-400 Nose Wheel Well sidewall panel web Model: 747-400; Serial No.: 27898 Israel Aerospace Industries Boeing Model 747-400 with Serial US 2016-06-07 13/08/2020 Active INDUSTRIES, LTD.IAI (2016-06-07 The Boeing Company: crack repair, stress and Number (S/N) 27898. Amendment 39-18438; Docket DamageToleranceAnalysis No.FAA-2014-0774; Directorate Identifier (DTA) document 2013-NM-154-AD)Israel Aerospace Industries CS-27898-010 Rev "A" has requested an AMOC to Nose Wheel Well datedApril 23, 2019 (NWW) initial and repeat inspections mandated by Airworthiness Directive(AD) 2016-0... 10073466 AMOC TO AD ISRAEL AEROSPACE 747-400 Escape Slides Latch ReplacementIsrael Boeing Model 747-400 converted 2013-19-13 10/06/2020 Active INDUSTRIES, LTD.IAI Aerospace Industries (IAI) has requested an to IAI special freighter perEASA AMOC to theinspections and rework of the STC10014423 (modified from PAX) latches in the main deck escape/sliderafts or per EASA STC 10015911 and the escape slides installed on the (modified fromCombi). airplane doors mandated byAirworthiness Directive (AD) 2013-19-13 affecting Boeing model 747-40... 10073467 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has 747-400 - Aircraft modified to special Boeing Model 747-400 converted EASA ADOPTED FAA AD 10/06/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theinspections for freighter per EASA STC 10014423 to IAI special freighter perEASA 2018-16-06 BMS 8-39 flexible urethane foam insulation in (modified from PAX) or per EASA STC STC10014423 (modified from PAX) the floorpanel assemblies and the power 10015911 (modified from Combi). or per EASA STC 10015911 drive unit (PDU) cover assembliesmandated (modified fromCombi). by Airworthiness Directive (AD) 2018-16-06 affecting Boeingmodel 747-400 series airplane conve... 10073474 AMOC TO AD ISRAEL AEROSPACE 747-400 Flight deck security door improvementIsrael Boeing Model 747-400 converted 2009-19-06 12/06/2020 Active INDUSTRIES, LTD.IAI Aerospace Industries (IAI) has requested an to IAI special freighter perEASA AMOC to the flightdeck door modifications STC10014423 (modified from PAX) mandated by Airworthiness Directive (AD) or per EASA STC 10015911 2019-09-06 affecting Boeing model 747-400 (modified fromCombi).Limited to series airplane converted toIAI special the all cargo configuration only. freighter.IAI freighter conversion in Any passenger accordance... configurationremains subject to actions required by AD 2009-19-06 10073475 AMOC TO AD ISRAEL AEROSPACE 747-400 Hot short protector (HSP) for the fuel Boeing Model 747-400 converted AD 2010-20-12 12/06/2020 Active INDUSTRIES, LTD.IAI quantity indicating system (FQIS)Israel to IAI special freighter perEASA Aerospace Industries (IAI) has requestedan STC10014423 (modified from PAX) AMOC to theinstallation of a hot short or per EASA STC 10015911 protector (HSP) for the fuel (modified fromCombi). quantityindicating system (FQIS) of the center fuel tank and, for certainairplanes, the horizontal stabilizer... 10073489 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has IAI removal instructions Boeing Model 747-400 converted EASA ADOPTED FAA AD 15/06/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theEnvironmental Report 366-21-00-A2407 issue to IAI special freighter perEASA 2010-14-01 Control System (ECS) duct assembly rework New dated 22 Nov2005IAI STC10014423 (modified from PAX) or replacementinstructions mandated by removal instructions Report or per EASA STC 10015911 Airworthiness Directive (AD) 366-21-00-A0076 Issue B (modified fromCombi). 2010-14-01affecting Boeing model 747-400 dated 17 July2007. series airplane converted to IAI specialfreighter.During the IAI speciali...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 16 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10073492 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted EASA ADOPTED FAA AD 15/06/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to themeasurement of to IAI special freighter perEASA 2011-06-03 the electrical bond resistance between STC10014423 (modified from PAX) themotor operatedvalve (MOV) actuators or per EASA STC 10015911 and airplane structure for the (modified fromCombi). horizontalstabilizer fuel tank (HST) and applicable corrective actions mandated byparagraph (h) of AirworthinessB... 10073497 AMOC TO AD ISRAEL AEROSPACE 747-400 Wing Side of Body Joint, Horizontal Stabilizer Israel Aerospace Industries, Boeing Model 747-400 converted 2010-05-03 16/06/2020 Active INDUSTRIES, LTD.IAI Side of BodyJoint, andFuselage Inspection of 747-400 SF to IAI special freighter perEASA Circumferential Splice InspectionIsrael FuselageCircumferential STC10014423 (modified from PAX) Aerospace Industries (IAI) has requested an Splices at IAI Straps, or per EASA STC 10015911 AMOC to wing andhorizontal stabiliser side- document 366-53-00-A5493 (modified fromCombi). of-body joints and fuselage datedJune 23, 2014. circumferentialsplice initial and repeat inspections mandated by p... 10073513 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has - IAI Service Bulletin Boeing Model 747-400 converted EASA ADOPTED FAA AD 16/06/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theinstructions 366-11-143 Rev 2 dated Nov. to IAI special freighter perEASA 2015-11-05 mandated by paragraph (g) and paragraph 2015 forAFT STC10014423 (modified from PAX) (h)(1) ofAirworthiness Directive (AD) CargoCompartment Heating or per EASA STC 10015911 2015-11-05 affecting Boeing model System Marker and Tape (modified fromCombi). 747-400series airplane converted to IAI Installation.- IAI Service special freighter.Paragraph (g) of AD Bulletin 366-21-152 Rev 1 2015-11-05 requires removal of the... dated Jan. 2019 for AFT CargoCompartment Heating System ZTS Installation. 10073528 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Israel Aerospace Industries Boeing Model 747-400 converted EASA ADOPTED FAA 18/06/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theinspection for 747-400SF report – to IAI special freighter perEASA 2013-19-15 cracks at the main entry door 5 fuselage SupplementalStructuralInspec STC10014423 (modified from PAX) cutout at theupper aft corner as mandated tion Document TR 366-00-00- by Airworthiness Directive (AD) A0316 Issue N dated March 2013-19-15affecting Boeing model 747-400 2020. seriesairplane converted to IAI specialfreighter.AD 2013-19-15 req... 10073536 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Aircraft converted to special EASA ADOPTED FAA AD 18/06/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to fuselageinitial and freighter by EASA STC 10014423 2010-01-01 repeat inspections mandated by (modifiedfrom PAX) or per EASA Airworthiness Directive (AD)2010-01-01 STC 10015911 (modified affecting Boeing model 747-400series fromCombi). airplane converted toIAI special freighter.AD 2010-01-01 requires repetitive inspections for cracking of certainf... 10073832 AMOC TO AD ISRAEL AEROSPACE 737-300/-400 US-2014-25-09: Fuselage - Forward Airstair 737-300 freighter conversion The AMOC is only valid for the 2014-25-09 / 2015-06-07 20/07/2020 Active INDUSTRIES, LTD.IAI Stowage Doorway Skin Assemblyand Bear STC ST01566LA.737-400 Boeing 737-300 and 737-400 Strap – InspectionUS-2015-06-07: Forward freighter conversion STC airplanemodels modified in Entry Doorway and Airstairs Cutout - ST01961SE.IAI SB 365-53-045 accordance with EASA STC InspectionThe EASA AD 2015-06-07, Revision 2, dated June 10016227 Rev. 5 or per EASASTC applicable to 737-100, 737-200, 737-200C, 2020.IAI Report 365-53-00- 10015542 Rev.5.Supersedure of 737-300, 737-400, and 737-500 series B9658 Revision A dated the EASAAD 2014-25-09 and airplanes, requires inspectio... January 23, 2019 - 2015-06-07, may invalidatethis Implementation of Boeing SB AMOC. 737-53-1058 and 737-53-1083 on 737-300 SFand 737-400 SF. 10073835 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 The EASA AD US-2008-17-13, applicable to 737-300 freighter conversion The AMOC is only valid for the AD US 2008-17-13 20/07/2020 Active INDUSTRIES, LTD.IAI 737-100, 737-200, 737-200C,737-300, STC ST01566LA.737-400 Boeing 737-300 and 737-400 737-400, and 737-500 series airplanes, freighter conversion STC airplanemodels modified in requires replacing theexisting straight-to-90- ST01961SE.IAI SB 365-38-032, accordance with EASA STC degree hose assembly for the Lavatory Revision 0, dated November 10016227 Rev. 5 or per EASASTC ''A''water supply with a new straight hose 2011. 10015542 Rev.5.Supersedure of assembly and a separate 90-degreeelbow the EASAEASA AD US-2008-17-13, fitting, in orderc... may invalidate this AMOC.

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 17 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10073836 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Fuselage - Seat Track Link Assembly - 737-300 freighter conversion The AMOC is only valid for the US 2015-02-26 20/07/2020 Active INDUSTRIES, LTD.IAI Modification / Repair/ReplacementThe EASA STC ST01566LA.737-400 Boeing 737-300 and 737-400 AD US-2015-02-26, superseding AD freighter conversion STC airplanemodels modified in 2013-24-13, applicable to737-100, 737-200, ST01961SE. accordance with EASA STC 737-200C, 737-300, 737-400, and 737-500 10016227 Rev. 5 or per EASASTC seriesairplanes, requires replacing the pivot 10015542 Rev. 5.Supersedure of link assembly, replacing theseat track link the EASA AD US-2015-02-26, may assemblies or... invalidate this AMOC. 10073856 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Fuselage - Fuselage - Forward Entry Door Skin 737-300 freighter conversion The AMOC is only valid for the US-2013-18-08 22/07/2020 Active INDUSTRIES, LTD.IAI Cutout - InspectionThe EASA AD STC ST01566LA.737-400 Boeing 737-300 and 737-400 US-2013-18-08, applicable to 737-200, freighter conversion STC airplanemodels modified in 737-200C, 737-300,737-400, and 737-500 ST01961SE. accordance with EASA STC series airplanes, supersedes AD 2004- 10016227 Rev. 5 or per EASASTC 18-06,retaining requirements for repetitive 10015542 Rev.5.Supersedure of inspections to find fatiguecracking of certain the EASAAD US-2013-18-08, may upper and lower s... invalidate this AMOC. 10073869 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Cracking in the upper corners of the forward 737-300 freighter conversion The AMOC is only valid for the US-2015-13-05 24/07/2020 Active INDUSTRIES, LTD.IAI entry door skin cutoutThe EASA AD STC ST01566LA737-400 Boeing 737-300 and 737-400 US-2015-13-05, applicable to 737-100, freighterconversion STC airplanemodels modified in 737-200, 737-200C,737-300, 737-400, and ST01961SE accordance with EASA STC 737-500 series airplanes, requires 10016227 Rev. 5 or per EASASTC repetitiveinspections for cracking in the 10015542 Rev.5.Supersedure of uppercorners of the forward entry doorskin the EASAAD US-2015-13-05 may cutout, and repair ifA... invalidate this AMOC. 10073879 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Cracking in the fuselage skin along the chem- 737-300 freighter conversion The AMOC is only valid for the US-2016-16-13 24/07/2020 Active INDUSTRIES, LTD.IAI mill steps at stringersS-1R and S-2R, between STC ST01566LA.737-400 Boeing 737-300 and 737-400 STA 400 and STA 460The EASA AD freighter conversion STC airplanemodels modified in US-2016-16-13, applicable to 737-100, ST01961SE.IAI SB 365-38-032, accordance with EASA STC 737-200, 737-200C,737-300, 737-400, and Revision 0, dated November 10016227 Rev. 5 or per EASASTC 737-500 series airplanes, requiring 2011. 10015542 Rev.5.Supersedure of repetitiveinspections to detect cracks in the the EASAEASA AD US-2016-16-13, fuselage skin alon... may invalidate this AMOC. 10074143 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Fuselage - Skin Panels - InspectionAD -IAI Service Bulletin -Only applicable to aircraft and US-2017-22-04 01/09/2020 Active INDUSTRIES, LTD.IAI US-2017-22-04, applicable to 737-200, -200C, 365-53-050 “Boeing SB areas affected by IAI STC EASA 300, -400, and -500series airplanes,requires 737-53A1349 10016227Rev. 5 or per IAI STC inspection, repair, and replacement ofdis- implementationon IAI Special EASA 10015542 Rev. 5, as bonded fuselage skin panels Boeing Service Freighters”, Rev 1 dated June applicable.-All other requirements Bulletin 737-53A1349,original issue, dated 2020.-IAI DTA report TR of AD US-2017-22-04 except those August 23, 2016.During the IAI 737 conversi... 365-53-00-92485 – stated aboveremain applicable. 737-300/-400 SF<(>,<)>Rev D. This AMOC does not constitute a terminating action toAD US- AD 2017-22-04 inspecti... 10074340 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Israel Aerospace Industries Boeing Model 747-400 converted #MULTIVALUE 24/09/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to the 747-400SF report – to IAI special freighter perEASA continuedstructural integrity inspections SupplementalStructuralInspec STC10014423 (modified from PAX) mandated by Airworthiness Directive(AD) tion Document TR 366-00-00- or per EASA STC 10015911 2018-04-07 affecting Boeing model 747-400 A0316 Issue N dated March (modified fromCombi). series airplane convertedto IAI special 2020. freighter.AD2018-04-07 requires revising the maintenance or inspection p... 10074341 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Service Bulletin (SB) Boeing Model 747-400 converted FAA 99-06-18 24/09/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to themodifications as 747-24A2193, Revision 1, to IAI special freighter perEASA per Boeing Service Bulletin (SB) 747-24A2193 datedJune 19,1997 STC10014423 (modified from PAX) Revision 1dated June 19 1997 mandated by or per EASA STC 10015911 paragraph (b) of Airworthiness Directive(AD) (modified fromCombi). 99-06-18 affecting Boeing model 747-400 series airplane convertedto IAI special freighter.... 10074407 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2000-26-05 28/09/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to the reworkand to IAI special freighter perEASA replacement requirements on the STC10014423 (modified from PAX) environmental control system (ECS)duct or per EASA STC 10015911 assemblies as per Boeing Alert Service (modified fromCombi). Bulletin (SB) 747-21A2416,Rev 0, dated 29 June 2000 mandated by paragraph (a) of AirworthinessDirective (AD) 2000-26-...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 18 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074420 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Service Bulletin Boeing Model 747-400 converted FAA 2000-02-10 29/09/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to therepetitive 747-53A2416, revision 3, to IAI special freighter perEASA inspections and repairs modifications as per dated April 25, 2002IAI STC10014423 (modified from PAX) Boeing ServiceBulletin (SB) 747-53A2416 Service Bulletin 366-53-121 or per EASA STC 10015911 Revision 1 dated May 6, 1999 mandated Rev 0 dated September 2011 (modified fromCombi). byAirworthiness Directive (AD) 2000-02-10 affecting Boeing model 747-400series airplane converted to IAI... 10074421 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Service Bulletin Boeing Model 747-400 converted FAA 2001-11-06 29/09/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to therepetitive 747-53A2390 Revision 1 to IAI special freighter perEASA inspections and repairs modifications dated July 6, 2000IAI STC10014423 (modified from PAX) mandatedby paragraphs(e) and (g) of Supplemental Structural or per EASA STC 10015911 Airworthiness Directive (AD) 2001-11-06 Inspection Document (SSID) (modified fromCombi). affecting Boeingmodel 747-400 series 366-00-00-A0316,Rev. N, airplane converted to IAI special freighter.AD dated March 2020 2001-11-06 requires repetiti... 10074431 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2009-15-12 30/09/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theinstallation and to IAI special freighter perEASA modifications instructions STC10014423 (modified from PAX) modificationsmandated byparagraph (f) of or per EASA STC 10015911 Airworthiness Directive (AD) 2009-15-12 (modified fromCombi). affectingBoeing model 747-400 series airplane converted to IAI special freighter.AD 2009-15-12 requires installi... 10074435 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2009-10-12 30/09/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to themodifications to IAI special freighter perEASA instructions of the inflation system of escape STC10014423 (modified from PAX) slides,ramp/slides and slides/raft mandated or per EASA STC 10015911 by Airworthiness Directive (AD)2009-10-12 (modified fromCombi). affecting Boeing model 747-400series airplane converted toIAI special freighter.AD 2009-10... 10074438 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2007-20-01 01/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theinstructions of to IAI special freighter perEASA reconfiguring the clamps of certain wire STC10014423 (modified from PAX) bundles andapplying insulating sealant to or per EASA STC 10015911 certain fasteners inside the auxiliaryfuel tank, (modified fromCombi). main fuel tanks and surge fuel tanks required by paragraph(f)(1) of Airworthiness Directiv... 10074439 AMOC TO AD ISRAEL AEROSPACE REV. 1 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2007-04-10 01/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to themodification of to IAI special freighter perEASA the decompression panels on the smoke STC10015911 (modified from barrier in themain deck cargo compartment Combi). or replacement of thesmoke barrier with animproved smoke barrier and subsequent inspection requirements mandatedby paragraphs (f) and (g) ofa... 10074440 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2006-21-05 01/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to therequirements of to IAI special freighter perEASA replacing the cell stack of the flight deck STC10014423 (modification from humidifierwith a supplier tested cell stack or PAX) or per EASA STC 10015911 replacing the cell stack with ablanking plate (modified fromCombi). and subsequently deactivating the flight deck humidifieras mandated by Airworthiness... 10074443 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has IAI Supplemental Structural Boeing Model 747-400 converted FAA 2004-07-22 R1 01/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to the revisionof the Inspection Document (SSID) to IAI special freighter perEASA maintenance inspection program to 366-00-00-A0316,Rev. G, STC10014423 (modified from PAX) includeinspections that willgive no less than dated May 2012 or per EASA STC 10015911 the required damage tolerance rating for (modified fromCombi). eachstructural significant item, as mandated by paragraphs (h) and (i) ofAirworthiness Directive (AD...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 19 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074456 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted 2008-03-05 02/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to thereplacement and to IAI special freighter perEASA inspection requirements for shear-pin STC10014423 (modified from PAX) restraints ofGoodrich evacuation slides or per EASA STC 10015911 mandated by Airworthiness Directive (AD) (modified fromCombi). 2008-03-05 affecting Boeing model 747-400 series airplane converted toIAI special freighter.During the I... 10074466 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted 2008-06-27 05/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to thereplacement and to IAI special freighter perEASA inspection requirements for shear-pin STC10014423 (modified from PAX) restraints ofGoodrich evacuation slides or per EASA STC 10015911 mandated by Airworthiness Directive (AD) (modified fromCombi). 2008-06-27 affecting the Goodrich evacuation slides fitted on Boeingmodel 747-400 series airplane conver... 10074479 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted 2008-01-01 06/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to thereplacement to IAI special freighter perEASA requirements for a certain flight deck door STC10014423 (modified from PAX) feature andrevision of the modification or per EASA STC 10015911 record placard mandated by (modified fromCombi). AirworthinessDirective (AD) 2008-01-01 affecting the Boeing model 747-400 seriesairplane converted to IAI special f... 10074518 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted 2007-19-16 09/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theinstructions of to IAI special freighter perEASA inspections in the water and drain lines in the STC10014423 (modified from PAX) cargocompartments, in accordance with or per EASA STC 10015911 Boeing Service Bulletin (SB)747-30A2080, (modified fromCombi). Revision 3 dated June 14, 2007, asrequired byAirworthiness Directive (AD) 2007-19-16 affecting... 10074519 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Service Bulletin Boeing Model 747-400 converted 2016-07-31 09/10/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to therepetitive 747-53A2688, revision 2, to IAI special freighter perEASA inspections and repairs modifications as per dated August 21, 2014IAI STC10014423 (modified from PAX) Boeing ServiceBulletin (SB) 747-53A2688, Service Bulletin 366-53-098 or per EASA STC 10015911 revision 2, dated August 21, 2014 mandated Rev 6 dated May 2020 (modified fromCombi). byAirworthiness Directive (AD) 2016-07-31 affecting Boeing model 747-400series airplane convertedA... 10074530 AMOC TO AD ISRAEL AEROSPACE 747-400 Repetitive inspection and modification of the Boeing Alert Service Bulletin Boeing Model 747-400 converted EASA ADOPTED FAA AD 12/10/2020 Active INDUSTRIES, LTD.IAI upper deck tension tiesSTA 1120 through 747-53A2507, revision 1, to IAI special freighter perEASA 2016-05-12 1220Israel Aerospace Industries (IAI) has dated January 14,2010IAI STC10014423 (modified from PAX) requested an AMOC to theinspections, Service Bulletin 366-53-077 or per EASA STC 10015911 modifications and post-modification Rev 6 datedMarch 2013 - (modified fromCombi). inspections of theupper deck tension ties and “FUSELAGE –Stretched Upper shear webs mandated by Deck Frame and Tension Tie - AirworthinessDirective (AD) 20... Inspection and Repair”IAI Service Bulletin 366-53-139 Rev 2 dated June 2016 - “Modification oftension ties and... 10074531 AMOC TO AD ISRAEL AEROSPACE 747-400 Replacement of tie rods of the center None Boeing Model 747-400 converted EASA ADOPTED FAA AD 12/10/2020 Active INDUSTRIES, LTD.IAI overhead stowage binsIsrael Aerospace to IAI special freighter perEASA 2006-13-09 Industries (IAI) has requested an AMOC to STC10014423 (modified from PAX) thereplacement requirements of specified tie or per EASA STC 10015911 rods of the center overheadstowage bins (modified fromCombi). mandated by Airworthiness Directive (AD) 2006-13-09affecting the Boeing model 747-400 series airp...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 20 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10074734 AMOC TO AD ISRAEL AEROSPACE 747-400 Inspection for corrosion and cracks of the None Boeing Model 747-400 converted FAA 2005-16-10 03/11/2020 Active INDUSTRIES, LTD.IAI station 980 upper deck floorbeam. to IAI special freighter perEASA (2005-16-10 Boeing: Amendment 39-14215. STC10014423 (modified from PAX) Docket No. FAA-2005-21088;Directorate or per EASA STC 10015911 Identifier 2004-NM-267-AD).Israel Aerospace (modified fromCombi). Industries (IAI) has requested an AMOC totheinspection for corrosion and cracks of the station 980 up... 10074735 AMOC TO AD ISRAEL AEROSPACE 747-400 Control panels for the galley cart lift None Boeing Model 747-400 converted FAA 2005-10-19 03/11/2020 Active INDUSTRIES, LTD.IAI replacement or modification.(2005-10-19 to IAI special freighter perEASA Boeing: Amendment 39-14096. Docket No. STC10014423 (modified from PAX) FAA-2004-19532;Directorate Identifier 2004- or per EASA STC 10015911 NM-87-AD).Israel Aerospace Industries (IAI) (modified fromCombi). has requested an AMOC to theinstructions for replacing or modifying the control panels for the... 10074747 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted 2004-07-20 04/11/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to theinvestigative and to IAI special freighter perEASA corrective actions, as applicable, for galley STC10014423 (modified from PAX) chillerboost fan wire bundle W4489, per or per EASA STC 10015911 Boeing Alert Service Bulletin (SB) (modified fromCombi). 747-21A2427, dated April 24, 2003 and as mandated by AirworthinessDirective (AD) 2004-07-20 affectin... 10074748 AMOC TO AD ISRAEL AEROSPACE 747-400 Discrepancies of the fuselage frame to None Boeing Model 747-400 converted FAA 2005-05-08 04/11/2020 Active INDUSTRIES, LTD.IAI tension tie joints at bodystations 1120 to IAI special freighter perEASA through 1220.(2005-05-08 Boeing: STC10014423 (modified from PAX) Amendment 39-13997; Docket No. or per EASA STC 10015911 FAA-2004-19470;Directorate Identifier 2003- (modified fromCombi). NM-268-AD).Israel Aerospace Industries (IAI) has requested an AMOC to theinspections of the fuselage frame to tens... 10074762 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted 2001-14-15 05/11/2020 Active INDUSTRIES, LTD.IAI requested an AMOC to therequirements of to IAI special freighter perEASA modification of the passenger entertainment STC10014423 (modified from PAX) system (PES)and revision of the Airplane or per EASA STC 10015911 Flight Manual (AFM) to ensure that theflight (modified fromCombi). crew is able to remove electrical power from the entire PES whennecessary, as mandated by Ai... 10074763 AMOC TO AD ISRAEL AEROSPACE REV. 1 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted EASA ADOPTED FAA AD 12/01/2021 Active INDUSTRIES, LTD.IAI requested an AMOC to therequirements of to IAI special freighter perEASA 98-06-29 inspection of the separation between the STC10014423 (modified from PAX) galley powerfeeder and static ground wiring, or per EASA STC 10015911 and the adjacent passenger oxygensystem (modified fromCombi). tubing in the forward ceiling area above the door 4 galley, andcorrective actions where necessar... 10074770 AMOC TO AD ISRAEL AEROSPACE 747-400 Longeron Extension Fitting Inspection, Boeing Service Bulletin Boeing Model 747-400 converted US 2020-15-14 06/11/2020 Active INDUSTRIES, LTD.IAI Repairs and Modification.(2020-15-14 The 747-53A2860 Revision 3 to IAI special freighter perEASA Boeing Company: Amendment 39-21177; dated November 11, 2019IAI STC10014423 (modified from PAX) Docket No.FAA-2020-0208; Product Identifier Supplemental Structural or per EASA STC 10015911 2019-NM-209-AD).Israel Aerospace Inspection Document (SSID) (modified fromCombi). Industries (IAI) has requested an AMOC to 366-00-00-A0316,Rev. N, theinstructions for inspections of the dated March 2020 longeron extension fitting... 10075038 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 AD 2014‐08‐08 was issued to detect and IAI SB 365-53-042 Rev 1 dated - All provisions of AD 2014-08-08 AD 2014-08-08 02/12/2020 Active INDUSTRIES, LTD.IAI correct fatigue Cracks in theskin at the lower July 2014FAA AMOC approval that are not corners of the forward entry doorway on 12S-14-471 specificallyreferencedabove airplanes thatdo not have an airstair door remain fully applicable and must cutout.During the conversion to special be complied accordingly.- This freighter a new main deck cargo AMOC is applicable to Boeing doorsurround structure is installed with an Model 737-300 series external double... airplanesmodified in accordance with EASA STC 10015542 Rev.5 and to Boeing Model737-400 series airplanes modif...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 21 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10075047 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Crown Skin Lap Joint - Inspection for Lower - STC EASA 10015542 Rev. 5- All provisions of AD 2015-16-08 (FAA) AD 2015-16-08 03/12/2020 Active INDUSTRIES, LTD.IAI Row Cracking atStringerS-4, Between BS 360 STC EASA 10016227 Rev. 5- that are not specifically and BS 1016AD 2015-16-08 requires FAA AMOC approval referencedabove remain fully inspections of the lap joint at stringers 120S-11-319 applicable and must be S-4Rand S-4L along the entire length from satisfiedaccordingly.This AMOC is body station (BS) 360 to BS 1016,in applicable to Boeing Model accordance with the Accomplishment 737-300series airplanesmodified in Instructions of BoeingS... accordance with EASA STC 10015542 Rev.5 and to Boeing Model737-400 series airplanes modified... 10075063 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Equipment / Furnishings - Passenger Service IAI report 365-25-00-92925 All provisions of AD 2020-17-04 (FAA) AD 2020-17-04 03/12/2020 Active INDUSTRIES, LTD.IAI Units and Lanyard Assemblieson the Life Vest Rev FIAI report 365-25-00- that are not specifically Panels - InstallationAD 2020-17-04, B4716 Rev CFAA AMOC referencedabove remain fully applicable to 737-300, -400, and -500 series approval 790-20-12281 applicable and must be complied airplanes,requires installing lanyard with accordingly.Only applicable to assemblies on the passenger service units Boeing 737-300 airplanesmodified (PSU) and, for certain airplanes, on the life to a 737-300special freighter (SF) vestS... or 737-300 SF with rigid barrier (RB)configuration in accordance with EASA S... 10075094 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 AD 2016-11-04 requires repetitive - IAI SB 365-53-036 Rev 2- FAA - All provisions of AD 2016-11-04 AD 2016-11-04 07/12/2020 Active INDUSTRIES, LTD.IAI inspections for cracking of the1.04-inch AMOC approval 120L-17-207 that are not nominal diameter wire penetration hole, and specificallyreferencedabove applicable relatedinvestigative and corrective remain fully applicable and must actions, in accordance with be satisfied accordingly.- This theAccomplishment Instructions of Boeing AMOC is applicable to Boeing Alert Service Bulletin737-53A1279, Revision Model 737-300 series 2<(>,<)> dated AprilB... airplanesmodified in accordance with EASA STC 10015542 Rev.5 and to Boeing Model737-400 series airplanes modi... 10075095 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 AD 2009-04-15, applicable to 737-300 and - IAI SB 365-53-050 Rev 1- FAA - All provisions of AD 2009-04-15 2009-04-15 07/12/2020 Active INDUSTRIES, LTD.IAI -400 series airplanes, requiresrepetitive AMOC approval 120S-14-440 that are not internal eddy current and detailed specificallyreferencedabove inspections to detectcracked stringer tie clips remain fully applicable and must between STA 360 to STA 907 and Stringer be satisfied accordingly.- This (S)-10L to S-10R; measuring the fastener AMOC is applicable to Boeing spacing and the edge margin ifapplicable, and Model 737-300 series doing ap... airplanesmodified in accordance with EASA STC 10015542 Rev.5 and to Boeing Model737-400 series airplanes modi... 10075333 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted 2006-22-09 06/01/2021 Active INDUSTRIES, LTD.IAI requested an AMOC to theaccomplishment to IAI special freighter perEASA of the repetitive mid-and low-frequency eddy STC10014423 (modified from currentinspections for cracks in the PAX). overlapped skin panels in the fuselageskin lap joints in sections 41, 42, 44 and46, and corrective actions ifnecessary, for certain Boeing M... 10075352 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2006-26-13 08/01/2021 Active INDUSTRIES, LTD.IAI requested an AMOC to theinspection of the to IAI special freighter perEASA attachment of the shoulder restraint harness STC10014423 (modified from PAX) to themounting bracket on certain observer or per EASA STC 10015911 and attendant seats to determine ifa C-clip is (modified fromCombi). used in the attachment, and corrective action if necessary,in accordance with Boeingd... 10075378 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has - Boeing Service Bulletin Boeing Model 747-400 converted FAA 2016-04-02 12/01/2021 Active INDUSTRIES, LTD.IAI requested an AMOC to theaccomplishment 747-53A2499, Revision 3, to IAI special freighter perEASA of repetitive inspections for cracks in the dated July 15, 2014- IAI STC10014423 (modified from overlapping(upper) skin of the upper fastener Service Bulletin 366-53-118 PAX). row of the lap joints of the fuselageskin in dated April 2012 sections 41, 42, and 46; and related investigative andcorrective actions, if necessary,B...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 22 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10075379 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted FAA 2012-04-09 12/01/2021 Active INDUSTRIES, LTD.IAI requested an AMOC to theaccomplishment to IAI special freighter perEASA of the inspections for scribe lines in affected STC10014423 (modified from lap andbutt splices, wing-to-body fairing PAX). locations, external repair and cutoutreinforcement areas; and related investigative and corrective actions ifnecessary, in accordance... 10075560 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 The AD 2018-04-06, superseding AD - IAI SB 365-53-020 revision 5, - The AMOC is only valid for the 2018-04-06 02/02/2021 Active INDUSTRIES, LTD.IAI 2012-12-05, requires repetitiveinspections of dated September 2020.- FAA Boeing 737-300 and the intercostal webs, attachment clips,straps, AMOC approval 737-400airplanemodels modified stringersand stringer splice channels for 790-20-14393. Dated 12 in accordance with EASA STC cracks; and corrective action ifnecessary, at November 2020. 10016227 Rev. 5 or per EASASTC Body Stations BS 360 toBS 348.2 (AFT of the 10015542 Rev.5.- All provisions of forward entrydoor) and BS 303.9 to BS 2... AD 2018-04-06 that are not specifically referencedabove remain fully applicable and must be satisfied accordingly. 10075595 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 Fuselage - Skin Panels - Inspection / Repair / FAA AMOC approval All provisions of AD 2020-26-04 (FAA) 2020-26-04 09/02/2021 Active INDUSTRIES, LTD.IAI InstallationAD 2020-26-04, superseding AD 120S-13-696 that are not specifically 2013-18-08, requires repetitiveinspections referencedabove remain fully for cracking of certain upper and lower skin applicable and must be complied panels of thefuselage and of the fuselage skin with accordingly.Only applicable to along certain chem-milled lines, Boeing 737-300 and 737-400 andcorrective actions if necessary, in acco... aeroplanes modified to aspecial freighter configuration in accordance with EASA STC 10015542 orEASA STC 10016227. 10075596 AMOC TO AD ISRAEL AEROSPACE 737-300 Fuselage Open Body Station Frames - IAI Service Bulletin All provisions of AD 2005-03-02 (FAA) 2005-03-02 09/02/2021 Active INDUSTRIES, LTD.IAI Inspection / Air ConditioningOverhead Ducts 365-21-007 Rev.0FAA AMOC that are not specifically - ModificationAD 2005-03-02 requires approval 150S-07-274a referencedabove remain fully inspection of the applicable body station applicable and must be complied frames,related investigative/corrective with accordingly.Only applicable to actions, and installation of Boeing 737-300 airplanesmodified lanyardhookbrackets and lanyard assemblies to a 737-300special freighter (SF) under the air conditioning o... or 737-300 737-300 Quick Change (QC)configuration in accordance with EASA ST... 10075597 AMOC TO AD ISRAEL AEROSPACE 737-300 Air Conditioning Outlet Extrusion Support IAI Service Bulletin All provisions of AD 2006-26-09 (FAA) 2006-26-09 09/02/2021 Active INDUSTRIES, LTD.IAI Bracket - Inspection / Repair/ ModificationAD 365-53-008 Rev.3FAA AMOC that are not specifically 2006-26-09 requires inspectionsfor cracks approval 120L-17-191 referencedabove remain fully and modification repair ofcertain locations applicable and must be complied having Air Conditioning Brackets attachment with accordingly.Only applicable to inaccordance with Boeing SB 737-53-1216, Boeing 737-300 airplanesmodified Revision 1.The IAI 737-300 conversion fr... to a 737-300special freighter (SF) or 737-300 737-300 Quick Change (QC)configuration in accordance with EASA ST... 10075598 AMOC TO AD ISRAEL AEROSPACE 737-300 Number 2 Galley Fuselage Support Structure FAA AMOC approval All provisions of AD 2004-23-07 (FAA) 2004-23-07 09/02/2021 Active INDUSTRIES, LTD.IAI - ModificationAD2004-23-07 requires 100S-05-9 that are not specifically modification of certain fuselage referencedabove remain fully supportstructure for the number2 galley, to applicable and must be complied prevent the galley from shifting, which could with accordingly.Only applicable to limit accessto the galley door during Boeing 737-300 airplanesmodified emergencies. During the IAI 737-300 to a 737-300special freighter conversionfrom passenge... configuration in accordance with EASA STC 10015542. 10075599 AMOC TO AD ISRAEL AEROSPACE 737-300 Water / Waste - Potable Water Tank Pressure FAA AMOC approval All provisions of AD 2003-26-08 (FAA) 2003-26-08 09/02/2021 Active INDUSTRIES, LTD.IAI Relief Valve - ReplacementTo prevent 100S-04-185 that are not specifically rupture of the potable water tank during referencedabove remain fully flight of theaeroplane, which could result in applicable and must be complied structural damage to the aeroplane andits with accordingly.Only applicable to inability to sustain flight loads, the AD Boeing 737-300 airplanesmodified 2003-26-08 requiresreplacing the existing to a 737-300special freighter pressu... configuration in accordance with EASA STC 10015542.

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 23 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10075625 AMOC TO AD ISRAEL AEROSPACE REV. 1 737-300, 737-400 CAAI AD ISR-I-53-2019-12-6 was prompted by IAI Service Bulletin - All provisions of CAAI AD ISR- CAAI AD ISR- 22/02/2021 Active INDUSTRIES, LTD.IAI a review of the manufacturingprocess for the 365-53-055 Rev. 0, dated I-53-2019-12-6 R2 that are I-53-2019-12-6 R2 9G rigid barrier installed on IAI 737-300, August 2020.CAAI AMOC notspecifically referenced above 737-400passenger to freighter conversions, approval letter G333- remain fully applicable andmust that identified a manufacturingnon- D200820001, dated 20 August becomplied with accordingly.- compliance.It has been found that the 2020.CS-27256-002 Rev. A, Only applicable to Boeing surface preparation before bonding might dated 10 February 2021. 737-300/-400 aeroplanes modified havebeen imp... to specialfreighter per EASA STC 10016227 or per EASA STC 10015542. 10075655 AMOC TO AD ISRAEL AEROSPACE 737-300, 737-400 The AD 2012-26-02, supersedes AD EASA approved freighter - All provisions of AD 2012-26-02 US AD 2012-26-02 17/02/2021 Active INDUSTRIES, LTD.IAI 2005-13-27, retaining requirements conversions: - STC EASA that are not forrepetitive inspections for cracking of the 10016227 Rev. 5. - STC specificallyreferencedin this AMOC crownarea of the fuselageskin. This new AD EASA 10015542 Rev. 5. remain fully applicable and must modifies certain compliance times and also be complied accordingly.- The requiresrepetitive inspections for cracking AMOC is only valid for the using different inspection Boeing737-300 and 737-400 methods,inspecting additiona... airplanemodels modified in accordance with EASA STC 10016227 Rev. 5 or per EASASTC 10015542 Rev.5. 10075701 AMOC TO AD ISRAEL AEROSPACE REV. 1 737-300, 737-400 CAAI AD ISR-I-53-2019-12-6 was prompted by IAI Service Bulletin - All provisions of CAAI AD ISR- (CAAI) ISR- 22/02/2021 Active INDUSTRIES, LTD.IAI a review of the manufacturingprocess for the 365-53-055 Rev. 0, dated I-53-2019-12-6 R2 that are I-53-2019-12-6 R2 9G rigid barrier installed on IAI 737-300, August 2020.CAAI AMOC notspecifically referenced above 737-400passenger to freighter conversions, approval letter G333- remain fully applicable andmust that identified a manufacturingnon- D200820001, dated 20 August becomplied with accordingly.- compliance.It has been found that the 2020.CS-28881-007 Rev -, Only applicable to Boeing surface preparation before bonding might dated 17 February 737-300/-400 aeroplanes modified havebeen imp... 2021.CS-29206-005 Rev -, to specialfreighter per EASA STC dated 17 February 2021. 10016227. 10075778 AMOC TO AD ISRAEL AEROSPACE 737-300 Equipment / Furnishings - Door Mounted Boeing Service Bulletin All provisions of FAA AD FAA 2004-03-34 R1 04/03/2021 Active INDUSTRIES, LTD.IAI Escape Slide Latch CableAttachment Parts - 737-25-1434, dated 22 March 2004-03-34 R1 that are not ReplacementAD 2004-03-34 R1 requires 2001.FAA AMOC approval specificallyreferenced above replacing existing screw, nut, and letter 100S-04-185, dated 2 remain fully applicable and must washersthat attach the latch cable assembly November 2004. be complied withaccordingly.Only to the latch block assembly of thedoor applicable to Boeing 737-300 mounted escape slides, with new, improved aeroplanes modified to screw, nut, and washe... specialfreighter per EASA STC 10015542, REV. 5. 10075786 AMOC TO AD ISRAEL AEROSPACE 737-300 AD 2002-07-10 requires replacement of IAI Engineering Order EI All provisions of FAA AD (FAA) 2002-07-10 05/03/2021 Active INDUSTRIES, LTD.IAI certain repairs in certainfuselage lap joints 365-53-00-99604 Issue New, 2002-07-10 that are not with improved repairs.During the IAI 737-300 dated 1November2004.FAA specifically referencedabove Special Freighter conversion, a section of AMOC approval letter remain fully applicable and must thefuselage is removed from BS 328 toBS 100S-05-9 dated 26 January be complied with accordingly.Only 500B, between stringers 4R and 21L and is 2005. applicable to Boeing 737-300 replaced by a new doorsurround structure. aeroplanes modified to Thej... specialfreighter per EASA STC 10015542, REV. 5. 10075787 AMOC TO AD ISRAEL AEROSPACE 737-300 AD 2003-14-06 requires repetitive IAI Engineering Order EI All provisions of FAA AD (FAA) 2003-14-06 05/03/2021 Active INDUSTRIES, LTD.IAI inspections for cracking of certainlap splices, 365-53-00-93774 Issue B, 2003-14-06 that are not and corrective action if necessary.During the dated 27 October 2004.FAA specifically referencedabove IAI 737-300 Special Freighter conversion, a AMOC approval letter remain fully applicable and must sectionof thefuselage is removed from BS 100S-05-9 dated 26 January be complied with accordingly.Only 328 toBS 500B, between stringers 4R and 21L 2005. applicable to Boeing 737-300 and is replaced by a new doorsurround stru... aeroplanes modified to specialfreighter per EASA STC 10015542, REV. 5. 10075892 AMOC TO AD ISRAEL AEROSPACE 737-400 CAAI AD ISR-I-53-2019-12-6 was prompted by IAI Service Bulletin All provisions of CAAI AD ISR- (CAAI) ISR- 18/03/2021 Active INDUSTRIES, LTD.IAI a review of the manufacturingprocess for the 365-53-055 Rev.0, dated I-53-2019-12-6 R2 that are I-53-2019-12-6 R2 9G rigid barrier installed on IAI 737-400 August 2020.CAAI AMOC notspecifically referenced above passenger tofreighter conversion, that approval letter G333- remain fully applicable and must identifieda manufacturing non-compliance.It D200820001, dated 20 August becomplied with accordingly.Only has been found that the surface preparation 2020.CS-27131-008 Rev -, applicable to Boeing 737-400 before bonding might havebeen improperly dated 15 March 2021. aeroplanes modified to d... specialfreighter per EASA STC 10016227.

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 24 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10076220 AMOC TO AD ISRAEL AEROSPACE 737-400 CAAI AD ISR-I-53-2019-12-6 was prompted by IAI Service Bulletin - All provisions of CAAI AD ISR- (CAAI) ISR- 14/04/2021 Active INDUSTRIES, LTD.IAI a review of the manufacturingprocess for the 365-53-055 Rev.0, dated I-53-2019-12-6 R2 that are I-53-2019-12-6 R2 9G rigid barrier installed on IAI 737-400 August 2020.CAAI AMOC notspecifically referenced above passenger tofreighter conversion, that approval letter G333- remain fully applicable andmust identifieda manufacturing non-compliance.It D200820001, dated 20 August becomplied with accordingly.- has been found that the surface preparation 2020.CS-29205-004 Rev -, Only applicable to Boeing 737-400 before bonding might havebeen improperly dated 6 April 2021. aeroplanes modified to d... specialfreighter per EASA STC 10016227. 10076732 AMOC TO AD ISRAEL AEROSPACE 747-400 Israel Aerospace Industries (IAI) has Boeing Model 747-400 converted EASA ADOPTED FAA AD 22/06/2021 Active INDUSTRIES, LTD.IAI requested an AMOC to therepetitive to IAI special freighter perEASA 2021-07-09 inspections of trim air diffuser ducts or STC10014423 (modified from PAX) sidewall riser ductassemblies (collectively or per EASA STC 10015911 referred to as TADDs) for damage and (modified fromCombi). applicableon-condition actions, per Boeing Alert Service Bulletin (SB)747-21A2577, Rev B dated FebruaryA... 10076920 AMOC TO AD ISRAEL AEROSPACE 737-400 Loading restrictions due to 9G barrier IAI Service Bulletin All provisions of CAAI AD ISR- ISR-I-53-2019-12-6 R2 13/07/2021 Active INDUSTRIES, LTD.IAI 737-300 manufacture non-complianceCAAI AD ISR- 365-53-055 Rev. 1, dated April I-53-2019-12-6 R2 that are I-53-2019-12-6 was prompted by a review 2021.CAAI AMOC approval notspecifically referenced above ofthe manufacturingprocess for the 9G rigid letter G333-D030521001, remain fully applicable and must barrier installedon IAI 737-300/-400 dated 3 May 2021. becomplied with accordingly.Only passengerto freighter conversions, applicable to Boeing 737-300/-400 thatidentified a manufacturingnon- aeroplanes modified to compliance.It has been found t... specialfreighter per EASA STC 10015542 or per EASA STC 10016227. 10075992 AMOC TO AD JET AVIATION AG A319-115 Deviations from SB No. A320-53-1262 - AIRBUS SB A320-53-1262- None 2016-0212 30/03/2021 Active installation instructions perJBSL-M-03629 JBSL-M-03629 applicable in the locations modified by JBSL duringInterior Completion of the aircrafts (ref. FOCA STC 25-20-99 / LBA EMZTA0740 & EASA-IM.A.S.01185) Deviations are:- adaptation of the JBSL modified partition instead of the... 10073562 AMOC TO AD LEONARDO S.p.A. REV. 1 AW 189 AND AW 169 Note: Rev. 1 cancels and supersedes the Annex 1 - Modification to the This AMOC is valid for the 2020-0048 23/06/2020 Active initial issue of thiscertificate.Repetitive Leonardo Leonardo S.p.A. ASB helicopters AW169 serial numbers: Thermal Strip Installation:As alternative 189-237original issue dated 69007, 69043, 69044, 69059, means of compliance to the requirement of § 29 May 2019, Revision A 69062, 69069, 69070, 69089, (3) of theEASA AD 2020-0048, accomplish the dated 05September 2019,and 69094 and 69096and for following action:(3) For Group 1 and Group Revision B dated 04 February helicopters AW189 serial numbers: 2 helicopters: Within 20 FH after lastacc... 2020 or Revision B dated04 49007, 49008, 49011, 89001, February 2020 with Errata 89002 and from 92001 to 92010. Corrige.Annex 2 - Modification to the Leonardo S.p.A. ASB 169-148 original issu... 10073827 AMOC TO AD CARGO 777F Fuel - Center Wing Tank Fuel Quantity Flight Crew Operations None US‐2020‐11‐11 17/07/2020 Active AG Indicating System - Check / Manual Bulletin for Lufthansa AFMRevisionLUFTHANSA CARGO AG Cargo AG No. LUB-32R1 date submitted an application to EASA for an June 17, 2020Maintenance AMOC to ADUS-2020-11-11.AD US-2020‐11‐ TIP No. 777 MT28-031 R2 11 paragraphs (g)(1) through (6) define work dated May 29, 2020 instructionsto be accomplished by performing a Refueling Station Door Cycling (RS...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 25 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10076146 AMOC TO AD MHI RJ AVIATION ALL Flight Management Computing Hardware MHI RJ Aviation ULC’s AFM This EASA AMOC is only valid for US-2020-10-05 09/04/2021 Active ULC System / Airplane Flight Manual -RevisionThe content as follows:-Airplane the CL-600 Series Airworthiness Directive 2020-10-05 was Flight Manual (AFM) CSP- aircraftregistered in European issued on May 25, 2020 by theFAA and B-012 for aircraft model Union Member States or in EASA endorsed by EASA.The component AD CL-600-2C10 -Chapter 2, associatedcountries (Iceland, 2020-10-05 was prompted by reports of the LIMITATIONS – Navigation Liechtenstein, Norway and FlightManagement Computer (FMC) software Systems Limitations- Switzerland) and equippedwith issuing incorrect turn co... prohibition ofuse of the FMS Rockwell Collins Pro Line 4Flight Temperature Compensation Management System feature - first FMC-4200Rockwell Collins Part introducedthrough AFM Numbe... Revision Submission RS-329, datedi... 10076749 AMOC TO AD MHI RJ AVIATION CL-600-2E25 (RJ SERIES 1000) Alternative Method of Compliance to MHI RJ Aviation Service This EASA AMOC is only valid for FAA AD 2020-10-05 23/06/2021 Active ULC CL-600-2D24 (RJ SERIES 900) Airworthiness DirectiveUS-2020-10-05.The Bulletin 670BA-34-053 the CL-600 Regional Jet Series CL-600-2D15 (RJ SERIES 705) Airworthiness Directive 2020-10-05 was “Navigation aircraftserial number listed in the CL-600-2C10 (RJ 700, 701, issued on May 25th, 2020 bythe FAA and −FlightManagement MHI RJ Aviation Service 702) endorsed by EASA.This component AD Computer − Removal of the Bulletin670BA-34-053 and 2020-10-05 was prompted by reports of the Flight Management System registered in European Union FlightManagement Computer (FMC) software (FMS)Temperature Member States or in issuing incorrect turn comm... Compensation Function” EASAassociated countries (Iceland, Initial Issue, dated June 18th Liechtenstein, Norway and 2021or later approved Switzerland)and equipped with revisions.The content of MHI Rockwell Co... RJ Service Bulletin 670BA-34-053 Initial Issue isb... 10075384 AMOC TO AD NOORDZEE REV. 1 AS 365 N3 As Alternative Method of Compliance EASA approval no. Limited to helicopters equipped 2015-0226 R05 13/01/2021 Active HELIKOPTERS (AMOC) to the requirements of 10074085.AH ASB with a Goodrich hoist having a VLAANDEREN N. AD2015-0226R5, Paragraph (7), Table 4, AS365-25.01 .65, Revision4. PartNumber (P/N) as listed in Interval applicable to All AffectedHelicopters, Table 1 of AD2015-0226R5 and apply the following action:At intervals of 36 installing a slip clutch MP/N months (+ 4 months tolerance), or 2000 44314-398. hoistoperating cycles, perform a mandatory check (CHK) of theM... 10075130 AMOC TO AD PARC AVIATION A320-232 Background:EASA AD 2015-0051 was Airbus SB A320-54-1028 Applicable to A320-232 S/N 4630. 2015‐0051 10/12/2020 Active ENGINEERING prompted by reports of cracks affecting the Revision 1, or later approved SERVICESLIMITED aftpylon moveable fairing Rib 5. A regime of revision.IndiGo Working repetitive inspections wasrequired by this Orders ref : 7028513, dated AD, until the embodiment of an optional 08 April 2016. modificationsupported by the Airbus SB A320-54-1028 accomplishment.The aft pylon moveable fairi... 10075131 AMOC TO AD PARC AVIATION A320‐232 Background:EASA AD 2015-0051 was Airbus SB A320-54-1028 Applicable to A320-232 S/N 4757. 2015‐0051 10/12/2020 Active ENGINEERING prompted by reports of cracks affecting the Revision 1, or later approved SERVICESLIMITED aftpylon moveable fairing Rib 5. A regime of revision.IndiGo Working repetitive inspections wasrequired by this Orders ref : 7028517, dated AD, until the embodiment of an optional 04 November 2018. modificationsupported by the Airbus SB A320-54-1028 accomplishment.The aft pylon moveable fairi... 10073287 AMOC TO AD PRECISION 757-200 Fuselage - Crown Skin Panel - Inspection / A-Precision Engineering Applicable to 757-200 MSN 25297 US-2017-20-05 18/05/2020 Active CONVERSIONS, LLC Repair / ReplacementAMOC to AD EA-19-1031, Rev. IR, dated only.This AMOC is valid for12 US-2017-20-05 for MSN 25297 - stage 06/01/19B-Precision months from 17/06/2019 onward. 1Precision Engineering, LLC Engineering Engineering EA-19-1031-SSR, Continuedvalidity after the Authorisation ref. EA-19-1031Rev. IR, dated Rev. IR, dated 06/01/19 expiration date is conditioned to 06/01/19, documenting the replacement on the approval of therelated certainB757-200, previously converted from Damage Tolerance data, and to “Passenger” to “Freigh... any change in the ICAs, ifany,resulting from this approval being incorporated in the o...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 26 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10073406 AMOC TO AD PRECISION 757-200 Fuselage - Fuselage Frame Web - Ref. A - Precision Conversions, Only applicable to 757-200 US-2019-23-06 04/06/2020 Active CONVERSIONS, LLC InspectionAirworthiness Directive LLC SERVICE BULLETIN converted to freighter US-2019-23-06 is applicable to Boeing PC-757-53-A0112<(>,<)> configuration perPrecision 757-200,-200CB,and -300 series airplanes, “Supplemental Instructions Conversions STC ST01529SE (EASA certificated in any category. The ADrequires for Inspection of Station 1640 STC 10015539).Completion of this open-hole HFEC inspections at STA 1640 for Fuselage Frame Web at S-14”, service bulletin as an AMOC only any crack of thefuselage frame web fastener Rev. 1, dated May 29,2020 addresses aircraft(or individual holes, on the left an... side(s) of an aircraft) for which no crack is foundduring the inspections. For on-conditionP... 10073478 AMOC TO AD PRECISION REV. 1 757-200 Fuselage – Fuselage Frame Web STA 1640 - A-Precision Engineering Applicable to B757-200 MSN (AD) US-2019-23-06 16/06/2020 Active CONVERSIONS, LLC InspectionFuselageFrame Web STA 1640 – EA-20-1007, Rev. IR, dated 27051 only.This AMOC is valid for MSN 27051 – stage 1MSN 27051 is converted 05/12/20B-Precision 12 months from 12 May 2020 from a passenger configuration to a Engineering EA-20-1007-SSR, onward. Continuedvalidity beyond cargoconfiguration by Precision Conversions Rev. IR, dated 05/12/20 this initial 12 months period is STC ST01529SE (EASA STC10015539). Cracks conditioned to theapproval of the were found common to S-14R OEM related repair Fatigue & Damage intercostal clipfasteners... Tolerance data<(>,<)>and to any change in the ICAs resulting from this approvali... 10073544 AMOC TO AD PRECISION 757-200 Time Limits / Maintenance Checks - A - Precision Engineering -Only applicable to MSN 24614- US-2020-01-18 19/06/2020 Active CONVERSIONS, LLC Airworthiness LimitationsInstructions - document EA 19-1038 Rev A, Aircraft converted to freighter Principal Structural Elements - Inspections / B757-200 – ExistingExternal configuration per Precision Maintenanceor Inspection Program Repair at STA 350 and S-4LB - ConversionsSTC ST01529SE (EASA RevisionAirworthiness Limitations Precision Engineering STC 10015539) Instructions - Principal Structural Elements - document EA 19-1038-SSR InspectionsThe subject aircraft is converted Rev A, B757-200 –Existing from a passenger conf... External Repair at STA 350 and S-4LC - Precision Engineering document EA 19-1038-DTE Rev. IR, B757-200 –Existing Exte... 10074050 AMOC TO AD PRECISION 757-200 Fuselage - Crown Skin Panel - Inspection / A-Precision Engineering EA Applicable to 757-200 MSN 25056 US 2017-20-05 17/08/2020 Active CONVERSIONS, LLC Repair / ReplacementAMOC to AD 20-1006, Rev. IR, dated only. US-2017-20-05 for MSN 27056MSN 27056 is 06/22/2020B-Precision converted from passenger to freighter by the Engineering EA 20-1006-SSR, PrecisionConversionsSTC ST01529SE (EASA Rev. IR, dated 06/22/2020C- STC 10015539) and has been modified bythe Precision Engineering EA lessor as listed in AD US-2017-20-05<(>,<)> 20-1006-DTE, Rev. IR, dated paragraph (k)(... 07/08/2020D- Precision document ENG180204 Revision 2<(>,<)> Customer ServiceLetter (No Technical Objection) 10074052 AMOC TO AD PRECISION 757-200 Fuselage - Crown Skin Panel - Inspection / A-Precision Engineering EA Applicable to B757-200 MSN US-2017-20-05 17/08/2020 Active CONVERSIONS, LLC Repair / ReplacementAMOC to AD 20-1028, Rev. IR, dated 27054 only.This AMOC is valid for US-2017-20-05 for MSN 27054 – stage 1MSN 6/22/2020B-Precision 12 months. Continued validity 27054 is converted from passenger to Engineering EA 20-1028 SSR, after theexpiration date is freighter by the PrecisionConversions STC Rev. IR, dated 6/22/2020C- conditioned to the approval of the ST01529SE (EASA STC 10015539) and has Precision document related DamageTolerance data, been modified bythe lessor as listed in AD ENG180204 Revision 2 and to any change in the ICAs, if US-2017-20-05, paragraphT... Customer Service Letter any<(>,<)> resultingfrom this (NoTechnical Objection) approval being incorporated in the operator’s mainte... 10074881 AMOC TO AD PRECISION REV. 1 757-200 Fuselage - Crown Skin Panel - Inspection / A-Precision Engineering EA Applicable to 757-200 MSN 27053 US-2017-20-05 19/11/2020 Active CONVERSIONS, LLC Repair / ReplacementAMOC to AD 20-1039, Rev. IR, dated only. US-2017-20-05 for MSN 27053MSN 27053 is 09/14/2020B-Precision converted from passenger to freighter by the Engineering EA 20-1039-SSR, PrecisionConversionsSTC ST01529SE (EASA Rev. IR, dated 09/14/2020C- STC 10015539) and has been modified bythe Precision Engineering EA lessor as listed in AD US-2017-20-05, 20-1039-DTE, Rev. IR, dated paragraph (k)(2) - O... 09/24/2020D- Precision document ENG180204 Revision 2, Customer Service Letter (NoTechnical Objection)

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 27 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10075901 AMOC TO AD PRECISION 757-200 Fuselage Frame Web STA 1640 – MSN A-Precision Engineering Applicable to B757-200 MSN FAA 2019-23-06 19/03/2021 Active CONVERSIONS, LLC 24614The subject aircraftis converted from a EA-20-1001, Rev. IR, dated 24614 only. passenger configuration to acargo 02/21/2020B-Precision configuration by Precision Conversions STC Engineering EA-20-1001-SSR, ST01529SE (EASA STC10015539). Cracks were Rev. IR, dated 02/21/2021C- found common to S-14L OEM intercostal Precision Engineering clipfasteners on the STA 1640 frame web EA-20-1001-DTE, Rev. IR, while performing SB 757... dated 11/10/2020. 10075919 AMOC TO AD PRECISION 757-200 Fuselage – Fuselage Frame Web STA 1640 - A-Precision Engineering Applicable to 757-200 MSN 24614 US-2020-20-10 22/03/2021 Active CONVERSIONS, LLC InspectionFuselageFrame Web STA 1640 – EA-20-1001, Rev. IR, dated only. MSN 24614The subject aircraft is converted 02/21/2020B-Precision from a passenger configuration to acargo Engineering EA-20-1001-SSR, configuration by Precision Conversions STC Rev. IR, dated 02/21/2021C- ST01529SE (EASA STC10015539). Cracks were Precision Engineering found common to S-14L OEM intercostal EA-20-1001-DTE, Rev. IR, clipfastener... dated 11/10/2020 10072553 AMOC TO AD SII DEUTSCHLAND A320-214 ATA 25- Equipment / Furnishing – Galley / - Engineering order Limited to Serial Number(s): 6026, 2019-0106 17/02/2020 Active GMBH Container End<(>,<)> Stop - EO-253-00088-000A- SB 6055, 6065, 6157Galley P/N: ReplacementBackground:EASA AD 2019-0106 601903-25-000101-002 601903-000101, S/N: 005, 006, was issuedto replace Atlas standard 007, 009 container unitcompartment end stops per Airbus SB A320-25-1BK9 and A320-25-1BKK, asapplicable<(>,<)> requesting to replace the end stops in standardcontai... 10074180 AMOC TO AD SR TECHNICS A320-214 ATA 25 – Equipment / Furnishings – -SR Technics Engineering None 2020-0103 03/09/2020 Active SWITZERLAND Ltd. Emergency Locator TransmitterProtection – Disposition, ref. C.OAED. ModificationsBackground:EASA AD 000708-ED01-SR Technics 2020-0103 was issued to remove a potential Aircraft Wiring Manual unsafe condition dueto lackof protection Supplement, ref. C.OAED. against current injection of 28 Volts DC or 000708-AWM01-SR Technics 115Volts AC on a non-rechargeable ELT Illustrated Part Catalogue lithium battery which co... Supplement, ref.C.OAED. 000708-IPC01 10073068 AMOC TO AD SWIFTAIR S.A. 757-200 AMOC to AD 2019-23-06 – SwiftairThe (1) Precision Engineering LLC - Valid only for msn 24614- Valid 2019-23-06 17/04/2020 Active subject airplane is converted from a EA 20-1001 “Engineering for 12 months. Validity’sextension passenger configuration to afreighter Authorization –B757-200 – beyond 12 months isconditioned configuration in accordance with Precision STA 1640 Existing Frame Web by the staged approval by the FAA Conversions LLCSupplemental Type Crack Damage at S-14L”, Rev. of the (ref 1) RepairDesign F/DT Certificate (STC) ST01529SE.The subject IR,dated 2/21/2020.(2) data. airplane also has Aviation Partners Boeing Precision Engineering LLC EA (APB) wingletsinstalled in acc... 20-1001 SSR, “Structural SubstantiationReport, B757-200-STA 1640 Existing Frame Web Crack Damage at S-14L” Rev.... 10073412 AMOC TO AD SWIFTAIR S.A. 757-200 Fuselage – Fuselage Frame Web STA 1640 - A - Precision Engineering LLC -Applicable to B757-200 MSN US-2019-23-06 05/06/2020 Active InspectionFuselageFrame Web STA 1640 – EA 20-1008 “Engineering 25296 only.-This AMOC is valid for MSN 25296 – stage 1MSN 25296 is converted Authorization –B757-200 – 12 months from 15 May 2020 from a passenger configuration to a STA 1640 Existing Frame onward. Continuedvalidity beyond cargoconfiguration by Precision Conversions Crack Damage atS-14L”, Rev. this initial 12 months period is STC ST01529SE (EASA IR,dated 4/10/2020.B - conditioned to theapproval of the STC10015539).Airworthiness Directive Precision Engineering LLC EA related repairs Fatigue & Damage US-2019-23-06 is applicable to Boeing 75... 20-1008 SSR, “Structural Tolerance data<(>,<)>and to any SubstantiationReport, change in the ICAs resulting from B757-200-STA 1640 Existing this approv... Frame Web Crack Damage at S-14L” Rev.IR,C... 10073101 AMOC TO AD TEXAS AIR SERVICES, DHC-6 SERIES 300/310/400 Repair of the MLG pivot fittings by weld Texas Air Services (TAS) The inspection measurement CF-2019-02 22/04/2020 Active Inc.d/b/a TEXAS AIR DHC-6 SERIES build-up and machining tooriginal Repair Specification TAS-MLG- record and repair of the MLG pivot REPAIR 100/110/200/210 manufacturing dimensions as per Texas Air C6UM,Revision C,dated 22 fitting isaccomplished in Services (TAS) RepairSpecification TAS-MLG- November 2019.Texas Air accordance with TAS Inspection C6UM, Revision C, dated 22 November 2019 Services (TAS) Form T-100 C-2 and Repair Sheets.The MLG pivot –Alternate Means of Compliance (AMOC) DHC-6 MLG Pivot fitting must be replaced if any with TCCA Airworthiness Directive(AD) FittingsInspection and measurement of the lugthickness CF-2019-02 applicable t... RepairSheets Revision IR, exceeds the repair limitmentioned dated 04 February 2020. in the TAS Inspection andRepair Sheets.All other r...

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 28 of 29 An agency of the European Union Alternative Method of Compliance (AMOC) easa.europa.eu

EASA Rev. Associated Technical AD Number (AMOC Date of Certificate Application Nature Certificate Holder Models Description Certification basis Limitations/Conditions Status level Documentation only) Issue Number 10073769 AMOC TO AD TEXAS AIR SERVICES, 100/110/200/210/300/310/4 Repair of the MLG axle housing bore, axle TCCA AMOC No. AARDG This AMOC does not cancel AD-CF-2019-02 13/07/2020 Active Inc.d/b/a TEXAS AIR 00 bolt holes, brakeflangeattachment holes and 2020/A52 to TCCA previously approved AMOCs REPAIR pivot fitting lugs by weld build-up and Airworthiness Directive (AD) 10072107 Rev 1 and10073101 Rev machiningto original manufacturing CF-2019-02 dated 26 June 0; they remain in effect for dimensions as perTexas Air Services (TAS) 2020.Texas Air Services (TAS) previous repairs that met Repair Specification TAS-MLG-C6UM, Repair Specification TAS-MLG- theconditions specified in those Revision D, dated 26 March 2020 –Alternate C6UM, Revision D,dated 26 two AMOCs.The MLG axle housing Means of Complianc... March 2020.Inspection must be replaced if any measurement record and measurement of the housingbore repair of the MLG axle exceeds the repair limit mentioned housing bore inaccordance in the T... with TAS Form T-100 C, “DHC-6 M... 10072631 AMOC TO AD AIRLINES A319-112 VLG has currently in its A320 family fleet AD 2016-0212SB Limited to A319-112 MSN 2751 2016-0212 17/03/2020 Active S.A. MSN 3028 (and soon also MSN2751) affected 53-1262EASA STC and MSN 3028. by AD 2016-0212, requiring embodiment of 100633316SB SB 53-1262 rev.01 or later.Both A/C have a A319-44-001Drawings in the previous modification from their Frontier applicationSupplement operation(installation of a LiveTV system, Manual S21.TEC-0568 (ICA for FAA STC ST0788SE), which included aircraft fitted with approval amodificatio... oraircraft changes remainingafter removal of Live-TV)

This report lists certificates issued during the period 01/01/2020 until 21/09/2021. In case you need a certificate not included, please contact [email protected]. Page 29 of 29 An agency of the European Union