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Tecnam P2008 Jc Aircraft Flight Manual 20081100 Doc. No. Ed.1-Rev.6 2016, 2a1h Jan uary , i' TECNAM P2008 JC MANUFACTURER: COSTRUZJONtAERONAUTtCHE TECNAMs.r.l. AIRCRAFf JC EASA TYPEMODEL:P2008 CERTIFICATE No:A .583 (DATED 2013, 27 SEPTEMBER) SERIAL NUMBER: . j<{):f .O..... REGISTRATION MARKI . GS: .H.B. K,ML This Aircraft Flight Manual is approved by European Aviation Safety Agency (EASA) and applies only EASA CS-VLAcertified airplanes. This Manual must be carried in the airplane at all times. The airplanehas to be operated in compliance with procedures and limitations contained herein. Costruzioni Aeronautiche TECNAM srl Via Maiorise CAPUA (CE)- Italy Tel. +39 (0) 823 997538 WEB: www II .tecnam.com ll Page - 2 0 SECTION 0 1. RECORD OF REVISIONS Any revision to the present Manual, except actual weighing data, is recorded: a of Revisions is in this Section and the operator is advised to INDEX Recordsure that the recordprovid eup-to-d date. make iskepl The Manual issue is identified by Edition and Revision codes reported on each page, lower right side. " " . .. ..... ... .. ..... ... The revision code is numerical and consists of the number subsequentrevi­ RECORD OF REVISIONS . 3 1. sions are identifiedby the change of the code from "O" to "l" Ofor; the firstrevision ........ ....................................... ....................................... .. .. ....... ............. ......... 2. LIST OF EFFECTIVE PAGES . ............ .... 8 . ........................ .... to the basic publication, "2" forthe second one, etc. 3, FOREWORD ............................................................ ....................... 11 4. SECTIONS LIST ..... .......... ........................................................................... ......... 12 Should be necessary tocompletely reissue a publication for contents and format . changes, the Edition code will change to the next number ("2" for the second edi­ tion, "3" forthe third edition etc). Additions, deletions and revisions to existing text will be identified by a revision bar (black line) in the left-hand margin of the page, adjacent to the change. When technical changes cause expansion or deletion of text which results in un­ changed text appearing on a different page, a revision bar will be placed in the right-hand margin adjacent to the page number of all affected pages providing no other revision bar appears on the page. These pages will be updated to the current regular revision date. NOTE: It is the responsibility of the owner to maintain this handbook in a current status when it is being used for operational purposes. 0 Ed.J,Rev.O Ed. l,Rev. Aircraft Flight Manual Aircraft Flight Manual INDEX RECORD OF REVISIONS 4 Page 0 r Page - 5 0 - �rEc'N'A'M Tecnam Approval EASA Approval or EASA Approval or Revised Description of Tecnam Approval Rev Under DOA of Under DOA page Revision Revised Description DO OoA HOO Privileges Rev OoA HDO Privileges page Revision DO Amended to add the wording "Ap- as part approved pi oved" in orde1 to better identify of Type 2-5 thru 30 "'D. Ronca C. Caruso M.O iva M.Oliva EASA the pages approved according to l Paduano M. Landi First issue G. 0 EASA regulation lnves1ion1ion . M.Oliva Amended to add the wording .Ap- D. Ronca M.Oliva 0-4 AmendROR proved" in orde1 to better identify 3-3 thru 22 D. Ronca C. Camso M.Oliva M.Oliva EASA approval D. Ronca M.Oliva the pages approved according to Approved under the au- Amend LOEP 0-8 N" 10052448 EASA regulation thority of DOA, ref M.Oliva Ronca M. Oliva 1 List Index D. Amended to add the wording "Ap- EASA.2 IJ 335 9-3 Amend Supplement . Oliva M.Oliva M. pioved" in 01de1 to bdter identify (MOD2008/068. I 60 l 20) S3 D. Ronca 6 4-3 thru 8 D. Ronca C. Caruso M.Oliva Add Supplement l the pages approved according to .Oliva M.Oliva - D. Ronca M EASA r�gulation 0-4 Amend ROR .Oliva M.Oliva Amended to add the wording "Ap- D. Ronca M 5-5, 0-8 Amend LOEP proved" in order to better identify M.Oliva 5-7 thru 5-10. D. Ronca C.Caruso M.Oliva D. Ronca M.Oliva the pages approved according to 3-5 and 7 Update procedure 14 M.Oliva EASA regulation D. Ronca M.Oliva procedure 4-12 thru 13 Update au- Approved lhe Supplement List Index amended D. Ronca C.Caruso M. Oliva M.Oliva M.Oliva under EASA approval D. Ronca ref Update procedure thor\ty 4-16 thru 17 DOA, N° 10041226 M.Oliva D. Ronca M,Oliva EASAof.21J.335 Add Supplement S7 D. Ronca C. Caruso M.Oliva procedure 3N-5 thru 6 Update .150401) - '.! M.Oliva (MOD2008/038 D. Ronca M.Oliva procedure 4N-l2 thru 13 Update M.Oliva D. Ronca M.Oliva procedure 4N-15 thru 17 Update M.Oliva D. Ronca M. Oliva Supplement List Index 9-3 Amend .Oliva M. Oliva ] D. Ronca M Add Supplement S2 Oliva M.Oliva - S3 D. Ronca M. Updated layout Supplement M_Oliva EASA approval i D. Ronca M,Oliva Supplement List Index l. 9-3 Amend N°l00530 l5 M.Oliva M. Oliva 3 S4 D. Ronca ] Add Supplement - of coolant tern- Add max limit M.Oliva ' D. Ronca M.Oliva and coolant liquid 2-7,8,10 perature specification amended I M.Oliva . D. Ronca M.Oliva Coolant placard amended EASA approval ] 2-23 N°l0054 136 - amended for include M. Oliva M.Oliva 4 Procedure D. Ronca 3-12, 13 CT include M.Oliva Procedure amended for D. Ronca M.Oliva 4-14,15 CT ] M.Oliva M.Oliva list D. Ronca 6-12 Updated equipment the au- C. Caruso M. Oliva List Index D. Ronca underDOA, ref 9-3 Amend Supplement ApprovedLhority EASA.201' \J.335 M_ Oliva 5 . Ronca C.Caruso 215) Add Supplement SS D 5 I (M002008J067.l Ed.l, Rev.5 Rev. Ed. 1, 6 Aircraft Flight Manual Aircraft Flight Manual RECORD OF REVISIONS RECORD OF REVISIONS - r INTENTIONALLY LEFT BLANK INTENTIONALLY LEFT BLANK l . ] ] Ed.1, Rev. 0 Ed. Rev. 0 J, Aircraft Flight Manual Aircraft Flight Manual 2. LIST OF EFFECTIVE PAGES [ J The List of Effective Pages (LOEP), applicable to manuals of every operator, lists all the basic AFM pages: each manual could contain either basic pages or one variant of these pages when the pages of some Supplements are embodied. Pages affected by the current revision are indicated by an asterisk (*) following the re­ vision code. Edition 1, Rev 0 ..................... 30111 July, 2013 Edition Rev 1 ..................... z5•h March, 2015 Edition 1, Rev 2 ..................... 071h April, 2015 Edition 1, Rev 3 ..................... 13th April, 2015 Edition 1, Rev 4 ..................... 14111 July, 2015 Edition 1, Rev 5 ..................... 15•h December, 2015 Edition 1, Rev 6 ..................... 20•h December, 2016 INTENTIONALLY LEFT BLANK Section Pages Revision Section 0 Pages thru 3, 6, 7, 9 thru 12 Rev O Section 0 Page 4 I Rev 5 Section 0 Page 5, 8 Rev6 Section 1 Pages thru 14 Rev O Section 2 Pages 1I thru Rev O Section 2 Pages 5 thru 430 Rev6 Section 3 Pages thru2 Rev O Section 3 Pages 3I thru 22 Rev6 1 Section 4 Pages 1 thru 3 Rev O Section 4 Pages 4 thru 22 Rev6 Section 5 Pages thru 11. 12. 13, Rev O Section 5 Pages 5_,I 7 thru4, 6, 10 14 15. 16 Rev6 Section 6 Pages thru 11 Rev O Section 6 Page 12I Rev 4 Section 7 Pages thru 16 Rev 0 Section 8 Pages I thru l 0 Rev O Section 9 Pages I 2, 4 Rev O Page 3 I, Rev6 1 Rev. Rev. 0 Ed. I, 6 Ed. l, Aircraft Flight Manual Aircraft Flight Manual LOEP 1 3. FOREWORD is a single-engine two-seat aircraftwith a strut braced high wing and Tccnamfixed landing P2008 JC gear. Section 1 provides gen eral information an d it contains definitions, sy mbols ex plana­ tions, acronyms and terminology used. using airplone, you ar e recommended to read car efully this manual: a deep knowledgeBefore ofthe airplan.e and limitations will al low you for oper atin g the airplane femure a ely f . For further information, please contact: INTENTIONALLY LEFT BLANK COSTRUZIONI AERONAUTICHETECNAMs.r.l. Via MAIORISE CAPUA (CE)- ITALY 'il+39 (0)823 997538 �[email protected] Ed.l, Rev. O Ed.l, Rev. 0 Aircraft Flight Manual Aircraft Flight Manual FOREWORD Page I - I SECTION 1 - GENERAL 4. SECTIONS LIST General(*) Section INDEX I Limitations(**) Section2 1- INTRODUCTION ••••••••••••••••••••••••• ••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 3 Emergency Procedures (**) Section 3 2. CERTIFICATION BASIS ••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 3 3. WARNINGS - CAUTIONS - NOTES •••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 3 Normal Procedures(**) Section 4 4. THREE-VIEW AND DIMENSIONS ••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••• 4 5. ENGINE ........................................ ................................................. ...... .... Performance(***) Section 5 PROPELLER............................................................................. ............................. -......... 6 6. FLIGHT CONTROL SURFACES TRAVEL .............................................................. 6 Weight and balance(*) Section 6 7. SPECIFIC LOADINGS ........................... ..... ................................... .................... .... 7 8. 7 9. ACRONYMS AND TERMINOLOGY ................... .................... ............ ............. ...... Airframe and Systems description (*) Section 7 10. UNIT CONVERSION CHART .............................................................................. 138 11. LITRES I US GALLONS CONVERSION CHART .................................................. 14 Ground Handling and Service(*) Section 8 AFM Supplements(***) Section 9 (*) non-approved Section (**)approved Section (***) partially approved Section Rev. 0 0 Ed. 1, Section - General Ed. 1, Rev Aircraft Flight Manual 1 INDEX SECTIONS LIST Page 1 2 1 - Page - 3 1. INTRODUCTION The Flight Manual has been prepared to provide pilots and instructors with in­ formationfor the safe and efficientopenition of this very light airplane. This manual includes the material required to be furnished to the pilot of CS­ VLA. It also contains supplemental data supplied by the airplane manufacturer. 2. CERTIFICATION BASIS !his type of airc�aft has been approved by the European Aviation Safety Agency with CS-VLA including Amendment and the Type Certificate ino.EASA.A.583 nccordnnce has been issued on (date) 27•h cptembcr2013.1 Category of Airworthiness: Normal Noise Certification Basis: EASA CS Amendment 2.
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