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This Document Was Created to Make Public Non-Proprietary Data Explanatory Note No.: A340 TCDS EASA.A.015 Issue 2 This document was created to make public non-proprietary data contained in Special Conditions (including Deviations, Equivalent Safety Findings) that are part of the applicable Certification Basis as recorded in TCDS EASA.A.015. Table of Content: A-01-CCD: CABIN CREW DATA REQUIREMENTS 4 A-1: DISCRETE GUST REQUIREMENTS 8 A-2: INTERACTION OF SYSTEMS AND STRUCTURE 9 A-3: DESIGN MANOEUVER REQUIREMENTS 10 A-4: DESIGN DIVE SPEED VD 13 A-5: LIMIT PILOT FORCES AND TORQUE 15 A-7: STALLING SPEEDS FOR STRUCTURAL DESIGN 16 A-11: AEROELASTIC STABILITY REQUIREMENTS 17 A-1001: REVISED LOADS REQUIREMENTS 20 A-1002: INTERACTION OF SYSTEMS AND STRUCTURE 32 A-1003: DESIGN MANOEUVER REQUIREMENTS 37 A-1004: DESIGN DIVE SPEED VD 39 A-1006: GROUND LOADS AND CONDITIONS FOR CENTRAL LANDING GEAR 41 A-1011: VIBRATION, BUFFET AND AEROELASTIC STABILITY REQUIREMENTS 44 A-1015: CHECKED PITCHING MANOEUVRE LOADS 47 A-1017: BRAKED ROLL CONDITIONS 50 A-1020: LANDING GEAR SHOCK ABSORPTION TESTS 52 A-1021: ENGINE FAILURE LOADS 54 A-1023: CONTINUOUS TURBULENCE LOADS 56 A-1024: CASTING FACTORS 61 A-1026: PROOF OF STRUCTURE 67 CCD-01: DETERMINATION OF CERTIFICATION BASIS FOR CHANGES TO A340 CCD 68 D-100: INSTALLATION OF MINI-SUITE TYPE SEATING 70 D-101: GREEN ARROW AND “OPEN” PLACARD FOR EMERGENCY EXIT MARKING 73 D-102: INCORPORATION OF INERTIA LOCKING DEVICE IN DYNAMIC SEATS 75 E-2: UNDERFLOOR CREW REST COMPARTMENT 78 E-5.1: LOWER DECK LAVATORIES COMPARTMENT 81 E-8.1: LOWER DECK STOWAGE AREA 86 E-11: BULK CREW REST COMPARTMENT 91 E-15: REINFORCED SECURITY COCKPIT DOOR STATUS 94 E-17: TROLLEY LIFT 97 E-18: LOWER DECK GALLEY COMPARTMENT 99 E-19: FIRST CLASS SLIDING SCREENS 101 E-21: EMERGENCY EXIT MARKING REFLECTANCE 104 E-27: FORWARD FACING SEAT, OVER 18 DEGREES TO A/C CENTRELINE 105 E-28: PARTIAL BULK CREW REST COMPARTMENT WITH ATTACHED GALLEY 107 E-29: FUSELAGE BURN THROUGH – AFT PRESSURE BULKHEAD 109 Disclaimer – This document is not exhaustive and it will be updated gradually. TE.CERT.00053-001 © European Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 1 of 275 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Explanatory Note No.: A340 TCDS EASA.A.015 Issue 2 E-30: FUSELAGE BURNTHROUGH SUBSTANTIATION FOR BELLY FAIRING 112 E-31: FUSELAGE BURNTHROUGH SUBSTANTIATION FOR BILGE AREA 114 E-128: IMPROVED FLAMMABILITY STANDARD FOR THERMAL/ACOUSTIC INSULATION MATERIALS – FLAME PENETRATION (EQUIVALENT TO FAR 25.856(B) AT AMENDMENT 111) 116 E-130: APPLICATION OF HEAT RELEASE AND SMOKE DENSITY REQUIREMENTS TO SEAT MATERIALS 131 E-134: INSTALLATION OF SEATS THAT MAKE AN ANGLE OF MORE THAN 18° WITH THE AIRCRAFT LONGITUDINAL AXIS 132 E-1014: HIC COMPLIANCE FOR FRONT ROW SEATING(INFLATABLE RESTRAINTS) 134 E-1022: IMPROVED FLAMMABILITY STANDARDS FOR THERMAL/ACOUSTIC INSULATION MATERIALS 138 E-1023: SIDE FACING SEATS WITH INFLATABLE RESTRAINTS 140 F-1: STALLING AND SCHEDULED OPERATING SPEEDS 144 F-2: MOTION AND EFFECT OF COCKPIT CONTROLS 152 F-3: STATIC LONGITUDINAL STABILITY 153 F-4: STATIC DIRECTIONAL AND LATERAL STABILITY 154 F-5: FLIGHT ENVELOPE PROTECTIONS 155 F-6: NORMAL LOAD FACTOR LIMITING SYSTEM 157 F-8: ACCELERATE STOP DISTANCES 158 F-8.1: ACCELERATE STOP DISTANCES AND RELATED PERFORMANCE 161 F-126: FLIGHT RECORDERS INCLUDING DATA LINK RECORDING 167 F-128: MINIMUM MASS FLOW OF SUPPLEMENTAL OXYGEN 169 F-129: CREW DETERMINATION OF QUANTITY OF OXYGEN IN PASSENGER OXYGEN SYSTEM 170 F-131: FLIGHT INSTRUMENT EXTERNAL PROBES – QUALIFICATION IN ICING CONDITIONS 172 F-137: SECURITY PROTECTION OF AIRCRAFT SYSTEMS AND NETWORKS 176 F-GEN-01: INSTALLATION OF NON-RECHARGEABLE LITHIUM BATTERY 178 F-1001: STALLING AND SCHEDULED OPERATING SPEEDS 180 F-1003: STATIC LONGITUDINAL STABILITY AND LOW ENERGY AWARENESS 187 F-1008: ACCELERATE STOP DISTANCES 188 F-1014: REVISION OF GATE REQUIREMENTS FOR HIGH-LIFT DEVICE CONTROLS 195 G-5: RESISTANCE TO FIRE TERMINOLOGY 196 G-7: FUNCTION AND RELIABILITY TESTING 197 H-01: ENHANCED AIRWORTHINESS PROGRAMME FOR AEROPLANE SYSTEMS - ICA ON EWIS 198 O-1001: FERRYING ONE ENGINE UNSERVICEABLE 201 P-1: FADEC 207 P-2: CENTRE OF GRAVITY CONTROL SYSTEM 208 P-27: FLAMMABILITY REDUCTION SYSTEM 211 P-32: FUEL TANK SAFETY 216 P-1008: FUEL TANK ACCESS COVERS 218 Disclaimer – This document is not exhaustive and it will be updated gradually. TE.CERT.00053-001 © European Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 2 of 275 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Explanatory Note No.: A340 TCDS EASA.A.015 Issue 2 P-1009: ROLLS-ROYCE TRENT 500 TURBINE OVERHEAT DETECTION 219 P-1011: THRUST REVERSER TESTING 220 P-1016: REAR CENTER TANK & TYRE FAILURE 222 P-1018: ENGINE SUSTAINED IMBALANCE 224 P-1020: APU INSTRUMENTS 226 P-1021: WINDMILLING WITHOUT OIL 227 P-1022: FALLING AND BLOWING SNOW 228 P-1024: ECAM EGT INDICATION 230 S-3: LANDING GEAR WARNING 232 S-6: LIGHTNING PROTECTION INDIRECT EFFECTS 234 S-10: EFFECT OF EXTERNAL RADIATION UPON AIRCRAFT SYSTEMS 236 S-10.1: EFFECT OF EXTERNAL RADIATION UPON AIRCRAFT SYSTEMS 238 S-10.2: EFFECT OF EXTERNAL RADIATION UPON AIRCRAFT SYSTEMS 241 S-13: AUTO-THRUST SYSTEM 244 S-16: CONTROL SIGNAL INTEGRITY 245 S-18: ELECTRICAL FLIGHT CONTROLS UNUSUAL FEATURES 246 S-20: EMERGENCY ELECTRICAL POWER 247 S-21: BRAKES WEAR LIMITS 248 S-23: MISCELLANEOUS ELECTRICAL REQUIREMENTS 252 S-24: DOORS 254 S-38: TOWBARLESS TOWING 255 S-45: OIL TEMPERATURE INDICATION 256 S-48: MINIMUM APPROACH BREAK-OFF HEIGHT 257 S-148: LONGITUDINAL TOUCHDOWN PERFORMANCE LIMIT AND MINIMUM APPROACH BREAK-OFF HEIGHT 259 S-1013: AUTO-THRUST SYSTEM (ATS) 261 S-1021: BRAKES AND BRAKING SYSTEM 262 S-1059: HYDRAULIC SYSTEMS 266 S-1065: PACKS OFF OPERATION 269 S-1066: CAT III OPERATIONS - EXCESS DEVIATION ALERT 271 S-1070 ESF: AFM - RVR LIMITS 273 Disclaimer – This document is not exhaustive and it will be updated gradually. TE.CERT.00053-001 © European Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 3 of 275 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Explanatory Note No.: A340 TCDS EASA.A.015 Issue 2 A-01-CCD: CABIN CREW DATA REQUIREMENTS SPECIAL CONDITION A-01-CCD: Cabin Crew Data Requirements APPLICABILITY: A330 / A340 REQUIREMENTS: Regulation (EU) 748/2012of 03 August 2012, as amended ISSUE: 1 dated 10/12/2015 Special Condition summary BACKGROUND The purpose of this CRI is to establish the certification basis for the grandfathered A330/-340 aircraft family Cabin Crew Operational Suitability Data. There were no applicable certification specifications for operational suitability data issued in accordance with point 21.A.16A, effective on the date of the Type Certificate application for the A330-200/-300; A340-200/-300; A340-500; A340-600. In accordance with Part 21, 21.A.17B (a), the operational suitability data certification basis needs to be defined for the A330/-340 aircraft Family Cabin Crew Operational Suitability Data, transferred from the “A330/-340 Family -OEB Cabin Crew Evaluation Report”. The purpose of the (J) OEB CC evaluations, as requested by Airbus, was to: determine whether the A340-600 is a variant of the A340-300(as per JAR-OPS 1.1030- Operation on more than one type or variant); determine whether the A330-200/-300; the A340-500; the A340-600 are variants of the A340-200/-300(as per JAR-OPS 1.1030- Operation on more than one type or variant), thus constituting the “A330/340 family”; provide recommendations to support the establishment by operators, of cabin crew differences training programs for variants (as per JAR-OPS 1.1010 – Conversion and differences training). NOTE: See also certification basis complement CCD-01 (published in this document), that comes in addition to the present SC A-01-CCD. SPECIAL CONDITION Disclaimer – This document is not exhaustive and it will be updated gradually. TE.CERT.00053-001 © European Aviation Safety Agency, 2019. All rights reserved. ISO9001 Certified. Page 4 of 275 Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet. An agency of the European Union Explanatory Note No.: A340 TCDS EASA.A.015 Issue 2 Having regard of the applicable JAR-OPS 1 requirements and in accordance with "Part 3-Procedure Document for Joint Operational Evaluation Board (JOEB)-Cabin Crew”, which governed the (J) OEB CC evaluations, the following aircraft type specific elements that would impact normal and/or emergency operations for cabin crew were compared and assessed, in order to fulfil the purpose of the evaluations: aircraft configuration: o number of aisles o number of passenger decks doors and exits o exit arming/disarming o direction of movement of the operating handle o direction of exit opening o power assist mechanism Note: In accordance with JAR-OPS 1.1030/EU-OPS 1.1030 and later on with ORO.CC.250, self- help exits, for example Type III and Type IV exits, need not to be included in the determination of new type or variant. assisting evacuation means aircraft systems for cabin crew duties: o emergency lighting system o smoke detection system o built-in fire extinguishing system o drop-down oxygen system o communication and public address system o control and indication panels Using the above categories as criteria, detailed Operator Differences Tables(ODRs) – the Airbus equivalent of Aircraft Differences Tables (ADTs) – were provided by Airbus, in order to highlight the exiting differences between the A340-200/-300 as the “base” aircraft and the A330-200/-300; the A340-500, the A340-600 as the “”candidate” aircraft within the comparisons.
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