European Aviation Safety Agency Collection
This collection contains documents from the following standards organization(s): European Aviation Safety Agency
| EASA/AVIATION EASA.AD.2006.0323 | EN-AD 2006-0323 Power Plant - Air Intake Box - Inspection/Modification (Applicable to APEX AIRCRAFT DR400/180 and DR400/180R) | |
| EASA/AVIATION EASA.AD.2006.0324 | EN-Emergency AD 2006-0324 Landing Gear - Main Landing Gear (MLG) Retraction Link - Replacement (Applicable to AIRBUS SAS A330 Aircraft and A340-200/-300 Series) (Superseded by AD 2007-0133) | |
| EASA/AVIATION EASA.AD.2006.0325 | EN-AD 2006-0325 R1 Fuel System - Prevention Against Explosion Risks - Fuel Tank Electrical Bonding - Inspection/Modification (Applicable to AIRBUS SAS A300 and A310 Aircraft) (Corrected: 26 July 2007) | |
| EASA/AVIATION EASA.AD.2006.0326 | EN-Emergency AD 2006-0326-E Propellers - Blades - Inspection / Rework (Applicable to Dowty Propellers (Part of Smiths Aerospace Limited) R321/4-82-F/8 R324/4-82-F/9 R333/4-82-F/12 and R334/4-82-F/13) | |
| EASA/AVIATION EASA.AD.2006.0327 | EN-Emergency AD 2006-0327-E Main Rotor - Main Rotor Head (MRH) Spindles - Check/Replacement (Applicable to EUROCOPTER AS 332 and SA 330 Series Helicopters) (Superseded by AD 2006-0349) | |
| EASA/AVIATION EASA.AD.2006.0328 | EN-AD 2006-0328 Landing Gear - Main Landing Gear Wheel Assembly - Inspection/Repair (Applicable to MESSIER BUGATTI Main Landing Gear (MLG) Wheel Assembly Part Numbers (P/N) C20500000 and P/N C20452000) | |
| EASA/AVIATION EASA.AD.2006.0329 | EN-Emergency AD 2006-0329-E Electrical Power Equipment & Furnishing - Galley Wiring - Inspection / Repair (Applicable to DASSAULT AVIATION MYSTERE-FALCON 50) | |
| EASA/AVIATION EASA.AD.2006.0330 | EN-Emergency AD 2006-0330-E Oxygen - 3rd Crew Member O2 Box & Feeder Cables - Inspection/Repair (Applicable to DASSAULT AVIATION MYSTERE-FALCON 900 FALCON 900EX) | |
| EASA/AVIATION EASA.AD.2006.0331 | EN-Emergency AD 2006-0331-E Placards & Markings - Pressure Altitude (PA) - Limitation & Rotorcraft Flight Manual - Amendment & Power Plant - Engine 'MAX N1' - Check (Applicable to EUROCOPTER DEUTSCHLAND MBB-BK 117 C-1" "MAVSZAAAAAAAAAAA | |
| EASA/AVIATION EASA.AD.2006.0332 | EN-AD 2006-0332 Fuselage - Skin - Inspection/Repair (Applicable to AIRBUS SAS A330 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0333 | EN-AD 2006-0333 Fuselage - Skin - Inspection/Repair (Applicable to AIRBUS SAS Aircraft A340-200/-300 Series) | |
| EASA/AVIATION EASA.AD.2006.0334 | EN-AD 2006-0334R1 Communications - Thales Communications VHF Data Radio - Modification (Applicable to THALES COMMUNICATIONS VHF Data Radio Part Numbers EVR716-11-0300A EVR716-11-0350A EVR716-01-0100A EVR716-01-0200A | |
| EASA/AVIATION EASA.AD.2006.0335 | EN-Emergency AD 2006-0335 Wings / Main Landing Gear (MLG) Attachment - Inspection (Applicable to AIRBUS SAS A310 Aircraft) (Superseded by AD 2007-0195) | |
| EASA/AVIATION EASA.AD.2006.0336 | EN-AD 2006-0336 Engine - HP Compressor Vanes Stages 4 To 11 - Introduction Of A New Setting Procedure To Increase The Minimum Vane TIP Clearance (Applicable to Rolls-Royce Deutschland Ltd & Co. KG TAY611 TAY620 TAY650 | |
| EASA/AVIATION EASA.AD.2006.0337 | EN-AD 2006-0337 Electrical Power - Starting - Starter Generator Limitation (Applicable to EUROCOPTER AS 350 and EC 130 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0338 | EN-AD 2006-0338 Electrical Power - Starting - Starter Generator Limitations (Applicable to EUROCOPTER AS 355 N) | |
| EASA/AVIATION EASA.AD.2006.0339 | EN-AD 2006-0339 Main Rotor - Swashplate Bearing Attaching Screw Heads - Check (Applicable to EUROCOPTER AS 332 L2 HELICOPTERS) | |
| EASA/AVIATION EASA.AD.2006.0340 | EN-AD 2006-0340 R1 Equipment and Furnishings - Seal of the Jettisonable Window Panel - Inspection / Rework (Applicable to EUROCOPTER EC 225 LP and AS 332 series helicopters) (Corrected: 02 August 2007) | |
| EASA/AVIATION EASA.AD.2006.0341 | EN-AD 2006-0341 Equipment & Furnishings - External Baggage Pod Restraint Net - Installation (Applicable to BAE SYSTEMS (OPERATIONS) LTD Jetstream Series 3100) | |
| EASA/AVIATION EASA.AD.2006.0342 | EN-AD 2006-0342 Equipment & Furnishings - Flight Deck ECS Grilles - Introduction of Bolt Attachment (Applicable to BAE SYSTEMS (OPERATIONS) LTD BAe 146 and Avro 146-RJ) | |
| EASA/AVIATION EASA.AD.2006.0343 | EN-AD 2006-0343 Landing Gear - Main Landing Gear Radius Rod - Inspection of Cylinder for Cracking (Applicable to BAE SYSTEMS (OPERATIONS) LTD HP 137 Jetstream MK1 Jetstream Series 200 3100 and 3200) | |
| EASA/AVIATION EASA.AD.2006.0344 | EN-AD 2006-0344-R1 Equipment & Furnishings - Emergency Flotation Gear - Electrical Harnesses and Attachment - Check / Repair / Replacement / Installation (Applicable to EUROCOPTER EC 130 B4 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0345 | EN-AD 2006-0345R1 Propeller - Blade Leading Edge Protection - Inspection/Replacement (Applicable to MT-Propeller Entwicklung GmbH Fixed Pitch Propellers MT Variable Pitch Propellers MTV-1 MTV-2 MTV-3 MTV-5 MTV-6 MT | |
| EASA/AVIATION EASA.AD.2006.0346 | EN-Emergency AD 2006-0346-E Flight Controls - Elevator Control & Pushrod - Inspection/Modification (Applicable to Binder Motorenbau GmbH ASH 25 EB 28) (This AD Supersedes AD 2006-0218-E) | |
| EASA/AVIATION EASA.AD.2006.0347 | EN-Emergency AD 2006-0347-E Wings - Lower Surface Fabric Covering - Inspection (Applicable to APEX AIRCRAFT DR 400 Series) (Superseded by AD 2007-0071) | |
| EASA/AVIATION EASA.AD.2006.0348 | EN-Emergency AD 2006-0348-E Ice Protection - Takeoff with Frost Ice Snow or Slush Contamination and Flight Into Icing Conditions - Operational Limitation (Applicable to EADS SOCATA MS760 Series) | |
| EASA/AVIATION EASA.AD.2006.0349 | EN-AD 2006-0349R1 Main Rotor - Main Rotor Head Spindles - Check / Replacement (Applicable to EUROCOPTER AS 332 C C1 L and L1 Helicopters) (Superseded by Emergency AD 2009-0164-E effective July 29 2009) | |
| EASA/AVIATION EASA.AD.2006.0350 | EN-AD 2006-0350 Equipment & Furnishings - Passenger Seat Backrest - Inspection / Replacement (Applicable to AVIOINTERIORS S.p.A. Passengers Seats 12M( )( )-( )( )( )( )( )( )) (Superseded by AD 2008-0135 effective July | |
| EASA/AVIATION EASA.AD.2006.0351 | EN-Emergency AD 2006-0351-E Wings - Centre Wing Lower Skin - Inspection (Applicable to EADS-CASA C-212-Series Aeroplanes) (Superseded by AD 2006-0365) | |
| EASA/AVIATION EASA.AD.2006.0352 | EN-Emergency AD 2006-0352-E Landing Gear - Carbon Brake Assembly - Inspection / Replacement (Applicable to RUAG Aerospace Services GmbH 228-212) | |
| EASA/AVIATION EASA.AD.2006.0353 | EN-AD 2006-0353 Tail Rotor - Tail Rotor Blades P/N 109-8132-01-111 - Inspection/Replacement (Applicable to Agusta S.p.A. A109E) (Superseded by AD 2007-0010) | |
| EASA/AVIATION EASA.AD.2006.0354 | EN-AD 2006-0354(Corrected) Equipment/Furnishings - Slide Rafts Fitted on Type A Doors - Modification (Applicable to AIRBUS SAS A330 and A340 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0355 | EN-AD 2006-0355 Engine - HP/IP Turbine Bearing Oil Vent Tubes - Inspection /Cleaning / Replacement (Applicable to ROLLS-ROYCE plc RB211 Trent 768-60 772-60 772B-60 and 772C-60) (Superseded by AD 2007-0201 effective A | |
| EASA/AVIATION EASA.AD.2006.0356 | EN-Emergency AD 2006-0356-E Fire Protection - Fire Detection System Integrity - Inspection / Replacement (Applicable to DASSAULT AVIATION FALCON 2000EX (Version F2000EX EASy)) | |
| EASA/AVIATION EASA.AD.2006.0357 | EN-AD 2006-0357R1 Fuselage - Frame 5700 Middle Section - Inspection (Applicable to Agusta S.p.A. AB139 and AW139 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0358 | EN-AD 2006-0358 (Corrected) Stabilizers - Fin Assembly - Inspection/Replacement (Applicable to Agusta S.p.A. AB 139 AW 139 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0359 | EN-Emergency AD 2006-0359-E Wings - Outer to Centre Wing Fitting Cracks - Inspection / Replacement (Applicable to EADS-CASA C-212-DF C-212-EE) | |
| EASA/AVIATION EASA.AD.2006.0360 | EN-Emergency AD 2006-0360-E Exhaust - Tailpipe Assembly - Inspection/Repair/Replacement (Applicable to Agusta S.p.A. AB 139 AW 139 Helicopters) (This AD Supersedes AD 2006-0242-E) | |
| EASA/AVIATION EASA.AD.2006.0361 | EN-Emergency AD 2006-0361-E Rotor Drive(s) - Main Gear Box (MGB) Main Casing - Check/Replacement (Applicable to EUROCOPTER AS 332 C C1 L and L1 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0362 | EN-Emergency AD 2006-0362-E Rotor (s) - Main Rotor Head Frequency Adapters - Modification (Applicable to EUROCOPTER SA 365 N AS 365 N SA 366 and SA 365 C Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0363 | EN-Emergency AD 2006-0363-E Rotor Flight Controls - Load Compensator Lever - Check (Applicable to EUROCOPTER AS 350 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0364 | EN-Emergency AD 2006-0364-E Wings - Main Landing Gear (MLG) Rib 6 Aft Bearing Lugs - Inspection (Applicable to AIRBUS SAS A330 and A340 Aircraft) (Superseded by AD 2007-0247 effective September 6 2007) | |
| EASA/AVIATION EASA.AD.2006.0365 | EN-Emergency AD 2006-0365-E Wings - Centre Wing Lower Skin - Inspection (Applicable to EADS-CASA C-212-Series Aeroplanes) (This AD Supersedes AD 2006-0351-E) (Superseded by AD 2007-0108-E) | |
| EASA/AVIATION EASA.AD.2006.0366 | EN-AD 2006-0366 Equipment - Life Raft - Inspection / Replacement (Applicable to DASSAULT AVIATION MYSTERE-FALCON 50) | |
| EASA/AVIATION EASA.AD.2006.0367 | EN-AD 2006-0367 Fuselage - Nose Landing Gear Well Structure between Frame 11 and Frame 17 - Rework (Applicable to AIRBUS SAS A310 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0368 | EN-Emergency AD 2006-0368-E Rotor - Rotor Mast Nut - Check / Replacement (Applicable to EUROCOPTER SA 365 N AS 365 N SA 366 and EC 155 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0369 | EN-AD 2006-0369 Fuselage Structure - Bonded Doublers - Inspection [Chromic Acid Anodising Lead Fleet Program] (Applicable to AIRBUS SAS A300 Series Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0370 | EN-AD 2006-0370 Instruments / Lighting - Standby Horizon Integral Lighting Logic - Modification / Operational Test (Applicable to AIRBUS SAS A300 A310 and A300-600 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0371 | EN-Emergency AD 2006-0371-E Main Rotor - Main Rotor Latch Bolts P/N 206-010-169-1/-3 and P/N 206-011-122-3 - Replacement (Applicable to Agusta S.p.a. AB206A and AB206B Series) | |
| EASA/AVIATION EASA.AD.2006.0372 | EN-Emergency AD 2006-0372-E Wings - Main Landing Gear (MLG) Attachment - Inspection (Applicable to AIRBUS SAS A300 A300-600 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0373 | EN-Emergency AD 2006-0373R1-E Propeller - Blade Follower 10AP-VM - Replacement (Applicable to STEMME GmbH & Co. KG STEMME S 10-V and S 10-VT Powered Sailplanes) (Corrected 05 January 2007) | |
| EASA/AVIATION EASA.AD.2006.0374 | EN-AD 2006-0374 Time Limits - Airworthiness Limitations- Structural Maintenance (Applicable to AIRBUS SAS A300-600 Aircraft) (Superseded by AD 2009-0155 effective July 17 2009) | |
| EASA/AVIATION EASA.AD.2006.0375 | EN-AD 2006-0375 Electrical Power - Switches - Inspection/Replacement (Applicable to Carling Technologies Inc. Rocker-type Switches Part Number (P/N) TA201-(XX)-(X) Series) | |
| EASA/AVIATION EASA.AD.2006.0376 | EN-AD 2006-0376 Flight Controls - Aileron Tab Bellcrank Assembly - Inspection (Applicable to ATR 42 and ATR 72 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0377 | EN-Emergency AD 2006-0377-E Flight Controls - Elevator Servo Controls - Dispatch Restriction (Applicable to AIRBUS SAS A340-500/-600 Series) (Superseded by AD 2007-0124 effective May 4 2007) | |
| EASA/AVIATION EASA.AD.2006.0378 | EN-Emergency AD 2006-0378-E Rotor Drive(s) - Main Gearbox (MGB) Lubrication Pump - Inspection/Replacement (Applicable to EUROCOPTER AS 355 Helicopters) (Superseded by AD 2007-0209 effective August 6 2007) | |
| EASA/AVIATION EASA.AD.2006.0379 | EN-Emergency AD 2006-0379-E Tail Rotor System - Control Lever With Weights - Inspection. (Applicable to EUROCOPTER DEUTSCHLAND MBB-BK 117 C-2) (Superseded by EASA AD-2007-0189-E) | |
| EASA/AVIATION EASA.AD.2007.0001 | EN-Emergency AD 2007-0001 R1-E Propellers - Slip-Clutch - Inspection/Modification (Applicable to SOLO Kleinmotoren GmbH 2 625) | |
| EASA/AVIATION EASA.AD.2007.0002 | EN-AD 2007-0002 Engine - 2nd Stage Nozzle Guide Vane (NGV2) - Inspection (Applicable to TURBOMECA S.A. ARRIEL 1 Turboshaft Engines) | |
| EASA/AVIATION EASA.AD.2007.0003 | EN-AD 2007-0003R1 Time Limits - Engine Critical Parts Lives (Applicable to ROLLS-ROYCE plc RB211 Trent 800 Series Engines) [Corrected: 06 February 2009] | |
| EASA/AVIATION EASA.AD.2007.0004 | EN-AD 2007-0004 Time Limits - HP Compressor Stage 5-6 Rotor Disc Cyclic Life (Applicable to Rolls-Royce plc RB211 Trent 800 series Engines) (This AD Supersedes AD 2006-0239 R2) | |
| EASA/AVIATION EASA.AD.2007.0005 | EN-AD 2007-0005 Air Conditioning - Automatic Opening Logic of Outflow Valve (OFV) - Modification (Applicable to AIRBUS SAS A300 A310 and A300-600 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0006 | EN-AD 2007-0006 Engine Fuel & Control - Hydro Mechanical Unit (HMU) Constant Delta Pressure Valve Diaphragm - Replacement (Applicable to TURBOMECA S.A. ARRIEL 2B1 Turboshaft Engines) (Superseded by AD 2007-0126 effecti | |
| EASA/AVIATION EASA.AD.2007.0007 | EN-AD 2007-0007 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) Implementation (Applicable to EADS CASA CN-235 Series C-295) (Superseded by AD 2009-0146 effective July 3 2009) | |
| EASA/AVIATION EASA.AD.2007.0008 | EN-AD 2007-0008 Flight Controls - Elevator Servo Controls - Test/Modification (Applicable to AIRBUS SAS A330 and A340-200 and -300 Series) | |
| EASA/AVIATION EASA.AD.2007.0009 | EN-AD 2007-0009 Flight Controls - Elevator Servo Controls Solenoid Valve O-ring Seals - Replacement & Airplane Flight Manual/Master MEL - Temporary Revision & Flight Controls - Elevator Servo Controls - Modification (Ap | |
| EASA/AVIATION EASA.AD.2007.0010 | EN-AD 2007-0010 Tail Rotor - Blades P/N 109-8132-01-111 - Inspection/Replacement (Applicable to Agusta S.p.A. A109E) (This AD Supersedes AD 2006-0353) | |
| EASA/AVIATION EASA.AD.2007.0011 | EN-AD 2007-0011 Flight Controls - Elevator Servo Controls - Mode Selector Valve Position Transducer - Inspection/Replacement/Modification (Applicable to AIRBUS SAS A330 and A340-200/-300 Series) | |
| EASA/AVIATION EASA.AD.2007.0012 | EN-Emergency AD 2007-0012-E Ice and Rain Protection - Main Rotor Blade De-Icing System Harness Connectors - Inspection / Modification (Applicable to EUROCOPTER EC 225 LP Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0013 | EN-AD 2007-0013 Structures - Essential Actions Required to Extend the Life of the Aircraft (Applicable to Short Brothers PLC SC7 Skyvan Series 3 3A and 3M) (This AD Supersedes AD 2006-0190) | |
| EASA/AVIATION EASA.AD.2007.0014 | EN-AD 2007-0014 Flight Controls - Routing of the Push To Talk Wiring - Inspection/Modification (Applicable to APEX AIRCRAFT CAP 10B) | |
| EASA/AVIATION EASA.AD.2007.0015 | EN-AD 2007-0015 Wing - Main Spar Wooden Centre Block - Inspection/Reinforcement (Applicable to APEX AIRCRAFT CAP 10B) | |
| EASA/AVIATION EASA.AD.2007.0016 | EN-AD 2007-0016 Nacelles/Pylons - Engine Cowlings Locking - Modification (Applicable to DASSAULT AVIATION FALCON 2000) | |
| EASA/AVIATION EASA.AD.2007.0017 | EN-AD 2007-0017 Wings - Internal Structure - Inspection (Applicable to APEX AIRCRAFT R 3000 Series) | |
| EASA/AVIATION EASA.AD.2007.0018 | EN-AD 2007-0018 R1 Engine - Gas Generator 2nd Stage Turbine - Inspection/Replacement (Applicable to TURBOMECA S.A. ARRIEL 1 Turboshaft Engines) (Superseded by AD 2009-0236 effective October 29 2009) | |
| EASA/AVIATION EASA.AD.2007.0019 | EN-AD 2007-0019 Landing Gear - MLG Side Brace Assembly - Inspection (Applicable to 328 Support Services GmbH 328 Series) | |
| EASA/AVIATION EASA.AD.2007.0021 | EN-Emergency AD 2007-0021-E Fuselage - Cable Channel - Inspection of Wire Harnesses and Modification of Side Channel Covers (Applicable to EUROCOPTER DEUTSCHLAND GmbH EC135) | |
| EASA/AVIATION EASA.AD.2007.0022 | EN-AD 2007-0022 Electrical System - Prevention Against Fuel Tank Explosion Risks - Fuel Pump Wiring - Modification (Applicable to AIRBUS A300-600ST Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0023 | EN-AD 2007-0023 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A330 Aircraft) (This AD Supersedes AD 2006-0204) |