European Aviation Safety Agency Collection
This collection contains documents from the following standards organization(s): European Aviation Safety Agency
| EASA/AVIATION EASA.AD.2006.0162 | EN-AD 2006-0162 Safe Life Airworthiness Limitation Items - ALS Part 1 (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0163 | EN-AD 2006-0163 R1 Fuselage - Main Gearbox (MGB) Suspension Bar Attaching Fittings - Checks (Applicable to EUROCOPTER AS 332 L2 and EC 225 LP Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0164 | EN-AD 2006-0164 Equipment/Furnishings - Untimely Firing of Squibs on GOODRICH Electric Hoists (Applicable to EUROCOPTER AS 350 and AS 355) | |
| EASA/AVIATION EASA.AD.2006.0165 | EN-AD 2006-0165 Airworthiness Limitation Items (ALI) - Structural Maintenance (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) (Superseded by AD 2010-0071 effective April 15 2010) | |
| EASA/AVIATION EASA.AD.2006.0166 | EN-AD 2006-0166 Doors - Hinges - Modification (Applicable to Robinson Helicopter Company R44) | |
| EASA/AVIATION EASA.AD.2006.0167 | EN-AD 2006-0167 Doors - Hinges - Modification (Applicable to Robinson Helicopter Company R22) | |
| EASA/AVIATION EASA.AD.2006.0168 | EN-AD 2006-0168 Flight Controls/Time Limits - Replacement (Applicable to MD Helicopters Inc. (MDHI) MD 600N) | |
| EASA/AVIATION EASA.AD.2006.0169 | EN-Emergency AD 2006-0169-E Rotor(s) - Main Rotor Hub Dome Fairing Attachment Screws (Applicable to EUROCOPTER EC 225 LP) (Superseded by AD 2009-0023 effective February 20 2009) | |
| EASA/AVIATION EASA.AD.2006.0170 | EN-AD 2006-0170 Time Limits - Replacement (Applicable to Brantly International Inc. Brantly (Hynes) Series Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0171 | EN-AD 2006-0171 R1 Fuel - Fuel Vent System - Modification (Applicable to Schweizer Aircraft Corporation Schweizer (Hughes) 269 Series) | |
| EASA/AVIATION EASA.AD.2006.0172 | EN-AD 2006-0172 R1 Tail Rotor - Blade Grip - Inspection and Rework (Applicable to Enstrom Helicopter Corporation F-28A and 280 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0173 | EN-AD 2006-0173 Auto Flight - Auto Pilot - Modification (Applicable to Bell Helicopter Textron Inc. Bell 212) | |
| EASA/AVIATION EASA.AD.2006.0174 | EN-AD 2006-0174 Landing Gear - Nose Landing Gear - Wheels at 90 Degrees (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0175 | EN-Emergency AD 2006-0175-E Main Rotor - Rotating Scissor Assembly of the Main Rotor Head (Applicable to Agusta S.p.a.EH-101-510) | |
| EASA/AVIATION EASA.AD.2006.0176 | EN-AD 2006-0176 Fuel system - Prevention against Explosion Risks - In Tank Bonding (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0177 | EN-AD 2006-0177 (Corrected) Fuselage - Inspection of the Lower Gantry Flanges between FR47 and FR54 (Applicable to AIRBUS SAS A300 A300-600 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0178 | EN-AD 2006-0178 R1 Landing Gear - Parking Brake Pressure Limiter - Replacement (Applicable to AIRBUS SAS A300 A300-600 and A300-600ST Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0179 | EN-AD 2006-0179 Wings - Inner Flap Inspection and Modification (Applicable to AIRBUS SAS A300 A300-600 and A300-600ST Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0180 | EN-AD 2006-0180 High Pressure Turbine (HPT) - Inspection of Disc Rim Cooling Air Holes for Cracks from Scoring Damage (Applicable to ROLLS-ROYCE PLC RB211-524 Series) | |
| EASA/AVIATION EASA.AD.2006.0181 | EN-AD 2006-0181 High Pressure Turbine (HPT) - Inspection of Disc Rim Cooling Air Holes for Cracks from Scoring Damage (Applicable to ROLLS-ROYCE PLC RB211-22B Series Engines (all marks) | |
| EASA/AVIATION EASA.AD.2006.0182 | EN-AD 2006-0182 Engine Turbine Section - High Pressure Turbine - Inspection (Applicable to ROLLS-ROYCE PLC RB211-535) | |
| EASA/AVIATION EASA.AD.2006.0183 | EN-Emergency AD 2006-0183-E Engine Controls - Twist Grip Assembly -Inspection/Replacement (Applicable to EUROCOPTER AS 350 Helicopters) | |
| EASA/AVIATION EASA.AD.2006.0184 | EN-AD 2006-0184 Equipment/Furnishings - Semi Automatic Cargo Loading - Modification of Fixed YZ Latches (Applicable to AIRBUS A319 A320 and A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0185 | EN-AD 2006-0185 Flight Controls - Elevator Bellcrank - Inspection/Modification (Applicable to DASSAULT AVIATION FAN JET FALCON All Series MYSTERE - FALCON 20-( )5 MYSTERE-FALCON 20GF MYSTERE-FALCON 200) | |
| EASA/AVIATION EASA.AD.2006.0186 | EN-AD 2006-0186 Fuel - Prevention Against Fuel Tank Explosion Risk-Adjacent Systems (Applicable to ATR ATR 42 and ATR72 Aircraft) (Superseded by AD 2007-0226) | |
| EASA/AVIATION EASA.AD.2006.0187 | EN-AD 2006-0187 Wings - Fuel tanks - Prevention against Fuel Explosion Risks - Bonding the Bracket of the Fuel System Diffusers to the Wing Structure and Equipment in Fuel Tanks (Applicable to AIRBUS AIRBUS A340-500/-6 | |
| EASA/AVIATION EASA.AD.2006.0188 | EN-AD 2006-0188 Landing Gear - Main Landing Gear Legs - Inspection/Replacement (Applicable to ISSOIRE AVIATION APM 20) | |
| EASA/AVIATION EASA.AD.2006.0189 | EN-AD 2006-0189 Landing Gear - Wheels and Brakes - Master Cylinder Yoke - Inspection/Replacement (Applicable to EADS SOCATA TBM 700) | |
| EASA/AVIATION EASA.AD.2006.0190 | EN-AD 2006-0190 Structures - Essential Actions Required to Extend the Life of the Aircraft (Applicable to SHORT BROTHERS PLC SC7 Skyvan Series 3 3A and 3M) (Superseded by AD 2007-0013) | |
| EASA/AVIATION EASA.AD.2006.0191 | EN-AD 2006-0191 Air Conditioning - Prevention against Fuel Explosion Risks - Installation of Heatshields in Belly Fairing (Applicable to AIRBUS A330-200 and A340-200/-300 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0192 | EN-AD 2006-0192 Lights - Anti-collision Lights Wing- & Tail Strobe Lights - Modification (Applicable to Fokker Aircraft B.V. Model F28 Mark 0100 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0193 | EN-AD 2006-0193 Equipment & Furnishings - Passenger Service Unit - Inspection/Modification (Applicable to Fokker Aircraft B.V. Model F27 Mark 050 and 0502 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0194 | EN-AD 2006-0194 Fuselage - Bottom Skin Chine Line - Inspection/Repair (Applicable to Fokker Aircraft B.V. Model F27 Mark 050 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0195 | EN-AD 2006-0195 Auto Flight - Autopilot Disconnect Unit - Installation (Applicable to Fokker Aircraft B.V. Model F28 Mark 0070 and Mark 0100 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0196 | EN-AD 2006-0196 Indicating/Recording Systems - Periodic Reset and Modification of Display Units (Applicable to AIRBUS SAS A330 and A340 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0197 | EN-AD 2006-0197 (Corrected) Fuel Tank Safety Fuel Airworthiness Limitations (FAL) (Applicable to AvCraft Aerospace GmbH Dornier 328 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0198 | EN-AD 2006-0198 Fuel - Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to SHORT BROTHERS PLC SD3-30 SD3-60 SD3-SHERPA & SD3-60 SHERPA) | |
| EASA/AVIATION EASA.AD.2006.0199 | EN-AD 2006-0199 Fuel - Fuel Tank Safety Fuel Airworthiness Limitations (FAL) (Applicable to Saab AB Saab Aerosystems SAAB 2000) | |
| EASA/AVIATION EASA.AD.2006.0200 | EN-AD 2006-0200 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A300 Aircraft) (Superseded by AD 2007-0094) | |
| EASA/AVIATION EASA.AD.2006.0201 | EN-AD 2006-0201 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A300-600 A300-600ST Aircraft) (Superseded by AD 2007-0095) | |
| EASA/AVIATION EASA.AD.2006.0202 | EN-AD 2006-0202 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A310 Aircraft) (Superseded by AD 2007-0096) | |
| EASA/AVIATION EASA.AD.2006.0203 | EN-AD 2006-0203 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A318/A319/A320/A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0204 | EN-AD 2006-0204 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A330 Aircraft) (Superseded by AD 2007-0023) | |
| EASA/AVIATION EASA.AD.2006.0205 | EN-AD 2006-0205 Fuel - Fuel Tank Safety ALS part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A340 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0206 | EN-AD 2006-0206 Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to Fokker Services B.V. F28 Mk 0070/0100 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0207 | EN-AD 2006-0207R1 Fuel Tank Safety - Fuel Airworthiness Limitations - Implementation (Applicable to Fokker Services B.V. F27 Aeroplanes) | |
| EASA/AVIATION EASA.AD.2006.0208 | EN-AD 2006-0208R1 Fuel Tank Safety - Fuel Airworthiness Limitations - Implementation (Applicable to Fokker Services B.V. F28 Aeroplanes) | |
| EASA/AVIATION EASA.AD.2006.0209 | EN-AD 2006-0209 (Corrected) Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to Fokker Services B.V. F27 Mk 0050/0502/0604 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0210 | EN-Emergency AD 2006-0210-E Wing Main Spar - Inspection of the Upper Cap (Applicable to APEX AIRCRAFT CAP231 CAP20L CAP21) | |
| EASA/AVIATION EASA.AD.2006.0211 | EN-Emergency AD 2006-0211R1-E Return to Flight - Fuselage/Wings - Modification/Reinforcement (Applicable to APEX AIRCRAFT CAP 230 CAP 231 231EX and CAP232) | |
| EASA/AVIATION EASA.AD.2006.0212 | EN-Emergency AD 2006-0212-E Engine - Icing Conditions During Descent - Operational Procedure (Applicable to AIRBUS SAS A330 Aircraft) (Superseded by AD 2006-0259 effective September 1 2006) | |
| EASA/AVIATION EASA.AD.2006.0213 | EN-AD 2006-0213 Landing Gear - Optional Ski Installation (Applicable to EUROCOPTER AS 365 N) | |
| EASA/AVIATION EASA.AD.2006.0214 | EN-AD 2006-0214 Indicating System/Rotor Drive - Main Gear Box - Low Oil Pressure Warning (Applicable to EUROCOPTER EC 155) | |
| EASA/AVIATION EASA.AD.2006.0215 | EN-AD 2006-0215 Fuselage - Inspection of Longeron at Rib '0' (Applicable to BAE SYSTEMS (OPERATIONS) LTD BAe 146 (All Series) | |
| EASA/AVIATION EASA.AD.2006.0216 | EN-Emergency AD 2006-0216-E Main Landing Gear - Shock absorber - Cross Locking Bolt of the Attachment Pin (Applicable to ATR ATR 42 and ATR 72 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0217 | EN-Emergency AD 2006-0217-E Exhaust-System - Inspection of Exhaust-System for Cracks (Applicable to STEMME AG STEMME S 10) | |
| EASA/AVIATION EASA.AD.2006.0218 | EN-Emergency AD 2006-0218-E Required Placard - Flight Envelope Limitation of Never Exceed Speed Vne (Applicable to BINDER MOTORENBAU GMBH ASH 25 EB 28) (Superseded by AD 2006-0346) | |
| EASA/AVIATION EASA.AD.2006.0219 | EN-AD 2006-0219R2 Fuel - Fuel Tank Safety - Fuel Airworthiness Limitations (Applicable to ATR - GIE Avions de Transport Régional ATR 42 and ATR72 Aircraft) (Superseded by AD 2009-0242 effective December 18 2009) | |
| EASA/AVIATION EASA.AD.2006.0220 | EN-AD 2006-0220 Equipment - Passenger Seats - Inspection of Seatbelt Shackle (Applicable to Recaro Aircraft Seating GmbH & Co. KG 3410 3510 (A B C D) 4400 4420 6510) | |
| EASA/AVIATION EASA.AD.2006.0221 | EN-AD 2006-0221 Fuel - Fuel Tank Safety Fuel Airworthiness Limitations (FAL) (Applicable to SAAB AB SAAB Aerosystems SAAB SF340A and SAAB 340B) | |
| EASA/AVIATION EASA.AD.2006.0222 | EN-AD 2006-0222 Fuel - Main Fuel Pump System/Fuel Pumps (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) (Superseded by AD 2007-0218 effective August 10 2007) | |
| EASA/AVIATION EASA.AD.2006.0223 | EN-AD 2006-0223 Flight Controls - Trimmable Horizontal Stabilizer Act (Applicable to AIRBUS A319 A320 and A321 Aircraft) (Superseded by AD 2008-0150 effective August 5 2008) | |
| EASA/AVIATION EASA.AD.2006.0224 | EN-AD 2006-0224 Time Limits - Airworthiness Limitations - Certification Maintenance Requirements (CMR) (Applicable to AIRBUS SAS A330 Aircraft) (Superseded by AD 2008-0138 Effecive July 23 2008) | |
| EASA/AVIATION EASA.AD.2006.0225 | EN-AD 2006-0225 Time Limits - Airworthiness Limitations - Certification Maintenance Requirements (CMR) (Applicable to AIRBUS SAS A340 Aircraft) (Superseded by AD 2007-0240 effective September 4 2007) | |
| EASA/AVIATION EASA.AD.2006.0226 | EN-Emergency AD 2006-0226-E Landing Gear - Nose Landing Gear Actuator Hinge Pin - Inspection/Replacement (Applicable to EADS SOCATA TBM 700 A & B) | |
| EASA/AVIATION EASA.AD.2006.0227 | EN-Emergency AD 2006-0227-E Power Plant - Engine Mount Structure (Pylon) (Applicable to Schempp-Hirth Flugzeugbau GmbH Ventus-2cT; Discus-2T Discus-2cT) | |
| EASA/AVIATION EASA.AD.2006.0228 | EN-Emergency AD 2006-0228-E Tail Rotor - Tail Rotor Pitch Control Link Assy P/N 109-0130-05-117 (Applicable to Agusta S.p.a. A109A AII C K2 E S LUH A119) | |
| EASA/AVIATION EASA.AD.2006.0229 | EN-Emergency AD 2006-0229-E (Corrected) Limitations - Change of Aircraft Flight Manual Supplement (Applicable to ADEFA AVIALSA BAQUERO SERVISIOS AEREOS MARTIN ECHEVARRIA MARTINEZ RIDAO PZL-M18 -M18A) | |
| EASA/AVIATION EASA.AD.2006.0230 | EN-AD 2006-0230 Engine Controls - Ground-idle Stop Assembly - Introduction (Applicable to Fokker Aircraft B.V. Model F.27 Mk.050 Mk.0502 and Mk.0604 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0231 | EN-AD 2006-0231 Ice & Rain Protection - Wing Leading Edge Heating Piccolo Tube Peri-seals - Inspection/Replacement (Applicable to Fokker Aircraft B.V. Model F28 Mark 0070 and Mark 0100 Aircraft) (Superseded by AD 2007-0 | |
| EASA/AVIATION EASA.AD.2006.0232 | EN-AD 2006-0232 Navigation - Inertial Reference Systems (Applicable to AIRBUS SAS A330 Aircraft and A340-200/-300 Series Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0233 | EN-Emergency AD 2006-0233-E Tail Rotor - Internal Bracket Replacement (Applicable to Agusta S.p.a. EH101-510) | |
| EASA/AVIATION EASA.AD.2006.0234 | EN-AD 2006-0234 Equipment and Furnishings - Seat Rail Stops - Inspection (Applicable to Costruzioni Aeronautiche Tecnam P92-J P92-JS and P2002-JF) | |
| EASA/AVIATION EASA.AD.2006.0235 | EN-Emergency AD 2006-0235-E Tail Rotor - Tail Rotor Blade Skin - Check (Applicable to EUROCOPTER AS 350 and AS 355 Helicopters) (Superseded by AD 2007-0138-E) | |
| EASA/AVIATION EASA.AD.2006.0236 | EN-AD 2006-0236 R1 Fuel Wings - Fuel System - Labels in Fuel Tank (Applicable to AIRBUS A319 and A320 Aircraft) | |
| EASA/AVIATION EASA.AD.2006.0237 | EN-AD 2006-0237 Fuel Control Unit (FCU) - Replacement of the Constant Delta Pressure Valve Diaphragm: Incorporation of Modification Tf55 (Applicable to TURBOMECA Turbo-shaft Engine ARRIUS 2F) | |
| EASA/AVIATION EASA.AD.2006.0238 | EN-AD 2006-0238 R2 Time Limits - Engine Critical Part Lives (Applicable to ROLLS-ROYCE plc RB211 Trent 800 Series Engines) (Superseded by AD 2007-0003) | |
| EASA/AVIATION EASA.AD.2006.0239 | EN-AD 2006-0239 R2 Time Limits - HP Compressor Stage 5-6 Rotor Disc Cyclic Life (Applicable to ROLLS-ROYCE plc RB211 Trent 800 Series Engines) (Superseded by AD 2007-0004) | |
| EASA/AVIATION EASA.AD.2006.0240 | EN-Emergency AD 2006-0240-E Engine - Flexible Lubrication Pipe Between Tank and Cooler - Inspection (Applicable to TURBOMECA TURMO IV) (Superseded by AD 2007-0061-E) |