European Aviation Safety Agency Collection
This collection contains documents from the following standards organization(s): European Aviation Safety Agency
| EASA/AVIATION EASA.AD.2007.0189 | EN-Emergency AD 2007-0189-E Tail Rotor System - Control Lever - Inspection/Replacement (Applicable to EUROCOPTER DEUTSCHLAND MBB-BK 117 C-2 Helicopters) (This AD Supersedes EASA AD 2006-0379-E) (Supersded by AD 2007-02 | |
| EASA/AVIATION EASA.AD.2007.0190 | EN-AD 2007-0190 Landing Gear - Emergency Blowdown Bottle - Replacement (Applicable to REIMS AVIATION INDUSTRIES F 406) | |
| EASA/AVIATION EASA.AD.2007.0191 | EN-Emergency AD 2007-0191-E Fuel - Differential Fuel Pressure Sensor - Inspection / Replacement (Applicable to STEMME GmbH & Co. KG S10-VT Powered Sailplanes) | |
| EASA/AVIATION EASA.AD.2007.0192 | EN-Emergency AD 2007-0192-E Power Plant - Lower Semichannel Assemblies p/n 109-0641- 10-213 or 109-0642-01-171 of the Forward Firewall - Inspection / Modification (Applicable to Agusta S.p.a. A109E A109S A109LUH) | |
| EASA/AVIATION EASA.AD.2007.0193 | EN-Emergency AD 2007-0193-E Airplane Flight Manual - Emergency and Abnormal Procedures - Amendment (Applicable to EMBRAER EMB-145 (-135)) | |
| EASA/AVIATION EASA.AD.2007.0194 | EN-Emergency AD 2007-0194-E Fuselage Wing & Stabilisers Structure - Inspection/Repair (Applicable to GROB AEROSPACE GmbH TWIN ASTIR and G103 Gliders all variants; and G103C TWIN III SL Powered Sailplanes) | |
| EASA/AVIATION EASA.AD.2007.0195 | EN-AD 2007-0195 Wings - Main Landing Gear (MLG) Attachment - Inspection (Applicable to AIRBUS SAS A310 Aircraft) (This AD supersedes EASA Emergency AD 2006-0335-E) | |
| EASA/AVIATION EASA.AD.2007.0196 | EN-AD 2007-0196R1-CN Cancels EASA AD 2007-0196R1 dated 15 October 2007 | |
| EASA/AVIATION EASA.AD.2007.0196 | EN-AD 2007-0196 R1 Engine - Engine Electronic Controller (EEC) - Inspection (Applicable to ROLLS-ROYCE PLC RB211 Trent 700 Series Engines) (Cancelled by EASA AD 2007-0196R1-CN effective January 13 2009) | |
| EASA/AVIATION EASA.AD.2007.0197 | EN-Emergency AD 2007-0197-E Main Rotor System - M/R Hub Coning Stop Support & Dome Fairing Support Attachments - Check / Replacement / Readjustment (Applicable to EUROCOPTER EC 225 LP Helicopters) (Superseded by AD 2009 | |
| EASA/AVIATION EASA.AD.2007.0198 | EN-AD 2007-0198 Landing Gear - Landing Gear Strut - Inspection / Replacement / Rework (Applicable to S.E.I. Servizi Elicotteristici Italiani S.p.A. (formerly Breda Nardi) NH-500D and AMD500N Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0199 | EN-AD 2007-0199 Placards & Markings - DO NOT TOUCH HANDLE DURING FLIGHT - Installation & Doors - Passenger Door Hinge Supports - Modification (Applicable to 328 Support Services GmbH 328-100 and 328-300 Aircraft) (Corre | |
| EASA/AVIATION EASA.AD.2007.0200 | EN-Emergency AD 2007-0200-E Introduction of new Airworthiness- and Operating Limitations (Applicable to Moravan Aviation s.r.o Z 42 Z 142 and Z 242 Series) | |
| EASA/AVIATION EASA.AD.2007.0201 | EN-AD 2007-0201 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) | |
| EASA/AVIATION EASA.AD.2007.0202 | EN-AD 2007-0202 Engine - HP/IP Turbine Bearing Oil Vent Tube Restrictor - Inspection / Cleaning / Replacement (Applicable to ROLLS-ROYCE plc RB211 Trent 768-60 772-60 772B-60 and 772C-60 (Corrected: 08 August 2007) | |
| EASA/AVIATION EASA.AD.2007.0203 | EN-AD 2007-0203 Propellers - Feathering Pump Interface Bobbin - Inspection / Replacement (Applicable to Fokker Services B.V. F27 Mark 050 Mark 0502 and Mark 0604 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0204 | EN-AD 2007-0204 Powerplant Aft Engine Mounting Centre Bracket - Inspection/Rework (Applicable to Saab AB Saab Aerosystems SAAB 2000) (Superseded by AD 2008-0068 effective April 11 2008) | |
| EASA/AVIATION EASA.AD.2007.0205 | EN-AD 2007-0205 Change to Civil Use Following Use by an Operator Not Controlled by a Civil Authority (Applicable to TURBOMECA Turbo-shaft engine ASTAZOU XIV) | |
| EASA/AVIATION EASA.AD.2007.0206 | EN-AD 2007-0206 Engine - HP Compressor - Test/Modification (Applicable to ROLLS-ROYCE PLC RB211 TRENT 768-60 772-60 772B-60) | |
| EASA/AVIATION EASA.AD.2007.0207 | EN-AD 2007-0207 R1 Wings - Centre Wing Box / Rear Spar Vertical Cruciform at Frame 47 - Inspection / Repair (Applicable to AIRBUS SAS A340-500/-600 series) | |
| EASA/AVIATION EASA.AD.2007.0208 | EN-AD 2007-0208-CN Propeller - High Crosswind Operation - Life Limitation (Applicable to Dowty Propellers Propeller R408/6-123-F/17) | |
| EASA/AVIATION EASA.AD.2007.0209 | EN-Emergency AD 2007-0209-E Rotor Drive - Main Gearbox (MGB) Lubrication Pump - Inspection / Replacement (Applicable to EUROCOPTER AS355 Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0210 | EN-AD 2007-0210 Fuel - Fuel Pump Electrical Grounding - Modification (Applicable to APEX AIRCRAFT (See Applicability Section) | |
| EASA/AVIATION EASA.AD.2007.0211 | EN-AD 2007-0211 Tail Rotor Drive - Rear Drive Shaft Friction Ring - Inspection / Replacement (Applicable to EUROCOPTER EC 120 B Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0212 | EN-AD 2007-0212 Flight Controls - Control Sticks and Bridge - Inspection/Replacement (Applicable to AIRCRAFT INDUSTRIES a.s. L13 BLANÍK Sailplanes) | |
| EASA/AVIATION EASA.AD.2007.0213 | EN-AD 2007-0213 Wings - Outer Wing Main Landing Gear Support Rib 5 Fitting - Inspection / Modification (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) (This AD Supersedes AD 2006-0069R1) | |
| EASA/AVIATION EASA.AD.2007.0214 | EN-AD 2007-0214 Equipment/Furnishings - 103VU Box - Hinge Pin Stopper - Modification (Applicable to AIRBUS A318 A319 A320 and A321) | |
| EASA/AVIATION EASA.AD.2007.0215 | EN-AD 2007-0215 Engine - Icing Conditions During Descent - Operational Procedure and Dispatch Restriction / Modification (Applicable to AIRBUS SAS A330 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0216 | EN-Emergency AD 2007-0216-E Fuel - Engine Feed Line - Operational Procedure (Applicable to AIRBUS A330 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0217 | EN-AD 2007-0217 Navigation - NORTHROP-GRUMMAN (Previously LITTON) ADIRU - Replacement (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0218 | EN-AD 2007-0218 Fuel - Main Fuel Pump System / Fuel Pumps - Airworthiness Limitations / Inspection / Replacement (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0219 | EN-Emergency AD 2007-0219-E Windows - Centre Windshield - Inspection/ Operating Limitation / Replacement (Applicable to EUROCOPTER EC130 B4 Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0220 | EN-AD 2007-0220 Tail Rotor Drive - Tail Rotor Blade Pitch Control Shafts - Identification/Replacement (Applicable to EUROCOPTER SA 365 N and AS 365 N Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0221 | EN-AD 2007-0221 Time Limits - Low Pressure Turbine Rear Frame - Life Reduction (Applicable to CFM International SA (CFM) CFM56-5B Series Engines) | |
| EASA/AVIATION EASA.AD.2007.0222 | EN-Emergency AD 2007-0222R1-E Flight Controls - Flap Down Drive Shaft - Initial Inspection (Applicable to AIRBUS A330 and A340-200/-300 Aircraft) (Superseded by AD 2008-0026 effective February 12 2008) | |
| EASA/AVIATION EASA.AD.2007.0223 | EN-AD 2007-0223 R2 Propellers - Blades Metallic Leading Edge Guard - Inspection (Applicable to Dowty Propellers R408 Series Propellers) | |
| EASA/AVIATION EASA.AD.2007.0224 | EN-AD 2007-0224 R1 (Correction) Equipment & Furnishings - CPT 609 Crash Position Transmitter Beacon Antenna - Inspection/Replacement (Applicable to EUROCOPTER AS 365 N3 and EC 155 B1 Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0225 | EN-AD 2007-0225 Fuselage - Frame of Emergency Exit Door - Modification (Applicable to PIAGGIO AERO INDUSTRIES S.p.A. P 180 Avanti) | |
| EASA/AVIATION EASA.AD.2007.0226 | EN-AD 2007-0226R1 Fuel - Fuel Tank System Wiring & Sensors - Modification/Replacement - Fuel Tank Safety (Applicable to ATR - GIE Avions de Transport Régional ATR 42 Series and ATR 72 Series Aeroplanes) | |
| EASA/AVIATION EASA.AD.2007.0227 | EN-AD 2007-0227 Ice & Rain Protection - Collapsed Wing Anti-ice Hoses - Replacement (Applicable to DASSAULT AVIATION MYSTERE- FALCON 20-()5) | |
| EASA/AVIATION EASA.AD.2007.0228 | EN-AD 2007-0228 Flight Controls - Elevator Booster Control Unit - Inspection / Replacement (Applicable to Fokker Services B.V. F28 Mark 0070 and Mark 0100) (Superseded by AD 2009-0032 effective February 17 2009) | |
| EASA/AVIATION EASA.AD.2007.0229 | EN-AD 2007-0229 Ice & Rain Protection - Wing Leading Edge Heating Piccolo Tube Peri-Seals - Inspection/Replacement (Applicable to Fokker Services B.V. F28 Mark 0070 and Mark 0100 Aircraft) (This AD Supersedes AD 2006-02 | |
| EASA/AVIATION EASA.AD.2007.0230 | EN-AD 2007-0230 Fuel - Electric / Electronic Common Installation Fuel System Route 2S - Modification (Applicable to AIRBUS SAS A310 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0231 | EN-AD 2007-0231 Hydraulic Power - Hydraulic Pipes P/N¿s 109-0761-64-103 and 109-0761-65-103 - Inspection / Replacement (Applicable to Agusta S.p.a. A109E and A119 Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0232 | EN-AD 2007-0232 Engine Oil System - Catchtank (Sump) Filter Adaptor - Installation (Applicable to Thielert Aircraft Engines TAE125-01 Engines) | |
| EASA/AVIATION EASA.AD.2007.0233 | EN-AD 2007-0233 Fuel System - Fuel Tank Electrical Bonding - Inspection /Modification [Fuel Tank Safety] (Applicable to AIRBUS SAS A300-600 Aircraft) (Superseded by AD 2007-0283 effective November 8 2007) | |
| EASA/AVIATION EASA.AD.2007.0234 | EN-Emergency AD 2007-0234 R1-E Wings - Slat Track Downstop Assembly & Parts - Inspection / Repair / Replacement (Applicable to The Boeing Company 737 Series Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0235 | EN-AD 2007-0235 Powerplant - Torque Oil Pressure Pipe & Hose Assemblies - Inspection/Replacement (Applicable to PILATUS AIRCRAFT Ltd. PC-12 Series) (Corrected: 14 September 2007) | |
| EASA/AVIATION EASA.AD.2007.0236 | EN-AD 2007-0236 Doors - Sliding Door Rear Roller Support Shaft and Rear Fitting Inspection/Replacement (Applicable to EUROCOPTER AS 350 and AS 355 Helicopters) (This AD Supersedes AD 2006-0251R2) | |
| EASA/AVIATION EASA.AD.2007.0237 | EN-AD 2007-0237 Tail Rotor System - Control Lever - Inspection/Replacement (Applicable to EUROCOPTER Deutschland GmbH MBB-BK117 C-2 Helicopters) (This AD Supersedes AD 2007-0189-E) | |
| EASA/AVIATION EASA.AD.2007.0238 | EN-AD 2007-0238 R1 Fuselage - Upper Frame Bases-to-Arches Junctions from FR43 to FR46 - Modification (Applicable to AIRBUS SAS A310 Aircraft) (Superseded by AD 2008-0212 effective December 4 2008) | |
| EASA/AVIATION EASA.AD.2007.0239 | EN-AD 2007-0239 Fuel - Refuel Isolation Valve - Replacement (Applicable to AIRBUS A330 and A340 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0240 | EN-AD 2007-0240 Time Limits / Maintenance Checks - Certification Maintenance Requirements (CMR) - Implementation (Applicable to AIRBUS SAS A340 Aircraft) (Superseded by AD 2009-0098 effective April 22 2009) | |
| EASA/AVIATION EASA.AD.2007.0241 | EN-AD 2007-0241R3 Wing - Wing Strut Fitting - Inspection / Replacement (Applicable to Pilatus Aircraft Ltd. PC-6 Series Aeroplanes) | |
| EASA/AVIATION EASA.AD.2007.0242 | EN-AD 2007-0242 Wings - Outer Wings Structural Fatigue - Inspection/Modification (Applicable to AIRBUS SAS A310 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0243 | EN-AD 2007-0243 Wings - Wing/Pylon Thrust- & Sideload Fitting (Spigot) - Inspection / Replacement (Applicable to AIRBUS SAS A300 A310 A300-600 & A300-600ST Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0244 | EN-AD 2007-0244 Equipment & Furnishings - Life Raft Inflation Cylinder - Replacement (Applicable to EUROCOPTER AS 332 L2 and EC 225 LP Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0245 | EN-AD 2007-0245 Flight Controls - Spoiler Actuators - Identification / Reporting (Applicable to AIRBUS SAS A300-600 A300-600ST Aircraft) (Superseded by AD 2008-0058R1 effective March 22 2010) | |
| EASA/AVIATION EASA.AD.2007.0246 | EN-AD 2007-0246 Flight Controls - Rudder Control Rod - Inspection/Replacement (Applicable to AIRBUS A330 and A340-200/-300 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0247 | EN-AD 2007-0247 R1-E Wings - Main Landing Gear (MLG) Rib 6 Aft Bearing Lugs - Inspection (Applicable to AIRBUS SAS A330 and A340 Aircraft) (Correction: 04 October 2007) | |
| EASA/AVIATION EASA.AD.2007.0248 | EN-AD 2007-0248 Fuel System - Fuel Tank Conduits Wiring Protection - Modification [Fuel Tank Safety] (Applicable to Saab AB Saab Aerosystems SF340A and 340B Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0249 | EN-AD 2007-0249 Fire Protection - Cargo Compartment Fire Extinguishing - Inspection of Bottle Wiring Connection - Inspection and Continuity Check (Applicable to AIRBUS A318 A319 A320 and A321 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0250 | EN-Emergency AD 2007-0250-E Exhaust - Thrust Reverser Pivoting Door Actuator Attachment - Inspection (Applicable to AIRBUS A340-200/-300 Aircraft) (Corrected: 20 December 2007) | |
| EASA/AVIATION EASA.AD.2007.0251 | EN-AD 2007-0251 Time Limits / Maintenance Checks - Airworthiness Limitations - Amendment (Applicable to BAE SYSTEMS (OPERATIONS) LTD ATP Series Aircraft) (Superseded by AD 2008-0141 effective July 28 2008) | |
| EASA/AVIATION EASA.AD.2007.0252 | EN-Emergency AD 2007-0252-E Landing Gear - Main Landing Gear System & Parts - Inspection (Applicable to Bombardier Inc. DHC-8-400 Series Aircraft) (Superseded by AD 2007-0272 effective October 16 2007) | |
| EASA/AVIATION EASA.AD.2007.0253 | EN-AD 2007-0253 Exhaust System - Heggemann Type Exhaust System - Inspection / Replacement (Applicable to AQUILA GmbH AQUILA AT01) | |
| EASA/AVIATION EASA.AD.2007.0254 | EN-AD 2007-0254 Engine - Flexible Lubrication Pipes Between Tank and Cooler and Between Intermediate Bearing and Oil Pump - Inspection/Replacement (Applicable to TURBOMECA TURMO Turboshaft Engines) (Superseded by AD 200 | |
| EASA/AVIATION EASA.AD.2007.0255 | EN-AD 2007-0255 Engine - IP Turbine Bearing Oil Vent & Scavenge Tube - Inspection / Modification (Applicable to Rolls-Royce plc RB211 TRENT 768-60 772-60 772B-60 Engines) (Superseded by AD 2009-0069 effective March 2 | |
| EASA/AVIATION EASA.AD.2007.0256 | EN-AD 2007-0256 Equipment and Furnishing - Seat Restraint System Plastic Rotary Buckle Handle - Inspection/Replacement (Applicable to Pacific Scientific Company HTL/KIN-TECH Division Restraint Systems: 2000029 2000067 | |
| EASA/AVIATION EASA.AD.2007.0257 | EN-AD 2007-0257 Main Rotor Drive - Transmission Pylon Support Spindle - Identification/Replacement (Applicable to Agusta S.p.A AB 206 Helicopters) | |
| EASA/AVIATION EASA.AD.2007.0258 | EN-AD 2007-0258 Engine - Low Pressure Compressor Case Assembly Ice Impact Panels - Inspection / Rework / Replacement (Applicable to Rolls-Royce Deutschland Ltd & Co KG TAY Series Engines) | |
| EASA/AVIATION EASA.AD.2007.0259 | EN-AD 2007-0259R1 Fuselage - Upper Fin / Fenestron Fittings - Inspection / Replacement (Applicable to Eurocopter EC 155 Helicopters) [Corrected: 26 February 2010] | |
| EASA/AVIATION EASA.AD.2007.0260 | EN-AD 2007-0260R1 Engine - IP Turbine Bearing Oil Feed Tube - Inspection / Modification (Applicable to Rolls-Royce plc RB211 TRENT 768-60 772-60 772B-60 772C-60 Engines) | |
| EASA/AVIATION EASA.AD.2007.0261 | EN-AD 2007-0261 Flight Controls - Control Sticks and Bridge - Inspection/Replacement (Applicable to AIRCRAFT INDUSTRIES a.s. L 23 SUPER-BLANÍK) | |
| EASA/AVIATION EASA.AD.2007.0262 | EN-AD 2007-0262 Fuselage Structure - Cockpit Windows Frames - Modification (Applicable to DASSAULT AVIATION Fan Jet Falcon Series Mystère- Falcon 20-( )5 Series Mystère-Falcon 20-GF and Mystère-Falcon 200 Aircraft) | |
| EASA/AVIATION EASA.AD.2007.0263 | EN-AD 2007-0263 Main Landing Gear - Side Brace Assembly - Inspection / Modification / Replacement (Applicable to ATR - GIE Avions de Transport Régional ATR 42-00 42-300 and 42-320) | |
| EASA/AVIATION EASA.AD.2007.0264 | EN-AD 2007-0264 Fuel System - Fuel Tank System Airworthiness Limitations (AWL) - Implementation (Applicable to Empresa Brasileira de Aeronáutica S.A. EMB-135BJ) | |
| EASA/AVIATION EASA.AD.2007.0265 | EN-AD 2007-0265 Fuel System - Fuel Tank System Airworthiness Limitations (AWL) - Implementation (Applicable to Empresa Brasileira de Aeronáutica S.A. EMB-135 (Except -135BJ) and EMB-145 Series) | |
| EASA/AVIATION EASA.AD.2007.0266 | EN-AD 2007-0266 Stabilizers - Vertical Stabilizer & Rudder Structure - Inspection / Repair Applicable to AIRBUS SAS A310 A300-600 Aircraft) |