| Doc Number |
Title |
| EASA.145.AO.CAN.INVALID |
Foreign EASA Part-145 Invalid/Suspended Approvals for Organisations Located in Canada |
| EASA.145.AO.CAN.VALID |
Foreign EASA Part-145 Valid Approvals for Organisations Located in Canada |
| EASA.145.AO.USA.INVALID |
Foreign EASA Part-145 Invalid/Suspended Approvals for Organisations Located in the USA |
| EASA.145.AO.USA.VALID |
Foreign EASA Part-145 Valid Approvals for Organisations Located in the USA |
| EASA.145.NB.AO |
Foreign EASA Part-145 Valid Approvals - List of Non Bilateral EASA Part-145 Approved Organisations |
| EASA.147.NB.AO |
Foreign EASA Part-147 Valid Approvals - List of Non-Bilateral EASA Part-147 Approved Organisations |
| EASA.AAM.GUID |
EASA AAM Guidance (AAM-G) For Canadian Approved Organisations Subject To The AAM Agreement |
| EASA.AD.01001 |
Emergency EASA.A.AD.01001 (Falcon 10) - Ice and Rain Protection - Collapsed Wing Anti-Ice Hoses (Superseded by Emergency AD 2005-0020) |
| EASA.AD.2003.822 |
AD 2003-822 Wings - Inspection / Adjustment of the Ground Spoiler (Applicable to AvCraft Aerospace GmbH Dornier 328-100) |
| EASA.AD.2004.0001 |
AD 2004-0001 (Cessna Citation 750) |
| EASA.AD.2004.0002 |
AD 2004-0002 (Lake) |
| EASA.AD.2004.0003 |
AD 2004-0003 (Puchacz) |
| EASA.AD.2004.0004 |
AD 2004-0004 (PW JT8D-200) |
| EASA.AD.2004.0005 |
AD 2004-0005 (Allison 501 Engine) |
| EASA.AD.2004.0006 |
AD 2004-0006 R1 (TCM GTSIO-520 Engine) |
| EASA.AD.2004.0007 |
AD 2004-0007 (CF6-50C Engine) |
| EASA.AD.2004.0008 |
AD 2004-0008 R1 (PW JT8D Engine) |
| EASA.AD.2004.0009 |
AD 2004-0009 R2 - Rolls Royce Corporation (Formerly Allison Engine Company) |
| EASA.AD.2004.0010 |
Emergency AD 2004-0010 (Embraer 170-100 - ATA 31 Indicating/Warning System) |
| EASA.AD.2004.6339 |
AD 2004-6339 Revision 1 - AQUILA GmbH - AQUILA AT01 - Wings - Bonding Defects Between Wing Shell and Wing Spar (Ref. NAA AD No. D-2004-303R1) |
| EASA.AD.2005.0001 |
Emergency AD 2005-0001 (Gulfstream GV-SP - ATA 31 - Indicating/Warning System - Operating Procedures and Flight Manual Limitations) |
| EASA.AD.2005.0011 |
AD 2005-0011 (TPE7331 Engine) |
| EASA.AD.2005.0012 |
AD 2005-0012 R1 (IAE V2500 Engine) |
| EASA.AD.2005.0013 |
AD 2005-0013 (LAK-19) |
| EASA.AD.2005.0014 |
AD 2005-0014 (LAK-17A) |
| EASA.AD.2005.0015 |
AD 2005-0015 (LAK-19) |
| EASA.AD.2005.0016 |
Emergency AD 2005-0016 R1 (Marganski Swift S-1 - Inspection of Control Column and Stops) |
| EASA.AD.2005.0017 |
Emergency AD 2005-0017 (Lake LA-4 Series - Inspection of Tailplane Attachments) (Superseded by FAA AD 2005-12-02, July 8, 2005) |
| EASA.AD.2005.0019 |
AD 2005-0019 (Robinson R22) |
| EASA.AD.2005.0020 |
Emergency AD 2005-0020 (Falcon 10) - Ice and Rain Protection - Collapsed Wing Anti-Ice Hoses - Replaces AD A.AD.01001 |
| EASA.AD.2005.0021 |
AD 2005-0021 (Honey-XPDR) |
| EASA.AD.2005.0022 |
AD 2005-0022 (Boeing 757, 767 Erroneous Overspeed or Stall Aural Warning - Modification; This AD Supersedes FAA AD 2004-10-05); (This EASA AD Superseded by EASA AD 2005-0026) |
| EASA.AD.2005.0023 |
AD 2005-0023 R3 - Engine - Exhaust Valve and Guide - Inspection (Applicable to Lycoming Engines All Lycoming Piston Engines) |
| EASA.AD.2005.0024 |
AD 2005-0024 - (Rolls-Royce Trent 700 Engine), Revision to G-2005-0016 R1, Inspection of HP/IP Support Assembly Oil Tubes |
| EASA.AD.2005.0025 |
Emergency EASA AD 2005-0025 (Rolls-Royce Trent 500, 700 and 800 Engines), Oil Filler Cap Assembly Inspection/Replacement |
| EASA.AD.2005.0026 |
AD 2005-0026 R1 - Erroneous Overspeed or Stall Aural Warning- Modification - Corrected - (This AD supersedes EASA AD 2005-0022) |
| EASA.AD.2005.0027 |
AD 2005-0027, APEX - All Robin DR Series - Structure - Tailplane - Inspection/Modification (See CRD to PAD-05-012) |
| EASA.AD.2005.0028 |
AD 2005-0028, Robin HR and R Series (See CRD to PAD 05-014) - Corrected |
| EASA.AD.2005.0029 |
AD 2005-0029 SMA Engine (see CRD to PAD 05-015 |
| EASA.AD.2005.0030 |
AD 2005-0030 Jodel (see CRD to PAD 05-013) - Corrected |
| EASA.AD.2005.0031 |
AD 2005-0031 Pitts (see CRD to PAD 05-016) |
| EASA.AD.2005.0032 |
AD 2005-0032 Piper PA-28 and PA-32 (see CRD to PAD 05-019) - Corrected 12/22/2005 |
| EASA.AD.2005.0033 |
Emergency AD 2005-0033 - Falcon 2000 - Oxygen - 3rd Crew Member O2 Box and Feeder Cables - Inspection/Repair (Cancelled - Superseded by EASA AD 2006-0003) |
| EASA.AD.2005.0034 |
AD 2005-0034 Piper PA-28 and PA-32 - Structure - Balance Weight Tube - Inspection (see CRD to PAD 05-017) |
| EASA.AD.2005.0035 |
AD 2005-0035 Piper PA-28 and PA-32 - Structure - Main Undercarriage - Inspection (see CRD to PAD 05-018) |
| EASA.AD.2005.0036 |
AD 2005-0036 Tiger Aircraft - AA-1 and AA-5 (see CRD to PAD 05-020) |
| EASA.AD.2005.6237 |
AD 2005-6237 This "ATR 72" AOM has been Covered by EASA AD 2005-6237, Issued on the 08-09-2005, This AD EASA 2005-06237 is Going to be Posted on DGAC-F AD Website |
| EASA.AD.2006.0003 |
Emergency EASA AD 2006-0003 Dassault Falcon 2000 and 2000EX - (This AD supersedes EASA AD 2005-0033) |
| EASA.AD.2006.0011 |
Emergency EASA AD 2006-0011 - PZL MIELEC- PZL M26 'ISKIERKA' - Inspection and Reinforcement of Fuselage Frame XI |
| EASA.AD.2006.0035 |
Emergency EASA AD 2006-0035 - A340-500/-600 Series Engines - Auxiliary Power Unit (APU) - Inspection for APU and APU Generator Interference |
| EASA.AD.2006.0037 |
AD 2006-0037 Dassault Falcon - Mystere Falcon 50, Mystere Falcon 900, Falcon 900EX, Falcon 2000, 2000EX - Ice and Rain Protection - Outboard Leading Edge Slats - Inspection/Repair |
| EASA.AD.2006.0040 |
Emergency AD 2006-0040 Eurocopter EC 225 LP Helicopters - Rotor(s) - Main Rotor Hub Dome Fairing Attachment |
| EASA.AD.2006.0044 |
AD 2006-0044 Thielert Aircraft Engines - TAE 125-01 (See CRD to PAD 06-011) |
| EASA.AD.2006.0045 |
AD 2006-0045 Airbus A340-200/-300 Series - Equipment/Furnishings - Inspection and Modification of Cockpit Instrument Panel |
| EASA.AD.2006.0046 |
AD 2006-0046 Airbus A340-500/-600 Series Aircraft - Ram Air Turbine (RAT) - Inspection of Anti-Stall Valve |
| EASA.AD.2006.0047 |
AD 2006-0047 Airbus A330 Aircraft - Equipment/Furnishings - Inspection and Modification of Cockpit Instrument Panel |
| EASA.AD.2006.0048 |
AD 2006-0048 Airbus A330 and A340-200/-300 Aircraft -Wings - Leading Edge - Modification of Blow-Down Panels |
| EASA.AD.2006.0049 |
AD 2006-0049 Airbus A340-500/-600 Aircraft - Inspection of Blocker Door Hinges - See PAD-CRD 06-010 |
| EASA.AD.2006.0050 |
AD 2006-0050 Airbus A340-500/-600 Aircraft - Electric Installation - Modification of Electrical Bundles Routing in Yellow and Blue Hydraulic Compartments |
| EASA.AD.2006.0051 |
Emergency AD 2006-0051 Eurocopter AS 365 N - SA 366 - EC 155 - Tail Rotor - Tail Rotor Pitch Control Rod Bearing (Superseded by EASA AD 2006-0258 R1-E) |
| EASA.AD.2006.0052 |
Emergency AD 2006-0052-E Eurocopter EC155 - Doors - Cabin Sliding Doors |
| EASA.AD.2006.0053 |
Emergency AD 2006-0053 Saab AB, Saab Aerosystems - Wings - Aileron - Control Surface Balancing of the Aileron |
| EASA.AD.2006.0055 |
Emergency AD 2006-0055 Eurocopter AS 350 and AS 355 Helicopters - Rotor Flight Controls - Main Servo-Controls |
| EASA.AD.2006.0056 |
Emergency AD 2006-0056 Eurocopter EC 225 LP Helicopters - Limitations - 14Hz-Vibrations at Low Density Altitude |
| EASA.AD.2006.0060 |
Emergency AD 2006-0060-E - Eurocopter AS 350 - Stabilizers - Upper and Lower Fins |
| EASA.AD.2006.0061 |
Emergency AD 2006-0061 Correction - BAE Systems (Operations) LTD - BAe 146 and AVRO 146-RJ (All Series) - Hydraulic System - Removal from Service of Accumulators with Suspect Defect Introduced at Manufacture |
| EASA.AD.2006.0062 |
AD 2006-0062 - Raytheon Aircraft Company - Raytheon HS 125 and Hawker Series - Power Plant - Possible Incorrect Assembly of the Fairlead for Starter/Generator Cables |
| EASA.AD.2006.0063 |
AD 2006-0063 - Raytheon Aircraft Company - Raytheon HS 125 700A, B and BAe 125 800 A, B - Electrical Power - Inspection of the Generator Control Unit Earth Wire |
| EASA.AD.2006.0064 |
AD 2006-0064 - Sikorsky Aircraft Corporation - S61N - Landing Gear - Modification |
| EASA.AD.2006.0065 |
AD 2006-0065 - Robinson Helicopter Company - R22- Landing Gear - Skids - Modification |
| EASA.AD.2006.0066 |
AD 2006-0066 - Airbus - A310 and A300-600 Aircraft - Stabilizers - CFRP (Carbon Fibre Reinforced Plastic) Rudder - Inspection |
| EASA.AD.2006.0067 |
AD 2006-0067 - Diamond Aircraft Industries - DA40 - Fuel - Inspection/Replacement of the Fuel Selector/Fuel Valve Universal Joint |
| EASA.AD.2006.0068 |
AD 2006-0068 - Turbomeca - Arriel 1 Series - Fuel - Engine - Fuel Leaks on the Start Electro Valve - Inspection - Please refer to EASA PAD-CRD 06-041 |
| EASA.AD.2006.0069 |
Emergency AD 2006-0069-E Revision 1 - Airbus - A318, A319, A320 and A321 Aircraft - Outer Wing - Inspection of the Main Landing Gear Support Rib 5 |
| EASA.AD.2006.0070 |
AD 2006-0070 - TURBOMECA - Turbo-shaft Engine MAKILA 1 - Engine and Fuel Control - Engine Control Unit - Replacement of LPG Board |
| EASA.AD.2006.0071 |
AD 2006-0071 - Airbus - A300 Aircraft - Time Limits - Airworthiness Limitation Items - Structural Maintenance (ALI) - Please Refer to EASA PAD-CRD 06-022 |
| EASA.AD.2006.0072 |
Emergency AD 2006-0072-E - Piaggio - P180 - Wings - Inspection of Forward Support of Main Wing Outboard Flap Tracks (Superseded by AD 2006-0305) |
| EASA.AD.2006.0073 |
AD 2006-0073 - Rolls-Royce - RB211 TRENT 768-60, 772-60, 772B-60, 772C-60 - Engine - IP Turbine Bearing/Oil Feed Tube Frettage - Inspection - Please refer to EASA PAD-CRD 06-063 |
| EASA.AD.2006.0074 |
AD 2006-0074 - Airbus - A300, A310 and A300-600 Aircraft - Fuel system - Prevention of Risks of Explosion - Wiring of Adjacent System and Fuel Pump |
| EASA.AD.2006.0075 |
AD 2006-0075 Revision 1 - Airbus - A300, A300-600 and A300-600ST Aircraft - Main Landing Gears - Inspection of Retraction Actuator Piston Rod |
| EASA.AD.2006.0076 |
AD 2006-0076 - Airbus - A300, A310, A300-600 and A300-600ST Aircraft - Fuel - Prevention Of Risks Of Explosion - Inspection Of Electrical Lines In The Wing Leading And Trailing Edges |
| EASA.AD.2006.0077 |
AD 2006-0077 - Airbus - A310 and A300-600 Aircraft - Lights - BRUCE Floor Proximity Emergency Escape Path Marking System FPEEPMS - Please refer to EASA PAD-CRD 06-036 |
| EASA.AD.2006.0078 |
AD 2006-0078 - Eurocopter - EC155 and AS 365N Helicopters - Tail Rotor - Blade Tuning Weights |
| EASA.AD.2006.0079 |
AD 2006-0079 - Eurocopter - EC 130 - Engine Controls - Twist Grip Assembly |
| EASA.AD.2006.0080 |
AD 2006-0080 - Eurocopter - AS 365 N - Equipment/Furnishings - Life Raft Installation |
| EASA.AD.2006.0081 |
AD 2006-0081 - Eurocopter - AS 355 - Rotors Flight Control - Yaw Control |
| EASA.AD.2006.0084 |
Emergency AD 2006-0084 - Eurocopter - SA 365 C, AS 365 N - Rotor(s) - Main Rotor - Check of the Main Rotor Hub-to-Mast Bolted Attachment |
| EASA.AD.2006.0085 |
AD 2006-0085 - EADS Socata - TBM 700 - Main Landing Gear Shock Strut Cylinder - Inspection/Replacement |
| EASA.AD.2006.0087 |
AD 2006-0087 - BAE SYSTEMS (OPERATIONS) LTD - HP 137 Jetstream MK 1, Jetstream Series 200, 3100 and 3200 - Landing Gear - Main and Nose Landing Gears - To Introduce Life Limitations and Provide Means of Establishing Total Flight Cycles Since New for Critical Components |
| EASA.AD.2006.0088 |
AD 2006-0088 - BAE SYSTEMS (OPERATIONS) LTD - Jetstream 4100 - Time Limits - Revised Airworthiness Limitations |
| EASA.AD.2006.0089 |
AD 2006-0089 - Rolls-Royce Deutschland Ltd. and Co. KG. - SPEY 555 All Models, Installed on Fokker 28 All Marks SPEY 506-14A, Installed on BAC One-Eleven - Engine - Low Pressure Turbine - Stage 2 Blades Modification Please refer to PAD-CRD 06-082 |
| EASA.AD.2006.0090 |
AD 2006-0090 - BAE SYSTEMS (OPERATIONS) LTD - British Aerospace ATP - Structures - Introduction of New and Revised Inspections for Fatigue and Environmental Damage |
| EASA.AD.2006.0091 |
Emergency AD 2006-0091-E - BAE SYSTEMS (OPERATIONS) LTD - BAe 146 and AVRO 146-RJ - Wings - Inspection of the Wing Top Skin Under Rib 0 Joint Strap |
| EASA.AD.2006.0092 |
AD 2006-0092 Propellers - Propeller Hub Inspection (Applicable to Hartzell Propeller Inc. ( )HC-( )2Y( )-( )) (Corrected September 7, 2006) |
| EASA.AD.2006.0093 |
AD 2006-0093 - EUROCOPTER - EC120 Helicopters - Engine Controls - Twist Grip Assembly |
| EASA.AD.2006.0094 |
AD 2006-0094 - EUROCOPTER - AS350 Helicopters - Engine Controls - Twist Grip Assembly |
| EASA.AD.2006.0095 |
AD 2006-0095 - EUROCOPTER - AS 350 helicopters - Stabilizers - Upper and Lower Fins |
| EASA.AD.2006.0096 |
AD 2006-0096 - EUROCOPTER - AS 355 Helicopters - Stabilizers - Upper and Lower Fins |
| EASA.AD.2006.0097 |
AD 2006-0097 R1 Stabilizers - Upper and Lower Fins (Applicable to EUROCOPTER AS 355) |
| EASA.AD.2006.0098 |
AD 2006-0098 - EUROCOPTER - AS 350, AS 355, AS 365 N, EC 155, AS 332, AS 332 L2, SA 330, SA 315, SA 341/342, SA 360, SA 365 C, SA 313/318 and SA 316/319 Helicopters - Equipment/Furnishings - Hoist Hooks |
| EASA.AD.2006.0099 |
AD 2006-0099 - EUROCOPTER - AS 365 N and EC 155 Helicopters - Tail Rotor - Tail Rotor Blade Check |
| EASA.AD.2006.0100 |
AD 2006-0100 - EUROCOPTER - AS 355 Helicopters - Tail Rotor Drive - Tail Rotor Drive Shaft Forward Shaft Section |
| EASA.AD.2006.0101 |
AD 2006-0101 - EUROCOPTER - AS 365 N, SA 366 and EC 155 Helicopters - Rotor Drive(s) - Check of Main Gearbox (MGB) Base Plate |
| EASA.AD.2006.0102 |
Emergency AD 2006-0102-E - EUROCOPTER - EC 225 LP Helicopters - Fuselage - Check of Frame 5295 and of the Outer Skin Panelling at the Attachment Points of the MGB Sliding Cowling Rails and of the Attachment of the MGB Suspension Bar Fitting |
| EASA.AD.2006.0103 |
Emergency AD 2006-0103-E - EUROCOPTER - AS 332 L2 Helicopters - Fuselage - Check of Frame 5295 and of the Outer Skin Paneling at the Attachment Points of the MGB Sliding Cowling Rails and of the Attachment of the MGB Suspension Bar Fitting |
| EASA.AD.2006.0104 |
Emergency AD 2006-0104-E R1 - Propeller - 14RF-9 - Blade Inspection for Patch Debonding (Applicable to Hamilton Sundstrand 14RF-9 Propeller) |
| EASA.AD.2006.0105 |
Emergency AD 2006-0105-E - Parachutes de France - Techno 240-B - Equipment - Temporary Grounding of Reserve Parachute |
| EASA.AD.2006.0106 |
Emergency AD 2006-0106-E - AIRBUS - A318, A319, A320 and A321 Aircraft - Fuel - Main Fuel Pump System/Fuel Pumps - Airworthiness Limitation (Superseded by AD 2006-0222 effective July 31, 2006) |
| EASA.AD.2006.0107 |
AD 2006-0107 Wings - Inspection of Wing Shroud Box Bottom Panel (Applicable to AIRBUS A330 and AIRBUS A340-200/-300 Aircraft) |
| EASA.AD.2006.0108 |
AD 2006-0108 - AIRBUS - A318, A319, A320 and A321 Aircraft - Indicating/Recording Systems- Temporary Loss of All Display Units (see PAD-CRD 06-051) |
| EASA.AD.2006.0110 |
AD 2006-0110 - Hoffmann GmbH & Co. KG - Propellers - Possible Hub Failure (see PAD-CRD 06-114) |
| EASA.AD.2006.0111 |
AD 2006-0111 Flight Controls - Flaps - Inspection of Transmission Shaft (Applicable to A310 Aircraft) |
| EASA.AD.2006.0112 |
AD 2006-0112 - Landing Gear - Main Landing Gear (MLG) - Door Actuator (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0113 |
AD 2006-0113 Landing Gear Components - Surface Protection Deficiency - Replacement (Applicable to FALCON 900EX, FALCON 2000, FALCON 2000EX) |
| EASA.AD.2006.0114 |
AD 2006-0114 Ice and Rain Protection-Collapsed Wing Anti-Ice Hoses-Replacement (Applicable to FALCON 10) |
| EASA.AD.2006.0115 |
AD 2006-0115 - Flight Controls - Trailing Edge Flaps Rotating Rods - Inspection/Modification (Applicable to MYSTERE-FALCON 50, MYSTERE-FALCON 900, FALCON 900EX, FALCON 2000, FALCON 2000EX) |
| EASA.AD.2006.0116 |
AD 2006-0116 - Rolls-Royce PLC - RB211 Trent 768-60, 772-60, 772B-60, 772C-60 - Engine - LP Compressor - Blade Annulus Filler Revised Lives |
| EASA.AD.2006.0117 |
AD 2006-0117 - Agusta-Westland - EH-101-510 - Tail Rotor - Tail Rotor Hub - Inspection |
| EASA.AD.2006.0118 |
Emergency AD 2006-0118 E R1 Air Conditioning - Prevention of Zonal Drying System Regeneration Air Duct Overheat (Applicable to Lufthansa Technik AG BOEING 747-430 BOEING 737-700 BOEING 737-800 AIRBUS A330-300 AIRBUS A330-200 BOMBARDIER CL600-2B19) (This AD Superseded by Emergency AD 2006-0140-E) |
| EASA.AD.2006.0120 |
Emergency AD 2006-0120-E Tail Rotor - Flange Assy P/N 109-0131-33-105 of the Tail Rotor Trunnion P/N 109- 0131-30-101 - Check (Applicable to A109S) |
| EASA.AD.2006.0121 |
AD 2006-0121 Exhaust - Inspection of the Exhaust Muffler Part No. 979402 and Part No. 979404 (Applicable to Rotax 914 F Series) |
| EASA.AD.2006.0122 |
AD 2006-0122 Hydraulic Power - RAT (Ram Air Turbine) - Limitation of Aircraft Speed with RAT Deployed (Applicable to A310, A300-600 and A300-600ST Aircraft) |
| EASA.AD.2006.0123 |
AD 2006-0123 Wings - Wing Spar Lower Boom - Inspection/Repair (Applicable to TB 20 and TB 21) |
| EASA.AD.2006.0124 |
AD 2006-0124 - Stabilizers - CFRP (Carbon Fibre Reinforced Plastic) Rudder-Inspection (Applicable to AIRBUS SAS A330 and A340-200/-300 Series Aircraft) |
| EASA.AD.2006.0125 |
AD 2006-0125 - Nacelles/Pylons - Pylon Lateral Panels at Rib 8 Level Near Upper Edge - Inspection (Applicable to AIRBUS A330 Aircraft) |
| EASA.AD.2006.0126 |
Emergency AD 2006-0126-E Equipment and Furnishings - CPT 609 Crash Position Transmitter Beacon (Applicable to AS 365 N - EC 155) |
| EASA.AD.2006.0127 |
AD 2006-0127 - Exhaust - Inspection of the Exhaust Muffler Part No. 979402 and Part No. 979404 (Applicable to BRP-Rotax GmbH and CoKG Rotax 914 F Series) |
| EASA.AD.2006.0128 |
AD 2006-0128 - Landing Gear - Introduction of a Steering Jack With a Modified Gland Housing (Applicable to BAE SYSTEMS (OPERATIONS) LTD HP 137 Jetstream MK 1, Jetstream Series 200, 3100 and 3200) |
| EASA.AD.2006.0129 |
AD 2006-0129 - ATA 05 Time Limits - Safe Life Airworthiness Limitation Items - ALS Part 1 (Applicable to AIRBUS A330 Aircraft) |
| EASA.AD.2006.0130 |
AD 2006-0130 - Time Limits - Safe Life Airworthiness Limitation Items - ALS Part 1 (Applicable to AIRBUS A340 Aircraft) |
| EASA.AD.2006.0131 |
AD 2006-0131 - Landing Gear - Inspection of Nose Landing Gear Capsule for Free Movement and Introduction of Nose Landing Gear With New Shortening Mechanism Bearings (Applicable to BAE SYSTEMS (OPERATIONS) LTD Jetstream 4100) |
| EASA.AD.2006.0132 |
AD 2006-0132 - Electrical Systems - Inspection of Three-Phase Circuit Breakers (Applicable to BAE SYSTEMS (OPERATIONS) LTD BAe 146 (All Series) |
| EASA.AD.2006.0133 |
Emergency AD 2006-0133-E - Rotor Drive - Main Gear Box - Inspection/Replacement (Applicable to AGUSTA S.p.A. EH-101-510) |
| EASA.AD.2006.0134 |
AD 2006-0134 - Electrical Power - Avionics Bus Circuit Breaker Switches - Inspection/Replacement (Applicable to REIMS AVIATION INDUSTRIES F 406) |
| EASA.AD.2006.0135 |
AD 2006-0135 - Hydraulic Power - RAT (Ram Air Turbine) - Speed Limitation When RAT Deployed (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0136 |
AD 2006-0136 - Nacelles/Pylons - Engine Pylon Spar Box Ribs (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0137 |
AD 2006-0137 - Landing Gear - Nose Landing Gear - Introduction of a Revised Axle Spacer (Applicable to BAE SYSTEMS (OPERATIONS) LTD BAe 146 and AVRO 146-RJ (All Series) |
| EASA.AD.2006.0138 |
AD 2006-0138 - Flight Controls - Life Limitation of Lift Spoiler Actuators, Part Numbers P308-45-0002, P308-45-0102 and P308-45-0202 (Applicable to BAE SYSTEMS (OPERATIONS) LTD - BAe 146 and AVRO 146-RJ) |
| EASA.AD.2006.0139 |
AD 2006-0139 - Flight Controls - Inspection of Lift Spoiler Actuators (Applicable to BAE SYSTEMS (OPERATIONS) LTD - BAe 146 and AVRO 146-RJ (All Series) |
| EASA.AD.2006.0140 |
Emergency AD 2006-0140-E - Air Conditioning - Zonal Drying System Deactivation (Applicable to Airbus - Bombardier - Boeing - McDonnell Douglas MD - CTT Systems AB) (This AD Supersedes EASA AD 2006-0018R1-E) |
| EASA.AD.2006.0141 |
AD 2006-0141 - Oil - Replacement of Check-Valve Piston O-Ring (Applicable to TURBOMECA ARRIUS 2F Turboshaft Engine) |
| EASA.AD.2006.0142 |
AD 2006-0142 - Oil - Replacement of Check-Valve Piston O-Ring (Applicable to TURBOMECA ARRIUS 2B and 2K Turboshaft Engines) |
| EASA.AD.2006.0143 |
AD 2006-0143 - Navigation - Pitot/Static Pressure Head - Inspection and Test (Applicable to B-N GROUP LTD BN2, BN2A, BN2B, BN2T, BN2T-4R and BN2T-4S Islander Series, BN2A-MkIII Trislander Series) |
| EASA.AD.2006.0144 |
AD 2006-0144 - Rotors - Blades - Inspection/Modification (Applicable to Sikorsky Aircraft Corporation Sikorsky S58 Series Helicopters) |
| EASA.AD.2006.0145 |
AD 2006-0145 - Flight Manual - Modification (Applicable to Robinson Helicopter Company Robinson R44 Series) |
| EASA.AD.2006.0146 |
AD 2006-0146 - Engine Indicating - Tests of Torquemeter Printed Circuit Boards (PCBs) (Applicable to EUROCOPTER EC 225 LP) |
| EASA.AD.2006.0147 |
AD 2006-0147 Doors - Over Wing Emergency Exit - Inspection (Applicable to DASSAULT AVIATION FALCON 10) |
| EASA.AD.2006.0148 |
AD 2006-0148 Doors - Over Wing Emergency Exit - Inspection (Applicable to DASSAULT AVIATION FALCON 2000 - FALCON 2000EX FALCON 2000EX (version F2000EX EASy)) |
| EASA.AD.2006.0149 |
AD 2006-0149 Doors - Over Wing Emergency Exit - Inspection (Applicable to DASSAULT AVIATION MYSTERE-FALCON 50 - MYSTERE-FALCON 900 FALCON 900EX FALCON 900EX (version F900EX EASy)) |
| EASA.AD.2006.0150 |
AD 2006-0150 R1 Horizontal Stabilizer - Elevator Attachment Bolt Replacement (Applicable to GROB Luft- und Raumfahrt ASTIR CS) |
| EASA.AD.2006.0151 |
AD 2006-0151 - Maintenance Checks - Unscheduled Check of the Exhaust System for Cracks and Deformations - Inspection/Replacement (Applicable to AQUILA GmbH AQUILA AT01) |
| EASA.AD.2006.0152 |
AD 2006-0152 - Landing Gear - Modification to the Electro-Valve Power Supply (Applicable to EUROCOPTER AS 332 C, C1, L and L1 Helicopters) |
| EASA.AD.2006.0153 |
AD 2006-0153 - Auxiliary Power Unit (APU) - Starter Motor and Air Intake System - Inspection/Cleaning (Applicable to AIRBUS SAS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0154 |
AD 2006-0154 - Engine and Fuel Control - Fuel Pipe (PN 0 202 12 800 0) - Inspection (Applicable to TURBOMECA ARTOUSTE III B and III B1 Turboshaft Engines) |
| EASA.AD.2006.0155 |
AD 2006-0155 Electrical Power, Nacelles/Pylons - CF6-80C2 Engine Pylon - Inspection of Forward Pyramid and Feeder Harness (Applicable to AIRBUS SAS A310, A300-600 and A300-600ST Aircraft) |
| EASA.AD.2006.0156 |
AD 2006-0156 Doors - Over Wing Emergency Exit - Inspection (Applicable to DASSAULT AVIATION FAN JET FALCON all series - MYSTERE- FALCON 20-()5 MYSTERE-FALCON 20GF - MYSTERE-FALCON 200) |
| EASA.AD.2006.0157 |
AD 2006-0157 Navigation - Segregation of ADC/IRS Wiring - Modification (Applicable to DASSAULT AVIATION FALCON 2000EX (version F2000EX EASy); FALCON 900EX (version F900EX EASy and F900DX)) |
| EASA.AD.2006.0158 |
AD 2006-0158 Flight Controls - Spoiler Servo-controls - Life limitations (Applicable to AIRBUS A340-200/-300 Series) |
| EASA.AD.2006.0159 |
AD 2006-0159 Flight Controls - Spoiler Servo-controls - Life limitations (Applicable to AIRBUS A330 Aircraft) |
| EASA.AD.2006.0160 |
Emergency AD 2006-0160 E Equipment - Reserve Parachute - Mandatory Packing Modifications, Slider and Steering Lines Replacement (Applicable to Parachutes de France Techno 240) |
| EASA.AD.2006.0161 |
AD 2006-0161 Exhaust - Thrust Reverser - Upper and Lower Track Beam Lugs Inspection (Applicable to AIRBUS A310 and A300-600 Aircraft) |
| EASA.AD.2006.0162 |
AD 2006-0162 Safe Life Airworthiness Limitation Items - ALS Part 1 (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0163 |
AD 2006-0163 Fuselage - Main Gearbox (MGB) Suspension Bar Attaching Fittings (Applicable to EUROCOPTER AS 332 L2 and EC 225 LP) |
| EASA.AD.2006.0164 |
AD 2006-0164 Equipment/Furnishings - Untimely Firing of Squibs on GOODRICH Electric Hoists (Applicable to EUROCOPTER AS 350 and AS 355) |
| EASA.AD.2006.0165 |
AD 2006-0165 Airworthiness Limitation Items (ALI) - Structural Maintenance (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0166 |
AD 2006-0166 Doors - Hinges - Modification (Applicable to Robinson Helicopter Company R44) |
| EASA.AD.2006.0167 |
AD 2006-0167 Doors - Hinges - Modification (Applicable to Robinson Helicopter Company R22) |
| EASA.AD.2006.0168 |
AD 2006-0168 Flight Controls/Time Limits - Replacement (Applicable to MD Helicopters Inc. (MDHI) MD 600N) |
| EASA.AD.2006.0169 |
Emergency AD 2006-0169-E Rotor(s) - Main Rotor Hub Dome Fairing Attachment Screws (Applicable to EUROCOPTER EC 225 LP) |
| EASA.AD.2006.0170 |
AD 2006-0170 Time Limits - Replacement (Applicable to Brantly International, Inc. Brantly (Hynes) Series Helicopters) |
| EASA.AD.2006.0171 |
AD 2006-0171 R1 Fuel - Fuel Vent System - Modification (Applicable to Schweizer Aircraft Corporation Schweizer (Hughes) 269 Series) |
| EASA.AD.2006.0172 |
AD 2006-0172 R1 Tail Rotor - Blade Grip - Inspection and Rework (Applicable to Enstrom Helicopter Corporation F-28A and 280 Helicopters) |
| EASA.AD.2006.0173 |
AD 2006-0173 Auto Flight - Auto Pilot - Modification (Applicable to Bell Helicopter Textron Inc. Bell 212) |
| EASA.AD.2006.0174 |
AD 2006-0174 Landing Gear - Nose Landing Gear - Wheels at 90 Degrees (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0175 |
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.AD.2006.0176 |
AD 2006-0176 Fuel system - Prevention against Explosion Risks - In Tank Bonding (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0177 |
AD 2006-0177 Fuselage - Inspection of the Lower Gantry Flanges between FR47 and FR54 (Applicable to AIRBUS SAS A300, A300-600 Aircraft) |
| EASA.AD.2006.0178 |
AD 2006-0178 Landing Gear - Parking Emergency Braking (Applicable to AIRBUS SAS A300, A310, A300-600 and A300-600ST Aircraft) |
| EASA.AD.2006.0179 |
AD 2006-0179 Wings - Inner Flap Inspection and Modification (Applicable to AIRBUS SAS A300, A300-600 and A300-600ST Aircraft) |
| EASA.AD.2006.0180 |
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.AD.2006.0181 |
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.AD.2006.0182 |
AD 2006-0182 Engine Turbine Section - High Pressure Turbine - Inspection (Applicable to ROLLS-ROYCE PLC RB211-535) |
| EASA.AD.2006.0183 |
Emergency AD 2006-0183-E Engine Controls - Twist Grip Assembly -Inspection/Replacement (Applicable to EUROCOPTER AS 350 Helicopters) |
| EASA.AD.2006.0184 |
AD 2006-0184 Equipment/Furnishings - Semi Automatic Cargo Loading - Modification of Fixed YZ Latches (Applicable to AIRBUS A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0185 |
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.AD.2006.0186 |
AD 2006-0186 Fuel - Prevention Against Fuel Tank Explosion Risk-Adjacent Systems (Applicable to ATR ATR 42 and ATR72 Aircraft) |
| EASA.AD.2006.0187 |
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/-600 Aircraft) |
| EASA.AD.2006.0188 |
AD 2006-0188 Landing Gear - Main Landing Gear Legs - Inspection/Replacement (Applicable to ISSOIRE AVIATION APM 20) |
| EASA.AD.2006.0189 |
AD 2006-0189 Landing Gear - Wheels and Brakes - Master Cylinder Yoke - Inspection/Replacement (Applicable to EADS SOCATA TBM 700) |
| EASA.AD.2006.0190 |
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) |
| EASA.AD.2006.0191 |
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.AD.2006.0192 |
AD 2006-0192 Lights - Anti-collision Lights, Wing- & Tail Strobe Lights - Modification (Applicable to Fokker Aircraft B.V. Model F28 Mark 0100 Aircraft) |
| EASA.AD.2006.0193 |
AD 2006-0193 Equipment & Furnishings - Passenger Service Unit - Inspection/Modification (Applicable to Fokker Aircraft B.V. Model F27 Mark 050 and 0502 Aircraft) |
| EASA.AD.2006.0194 |
AD 2006-0194 Fuselage - Bottom Skin Chine Line - Inspection/Repair (Applicable to Fokker Aircraft B.V. Model F27 Mark 050 Aircraft) |
| EASA.AD.2006.0195 |
AD 2006-0195 Auto Flight - Autopilot Disconnect Unit - Installation (Applicable to Fokker Aircraft B.V. Model F28 Mark 0070 and Mark 0100 Aircraft) |
| EASA.AD.2006.0196 |
AD 2006-0196 Indicating/Recording Systems - Periodic Reset and Modification of Display Units (Applicable to AIRBUS SAS A330 and A340 Aircraft) |
| EASA.AD.2006.0197 |
AD 2006-0197 Fuel Tank Safety Fuel Airworthiness Limitations (FAL) (Applicable to AvCraft Aerospace GmbH Dornier 328 Aircraft) |
| EASA.AD.2006.0198 |
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.AD.2006.0199 |
AD 2006-0199 Fuel - Fuel Tank Safety Fuel Airworthiness Limitations (FAL) (Applicable to Saab AB, Saab Aerosystems SAAB 2000) |
| EASA.AD.2006.0200 |
AD 2006-0200 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A300 Aircraft) |
| EASA.AD.2006.0201 |
AD 2006-0201 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A300-600, A300-600ST Aircraft) |
| EASA.AD.2006.0202 |
AD 2006-0202 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A310 Aircraft) |
| EASA.AD.2006.0203 |
AD 2006-0203 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A318/A319/A320/A321 Aircraft) |
| EASA.AD.2006.0204 |
AD 2006-0204 Fuel - Fuel Tank Safety ALS Part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A330 Aircraft) |
| EASA.AD.2006.0205 |
AD 2006-0205 Fuel - Fuel Tank Safety ALS part 5 - Fuel Airworthiness Limitations (FAL) (Applicable to AIRBUS A340 Aircraft) |
| EASA.AD.2006.0206 |
AD 2006-0206 Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to Fokker Services B.V. F28 Mk 0070/0100 Aircraft) |
| EASA.AD.2006.0207 |
AD 2006-0207 Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to Fokker Services B.V. F27 Mk 200/300/400/500/600/700 Aircraft) |
| EASA.AD.2006.0208 |
AD 2006-0208 Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to Fokker Services B.V. F28 Mk 1000/2000/3000/4000 Aircraft) |
| EASA.AD.2006.0209 |
AD 2006-0209 Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to Fokker Services B.V. F27 Mk 0050/0502/0604 Aircraft) |
| EASA.AD.2006.0210 |
Emergency AD 2006-0210-E Wing Main Spar - Inspection of the Upper Cap (Applicable to APEX AIRCRAFT CAP231, CAP20L, CAP21) |
| EASA.AD.2006.0211 |
Emergency AD 2006-0211R1-E Return to Flight - Fuselage/Wings - Modification/Reinforcement (Applicable to APEX AIRCRAFT CAP 230, CAP 231, 231EX and CAP232) |
| EASA.AD.2006.0212 |
Emergency AD 2006-0212-E Engine - Icing Conditions During Descent - Operational Procedure (Applicable to AIRBUS SAS A330 Aircraft) |
| EASA.AD.2006.0213 |
AD 2006-0213 Landing Gear - Optional Ski Installation (Applicable to EUROCOPTER AS 365 N) |
| EASA.AD.2006.0214 |
AD 2006-0214 Indicating System/Rotor Drive - Main Gear Box - Low Oil Pressure Warning (Applicable to EUROCOPTER EC 155) |
| EASA.AD.2006.0215 |
AD 2006-0215 Fuselage - Inspection of Longeron at Rib '0' (Applicable to BAE SYSTEMS (OPERATIONS) LTD BAe 146 (All Series) |
| EASA.AD.2006.0216 |
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.AD.2006.0217 |
Emergency AD 2006-0217-E Exhaust-System - Inspection of Exhaust-System for Cracks (Applicable to STEMME AG STEMME S 10) |
| EASA.AD.2006.0218 |
Emergency AD 2006-0218-E Required Placard - Flight Envelope Limitation of Never Exceed Speed Vne (Applicable to BINDER MOTORENBAU GMBH ASH 25 EB 28) |
| EASA.AD.2006.0219 |
AD 2006-0219 Fuel - Fuel Tank Safety Fuel Airworthiness Limitations (Applicable to ATR; ATR 42 and 72 Aircraft) |
| EASA.AD.2006.0220 |
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.AD.2006.0221 |
AD 2006-0221 Fuel - Fuel Tank Safety Fuel Airworthiness Limitations (FAL) (Applicable to SAAB AB, SAAB Aerosystems SAAB SF340A and SAAB 340B) |
| EASA.AD.2006.0222 |
AD 2006-0222 Fuel - Main Fuel Pump System/Fuel Pumps (Applicable to AIRBUS A318, A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0223 |
AD 2006-0223 Flight Controls - Trimmable Horizontal Stabilizer Act (Applicable to AIRBUS A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0224 |
AD 2006-0224 Time Limits - Airworthiness Limitations - Certification Maintenance Requirements (CMR) (Applicable to AIRBUS SAS A330 Aircraft) |
| EASA.AD.2006.0225 |
AD 2006-0225 Time Limits - Airworthiness Limitations - Certification Maintenance Requirements (CMR) (Applicable to AIRBUS SAS A340 Aircraft) |
| EASA.AD.2006.0226 |
Emergency AD 2006-0226-E Landing Gear - Nose Landing Gear Actuator Hinge Pin - Inspection/Replacement (Applicable to EADS SOCATA TBM 700 A & B) |
| EASA.AD.2006.0227 |
Emergency AD 2006-0227-E Power Plant - Engine Mount Structure (Pylon) (Applicable to Schempp-Hirth Flugzeugbau GmbH Ventus-2cT; Discus-2T, Discus-2cT) |
| EASA.AD.2006.0228 |
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.AD.2006.0229 |
Emergency AD 2006-0229-E Limitations - Change of Aircraft Flight Manual Supplement (Applicable to ADEFA, AVIALSA, BAQUERO SERVISIOS AEREOS, MARTIN ECHEVARRIA, MARTINEZ RIDAO PZL-M18, -M18A) |
| EASA.AD.2006.0230 |
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.AD.2006.0231 |
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) |
| EASA.AD.2006.0232 |
AD 2006-0232 Navigation - Inertial Reference Systems (Applicable to AIRBUS SAS A330 Aircraft and A340-200/-300 Series Aircraft) |
| EASA.AD.2006.0233 |
Emergency AD 2006-0233-E Tail Rotor - Internal Bracket Replacement (Applicable to Agusta S.p.a. EH101-510) |
| EASA.AD.2006.0234 |
AD 2006-0234 Equipment and Furnishings - Seat Rail Stops - Inspection (Applicable to Costruzioni Aeronautiche Tecnam P92-J, P92-JS and P2002-JF) |
| EASA.AD.2006.0235 |
Emergency AD 2006-0235-E Tail Rotor - Tail Rotor Blade Skin - Check (Applicable to EUROCOPTER AS 350 and AS 355 Helicopters) |
| EASA.AD.2006.0236 |
AD 2006-0236 Fuel, Wings - Fuel system - Labels in Fuel Tank (Applicable to AIRBUS A319 and A320 Aircraft) |
| EASA.AD.2006.0237 |
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.AD.2006.0238 |
AD 2006-0238 R2 Time Limits - Engine Critical Part Lives (Applicable to ROLLS-ROYCE plc RB211 Trent 800 Series Engines) |
| EASA.AD.2006.0239 |
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) |
| EASA.AD.2006.0240 |
Emergency AD 2006-0240-E Engine - Flexible Lubrication Pipe Between Tank and Cooler - Inspection (Applicable to TURBOMECA TURMO IV) |
| EASA.AD.2006.0241 |
AD 2006-0241 Navigation - Automatic Deployable Emergency Locator Transmitter (ADELT) and Automatic Deployable/Automatic Fixed Emergency Locator Transmitter (AD/AFELT) (Applicable to CALEDONIAN AIRBORNE SYSTEMS CPT-600 Series/CPT-900 Series ADELT and AD/AFELT) |
| EASA.AD.2006.0242 |
Emergency AD 2006-0242-E Exhaust - Tailpipe Assy LH P/N 3G7800L00131 and Tailpipe Assy RH P/N 3G7800L00231 - Inspection (Applicable to Agusta S.p.A. AB139) |
| EASA.AD.2006.0243 |
Emergency AD 2006-0243-E Flight Controls - Rudder Attachment - Inspection/Replacement (Applicable to ALLSTAR PZL GLIDER Sp. z o.o. SZD-50-3 PUCHACZ) |
| EASA.AD.2006.0244 |
AD 2006-0244 Rotor Flight Controls - Collective Lever Control (Applicable to EUROCOPTER AS 332 L2 and EC 225 LP Helicopters) |
| EASA.AD.2006.0245 |
AD 2006-0245 Rotor(s) - Bushes Installed on Starflex Star Arm Ends (Applicable to EUROCOPTER AS 365 N, SA 366 and SA 365C Helicopters) |
| EASA.AD.2006.0246 |
AD 2006-0246 Electrical Power - Battery Overheat Sensing Circuit Wiring (Applicable to EUROCOPTER EC 130 Helicopters) |
| EASA.AD.2006.0247 |
AD 2006-0247 Rotor Flight Controls - Tail Servo-Control (Applicable to EUROCOPTER AS 350 Helicopters) |
| EASA.AD.2006.0248 |
AD 2006-0248 Equipment and Furnishings - Emergency Flotation Gear - All-Up Operating Weight Limitation (Applicable to EUROCOPTER AS 350 Helicopters) |
| EASA.AD.2006.0249 |
AD 2006-0249 Doors - Sliding Door - Wear on Rollers and Rails (Applicable to EUROCOPTER AS 350 and 355 Helicopters) |
| EASA.AD.2006.0250 |
AD 2006-0250 Main Rotor Drive - Main Gearbox (MGB) Free-Wheel (Applicable to EUROCOPTER AS 355 Helicopters) |
| EASA.AD.2006.0251 |
AD 2006-0251 R1 Doors - Sliding Door Rear Roller Support Shaft and Rear Fitting (Applicable to EUROCOPTER AS 350 AND AS 355 Helicopters) |
| EASA.AD.2006.0252 |
AD 2006-0252 Equipment and Furnishings - Hoist Operator's Belt Snap Hook (Applicable to EUROCOPTER SA 330, AS 332, SA 341/342, AS 350, AS 355, SA 360, SA 365, AS 365, EC 155, SE 3160 and SA 316/319 Helicopters) |
| EASA.AD.2006.0253 |
AD 2006-0253 Engine Controls - Twist Grip Assembly (Applicable to EUROCOPTER EC 120 Helicopters) |
| EASA.AD.2006.0254 |
AD 2006-0254 Starting - Starter Generator Vibration (Applicable to EUROCOPTER AS 355N Helicopters) |
| EASA.AD.2006.0255 |
AD 2006-0255 Engine Controls - Engine Control Selector Switch Guard on Panel 12 ALPHA (Applicable to EUROCOPTER AS 365 N Helicopters) |
| EASA.AD.2006.0256 |
AD 2006-0256 Engine Controls - Engine Control Selector Switch Guard on Panel 12 ALPHA (Applicable to EUROCOPTER EC155 Helicopters) |
| EASA.AD.2006.0257 |
AD 2006-0257 Fuselage - Wing-to-Fuselage Junction Taperlocks - Inspection (Applicable to AIRBUS SAS A300-600 Series Airplanes) |
| EASA.AD.2006.0258 |
Revised Emergency AD 2006-0258 R1-E Tail Rotor - Tail Gearbox Oil Level and Tail Rotor Pitch Control Rod Bearing - Inspection/Replacement (Applicable to EUROCOPTER AS 365 N, SA 366 and EC 155 Series) (This AD Supersedes EASA AD 2006-0051-E) |
| EASA.AD.2006.0259 |
Emergency AD 2006-0259-E Engine - Icing Conditions During Descent - Operational Procedure and Dispatch Restriction (Applicable to AIRBUS A330 Aircraft) |
| EASA.AD.2006.0260 |
AD 2006-0260 Airworthiness Limitations- Structural Maintenance (Applicable to AIRBUS SAS A310 Aircraft) |
| EASA.AD.2006.0261 |
Emergency AD 2006-0261-E Oxygen - Oxygen Cylinders - Removal/Emptying (Applicable to EUROCOPTER AS 350 and SA 315 Helicopters) (Superseded by AD 2006-0286) |
| EASA.AD.2006.0262 |
AD 2006-0262 Stabilizers - Rudder Actuator Fittings - Replacement (Applicable to AIRBUS A320 Aircraft) |
| EASA.AD.2006.0263 |
AD 2006-0263 Landing Gear - MLG Shock Strut & Axle Adaptors - Inspection/Modification (Applicable to Saab AB, Saab Aerosystems SAAB SF340A and SAAB 340B Aircraft) |
| EASA.AD.2006.0264 |
AD 2006-0264 Equipment & Furnishings - Passenger Seats Rear Fitting Assembly Attachment - Replacement (Applicable to AVIOINTERIORS S.p.A. Passengers Seats, Various Part Numbers) |
| EASA.AD.2006.0265 |
AD 2006-0265 Navigation Systems - Mode S and C Transponders - Check (Applicable to Various Mode 'C' and Mode 'S' Transponder Systems Utilising Gilham Code Altitude Input) |
| EASA.AD.2006.0266 |
AD 2006-0266 Fuselage - Frame 53.3 Circumferential Joint - Reinforcement (Applicable to AIRBUS SAS A330 Aircraft) |
| EASA.AD.2006.0267 |
AD 2006-0267 Stabilizers - Horizontal and Vertical Stabilizer Attachment - Inspection/Replacement (Applicable to Cessna Aircraft Company (Previously held by REIMS AVIATION) F150, FA150, FRA150, F152 and FA152 Series) |
| EASA.AD.2006.0268 |
Emergency AD 2006-0268-E Engine Fuel and Control - Engine Electronic Controller (EEC) - Inspection/Replacement (Applicable to Rolls-Royce Deutschland Ltd & Co. KG TAY 620/Tay 611-8C Engines) |
| EASA.AD.2006.0269 |
AD 2006-0269 Navigation Systems - Mode S Transponder - Modification (Applicable to Honeywell International Inc. MST 67A Mode 'S' Transponder) |
| EASA.AD.2006.0270 |
AD 2006-0270 Electrical Power - Feeder at Frames 22/23 - Inspection/Protection/Repair (Applicable to DASSAULT AVIATION Mystere-Falcon 900 & Falcon 900EX) |
| EASA.AD.2006.0271 |
Emergency AD 2006-0271-E Landing Gear - Nose Landing Gear Actuator Hinge Pin - Inspection/Replacement (Applicable to EADS SOCATA TBM 700 A & B) |
| EASA.AD.2006.0272 |
AD 2006-0272 Engine Controls - Twist Grip Assembly - Inspection/Modification (Applicable to EUROCOPTER EC 130 B4 Helicopters) |
| EASA.AD.2006.0273 |
AD 2006-0273 Fuselage - RH Cabin Vibration Damper & Blade - Inspection/Replacement/Modification (Applicable to EUROCOPTER AS 350 and AS 355 Helicopters) |
| EASA.AD.2006.0274 |
AD 2006-0274 Electrical Power - Switches - Inspection/Replacement (Applicable to Carling Technologies, Inc. Rocker-type Switches, Part Number (P/N) TA 201TBW) |
| EASA.AD.2006.0275 |
AD 2006-0275 Stabilizers - Vertical Fin Supports - Inspection (Applicable to Agusta S.p.a. AB206A and AB206B Helicopters) |
| EASA.AD.2006.0276 |
AD 2006-0276 Ice & Rain Protection - Wing Anti-Ice Telescopic Tubes - Modification (Applicable to DASSAULT AVIATION FALCON 2000) |
| EASA.AD.2006.0277 |
AD 2006-0277 Engine - Propeller System Check Valve Bracket - Installation (Applicable to Diamond Aircraft Industries GmbH DA42) |
| EASA.AD.2006.0278 |
AD 2006-0278 Fuselage - Cabin Vibration Dampers - Inspection / Modification (Applicable to Eurocopter EC130 Helicopters) |
| EASA.AD.2006.0279 |
AD 2006-0279 Equipment/Furnishings - Parachute Equipment - Removal from Service (Applicable to PARACHUTE SHOP Parachute Harnesses and Reserve Canopies) |
| EASA.AD.2006.0280 |
AD 2006-0280 Electrical Power, Engine - Integrated Drive Generator Connector on IAE V2500 Engine - Operational Procedure (Applicable to AIRBUS A319, A320 and A321 Aircraft) |
| EASA.AD.2006.0281 |
AD 2006-0281 Fuselage - Upper Longeron at Horizontal Stabilizer - Inspection/Modification (Applicable to EXTRA Flugzeugproduktions - und Vertriebs-GmbH EA300) |
| EASA.AD.2006.0282 |
AD 2006-0282 Wings - Lower Skin Panel No. 2 Inboard of Rib 9 - Inspection (Applicable to AIRBUS A300 and A300-600 Aircraft) |
| EASA.AD.2006.0283 |
AD 2006-0283 Electrical Power - 120 VU Electrical Harness - Inspection (Applicable to ATR 42 and ATR 72 Aircraft) |
| EASA.AD.2006.0284 |
AD 2006-0284 Electrical Power - Prevention against Explosion Risks - Fuel Pump Wiring - Modification (Applicable to AIRBUS A300, A310 and A300-600 Aircraft) |
| EASA.AD.2006.0285 |
AD 2006-0285 Ageing Transport Systems Rulemaking Advisory Committee (ATSRAC) Aged Aircraft Design Improvements And Inspection Against Potential Unsafe Conditions (Applicable to AIRBUS SAS A310 and A300-600 Aircraft) |
| EASA.AD.2006.0286 |
Emergency AD 2006-0286-E Oxygen - Oxygen Reserve Cylinders - Removal/Emptying (Applicable to INTERTECHNIQUE, Zodiac Aircraft Systems Oxygen Reserve Cylinders) (This AD Supersedes AD 2006-0261) |
| EASA.AD.2006.0287 |
AD 2006-0287 Fuel, Indicating & Recording System - Fuel Control and Monitoring System ( FCMS) and Flight Warning Computer (FWC) - Modification (Applicable to AIRBUS SAS Aircraft A340-500/600 Series) |
| EASA.AD.2006.0288 |
AD 2006-0288 Engine - Low Pressure Turbine Discs Stage 2 and 3 - Inspection/Replacement (Applicable to Rolls-Royce Deutschland Ltd & Co KG TAY 650 / TAY 650-15) |
| EASA.AD.2006.0290 |
AD 2006-0290 Time Limits / Maintenance Checks - Life Limited Components - Replacement (Applicable to Enstrom Helicopter Corporation Enstrom 480 Series Helicopters) |
| EASA.AD.2006.0291 |
AD 2006-0291 Fuel System - Prevention against Explosion Risks- FQIS wiring - Modification (Applicable to AIRBUS SAS A310 Aircraft) |
| EASA.AD.2006.0292 |
AD 2006-0292 Tail Rotor - Pitch Link & Pitch Arm Plate - Inspection/Replacement (Applicable to Enstrom Helicopter Corporation Enstrom F-28 and 280 Series Helicopters) |
| EASA.AD.2006.0293 |
Emergency AD 2006-0293-E Tail Rotor - Pitch Horn - Inspection / Rework / Repair (Applicable to AGUSTA S.p.A. EH-101-510) |
| EASA.AD.2006.0294 |
Emergency AD 2006-0294-E Propellers - Propeller Hub - Inspection / Overhaul (Applicable to Schempp-Hirth Flugzeugbau GmbH Duo Discus T and Nimbus 4DT) |
| EASA.AD.2006.0295 |
Emergency AD 2006-0295-E Engine - Contamination of the Engine Fuel System - Inspection (Applicable to Diamond Aircraft Industries GmbH DA 40) |
| EASA.AD.2006.0297 |
AD 2006-0297 Fire Protection - Engine Fire Extinguishing Bottle Pipe - Inspection (Applicable to AIRBUS SAS A330 Aircraft) |
| EASA.AD.2006.0298 |
AD 2006-0298 Exhaust - Thrust Reverser Outer Fixed Structure - Modification (Applicable to AIRBUS SAS Aircraft A340-200/-300 Series) |
| EASA.AD.2006.0299 |
AD 2006-0299 Equipment/Furnishings - CPI (Crash Position Indicator) ELT Interface Unit - Repair/Replacement (Applicable to EUROCOPTER AS 332 L2 and EC 225 LP Helicopters) |
| EASA.AD.2006.0300 |
AD 2006-0300 Equipment / Furnishings - CPI (Crash Position Indicator) ELT Water-activated Switch - Replacement (Applicable to EUROCOPTER AS 332 L2 and EC 225 LP Helicopters) |