560 results found (1465ms)
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: fatigue damage of various airplane structures and failure of certain structurally significant items, which could result in reduced structural integrity of the airplane, and fuel vapor ignition sour...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes
Unsafe Condition: unsafe condition.
Why matched: Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes
Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes
Unsafe Condition: Wings
Why matched: Airworthiness Directives; BAE SYSTEMS (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: Cracking on the radius of the rib 0 forward longeron at frame 26, which could lead to failure of adjacent structure, fuselage skin failure, and potential rapid decompression or loss of the airplane.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: cracking on the shoulders of an MLG side stay outer link, which could lead to failure of the MLG side stay outer link and MLG collapse, resulting in a runway departure and the engine or wing contac...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: in-service cracking of the passenger door edge member, seal carrier, and inner skin, adjacent to the roller guide bracket
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; Transport and Commuter Category Airplanes
Unsafe Condition: Radio altimeter anomalies that are undetected by the automation or pilot, particularly close to the ground (e.g., landing flare), could lead to loss of continued safe flight and landing. Additional...
Why matched: Airworthiness Directives; Transport and Commuter Category Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: IRUs having outdated MagVar lookup tables, which could lead to inaccurate inertial reference system calculations, possibly resulting in increased risk of controlled flight into terrain, or collisio...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: unsafe condition.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: fatigue damage of various airplane structures and failure of certain structurally significant items, which could result in reduced structural integrity of the airplane, and fuel vapor ignition sour...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: When the autopilot is engaged, the architecture of the autopilot system does not automatically disconnect the autopilot in response to pilot application of a pitch input or when the electric pitch ...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes; Correction
Unsafe Condition: Reports of cracking on the shoulders of a main landing gear (MLG) side stay outer link.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes; Correction
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: Cracking, corrosion, and other defects on the rear fuselage aft skin joints and frames and in the fuselage panels, which could affect the structural integrity of the airplane.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: insufficient bonding of the crossfeed valve in the fuel tank area, which, if not corrected, could lead to ignition of fuel vapors and subsequent fuel tank explosion.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes
Unsafe Condition: Cracks were found during early fatigue testing and in service on the main landing gear (MLG) main fitting at the pintle to cylinder interface. This condition, if not detected and corrected, could l...
Why matched: Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes
Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes
Unsafe Condition: stress corrosion cracking of the primary flight control cable terminals
Why matched: Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: fatigue cracking of certain structural elements, which could adversely affect the structural integrity of the airplane.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes
Unsafe Condition: A bent control rod within the gust lock system may enable both power levers to be pushed into the flight range with the gust lock lever fully engaged.
Why matched: Airworthiness Directives; British Aerospace (Operations) Limited and British Aerospace Regional Aircraft Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: heat damage of the printed circuit boards (PCBs) for power units LE 10 and LE 22 (Illustrated Parts Catalog (IPC) 33-50-00) could lead to battery discharge and possibly result in lack of power supp...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; Zodiac Aero Evacuation Systems (Also Known as Air Cruisers Company) Airplanes
Unsafe Condition: Reports indicating that affected fusible plugs activated (vented gas) below the rated temperature.
Why matched: Airworthiness Directives; Zodiac Aero Evacuation Systems (also known as Air Cruisers Company)
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: cracking in fuselage frame 90, which could cause it to fail and thereby compromise the structural integrity of the aircraft pressure hull; and fatigue damage of various airplane structures, which c...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: During scheduled maintenance, it was noted that on the extinguisher cartridge, the blue spacer around the electrical pins appeared to be located too far forward. It was discovered that, inadvertent...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: Fatigue cracking of certain structural elements, which could adversely affect the structural integrity of the airplane.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Airworthiness Directives; BAE Systems (Operations) Limited
Unsafe Condition: Cracking and surface anomalies (bulges and/or dents) of the fuselage skin at the water trap/air drier unit of the forward discharge valve, located between fuselage frame (FR) 22 and FR23 and betwee...
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Unsafe Condition: Cracking in the wing rear spar, initiated at adjacent fastener bores in the rear spar upper boom and progressing into the rear spar web, due to fatigue.
Why matched: Airworthiness Directives; BAE Systems (Operations) Limited Airplanes