145 results found (3171ms)
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: A hollow pin cap on the right-side engine aft thrust strut mount interface was found broken due to a missing sleeve bushing.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: failure of principal structural elements throughout the service life of each part, which could compromise the structural integrity of the airplane.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: Failure of principal structural elements throughout the service life of each part, which could compromise the structural integrity of the airplane.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: Cracking and corrosion in the electrical grounding receptacles located on the left and right wings.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: A partially disengaged rear engine mount was discovered on an in-service Model GVII-G600 airplane due to the upper, aft engine mount fastener migrating out of position in the pylon area. The cause ...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: The ignition of flammable vapors in the fuel tank as a result of frictional heating or sparks caused by a missing, misplaced, or dislodged impeller shaft key inside the fuel boost pump.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: The unsafe condition, if not addressed, could result in the flaps being jammed in position, if fracture occurred. Additional failures in the flap actuator force limiter, or flap yoke actuator disco...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: inappropriate alpha limiter engagement during the landing flare, which can limit pilot pitch authority during a critical phase of flight near the ground, and result in a high rate of descent landin...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: The ground spoiler actuator installation does not preclude improper hydraulic line connections that could result in unintended asymmetrical spoiler deployment.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation 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; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: A main landing gear (MLG) trunnion pin remaining in service beyond its life limit could lead to fracture and failure of the trunnion pin. This condition, if not addressed, could result in MLG failu...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: corrosion of the horizontal stabilizer lower bonded skin assemblies
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: Inappropriate alpha limiter engagement during the landing flare, which can limit pilot pitch authority during a critical phase of flight near the ground, and result in a high rate of descent landin...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: moisture from entering the nose steering wheel servo valve, which could freeze and cause an un-commanded nose wheel steering position during touchdown.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: The omission of a life limit in the airworthiness limitations section (ALS) for a certain main landing gear (MLG) trunnion pin. The FAA is issuing this AD to prevent a MLG trunnion pin from remaini...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: flap yoke fittings with design features that cause decreased fatigue life
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: Seizure of the lower bushing in the floor beam support links at RBL 6, FS 499, 531, and 569.5, resulting in bending stress and potential failure of the link, which may compromise the integrity of t...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: A misassembled fuel boost pump could result in a woodruff key becoming dislodged and causing friction between static and rotating components internal to the fuel boost pump. This friction could gen...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: The primary flight control actuation system (PFCAS) linear variable displacement transducer (LVDT) mechanical disconnect monitor may not trigger the disconnect of the affected control surfaces as r...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: The supplier compromised the seals during assembly of the electro-hydraulic servo valves, which allows moisture to enter the valve. During cold soak conditions, the moisture forms ice crystals in t...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: The alpha limiter can engage even when the airplane is not near a critical angle of attack and limit the pilot's pitch authority in the flare, resulting in a landing at a high rate of descent.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: Loss of flight control surface protection could lead to loss of structural integrity of the airplane and loss of control of the airplane.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: An unstable rudder hinge moment when the aircraft is in a sideslip condition, combined with a rudder surface shutdown, which is inherent to the GVI aircraft type design.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: detect and correct fatigue cracking of principal structural elements (PSEs) to prevent reduced structural integrity of a PSE or critical component and loss of control of the airplane.
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
Unsafe Condition: Loss of bi-directional (Transmit/Receive) BD429 communication between the REU and the FCC due to wire/connector failures, which can result in the display of a cyan ``FCS MAINTENANCE REQUIRED'' advi...
Why matched: Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes
