139 results found (869ms)
Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: cracks on the vertical stabilizer attachment fitting which, if not addressed, could result in reduced structural integrity of the vertical stabilizer.
Why matched: Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: certain emergency procedures in the existing pilot's operating handbook (POH) that cannot be fully accomplished since certain equipment cannot be disconnected by the pilot(s) from the flight deck.
Why matched: Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: wear of the inner flap actuator drive nut, which could result in improper play between the actuator threaded rod and the drive nut, and potential loss of flap control and consequent reduced or loss...
Why matched: Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: chafing and cracking of the nose landing gear (NLG) wheel axle, which could lead to failure of the NLG with consequent damage to the airplane and/or injury to occupants.
Why matched: Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: interference between the emergency exit trim panel and the upholstery panel, which could result in additional effort required to open the emergency exit door
Why matched: Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; Various Airplanes
Unsafe Condition: The displayed fuel quantity can have an error as much as four gallons/fuel tank with the display indicating four gallons with an empty tank. In the context of this event, the end level effect is th...
Why matched: Airworthiness Directives; Various Airplanes
Airworthiness Directives; Daher Aerospace (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: ice accumulation on the oil cooler air inlet duct fin
Why matched: Airworthiness Directives; Daher Aerospace (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; Daher Aerospace (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: cracks on the main landing gear (MLG) legs
Why matched: Airworthiness Directives; Daher Aerospace (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; Daher Aerospace (Type Certificate Previously Held by SOCATA) Airplanes
Unsafe Condition: a non-conforming dump switch ejecting from its slot, which, in case of smoke/fumes in the cabin, could prevent evacuation of the smoke/fumes, possibly resulting in excessive flight crew workload an...
Why matched: Airworthiness Directives; Daher Aerospace (Type Certificate Previously Held by SOCATA) Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: fatigue cracking of the wing front attachments on the wing and fuselage sides
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: The flight control wheel traveling beyond normal roll control limits and jamming in a position that could cause loss of control.
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: fatigue failure of the nose landing gear wheel axle
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: Corrosion of the horizontal stabilizer (HS) spar, caused by humidity ingress in airplanes subject to severe environmental conditions, which could result in buckling and permanent HS distortion, pos...
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: Cracks found on the main landing gear cylinders, which could lead to fatigue cracks in the shock strut cylinder, potentially causing a collapsed main landing gear during take-off or landing and red...
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: Cracks on the outboard hinge fittings of the horizontal stabilizer, caused by incorrect installation during production, inducing stress.
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: Landing gear actuator rod and piston becoming unscrewed during operation and the landing gear actuator ball joint becoming uncrimped.
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: Installation of an incorrect part number during overhaul of the nose landing gear, which could lead to rupture of the bolt attaching the actuator hinge axle on the nose landing gear (NLG).
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; Socata Airplanes
Unsafe Condition: Installation of the wrong (switched) aileron control cables in the wing, leading to restricted movement of the aileron and reduced control of the airplane.
Why matched: Airworthiness Directives; Socata Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: The electrical protection of some TBM 700 airplanes is insufficient to allow in-flight handling of the standby compass lighting cover when energized, leading to failure of both essential bus bars (...
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Airplanes
Unsafe Condition: A discrepancy in the PRECILEC manufacturing process of elevator trim tab actuators caused jamming once the trim tab arrived to stop, affecting a batch of Serial Numbers (S/N).
Why matched: Airworthiness Directives; SOCATA Airplanes
Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Unsafe Condition: Rupture of the alternator and vapor cycle cooling system pulley drive assembly, compressor drive shaft, and cracks on the standby-alternator and compressor support could lead to loss of the alterna...
Why matched: Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Unsafe Condition: Due to the design of the oxygen generator release pin, one of the mask's lanyard linked to the pin could be jammed when pulled by a pilot or a passenger, leading to a risk of generator fault and su...
Why matched: Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Unsafe Condition: The use of Halon 1211 gas, determined to be outside the required specification, in P/N 863520-00 portable fire extinguishers may provide reduced fire suppression and release toxic fumes, endangerin...
Why matched: Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Unsafe Condition: The foam inside the towing bar box is not conformed to the certification specification, especially the flame resistance properties. In case of fire in the front baggage compartment, the non-conform...
Why matched: Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Airworthiness Directives; SOCATA Model TBM 700 Airplanes
Unsafe Condition: Elongation of bolts connecting power leads on R700 and R701 shunts, likely caused by incorrect tightening torque value. This could lead to heating, electrical arcing, or smoke, resulting in an in-f...
Why matched: Airworthiness Directives; SOCATA Model TBM 700 Airplanes