431 results found (7645ms)
Airworthiness Directives; FS 2001 Corp, FS 2002 Corporation, FS 2003 Corporation, Piper, and Piper Aircraft, Inc. Airplanes
Unsafe Condition: The rudder posts made from 1025 carbon steel can fracture due to fatigue, resulting in a broken rudder and reduced ability of the flight crew to maintain the safe flight and landing of the airplane.
Why matched: Airworthiness Directives; FS 2001 Corp, FS 2002 Corporation, FS 2003 Corporation, Piper, and Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Various Airplanes
Unsafe Condition: an un-commanded automatic pitch trim runaway when the autopilot was first engaged, which could result in un-commanded automatic pitch trim runaway and loss of control of the airplane.
Why matched: Airworthiness Directives; Various Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: A double-drilled bolt hole of the rear wing spar attachment fitting reduces its strength below its limit load, and, if not addressed, could result in separation of the wing and loss of control of t...
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: A missing retaining ring in a control column mount, if not addressed, could lead to a major failure in the aileron quadrant assembly and result in loss of pitch and roll control of the airplane dur...
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Various Airplanes, Helicopters, and Engines
Unsafe Condition: Multiple failures of spot-welded, multi-segment v-band couplings at the tailpipe to the turbocharger exhaust housing flange.
Why matched: Airworthiness Directives; Various Airplanes, Helicopters, and Engines
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Failure of the wing splice assembly could result in loss of airplane control.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Failure of the nose landing gear could occur, which could result in loss of airplane control during take-off, landing, or taxi operations.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. 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; Piper Aircraft, Inc. Airplanes
Unsafe Condition: The repetitive inspections in AD 78-02-03 for all serial-numbered airplanes had no terminating action and were required regardless of any corrective actions performed.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: The life limits for the spar carry through assembly, P/N 97370-00 or 76824-02, were inadvertently omitted from AD 83-20-03 for certain airplanes.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Without the proper stall warning heat control modification kit, during flights into icing conditions with the landing gear down, ice can form on the stall vane, which may result in failure of the s...
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: A fatigue crack in a visually inaccessible area of the lower main wing spar cap can cause wing separation.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: damage to the rudder flight control cables and the emergency power supply (EPS) system wiring due to inadequate clearance from the EPS wiring harness, which can cause electrical arcing between the ...
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Corrosion of the main wing spar, if not detected and corrected, could cause the main wing spar to fail with consequent loss of control of the airplane.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc.
Unsafe Condition: The rivets installed in the bulkhead assembly at fuselage station (FS) 79.00 during the manufacture of certain serial-numbered Model PA-46-600TP (M600) airplanes were not in accordance with the typ...
Why matched: Airworthiness Directives; Piper Aircraft, Inc.
Airworthiness Directives; Piper Aircraft, Inc.
Unsafe Condition: undersized and understrength rivets through the fuselage skin at the cockpit area could result in failure of the skin joint, which could result in loss of pressurization or fuselage structural fail...
Why matched: Airworthiness Directives; Piper Aircraft, Inc.
Airworthiness Directives; Piper Aircraft, Inc.
Unsafe Condition: The installation of fuel tank selector covers with the placement of the left and right fuel tank selector placards installed in reverse, which could result in fuel management error, fuel starvation...
Why matched: Airworthiness Directives; Piper Aircraft, Inc.
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: The potential of carbon monoxide entering the airplane cabin due to failure of the combustion heater exhaust extension.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Oil cooler hose assemblies that do not meet TSO-C53a Type D requirements may fail, leading to potential oil leaks and engine damage.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Aft wing spar cracking during wing assembly, potentially leading to wing separation and loss of control.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Fatigue cracking in the fuselage station (FS) 332.00 bulkhead common to the horizontal stabilizer front spar attachment.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Electrical arcing and possible inflight fire in an area not accessible by the crew, due to rubbing or chafing of electrical wires to adjacent structure or flammable fluid lines.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Engine fire caused by a leak in the fuel pump inlet hose.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Cracks in the right wing rib at wing station 140.09, caused by a production quality control issue, reduce structural integrity of the wing, potentially leading to the inability of the wing rib to c...
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Unsafe Condition: Cracks in the fuselage station (FS) at 317.75 upper bulkhead, which could cause structural failure of the vertical fin forward spar and lead to loss of control.
Why matched: Airworthiness Directives; Piper Aircraft, Inc. Airplanes