95 results found (3272ms)
Airworthiness Directives; Kelowna Flightcraft R & D Ltd. Airplanes
Unsafe Condition: Fatigue cracking of the lower skin of the wings around the inboard side of the wing station (WS) 6 and 7 access panel doubler fingers and between stringers 5 and 11, as well as around stringers 6, ...
Why matched: Airworthiness Directives; Kelowna Flightcraft R & D Ltd. Airplanes
Airworthiness Directives; Turbo-Propeller Powered General Dynamics (Convair) Model 240, 340, and 440 Series Airplanes
Unsafe Condition: Positioning the power levers below the flight idle stop during flight may lead to loss of airplane controllability or engine overspeed and consequent loss of engine power.
Why matched: Airworthiness Directives; Turbo-Propeller Powered General Dynamics (Convair) Model 240, 340, and 440 Series Airplanes
Airworthiness Directives; Pacific Scientific Company, HTL/Kin-Tech Division, Fire Extinguisher Bottle Cartridges
Unsafe Condition: Electrical shorting of the pins in the fire extinguisher bottle cartridges, caused by the presence of aluminum foil, could result in failure of the fire extinguisher bottle to discharge when comman...
Why matched: Airworthiness Directives; Pacific Scientific Company, HTL/Kin-Tech Division, Fire Extinguisher Bottle Cartridges
Airworthiness Directives; Sundstrand T-62T-40C Series Auxiliary Power Units
Unsafe Condition: Compressor wheel ruptures due to low cycle fatigue could result in an uncontained APU failure and damage to the aircraft.
Why matched: Airworthiness Directives; Sundstrand T-62T-40C Series Auxiliary Power Units
Airworthiness Directives; Allied Signal Commercial Avionics Systems CAS-81 Traffic Alert and Collision Avoidance Systems (TCAS) as Installed in, but not Limited to, Various Transport Category Airplanes
Unsafe Condition: Failure of the audio output of the CAS-81 TCAS may result in the flightcrew not receiving necessary traffic alerts and collision avoidance information.
Why matched: Airworthiness Directives; Allied Signal Commercial Avionics Systems CAS-81 Traffic Alert and Collision Avoidance Systems (TCAS) as Installed in, but not Limited to, Various Transport Category Airplanes
Airworthiness Directives; General Dynamics Model 240 Series Airplanes, Including Model T-29 (Military) Airplanes; Model 340 and 440 Series Airplanes; and Model C-131 (Military) Airplanes
Unsafe Condition: Ice contaminated tailplane stall (ICTS) can occur during or following flight in icing conditions if flap settings are increased, leading to adverse elevator control and potential uncontrollable des...
Why matched: Airworthiness Directives; General Dynamics Model 240 Series Airplanes, Including Model T-29 (Military) Airplanes; Model 340 and 440 Series Airplanes; and Model C-131 (Military) Airplanes
Airworthiness Directives: Allied Signal Aerospace Company, Air Transport Avionics (formerly Bendix\\King Air Transport Avionics Division) Traffic Alert and Collision Avoidance System II Processors
Unsafe Condition: Incompatibility between TCAS II processors and the current air traffic control system could cause collisions or near misses.
Why matched: Airworthiness Directives: Allied Signal Aerospace Company, Air Transport Avionics (formerly Bendix\\King Air Transport Avionics Division) Traffic Alert and Collision Avoidance System II Processors
Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C-131B through C-131H (military) Series Airplanes
Unsafe Condition: Loss of an elevator or rudder resulting from installation of a suspected unapproved part.
Why matched: Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C-131B through C-131H (military) Series Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 240, T-29A through D, and C-131A (military) Series Airplanes
Unsafe Condition: Loss of an elevator or rudder resulting from the installation of a suspected unapproved part (SUP) due to worn hinge pins and bushings, cracked bearing plate assemblies, or discrepant bearings.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 240, T-29A through D, and C-131A (military) Series Airplanes
Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes
Unsafe Condition: Failure of the stabilizer attach fittings, and potential subsequent loss of a horizontal or vertical stabilizer.
Why matched: Airworthiness Directives; General Dynamics Model 340, 440, and C-131B through C-131H (military) Series Airplanes
Airworthiness Directives; General Dynamics, Convair Division Model 240, 340, 440, and C-131 (Military) Airplanes
Unsafe Condition: Degradation of the structural capabilities of the airplane due to problems associated with corrosion.
Why matched: Airworthiness Directives; General Dynamics, Convair Division Model 240, 340, 440, and C-131 (Military) Airplanes
Airworthiness Directives; General Dynamics Model 340, 440, and C-131 (Military) Series Airplanes
Unsafe Condition: Insp. Program Revision Structure
Why matched: Airworthiness Directives; General Dynamics Model 340, 440, and C-131 (Military) Series Airplanes
Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes
Unsafe Condition: Loss of the elevator hinge pins due to non-conforming dimensions, cracked bearing plate assemblies, or loose, chattering, dry, or seized bearings (P/N AN201KP1A).
Why matched: Airworthiness Directives; General Dynamics (CONVAIR) Model 340, 440, and C131, B, C, D, E, and F (Military) Series Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 240, T-29, and C-131A (Military) Series Airplanes
Unsafe Condition: Loss of the elevator hinge pins due to non-conforming dimensional limitations, cracked bearing plate assemblies, loose, chattering, dry, or seized bearings (P/N AN201KP10A).
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 240, T-29, and C-131A (Military) Series Airplanes
GENERAL DYNAMICS (CONVAIR) Models 340, 440, and C-131, B, C, D, E, F, and G (Military) series airplanes
Unsafe Condition: Progressive damage to the airframe due to non-conforming or cracked holes in fuselage frames.
Why matched: GENERAL DYNAMICS (CONVAIR) Models 340, 440, and C-131, B, C, D, E, F, and G (Military) series airplanes
Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes
Unsafe Condition: Failure of the main landing gear drag strut pivot bolt and possible subsequent main landing gear collapse.
Why matched: Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340, 440, and C-131 (Military) Series Airplanes
Airworthiness Directives; GENERAL DYNAMICS (Convair) Model 240 Series Airplanes
Unsafe Condition: Separation of the main entrance door in flight due to malfunction of the door latching systems, which may result from rust, corrosion, broken components, or foreign material in the latch housing, o...
Why matched: Airworthiness Directives; GENERAL DYNAMICS (Convair) Model 240 Series Airplanes
Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 240-27 Aircraft
Unsafe Condition: Undetected failure of the door open warning system
Why matched: Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 240-27 Aircraft
Airworthiness Directives; GENERAL DYNAMICS (Convair) Model 240 Airplanes
Unsafe Condition: Fracture of the nose landing gear (NLG) axle caused by fatigue cracks.
Why matched: Airworthiness Directives; GENERAL DYNAMICS (Convair) Model 240 Airplanes
Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340/440 Airplanes
Unsafe Condition: Fracture of the nose landing gear (NLG) axle caused by fatigue cracks.
Why matched: Airworthiness Directives; GENERAL DYNAMICS (Convair) Models 340/440 Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 240 Airplanes
Unsafe Condition: Structural failure of the wing structure due to corrosion and cracking at the wing outer panel/wing center section joint.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 240 Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 340 and 440
Unsafe Condition: Fatigue cracks in the horizontal stabilizer attachment fittings (P/Ns 340-8510150 and 340-8510151) could cause loss of the horizontal stabilizer.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 340 and 440
Airworthiness Directives; GENERAL DYNAMICS Model 340 and 440 Airplanes
Unsafe Condition: Loosening and shearing of elevator flange to outer torque tube aluminum rivet fasteners could result in potential loss of elevator control.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 340 and 440 Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 240, T-29, 340, 440 Airplanes
Unsafe Condition: Failure of pilots' windshield, direct vision windows, sliding windows (P/N 340-3110307-7 or -8), and cabin windows due to aging or damage exceeding service bulletin limits, and door collapse on cer...
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 240, T-29, 340, 440 Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 240 Series Airplanes
Unsafe Condition: Failure of the elevator flight tab spring tube.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 240 Series Airplanes