30 results found (1378ms)
Airworthiness Directives; GENERAL DYNAMICS Models 22, 22M, 30, and 30A Series Airplanes
Unsafe Condition: The unsafe condition involves potential fire hazard due to wear, abrasion, and corrosion of electrical appurtenances, including wiring, terminal boxes, switches, and hot water heaters within lavato...
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 22, 22M, 30, and 30A Series Airplanes
Airworthiness Directives; GENERAL DYNAMICS Models 22, 22M, and 30A Airplanes
Unsafe Condition: Partial or total loss of generator power due to electric freon pack compressor motor failure.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 22, 22M, and 30A Airplanes
Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Airplanes
Unsafe Condition: Failures of the flap track support structure due to cracks in the flap track support rails 22-17463-57, -58, -59, -60, fittings 22-18994-1, -3 or -5, and track supporting structure.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 22M Series Airplanes
Unsafe Condition: Crack in rudder boost actuator fitting P/N 30-15701-1
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 22M Series Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 22 and 22M Airplanes
Unsafe Condition: Cracks in main landing gear beams (P/N 22-16732-5 or -6) due to fatigue, leading to potential failure.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 22 and 22M Airplanes
Airworthiness Directives; GENERAL DYNAMICS Model 30 and 30A Airplanes
Unsafe Condition: Fatigue cracks in the main landing gear support beams may lead to possible failure of the beams.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 30 and 30A Airplanes
Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft
Unsafe Condition: Cracks originating near the center jack pad on the lower surface of the main landing gear axle beam, progressing upward and causing failure above the pivot pin due to stress corrosion or hydrogen e...
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft
Airworthiness Directives; GENERAL DYNAMICS (CONVAIR) Model 30A Airplanes
Unsafe Condition: The seat support structure at fuselage station 1344 (row 28) may fail due to insufficient strength, posing a risk of passenger injury during normal seating loads.
Why matched: Airworthiness Directives; GENERAL DYNAMICS (CONVAIR) Model 30A Airplanes
Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft
Unsafe Condition: Failures of the No. 1 and No. 4 engine fuel supply tubes under the support clamp at Wing Station 579 have occurred, resulting in engine malfunction and flameout.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft
Airworthiness Directives; GENERAL DYNAMICS Model 30 Series Aircraft
Unsafe Condition: Emergency electrical stabilizer trim system circuits altered under American Airlines Fleet Campaign Directive No. 194K or General Dynamics/Convair Service Bulletin No. 27-66 could permit a runaway ...
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 30 Series Aircraft
Airworthiness Directives; GENERAL DYNAMICS Models 22, 22M, 30 and 30A Aircraft
Unsafe Condition: Inadvertent operation of the engine air turbine starter at continuous overspeeds caused starter failure with resultant damage to surrounding nacelle structure and propulsion systems.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 22, 22M, 30 and 30A Aircraft
Airworthiness Directives, GENERAL DYNAMICS Models 22, 22M, 30 and 30A Aircraft
Unsafe Condition: Slipping of the aileron trim tab dial assembly in relation to the cable drum within the aileron and rudder trim gearbox assembly, damage to gear teeth on the aileron trim tab dial gear, and rubbing...
Why matched: Airworthiness Directives, GENERAL DYNAMICS Models 22, 22M, 30 and 30A Aircraft
Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft
Unsafe Condition: Failures of flap actuator screwjacks due to cracked screwjack shafts and insufficient lateral movement in end cap assemblies P/N 1162D53 and P/N 1162D54.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 22 and 22M Aircraft
Airworthiness Directives; GENERAL DYNAMICS Model 30 Aircraft
Unsafe Condition: Ground fault in the landing gear ground safety switch causing loss of braking without a warning indication.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 30 Aircraft
Airworthiness Directives; GENERAL DYNAMICS Models 30 and 30A Aircraft
Unsafe Condition: Frayed or damaged horizontal stabilizer trim control cables in the vicinity of the aft pressure bulkhead could result in loss of control of the horizontal stabilizer trim system.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Models 30 and 30A Aircraft
Airworthiness Directives; GENERAL DYNAMICS Model 22 Aircraft
Unsafe Condition: Cracks have been found in foreflaps P/N 22-18600-5/-807.
Why matched: Airworthiness Directives; GENERAL DYNAMICS Model 22 Aircraft
GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft
Unsafe Condition: Mechanical interference between rudder pedals in full forward position and rudder fully deflected can prevent application of brakes on the side with deflected rudder.
Why matched: GENERAL DYNAMICS/CONVAIR Models 22 and 22M Series Aircraft
Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Model 30 Aircraft
Unsafe Condition: Cracking of the main landing gear door upper forward attachment fitting, P/N 30-55153, in the vicinity of the attachment of the door actuator, particularly at the radii between the leg and base of ...
Why matched: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Model 30 Aircraft
Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M and 30 Series Aircraft
Unsafe Condition: The aileron override spring may jam in the compressed position if full opposition loads are applied to the lateral control system.
Why matched: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M and 30 Series Aircraft
Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Model 30 Series Aircraft
Unsafe Condition: Cracking of the pylon forward engine thrust beacon channels, part numbers 30-24011-71 and -72, particularly in the area of the relief radius near the aft end of each channel.
Why matched: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Model 30 Series Aircraft
Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M, and 30 Series Aircraft
Unsafe Condition: Loose rudder flight tab balance weights, missing weights, missing attachment nuts/bolts, and elongation of attachment bolt holes in balance weights and attachment arms.
Why matched: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22, 22M, and 30 Series Aircraft
Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 Aircraft
Unsafe Condition: Cracked inboard wing flap carriage support fittings P/N's 22-18703-11, -12 and 22-18702-11, -12 attributed to fatigue.
Why matched: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 Aircraft
Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 and 22M Aircraft
Unsafe Condition: Failure or cracking of the forward support trunnions for elevator and rudder balance boards P/N 22-14715-7, 9, 15, and 17.
Why matched: Airworthiness Directives; GENERAL DYNAMICS/CONVAIR Models 22 and 22M Aircraft
Airworthiness Directives; CONVAIR Models 22 (880) and 22M (880M) Aircraft
Unsafe Condition: An inflight engine pod explosion caused by an open starter bleed air supply valve leading to continued rotation, overheating, and disintegration of the air turbine starter.
Why matched: Airworthiness Directives; CONVAIR Models 22 (880) and 22M (880M) Aircraft
Airworthiness Directives; CONVAIR Model 22 (880) Aircraft
Unsafe Condition: A single malfunction in the pressurization static system could cause the aircraft to be pressurized beyond the structural limits.
Why matched: Airworthiness Directives; CONVAIR Model 22 (880) Aircraft