Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation Airworthiness Directives

41 ADs indexed for Airlift International, Inc. | Curtiss-Wright Corporation | Flying Tiger Line, Inc. | L. B. Smith Aircraft Corporation | Skyways International Trading and Transport Co. | Tempo Design Corporation aircraft.

Models

Recent ADs

79-05-10

final rule

CURTISS-WRIGHT C-46 Series Aircraft

Unsafe Condition: Engine fire entering the wheel well area through the nacelle ram air scoop(s).

Effective: Mar 15, 1979 Category: aircraft Compliance: within the next 100 hours' time in service after the effective date of the AD

Why matched: CURTISS-WRIGHT C-46 Series Aircraft

74-18-03

final rule

CURTISS-WRIGHT Model C-46 Series Airplanes

Unsafe Condition: Failures of the main landing gear axle elbows, Part Number 8107-63L and 8107-63R, due to cracks.

Effective: Aug 30, 1974 Category: aircraft Compliance: Within 200 hours' time in service after the effective date (August 30, 1974) for aircraft with el...

Why matched: CURTISS-WRIGHT Model C-46 Series Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

66-05-01

final rule

CURTISS-WRIGHT Model C-46 Series Airplanes

Unsafe Condition: Failure of the main landing gear drag struts due to cracks in the weld area between the lower end fittings (P/N 20-310-1018-2) and the drag strut tubes (P/N's 20-310-1017-7 and -8).

Effective: Feb 25, 1966 Category: aircraft Compliance: within 200 hours' time in service after the effective date of this AD

Why matched: CURTISS-WRIGHT Model C-46 Series Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

66-02-02

final rule

CURTISS-WRIGHT Model C-46 Airplanes

Unsafe Condition: Failure of the main hydraulic accumulator, Vickers P/N AA-14008, due to cracks in the rim mating threads.

Effective: Feb 5, 1966 Category: aircraft Compliance: Within the next 300 hours' time in service after the effective date and thereafter at intervals n...

Why matched: CURTISS-WRIGHT Model C-46 Airplanes

65-17-02

final rule

CURTISS-WRIGHT Model C-46 Series Airplanes

Unsafe Condition: Erroneous indication by the landing gear position warning light that the landing gear is down and locked.

Effective: Sep 2, 1965 Category: aircraft Compliance: within the next 300 hours' time in service after the effective date of this AD unless already acc...

Why matched: CURTISS-WRIGHT Model C-46 Series Airplanes

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

62-27-03

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: Failure of the rudder spring tab rod terminal can cause free flutter of the rudder spring tab and oscillation of the rudder, leading to loss of control of the aircraft.

Effective: Jan 29, 1963 Category: aircraft Compliance: Compliance required as indicated in the AD, with inspections due before reaching specific time-in...

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

60-25-01

final rule

CURTISS-WRIGHT Models C-46A, D. E. F. and R; C-46/CW20T; Super C-46/CW20T; Super 46; and Super 46C Aircraft

Unsafe Condition: Fatigue failures in outer wing panel attachment bolts.

Effective: Dec 6, 1960 Category: aircraft Compliance: Prior to the next flight for aircraft requiring inspection under (a), within the next 25 hours of...

Why matched: CURTISS-WRIGHT Models C-46A, D. E. F. and R; C-46/CW20T; Super C-46/CW20T; Super 46; and Super 46C Aircraft

60-23-02

final rule

Airworthiness Directives; CURTISS-WRIGHT C-46 Series aircraft.

Unsafe Condition: Unapproved inspection openings approximately 3 inches by 5 inches in the wing rear spar web at the inboard flap actuator.

Effective: Nov 4, 1960 Category: aircraft Compliance: Prior to further flight (initial inspection); within not more than 25 flight hours for cargo airc...

Why matched: Airworthiness Directives; CURTISS-WRIGHT C-46 Series aircraft.

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

51-10-06

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: Cracks, loose rivets, worn bolts, and degraded bearings in aileron, rudder, and elevator hinge fittings and adjacent structure could lead to loss of control.

Category: aircraft Compliance: next periodic inspection, not to exceed 100 hours, and each 200 hours or nearest regular inspecti...

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

58-20-01

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: Cracks or breaks in the tail wheel retract yoke (P/N 20-360-1058-2) due to insufficient radius at the base (less than 0.120 inch) leading to potential failure.

Category: aircraft Compliance: next regular inspection, but not later than December 1, 1958

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

59-07-02

final rule

CURTISS-WRIGHT Model C46 Aircraft

Unsafe Condition: The auxiliary hydraulic pump is unsatisfactory for use in compliance with the minimum gear retraction time.

Category: aircraft Compliance: not later than August 1, 1959

Why matched: CURTISS-WRIGHT Model C46 Aircraft

52-17-02

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: Cracks or damage to the tail wheel shimmy damper support (P/N 20-360-3108-4) and non-compliant tail wheel locks (P/N 20-360-1033) may lead to failure, compromising aircraft stability and control.

Category: aircraft Compliance: Within 400 hours' time in service after the effective date of this amendment, and subsequent comp...

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

52-19-01

final rule

CURTISS-WRIGHT Models of C-46 Series Airplanes

Unsafe Condition: The adequacy of powerplant fire protection installations in Curtiss-Wright C-46 series airplanes used in passenger operations is questionable, with potential fire hazards from fluid leaks, inadequa...

Category: aircraft Compliance: Item (5) must be accomplished by November 1, 1952. Other items should be done as soon as possible...

Why matched: CURTISS-WRIGHT Models of C-46 Series Airplanes

57-15-02

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: Repeated service failures of H-3-38-M1 wheel assemblies (Hayes and/or Goodrich Model No. 1900M) due to cracks in the demountable flange area of lightening holes and corrosion in the lock ring groov...

Category: aircraft Compliance: Compliance required as indicated.

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

54-05-01

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: Fatigue cracks occurring in the radius of the O ring groove of the Landing Gear Retraction Cylinder Heads (Curtiss-Wright P/N S20-313-3044) leading to failures.

Category: aircraft Compliance: as soon as practicable but not later than July 15, 1954

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

52-18-01

final rule

CURTISS-WRIGHT Model C-46 Aircraft

Unsafe Condition: Splitting and tearing of the neoprene carburetor adapter gasket (P/N S20-480-1101-2) can block the carburetor air passage, resulting in abrupt engine cutout.

Category: aircraft Compliance: not later than December 1, 1952

Why matched: CURTISS-WRIGHT Model C-46 Aircraft

47-51-03

final rule

Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: The aileron closure rib assembly 20-030-5039 has failed on some aircraft by cracking at the point of attachment to gusset and adjacent to the bolts which secure the aileron hinge assembly.

Category: aircraft Compliance: within every 100 hours' time in service after the effective date of this amendment until rework i...

Why matched: Airworthiness Directives; CURTISS-WRIGHT Model C-46 Series Aircraft

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

52-12-02

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: The main passenger cabin door locking means lacks both internal and external handles, preventing emergency opening from either side.

Category: aircraft Compliance: by September 1, 1952

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

50-29-01

final rule

CURTISS-WRIGHT Model C-46 Series Aircraft

Unsafe Condition: Loose rivets (5/32-A17ST modified brazier head) in the lower surface of the wing center section between Stations 82.5 and 107.5 near the front and rear spars.

Category: aircraft Compliance: Within 25 hours' time in service after the effective date, unless already accomplished within the...

Why matched: CURTISS-WRIGHT Model C-46 Series Aircraft

58-17-03

final rule

CURTISS-WRIGHT AND MARTIN Model C-46 Series

Unsafe Condition: Engine cylinder failures, specifically from studs loosening or breaking, dislodged cylinders severing the propeller hydraulic feathering line, leading to inability to feather the propeller and incr...

Category: aircraft Compliance: Compliance recommended at the next engine overhaul but required by June 1, 1959.

Why matched: CURTISS-WRIGHT AND MARTIN Model C-46 Series

Technical illustration of an aircraft propeller assembly
Problem area Propeller

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