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129 results found (1963ms)

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2024-01-02

final rule

Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

Unsafe Condition: certain aft fuselage sloping longerons may have been exposed to excessively hot forming temperatures for excessive amounts of time, which will reduce the mechanical properties of the longerons and ...

Effective: Jan 24, 2024 Category: aircraft Compliance: Within 50 flight hours

Why matched: Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes

2005-01-19

final rule

Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...

Effective: Feb 23, 2005 Category: aircraft Compliance: Within 12 months of the effective date (February 23, 2005).

Why matched: Airworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders

99-19-08

final rule

Airworthiness Directives; Lockheed Model L-14 and L-18 Series Airplanes

Unsafe Condition: Failure to activate the airframe pneumatic deicing boots at the first signs of ice accumulation in icing conditions can lead to reduced controllability due to adverse aerodynamic effects of ice adh...

Effective: Dec 27, 1999 Category: aircraft Compliance: Within 10 days after the effective date of this AD

Why matched: Airworthiness Directives; Lockheed Model L-14 and L-18 Series Airplanes

98-04-32

final rule

Airworthiness Directives; Lockheed Model L-14 and L-18 Series Airplanes

Unsafe Condition: The unsafe condition is the lack of adequate procedures and limitations in the Airplane Flight Manual (AFM) to recognize and exit severe icing conditions, increasing the risk of operating in icing ...

Effective: Mar 25, 1998 Category: aircraft

Why matched: Airworthiness Directives; Lockheed Model L-14 and L-18 Series Airplanes

93-14-12

final rule

Airworthiness Directives; ESSEX PB&R CORPORATION (formerly E.I. DuPont de Nemours and Company \\nIncorporated) PELS Model 4566M37B Crewmember Protective Breathing Equipment (PBE) Units

Unsafe Condition: Leakage of the PBE neck seal could compromise the crew's ability to combat an aircraft fire.

Effective: Sep 2, 1993 Category: appliance Compliance: Within the next 15 months after the effective date of this AD

Why matched: Airworthiness Directives; ESSEX PB&R CORPORATION (formerly E.I. DuPont de Nemours and Company \\nIncorporated) PELS Model 4566M37B Crewmember Protective Breathing Equipment (PBE) Units

77-10-03

final rule

LOCKHEED Model 18 Airplanes

Unsafe Condition: Flexible hose components of propeller feathering lines forward of the firewall may fail due to damage from a powerplant fire, compromising fire resistance integrity.

Effective: Jun 16, 1977 Category: aircraft Compliance: by the first engine change after June 16, 1977 or October 1, 1977, whichever occurs earlier, unle...

Why matched: LOCKHEED Model 18 Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

71-07-02

final rule

LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes

Unsafe Condition: Failure to provide an acceptable obstacle clearance profile when computing the takeoff flight path.

Effective: Apr 3, 1971 Category: aircraft Compliance: prior to the first flight after May 3, 1971 unless already accomplished

Why matched: LOCKHEED Models 49, 149, 649, 749, 1049, and 1649 Series Airplanes

67-03-05

final rule

LOCKHEED Models 649, 749, and 1049 Airplanes

Unsafe Condition: Propeller vibratory stresses due to continuous ground running between 2,300 and 2,650 r.p.m. with propeller governing and continuous static ground running in a crosswind above 2,650 r.p.m.

Effective: Jan 23, 1967 Category: aircraft Compliance: within the next 200 hours' time in service after the effective date of this AD

Why matched: LOCKHEED Models 649, 749, and 1049 Airplanes

Technical illustration of an aircraft propeller assembly
Problem area Propeller

66-02-01

final rule

Airworthiness Directives; Beechcraft: Applies To All Airplanes Equipped With Model BAK-109 Air Conditioners

Unsafe Condition: Failure of the compressor motor fan in the Model BAK-109 air conditioner.

Effective: Feb 10, 1966 Category: appliance Compliance: within the next 100 hours' time in service after the effective date of this AD unless already acc...

Why matched: Airworthiness Directives; Beechcraft: Applies To All Airplanes Equipped With Model BAK-109 Air Conditioners

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

65-13-06

final rule

LOCKHEED Models 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

Unsafe Condition: Cracked beam cap tie-in fittings, Lockheed P/N's 311134L and 311134R, in the area of the 0.16 inch radius near the center of the fitting.

Effective: Jul 23, 1965 Category: aircraft Compliance: Compliance required as indicated.

Why matched: LOCKHEED Models 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

65-11-03

final rule

LOCKHEED Models 1049C, 1049E, 1049G, and 1049H Series Aircraft

Unsafe Condition: The presence of wire clippings in the radio transfer switch assembly, part number 319122, could result in electrical short circuits or failures of the radio transfer system.

Effective: May 20, 1965 Category: aircraft Compliance: within the next 300 hours' time in service after the effective date of this AD unless already acc...

Why matched: LOCKHEED Models 1049C, 1049E, 1049G, and 1049H Series Aircraft

Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

64-13-03

final rule

LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

Unsafe Condition: Cracks and failure in the nose landing gear retract cylinder rod terminal ends (P/N 404052 or 1005032) due to fatigue.

Effective: Jun 12, 1964 Category: aircraft Compliance: Within 100 landings after the effective date (June 12, 1964) for aircraft with 4,500+ landings; p...

Why matched: LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

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

64-07-04

final rule

LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G and 1049H Series Aircraft

Unsafe Condition: Loose or unsafetied bolts in the parallelogram linkages of the primary flight control boost systems could result in loss of flight control system integrity.

Effective: Apr 14, 1964 Category: aircraft Compliance: within 400 hours' time in service after the effective date of this AD

Why matched: LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G and 1049H Series Aircraft

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

64-03-03

final rule

HAMILTON STANDARD Models All Standard Aluminum-Alloy Propellers

Unsafe Condition: Propeller blades may have undetected damage from impact with solid objects, leading to bending, twisting, or other structural failures that could result in blade separation or loss of thrust.

Effective: Mar 1, 1964 Category: appliance Compliance: before further flight

Why matched: HAMILTON STANDARD Models All Standard Aluminum-Alloy Propellers

Technical illustration of an aircraft propeller assembly
Problem area Propeller

64-02-05

final rule

LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G, 1049H and 1649A Series Aircraft

Unsafe Condition: The openable window in the crew door could jam, preventing the crew door from opening.

Effective: Jan 10, 1964 Category: aircraft Compliance: within 325 hours' time in service after the effective date of this AD

Why matched: LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G, 1049H and 1649A Series Aircraft

63-21-04

final rule

LOCKHEED Models L-18 and PV-1 Airplanes

Unsafe Condition: Runaway operation of the electrically operated trim tab actuators

Effective: Jan 10, 1964 Category: aircraft Compliance: within 30 hours' time in service after the effective date

Why matched: LOCKHEED Models L-18 and PV-1 Airplanes

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

63-25-02

final rule

LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

Unsafe Condition: Fatigue failures of the nose landing gear actuating cylinder attach bolts.

Effective: Dec 30, 1963 Category: aircraft Compliance: Within the next 1,000 landings or 1,000 hours' time in service after December 30, 1963, unless al...

Why matched: LOCKHEED Models 49, 149, 649, 649A, 749, 749A, 1049-54, 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

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

63-03-03

final rule

LOCKHEED Models 18 and Learstar Aircraft

Unsafe Condition: Malfunctioning of the anchor fitting securing the main landing gear drag strut to the center section due to loose bolts and elongated bolt holes.

Effective: Mar 5, 1963 Category: aircraft Compliance: Within the next 25 landings after the effective date of this AD and thereafter at intervals not t...

Why matched: LOCKHEED Models 18 and Learstar Aircraft

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

62-27-07

final rule

LOCKHEED Models 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

Unsafe Condition: Fatigue cracking of the wing front spar lower cap and web at wing Station 325.

Effective: Jan 28, 1963 Category: aircraft Compliance: Within the next 400 hours' time in service following the effective date of this AD, and at period...

Why matched: LOCKHEED Models 1049C, 1049D, 1049E, 1049G, and 1049H Series Aircraft

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

62-26-03

final rule

LOCKHEED Models 49, 149, 649, 649A, 749, 749A, and 1049-54 Series Aircraft

Unsafe Condition: Fatigue cracking in the 0.25-inch radii adjacent to the one-inch diameter bearing surfaces on main landing gear crossheads, which could prevent normal extension and retraction of the main landing g...

Effective: Jan 7, 1963 Category: aircraft Compliance: Within the next 700 hours' time in service after the effective date of this AD, unless already ac...

Why matched: LOCKHEED Models 49, 149, 649, 649A, 749, 749A, and 1049-54 Series Aircraft

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

62-19-02

final rule

LOCKHEED All Models 49, 149, 649, 749, and 749A Series Aircraft

Unsafe Condition: Cracks in the main landing gear pistons in the area immediately above the weld retaining the metering pin bulkhead, with some cases of complete fatigue failure.

Effective: Sep 24, 1962 Category: aircraft Compliance: Within 800 hours' time in service after the effective date (September 24, 1962), and thereafter e...

Why matched: LOCKHEED All Models 49, 149, 649, 749, and 749A Series Aircraft

62-16-03

final rule

LOCKHEED Models 1049-54, 1049B, 1049C, 1049D, 1049E, 1049F, 1049G, and 1049H Series Aircraft

Unsafe Condition: Corrosion on the wing rear spar upper cap exposed surfaces exceeding negligible damage limits.

Effective: Aug 13, 1962 Category: aircraft Compliance: Within the next 700 hours' time in service after the effective date of this AD.

Why matched: LOCKHEED Models 1049-54, 1049B, 1049C, 1049D, 1049E, 1049F, 1049G, and 1049H Series Aircraft

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

62-01-02

final rule

LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft

Unsafe Condition: Failures of the cap weld on main landing gear cylinders which have been returned to service following compliance with AD 59-07-03, as amended.

Effective: Jan 9, 1962 Category: aircraft Compliance: Within the next 400 or 1,200 hours' time in service after the effective date (January 9, 1962), d...

Why matched: LOCKHEED Models 49, 149, 649, 749, and 1049 Series Aircraft

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

61-24-04

final rule

LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft

Unsafe Condition: Cracking in the horizontal stabilizer rear spar-to-fuselage attachment due to fatigue.

Effective: Dec 14, 1961 Category: aircraft Compliance: Within 400 hours' time in service after effective date (December 14, 1961), unless already accomp...

Why matched: LOCKHEED Models 049, 149, 649, 749, and 1049 Series Aircraft

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

61-22-06

final rule

LOCKHEED Model PV-1, B-34, and 18 Series Aircraft

Unsafe Condition: Cracks in the elevator control mast assembly castings P/N 11467 or 56045 in the attach bolt lugs, which could lead to failure of the elevator control system.

Effective: Nov 21, 1961 Category: aircraft Compliance: within the next 100 hours' time in service after effective date

Why matched: LOCKHEED Model PV-1, B-34, and 18 Series Aircraft

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