Air Trading Corporation | Lockheed Aircraft Corporation Airworthiness Directives

11 ADs indexed for Air Trading Corporation | Lockheed Aircraft Corporation aircraft.

Models

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67-03-04

final rule

Howard Model 500 Series and Lockheed Model PV-1 Series Airplanes

Unsafe Condition: Cracks in the flap cable support clamps, P/N 5-104268-1, at the bend radius could lead to flap failure.

Effective: Jan 25, 1967 Category: aircraft Compliance: within the next 10 hours' time in service after the effective date of this AD

Why matched: Howard Model 500 Series and Lockheed Model PV-1 Series Airplanes

67-03-03

final rule

All Howard Model 500 Series and Lockheed Model PV-1 Series Airplanes

Unsafe Condition: Cracked elevator torque tube collars, P/N 5-408380-1, in the radius could lead to failure of the elevator control system.

Effective: Jan 23, 1967 Category: aircraft Compliance: within the next 10 hours' time in service after the effective date of this AD, and thereafter at ...

Why matched: All Howard Model 500 Series and Lockheed Model PV-1 Series Airplanes

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

64-26-03

final rule

Airworthiness Directives; Grumman Models TBM and TBF Series Aircraft

Unsafe Condition: The unsafe condition could occur if the elevator control system components, including the bellcrank, pushrod, and bellcrank arm, become disconnected or fail, resulting in loss of elevator control.

Effective: Dec 25, 1964 Category: aircraft Compliance: Before further flight.

Why matched: Airworthiness Directives; Grumman Models TBM and TBF Series Aircraft

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

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

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

61-21-06

final rule

LOCKHEED Models PV-1 and B-34

Unsafe Condition: Main landing gear lower drag strut P/N 112004 is understrength due to lack of specified heat treatment, resulting in potential failure.

Effective: Nov 3, 1961 Category: aircraft Compliance: Within the next 50 hours' time in service from the effective date of this directive

Why matched: LOCKHEED Models PV-1 and B-34

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

61-04-04

final rule

LOCKHEED Models PV-1 and B-34 Aircraft

Unsafe Condition: Failure of the main landing gear drag strut attach plates (P/N 112900 or P/N 12665) can cause main landing gear collapse.

Effective: Mar 14, 1961 Category: aircraft Compliance: Within the next 25 landings and every 50 landings thereafter (option 1) or within the next 25 lan...

Why matched: LOCKHEED Models PV-1 and B-34 Aircraft

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

58-19-01

final rule

Airworthiness Directives; Grumman TBF-1, TBF-1C, TBM-1, TBM-1C, TMB-3, TMB-3E Aircraft

Unsafe Condition: A broken aluminum flammable fluid carrying line can cause a powerplant fire.

Category: aircraft Compliance: December 1, 1958

Why matched: Airworthiness Directives; Grumman TBF-1, TBF-1C, TBM-1, TBM-1C, TMB-3, TMB-3E Aircraft

58-08-03

final rule

Airworthiness Directives; DOUGLAS All DC3 and LOCKHEED 18, PV-1 Aircraft

Unsafe Condition: The Bromochloromethane (CB) fire extinguishing system poses a toxicity hazard to crew and passengers, particularly when agent containers are installed in the fuselage.

Category: aircraft Compliance: October 1, 1958

Why matched: Airworthiness Directives; DOUGLAS All DC3 and LOCKHEED 18, PV-1 Aircraft

59-16-02

final rule

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

Unsafe Condition: Fatigue cracks have been found in the horizontal stabilizer spars in the area of the vertical fin attachments.

Category: aircraft Compliance: Within the next 50 hours of flight and at 300-hour intervals thereafter

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

58-11-03

final rule

LOCKHEED Models 18 Series and PV-1 Aircraft

Unsafe Condition: Cracks occurring at the base of the rudder cable attachment tangs on rudder control quadrant Lockheed P/N 53026 due to excessive clearance between tangs and rudder cable attach fittings, causing be...

Category: aircraft Compliance: as soon as possible, but not later than December 1, 1958

Why matched: LOCKHEED Models 18 Series and PV-1 Aircraft

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

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