P. V. Shields Airworthiness Directives

7 ADs indexed for P. V. Shields aircraft.

Models

Recent ADs

84-15-02

final rule

Airworthiness Directives; DOUGLAS A-26/B26 Series Airplanes

Unsafe Condition: Failure of a lower spar cap due to cracking or fretting in the area where the nacelle fairing upper edge contacts the lower spar cap surface.

Effective: Apr 16, 1985 Category: aircraft Compliance: Within ten (10) hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; DOUGLAS A-26/B26 Series Airplanes

64-12-03

final rule

Airworthiness Directives; DOUGLAS Models A-26B and A-26C

Unsafe Condition: Failure of the wing rear spar caps in the vicinity of the flap inboard hinges and failure of the wing rear spar lower caps near the inboard end of the fore and aft flanges and the forward flange 3/...

Effective: Jul 15, 1975 Category: aircraft Compliance: Compliance required as indicated. Inspections under (a) must be conducted within 250 hours' time ...

Why matched: Airworthiness Directives; DOUGLAS Models A-26B and A-26C

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

61-11-05

final rule

Airworthiness Directives; DOUGLAS All Models A-26 (B-26) Series Aircraft

Unsafe Condition: Severe corrosion of the wing structure beneath the wing fuel tanks and deterioration of sponge rubber mats under fuel cells.

Effective: Jun 29, 1961 Category: aircraft Compliance: at the next periodic inspection and every periodic inspection thereafter until (b) is accomplished

Why matched: Airworthiness Directives; DOUGLAS All Models A-26 (B-26) Series Aircraft

55-26-01

final rule

Airworthiness Directives; DOUGLAS A-26 Aircraft

Unsafe Condition: Explosion in the air due to potential fuel tank fumes ignition in the rear fuselage fuel tank compartment.

Category: aircraft Compliance: prior to actuation of fuselage fuel tank

Why matched: Airworthiness Directives; DOUGLAS A-26 Aircraft

Technical illustration of an aircraft fuel pump, filter, valve, and lines
Problem area Fuel system

56-18-03

final rule

Airworthiness Directives; DOUGLAS All Models A-26B and A-26C Aircraft

Unsafe Condition: Cracks in the nose gear cross beam assembly at the inboard end of the trunnion journal.

Category: aircraft Compliance: prior to September 5, 1956, and each periodic inspection thereafter

Why matched: Airworthiness Directives; DOUGLAS All Models A-26B and A-26C Aircraft

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

47-36-01

final rule

Airworthiness Directives; DOUGLAS A-26B and A-26C Aircraft

Unsafe Condition: Failure of the wing bulkhead assemblies and subsequent loss of the ailerons.

Category: aircraft Compliance: prior to November 15, 1947

Why matched: Airworthiness Directives; DOUGLAS A-26B and A-26C Aircraft

47-36-02

final rule

Airworthiness Directives; DOUGLAS A-26B and A-26C Aircraft

Unsafe Condition: Collapse of the oil screen during cold weather starting.

Category: aircraft Compliance: Prior to operation in cold weather and not later than next engine overhaul.

Why matched: Airworthiness Directives; DOUGLAS A-26B and A-26C Aircraft

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