Aerotek II, Inc. Airworthiness Directives

3 ADs indexed for Aerotek II, Inc. aircraft.

Models

Recent ADs

79-16-04

final rule

Airworthiness Directives; SL Industries Models B-1 and B-1A Airplanes

Unsafe Condition: Failure of the wing rear spar at the wing-fuselage attachment fitting (P/N 160049) due to cracking.

Effective: Sep 7, 1979 Category: aircraft Compliance: Within the next 50 hours after the effective date of this AD, unless already accomplished within ...

Why matched: Airworthiness Directives; SL Industries Models B-1 and B-1A Airplanes

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

74-02-02

final rule

Airworthiness Directives; SL Industries, Inc Models B-1 and B-1A Airplanes

Unsafe Condition: Failure of the front wing spar due to cracks, elongated fastener holes, or corrosion in the spar web area of the P/N 16045-1 and -2 fittings.

Effective: Jan 18, 1974 Category: aircraft Compliance: within the next 100 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; SL Industries, Inc Models B-1 and B-1A Airplanes

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

72-21-01

final rule

Airworthiness Directives; Aero Commander Models B-1 and B-1A Series Airplanes

Unsafe Condition: Failures of the landing gear shock struts, specifically P/N 18004-1 and P/N 18004-2, which could lead to loss of structural integrity.

Effective: Oct 6, 1972 Category: aircraft Compliance: within the next 100 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Aero Commander Models B-1 and B-1A Series Airplanes

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

View all Aerotek II, Inc. ADs →