AD 58-20-01

Airworthiness directive · Tail Wheel Retract Yoke · Airlift International C-46A, C-46D, C-46F and 12 more

Models
C-46A, C-46D, C-46F, C-46R, C-46E, C-46A and 9 more
Data sheets
TCDS2A5TCDS3A2
Registered aircraft
7 matched by model
Product
Aircraft · Large airplane

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

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The airworthiness directive

58-20-01 CURTISS-WRIGHT: Applies to all C-46 Series aircraft P/N 20-360-1058-2 (Tail Wheel Retract Yoke).

Compliance required at next regular inspection, but not later than December 1, 1958.

Several P/N 20-360-1058-2 tail wheel retract yokes have been found cracked or broken. Many of these parts have had a radius at the base of the yoke of less than the required 0.120 inch.

As a result of these failures, the subject parts must be inspected for the proper radius and magnetic particle, or equivalent inspection for cracks at the base of the yoke.

Parts which have a radius at the base of the yoke of less than 0.110 inch or in which cracks are found, are considered unairworthy and must be replaced.

Affected TCDS · 2

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 7

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Curtiss Wright7 aircraft
By year built
19421959
Registered aircraft by year built: 7 aircraft
19421
19444
19451
19591

By model

Aircraft