AD 81-09-04

Airworthiness directive · Main Landing Gear Wheels · Short Brothers SD3-30

Effective
May 4, 1981
Model
SD3-30
Registered aircraft
4 matched by model
Product
Aircraft · Large airplane
Amendment
39-4093

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

81-09-04 SHORT BROTHERS LIMITED: Amendment 39-4093. Applies to Model SD3-30 series airplanes, with main landing gear wheel, P/N AH53369, installed, certificated in all categories.

Compliance is required as indicated, unless already accomplished.

To prevent failure of the main landing gear wheels, accomplish the following:

(a) Prior to the accumulation of 150 hours time in service or 250 landings after the effective date of this AD, whichever occurs sooner, and thereafter at intervals not to exceed 250 landings since the last inspection, inspect the valve side half, P/N AH43782 Mod State 1, of the main landing gear wheel, P/N AH53369, for cracks using the eddy current method in accordance with the Dunlop Component Maintenance Manual 32-40-65, Revision 6, dated May 11, 1979, or an FAA-approved equivalent.

(b) Prior to the accumulation of 300 hours time in service or 500 landings since new, or prior to the accumulation of 150 hours time in service or 250 landings after the effective date of this AD, whichever occurs later, and thereafter at intervals not to exceed 250 landings since the last inspection, inspect the valve side half, P/N AH43782 Mod State 2, of the main landing gear wheel, P/N AH53369, for cracks using the eddy current method in accordance with the Dunlop Component Maintenance Manual 32-40-65, Revision 6, dated May 11, 1979, or an FAA-approved equivalent.

(c) If as a result of the inspection required in paragraph (a) or (b) of this AD, any crack or cracks are found, replace the wheel with a serviceable wheel of the same part number, or an FAA-approved equivalent and continue the repetitive inspection required by paragraph (a) or (b) of the AD as appropriate.

(d) If an equivalent means of compliance is used in complying with this AD, that equivalent must be approved by the Chief, Aircraft Certification Staff, Europe, Africa, and Middle East Office, c/o American Embassy, Brussels, Belgium.

NOTE: Shorts Service Bulletin SD3-32-64, Revision 2, dated January 25, 1980, and Dunlop Aviation Division Service Bulletin No. 32-920, Revision 2, dated November 16, 1979, refer to this subject.

This amendment becomes effective May 4, 1981.

Registered aircraft · 4

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
  • Short Bros. & Harland3 aircraft
  • Short Bros1 aircraft
By year built
19781985
Registered aircraft by year built: 4 aircraft
19781
19841
19852

By model

Aircraft