- Effective
- August 7, 1980
- Model
- SD3-30
- Registered aircraft
- 4 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-3857
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.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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The airworthiness directive
80-03-02 R1 SHORT BROTHERS LTD.: Amendment 39-3679 as amended by Amendment 39-3857. Applies to Model SD3-30 airplanes, certificated in all categories.
Compliance is required as indicated unless already accomplished.
To prevent possible failure of the main landing gear beam sub-assembly, accomplish the following:
Prior to the accumulation of 6500 landings or within 25 landings after the effective date of this AD, whichever occurs later, replace the beam sub-assembly, Menasco P/N 17604-5 or 17604- 7, with a new beam sub-assembly, Menasco P/N 17604-15 (Left Hand) and P/N 17604-16 (Right Hand) or Menasco P/N 17604-17 (Left Hand) and P/N 17604-18 (Right Hand) in accordance with Section 10, "Accomplishment Instructions," of Menasco Manufacturing Service Bulletin 32-15, revision 4, dated May 25, 1979, or an equivalent approved by the Chief, Aircraft Certification Staff, AEU-100, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, Brussels, Belgium. Upon replacement of the beam sub-assembly, make appropriate logbook entry indicating compliance with the provisions of this AD.
NOTE: Short Brothers Ltd. Service Bulletin SD3-32-28, revision 6, dated November 27, 1979, covers this same subject.
Amendment 39-3679 became effective February 7, 1980.
This Amendment 39-3857 becomes effective August 7, 1980.
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.
| 1978 | 1 |
|---|---|
| 1984 | 1 |
| 1985 | 2 |