- Effective
- August 18, 1993
- Model
- SD3-60
- Registered aircraft
- 26 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-8619
- Docket
- 92-NM-176-AD
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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On this page
The airworthiness directive
93-13-06 SHORT BROTHERS, PLC: Amendment 39-8619. Docket 92-NM-176-AD. Applicability: Model SD3-60 series airplanes; equipped with main landing gear (MLG) actuator part number (P/N) 104796004, having serial number DRG/4729/86, DRG/4730/86, DRG/5057/86, DRG/5059/86, DRG/5060/86, or DRG/5061/86; certificated in any category.
Compliance: Required as indicated, unless accomplished previously.
To prevent failure of the MLG actuator to unlock, which would prevent the extension of the MLG, accomplish the following:
(a) Within 6 months after the effective date of this AD, replace the MLG actuator with a serviceable actuator that is marked "32-69SD" in accordance with Dowty Aerospace Hydraulics - Cheltenham Service Bulletin 32-69SD, Revision 2, dated January 20, 1993.
(b) As of the effective date of this AD, no person shall install on any airplane a MLG actuator P/N 104796004, having serial number DRG/4729/86, DRG/4730/86, DRG/5057/86, DRG/5059/86, DRG/5060/86, or DRG/5061/86, that is not marked "32-69SD."
(c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113.
NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113.
(d) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.
(e) The replacement shall be done in accordance with Dowty Aerospace Hydraulics - Cheltenham Service Bulletin 32-69SD, Revision 2, dated January 20, 1993. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Short Brothers, PLC, 2011 Crystal Drive, suite 713, Arlington, Virginia 22202-3719. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.
(f) This amendment becomes effective on August 18, 1993.
Registered aircraft · 26
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1982 | 1 |
|---|---|
| 1983 | 2 |
| 1984 | 1 |
| 1986 | 3 |
| 1987 | 2 |
| 1988 | 5 |
| 1989 | 4 |
8 with no year recorded