- Effective
- November 27, 1974
- Models
- 382, 382B, 382E, 382F, 382G
- Data sheet
- TCDSA1SO
- Registered aircraft
- 6 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-2020
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.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 21 KB | 66ff310f…f5e8d59 | FAA DRS (API key needed) |
On this page
The airworthiness directive
74-24-08 LOCKHEED-GEORGIA COMPANY: Amendment 39-2020. Applies to all Lockheed Models 382, 382B, 382E, 382F, and 382G airplanes certificated in all categories.
Compliance required as indicated below for aircraft with serial numbers below 4559 unless already accomplished.
A. For aircraft with 2000 hours or more time in service: This inspection is to be accomplished at the first convenient maintenance period, but not to exceed 200 hours time in service after the effective date of this airworthiness directive.
B. On aircraft with less than 2000 hours time in service, this inspection is to be accomplished prior to the accumulation of 2000 hours or 200 hours time in service after the effective date of this airworthiness directive, whichever is greater.
Accomplish the following: Inspect and replace as required the engine throttle cables located at F.S. 245 upper and lower pulleys and at all engine horsecollar pulleys on the front wing beam as defined and in accordance with Lockheed Service Bulletin A382-175 or later approved revision or an equivalent inspection procedure approved by the Chief, Engineering and Manufacturing Branch, Southern Region.
This amendment is effective November 27, 1974.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 6
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1975 | 1 |
|---|---|
| 1977 | 1 |
| 1985 | 1 |
| 1991 | 1 |
2 with no year recorded