- Effective
- April 7, 1975
- Models
- DC-10-30, DC-10-30F (KC-10A, KDC-10)
- Data sheet
- TCDSA22WE
- Registered aircraft
- 19 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-2151
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 |
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| FAA DRS HTML | 19 KB | 52531558…63b8efe | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-07-12 MCDONNELL DOUGLAS: Amendment 39-2151. Applies to all Douglas Aircraft Company DC-10-30 series airplanes, certificated in all categories.
Compliance required as indicated unless previously accomplished.
After the effective date of this airworthiness directive do not install Autothrottle/Speed Control Computer Part Number 2593342-910C.
Note: Refer to paragraph 2 of McDonnell Douglas DC-10 Service Bulletin No. 22-67 dated February 21, 1975 or later FAA-approved revision.
This amendment becomes effective April 7, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 19
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1975 | 1 |
|---|---|
| 1976 | 1 |
| 1978 | 1 |
| 1988 | 1 |
15 with no year recorded