- Effective
- April 10, 1975
- Model
- 690A
- Data sheet
- TCDS2A4
- Registered aircraft
- 56 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2160
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 | 20 KB | af39e24e…ecc3249 | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-08-07 ROCKWELL INTERNATIONAL CORP., GENERAL AVIATION DIVISION: Amendment 39-2160. Applies to Model 690A airplanes, Serial Numbers 11100 through 11208.
Compliance required within 25 hours' time in service after the effective date of this AD, unless otherwise accomplished.
To minimize the possibility of bleed air line failure and resultant leakage, accomplish the following:
Modify Model 690A airplanes in accordance with Rockwell International, General Aviation Division, Service Bulletin Number 147 dated November 27, 1974, except that the requirements of Paragraphs "s" and "u" may be ignored and the first item under "SUPPLY DATA" may be deleted, or later approved revision, or in accordance with an equivalent procedure approved by the Chief, Engineering and Manufacturing Branch, Flight Standards Division, Southwest Region, Federal Aviation Administration.
This amendment becomes effective on April 10, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 56
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1973 | 1 |
|---|---|
| 1974 | 11 |
| 1975 | 20 |
| 1976 | 11 |
13 with no year recorded