- Effective
- January 3, 1970
- Models
- 727-200 Series, 727 Series, 727C Series
- Data sheet
- TCDSA3WE
- Registered aircraft
- 24 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-882
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 | 19 KB | 82cc62c0…20e958d | FAA DRS (API key needed) |
On this page
The airworthiness directive
69-25-01 BOEING: Amdt. 39-882. Applies to Model 727, 727C and 727-200 series airplanes. Compliance required within the next 2500 hours time in service after the effective date of this AD, unless already accomplished. To prevent malfunction of the generator control circuit caused by induced electrical interference, accomplish the following or an equivalent modification procedure and parts installation approved by the Chief, Aircraft Engineering Division, FAA Western Region. Within 2500 hours time in service after the effective date of this AD, unless already accomplished, modify the generator control panels in accordance with Section II, Boeing Service Bulletin No. 24-47, dated March 3, 1969, or later FAA approved revisions. This amendment becomes effective January 3, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 24
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1971 | 1 |
|---|---|
| 1973 | 1 |
| 1975 | 2 |
| 1976 | 3 |
| 1977 | 2 |
| 1978 | 2 |
| 1979 | 1 |
| 1981 | 5 |
| 1982 | 1 |
6 with no year recorded