- Effective
- July 25, 1969
- Models
- 727-100 Series, 727-100C Series, 727-200 Series, 727-200F Series, 727 Series, 727C Series
- Data sheet
- TCDSA3WE
- Registered aircraft
- 25 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-804
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 | 22 KB | 1814da52…7bd0539 | FAA DRS (API key needed) |
On this page
The airworthiness directive
69-15-05 BOEING: Amdt. 39-804. Applies to Model 727 Series airplanes.
Compliance required as indicated.
To prevent a slow discharge or no discharge of the engine fire extinguisher container, accomplish the following:
(a) Within the next 1000 hours' time in service after the effective date of this AD unless already accomplished, and after each discharge regardless of time in service, inspect the Accessory Products Company (APCO) fire extinguisher outlet body P/N 805516 to determine that the gas port diameter has not been reduced below the allowable limit as set out in APCO Service Bulletin No. 26-04, dated March 31, 1969, or later FAA approved revision or an equivalent method approved by the Chief, Aircraft Engineering Division, FAA Western Region.
(b) If an outlet body is found which is below the allowable limit, replace it, or modify it in accordance with APCO Service Bulletin No. 26-04 or later FAA approved revision or an equivalent method approved by the Chief, Aircraft Engineering Division, FAA Western Region.
(c) Within the next 3000 hours' time in service after the effective date of this AD unless already accomplished, modify the APCO fire extinguisher outlet body P/N 805516 in accordance with APCO Service Bulletin NO. 26-04 or later FAA approved revision or an equivalent method approved by the Chief, Aircraft Engineering Division, FAA Western Region.
(d) Upon completion of the modification described in (b) or (c), the inspection requirement of (a) is no longer applicable.
This amendment becomes effective on July 25, 1969.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 25
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 |
7 with no year recorded