- Effective
- May 8, 1971
- Model
- 17-30
- Data sheet
- TCDS1A3
- Registered aircraft
- 83 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1205
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 | 0f22cf8b…9631ab2 | FAA DRS (API key needed) |
On this page
The airworthiness directive
71-10-01 BELLANCA: Amendment 39-1205. Applies to Model 17-30 (Serial Numbers 30002 through 30216) Airplanes.
Compliance: Required as indicated unless already accomplished.
To prevent hazardous fuel leakage in these airplanes, accomplish the following:
Within 50 hours time in service after the effective date of this AD, install an electric fuel pump seal chamber drain in accordance with instructions contained in Bellanca Service Letter No. 64, dated April 6, 1971, or any other method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective May 8, 1971.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 83
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1962 | 1 |
|---|---|
| 1966 | 3 |
| 1967 | 20 |
| 1968 | 11 |
| 1969 | 27 |
| 1970 | 2 |
19 with no year recorded