- Effective
- September 10, 1979
- Models
- 14-13, 14-13-2, 14-13-3, 14-13-3W
- Data sheet
- TCDSA-773
- Registered aircraft
- 131 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-3551
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 | cd8ff943…2b69cb7 | FAA DRS (API key needed) |
On this page
The airworthiness directive
79-19-05 BELLANCA: Amendment 39-3551. Applies to all Bellanca Model 14-13 aircraft, certificated in all categories.
Compliance required within the next 10 hours in service after the effective date of this AD, unless already accomplished.
Inspect the aileron control system for correct rigging and proper operation. If reversal of control system is detected, rerig the system correctly.
NOTE: Do not use the Bellanca 14-13 Handbook for guidance in rigging procedure as the aileron system depicted on page 14, Figure 11, is shown in reverse.
This amendment is effective September 10, 1979.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 131
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1946 | 66 |
|---|---|
| 1947 | 25 |
| 1948 | 6 |
| 1949 | 5 |
29 with no year recorded