- Effective
- October 21, 1963
- Published
- September 19, 1963
- 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
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 | fdfe9b0c…c9f885b | FAA DRS (API key needed) |
On this page
The airworthiness directive
63-20-01 BELLANCA: Amdt. 620 Part 507 Federal Register September 19, 1963. Applies to All Model 14-13 Series Aircraft.
Compliance required as indicated.
Within 50 hours' time in service after the effective date of this AD, and at intervals thereafter not to exceed 50 hours' time in service from the last inspection, accomplish the following:
(a) Inspect for cracks in the welds and the structure immediately adjacent to the area where the left and right brake-cylinder support brackets, P/N's 9811-17 and -21, are attached to the fuselage cross tube P/N 9802-47 (located directly aft of the firewall, below the cabin floor), using a dye penetrant and a 10-power glass or an FAA approved equivalent. Prior to inspection, all grease and dirt shall be removed from the surfaces involved.
(b) If cracks are found, that part must be repaired in accordance with an FAA approved repair, or replaced by a part of the same part number, or an FAA approved equivalent part before further flight.
This directive effective October 21, 1963.
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