- Effective
- May 15, 1960
- Models
- A-4, A-5, A-5T, A-6
- Data sheet
- TCDSA-758
- Registered aircraft
- 14 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 | 0accb5af…88e9920 | FAA DRS (API key needed) |
On this page
The airworthiness directive
60-07-03 CALLAIR: Amdt. 119 Part 507 Federal Register March 25, 1960. Applies to All CallAir Models A-4, A-4 Modified, A-5 Up To and Including Serial Number 292 and A-6 Aircraft Serial Numbers 202, 244, 248, 252, 262, 264, 268, 269, 270 and 271.
Compliance required not later than May 15, 1960, and at each 50 hours' time in service thereafter.
Due to reports of cracks and separation of the lower diagonal brace member on the engine mount the following inspection shall be conducted.
Visually inspect the lower diagonal brace member of the engine mount especially in the area of the gusset plates at the ends of the members. If cracks are found, replace with CallAir redesigned mount, P/N 6-11-4A, or repair in accordance with the method outlined in CallAir Service Bulletin No. 7, or equivalent. After replacement with P/N 6-11-4A or repair, this special inspection may be discontinued. (CallAir Service Bulletin No. 7 covers this same subject.)
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 14
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1954 | 1 |
|---|---|
| 1955 | 1 |
| 1956 | 1 |
| 1957 | 2 |
| 1958 | 1 |
| 1959 | 4 |
| 1960 | 2 |
2 with no year recorded