- Model
- 240 Series
- Data sheet
- TCDSA-793
- Product
- Aircraft · Large 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 | 18 KB | 22fdf17f…7c076ea | FAA DRS (API key needed) |
On this page
The airworthiness directive
48-41-01 CONVAIR: Applies to All Model 240 Aircraft.
Compliance required as indicated.
I. Inspect wing bulkhead flanges and stringers at their intersections in the fuel tank area for cracks and repair as necessary at each No. 2 inspection (or equivalent periodic inspection approximating 100 hours) until permanent repairs and rework are accomplished.
II. Complete rework in accordance with CVAC Service Bulletin No. 240-166A dated September 27, 1948, or equivalent should be accomplished not later than the next engine change.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.