- Models
- Army AT-11, C18S
- Data sheets
- TCDSA-2-582TCDSA-757
- Registered aircraft
- 13 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 January 21, 2026.
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 | eeb62781…5f3ce1b | FAA DRS (API key needed) |
On this page
The airworthiness directive
48-14-03 BEECH: Applies to Models AT-11 and C18S.
Compliance required by next periodic inspection but not later than July 1, 1948.
Inspect the lower member of the center section main wing spar in the landing gear nacelle area for evidence of wear caused by chafing of the cabin heater control housing. To prevent chafing either use clamps to support housing or cover control housing with 20-inch length of synthetic rubber hose.
Affected TCDS · 2
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 13
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1942 | 1 |
|---|---|
| 1943 | 2 |
| 1944 | 5 |
| 1945 | 1 |
4 with no year recorded