- Effective
- October 15, 1965
- Published
- September 15, 1965
- Model
- Army L-13 Series
- Data sheet
- TCDSTC AR-10
- Product
- Aircraft · Large airplane
- Amendment
- 39-137
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 | 9ce9ec3f…3ee5057 | FAA DRS (API key needed) |
On this page
The airworthiness directive
65-22-01 CONVAIR: Amdt. 39-137 Part 39 Federal Register September 15, 1965. Applies to Army Surplus L-13 Series Airplanes (Basic and Modified) Including Restricted Category Airplanes.
Compliance required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished.
There have been failures of channel, P/N 105-1011321-14, which transmits loads from the wing to the lift strut. To correct this condition, accomplish the following:
For aircraft certificated under T.C. 4A15, and for aircraft certificated in the restricted category under Part 8, replace block assemblies, P/N 105-1011321-16 (consisting of .064 24STAL channel, P/N 105-1011321-14 and block P/N 105-1011327) with one piece fittings as indicated in Figures 1 and 2 or an equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region.
This directive effective October 15, 1965.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.