- Model
- Military Cyclone R-1300 Series
- Data sheet
- TCDSTC 5E-14
- Product
- Engine
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 | b178756d…8012550 | FAA DRS (API key needed) |
On this page
The airworthiness directive
59-12-07 WRIGHT: Applies to R-1300-1A Engines Installed in North American T-28A Aircraft. Compliance required by July 1, 1959, or within the next 10 hours of operation, whichever occurs first. There is a possibility that a small number of R-1300-1A engines were released by the military for civil sale and use with crankshafts that had undergone a chrome plating salvage repair operation during the last military overhaul. This operation was found to render the crankshaft unsafe and accordingly was discontinued. Engines with these salvaged crankshafts have a note to this effect in the records and log sheets kept for the engine. No other identification of such engine was provided. A re-examination of the military records of these engines must be made and if any indication is found that the crankshaft has been salvaged by chrome plating it is mandatory that the engine be removed from service consistent with the above stipulated compliance provisions and prior to reuse of the engine in civil aircraft the affected crankshaft must be replaced.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.