- Model
- Kinner R-5 Series 2
- Data sheet
- TCDSTC 153
- 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 | 19 KB | 43361999…0a92db2 | FAA DRS (API key needed) |
On this page
The airworthiness directive
46-06-02 KINNER: (Was Mandatory Note 8 of AD-749-1 and Special Note 11 of AM-231.) Applies Only to Jobmaster DGA-18K and Ryan ST-3KR Airplanes With R-5 Series 2 Engines With the Following Serial Numbers: 371, 378, 379, 380, 383, 386, 398, 399, 400, 401, 404, 405, 406, 407, 409, 410, 411, 413, 414, 415. Install master rod (P/N 835) before exceeding 200 hours total operation with the early type rod. This replacement should preclude further master rod failures and involves the rebalancing of the crankshaft and rod assembly. (Kinner Service Bulletin No. E-1-8 dated July 24, 1942, covers this same subject.)
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.