- Models
- 6V4-178-B3, 6V4-178-B31, 6V4-178-B32, 6V4-178-B33, 6V4-200-C32, 6V4-200-C33
- Data sheet
- TCDSE-244
- Registered aircraft
- 84 matched by model
- 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 | 12349045…e5f4e7e | FAA DRS (API key needed) |
On this page
The airworthiness directive
51-28-02 FRANKLIN: Applies to Model 6V4-178 Series Engines Prior to Serial Number 17690 and 6V4- 200 Series Engines Prior to Serial Number 26235. Compliance required as indicated. To preclude the possibility of oil pump failure, oil pump gears (P/N 10673 and 17736) must be inspected at each 300 hours of operation. Excessively galled gears must be replaced. If same part numbers are used for replacements, the 300-hour inspections will still apply. If carbonitrided oil pump drive gear, P/N 19377, and oil pump driven gear, P/N 19373, are installed, no further inspection is required. When these new carbonitrided gears are installed, suffix "P" must be stamped after the serial number of the engine on the nameplate - example: No. 1700P. (Franklin Service Bulletin No. 86, revised November 1, 1951, covers this same subject.) This supersedes AD's 51-22-02 and 51-11-03.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 84
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1942 | 1 |
|---|---|
| 1946 | 1 |
| 1947 | 6 |
| 1948 | 2 |
| 1949 | 4 |
| 1950 | 2 |
| 1951 | 4 |
| 1952 | 7 |
| 1953 | 4 |
| 1954 | 1 |
| 1955 | 7 |
| 1956 | 8 |
| 1957 | 2 |
| 1958 | 3 |
| 1959 | 4 |
| 1960 | 2 |
| 1962 | 1 |
| 1963 | 7 |
| 1964 | 1 |
| 1965 | 1 |
| 1966 | 1 |
| 1967 | 1 |
14 with no year recorded