- Effective
- August 14, 1966
- Models
- 210, 210A
- Data sheet
- TCDS3A21
- Registered aircraft
- 273 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-270
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 | 0ffcebf9…4dfa11c | FAA DRS (API key needed) |
On this page
The airworthiness directive
66-19-02 CESSNA: Amdt. 39-270 Part 39 Federal Register August 4, 1966. Applies to Models 210 and 210A Airplanes, Serial Numbers 616, 618, 57001 through 57575, and 21057576 through 21057840.
Compliance required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent engine power failures caused by the loss of fuel flow resulting from the uncovering of the fuel tank outlet during landing approaches and prolonged slips, install an operating limitation placard, reading as follows, adjacent to the fuel gauges:
"Avoid landing approach in red arc and over 30 seconds slips under 1/2 tank (Reference Owner's Manual)".
(Cessna Service Letter 65-39 pertains to this subject.)
This directive effective August 14, 1966.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 273
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1958 | 1 |
|---|---|
| 1959 | 15 |
| 1960 | 133 |
| 1961 | 44 |
| 1962 | 6 |
| 1964 | 2 |
| 1976 | 2 |
| 1977 | 2 |
| 1981 | 1 |
67 with no year recorded
By model
Aircraft
NTSB investigations that cite this AD · 1
Their narratives or probable cause name AD 66-19-02, often to say whether the aircraft complied with it.