- Effective
- November 13, 1975
- Models
- 310Q, 310R, T310Q, T310R
- Data sheet
- TCDS3A10
- Registered aircraft
- 828 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2418
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 | cb5fc18e…6e6c066 | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-23-07 CESSNA: Amendment 39-2418. Applies to Models 310Q/T310Q (Serial Numbers 310Q0401 thru 310Q1160) and 310R/T310R (Serial Numbers 310R0001 thru 310R0330) airplanes.
Compliance: Required as indicated, unless already accomplished.
To assure proper operation of the emergency exit window, within the next 50 hours' time in service after the effective date of this AD, accomplish the window modification, screw inspection, trim modification and placard installation, as applicable, in accordance with Cessna Service Letter ME75-26 or later approved revision or by any equivalent method of compliance approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
This amendment becomes effective November 13, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 828
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1969 | 12 |
|---|---|
| 1970 | 23 |
| 1971 | 29 |
| 1972 | 58 |
| 1973 | 87 |
| 1974 | 88 |
| 1975 | 88 |
| 1976 | 73 |
| 1977 | 53 |
| 1978 | 78 |
| 1979 | 58 |
| 1980 | 17 |
| 1981 | 8 |
| 1990 | 1 |
155 with no year recorded