- Effective
- June 9, 1970
- Models
- 36, A36
- Data sheet
- TCDS3A15
- Registered aircraft
- 2,467 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1001
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 January 21, 2026.
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 | 0d5ff94e…bf758ef | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-12-02 BEECH: Amdt. 39-1001. Applies to Models 36 and A36 (Serial Numbers E-1 through E-201) Airplanes.
Compliance: Required as indicated, unless already accomplished.
To effect compliance with a certification regulatory requirement, accomplish the following:
Within 50 hours' time in service after the effective date of this AD, modify the seat tracks on the two center seats in accordance with Beechcraft Service Instructions No. 0343-314, or an equivalent method approved by the Chief, Engineering & Manufacturing Branch, FAA, Central Region.
This amendment becomes effective June 9, 1970.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 2,467
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1968 | 77 |
|---|---|
| 1969 | 30 |
| 1970 | 26 |
| 1971 | 28 |
| 1972 | 47 |
| 1973 | 73 |
| 1974 | 65 |
| 1975 | 98 |
| 1976 | 104 |
| 1977 | 147 |
| 1978 | 151 |
| 1979 | 130 |
| 1980 | 89 |
| 1981 | 108 |
| 1982 | 65 |
| 1983 | 43 |
| 1984 | 60 |
| 1985 | 51 |
| 1986 | 37 |
| 1987 | 35 |
| 1988 | 47 |
| 1989 | 29 |
| 1990 | 45 |
| 1991 | 57 |
| 1992 | 31 |
| 1993 | 46 |
| 1994 | 62 |
| 1995 | 47 |
| 1996 | 37 |
| 1997 | 62 |
| 1998 | 52 |
| 1999 | 52 |
| 2000 | 56 |
| 2001 | 45 |
| 2002 | 27 |
| 2003 | 8 |
| 2004 | 18 |
| 2005 | 8 |
| 2007 | 1 |
273 with no year recorded