- Effective
- July 10, 1974
- Models
- B19, C23
- Data sheet
- TCDSA1CE
- Registered aircraft
- 604 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1892
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 | 23 KB | 22afb324…f00380b | FAA DRS (API key needed) |
On this page
The airworthiness directive
74-14-05 BEECH: Amendment 39-1892. Applies to those Model B-19 (Serial Numbers MB-481 through MB-634 and MB-649) and those Model C-23 (Serial Numbers M-1285 through M-1493, except M-1437 and M-1491) airplanes which were originally approved in the Acrobatic Category and intentional spins in the Utility and Acrobatic Categories.
Compliance: Required as indicated, unless already accomplished.
To prevent inflight situations in which prompt spin recovery may not be assured, accomplish the following:
A) Effective immediately intentional spins in the Utility and Acrobatic Categories are prohibited.
B) Within the next 20 hours' time in service or ten (10) calendar days, whichever comes first, after the effective date of this AD, unless already accomplished per AD 73-14-8, Amendment 39-1683, remove all placards pertaining to intentional spins and acrobatic flight and install in place thereof a placard to be conspicuously located on the instrument panel which reads as follows:
"THIS AIRPLANE MUST BE OPERATED AS A NORMAL OR UTILITY CATEGORY AIRPLANE. INTENTIONAL SPINS ARE PROHIBITED. NO ACROBATIC MANEUVERS APPROVED EXCEPT: CHANDELLES, LAZY EIGHTS, STEEP TURNS, AND STALLS (EXCEPT WHIP STALLS)."
C) To reinstate the acrobatic category for those airplanes originally approved in the Acrobatic Category and intentional spins in Utility and Acrobatic Categories, install Beech spin improvement Kit No. 23-4007-1 S in accordance with instructions contained therein, or any equivalent method approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region. Upon installation of said Kit, requirements of Paragraphs A) and B) of this AD are no longer applicable.
This AD supersedes AD 73-14-8, Amendment 39-1683.
This amendment becomes effective July 10, 1974.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 604
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1969 | 1 |
|---|---|
| 1970 | 12 |
| 1971 | 14 |
| 1972 | 22 |
| 1973 | 41 |
| 1974 | 71 |
| 1975 | 52 |
| 1976 | 71 |
| 1977 | 56 |
| 1978 | 67 |
| 1979 | 38 |
| 1980 | 28 |
| 1981 | 18 |
| 1982 | 13 |
| 1983 | 14 |
86 with no year recorded