- Effective
- June 11, 1975
- Model
- 200
- Data sheet
- TCDSA24CE
- Registered aircraft
- 234 matched by model
- Product
- Aircraft · Small/large airplane
- Amendment
- 39-2248
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.
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|---|---|---|---|
| FAA DRS HTML | 21 KB | 5b201a76…55f8d90 | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-14-03 BEECH: Amendment 39-2248. Applies to Model 200 series (Serial Numbers BB-2 through BB-66) airplanes in which the Collins AP105 autopilot is installed.
Compliance: Required as indicated, unless already accomplished.
To prevent the aircraft from exceeding 60 degrees bank angle as a result of an autopilot hard over, accomplish the following:
A) Within the next 10 hours' time in service after receipt of the air mail letter dated June 11, 1975, or after the effective date of this AD, whichever occurs first, install the following placard adjacent to the autopilot controller:
UNCOUPLE AUTOPILOT ABOVE 10,000 FEET MSL"
and operate the aircraft in accordance with this limitation.
B) Modify the Collins AP105 autopilot in accordance with Beechcraft Service Instructions No. 0744-180 or later revisions, or by the accomplishment of any equivalent modification approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.
C) Upon accomplishment of the modification provided in Paragraph B, compliance with the provisions of Paragraph A is no longer required.
This amendment becomes effective July 3, 1975, to all persons except those to whom it was made effective earlier by air mail letter issued June 11, 1975.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 234
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1975 | 14 |
|---|---|
| 1976 | 16 |
| 1977 | 20 |
| 1978 | 28 |
| 1979 | 49 |
| 1980 | 47 |
| 1981 | 30 |
| 1982 | 3 |
| 1983 | 1 |
| 1984 | 3 |
23 with no year recorded