- Effective
- May 14, 1987
- Model
- A36TC
- Data sheet
- TCDS3A15
- Registered aircraft
- 174 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-5598
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 | 21 KB | 68ed944f…99b412c | FAA DRS (API key needed) |
On this page
The airworthiness directive
87-08-05 BEECH: Amendment 39-5598. Applies to Model A36TC (Serial Numbers EA-1 through EA-241, and EA-243 through EA-272) airplanes certificated in any category.
Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.
To reduce the possibility of engine flooding caused by inadvertent pilot action, accomplish the following:
(a) Modify the fuel system as described in Beechcraft Mandatory Service Bulletin No. 2033, dated August 1985.
(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.
(c) An equivalent means of compliance with this AD may be used if approved by the Manager, Aircraft Certification Office, Federal Aviation Administration, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209.
All persons affected by this directive may obtain copies of the document(s) referred to herein upon request to Beech Aircraft Corporation, Commercial Service, Department 52, P.O. Box 85, Wichita, Kansas 67201-0085; or may examine the document(s) referred to herein at the FAA, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.
This amendment becomes effective on May 14, 1987.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 174
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1979 | 36 |
|---|---|
| 1980 | 69 |
| 1981 | 45 |
| 1983 | 1 |
23 with no year recorded
By model
Aircraft
NTSB investigations that cite this AD · 1
Their narratives or probable cause name AD 87-08-05, often to say whether the aircraft complied with it.