| AD Number | 88-20-01 | Status | Active |
| Effective Date | October 19, 1988 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-6017 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | A36 B36TC F33A |
88-20-01 BEECH: Amendment 39-6017. Applies to the following airplanes certificated in any category:
MODEL
SERIAL NUMBER
F33A
CE-1162 through CE-1223
A36
E-2383 through E-2405
E-2407 through E-2409
B36TC
EA-468 through EA-470
EA-472 through EA-474
Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.
To prevent a potential fire in the cabin, accomplish the following:
(a) Remove the Mortell 931 sound deadener material from the aft side of the firewall in accordance with the instructions in Beech Service Bulletin Number 2249, dated April 1988.
(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, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; Telephone(316) 946-4400.
All persons affected by this directive may obtain copies of this document referred to herein upon request to Beech Aircraft Corporation, Commercial Service, Dept. 52, P.O. Box 85, Wichita, Kansas 67201-0085; or may examine this document at the FAA, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.
This amendment, 39-6017, becomes effective on October 19, 1988.