AD 93-01-07

Airworthiness directive · End Clevis Fitting · Textron 400A and 400T

Effective
March 2, 1993
Models
400A, 400T
Data sheet
TCDSA16SW
Registered aircraft
299 matched by model
Product
Aircraft · Large airplane
Amendment
39-8461
Docket
92-NM-164-AD

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.

On this page

The airworthiness directive

93-01-07 BEECH AIRCRAFT CORPORATION: Amendment 39-8461. Docket 92-NM-164- AD.

Applicability: Model 400A series airplanes having serial numbers RK-1 through RK-32, inclusive; and Model 400T series airplanes having serial numbers TT-1 through TT-6, inclusive; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent snagging of the end clevis fitting and kinking (and subsequent failure) of the emergency release cable of the main landing gear, which may prevent extension of the main landing gear, accomplish the following:

(a) Within 100 flight hours after the effective date of this AD, replace the existing link assembly from the uplink mechanism of the main landing gear door with an improved link assembly, in accordance with Beechcraft Service Bulletin 2447, dated June 1992.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used ifapproved by the Manager, Wichita Aircraft Certification Office (ACO), FAA, Small Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Wichita ACO.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The replacement shall be done in accordance with Beechcraft Service Bulletin 2447, dated June 1992. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Beech Aircraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(e) This amendment becomes effective on March 2, 1993.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 299

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Raytheon216 aircraft
  • Beech44 aircraft
  • Hawker Beechcraft39 aircraft
By year built
19882016
Registered aircraft by year built: 226 aircraft
19881
19903
19916
19928
19932
19947
19954
19968
199717
199820
199928
200021
200117
20029
20032
20048
200510
200612
200720
200819
20091
20102
20161

73 with no year recorded

By model

Aircraft

See all 299 aircraft