AD 93-01-08

Airworthiness directive · Airplane Flight Manual (AFM) Revision · Textron 400, 400A, 400T and 1 more

Effective
March 4, 1993
Models
400, 400A, 400T, MU-300-10
Data sheet
TCDSA16SW
Registered aircraft
312 matched by model
Product
Aircraft · Large airplane
Amendment
39-8462
Docket
92-NM-134-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

93-01-08 BEECH AIRCRAFT CORPORATION: Amendment 39-8462. Docket 92-NM-134-AD.

Applicability: All Beech Model 400 airplanes and Mitsubishi Model MU-300-10 airplanes, certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To ensure that the required minimum takeoff and climb performance can be achieved for each approved combination of takeoff or landing configuration, weight, pressure altitude, and temperature, accomplish the following:

(a) Within 30 days after the effective date of this AD, revise the Limitations Section of the FAA-approved BEECHJET 400 Airplane Flight Manual by inserting the new pages contained in the BEECHJET 400 Airplane Flight Manual, A9 Revision, part number 128-590001-13A9, dated August 14, 1992.

(b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Wichita Aircraft Certification Office(ACO), ACE-115W, 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 revision of the AFM shall be done in accordance with BEECHJET 400 Airplane Flight Manual, A9 Revision, part number 128-590001-13A9, dated August 14, 1992, which contains the list of effective pages specified on pages 1 through 3 of the "Instruction Sheet" (A9 Revision, dated August 14, 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, Small Airplane Directorate, 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 4, 1993.

Affected TCDS · 1

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

Registered aircraft · 312

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
  • Beech57 aircraft
  • Hawker Beechcraft39 aircraft
By year built
19852016
Registered aircraft by year built: 236 aircraft
19852
19861
19871
19886
19903
19916
19928
19932
19947
19955
19968
199717
199820
199928
200021
200117
20029
20032
20048
200510
200612
200720
200819
20091
20102
20161

76 with no year recorded

By model

Aircraft

See all 312 aircraft