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FAA orders · airworthiness directive · historical

92-07-05: Rudder Trim Tab

FAA order 92-07-05 is an airworthiness directive in force since April 30, 1992. The FAA's subject line: Rudder Trim Tab. It names Beechcraft 100, Beechcraft 65, Beechcraft 99 Airliner, Beechcraft A100, Beechcraft B-99, Beechcraft B100, Beechcraft B90, Beechcraft C-99, Beechcraft C90 King Air C90, Beechcraft E-90 King Air E90: about 1,165 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Raytheon Aircraft Company; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation
Models
100 Model or Series (all), 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, 99 Model or Series (all), 99A, A100 Model or Series (all), A99A, B100, B90, B99, C90, C90A, C99, E90, H90
On this site
Beechcraft 100 14 registered
Beechcraft 65 201 registered
Beechcraft 99 Airliner 34 registered
Beechcraft A100 15 registered
Beechcraft B-99 6 registered
Beechcraft B100 59 registered
Beechcraft B90 29 registered
Beechcraft C-99 54 registered
Beechcraft C90 King Air C90 607 registered
Beechcraft E-90 King Air E90 146 registered

Dates and paperwork

In force since
April 30, 1992
Docket
91-CE-90-AD
Replaced by
2006-13-10
Status
Historical
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (2,741 characters)
92-07-05 BEECH: Amendment 39-8201. Docket No. 91-CE-90-AD. Supersedes AD 91-12-12, Amendment 39-7023. Applicability: Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, B90, and C90 airplanes (all serial numbers (S/N)); Model C90A airplanes (S/N LJ-1063 through LJ-1280); Models E90, H90, 99, 99A, A99A, B99, C99, 100, A100, and B100 airplanes (all S/N), certificated in any category. Compliance: Required within the next 150 hours time-in-service after the effective date of this AD, unless already accomplished (superseded AD 91-12-12, Amendment 39-7023). To prevent structural damage or imbalance to the rudder caused by improper drainage of water from the rudder trim tab, accomplish the following: (a) Inspect the rudder trim tab for proper moisture drainage provisions in accordance with the instructions in Beech Service Bulletin No. 2365, Revision 1, dated December 1991. If the correct drainage provisions do not exist, prior to further flight, modifythe rudder trim tab in accordance with the instructions in the referenced service bulletin. NOTE: The requirements of this AD may have already been accomplished in accordance with superseded AD 91-12-12, Amendment 39-7023. A change in the Applicability paragraph is the only difference between this action and superseded AD 91-12-12. (b) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a location where the requirements of this AD can be accomplished. (c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Mid-Continent Airport, Wichita, Kansas 67209. The request should be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita Aircraft Certification Office. (d) The inspection and possible modification required by this AD shall be done in accordance with Beech Service Bulletin No. 2365, Revision 1, dated December 1991. 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 the Beech Aircraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 1100 L Street, NW, Room 8401, Washington, DC. (e) This amendment (39-8201) supersedes AD 91-12-12, Amendment 39-7023. (f) This amendment (39-8201, AD 92-07-05) becomes effective on April 30, 1992.

Related safety bulletins advice on the same designs, not orders

2026-09-102026-16 · Elevator Control System
2013-08-30CE-10-34R2 · Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08
2013-08-20CE-10-34R1 · Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08
2012-06-19CE-12-36 · Flight Controls: Aileron
2010-12-02CE-11-04 · Wings Wing Spar

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 5, 2026. Connections as data: /graph/directive/92-07-05.json · aircraft systems.