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91-18-19: Pilot Shoulder Harnesses

FAA order 91-18-19 is an airworthiness directive in force since October 21, 1991. The FAA's subject line: Pilot Shoulder Harnesses. It names Beechcraft 58 Baron, Beechcraft 95 Travel Air and Baron 55, Beechcraft A36 Bonanza, Beechcraft B36 Bonanza, Beechcraft E-55, Beechcraft F33 Bonanza, Beechcraft V35 Bonanza: about 8,262 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
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
58 Model or Series (all), 58A, 58P, 58PA, 58TC, 58TCA, 95-B55, 95-B55A, A36, B36TC, E55, E55A, F33A, V35B
On this site
Beechcraft 58 Baron 1,295 registered
Beechcraft 95 Travel Air and Baron 55 1,245 registered
Beechcraft A36 Bonanza 2,530 registered
Beechcraft B36 Bonanza 308 registered
Beechcraft E-55 215 registered
Beechcraft F33 Bonanza 1,008 registered
Beechcraft V35 Bonanza 1,661 registered

Dates and paperwork

In force since
October 21, 1991
Docket
91-CE-16-AD
Replaced by
2009-25-01
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 (2,485 characters)
91-18-19 BEECH: Amendment 39-8022. Docket No. 91-CE-16-AD. Applicability: The following model airplanes, certificated in any category: Models Serial Numbers F33A CE-634 through CE-1536 V35B D-9862 through D-10403 A36 E-825 through E-2578 B36TC EA-1 through EA-509 95-B55, 95-B55A TC-1947 through TC-2456 E55, E55A TE-1078 through TE-1201 58, 58A TH-733 through TH-1609 58P, 58PA TJ-3 through TJ-497 58TC, 58TCA TK-1 through TK-151 Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished. To prevent malfunctioning pilot and copilot shoulder harnesses that could result in occupant injury during an emergency situation, accomplish the following: (a) Inspect the washers on the "D" ring of the pilot and copilot shoulder harnesses in accordance with the instructions of Beech Service Bulletin (SB) No. 2394, dated December 1990. (b) If the washers installed on the "D" ring do not meet the criteria in the instructions of Beech SB No. 2394, dated December 1990, prior to further flight, replace the washers with part number 100951X060YA. (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) 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, 1801 Airport Road, Room 100, 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. (e) The inspections and possible replacements required by this AD shall be done in accordance with Beech Service Bulletin No. 2394, dated December 1990. 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. This amendment (39-8022, AD 91-18-19) becomes effective on October 21, 1991.

Related safety bulletins advice on the same designs, not orders

2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2018-07-13CE-18-22 · Alternative Method of Compliance to Airworthiness Directive 2018-06-11
2015-09-15CE-15-22 · Wing Leading Edge Hinge-Pin Corrosion
2013-03-13CE-13-22 · Electrical Power System Circuit Breaker Switch
2012-06-19CE-12-36 · Flight Controls: Aileron

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/91-18-19.json · aircraft systems.