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.
