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91-22-01: Electrical Wires

FAA order 91-22-01 is an airworthiness directive in force since November 4, 1991. The FAA's subject line: Electrical Wires. It names Cessna 210 Centurion: about 1,526 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: electrical power.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company
Models
210, 210-5 (205), 210-5A (205A), 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, 210R
On this site
Cessna 210 Centurion 1,526 registered

Dates and paperwork

In force since
November 4, 1991
Docket
91-CE-64-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (2,378 characters)
91-22-01 CESSNA: Amendment 39-8061. Docket No. 91-CE-64-AD. Applicability: Model 210 airplanes (serial numbers (S/N) 21059062 through 21064535, S/N T210-0393 through T210-0454, and S/N P21000001 through P21000760), certificated in any category. Compliance: Required within the next 50 hours time-in-service, unless already accomplished. To prevent fuel leakage caused by damaged fuel lines, which could result in an in-flight fire, accomplish the following: (a) Inspect the electrical wires in the nose gear tunnel area and the fuel line to the engine-driven fuel pump for cracks or chafing. (1) If any cracked or chafed electrical wire or fuel line is found, prior to further flight, replace with a new electrical wire or fuel line. Ensure that the electrical wires are bundled and route or clamp the wire bundle so there is a clearance of .25 inches between the wire bundle and fuel line to the engine-driven fuel pump. (2) If no cracked or chafed electrical wire or fuel line is found, ensure that the electrical wires are bundled and route or clamp the wire bundle so there is a clearance of .25 inches between the wire bundle and fuel line to the engine-driven fuel pump. NOTE: Cessna Service Information Letter SE82-32, dated July 23, 1982, includes a photo that highlights the inspection areas and clearance area that is referenced in this AD. This service information may be obtained from the Cessna Aircraft Company, P.O. Box 7704, Wichita, Kansas 67277. (b) 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. (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 throughan appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita Aircraft Certification Office. (d) Information that is related to this AD may be obtained from the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri. This amendment (39-8061, AD 91-22-01) becomes effective on November 4, 1991.

Related safety bulletins advice on the same designs, not orders

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2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2017-06-09CE-17-16 · Main Landing Gear Actuator Inspection
2013-02-08CE-13-16 · Hydraulic Power Pack/Landing Gear System
2012-08-09CE-12-41 · Flight Controls Loose Glide Screw

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 November 6, 2026. Connections as data: /graph/directive/91-22-01.json · aircraft systems.