AD 91-22-01

Airworthiness directive · Electrical Wires · Cessna 210, 210-5 (205), 210-5A (205A) and 14 more

Effective
November 4, 1991
Models
210, 210-5 (205), 210-5A (205A), 210A, 210B, 210C and 11 more
Data sheet
TCDS3A21
Registered aircraft
1,527 matched by model
Product
Aircraft · Small airplane
Amendment
39-8061
Docket
91-CE-64-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 May 30, 2024.

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The airworthiness directive

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.

Affected TCDS · 1

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

Registered aircraft · 1,527

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
  • Cessna1,527 aircraft
By year built
19581999
Registered aircraft by year built: 1,253 aircraft
19581
195915
1960133
196150
1962150
1963181
1964121
196551
196627
196732
196837
196943
197022
197122
197229
197325
197439
197556
197656
197772
197831
197921
198013
198114
19825
19832
19844
19991

274 with no year recorded

By model

See all 19 models

Aircraft

See all 1,527 aircraft