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98-25-03: Aileron Control Cable

FAA order 98-25-03 is an airworthiness directive in force since December 18, 1998. The FAA's subject line: Aileron Control Cable. It names Cessna 172 Skyhawk: about 20,670 aircraft on the U.S. register today, 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
Cessna Aircraft Company
Models
172R
On this site
Cessna 172 Skyhawk 20,670 registered

Dates and paperwork

In force since
December 18, 1998
Published
December 3, 1998
Docket
98-CE-109-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This amendment adopts a new airworthiness directive (AD) that applies to certain Cessna Aircraft Company (Cessna) Model 172R airplanes that are not equipped with an autopilot. This AD requires inspecting the right wing for an incorrectly routed, frayed, or damaged aileron control cable, and re-routing any incorrectly routed cable or replacing any frayed or damaged cable. The AD also requires reporting any incorrectly routed, frayed, or damaged cable to the Federal Aviation Administration (FAA). This AD is the result of a report of an incorrectly routed aileron control cable in the right wing of an airplane of the same type design to those affected by this AD. The cable was routed over the aileron auto pilot actuator pulley and the cable was rubbing on the cable guard. The actions specified by this AD are intended to prevent loss of aileron control caused by a damaged or frayed aileron control cable, which could result in loss of directional control of the airplane.

The order itself the regulatory text, as published

Show the full text (4,647 characters)
98-25-03 CESSNA AIRCRAFT COMPANY: Amendment 39-10925; Docket No. 98-CE-109-AD. Applicability: Model 172R airplanes, serial numbers 17280437, 17280439, 17280454, 17280456, and 17280459; certificated in any category, that were not factory equipped with an autopilot. NOTE 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (e) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it. Compliance: Required within the next 25 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished. To prevent loss of aileron control caused by a damaged or frayed aileron control cable, which could result in loss of directional control of the airplane, accomplish the following: (a) Inspect the right wing for an incorrectly routed, frayed, or damaged aileron control cable, in accordance with the Accomplishment Instructions in Cessna Service Bulletin SB98-27-05, which incorporates the following pages: Pages Revision Level Date 1, 2, 9 and 10 Revision 1 August 17, 1998 3 through 8 Original Issue June 1, 1998 (b) Prior to further flight, re-route any incorrectly routed cable and replace any frayed or damaged cable, in accordance with the applicable maintenance manual. (c) If an incorrectly routed, damaged, or frayed cable is found during the inspection required by paragraph (a) of this AD, at the applicable time specified in paragraph (c)(1) or (c)(2) of this AD, submit a report of inspection findings to the Manager, Wichita Manufacturing Inspection Office, 1801 Airport Road, Room 101, Mid-Continent Airport, Wichita, Kansas, 67209; telephone: (316) 946-4175; facsimile: (316) 946-4452. The report must include the condition found, date of inspection, and the serial number of the airplane. Information collection requirements contained in this regulation have been approved by the Office of Management and Budget (OMB) under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C. 3501 et seq.) and have been assigned OMB Control Number 2120-0056. (1) For airplanes on which the inspection is accomplished after the effective date of this AD: Submit the report within 10 days after performing the inspection required by paragraph (a) of this AD. (2) For airplanes on which the inspection has been accomplished prior to the effective date of this AD: Submit the reportwithin 10 days after the effective date of this AD. (d) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. (e) An alternative method of compliance or adjustment of the compliance times that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office (ACO), 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas, 67209. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita ACO. NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. (f) The inspection required by this AD shall be done in accordance with Cessna Service Bulletin SB98-27-05,which incorporates the following pages: Pages Revision Level Date 1,2, 9 and 10 Revision 1 August 17, 1998 3 through 8 Original Issue June 1, 1998 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 Cessna Aircraft Company, P.O. Box 7706, Wichita, Kansas 67277. Copies may be inspected at the FAA, Central Region, Office of the Regional Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC. (g) This amendment becomes effective on December 18, 1998.

Related safety bulletins advice on the same designs, not orders

2022-12-06CE-19-01 R1 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure
2021-08-26AIR-21-16 · FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt Inspection
2019-02-12CE-19-01 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2018-07-19CE-18-23 · Passenger Compartment Equipment - Installation of F. Atlee Dodge Aircraft Services LLC. Folding Jump Seats

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 8, 2026. Connections as data: /graph/directive/98-25-03.json · aircraft systems.