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2002-17-01: Foot Warm circuit breaker

FAA order 2002-17-01 is an airworthiness directive in force since September 12, 2002. The FAA's subject line: Foot Warm circuit breaker. It names Learjet 45: about 432 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
Learjet Inc.
Models
45
On this site
Learjet 45 432 registered

Dates and paperwork

In force since
September 12, 2002
Published
August 28, 2002 (signed August 20, 2002)
Docket
2002-NM-167-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 is applicable to certain Learjet Model 45 airplanes. This action requires pulling the FOOT WARM circuit breaker located on the copilot's circuit breaker panel, and installing a collar on that circuit breaker. This action is necessary to prevent an electrical short circuit between the pilot's and copilot's foot warmers and the composite floorboards, which could result in outgassing of the faceply material of the composite floorboards, and consequent smoke in the cockpit. This action is intended to address the identified unsafe condition.

The order itself the regulatory text, as published

Show the full text (3,208 characters)
2002-17-01 Learjet: Amendment 39-12866. Docket 2002-NM-167-AD. Applicability: Model 45 airplanes, serial numbers 45-005 through 45-213 inclusive; certificated in any category. 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 (b) 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 as indicated, unless accomplished previously. Toprevent an electrical short circuit between the pilot's and copilot's foot warmers and the composite floor boards, which could result in outgassing of the faceply material of the composite floorboards, and consequent smoke in the cockpit, accomplish the following: Circuit Breaker Deactivation and Collar Installation (a) Within 25 flight hours after the effective date of this AD, pull the FOOT WARM circuit breaker located on the copilot's circuit breaker panel, and install a collar on the FOOT WARM circuit breaker, per Learjet Alert Service Bulletin SB A45-21-14, dated May 3, 2002. Alternative Methods of Compliance (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Wichita Aircraft Certification Office (ACO), FAA. Operators shall submit their requests through an appropriate FAA Principal 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. Special Flight Permits (c) 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. Incorporation by Reference (d) The actions shall be done in accordance with Learjet Alert Service Bulletin SB A45-21-14, dated May 3, 2002. 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 Learjet, Inc., One Learjet Way, Wichita, Kansas 67209- 2942. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Effective Date (e) This amendment becomes effective on September 12, 2002.

Related safety bulletins advice on the same designs, not orders

2021-09-16AIR-21-15R1 · Navigation System
2021-08-26AIR-21-15 · Navigation System

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/2002-17-01.json · aircraft systems.