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2005-24-13: Electrical wire bundle for the alternator on the left-hand engine

FAA order 2005-24-13 is an airworthiness directive in force since December 20, 2005. The FAA's subject line: Electrical wire bundle for the alternator on the left-hand engine. It names Learjet 45: about 433 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Learjet Inc.
Models
45
On this site
Learjet 45 433 registered

Dates and paperwork

In force since
December 20, 2005
Published
December 5, 2005 (signed November 18, 2005)
Docket
FAA-2005-23144
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain Learjet Model 45 airplanes. This AD requires modifying the electrical wire bundle for the alternator on the left-hand engine, inspecting for clearance between wire harnesses and engine tubing for each engine, and corrective actions if necessary. For certain airplanes, this AD also requires replacing the fuses for the hydraulic shutoff valves with fuses having higher amperage. This AD results from a report of a fire in the left-hand engine nacelle. We are issuing this AD to prevent chafing between the wire bundle for the alternator on each engine and the hydraulic lines, which could result in a fire in the engine nacelle.

The order itself the regulatory text, as published

Show the full text (5,016 characters)
2005-24-13 Learjet: Amendment 39-14393. Docket No. FAA-2005-23144; Directorate Identifier 2005-NM-218-AD. Effective Date (a) This AD becomes effective December 20, 2005. Affected ADs (b) None. Applicability (c) This AD applies to Learjet Model 45 airplanes, certificated in any category; serial numbers (S/Ns) 45-005 through 45-273 inclusive, and 45-2001 through 45-2029 inclusive. Unsafe Condition (d) This AD results from a report of a fire in the left-hand engine nacelle. We are issuing this AD to prevent chafing between the wire bundle for the alternator on each engine and the hydraulic lines, which could result in a fire in the engine nacelle. Compliance (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Modification (f) Within 50 flight hours after the effective date of this AD: Modify the electrical wire bundle for the alternator on the left- hand engine; and do a general visual inspection of the left and right engines to make sure that the proper clearances are maintained between all wiring harnesses and engine tubing. Correct improper clearances before further flight. Do all actions in accordance with the Accomplishment Instructions of the applicable service bulletin in paragraph (f)(1) or (f)(2) of this AD. (1) For Learjet Model 45 airplanes with S/Ns 45-2001 through 45- 2029 inclusive: Bombardier Alert Service Bulletin SB A40-71-01, dated September 29, 2005. (2) For Learjet Model 45 airplanes with S/Ns 45-005 through 45- 273 inclusive: Bombardier Alert Service Bulletin SB A45-71-4, dated September 29, 2005. Note 1: For the purposes of this AD, a general visual inspection is: "A visual examination of an interior or exterior area, installation, or assembly to detect obvious damage, failure, or irregularity. This level of inspection is made from within touching distance unless otherwisespecified. A mirror may be necessary to ensure visual access to all surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight, or droplight and may require removal or opening of access panels or doors. Stands, ladders, or platforms may be required to gain proximity to the area being checked." Concurrent Requirement (g) For airplanes with S/Ns identified in paragraphs (g)(1) and (g)(2) of this AD: Before or concurrently with the modification required by paragraph (f) of this AD, replace the fuses for the hydraulic shutoff valves with fuses having higher amperage in accordance with the Accomplishment Instructions of the applicable service bulletin in paragraph (g)(1) or (g)(2) of this AD. (1) For Learjet Model 45 airplanes with S/Ns 45-2001 through 45- 2015 inclusive: Bombardier Service Bulletin SB 40-24-01, dated April 22, 2005. (2) For Learjet Model 45 airplanes with S/Ns 45-005 through 45- 254 inclusive: Bombardier Service Bulletin SB 45-24-6, dated April 22, 2005. No Reporting Requirement (h) Although Bombardier Alert Service Bulletin SB A40-71-01, dated September 29, 2005; and Bombardier Alert Service Bulletin SB A45-71-4, dated September 29, 2005; specify sending a compliance report to the manufacturer, this AD does not include that requirement. Alternative Methods of Compliance (AMOCs) (i)(1) The Manager, Wichita Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with Sec. 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Material Incorporated by Reference (j) You must use the service information listed in Table 1 of this AD to perform the actions thatare required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Learjet, Inc., One Learjet Way, Wichita, Kansas 67209-2942, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html . Table 1.--Material Incorporated by Reference Bombardier service bulletin Date Alert Service Bulletin SB A40 71 01. September 29, 2005. Alert Service Bulletin SB A45 71 4. September 29, 2005. Service Bulletin SB 40 24 01. April 22, 2005. Service Bulletin SB 45 24 6. April 22, 2005.

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 October 26, 2026. Connections as data: /graph/directive/2005-24-13.json · aircraft systems.