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FAA orders · airworthiness directive · current

2009-03-01: Lavatory light assembly

FAA order 2009-03-01 is an airworthiness directive in force since March 5, 2009. The FAA's subject line: Lavatory light assembly. It names Learjet 55: about 67 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: emergency equipment.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Learjet Inc.
Models
55, 55B, 55C
On this site
Learjet 55 67 registered

Dates and paperwork

In force since
March 5, 2009
Published
February 18, 2009 (signed January 21, 2009)
Docket
FAA-2009-0054
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for certain Learjet Model 55, 55B, and 55C airplanes. This AD requires inspecting the installation of the forward light assembly in the aft lavatory to determine the location of the terminal connector; inspecting for damage of the light assembly terminals, wires, and oxygen lines; inspecting to determine if the cable nipple is installed over the light assembly terminal; and doing corrective actions if necessary. This AD also requires installing a clamp to the forward side of the frame to maintain a positive distance between the light assembly and oxygen line. This AD results from a report of a cabin fire in the left-hand upper cabin fuselage above the aft cabin window at frame 23. We are issuing this AD to detect and correct improper installation of the lavatory light assembly, which could result in contact between the electrical terminals of the light assembly and an adjacent oxygen supply line, and consequent short circuit or fire hazard.

The order itself the regulatory text, as published

Show the full text (5,034 characters)
2009-03-01 Learjet: Amendment 39-15802. Docket No. FAA-2009-0054; Directorate Identifier 2008-NM-222-AD. Effective Date (a) This airworthiness directive (AD) is effective March 5, 2009. Affected ADs (b) None. Applicability (c) This AD applies to Learjet Model 55, 55B, and 55C airplanes, certificated in any category; serial numbers 002 through 147 inclusive. Subject (d) Air Transport Association (ATA) of America Code 25: Equipment/Furnishings. Unsafe Condition (e) This AD results from a report of a cabin fire in the left- hand upper cabin fuselage above the aft cabin window at frame 23. We are issuing this AD to detect and correct improper installation of the lavatory light assembly, which could result in contact between the electrical terminals of the light assembly and an adjacent oxygen supply line, and consequent short circuit or fire hazard. Compliance (f) Comply with this AD within the compliance times specified, unless already done. Inspections, Corrective Actions, and Installation (g) Within 30 days or 25 flight hours after the effective date of this AD, whichever occurs first, do the actions specified in paragraphs (g)(1) and (g)(2) of this AD. Do the actions in accordance with the Accomplishment Instructions of Bombardier Alert Service Bulletin A55-25-7, dated December 17, 2008. (1) Do a general visual inspection of the installation of the forward light assembly in the aft lavatory to determine the location of the terminal connector; do a general visual inspection for damage of the light assembly terminals, wires, and oxygen lines; do a general visual inspection to determine if the cable nipple is installed over the light assembly terminal; and do all applicable corrective actions. Do all applicable corrective actions before further flight. 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 otherwise specified. 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.'' (2) Install a clamp and hardware to the forward side of the frame to maintain the distance specified in Bombardier Alert Service Bulletin A55-25-7, dated December 17, 2008, between the light assembly and oxygen line. No Reporting (h) Although Bombardier Alert Service Bulletin A55-25-7, dated December 17, 2008, specifies to submit certain information to the manufacturer, this AD does not include that requirement. Alternative Methods of Compliance (AMOCs) (i)(1) The Manager, Wichita Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Daniel Hilton, Aerospace Engineer, Electrical Systems and Avionics Branch, ACE-119W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4173; fax (316) 946-4107. (2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office (FSDO). The AMOC approval letter must specifically reference this AD. Material Incorporated by Reference (j) You must use Bombardier Alert Service Bulletin A55-25-7, dated December 17, 2008, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Learjet, Inc., One Learjet Way, Wichita, Kansas 67209-2942; telephone 316-946-2000; fax 316-946-2220; e-mail [email protected]; Internet http://www.bombardier.com. (3) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221 or 425-227-1152. (4) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal_register/code_of_federal_ regulations/ibr_locations.html.

Related safety bulletins advice on the same designs, not orders

2026-03-192026-07 · MAIN LANDING GEAR ATTACH SECTION, Trunnion Pins
2016-09-15NM-16-24 · Fuselage: Main Plate/Skin

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 27, 2026. Connections as data: /graph/directive/2009-03-01.json · aircraft systems.