# AD 92-27-11 R1: Engine Emergency Fire Extinguisher - Type: Airworthiness directive - Status: Current - Products: Boeing MD-11 and MD-11F - Effective: February 8, 1993 - Superseded by: Nothing supersedes this AD - Product type: Aircraft, Large airplane - Amendment: 39-8491 - Docket: 93-NM-07-AD - Registered aircraft: 108 may be affected, by airframe or engine model (OpenAirDocs) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/61D42BC2259FEAAE86256A080065CD93.0001 - DRS record last changed: May 30, 2024 - Page: https://openairdocs.org/ad/92-27-11-R1 ## The airworthiness directive 92-27-11 R1 MCDONNELL DOUGLAS: Amendment 39-8491. Docket 93-NM-07-AD. Revises AD 92-27-11, Amendment 39-8446. Applicability: McDonnell Douglas Model MD-11 and MD-11F series airplanes; as listed in McDonnell Douglas MD-11 Alert Service Bulletin A76-3, dated November 17, 1992; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent inhibited operation of the engine emergency fire extinguisher system, accomplish the following: (a) Within 30 days after the effective date of this AD, perform a functional inspection for proper actuation of the fire bottle switch, and a visual inspection of the fire shutoff handle cover assembly to verify whether a minimum clearance of 0.030 inch (0.76 mm) exists between the fire shutoff handles, cover assembly, and rub strips in the flight compartment, in accordance with the Accomplishment Instructions of McDonnell Douglas MD-11 Alert Service Bulletin A76-3, dated November 17, 1992. (1) If any fire bottle switch actuates (audible click), and if any handle clearance is found to be 0.030 inch (0.76 mm) or greater, no further action is necessary; or (2) If any fire bottle switch does not actuate (click is not audible), and/or any handle clearance is not found to be 0.030 inch (0.76 mm) or greater, prior to further flight, trim the cover assembly handle cutout and rub strips to achieve a clearance of 0.030 inch (0.76 mm) or greater, and repeat the functional inspection requirements for proper switch actuation in accordance with paragraph (a) of this AD. (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, Los Angeles Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, LosAngeles ACO. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Manager, Los Angeles ACO. (c) 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. (d) The functional inspection and trim shall be done in accordance with McDonnell Douglas MD-11 Alert Service Bulletin A76-3, dated November 17, 1992. This incorporation by reference was approved previously by the Director of the Federal Register, in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51, as of January 13, 1993 (57 FR 61791, December 29, 1992). Copies may be obtained from McDonnell Douglas Corporation, P.O. Box 1771, Long Beach, California 90846-1771, Attention: Business Unit Manager, Technical Publications - Technical Administrative Support, C1-L5B. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at FAA, Transport Airplane Directorate, Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on February 8, 1993. ## Affected data sheets (1) (OpenAirDocs) The type certificate data sheets whose models the AD names. - [TCDS A22WE](https://openairdocs.org/tcds/A22WE): The Boeing Company; names 2 of 11 models: MD-11, MD-11F ## Registered aircraft it may apply to (OpenAirDocs) Matched by airframe and engine model; the AD's applicability may narrow it by serial number, part number or equipment. - Aircraft: 108 (108 by airframe model, 0 by engine model) - Makers: Mcdonnell Douglas 104, Boeing 4 Models with the most aircraft: - [Mcdonnell Douglas MD-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f): 100 aircraft (airframe model) - [Mcdonnell Douglas MD-11](https://openairdocs.org/model/mcdonnell-douglas-md-11): 4 aircraft (airframe model) - [Boeing MD-11F](https://openairdocs.org/model/boeing-md-11f): 4 aircraft (airframe model) All 3 models: https://openairdocs.org/ad/92-27-11-R1/models.md Every aircraft: https://openairdocs.org/ad/92-27-11-R1/aircraft.md Its text cites no advisory circulars or STCs. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.