92-08-05: AFT Galley Tire Rods
FAA order 92-08-05 is an airworthiness directive. The FAA's subject line: AFT Galley Tire Rods. It names Boeing 767: about 585 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: landing gear.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- The Boeing Company
- Models
- 767-200 Series, 767-300 Series, 767-300F Series
- On this site
- Boeing 767 585 registered
Dates and paperwork
- Docket
- 91-NM-249-AD
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (2,159 characters)
92-08-05 BOEING: Amendment 39-8216. Docket No. 91-NM-249-AD.\n\n\tApplicability: Model 767 series airplanes listed in Boeing Service Bulletin 767-25-0160, dated July 18, 1991; and airplane having variable number VF093; certificated in any category.\n\n\tCompliance: Required within 60 days after the effective date of this AD, unless previously accomplished.\n\n\tTo prevent the galley from coming loose during an emergency landing, accomplish the following:\n\n\t(a)\t Replace the aft galley tie rods in accordance with Boeing Service Bulletin 767-25-0160, dated July 18, 1991; or Revision 1, dated February 13, 1992.\n\n\t(b)\tAn alternative method of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. The request shall be forwarded through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Seattle ACO.\n\n\t(c)\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.\n\n\t(d)\tThe modification shall be done in accordance with Boeing Service Bulletin 767-25-0160, dated July 18, 1991; or Revision 1, dated February 13, 1992; which include the following list of effective pages:\n\nService Bulletin\tPage Number\tRevision Level\tDate\n\n767-25-0160\t1-9\tOriginal\tJuly 18, 1991\nOriginal\n\n767-25-0160\t1, 3, 4, 5\t1\tFebruary 13, 1992 \nRevision 1\n\t2, 6, 7, 8, 9\tOriginal\tJuly 18, 1991\n\nThis 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 Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. Copies may be inspected at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington; or at theOffice of the Federal Register, 1100 L Street NW., Room 8401, Washington, DC.\n\n\t(e)\tThis amendment becomes effective on June 23, 1992.
Related safety bulletins advice on the same designs, not orders
2020-04-16NM-20-07 · Navigation - Glideslope System
2018-12-17NM-18-33 · Engine Fuel and Control
2017-06-19NM-17-17 · Oxygen System
2017-04-13NM-17-10 · Maintenance Practices
2017-03-09NM-17-09 · Flight Control 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/92-08-05.json · aircraft systems.
