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85-21-51: Elevator Actuator Rod End Bolt Retaining Nuts

FAA order 85-21-51 is an airworthiness directive in force since February 24, 1986. The FAA's subject line: Elevator Actuator Rod End Bolt Retaining Nuts. 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: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
The Boeing Company
Models
767-200 Series
On this site
Boeing 767 585 registered

Dates and paperwork

In force since
February 24, 1986
Published
February 4, 1986 (signed January 28, 1986)
Docket
85-NM-125-AD
Replaces
T85-21-51
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

This action publishes in the Federal Register and makes effective as to all persons an amendment adopting a new airworthiness directive (AD) which was previously made effective to all known U.S. owners and operators of certain Boeing Model 767-200 airplanes by individual telegrams. The AD requires inspection and replacement, if necessary, of self-locking nuts located in certain critical areas of the airplanes. This action was prompted by the discovery that two elevator actuator rod end bolt retaining nuts on one recently delivered Model 767 airplane did not have their intended self-locking feature. Such a nut could back off its mating bolt and result in a disconnection of the affected joint. Multiple disconnections of elevator to actuator joints could result in partial or complete loss of airplane control. These nuts have other critical applications on the Model 767 airplane, which are also addressed in the AD.

The order itself the regulatory text, as published

Show the full text (2,024 characters)
85-21-51 Boeing; Applies to Boeing Model 767-200 airplanes, certificated in any category. To prevent loss of certain critical airframe self-locking nuts, accomplish the following, unless previously accomplished:\n\n\tA. Within 35 landings or 10 days after the effective date of this AD, whichever occurs first, inspect the horizontal elevator self-locking nuts in accordance with Boeing Alert Service Bulleting 767-27A0064, dated October 25, 1985, or later FAA-approved revision. Self-locking nuts found to be insecure in accordance with the criteria specified in the service bulletin must be replaced before further flight with serviceable self-locking nuts.\n\n\tB. Within 50 landings or 20 days after the effective date of this AD, whichever occurs first, inspect the inboard aft trailing edge flap self-locking nuts and the outboard wing spoiler actuator self-locking nuts in accordance with Boeing Alert Service Bulletin 767-27A0064, dated October 25, 1985, or later FAA-approved revision.Self-locking nuts found to be insecure in accordance with the criteria specified in the service bulletin must be replaced before further flight with serviceable self-locking nuts.\n\n\tC. Alternate means of compliance which provide an acceptable level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.\n\n\tAll persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Company, P. O. Box 3707, Seattle, Washington 98124. This document may also be examined at FAA Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.\n\n\tThis amendment becomes effective February 24, 1986 as to all persons, except those persons to whom it was made immediately effective by telegraphic AD T85-21-51, issued October 25, 1985.

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/85-21-51.json · aircraft systems.