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88-20-07: Pivot Trunnion

FAA order 88-20-07 is an airworthiness directive in force since November 1, 1988. The FAA's subject line: Pivot Trunnion. It names Boeing 727: about 37 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
The Boeing Company
Models
727-100 Series, 727-100C Series, 727-200 Series, 727-200F Series, 727 Series, 727C Series
On this site
Boeing 727 37 registered

Dates and paperwork

In force since
November 1, 1988
Docket
Unknown
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 (2,166 characters)
88-20-07 BOEING: Amendment 39-6024. Applies to all Model 727 series airplanes, certificated in any category.\n \n\tCompliance required as indicated, unless previously accomplished. \n\n\tTo prevent jamming of the main landing gear door actuator caused by fracturing of the pivot trunnion, accomplish the following: \n\n\tA.\tWithin the next 1,600 flight cycles after the effective date of this AD, accomplish the visual inspection of the main landing gear door actuator pivots in accordance with Boeing Service Bulletin 727-32-0358, dated May 31, 1988. Repeat this inspection at intervals not to exceed 800 flight cycles. \n\n\tB.\tIf any of the pivot trunnion shafts are found loose or missing during the inspection performed in accordance with paragraph A., above, prior to further flight, replace the pivot in accordance with Boeing Service Bulletin 727-32-0358, dated May 31, 1988. \n\n\tC.\tAccomplishing the pivot replacement with a part number 3-3141-54 pivot, in accordance with Sargent Controls Service Bulletin 7-3141-32-06, Revision 1, dated November 2, 1987, constitutes terminating action for the initial and repetitive inspections required by paragraph A., above. \n\n\tD.\tAn alternate means 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, FAA, Northwest Mountain Region. \n\n\tNOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who may add any comments and then send it to the Manager, Seattle Aircraft Certification Office. \n\n\tAll persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington, 98124. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington or Seattle Aircraft CertificationOffice, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington. \n\n\tThis Amendment, 39-6024, becomes effective November 1, 1988.

Related safety bulletins advice on the same designs, not orders

2014-11-24NM-15-03 · Flight Controls
2014-11-06NM-15-02 · Cabin Equipment/Furnishings
2010-01-07NM-10-13 · Navigation: Flight Management System
2006-07-19NM-06-56 ·
2002-03-13NE-02-18 · Air Cruisers Company Evacuation Slide and Slide/Raft Systems

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/88-20-07.json · aircraft systems.