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84-21-03: Fitting Assembly (Rod End) Inspection

FAA order 84-21-03 is an airworthiness directive in force since November 26, 1984. The FAA's subject line: Fitting Assembly (Rod End) Inspection. It names Douglas DC-9, Mcdonnell Douglas DC-9: about 100 aircraft on the U.S. register today across them, 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
DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-32F (C-9A), DC-9-32F (C-9B), DC-9-33F, DC-9-34, DC-9-34F, DC-9-41, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87)
On this site
Douglas DC-9 7 registered
Mcdonnell Douglas DC-9 93 registered

Dates and paperwork

In force since
November 26, 1984
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 (2,052 characters)
84-21-03 McDONNELL DOUGLAS: Amendment 39-4939. Applies to McDonnell Douglas Model DC-9, and C-9 (Military) series airplanes, certificated in all categories. Compliance required as indicated unless previously accomplished. To prevent jamming of the elevator controls by a detached forward rod end, accomplish the following: \n\n\tA.\tWithin the next 650 hours time in service or 90 calendar days, whichever occurs first after the effective date of this AD, visually inspect the fitting assembly (rod end) part number (P/N) 3938704-1 and pushrod P/N 3938705-501, in accordance with McDonnell Douglas DC-9 Alert Service Bulletin A27-266, dated March 12, 1984, hereinafter referred to as ASB27-266, or later FAA approved revisions. \n\n\tB.\tIf results of visual inspection are satisfactory, accomplish paragraph 4 of Part 2, Accomplishment Instructions, of ASB27-266. \n\n\tC.\tIf results of visual inspection are unsatisfactory, proceed in accordance with paragraph 5, Accomplishment Instructions of ASB27-266. \n\n\tNOTE: If rod end P/N SM4-6T3 (exclude DC-9-80 series) is required and not available, P/N SM4-6T may be substituted. The latter has only one grease fitting which must be oriented to allow access for scheduled lubrication. \n\n\tD.\tAlternative inspections, modifications, or other actions which provide an equivalent level of safety may be used when approved by the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tAll persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Los Angeles Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California. \n\n\tThis amendment becomes effective November 26, 1984.

Related safety bulletins advice on the same designs, not orders

2019-02-19NE-19-03 · Escape Slide Maintenance Tasks and Intervals - JASC 2565
2014-11-24NM-15-03 · Flight Controls
2008-09-03NM-08-43 · Cabin Equipment/Furnishings - Seats
2006-07-27NM-06-57 · Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.

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/84-21-03.json · aircraft systems.