89-14-10: Engine Mount Cone Bolts
FAA order 89-14-10 is an airworthiness directive in force since July 17, 1989. The FAA's subject line: Engine Mount Cone Bolts. 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: engine.
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
- On this site
- Douglas DC-9 7 registered
Mcdonnell Douglas DC-9 93 registered
Dates and paperwork
- In force since
- July 17, 1989
- 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 (2,609 characters)
89-14-10 McDONNELL DOUGLAS: Amendment 39-6253. \n\n\tApplicability: Model DC-9-10, -20, -30, -40, -50, and C-9 series airplanes, certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo prevent premature fatigue failure of engine mount cone bolts, accomplish the following: \n\n\tA.\tWithin 90 days after the effective date of this AD, determine if forward engine mount cone bolts, Barry Controls part number R18210-2, serial numbers 15B8021 through 15B8329, 15B8332 through 15B8382, 15B8396 through 15B8399; or aft engine mount cone bolt, Barry Controls part number R18211-2, serial numbers 15B5242 through 15B5320; are installed. \n\n\tNOTE: This determination may be accomplished by conducting either a thorough review of receiving inventory and/or maintenance records, or a visual inspection of each installed cone bolt. \n\n\tB.\tIf any of the cone bolts identified in paragraph A., above, are installed, or if a determination of the installation of discrepant bolts cannot be made, remove the cone bolt(s) and replace it with a properly heat-treated cone bolt within 2,000 flight hours after installation or 15 days after discovery, whichever occurs later, in accordance with McDonnell Douglas Service Bulletin 71-46, dated April 24, 1989. \n\n\tC.\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, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tNOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Los Angeles Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tD.\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\tAll persons affected by this directive whohave not already received the appropriate service documents from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publication and Training, C1-750 (54-60). These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Los Angeles Aircraft Certification Office, 3229 East Spring Street, Long Beach, California. \n\n\tThis amendment (39-6253, AD 89-14-10) becomes effective on July 17, 1989.
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 October 30, 2026. Connections as data: /graph/directive/89-14-10.json · aircraft systems.
