77-14-19: Engine Pylon
FAA order 77-14-19 is an airworthiness directive in force since August 23, 1977. The FAA's subject line: Engine Pylon. 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
- McDonnell Douglas Corporation
- 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
- August 23, 1977
- Docket
- Unknown
- Replaced by
- 2000-22-14
- Status
- Historical
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (2,283 characters)
77-14-19\tMCDONNELL DOUGLAS: Amendment 39-2971. Applies to Model DC-9-10, -20, -30, -40, -50 series and VC-9C (DC-9-32) airplanes certificated in all categories, fuselage numbers, F/N-1 thru F/N-837, which correspond to the factory serial numbers listed in Douglas DC-9 Service Bulletin 54-30 dated January 19, 1977, or later FAA approved revisions.\n \n\tCompliance required as indicated.\n\n\tTo detect fatigue cracks and/or failure of the engine pylon front spar attachments and upper cap, accomplish the following: \n\n\t(a)\tWithin the next 1800 flight hours after the effective date of this AD, or before accumulating 9800 total flight hours, whichever occurs later, unless already accomplished within the last 1800 flight hours, and thereafter at intervals not to exceed 3600 flight hours from the last inspection, accomplish radiographic and ultrasonic or eddy current inspections in accordance with the instructions in Douglas Service Bulletin 54-30, dated January 19, 1977, or later FAA approved revision. \n\n\tFor those operators who have conducted only the radiographic inspections per Douglas All Operators Letter, AOL 9-835, dated October 30, 1974, perform the ultrasonic or eddy current inspection, and thereafter, the radiographic and ultrasonic or eddy current inspection per the requirements of this AD, as applicable. \n\n\t(b)\tIf cracks or failures are found, before further flight, accomplish the modification described in Condition II in Douglas Service Bulletin 54-30 in accordance with the instructions in Douglas Service Bulletin 54-30, dated January 19, 1977, or later FAA approved revision. \n\n\t(c)\tThe inspections required by paragraph (a) may be discontinued for that pylon(s) upon accomplishment of either or both modifications (Condition I; Condition II) specified in Douglas Service Bulletin 54-30, dated January 19, 1977, or later FAA approved revision. \n\n\t(d)\tEquivalent inspection procedures and modifications may be used when approved by the Chief, Aircraft Engineering Division, FAA Western Region.\n \n\t(e)\tSpecial flight permits may be issued in accordance with FARs 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections required by this A.D.\n \n\tThis amendment becomes effective August 23, 1977.
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/77-14-19.json · aircraft systems.
