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84-24-04: Emergency Evacuation Slide/Rafts

FAA order 84-24-04 is an airworthiness directive in force since December 17, 1984. The FAA's subject line: Emergency Evacuation Slide/Rafts. It names Boeing 747: about 192 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: emergency equipment.

What it applies to as the FAA lists it

Kind of product
Appliance
Makes
BFGoodrich; The Boeing Company
Models
Emergency Evacuation Slide/Rafts, 747-100 Series, 747-100B Series, 747-100B SUD Series, 747-200B Series, 747-300 Series, 747SR Series
On this site
Boeing 747 192 registered

Dates and paperwork

In force since
December 17, 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 (2,179 characters)
84-24-04 BF GOODRICH: Amendment 39-4960. Applies to BF Goodrich Emergency Evacuation Slide/Rafts P/N's 7A1340 series, 7A1342 series, 7A1371 series, and 7A1373 series installed on Boeing Model 747-100 and 747-200B airplanes in accordance with Supplemental Type Certificate (STC) SA574GL, and on Boeing Model 747-100B, 747SR, and 747-300 airplanes in accordance with STC SA575GL; and BF Goodrich Emergency Evacuation Slide/Rafts P/N's 7A1437 series, 7A1439 series, 7A1447 series, and 7A1448 series installed on Boeing Model 747-100 and 747-200B airplanes in accordance with STC SA744GL, and on Boeing Model 747-100B, 747SR, and 747-300 airplanes in accordance with STC SA745GL. \n\n\tCompliance is required as indicated, unless already accomplished. \n\n\tInspect and replace, as required, the girt bar attachment assemblies in accordance with the following: \n\n\tA.\tWithin the next 15 days after the effective date of this airworthiness directive (AD), inspect the applicable slide/rafts and replace the girt bar attachment assemblies in accordance with the procedures contained in BF Goodrich Alert Service Bulletin 25-093, Revision 1, dated November 21, 1984, or subsequent FAA approved revisions. \n\n\tB.\tDestroy the replaced girt bar attachment assemblies to preclude their installation at a later date. \n\n\tC.\tAlternate means of compliance with this AD which provide an equivalent level of safety may be used when approved by the Manager, Chicago Aircraft Certification Office, FAA, Central 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 for the accomplishment of inspections and/or modifications required by this AD. \n\n\tAll persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to BF Goodrich Company, Attn: Mr. David Smith, Dept. 1809, Bldg. 17F, 500 South Main Street, Akron, Ohio 44318; telephone (216) 374-2886. These documents also may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington. \n\n\tThis amendment becomes effective December 17, 1984.

Related safety bulletins advice on the same designs, not orders

2020-11-16AIR-20-18 · Flight Management Computing Software System
2020-04-16NM-20-07 · Navigation - Glideslope System
2018-12-17NM-18-33 · Engine Fuel and Control
2017-04-13NM-17-10 · Maintenance Practices
2014-11-24NM-15-03 · Flight Controls

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/84-24-04.json · aircraft systems.