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87-23-01: Wire Bundles

FAA order 87-23-01 is an airworthiness directive in force since December 10, 1987. The FAA's subject line: Wire Bundles. 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: electrical power.

What it applies to as the FAA lists it

Kind of product
Appliance
Makes
The Boeing Company; Heath Tecna
Models
747-100 Series, 747-100B Series, 747-100B SUD Series, 747-200B Series, 747-200C Series, 747-200F Series, 747-300 Series, 747-400 Series, 747-400D Series, 747-400F Series, 747SP Series, 747SR Series, Wire Bundles
On this site
Boeing 747 192 registered

Dates and paperwork

In force since
December 10, 1987
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 (2,030 characters)
87-23-01 HEATH TECNA: Amendment 39-5759. Applies to Boeing Model 747 airplanes, certificated in any category, that have been modified in accordance with Supplemental Type Certificate SA2365NM, listed in Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987. Compliance required as indicated, unless previously accomplished.\n \n\tTo minimize fire hazard caused by chafing of ceiling light wire bundles, accomplish the following:\n \n\tA.\tWithin 60 days after the effective date of this AD, inspect lighting wire bundles which rest atop the Heath Tecna "Superbins" for evidence of damage and chafing, and repair, if necessary, before further flight; and accomplish either 1. or 2., below: \n\n\t\t1.\tInstall spacers to protect lighting wire bundles from chafing in accordance with Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987, or later FAA-approved revision. \n\n\t\t2.\tTrim the outboard edges of the ceiling panels in accordance with paragraph 2C of Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987, or later FAA-approved revision. \n\n\tB.\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\tC.\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 the modification required by this AD. \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 Heath Tecna Aerospace Company, 19819 84th Avenue South, Kent, Washington 98032. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington 98108.\n \n\tThis amendment becomes effective December 10, 1987.

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/87-23-01.json · aircraft systems.