AD 87-23-01

final rule
Data completeness: 70%

Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.

AD Number
87-23-01
Status
final_rule
Effective Date
Product Category
appliance
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company | Heath Tecna 747-100 Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-100B Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-100B SUD Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-200B Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-200C Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-200F Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-300 Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-400 Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-400D Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.
aircraft The Boeing Company | Heath Tecna 747-400F Series Airworthiness Directives; Heath Tecna Service Bulletin 74000-25-007, dated March 6, 1987.

Unsafe Condition

Chafing of ceiling light wire bundles causing fire hazard.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect lighting wire bundles atop the Heath Tecna 'Superbins' for damage and chafing within 60 days after the effective date, repair before further flight, and either install spacers per SB 74000-25-007 or trim ceiling panel edges per paragraph 2C of the SB.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 60 days after the effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Boeing Model 747 airplanes modified under Supplemental Type Certificate SA2365NM and listed in Heath Tecna Service Bulletin 74000-25-007.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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