AD 94-05-07

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747 Series Airplanes

AD Number
94-05-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
93-NM-09-AD
FR Citation
(Federal Register: March 04, 1994 (Volume 59, Number 43))

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-100B Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-100B SUD Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-200B Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-200C Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-200F Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-300 Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747SP Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747SR Series Airworthiness Directives; Boeing Model 747 Series Airplanes

Unsafe Condition

Damage due to chafing of wire bundles above the P6 panel around station 400, water line 385, right buttock line 25, specifically bundles W418, W718, W998, W1100, and W1362, leading to potential smoke and fire in the cockpit and loss of essential cockpit instruments necessary for continued safe flight and landing.

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

Required Actions

Perform a visual inspection to detect chafing damage on specified wire bundles, repair or replace damaged wires, measure clearance between wire bundles, and install modifications per Boeing Alert Service Bulletin 747-24A2186 or Revision 1. Repeat inspections every 120 days if clearance is less than 0.25 inch until terminating actions are completed.

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

Compliance Time

Within 15 days after January 8, 1993 for initial inspection under paragraph (a), and within the next 4,000 flight hours after the effective date of this AD (April 4, 1994) for requirements under paragraph (b).

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

Affected Aircraft

Boeing Model 747 series airplanes excluding Model 747-400 series, certificated in any category.

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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