AD 84-03-06

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series

AD Number
84-03-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-100B Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-100B SUD Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-200B Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-200C Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-200F Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-300 Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-400 Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-400D Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series
aircraft The Boeing Company 747-400F Series Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series

Unsafe Condition

The installation of certain components listed by serial number in Table I of this AD in the landing gear assembly could result in failure of the fuel tank pump conduits due to inadequate design or manufacturing conformity.

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

Required Actions

Within 180 days from the effective date, determine if any components listed in Table I are installed. Replace affected components with approved parts before further flight. Prohibit future use of listed components unless manufacturer confirms conformity to type design.

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

Compliance Time

within 180 days from 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 (747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-SP series) and McDonnell Douglas Model DC-9 and DC-10 series airplanes. Components purchased prior to January 1, 1979, or obtained from Boeing, Douglas, or Cleveland Pneumatics as spares are excluded.

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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