AD 2007-04-06

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8-63F Airplanes

AD Number
2007-04-06
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2006-26084
FR Citation
72 FR 6921

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-8-62 Airworthiness Directives; McDonnell Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8-63F Airplanes

Unsafe Condition

The thrust reverser systems do not adequately preclude inadvertent deployment of the thrust reversers.

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

Required Actions

Revise the wiring for the engine thrust brake circuit and indicating circuit, or reroute the wiring at plug P1-1762A on the electrical power center generator control panel, as necessary.

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

Compliance Time

Before further flight.

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

Affected Aircraft

McDonnell Douglas Model DC-8-62, DC-8-63, DC-8-62F, and DC-8-63F airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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