AD 2000-22-15

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747-100, -200B, -200C, -200F, and -300 Series Airplanes Delivered In or Modified Into the Stretched Upper Deck Configuration

AD Number
2000-22-15
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 2000-NM-136-AD
FR Citation
65 FR 66607

Applicability

TypeManufacturerModelDetails
aircraft Boeing 747-100 Airworthiness Directives; Boeing Model 747-100, -200B, -200C, -200F, and -300 Series Airplanes Delivered In or Modified Into the Stretched Upper Deck Configuration

Unsafe Condition

Chafing between certain engine thrust control cables and cable penetration holes, which could lead to cable failure and a severe asymmetric thrust condition during landing, reducing controllability.

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

Required Actions

Inspect the clearance between engine thrust control cables and cable penetration holes; measure the clearance; perform additional inspection for cable wear if insufficient clearance is found; replace the cable if 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

Boeing Model 747-100, -200B, -200C, -200F, and -300 series airplanes delivered in or modified into the stretched upper deck configuration.

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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