AD 2002-24-05

final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 727 Series Airplanes

AD Number
2002-24-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-271-AD
FR Citation
67 FR 71808

Applicability

TypeManufacturerModelDetails
aircraft Boeing 727 Airworthiness Directives; Boeing Model 727 Series Airplanes

Unsafe Condition

Stress corrosion cracking of the upper chord of the rear spar of the wing between Wing Butt Line (WBL) 70.5 and the wing tip, which could result in structural failure of the wing and fuel leaks in the airplane.

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

Required Actions

Perform repetitive external detailed inspections to detect cracking and corrosion of the upper chord of the rear spar of the wing, repair any detected cracking and corrosion, inspect for any cracking that has been previously repaired by stop-drilling, and permanently repair any previously stop-drilled cracking.

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 727 series airplanes, serial numbers 1 through 1832 inclusive, 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 4, 2026

Rights: U.S. Government Public Domain

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View Official Source ↗ Find More ADs for Boeing 727

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