AD 2002-05-07

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes

AD Number
2002-05-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-NM-21-AD
FR Citation
67 FR 11891

Applicability

TypeManufacturerModelDetails
aircraft Boeing 737-100 Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes

Unsafe Condition

Discrepancies of the rear spar attachments and cracks in the upper flange of the inboard track at the rear spar attachment of each outboard flap could result in loss of the outboard trailing edge flaps and consequent reduced controllability of the airplane.

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

Required Actions

For certain airplanes, repetitive inspections for discrepancies of the rear spar attachments and cracks in the upper flange of the inboard track are required, followed by rework of the flap track assembly and rear spar attachments, including replacement of the flap track if necessary. For all airplanes, repetitive inspections for cracks in the upper flange of the inboard flap tracks at the rear spar attachments are required, with corrective action taken if necessary.

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

Compliance Time

Not specified in the provided text.

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

Affected Aircraft

Boeing Model 737-100, -200, -200C, -300, -400, and -500 series 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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