AD 2008-17-03

Recurring final rule
Data completeness: 80%

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

AD Number
2008-17-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2007-29174
FR Citation
73 FR 48288

Applicability

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

Unsafe Condition

Cracking of the body station 303.9 frame, inboard of stringer 16L, could prevent the left forward entry door from sealing correctly and could cause in-flight decompression.

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

Required Actions

Conduct repetitive inspections to detect cracking of the body station 303.9 frame. Take corrective action if cracking is found. Optional terminating action is provided for the repetitive inspections.

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

Compliance Time

Within 2,250 flight cycles after the effective date of the AD.

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 4, 2026

Rights: U.S. Government Public Domain

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