AD 2003-23-03

Recurring final rule
Data completeness: 70%

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

AD Number
2003-23-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-150-AD
FR Citation
68 FR 64980

Applicability

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

Unsafe Condition

Discrepancies in the upper and lower skins of the fuselage lap joint and circumferential joint, which could result in sudden fracture and failure of a lap joint or circumferential joint and rapid decompression of the airplane fuselage.

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

Required Actions

Perform initial and repetitive inspections as specified in Figures 1 through 9 of Boeing Alert Service Bulletin 737-53A1224, Revision 1, dated March 14, 2002, to detect discrepancies in the fuselage lap joint and circumferential joint. Repair any discrepancies detected in accordance with the service bulletin or an approved method. Accomplish a terminating modification as specified in the AD.

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

Compliance Time

Within the intervals specified in the service bulletin after the effective date of this AD.

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

Affected Aircraft

Boeing Model 737-100, -200, and -200C series airplanes; line numbers 1 through 291 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 6, 2026

Rights: U.S. Government Public Domain

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