AD 2005-25-03

final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 737-600, -700, -700C, and -800 Series Airplanes

AD Number
2005-25-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-23176
FR Citation
70 FR 72595

Applicability

TypeManufacturerModelDetails
aircraft Boeing 737-600 Airworthiness Directives; Boeing Model 737-600, -700, -700C, and -800 Series Airplanes

Unsafe Condition

Failure of the point 'D' splice fitting between windows number 1 and 2 prior to the design service objective, which may result in cracking through the skin and consequent decompression of the flight cabin.

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Required Actions

Replace the point 'D' splice fitting between windows number 1 and 2 with a new splice fitting. Perform an eddy current inspection for cracking of the holes in the structure common to the new splice fitting. Take corrective actions if cracking is detected, in accordance with a method approved by the Manager, Seattle Aircraft Certification Office.

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Compliance Time

Before further flight

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Affected Aircraft

Boeing Model 737-600, -700, -700C, and -800 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin (ASB) 737-53A1222, Revision 2, dated October 20, 2005.

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Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

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