AD 2005-10-11

Recurring final rule
Data completeness: 80%

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

AD Number
2005-10-11
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2004-19531
FR Citation
70 FR 28419

Applicability

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

Unsafe Condition

Discrepancies of certain connectors located in the main wheel well could result in electrical arcing of the connectors, uncommanded closure of the engine fuel shut-off valves, and consequent in-flight loss of thrust or engine shutdown from lack of fuel.

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Required Actions

Modify the electrical connectors located in the main wheel well by following the Accomplishment Instructions of Boeing Special Attention Service Bulletin 737-28-1196, Revision 3, dated April 1, 2004. Any corrective action must be done before further flight in accordance with the service bulletin.

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Compliance Time

Within 12 months after the effective date of this AD for airplanes on which no inspection required by AD 2001-14-06 has been done as of the effective date of this AD. For airplanes on which any inspection required by AD 2001-14-06 has been done as of the effective date of this AD, the modification must be accomplished at the later of the times specified in paragraph (f)(2)(i) or (f)(2)(ii) of this AD.

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Affected Aircraft

All Boeing Model 737-300, -400, and -500 series airplanes, 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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