AD 2014-08-11

Recurring final rule
Data completeness: 70%

Airworthiness Directives; the Boeing Company Airplanes

AD Number
2014-08-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0690
FR Citation
79 FR 23903

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; the Boeing Company Airplanes

Unsafe Condition

Stress corrosion cracking of the forward trunnion pins, which could result in fracture of the pins and consequent collapse of the main landing gear (MLG).

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

Required Actions

Inspect the transition radius of the MLG forward trunnion pins for discrepancies, including finish damage, corrosion, pitting, and base metal scratches. Perform repetitive lubrications of the right and left MLG forward trunnion pins. Take corrective actions if necessary, including replacing or overhauling the trunnion pins to terminate the required actions.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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

Affected Aircraft

The Boeing Company Model 737-600, -700, -700C, and -800 series airplanes, including additional airplanes added to the applicability of AD 2009-24-07.

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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