AD 2014-03-06

Recurring final rule
Data completeness: 80%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2014-03-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2013-0866
FR Citation
79 FR 12368

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Reports of cracks found in the aft support fitting for the main landing gear (MLG) beam, and the rear spar upper chord and rear spar web.

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

Required Actions

Repetitive inspections for cracking of the aft support fitting for the MLG beam, and the rear spar upper chord and rear spar web in the area of RSS 224.14; repair if necessary.

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

Compliance Time

Within the compliance times specified in Boeing Special Attention Service Bulletin 737-57-1318, dated May 15, 2013.

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

Affected Aircraft

All The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category. Installation of Supplemental Type Certificate (STC) ST01219SE does not affect applicability.

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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