AD 2006-14-07

Recurring final rule
Data completeness: 80%

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

AD Number
2006-14-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-24432
FR Citation
71 FR 40391

Applicability

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

Unsafe Condition

Reports of cracks in the elevator rear spar web at the tab hinge bracket locations. Cracking, corrosion, interlaminar corrosion, delamination, and disbonding in the elevator rear spar may reduce elevator stiffness and lead to in-flight vibration.

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

Required Actions

For airplanes with laminated rear spars, conduct repetitive inspections for interlaminar corrosion, delamination, or disbonding in the rear spar, and for cracking in the spar web. For airplanes with solid rear spars, conduct repetitive inspections for cracking in the spar web. Repair, including related investigative/corrective actions, is required if necessary.

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Compliance Time

Within the compliance times specified in the AD, unless the actions have already been done.

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Affected Aircraft

Boeing Model 737-100, -200, and -200C series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-55A1078, dated October 27, 2005.

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Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

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