AD 2008-08-10
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 737-100 | Airworthiness Directives; Boeing Model 737-100, -200, -200C, -300, -400, and -500 Series Airplanes |
Unsafe Condition
Fatigue cracking of the outboard stabilizing fitting and stress corrosion cracking of the bolts attaching the fitting to the wing rear spar.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the outboard stabilizing fitting and certain adjacent components of the main landing gear support beam. Perform repetitive inspections for discrepancies of the outboard stabilizing fitting, walking beam hanger, and rear spar attachment, with corrective actions if necessary. Perform a one-time inspection of the outboard stabilizing fitting for discrepancies, with corrective actions if necessary, for certain airplanes. Perform a torque check of the aft pin of the outboard stabilizing fitting, with corrective actions if necessary, for certain other airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight for replacement actions; within specified intervals for repetitive inspections; within specified intervals for one-time inspections and torque checks.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes.
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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