AD 2014-15-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Fractured wing-to-fuselage strut attachment joint bolt due to stress corrosion cracking, which could compromise structural integrity and lead to wing loss.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Torque check all wing-to-fuselage strut attachment joint bolts; repair or replace if necessary. For certain airplanes, perform a detailed inspection for corrosion, damage, and wear of each bolt and associated hardware, and replace if necessary. Conduct a borescope inspection for corrosion and damage of the bore hole and barrel nut threads, and repair or replace if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 2,000 flight cycles or 12 months, whichever occurs first, after the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.