AD 2015-05-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Cracking on the skin panels and skin splice joints and angles at certain stringers between fuselage stations 409.00 to 589.00, which could lead to widespread fatigue damage (WFD) and adversely affect structural integrity or cause rapid decompression.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the maintenance or inspection program to incorporate new or revised maintenance requirements and airworthiness limitations. Incorporate structural repairs and modifications to preclude widespread fatigue damage (WFD).
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 12 months of the effective date (April 21, 2015).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) 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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