AD 2015-03-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | Various | Airworthiness Directives; Bombardier, Inc. Airplanes |
Unsafe Condition
Reports of dislodged engine fan cowl panels, which may cause damage to the fuselage and flight control surfaces of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install additional attaching hardware on the left and right fan cowl access panels and the nacelle attaching structures, in accordance with Bombardier Service Bulletin 601R-71-034, Revision B, dated August 1, 2014.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 6,000 flight hours after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category, all manufacturer serial numbers.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.