AD 96-14-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | DHC-8-301 | Airworthiness Directives; de Havilland Model DHC-8-301, -311, and -315 Series Airplanes |
| aircraft | Bombardier Inc. | DHC-8-311 | Airworthiness Directives; de Havilland Model DHC-8-301, -311, and -315 Series Airplanes |
| aircraft | Bombardier Inc. | DHC-8-315 | Airworthiness Directives; de Havilland Model DHC-8-301, -311, and -315 Series Airplanes |
Unsafe Condition
Structural failure of the outboard flaps of the wings due to the installation of incorrect rivets in the flap assemblies, which could result in reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install Modification 8/2498 to modify airspeed limitation placards within 30 days after February 27, 1996. Revise the AFM to include specified airspeed limitations before further flight. For DHC-8-311 and -315 models, install Modification 8/2066 within 2 years after the AD's effective date to terminate prior requirements.
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Compliance Time
Within 30 days after February 27, 1996 (for Modification 8/2498) and within 2 years after the effective date of this AD (for Modification 8/2066 on DHC-8-311 and -315 models).
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Affected Aircraft
de Havilland Model DHC-8-301, -311, and -315 series airplanes certificated in any category, as listed in Service Bulletin S.B. 8-57-24, Revision 'A'.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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