AD 2005-07-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier | DHC-8-102 | Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes |
Unsafe Condition
A leak in the static pressure system could result in loss of the static systems and consequent erroneous data displayed on the pilot's flight instruments.
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Required Actions
Revise the airplane flight manual to include procedures for abnormal indications of airspeed, altitude, or vertical airspeed. Modify the static system according to Bombardier Service Bulletin 8-34-221, Revision `A,' dated September 15, 2003.
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Compliance Time
Within 10 days for AFM revision; within 24 months for static system modification.
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Affected Aircraft
Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes, serial numbers 003 through 598 inclusive.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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