AD 2004-19-07

final rule
Data completeness: 70%

Airworthiness Directives; Bombardier Model DHC-8-102 Airplanes

AD Number
2004-19-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-185-AD
FR Citation
69 FR 56682

Applicability

TypeManufacturerModelDetails
aircraft Bombardier DHC-8-102 Airworthiness Directives; Bombardier Model DHC-8-102 Airplanes

Unsafe Condition

Component failure in the radar indicator, resulting in an overcurrent condition and consequent overheating or burning of an internal component or the ribbon cable, which could lead to smoke in the cockpit, resulting in incapacitation of the crew and loss of control of the airplane.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Modify the electrical power circuit by accomplishing all the actions in the Accomplishment Instructions of Bombardier Modification Summary Package (ModSum) IS8Q3450000, Revision A, dated October 15, 2002; as applicable. Do the actions per the ModSum.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within 12 months after the effective date of this AD.

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Affected Aircraft

Bombardier Model DHC-8-102 airplanes, serial numbers 023 through 392 inclusive; certificated in any category; equipped with an RDS86 Weather Radar System, excluding those airplanes equipped with option CR834CH00284.

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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