AD 94-04-01

final rule
Data completeness: 70%

Airworthiness Directives: de Havilland DHC-6 Series Airplanes

AD Number
94-04-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-CE-88-AD
FR Citation
Federal Register: February 10, 1994 (Volume 59, Number 28)

Applicability

TypeManufacturerModelDetails
aircraft Viking Air Limited DHC-6-1 Airworthiness Directives: de Havilland DHC-6 Series Airplanes
aircraft Viking Air Limited DHC-6-100 Airworthiness Directives: de Havilland DHC-6 Series Airplanes
aircraft Viking Air Limited DHC-6-200 Airworthiness Directives: de Havilland DHC-6 Series Airplanes
aircraft Viking Air Limited DHC-6-300 Airworthiness Directives: de Havilland DHC-6 Series Airplanes

Unsafe Condition

Cracked wing attachment fittings could cause loss of control of the airplane.

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

Required Actions

Within 100 hours time-in-service after the effective date, inspect top inner faces of left and right forward wing attachment fittings using dye penetrant and 10-power magnification. If cracks found, replace fittings with new steel adapter fittings (P/N C6WM1162-3 and C6WM1162-4) before further flight. By 2,000 hours TIS, replace fittings even without cracks.

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

Compliance Time

Within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished within the last 400 hours TIS, and thereafter at intervals not to exceed 500 hours TIS until compliance with paragraph (b) or (c).

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

Affected Aircraft

Viking Air Limited models DHC-6-1, DHC-6-100, DHC-6-200, DHC-6-300 (all serial numbers)

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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