AD 96-20-03

final rule
Data completeness: 70%

Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes

AD Number
96-20-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
95-NM-72-AD
FR Citation
Federal Register: September 30, 1996 (Volume 61, Number 190)

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Inc. DHC-8-101 Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes
aircraft Bombardier Inc. DHC-8-102 Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes
aircraft Bombardier Inc. DHC-8-103 Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes
aircraft Bombardier Inc. DHC-8-106 Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes
aircraft Bombardier Inc. DHC-8-301 Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes
aircraft Bombardier Inc. DHC-8-311 Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes
aircraft Bombardier Inc. DHC-8-315 Airworthiness Directives; de Havilland Model DHC-8-100 and -300 Series Airplanes

Unsafe Condition

Loose actuator support bolts or cracks in the relief radius of the boss at the forward surface of the fittings could cause loss of hydraulic systems and reduced controllability of the airplane.

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

Required Actions

Inspect the three actuator attachment fitting bolts on the main landing gears using a torque of not less than 10 foot-pounds. Replace loose bolts with new ones of the same part number. Perform magnetic particle inspections on fittings to detect cracks, replacing cracked fittings. Install modified brackets with new fasteners and remove enamel application (Modification 8/1830).

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

Compliance Time

Within specified intervals (e.g., 24 hours after September 9, 1991; 250 landings after October 7, 1991; 90 days after the effective date of this AD).

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

Affected Aircraft

Bombardier Inc. Model DHC-8-101, DHC-8-102, DHC-8-103, DHC-8-106, DHC-8-301, DHC-8-311, DHC-8-315 airplanes, serial numbers 3 through 400 inclusive, except serial number 391.

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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