Airworthiness Directive

AD 2002-08-05 67 FR 19101 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-9391
Amendment
39-12713
Published
2002-04-18
Effective
2002-04-23
Models covered
1
Last live check
2026-10-03
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AD

2002-08-05

FR doc 02-9391 · 67 FR 19101

AD 2002-08-05Published 2002-04-18Effective 2002-04-23

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires revising the Airplane Flight Manual to advise the flight crew of appropriate procedures to follow in the event that a main landing gear (MLG) fails to extend following a gear-down selection.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain Bombardier Model DHC-8-400, -401, and -402 series airplanes. This action requires revising the Airplane Flight Manual to advise the flight crew of appropriate procedures to follow in the event that a main landing gear (MLG) fails to extend following a gear-down selection. This action also requires replacement of the left and right MLG uplock assemblies with new assemblies; and an inspection of the left and right MLG uplock rollers for the presence of an inner low friction liner, and corrective actions if necessary. This action is necessary to ensure that the flight crew has the procedures necessary to address failure of an MLG to extend following a gear-down selection; and to detect and correct such failure, which could result in a gear-up landing and possible injury to passengers and crew.

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Applies to 1 model in our index