Airworthiness Directive

AD 2007-12-01 72 FR 30959 Active

Federal Aviation Administration · 14 CFR part 39

Prompted by reports of over-extension of the MLG shock strut piston, which allows the torque links to go over-center and rest on the piston.

FR document
E7-10670
Amendment
39-15079
Published
2007-06-05
Effective
2007-07-10
Models covered
1

Last live check: 2026-08-19

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AD

2007-12-01

FR doc E7-10670 · 72 FR 30959

AD 2007-12-01Published 2007-06-05Effective 2007-07-10

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.

Prompted by reports of over-extension of the MLG shock strut piston, which allows the torque links to go over-center and rest on the piston.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-100, DHC-8-200, and DHC-8-300 series airplanes. This AD requires, for certain airplanes, modification of the upper bearing of the main landing gear (MLG) shock strut. This AD also requires, for certain airplanes, revising the de Havilland DHC-8 Maintenance Program Manual to include the MLG shock strut servicing task. This AD results from reports of over-extension of the MLG shock strut piston, which allows the torque links to go over-center and rest on the piston. We are issuing this AD to prevent loss in shock absorption during touchdown and failure of the shock strut housing, which could result in a subsequent loss of directional control.

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Applies to 1 model in our index