Airworthiness Directive

AD 99-19-34 64 FR 51199 Active

Federal Aviation Administration · 14 CFR part 39

FR document
99-24148
Amendment
39-11321
Published
1999-09-22
Effective
1999-10-27
Models covered
1
Last live check
2026-10-03
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AD

99-19-34

FR doc 99-24148 · 64 FR 51199

AD 99-19-34Published 1999-09-22Effective 1999-10-27

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 modification of certain hydraulic systems that provide hydraulic pressure for the control of the rudder and for the main landing gear brakes.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-100 and -300 series airplanes, that requires modification of certain hydraulic systems that provide hydraulic pressure for the control of the rudder and for the main landing gear brakes. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent damage to certain hydraulic system components in the number 2 engine nacelle, which could result in loss of the number 1 and number 2 hydraulic systems, and consequent reduced controllability of the airplane.

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Applies to 1 model in our index