Airworthiness Directive

AD 2002-13-08 67 FR 44028 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-16306
Amendment
39-12796
Published
2002-07-01
Effective
2002-08-13
Models covered
1
Last live check
2026-10-01
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AD

2002-13-08

FR doc 02-16306 · 67 FR 44028

AD 2002-13-08Published 2002-07-01Effective 2002-08-13

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 you to modify the elevator tip rib on each elevator; repetitively inspect underneath the mass balance weights at each elevator tip rib for corrosion; and either remove the corrosion or replace a corroded elevator tip rib…

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain de Havilland Inc. (de Havilland) Models DHC-2 Mk. I, DHC-2 Mk. II, and DHC-2 Mk. III airplanes. This AD requires you to modify the elevator tip rib on each elevator; repetitively inspect underneath the mass balance weights at each elevator tip rib for corrosion; and either remove the corrosion or replace a corroded elevator tip rib depending on the corrosion damage. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Canada. The actions specified by this AD are intended to detect and correct corrosion in the mass balance weights at the elevator tip ribs, which could result in loss of balance weight during flight and the elevator control surface separating from the airplane.

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All de Havilland DHC-2 Beaver directives

Applies to 1 model in our index