Airworthiness Directive

AD 2003-14-22 68 FR 42581 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-18083
Amendment
39-13241
Published
2003-07-18
Effective
2003-08-22
Models covered
1

Last live check: 2026-08-19

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AD

2003-14-22

FR doc 03-18083 · 68 FR 42581

AD 2003-14-22Published 2003-07-18Effective 2003-08-22

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 the No.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, -201, - 202, -301, -311, and -315 airplanes. This AD requires modification of the No. 3 electrical equipment panel behind the avionics rack, and modification of the No. 2 propeller de-ice timer. This action is necessary to prevent incorrect altitude information transmitted by the Mode S transponder and simultaneous loss of the Traffic Alert and Collision Avoidance System (TCAS), and increasing the possibility of an air traffic conflict. This action is intended to address the identified unsafe condition.

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Applies to 1 model in our index