Airworthiness Directive

AD 96-11-06 61 FR 26088 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-12729
Amendment
39-9631
Published
1996-05-24
Effective
1996-06-28
Models covered
1

Last live check: 2026-08-19

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AD

96-11-06

FR doc 96-12729 · 61 FR 26088

AD 96-11-06Published 1996-05-24Effective 1996-06-28

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 emergency lights circuitry.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain de Havilland Model DHC-7 series airplanes, that requires modification of the emergency lights circuitry. This amendment is prompted by reports of the emergency lights turning on inadvertently due to voltage spikes from other equipment; and reports that the existing emergency light switch arrangement allows the flight compartment and flight attendant's panel switches to override each other. The actions specified by this AD are intended to prevent such failures of the emergency light systems, which could prevent the use of the emergency lights in the event of an emergency.

More directives for de Havilland DHC-7 Dash 7

  1. AD 2015-20-06 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2015-11-10
  2. AD 2010-23-21 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2010-12-22
  3. AD 2009-06-03 Airworthiness Directives; Viking Air Limited Model DHC-7 Airplanes Effective 2009-04-20
  4. AD 2007-20-02 Airworthiness Directives; Viking Air Limited Model DHC-7 Airplanes Effective 2007-10-31
  5. AD 2006-12-04 Airworthiness Directives; Viking Air Limited Model DHC-7 Airplanes Effective 2006-06-21

All de Havilland DHC-7 Dash 7 directives

Applies to 1 model in our index