Instrument Number AEB 17/1583
Instrument Number AEB 17/1583
I, Pieter van Dijk, a delegate of the Civil Aviation Safety Authority, make this instrument under paragraph 39.004(3)(a) of the Civil Aviation Safety Regulations 1998.
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Pieter van Dijk
Continuing Airworthiness Section Manager
30 March 2017
Approval – Means of Compliance with Transport Canada Airworthiness Directive (AD) CF-2011-24 - Wing to Fuselage Attachment Joints - Barrel Nut Cracking
- Duration
This instrument:
(a) commences on the date of registration; and
(b) ceases to have effect if Transport Canada AD CF-2011-24 (the AD) is amended.
- Application
This instrument applies to a registered operator who operates a type of aircraft mentioned in the AD, as in force at the date of this instrument, issued by Transport Canada.
- Approval
I approve, as a means of compliance with the AD, the replacement of alloy steel barrel nuts with INCONEL barrel nuts in accordance with either:
(a) Bombardier modification summary package 4-123841, 4-113769 or 4-113768, as in force at the date of this instrument, or
(b) Bombardier service bulletin 84-57-26, as in force at the date of this instrument.