Document ID: chunk:federal_register_of_legislation:F2008L00783:body:0:p1
Version: federal_register_of_legislation:F2008L00783
Segment Type: other
Provision Reference: 
Character Range: 0–3171

AIRWORTHINESS DIRECTIVE
On the effective date specified below, and for the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/DHC-3/37 and issues the following AD under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

DHC-3 (Otter) Series Aeroplanes
AD/DHC-3/37 Amdt 1  Magneto Cannon Plug  4/2008

Applicability:  All Model DHC-3 aeroplanes powered by radial engines incorporating a firewall magneto connector plug as described in Viking Air Limited Service Bulletin (SB) V3/0001.
Requirement:       1. If not previously accomplished in accordance with the original issue of this Directive, perform a visual inspection of the firewall ignition plug and receptacle for proper lock wiring and security in accordance with the Accomplishment Instructions of Bombardier Aerospace de Havilland Otter Alert Service Bulletin A3/53, Revision 'A' dated 30 August 2001 or later revision approved by the Chief, Continuing Airworthiness, Transport Canada.
                   2. Replace any damaged parts detected during the Requirement 1 inspection.
                   3. If not previously accomplished in accordance with the original issue of this Directive, incorporate Maintenance Manual PSM 1-3-2 Temporary Revision TR14, dated 24 August 2001, into the periodic inspection of the aircraft approved maintenance schedule.  Once incorporated, this inspection is considered a routine task subject to normal maintenance program development and escalation.
                TR14 may be removed from the Maintenance Manual when it is superseded by a normal revision to the manual.
                   4. Replace the firewall magneto connector in accordance with the accomplishment instructions of Viking Air Limited SB V3/0001 dated 27 June 2007, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada.
                Note:  Transport Canada AD CF-2001-37R1 refers.
Compliance:     For Requirement 1 - Within 3 months or 110 hours time in service after the effective date of this Directive, whichever occurs first.
                For Requirement 2 - Before further flight after the Requirement 1 inspection.
                For Requirement 3 - Within 3 months after the effective date of this Directive.
                For Requirement 4 - Before 1 August 2008.

             This Amendment becomes effective on 10 April 2008.
Background:  Transport Canada has advised that a complete loss of both ignition systems occurred on a DHC-3 Otter when the lock wire hole in the ignition connector plug on the firewall broke out, allowing the plug to vibrate loose.  A maintenance safety feature grounds out both magneto systems through