Number |
CF-2007-20R2 |
Issued by |
Canada |
Issue date |
2009-02-25 |
Effective date |
2009-03-09 |
EASA approval number |
|
ATA Chapter |
32 |
Approval Holder / Type Designation |
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
-
DHC-8
-
DHC-8-400
-
DHC-8-401
-
DHC-8-402
|
Revision |
This AD revises AD CF-2007-20R1 issued on 11 October 2007.
|
Correction |
Not applicable
|
Supersedure |
This AD supersedes AD CF-2007-20R1 issued on 11 October 2007 and replaces EASA AD 2007-0272 dated 16 October 2007, which has been cancelled.
|
Publication(s) and related information |
Bombardier DHC-8 Series 400 Maintenance Requirements Manual PSM 1-84-7, including Temporary Revision (TR) MRB–35.
Bombardier Repair Drawing (RD) 8/4-32-059, Issue 5, or later approved revision.
Bombardier All Operators Message No. 236 Rev A or later revisions.
Bombardier Service Bulletin (SB) 84-32-55, Revision A, dated 10 March 2008, or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada provides approved instructions for incorporating Modsum 4-901603. |
Remarks |
In deviation from paragraph E “Flight Crew Limitations and Procedures” points 4, 5 and 6 of TCCA EAD CF-2007-20R1, ferry flights are permitted only in accordance with the instructions, procedures and limitations as specified in EASA-approved Supplement No.94 “Ferry Flight with Landing Gear Extended” to DHC-8 Series 400 (Q400) AFM Document No. PSM 1-84-1A (JAA).
Note: Any actions already accomplished in accordance with EASA Emergency AD 2007-0252-E or EASA AD 2007-0272 can be considered in compliance with the corresponding tasks as required by TCCA AD CF-2007-20R2.
At the moment of adoption of this AD, the model 400 has not been validated in Europe.
|