| Number |
CF-2006-21R1 |
| Issued by |
 Canada |
| Issue date |
2006-10-10 |
| Effective date |
2006-10-16 |
| EASA approval number |
|
| ATA Chapter |
27 |
Approval Holder
/ Type Designation |
-
BOMBARDIER
-
CL-600 (Challenger)
-
CL-600-2B16 (604 Variant)
|
| Revision |
This revised AD enhances the airplane flight manual (AFM) stabilizer trim runaway procedure, mandates the installation of circuit breaker (CB) quick identification collars for the HSTCU CBs, and introduces some additional trim system preflight checks for the flight crew. The installation of a modified HSTCU with environment protection on the motherboard provides terminating action.
|
| Correction |
Not applicable
|
| Supersedure |
This AD revision supersedes Transport Canada AD CF-2006-21, issued 23 August 2006.
|
| Publication(s) and related information |
Bombardier Alert Service Bulletin (ASB) A604-27-029 dated 28 September 2006, or later revision approved by the Chief, Continuing Airworthiness. |
| Remarks |
Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail:
ADs [at] easa.europa [dot] eu
|
