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edition of the following:

Airplane Flight Manual, and

Flight Management System FMS−6000 Pilot’s Guide, part number
523−0780609−001117, dated 04−01−01 or later applicable revision.

The FMS is approved for use only with the following software program version or later
applicable revision:
Without SB 604−34−034 With SB 604−34−034
SCID 832−4117−033 SCID 832−4117−034

FMS database information must be verified as being current. Waypoints must be checked
for accuracy prior to use.

Use of pilot defined FMS approaches, in instrument meteorological conditions, is
prohibited.

The FMS must not be used for navigation unless it is receiving suitable navigation
information from the following sources:

One VOR /DME, or

Two DMEs, or

One inertial reference system (IRS)

GPS (if installed). If GPS is the only available sensor, use of FMS for navigation is not
approved unless the Collins prediction program 832−3443−005, or later applicable
version, has been run.

Airplane operation must not be predicated upon performance data; ETE / ETA and fuel
remaining.

FMS flight plans must be identical when conducting dual FMS approach operations.

Use of FMS instrument approaches past the Final Approach Fix is prohibited, unless APPR
is annunciated on the PFD.

Use of VNAV vertical guidance for a V-MDA type approach between the final approach fix
and the missed approach fix is prohibited.

Barometric VNAV guidance during approach, including published procedure altitudes,
minimum sector altitudes, DME arcs, and final approach segment, is not temperature
compensated. Expected terrain and obstacle clearance will not be provided for
temperatures below ISA.

The FMS with inputs from GPS may only be used for approach guidance if the reference
coordinate data system for the instrument approach is WGS−84 or NAD−83.
On airplanes 5301 to 5560 NOT incorporating Canadair Service Bulletin 604−31−015
or 604−34−031 Rev 1 or later revision:

Navigation must not be predicated on the expanded localizer displayed on the PFDs.


CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 58, Dec 05/05
TEMPORARY REVISION 604/18
Page 2 of 4
Oct 04/06
INSERT IN LIMITATIONS
FACING PAGE 02−09−2
REASON FOR ISSUE
Temporary revision to advise the flight crew of the following:
 FMS limitation applicable to airplanes 5631 and subsequent and airplanes incorporating
Canadair Service Bulletin 604−34−042.
ACTION
Add the following to paragraph 1.:
On airplanes 5631 and subsequent and airplanes incorporating Canadair Service Bulletin
604−34−042:
 For a WET runway condition selection on the FMS performance (Approach Ref page),
a VSPEED OUT OF RANGE scratchpad message will be posted. At this time, the AFM
performance tables must be used to crosscheck the performance data posted by the FMS.
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
LIMITATIONS 02−09−2
Navigation Systems Limitations
1. FLIGHT MANAGEMENT SYSTEM (CONT’D)

The FMS thrust setting data is the primary means of information provided two air data
computers are available.

The FMS V speed data is the primary means of information provided two flight
management computers are available.

The following performance database must be verified to be current and valid:
All Registries except CAA (UK) CAA (UK) Registry
part number 815−2058−001 part number 815−2059−001

The following V speed database must be verified to be current and valid:
All Registries except FAA FAA Registry
Airplanes 5301 to 5639
without SB 604−11−001
part number
815−2055−002
part number
815−2057−002
Airplanes 5640 and Subs
and Airplanes 5301 to 5639
with SB 604−11−001
part number
815−2054−002
part number
815−2056−002
On airplanes NOT incorporating Canadair Service Bulletin 604−34−035:

The following V speed database must be verified to be current and valid:
All Registries except FAA FAA Registry
Airplanes 5301 to 5639
without SB 604−11−001
part number
815−2055−001
part number
815−2057−001
Airplanes 5640 and Subs
and Airplanes 5301 to 5639
with SB 604−11−001
part number
815−2054−001
　
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