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after 1 hour 30 minutes.
When airplanes, not equipped with GPS, operate on routes, having a width of ±10 kilometers,
not covered by VOR/DME, it is recommended that the airplane position be confirmed by ATC
after 3 hours.
LIMITATIONS
Systems Limitations
Vol. 1 02−08−3
REV 68, Apr 16/07
CL−604 Operating Manual
PSP 604−6
AR Certified Airplanes
15. GROUND OPERATIONS IN HIGH WIND CONDITIONS
In the event that the airplane is parked and sustains winds or gust loads in excess of
27 meters/second, an inspection and functional check of the aileron, elevator and rudder
power control units is required.
AR Certified Airplanes
16. OPERATIONS FROM GRAVEL RUNWAYS
Operations from gravel runways are prohibited.
LIMITATIONS
Systems Limitations
Vol. 1 02−08−4
REV 68, Apr 16/07
CL−604 Operating Manual
PSP 604−6
1. FLIGHT MANAGEMENT SYSTEM
The flight management system (FMS) must be operated in accordance with the latest edition of
the following:
• Airplane Flight Manual, and
• Flight Management System FMS–6000 Pilot’s Guide, part number 523–0808879–001117, or
later applicable revision.
On airplanes 5301 to 5665 NOT incorporating Service Bulletin 604–34–050 and on
airplanes 5301 to 5499 incorporating Service Bulletin 604–34–031:
• Flight Management System FMS–6000 Pilot’s Guide, part number 523–0780609–001117,
dated 04–01–01 or later applicable revision.
On airplanes 5301 to 5499 NOT incorporating Service Bulletin 604–34–031:
• Flight Management System FMS–6000 Pilot’s Guide, part number 523–0777833–004117,
dated 08–14–95 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
WITH SB 604–34–050 SCID 832–4117–094 SCID 832–4117–095
WITH SB 604–34–042 SCID 832–4117–074 SCID 832–4117–075
WITHOUT SB 604–34–042 SCID 832–4117–033 SCID 832–4117–034
On airplanes 5301 to 5499 NOT incorporating Service Bulletin 604–34–031:
The FMS is approved for use only with software program version SCID 829–7739–008 or later
applicable revision.
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), or
• GPS (if installed). If GPS is the only available sensor, use of FMS for navigation is not
approved unless an appropriate RAIM availability prediction program has been run. Refer to
Collins FMS and Database Services for the latest applicable prediction program.
Airplane operation must not be predicated upon performance data; ETE/ETA and fuel remaining.
On airplanes 5301 to 5499 NOT incorporating Service Bulletin 604–34–031:
The FMS latitude limits are ±80°.
FMS flight plans must be identical when conducting dual FMS approach operations.
LIMITATIONS
Navigation Systems Limitations
Vol. 1 02−09−1
REV 75, Feb 17/09
CL−604 Operating Manual
PSP 604−6
1. FLIGHT MANAGEMENT SYSTEM (CONT'D)
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.
CAUTION
Errors to VNAV defined paths may occur because of coding errors in
the navigation data base and because of altimetry errors. The actual
VNAV path may deviate significantly below the intended VNAV path in
very cold temperatures, unless an approved temperature compensation
function (if equipped) is used to correct for non−standard temperatures.
Database coding of VNAV altitudes for approach waypoints may result
in VNAV paths continuing below Minimum Descent Altitude (MDA),
Decision Altitude (DA), or Decision Height (DH), or ending at an altitude
too high to continue a safe descent to landing. Baro VNAV paths (often
called pseudo−glide paths) are not equivalent to an ILS glideslope.
Position along an approach must be verified prior to commencement of
　
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