Bombardier_Challenger_Global_00-Limitations(8)

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criteria of FAA Order 8400.12A as a means of navigation for flights without
time limitations.
Vertical Navigation — The FMS has been demonstrated capable of and has
been shown to meet the accuracy requirements of: VFR/IFR en route and terminal
VNAV operation within the contiguous United States and Alaska in accordance
with the criteria of AC 20-129.
NOTE: The above statements do not constitute an operational approval.
STANDBY INSTRUMENT
Use of the standby instrument localizer deviation guidance is prohibited during
localizer backcourse approaches.
STANDBY COMPASS
L and R WSHLD /WINDOW switches must be temporarily selected OFF
while the standby compass is being read.
(Continued)
LIMITATIONS
DOT Approved Sep 29/2006 Airplane Flight Manual 02-04-06A
REV 7 CSP 100-1
SYSTEMS LIMITATIONS (Cont)
INTEGRATED FLIGHT INFORMATION SYSTEM (If installed)
􀁹 Incorporation of Dual IFIS does not constitute operational
approval to dispatch without adequate backup documentation.
􀁹 The IFIS related databases utilized (i.e. charts, airspace, airways,
geographic, political, graphical weather) must incorporate the current
update cycle.
􀁹 The IFIS does not include enroute charts.
􀁹 The use of the aircraft symbol on the Electronic Charts for navigation
is prohibited.
􀁹 The display of geo-political boundaries, airspace and airways on
the MFD (Enhanced Map overlays) is for enhanced situational
awareness only, and use for navigation is prohibited.
􀁹 All weather products data linked to the aircraft are advisory.
􀁹 For a single IFIS, adequate backup documentation must be immediately
available to the flight crew.
􀁹 Use of the aircraft symbol for guidance during taxi operations is
prohibited.

LIMITATIONS
DOT Approved Jul 31/2006 Airplane Flight Manual 02-04-07
REV 6 CSP 100-1
SYSTEMS LIMITATIONS (Cont)
AVIONICS (Cont)
TERRAIN AWARENESS AND WARNING SYSTEM (TAWS)
Do not use the Terrain Awareness and Warning System for navigation.
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)
Pilots are authorized to deviate from their Air Traffic Control (ATC) clearance
in order to comply with a resolution advisory (RA) command.
Maneuvers must not be based solely on information presented on the traffic
map overlay.
ELECTRICAL
Ground or Flight Operations
Continuous:
- Two or three generators operating............................... 400 amps.
- One generator operating (on the ground) .................... 400 amps.
- One generator operating (in flight) ............................. 500 amps.
Transient (5 minutes) ........................................................ 600 amps.
For aircraft on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
NAVIGATION
During normal flight, reversion of ATT, HDG and ADC is not permitted.
EFFECTIVITY
For aircraft on the Russian Federation (RF) and Commonwealth of
Independent States (CIS) countries’ registry:
Flight is not permitted along routes where ATC service provided is not in
RBS mode.
TCAS II TA/RA mode is not recommended on routes where ATC modes not
limited to RBS are provided. On these routes, while in TA mode, the pilot
action shall be coordinated with ATC.
WEATHER RADAR
Weather Radar information must be displayed continuously on at least one
(1) PFD or MFD during the entire flight.
Following a TAWS terrain caution or terrain warning, the Weather Radar
information must be reinstated on at least one (1) PFD or MFD, after the
encounter has been resolved.
EFFECTIVITY
LIMITATIONS
02-04-08 Airplane Flight Manual DOT Approved Jul 31/2006
CSP 100-1 REV 6
SYSTEMS LIMITATIONS (Cont)
ELECTRICAL (Cont)
NOTE: Refer to APU LIMITATIONS in this chapter for APU generator
altitude limits.
Do not take off if battery temperatures are below -20 oC (-4 oF).
FLIGHT CONTROLS
FLAPS
Do not extend the flaps above 18 000 ft.
SPOILERS
Do not select Flight Spoilers to EMER except during emergency conditions or
as required by procedure.
Flight spoilers must not be extended in flight at airspeeds below approach
speed + 8 KIAS.
Flight spoilers must not be extended in flight below 500 ft AGL.
HYDRAULICS
Hydraulic fluid of type Phosphate Ester Fire-Resistant per BAMS 564-003
Type IV, Skydrol LD-4, Hyjet IV-a Plus is approved for use.
LANDING GEAR, WHEELS & BRAKES
Do not extend the gear above 18 000 ft.
Brake cooling times (established in accordance with the procedures in
　
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