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CL-601 Ops Limits
Challenger 601 Study guide
84
Aviation
Graduate
04/20/2017

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Term
Max Taxi and Ramp weight
Definition
45,250 lbs
Term
Max takeoff (MTOW)
Definition
45,100 lbs
Term
Max Landing (MLW)
Definition
36,000 lbs
Term
Max Zero Fuel (ZFW)
Definition
31,000 lbs
Term
Max airport pressure altitude
Definition
10,000 ft
Term
Max operating altitude
Definition
41,000 ft
Term
Max temp for takeoff/land
Definition
ISA + 35C (+50C/+122F)
Term
Min temp for takeoff
Definition
-40C or -40F
Term
Max runway slope
Definition
+/- 2%
Term
Max TW component takeoff or landing
Definition
10 knots
Term
max demonstrated crosswind with TRs
Definition
24 knots
Term
Min Oil Temp for starting:
Definition
-40C
Term
Max ITT to begin Start
Definition
120C
Term
Min N2 to begin start
Definition
20%
Term
[Engine Start]
Max ITT (16 sec)
Definition
930C
Term
[Engine Start]
Max ITT (50 sec)
Definition
903C
Term
[Engine Start]
Max starter duty
Definition
3 cycles, 5 minutes cooling before additional cycles
Term
Max T/O N1, N2, ITT (5 minutes)
Definition
98.6, 99.4, 899
Term
Max T/O N1, N2, ITT (with APR, 2 minutes)
Definition
98.6, 99.4, 928C
Term
Normal T/O N1, N2, ITT, (5 Minutes)
Definition
96.2, 98.3, 884C
Term
Normal T/O N1, N2, ITT (2 minute limit)
Definition
96.2, 98.3, 900C
Term
Max continuous N1, N2, ITT
Definition
98.6, 99.2, 860C
Term
Max permissible oil temp:
Definition
163C (15 minutes max)
Term
Max oil temp for single engine climb:
Definition
155C, 60 minutes max
Term
max continuous oil temp:
Definition
150C
Term
max continuous oil pressure
Definition
110 PSI
Term
min oil pressure at steady state idle
Definition
25 PSI
Term
min oil pressure at takeoff power
Definition
45 PSI
Term
[APU]
Min temp for start
Definition
-40C
Term
APU max RPM (-150)
Definition
107%
Term
APU max EGT
Definition
743C
Term
APU Max EGT (start)
Definition
974C
Term
[APU]
Max altitude for engine start using APU
Definition
13,000 ft
Term
[APU]
Max altitude for bleed air extraction
Definition
15,000 ft
Term
[APU]
max altitude for start
Definition
30,000 ft
Term
[APU]
max operating altitude
Definition
37,000 ft
Term
APU Max gen load
Definition
30 kVA in flight
Term
APU Max starter Duty Cycle
Definition
2 cycles, then 20 minutes cooling before additional cycles
Term
[Max operating speeds]
0 - 10,000 ft
Definition
301 KIAS
Term
[Max operating speeds]
10,000 - 21,330
Definition
360 KIAS
Term
[Max operating speeds]
21,330 - 25,640
Definition
0.79 Mach
Term
[Max operating speeds]
25,640 - 28,720
Definition
330 KIAS
Term
[Max operating speeds]
28,720 and above
Definition
0.835 Mach
Term
[Max operating speeds]
RVSM
Definition
0.82M
Term
[Additional Speed Limits]
Vfe flaps 20
Definition
232 KIAS
Term
[Additional Speed Limits]
Vfe flaps 30
Definition
198 KIAS
Term
[Additional Speed Limits] Vfe Flaps 45
Definition
190 KIAS
Term
[Additional Speed Limits]
Vlo Ldg gear operating
Definition
197 KIAS / 0.7M
Term
[Additional Speed Limits]
Vle Ldg gear extended
Definition
250 KIAS / 0.7 M
Term
[Additional Speed Limits]
Max tire speed
Definition
183 kts ground speed
Term
Vmcg
Definition
108 KIAS
Term
Vmca
Definition
116 KIAS
Term
V1 min
Definition
108 KIAS
Term
VR min
Definition
121 KIAS
Term
V2 min (actual)
Definition
132 KIAS
Term
[Additional Speed Limits]
Max speed for ADG ops
Definition
250 KIAS after auto or manual deployment; 330 KIAS for 12 minutes reducing to 4 minutes at Vmo. flight test and training max is 215 KIAS
Term
[Additional Speed Limits]
turbulence penetration speed
Definition
lower of 280 KIAS /0.75M
Term
[Electrical]
Main Gen load limit below 35,000 ft
Definition
30kVA, APU same
Term
[Electrical]
Main Gen load limit, above 35,000 ft
Definition
25 kVA, APU n/a
Term
[Electrical]
max continuous load on TR1 or 2
Definition
100 amps
Term
[Electrical]
max continuous load on ESS TRU1 and ESS TRU2 combined
Definition
75 amps
Term
[Fuel]
max fuel imbalance between main tanks
Definition
800 lbs
Term
[Fuel]
Left/Right main tank capacity
Definition
4909 lbs
Term
[Fuel]
fuselage tank capacity
Definition
6868 lbs
Term
[Fuel]
Tail tank capacity
Definition
1,276 lbs
Term
[Fuel]
Takeoff with up to ___ in the aux tank is permitted provided there is at least ___ in each wing tank
Definition
500 lbs, 1500 lbs
Term
[Fuel] Max flaps for fuel jettison
Definition
zero
Term
[Fuel] Min tail tank fuel for fuel jettison
Definition
30 lbs
Term
[Load limits]
flaps up
Definition
-1.0 to +2.56 Gs
Term
[Load Limits] Flaps down G limit
Definition
-1.0 to +2.0 Gs
Term
Max time for taxi light use if stationary
Definition
10 minutes
Term
Maximum main tire pressure
Definition
206 +5/-0 PSI
Term
max nosewheel tire pressure is ___ on the ground
Definition
151 PSI +5/-0%
Term
[Flight Controls]
Max altitude flaps extended
Definition
15,500 ft
Term
[Flight Controls]
Min altitude spoilers extended
Definition
300 ft AGL
Term
[Flight Controls]
Spoilers must not be extended in flight below ____ (speed)
Definition
Vappr + 10 KIAS
Term
[automatic flight control system]
use of autopilot prohibited below
Definition
200ft
Term
[Pressurization]
Max relief differential
Definition
9.2 PSI
Term
[Pressurization]
Taxi, takeoff and landing
Definition
not to exceed 1.0 PSI
Term
Max rotation rate on takeoff
Definition
3 degrees/sec
Term
initial pitch target on rotation
Definition
10 degrees
Term
cowl anti-ice must be on:
Definition
OAT <10C, visible moisture or runways wet or contaminated
Term
wing anti-ice must be on:
Definition
Visible moisture present in any form below 400 ft AGL or the runway is wet or contaminated. Must be on for final taxi prior to takeoff if OAT <5C. If anti-ice fluid has been applied, wing anti-ice must be selected and confirmed ON just prior to thrust increase for takeoff
Term
Cowl/Wing anti-ice must be on >= 22000 ft:
Definition
ice indicated by ice detection system; or in icing conditions if ice detector failed
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