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Max Taxi/Ramp Wt
39,000 lb
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-
-
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Max Operating Altitude
45,000 ft
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Max Takeoff & Landing Altitude
10,000 ft
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Max Altitude with Y/D Off
31,000 ft
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Max Gear Extension Altitude
18,000 ft
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Max Flap Extension Altitude
18,000 ft
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Min Enroute Altitude for Autopilot
700 ft AGL
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Min Altitude for Autopilot: Visual/Non-Precision Approach
200 ft AGL
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Min Altitude for Autopilot: Precision Approach G/P < 3.5°
80 ft AGL
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Min Altitude for Autopilot: Precision Approach G/P 3.5° - 4.5°
160 ft AGL
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Vmo up to 8,000 ft
300 KIAS
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Vmo 8,001 - 29,475
320 KIAS
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Mmo above 29,475
.83 Mach
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Rough Air Pen Vra
265 KIAS/.75 Mach
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-
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-
-
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Tire Speed Limit
182 knots groundspeed
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Min Engine Oil Temp Starting
- 40° C
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Min Engine Oil Press Idle
28 psi
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Max Ground Engine Start ITT
650° C
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Max ITT to Begin Engine Start
350° C
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__ Engine start attempts followed by __ minute cooling period
3 Engine start attempts followed by 15 minute cooling period
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Engine must be motored for __ seconds after an aborted start
Engine must be motored for 30 seconds after an aborted start
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Engine may be cranked for up to __ minutes followed by __ minutes cooling
Engine may be cranked for up to 5 minutes followed by 15 minutes cooling
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Max Gen Electrical Load
2 or 3 Gens operating
400 Amps
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Max Gen Electrical Load
1 Gen operating (ground)
400 Amps
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Max Gen Electrical Load
1 Gen operating (flight)
500 Amps
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Max Gen Electrical Load
Transient (5 minutes)
600 Amps
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Max Pressure Refuel load
14,150 lb
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Max Gravity Refuel load
13,000 lb
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Min Go Around Fuel (per wing)
500 lb
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Max Fuel Imbalance
250 - 600 lb
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Max Bulk Fuel Temp T/O
50° C
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Min Bulk Fuel Temps T/O
Jet A
- 30° C
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Min Bulk Fuel Temps T/O
Jet 1
- 35° C
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Min Bulk Fuel Temps T/O
Jet B
- 40° C
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Power/Gravity fuel xflow valves must be ___ for Takeoff
Power/Gravity fuel xflow valves must be off for Takeoff
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Max Altitude APU operation
37,000 ft
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Max Altitude to start the APU
- 30,000 ft inflight
- 14,000 ft on ground
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Max Altitude APU GEN
30,000 ft
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Max Altitude APU Bleed Air for ECS
20,000 ft
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Max Altitude APU Bleed Air for Engine Start
20,000 ft
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Do NOT use APU to start the left engine on the ground above _____ ft
Do NOT use APU to start the left engine on the ground above 9,000 ft
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Max KIAS for APU Start
300 KIAS
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Max APU EGT (start)
973° C
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Max APU EGT (norm)
718° C
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APU operation during __ /____ prohibited.
APU operation during de/anti-icing prohibited.
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Do NOT takeoff with ___ _____ CAS message displayed without inspection.
Do NOT takeoff with _APU SHUTDOWN_ CAS message displayed without inspection.
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__ APU start attempts, each followedby a __ minute cooling period; __ minute cooling period after __ attempt
3 APU start attempts, each followedby a 1 minute cooling period; 20 minute cooling period after 3rd attempt
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__ successful APU start attempts may be made at __ minute intervals, followed by a __ ___ cooling period
6 successful APU start attempts may be made at 10 minute intervals, followed by a 1 hour cooling period
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Max Tailwind Component
10 knots
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Max Demonstrated Crosswind
Takeoff
28 knots
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Max Demonstrated Crosswind
Landing
24 knots
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Max Crosswind
Nosewheel Stearing Inop
15 knots
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Max Crosswind
One AHRS Channel Inop
15 knots
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Max Demonstrated Headwind
Cat II Operations
19 knots
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Max Demonstrated Crosswind
Cat II Operations
20 knots
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Thrust Reverser ground operations on ____ surface only
Thrust Reverser ground operations on paved surface only
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Do NOT attempt to deploy reversers __ ___
Do NOT attempt to deploy reversers in flight
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Do NOT use reverse to ___ __ aircraft
Do NOT use reverse to back up aircraft
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Do NOT use reverse for ___ _ ___ landings
Do NOT use reverse for touch & go landings
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Below __ KIAS, reverse limited to ___ only
Below 40 KIAS, reverse limited to IDLE only
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ECS/Pressurization:
____ ___ ____ prohibited on ground
TRIM AIR ONLY prohibited on ground
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Max Cabin Altitude for Crew/Pax O2 Masks
40,000 ft
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Max Pressurization Differential on ground
0.1 psi
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Max Pressurization Differential during landing
1.0 psi
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Max Positive Pressuriztion Differential
9.4 psi
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Max Negative Pressurization Differential
- 0.5 psi
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Engine Anti-Ice ON (ground ops):
OAT is 10° C or below & visible moisture or contaminated surfaces
-
Engine Anti-Ice ON (flight ops):
- SAT 10° C to -40° C & visible moisture
- OR
- _ICE DETECTED_ CAS mssg displayed
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Wing Anti-Ice ON (same as Engine):
- Except on ground OAT is 5° C or below
- Also, if deiced w/ Type II or Type IV fluid, turn on Wing anti-ice just prior to thrust increase for takeoff
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Wing Anti-Ice ON in flight
- _ICE DETECTED_ CAS mssg displayed
- OR
- Icing conditions & airspeed is less than 210 KIAS
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Min Temperature for Takeoff
- 40° C/F
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FMS V-speed use prohibited above ___ __° C
FMS V-speed use prohibited above ISA + 33° C
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FMS ____ /___ information is advisory only
FMS range/fuel information is advisory only
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FMS approaches prohibited without ____ displayed
FMS approaches prohibited without APPR displayed
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VNAV prohibited on ____ inside ___
VNAV prohibited on V-MDA inside FAF
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VNAV prohibited during ___ operations
VNAV prohibited during QFE operations
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Max ILS Glidepath Angle ___ degrees
Max ILS Glidepath Angle 4.5 degrees
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Maneuvering Load Factors:
Flaps Up
+2.6 g to - 1.0 g
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Maneuvering Load Factors:
Flaps extended
+2.0 g to 0.0 g
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