Non-red limitations Flashcards
45 minute IFR reserve fuel
2500 lbs
Hot spare fuel
8500 lbs
Emergency fuel
1500 lbs
Inclement weather fuel
20,000 lbs
Minimum runway length
4500’
Minimum runway width
98’/30m
Maximum runway slope
2%
Ops review required for contaminated runway shorter than___
5800’
Runways under 98’/30m but greater than 72’ wide require what?
FPD or CP approval
LP must accomplish landing
Crosswind limited to 20 kts
Both TRs required for dispatch
Narrow runway landing is prohibited with which CAS messages?
RUDDER FAIL
NORMAL BRAKE FAIL
L or R INBD BRAKE FAIL
L or R OUTBD BRAKE FAIL
QFE field limitations
Manually set landing elevation to 0’
Do not use VSD
Do not use SMS/TLAF; TAWS RUNWAY switch must be off
If none of the GPS sensors are available TAWS TERRAIN switch must be OFF
Do not use VNAV
Do not use FMS TOLD function
Max ramp and Taxi weight
115,100 lbs
Maximum ZFW
67,500 lbs
Baggage compartment weight limit
2500 lbs
Maximum takeoff & landing altitude
10,000’
Maximum SLAT/FLAP extended altitude
18,000’
Maximum gear extended altitude
20,000’
Minimum takeoff temp
-40C
Maximum takeoff/landing temp
ISA +40
Maximum speeds 0’ - 51,000’
Below 8000’ - 300 kts
8-10,000 - 300 linear increase to 335
10-16,000’ - 335
16-20,000’ - 335 linear decrease to 320
20-35,000 - 320
35-51,000’ -.925
Minimum speed with flight spoiler extended
Vref+10
Maximum landing gear extended speed
250 kts
Maximum tire speed
195
Turbulent air penetration speed MSL to 8000’
265 Linear to 285
Maximum pressure differential
10.73 PSI
Maximum negative pressure relief
-0.5 PSI
Maximum differential taxi and takeoff
0.1 PSI
Maximum differential landing
1.0 PSI
Maximum number of passengers
17 (including children under 2)
Children under 2 only allowed to occupy ___
seat 4 or crew rest seat. Not allowed on divan seats during taxi/takeoff/landing
Minimum temperature for APU start on ground
-40C
Maximum temperature during APU start
Red max limit
Maximum APU bleed extraction altitude
25,000’
Maximum APU bleed extraction temp on ground
+48C
Engine generator load limits
60 kVA continuous
67.5 kVA for 5 minutes
75 kVA for 2 minutes
Do not use MAX spoilers unless ____
Dictated by AFM procedures or in case of emergency
Maximum fuel imbalance in flight and on ground
1100 in flight
600 on ground
Minimum go around fuel
750 lb per tank (wings level)
Fuel capacity
Wings - 35,100 lbs
Center - 14,200 lbs
Aft - 2550 lbs
Total 51,850 lbs
Fuel capacity when gravity refueling?
Wing tanks only - 29,700 lbs
Do not select AFT XFER - ON if either wing tank quantity exceeds _____
15,000 lbs
Fuel crossfeed must be closed for _____
takeoff and landing
Do not use fuel crossfeed below _____
10,000’ (for duel engine operations)
Minimum fuel quantity is __________ for wing-to-wing fuel transfer
2500 lb per wing tank
Do not takeoff if engine fuel temperature is below ____
5C
Minimum bulk fuel temperature for takeoff is _____
-30C
Bulk fuel freezing point of Jet A is ____
-40C
Do not power on display units on the ground when cabin and flight compartment temps exceed ____
40C for more than 30 minutes
FMS operations are limited to N___
89.5
Do not use FPLN UPLINK _____
in flight, FPLN UPLINK must be completed or canceled prior to taxi
Do not alter the FMS while _____
a FPLN UPLINK is in pending
Do not select FANS CPDLC INSERT MOD_____
Within 2 minutes of a TO waypoint
Do not select WX DEV TO from the____
CPDLC ROUTE REQ 1/2 page
Do not select DIVERT TO from the____
CPDLC EMERGENCY MSG 1/2 page
Do not conduct an approach with a glidepath angle greater than ____ with tailwinds greater than ____
4.5
5 kts
Straight in Vref at maximum landing weight
124 kts
ITT start limits
750 (ground)
875 (flight)
Idle ITT limit
995
Takeoff ITT limit
1035 for 5 minutes, 10 minutes with single engine.
Go around ITT limit
1077 for 15 seconds
N1/N2/ITT limit takeoff/max continuous
103.7/114.9/995
Ensure takeoff N1 is within __ prior to 80 kts
2%
Minimum oil temp for starting
-40C
Maximum oil temp
165C
Normal oil pressure
35-45 PSI
Oil can be replenished if engines have been shut down for ___
15-60 minutes
Use of FMS speed mode is prohibited when_____
Single engine
Do not arm approach mode until____
Within 70 degrees of final approach course