Limitations Flashcards
Max allowable weight of the acft at the gate?
53,250 lbs
Max TOW
53,000 lbs
Max ZFW
44,000 lbs
Max Landing Weight
47,000 lbs
Min OAT for takeoff?
-40 Degrees C
Max tailwind for t/o and landing?
10 knots
Max alt
FL410
Flight must be w/in 45 min of nearest suitable airport under what conditions?
If cargo is carried in cargo compartment.
With BTMS operative, min brake cooling time between landing or rejected t/o and subsequent t/o?
15 minutes
Max weight in the cargo compartment?
3,500 lbs
Max crosswind on a wet runway?
27 knots
Max crosswind on contaminated runway w/braking action less than good?
15 knots
Max crosswind if the Capt has less than 100 hours PIC in type?
27 knots
Max speed to lower landing gear?
250 knots
Max speed to raise landing gear?
200 knots
Max speed with landing gear extended?
250 knots
Vfo for flaps 8?
200 knots
Vfo for flaps 20?
200 knots
Vfo for flaps 30?
185 knots
Vfo for flaps 45?
170 knots
Vfe for flaps 8?
215 knots
Vfe for flaps 20?
215 knots
Max cargo loading weight
3500 lbs
Max airport pressure alt for t/o and landing
10,000 ft
Max ambient air temp approved for t/o and landing
ISA + 35 degrees C
Mx action is required if L(R) COWL A/ICE messages are not extinguished above what N2?
78%
The engine cowl anti-ice system must be ON when:
1) When in icing conditions
2) When ICE is annunciated by the ice detection system
T/F Aircraft indicated SAT or TAT may not be used on the ground.
True
Maximum runway slope
+/- 2 degrees
Minimum flight crew
One pilot and one copilot
Engines must be running how many minutes prior to takeoff?
2 minutes
Operate engines at IDLE for a minimum of now many minutes prior to shutdown?
2 minutes
Taxi-in time with engines below what percent may be included in the two minute cool down period?
80% N2
Cold Soak definition
Before the first flight of the day and the aircraft has been at an ambient temp of -30 degrees C or below for more than eight hours.
Cold Soak engine start requirements
Motor for 60 seconds AND verify fan rotation.
Cold Soak thrust reverser requirements
Actuate thrust reversers until the deploy and stow cycles are less than 5 seconds.
Starter Cranking Limits
First Start: one minute on, 10 seconds off
Max N2 for starter use
55%
Max ITT to initiate all ground starts
120 degrees C
L and R main fuel tank max fuel imbalance
800 lbs
Minimum fuel quantity for a go-around
450 lbs per wing in a level aircraft
APU starting limits using aircraft batteries on the ground or for normal in-flight start
1st Start, 30 seconds
2nd Start, 30 seconds followed by 20 minutes off
*A two minutes delay should be observed between cranking attempts to allow for cooling of starter and start contractor and for APU drainage.
APU starting limits using ground power
1st start, 15 seconds
2nd start, 15 seconds followed by 20 minutes off
*A two minutes delay should be observed between cranking attempts to allow for cooling of starter and start contractor and for APU drainage.
Max altitude to use APU bleed air
15,000’
APU bleed limit for engine start on the ground
No bleed air extraction limit, but once started, engines thrust must not exceed 70% N2.
APU bleed limit for engine start during flight, single engine
APU bleed air extraction for an engine start is not permitted
APU bleed limit for engine start during flight during double engine failure
APU bleed air extraction for engine starts is permitted 13,000’ and below.
Turbulence penetration airspeed
280 KIAS or 0.75 mach, whichever is lower
Max speed for windshield wiper operations
220 KIAS
Wind limits for takeoff
60 knots or a headwind component of >55 knots
(T/F) The ADC source coupled to the active autopilot must be the same as that coupled to the ATC transponder during flight in RVSM airspace
True
Max alt to extend flaps
15,000’
Min alt (AGL) to extend spoilers
800’ AGL
Max flap setting to use spoilers
30 degrees
Max taxi light operation time when stationary
10 minutes
Minimum airspeed to use max reverse thrust
60 KIAS
(T/F) Use of the ISI localizer and back course information is prohibited during back course approaches.
True
Max ITT allowed during engine start.
900 deg C
Max N2 split at idle?
2%
