Card - General Information Flashcards
Max Normal Fuel Imbalance
200 lbs
Max Emergency Fuel Imbalance
800 lbs
No more than _____ vortex generator per wing may be missing to dispatch for flight.
ONE
No more than a total of _____ static discharge wicks may be missing from the entire airframe to dispatch for flight.
Their can’t be _______ adjacent static discharge wicks missing at one time
TWO
TWO
Max baggage compartment load w/out APU
700 lbs
Max baggage compartment load w/ APU
500 lbs
Type of start equals how many Batt Starts
EPU/GPU start ____Batt Start
Generator Asst Start ____Batt Start
Batt Start. ____Batt Start
APU Start ____Batt Start
Airborne Start ____Batt Start
EPU/GPU start 0 Batt Start
Generator Asst Start 1/3 Batt Start
Batt Start. 1 Batt Start
Aput Start 1 Batt Start
Airborne Start 1 Batt Start
Cabin Alt Limit
13,500 ft
Pax O2 Release
13,500 ft
Emergency. Press
13,500 ft
Min fuel required for all ops is ____ per side
350 lbs
Fuel remaining in the fuel tank when the fuel quantity indicator reads _____ is not usable in flight
Zero
Maximum takeoff and landing alt
14,000 ft
Max water/slush on Runway
0.75 in
The AP and yaw damper must be ____ for takeoff and landing
OFF
Vertical Nav sys must be off below _____ ft AGL
500
All anti ice systems shall be turned ___ when operating in icing conditions defined in Section III, Anti-Ice sys
ON
Operation of the engine bleed anti-ice system for longer then ____ seconds in Static air temperature of ______ or greater is _______
On
10 seconds
+10C
Prohibited
The use of the engine synch sys is _________ during takeoff, landing and single engine ops
prohibited
The horizontal stab anti-ice system must be turned _____ when operating in icing conditions defined in Section III, Anti-Ice Sys
Operations of the horizontal stab anti-ice sys above ____ ft is prohibited
ON
41,000 feet
Max Operating Altitude
51,0000
Min and Max GPU Amps
GPU Volts
1,000 amps
2,000 amps
28VDC
Avoid N1 fan speeds between ____ and ____ when the engine ice protection is on above 25,000 ft
85 -91% N1
Unusable fuselage tank fuel
3.0 lbs
Extension of landing gear or flaps is prohibited above ________ ft
20,000 ft
Nose tires must be inflated to _______ up to 21,000 lbs
and inflated to _______ above 21,000 lbs
125 PSIG (Gauge)
138 PSIG
Minimum Crew
Pilot and Copilot
Max number of seats
15 (2 Pilots - 13 Pax)
Max Crosswind with or without TR
25 kts
Operation of cockpit and cabin PAC selector switches in ______ mode is not approved for _________ and ________ and flight above ________ ft
High
Takeoff and Landing
45,000 feet
Operation of cockpit and cabin PAC selector switches in ______ mode is not approved during normal operation when using: windshield bleed air, wing anti-ice or engine anti-ice except during an _________
High
Emergency
Crew O2 mask are not approved above __________ ft
Pax O2 is not approved above ______ ft
40,000 ft
25,000 ft
EEC/DEEC must be ____ and operational for ________
On
Takeoff
Disregard the ____ bearing and LH / RH engine _____ pressure indications during periods of HF transmission
Disregard the Wx radar display during periods of HF transmission in the ____ MHz and above
ADF
Oil
29.0 MHz
Rudder bias sys must be ___ and operative for _______
On
Takeoff
Spoilers are restricted to ________ and ________ use only
Emergency Descent
Ground Use
Ext of speed brake with flaps in any position other than UP is prohibited below ______ ft AGL
500 ft
with the W/S bleed air inoperative the airplane must leave icing conditions within _____ min after windshield alcohol is turned on
15 min
Ground idle switch must be in ______ when conducting touch and gos
HIGH
PAC BLD SELECT switch must be positioned to NORM or HP for flight above ________ft
45,000
TR must be idle by _____ kIAS
65 KIAS
Aileron Boost sys inop or off restricts AP operation to the following modes:
Heading Select, Altitude Hold and Basic AP
Define Icing Conditions
TAT +10C and blw in vis moisture or when Temp dew point is less than 4 degrees in vis moisture
During sustained ground operations the engines should be operated for ______ seconds out of every _______ minutes at ______%RPM or higher to prevent possible ice accumulation
15 seconds
4 minutes
50%
Turn ON Fuselage Fuel Tank Transfer Switch before reaching __________ ft
30,000 ft
