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CE-650 FSI GS > Card - General Information > Flashcards

Card - General Information Flashcards

1
Q

Max Normal Fuel Imbalance

A

200 lbs

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2
Q

Max Emergency Fuel Imbalance

A

800 lbs

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3
Q

No more than _____ vortex generator per wing may be missing to dispatch for flight.

A

ONE

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4
Q

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

A

TWO

TWO

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5
Q

Max baggage compartment load w/out APU

A

700 lbs

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6
Q

Max baggage compartment load w/ APU

A

500 lbs

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7
Q

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

A

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

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8
Q

Cabin Alt Limit

A

13,500 ft

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9
Q

Pax O2 Release

A

13,500 ft

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10
Q

Emergency. Press

A

13,500 ft

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11
Q

Min fuel required for all ops is ____ per side

A

350 lbs

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12
Q

Fuel remaining in the fuel tank when the fuel quantity indicator reads _____ is not usable in flight

A

Zero

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13
Q

Maximum takeoff and landing alt

A

14,000 ft

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14
Q

Max water/slush on Runway

A

0.75 in

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15
Q

The AP and yaw damper must be ____ for takeoff and landing

A

OFF

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16
Q

Vertical Nav sys must be off below _____ ft AGL

A

500

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17
Q

All anti ice systems shall be turned ___ when operating in icing conditions defined in Section III, Anti-Ice sys

A

ON

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18
Q

Operation of the engine bleed anti-ice system for longer then ____ seconds in Static air temperature of ______ or greater is _______

A

On

10 seconds

+10C

Prohibited

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19
Q

The use of the engine synch sys is _________ during takeoff, landing and single engine ops

A

prohibited

20
Q

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

A

ON

41,000 feet

21
Q

Max Operating Altitude

A

51,0000

22
Q

Min and Max GPU Amps

GPU Volts

A

1,000 amps
2,000 amps

28VDC

23
Q

Avoid N1 fan speeds between ____ and ____ when the engine ice protection is on above 25,000 ft

A

85 -91% N1

24
Q

Unusable fuselage tank fuel

A

3.0 lbs

25
Q

Extension of landing gear or flaps is prohibited above ________ ft

A

20,000 ft

26
Q

Nose tires must be inflated to _______ up to 21,000 lbs

and inflated to _______ above 21,000 lbs

A

125 PSIG (Gauge)

138 PSIG

27
Q

Minimum Crew

A

Pilot and Copilot

28
Q

Max number of seats

A

15 (2 Pilots - 13 Pax)

29
Q

Max Crosswind with or without TR

A

25 kts

30
Q

Operation of cockpit and cabin PAC selector switches in ______ mode is not approved for _________ and ________ and flight above ________ ft

A

High

Takeoff and Landing

45,000 feet

31
Q

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 _________

A

High

Emergency

32
Q

Crew O2 mask are not approved above __________ ft

Pax O2 is not approved above ______ ft

A

40,000 ft

25,000 ft

33
Q

EEC/DEEC must be ____ and operational for ________

A

On

Takeoff

34
Q

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

A

ADF

Oil

29.0 MHz

35
Q

Rudder bias sys must be ___ and operative for _______

A

On

Takeoff

36
Q

Spoilers are restricted to ________ and ________ use only

A

Emergency Descent

Ground Use

37
Q

Ext of speed brake with flaps in any position other than UP is prohibited below ______ ft AGL

A

500 ft

38
Q

with the W/S bleed air inoperative the airplane must leave icing conditions within _____ min after windshield alcohol is turned on

A

15 min

39
Q

Ground idle switch must be in ______ when conducting touch and gos

A

HIGH

40
Q

PAC BLD SELECT switch must be positioned to NORM or HP for flight above ________ft

A

45,000

41
Q

TR must be idle by _____ kIAS

A

65 KIAS

42
Q

Aileron Boost sys inop or off restricts AP operation to the following modes:

A

Heading Select, Altitude Hold and Basic AP

43
Q

Define Icing Conditions

A

TAT +10C and blw in vis moisture or when Temp dew point is less than 4 degrees in vis moisture

44
Q

During sustained ground operations the engines should be operated for ______ seconds out of every _______ minutes at ______%RPM or higher to prevent possible ice accumulation

A

15 seconds

4 minutes

50%

45
Q

Turn ON Fuselage Fuel Tank Transfer Switch before reaching __________ ft

A

30,000 ft

CE-650 FSI GS (32 decks)

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