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CE700 Flashcards

1
Q

Max gross weight

A

39,700 lbs

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2
Q

Max takeoff weight

A

39,500 lbs

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3
Q

Max Vmo

A

.84 Mach 325 knots

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4
Q

Max speed below 18000 feet

A

290 knots

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5
Q

Max turbulence speed

A

.75 Mach

235 knots

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6
Q

Flaps speeds

A

Flaps 1. 250 knots

Flaps 2. 230 knots

Full flaps. 180 knots

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7
Q

Max tire speed

A

195 knots

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8
Q

Minimum battery temperature

A

-20 C

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9
Q

Maximum GPU volts

A

30 volts

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10
Q

Maximums GPU Amps

A

1500 Amps

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11
Q

Max engine Generator load

Airborne and ground

A

100% Both airborne and ground

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12
Q

External power unit ( GPU) must be what Volts and Amps ?

A

Between 26-30 volts

And

Max - 1500 Amps

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13
Q

Certification Status

A

14 CFR

Part 25

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14
Q

Max Landing weight

A

33,500 lbs

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15
Q

Max Zero fuel weight

A

26,000 lbs

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16
Q

Pitot Static ground limit

A

Limited to 2 minutes on maximum

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17
Q

Wing Ice Protection Ground limits

While stationary and tailwind >10 knots or xwind > 25 knots

A

Thrust never above idle for more than 15 seconds

While stationary between 45-55 % power is prohibited with the tailwind > 10 knots
Or xwinds > 25 knots

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18
Q

How many inverters are in the nose compartment.

A

6 inverters

DC>AC for the windshield heat.

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19
Q

45 minute reserve fuel

A

1627 lbs

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20
Q

Minimum release fuel

A

2994 lbs

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21
Q

Min Hot Spare fuel

A

5400 lbs

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22
Q

Emergency fuel

A

1367 lbs

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23
Q

Minimum runway length

Dry runway

A

4000 feet long

+_ 2% slope

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24
Q

Minimum runway width

Dry runway

A

60 feet wide

+_ 2% slope

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25
Q

If the runway is wet/contaminated what minimums length needs OPS review

A

Wet/contaminated less than 5000 feet

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26
Q

What is the maximum xwind for wet and for dry runway for takeoff and landing.

A

25 knots xwind

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27
Q

Max xwind for contaminated runway

Width > 150 feet wide

A

15 knot xwind max

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28
Q

Max xwind for contaminated runway

150 or less

A

10 knot xwind max

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29
Q

What is the maximum APU operating altitude

A

35,000 feet max operating altitude

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30
Q

What are the limits for the successfull APU starts

A

6 starts @ 10 min intervals then 1 hr rest

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31
Q

What are the APU unsuccessful start limits

A

3 start attempts then 20 min off

Then

2 start attempts then 1 hour off

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32
Q

What is the maximum altitude for an APU start

A

15,000 feet

33
Q

What is the temperature minimum for APU start

A

No Starts below -40 c

34
Q

What % N2 is required for an airborne APU start

35
Q

APU start limit with an “Batt Volt”

EICAS message

A

No APU start

36
Q

What is the Maximume aircraft operating Altitude

37
Q

What is the maximum altitude for flap operations

38
Q

What is the maximum altitude for gear extended

A

18,000 feet

39
Q

What is the maximum altitude for takeoff or landing

40
Q

What’s the minimum oil temperature for an engine start

41
Q

What is the minimum oil temperature to bring the power above idle

42
Q

What is the minimum oil temperature for takeoff and climb

A

15 c.

It can go lower after takeoff as long as it remains above 5 c

43
Q

What is the maximum total fuel load

A

14,511 lbs

44
Q

What is the maximum fuel imbalance

45
Q

Can you use the cockpit fuel temp to determine the actual fuel tank temperature prior to flight ?

A

No. Measured inside wheel well

46
Q

What is the minimum altitude for using the auto pilot en route

A

1000 feet min

47
Q

What is the minimum altitude for using the autopilot during an approach

48
Q

What is the minimum altitude to use the autopilot for take off or missed approach

49
Q

What is the limitation for use of the ECS knob?

A

ECS knob must not be in Heat Exchange only unless required by an AFM procedure

50
Q

What is the limitation for use of the air conditioning above fl410

A
  1. Both Pressurization sources in Normal
  2. Both engine bleed buttons in Normal
  3. ECS knob in Normal
51
Q

What is the Normal PSI for pressurization ?

A

10.2 PSI or less

52
Q

What is the maximum Pressurization PSI?

53
Q

What is the aircraft length ?

54
Q

How wide is the aircraft?

55
Q

How high is the aircraft tail ?

56
Q

What degree wing sweep the the aircraft have ?

A

31.8 degrees

57
Q

What is the speed brake max speed?

A

No max speed

58
Q

What is the minimum altitude for speed brake usage?

A

500 ft AGL

59
Q

Auto throttle speed must be set to what speed during an approach?

A

Vref +3 or greater

60
Q

What are the Volts and Amps of the main engine generators ?

A

28.5 Volts

500 amps in the air
400 amps on the ground

61
Q

What are the Volts and Amps of the APU generator

A

28.5 volts

400 Amps in the air
500 Amps on the ground

62
Q

How many Hydraulic pumps are on the aircraft?

A

4 pumps.

2 engine driven pumps

1 rudder standby pump for A side lower rudder PCU

1 electric pump

63
Q

What kind of batteries are installed in the aircraft? Main batteries

64
Q

What are the volts and amps of the two main batteries

A

28 volts

44 amps

65
Q

How many standby batteries on the aircraft

A

1 standby battery.

24 volts 10.4 amps

3 hrs for the standby bus

66
Q

Maximum tailwind for takeoff or landing

67
Q

What is the minimum start pressure for an engine start

68
Q

What is the maximum tail wind

For an engine start

69
Q

Starter Limitations.

Engine start

Dry motoring cycle

A

Engine start-3 attempts/15 min cooling

Dry motoring-5 minutes/15 minutes rest

(Motoring longer than20 seconds counts as one normal start

70
Q

On landing when must the thrust reverser she stowed?

71
Q

PTCU check

A

EMER/Park BRAKE. Off, then On

Hyd pump Aor B. MIN

Verify press cycles between

A. 1400-2900

B. 1800-3250

Hydraulic pump - NORM

72
Q

After Start Flow. Left pilot

A

Control lock- unlock

Aileron/ roll spoilers - Check

Elevators check

Master disconnect - press and Hold
Rudder check

Tiller - Check

Master disconnect -Release

Control lock as required

Speed brake - check

PTCU check

Map setting- safe taxi

After Start checklist

73
Q

After start flow. RP

A

EICAS review

Transponder. Auto

Flaps Set for takeoff

APU. As required.

After start checklist

74
Q

Power plant

Thrust

A

Two Honeywell HTF7000 turbofan engines

7609 pounds of thrust

75
Q

EMEDS

A

Electromechanical
Expulsive
Deicing
System

76
Q

Hydraulic pressure is used for what systems components

A

Rudder control

Spoilers

Thrust reverser

Nose wheel steering

Landing gear

Emergency Landing gear actuator

Wheel brakes

PTCU. Power transfer control unit

77
Q

The PTCU

Can be used for what?

A

A bidirectional pump power transfer unit

An electric motor driven auxiliary pump on system A and B

Hydraulic motor driven generator supplying 200 amps to the right emer bus

78
Q

Engine start abort criteria

A
  1. No ITT after 20 seconds
  2. No out pressure after 30% N2
  3. ITT red lines
  4. No stabilized idle by 50 seconds of
    ITT rise
79
Q

PTCU hydraulic generator produces how much power to buses?

A

200 amps at 28 volts powered by the A or B hydraulic system

It can supply electric to all the EMER and Mission buses

Aircraft (3 decks)

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