CE700 Flashcards
(79 cards)
1
Q
Max gross weight
A
39,700 lbs
2
Q
Max takeoff weight
A
39,500 lbs
3
Q
Max Vmo
A
.84 Mach 325 knots
4
Q
Max speed below 18000 feet
A
290 knots
5
Q
Max turbulence speed
A
.75 Mach
235 knots
6
Q
Flaps speeds
A
Flaps 1. 250 knots
Flaps 2. 230 knots
Full flaps. 180 knots
7
Q
Max tire speed
A
195 knots
8
Q
Minimum battery temperature
A
-20 C
9
Q
Maximum GPU volts
A
30 volts
10
Q
Maximums GPU Amps
A
1500 Amps
11
Q
Max engine Generator load
Airborne and ground
A
100% Both airborne and ground
12
Q
External power unit ( GPU) must be what Volts and Amps ?
A
Between 26-30 volts
And
Max - 1500 Amps
13
Q
Certification Status
A
14 CFR
Part 25
14
Q
Max Landing weight
A
33,500 lbs
15
Q
Max Zero fuel weight
A
26,000 lbs
16
Q
Pitot Static ground limit
A
Limited to 2 minutes on maximum
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
18
Q
How many inverters are in the nose compartment.
A
6 inverters
DC>AC for the windshield heat.
19
Q
45 minute reserve fuel
A
1627 lbs
20
Q
Minimum release fuel
A
2994 lbs
21
Q
Min Hot Spare fuel
A
5400 lbs
22
Q
Emergency fuel
A
1367 lbs
23
Q
Minimum runway length
Dry runway
A
4000 feet long
+_ 2% slope
24
Q
Minimum runway width
Dry runway
A
60 feet wide
+_ 2% slope
25
If the runway is wet/contaminated what minimums length needs OPS review
Wet/contaminated less than 5000 feet
26
What is the maximum xwind for wet and for dry runway for takeoff and landing.
25 knots xwind
27
Max xwind for contaminated runway
| Width > 150 feet wide
15 knot xwind max
28
Max xwind for contaminated runway
| 150 or less
10 knot xwind max
29
What is the maximum APU operating altitude
35,000 feet max operating altitude
30
What are the limits for the successfull APU starts
6 starts @ 10 min intervals then 1 hr rest
31
What are the APU unsuccessful start limits
3 start attempts then 20 min off
Then
2 start attempts then 1 hour off
32
What is the maximum altitude for an APU start
15,000 feet
33
What is the temperature minimum for APU start
No Starts below -40 c
34
What % N2 is required for an airborne APU start
72% N2
35
APU start limit with an “Batt Volt”
| EICAS message
No APU start
36
What is the Maximume aircraft operating Altitude
45,000 ft
37
What is the maximum altitude for flap operations
18,000 ft
38
What is the maximum altitude for gear extended
18,000 feet
39
What is the maximum altitude for takeoff or landing
10,000
40
What’s the minimum oil temperature for an engine start
-40 c
41
What is the minimum oil temperature to bring the power above idle
5 c
42
What is the minimum oil temperature for takeoff and climb
15 c.
| It can go lower after takeoff as long as it remains above 5 c
43
What is the maximum total fuel load
14,511 lbs
44
What is the maximum fuel imbalance
500 lbs
45
Can you use the cockpit fuel temp to determine the actual fuel tank temperature prior to flight ?
No. Measured inside wheel well
46
What is the minimum altitude for using the auto pilot en route
1000 feet min
47
What is the minimum altitude for using the autopilot during an approach
160 feet
48
What is the minimum altitude to use the autopilot for take off or missed approach
400 feet
49
What is the limitation for use of the ECS knob?
ECS knob must not be in Heat Exchange only unless required by an AFM procedure
50
What is the limitation for use of the air conditioning above fl410
1. Both Pressurization sources in Normal
2. Both engine bleed buttons in Normal
3. ECS knob in Normal
51
What is the Normal PSI for pressurization ?
10.2 PSI or less
52
What is the maximum Pressurization PSI?
10.3
53
What is the aircraft length ?
73.2 ft
54
How wide is the aircraft?
68.11 ft
55
How high is the aircraft tail ?
19.5 ft
56
What degree wing sweep the the aircraft have ?
31.8 degrees
57
What is the speed brake max speed?
No max speed
58
What is the minimum altitude for speed brake usage?
500 ft AGL
59
Auto throttle speed must be set to what speed during an approach?
Vref +3 or greater
60
What are the Volts and Amps of the main engine generators ?
28.5 Volts
500 amps in the air
400 amps on the ground
61
What are the Volts and Amps of the APU generator
28.5 volts
400 Amps in the air
500 Amps on the ground
62
How many Hydraulic pumps are on the aircraft?
4 pumps.
2 engine driven pumps
1 rudder standby pump for A side lower rudder PCU
1 electric pump
63
What kind of batteries are installed in the aircraft? Main batteries
Lithium
64
What are the volts and amps of the two main batteries
28 volts
44 amps
65
How many standby batteries on the aircraft
1 standby battery.
24 volts 10.4 amps
3 hrs for the standby bus
66
Maximum tailwind for takeoff or landing
10 knots
67
What is the minimum start pressure for an engine start
32 PSI
68
What is the maximum tail wind
| For an engine start
16 Knots
69
Starter Limitations.
Engine start
Dry motoring cycle
Engine start-3 attempts/15 min cooling
Dry motoring-5 minutes/15 minutes rest
(Motoring longer than20 seconds counts as one normal start
70
On landing when must the thrust reverser she stowed?
45 it’s
71
PTCU check
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
After Start Flow. Left pilot
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
After start flow. RP
EICAS review
Transponder. Auto
Flaps Set for takeoff
APU. As required.
After start checklist
74
Power plant
Thrust
Two Honeywell HTF7000 turbofan engines
7609 pounds of thrust
75
EMEDS
Electromechanical
Expulsive
Deicing
System
76
Hydraulic pressure is used for what systems components
Rudder control
Spoilers
Thrust reverser
Nose wheel steering
Landing gear
Emergency Landing gear actuator
Wheel brakes
PTCU. Power transfer control unit
77
The PTCU
Can be used for what?
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
Engine start abort criteria
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
PTCU hydraulic generator produces how much power to buses?
200 amps at 28 volts powered by the A or B hydraulic system
| It can supply electric to all the EMER and Mission buses
