1
Q
Mmo with ventral tank empty?
A
Mach 0.80
2
Q
Maximum air temperature for flight?
A
ISA + 35°C
3
Q
Minimum temperature for take-off and landing?
A
-40°C
4
Q
Minimum temperature enroute?
A
-75°C
5
Q
Maximum tailwind for takeoff and landing?
A
10kts
6
Q
Maximum Runway slope for takeoff and landing?
A
+2% and -2%
7
Q
Maximum and minimum field pressure altitude for takeoff and landing?
A
-2.000ft and 9.000ft
8
Q
Maximum altitude for takeoff and landing with the use of cabin High Datum switch?
A
13.000ft
9
Q
Is permitted to smoke in the lavatory in air transport operations?
A
No
10
Q
The Maximum battery charge rate immediately before takeoff shall not be greater then:
A
20 amps
11
Q
Minimum oil pressure in idle?
A
25 psi
12
Q
Before taking off with ventral tank full, each wing must contain at least how many pounds of fuel?
A
3.450 lb
13
Q
The maximum difference in weight of the fuel in wings tanks in flight is?
A
500 lbs
14
Q
If the ventral tank contains fuel, commence transfer to the wings when it contents indicated for each wings has reduced to:
A
3.300 lbs
15
Q
Minimum required breaking cooling time after one rejected takeoff?
A
25 minutes
16
Q
Minimum required breaking cooling after two rejected takeoff?
A
45 minutes
17
Q
The Rudder Bias system is a no go item?
A
Yes
18
Q
Can lift dump be used in flight?
A
No
19
Q
Can flaps and airbrakes used in flight?
A
No
20
Q
Maximum flap extension speed for 25°
A
175 kts
21
Q
Maximum flap extension speed for 45°
A
165 kts
22
Q
Maximum flap extension speed for 15°
A
220 kts
23
Q
Maximum altitude for procedural use of flaps for descend or holding?
A
15.000 ft
24
Q
Maximum ramp weight?
A
28.120 lb
25
Maximum takeoff weight?
28.000 lb
26
Maximum landing weight?
23.350 lb
27
Maximum zero fuel weight?
18.450 lb
28
Where can the maximum weight that may be carried in the baggage compartments be determined?
In the Weight and Balance manual and limitation placards on the baggage compartments.
29
Windshield heat must be ON prior to takeoff at least ____ minutes in ambient temperature below to ____ or ____ minutes below _____ for maximum bird strike protection.
Windshield heat must be ON prior to takeoff at least **5** minutes in ambient temperature below to **-10°C** or **15** minutes below **-20°C** for maximum bird strike protection.
30
If it’s not possible for windshield heat to be ON for the prescribed period before takeoff, airspeed must be restricted to:
257 kts until 8.000 ft
31
Vmo with fuel in ventral tank?
280 kts up to 33,730 ft
32
Vmo with ventral tank empty?
335 kts until 12.000 ft
33
Mmo?
Mach 0.80
34
Rought air speed, Vra/Mra?
230 kts / Mach 0.70
35
Va Maneuvering speed?
196 kts
36
Vlo / Vle landing gear speeds?
220 kts
37
Bird strike speed up to 8.000 ft?
280 kts
38
Maximum permissible altitude for flight?
41.000 ft
39
Maximum generator load?
300 amps in flight
280 amps on ground
Transient 400 amps for 2 min
40
Maximium ITT for normal takeoff, starting and relight?
978°C
41
Maximum continuous ITT?
968°C
42
Maximum ITT for takeoff with APR operating?
996°C
43
When icing conditions do not exists, the engine inlet anti-icing should not be used for more than _______ at temperatures above ________.
When icing conditions do not exists, the engine inlet anti-icing should not be used for more than **10 segunds** at temperatures above **10°C**.
44
Mmo with trim system fail/inop and autopilot disengaged?
Mach 0.73
45
Maximum crosswind
30 kts
46
Vmca flaps 15°
108 kts
47
Vmca flaps 0°
114 kts
48
Vmcg flaps 0° or 15°
115.5 kts
49
Flap retraction speed when Single engine
V2 + 10 kts
50
Recommended climb speed?
250 kts until 32.000ft and mach 0.70 above
51
Minimum zero fuel weight?
14.120 lb
52
Maximum altitude with gear and flap lowered?
20.000 ft
53
Maximum fuel temperature?
57° C
54
Approved fuels:
JET A and JET A1
55
Approved Oil consumption
0,01 us gal per hour
56
Maximum Oil temperature
127°C up to 30.000 ft
140°C above 30.000 ft
149°C for 2 minutes
57
Minimum temperature for starting?
-40°C
58
Minimum oil temperature for takeoff?
30°C
59
Oil pressure range for takeoff, maximum continuous and climb?
38 to 46 psi
60
Oil pressure for idle?
25 psi minimum
61
Transient maximum oil pressure:
55°C for 3 minutes
62
Turbine model
Honeywell
TFE731-5BR-1H
63
Thrust at sealevel
4.660 lb
64
Thrust with APR
4.750 lb
65
Maximum continuous thrust
4.634 lb
66
APU model
Honeywell GTCP-36-150
67
In flight use of APU
Use below 30.000ft
Starting below 20.000ft
68
Type Rating
HS125
69
Lenght
51ft 1.64in (15.59m)
70
Wingspan
51ft 4.5 (15.66m) in 800XP
54ft 4in (16.55m) in 850XP
71
Wheelbase
21ft 0.5in (6.41m)
72
Track
9ft 2in (2.79m)
73
Tailspan
20ft
74
Height
17ft 5in (5.31m)
75
Type ICAO
H25B
76
Maximum differential pressure
8.55psi (8.000ft at 41.000ft)
77
Pressure relief valves open at:
8.6 to 8.8psi
78
G-Load
Flaps UP: 2.73
Flaps Extended: 2.0
79
Main air valves should be closed for:
Takeoff and Landing
80
Rudder Bias should be:
Operative and ON for takeoff
81
Brake cooling time after rejected takeoff above 90kts?
Maintenance required
82
Main Batteries
2 x 24V 25 or 28 Amp or
2 x 24V 23 Amp
83
Circuit breaker reset
Not unless specified
84
Starter-Generators
2 x 28VDC
85
Engine starter duty cicle
30 seg ON, 1 min OFF
30 seg ON, 1 min OFF
30 seg ON, 30 min OFF
86
Alternators
2 x 208V random frequency
87
Inverters
2 x 115V 400Hz 1500VA
88
APU starter-generator
28VDC
89
Maximum Nosewheel angle using nosewheel steering?
45° each side
90
What is the maximum allowable duration of APR power?
Five minutes including the takeoff run
91
The Maximum tailwind component for starting engines is:
15 kts
92
Before filling the ventral tank full, each wing must contain at least ________ lbs of fuel per side.
Before filling the ventral tank full, each wing must contain at least **1.000** lbs of fuel per side.
93
Hawker 800XP fuel capacity when pressure refueled is:
9.957 lb
94
Maximum allowable refuel pressure from the truck is:
50 psi
95
Maximum allowable de-fuel suction is:
11 psi
96
With both DC boost pumps operating, the transfer of fuel from the ventral tank to the wing tanks takes approximately:
12 minutes
97
The are how many water drains in the fuel system?
5 water drais
98
Fuel is supplied to the engines by two:
28 VDC BOOST PUMPS
99
Where the gravity fuel port for the ventral tank is located?
On the left side of the aft fuselage
100
Normal pressure in the main hydraulic system is:
3.000 psi
101
The Pressure Maintaining Valve (PMV) closes when pressure drops below:
2.300 psi
102
In order to ensure adequate braking, before engine start there should be a minimum of _________ psi displayed on the emergency brake accumulator.
1.750 psi
103
When the landing gear horn will sound?
Less than 65% N1 and airspeed below 150 kts.
104
The brakes applied gauge indicators are powered by:
PS1 bus
105
Minimum pressure required in the Emergency Brake accumulator before starting engines in order to ensure adequate braking during the start.
1.750 PSI
106
When the amber EMRG BRAKE LOW PRESS annunciator is ON, it indicates that:
Emergency Brake Accumulator pressure is below 2.250 PSI
107
How many hydraulic pressure is required for normal braking with anti-skid and stick pusher operation?
At least 2.300 PSI
108
The speed of electrical pitch trim operation is determined by:
The position of the flaps
109
Warning of an impending stall is provided by:
The STICK SHAKER
110
Which flight controls are hydraulically operated?
Flaps and Airbrakes
111
The third crew member seat, when not in use, must be:
Folded, locked and stowed
112
Where the ground power receptacle is located?
Right rear fuselage
113
Minimum battery temperature at takeoff with (NiCad batteries)
-10°C
114
With both generators on line and the bus tie closed, the maximum permissible discrepancy between generator 1 and 2 ammeter readings is:
40 Amps
115
When charging the aircraft batteries using ground power, the EXT BATT CHG switch should be selected off when the charge current drops to less than ____ Amps.
When charging the aircraft batteries using ground power, the EXT BATT CHG switch should be selected off when the charge current drops to less than **5** Amps.
116
Why should the landing lights be used only briefly on the ground?
To protect the leading edge transparencies from damage.
117
In Pro-Line 21 equipped airplanes, the maximum demonstrated adverse wind components for autopilot coupled approaches are:
17 Kts crosswind
11 Kts tailwind
118
If the fuel quantity is less than ______ lbs, a go-around should not be attempted.
If the fuel quantity is less than **400** lbs, a go-around should not be attempted.
119
In the event of an AUXILIARY FUEL TRANSFER FAILURE may the flight be continued?
Land before airplane weight reduces to below 22,500 lbs.
120
How many minutes of priming and protection does the TKS system provide?
85 minutes
121
The TKS FLUID gauge first reads empty when there are how many minutes of priming and protection available?
15 minutes
122
Wing/Tail ANTICE should not be used in flight when the temperature is below how many degrees?
-28°C
123
On a normal takeoff, flaps are to be retracted when:
The airplane reaches 400ft AGL and a speed of Vfto.
124
On a non-precision approach, at the Final Approach Fix (FAF) the configuration should be:
Gear Down, flaps 25°, Airspeed Vref + 20kts
125
APU starting limitations
30 seg ON - 3 min OFF
30 seg ON - 3 min OFF
30 seg ON - 30 min OFF
Hawker 800XP
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