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HS125 > Limitations > Flashcards

Limitations Flashcards

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1
Q

Minimum Crew for 800 / 800XP

A

Two

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2
Q

Maximum Number of Occupants

A

17

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3
Q

When not in use, the third crew member seat must be:

A

Folded and Stowed

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4
Q

Mmo with the ventral tank empty

A

.80 IMN

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5
Q

Maximum Air Temperature for flight

A

ISA +35°C

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6
Q

Minimum Air Temperature for flight

A

-40°C

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7
Q

Minimum Temperature Enroute

A

-75°C

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8
Q

Maximum Tailwind Component for takeoff or landing

A

10 knots

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9
Q

Maximum Runway Slope

A

2%

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10
Q

The ENT DOOR UNLOCKED annunciator extinguishes when:

A

The door closed and locked microswitches are both depressed

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11
Q

Maximum and minimum altitudes for takeoff or landing without use of a Cabin High Datum Switch

A

9,000ft - 2,000ft

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12
Q

Maximum altitude for takeoff or landing with the use of a Cabin High Datum

A

13,000 ft

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13
Q

In air transport operations, is smoking in the lavatory

A

NO

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14
Q

Minimum battery temperature at takeoff with(NiCad batteries)

A

-10°C

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15
Q

The maximum battery charge rate immediately before takeoff shall not be greater than:

A

20 amps

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16
Q

With both generators on line and the bus tie closed, the maximum permissible discrepancy between generator 1 and 2 ammeter readings is:

A

40 amps

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17
Q

For external starts, the ground power unit must supply _______ Volts. It must have a short term capacity _______ Amps and be fitted with _______ Amps current limiter

A

28 Volts
1,500amps
1,100 amps

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18
Q

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.

A

5 amps

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19
Q

Why should the landing lights be used only briefly on the ground?

A

The 450 Watt landing lights should be used only briefly on the ground to protect the leading edge transparencies from damage

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20
Q

In pro-line 21 equipped planes, the maximum demonstrated adverse wind components for autopilot coupled approaches are

A

17 Kts crosswind

11 kts tailwind

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21
Q

Minimum oil pressure for idle

A

25 psi

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22
Q

Before filling the ventral tank, the wings must contain how much fuel in each side?

A

At least 1,000 lbs of fuel per side.

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23
Q

Before taking off with the ventral tank full, each wing must contain at least how many lbs of fuel?

A

3,450lbs

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24
Q

Maximum allowable refuel pressure from the truck

A

50psi

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25
Maximum allowable de-fuel suction
11psi
26
Maximum difference in weight of the fuel in the wing tanks in flight is:
500 lbs
27
If the ventral tank contains fuel, commence transfer to the wings when the contents indicated for each wing has reduced to
3,300 LBS.
28
If the fuel quantity is less than ____ lbs. go-around should not be attempted.
400 lbs.
29
In the event of AUXILIARY FUEL TRANSFER FAILURE may the fight be continued?
Hawker 800: Land as soon as possible Hawker 800XP: Land before airplane weight reduces to below 22,500 lbs.
30
Minimum required brake cooling time after one rejected takeoff:
25 minutes
31
Minimum required brake cooling time after two rejected take
45 minutes
32
To ensure adequate pressure for normal braking, a pressure of at least how many PSI should be observed on the main hydraulic pressure gauge
2,300 PSI
33
Is the rudder bias system a no-go item?
Yes
34
May lift dump be used in flight?
No
35
Where may flaps and airbrakes be used at the same time?
On The Ground
36
Flap Extension speeds•
Flaps 15º ─ 220 Kts Flaps 25º ─ 175 Kts Flap 45º ─ 165 Kts
37
Single engine flap retraction speed following engine failure on takeoff
Hawker 800: V2 + 9 Kts | Hawker 800XP: V2 + 10Kts
38
Maximum altitude for procedural use of flaps for descent or holding:
15,000 ft
39
How many minutes of priming and protection does the TKS system provide?
* Hawker 800: 61 minutes | * Hawker 800XP: 85 minutes
40
When the ANTICE LO QTY annunciator first illuminates how many minutes of priming and protection are available?
30 minutes
41
The TKS FLUID gauge first reads empty when there are how many minutes of priming and protection available?
15 minutes
42
Engine ANTICE should be used when in visible moisture and at or below a temperature of ____
10°C
43
When not in icing conditions at above 10°C, the engine ANTICE must not be selected on for more than how many seconds?
10 seconds
44
Wing/Tail ANTICE should not be used in fight when the temperature is below how many degrees?
-28°C
45
Windshield heat must be ON prior to takeoff for at least _____ in ambient temperatures below___ or ______in ambient temperatures below______for maximum bird strike protection.
5 minutes -10°C 15 minutes -20° C
46
ICE AND RAINIf it is not possible for the windshield heat to be on for the prescribed period before takeoff, airspeed must be restricted to ______Kts indicated airspeed until an altitude of _____ ft is reached
257 Kts | 8,000 ft
47
Maximum ramp weight
Hawker 800: 27,520 | Hawker 800XP: 28,120
48
Maximum takeoff weight
Hawker 800: 27,400 | Hawker 800XP: 28,000
49
Maximum landing weight
23,350 lbs.
50
Maximum zero fuel weight
Hawker 800: 17,520 | Hawker 800XP: 18,450
51
Where can the maximum weight which may be carried in the baggage compartments be determined?
The weight and balance manual and limitation placards on the baggage compartments.
52
FLIGHT PROFILES AND MANEUVERSOn a normal takeoff, flaps are to be retracted when:
The airplane reaches 400ft. AGL and Vfto
53
On completion of an ILS approach, speed at the threshold should be:
Vref
54
On a non-precision approach, at the Final Approach Fix (FAF) the configuration should be:
Gear down Flaps 25 Vref +20
55
VMO when the ventral tank contains fuel
280 Kts up to 33,730
56
VMO when the ventral tank is empty
335 Kts up to 12,000 ft
57
Maximum Mach Operating Speed (MMO) .
.80 IMN
58
Rough Air Speed (VRA/MRA)
230 KIAS / 0.7IMN
59
Maneuvering Speed (VA)
196 Kias
60
VLO/VLE
220 Kias
61
Bird Strike Speed up to 8,000
280 Kias
62
APU Starting Limitations | Honeywell GTCP 36-150 (W)
``` Honeywell GTCP 36-150 (W) 30 seconds operating 3 minutes cooling 30 seconds operating 3 minutes cooling 30 seconds operating 30 minutes cooling before ```
63
APU STARTING LIMITATIONS | Turbomach T62T-401
``` Turbomach T62T-401 30 seconds operating 1 minute cooling 30 seconds operating 1 minute cooling 30 seconds operating 30 minutes cooling before ```
64
Maximum permissible altitude for fight
FL410
65
Maximum altitude for takeoff or landing
9,000 feet if not Cabin Hi Datum Equipped 13,000 feet if Cabin Hi Datum Equipped
66
Minimum altitude for takeoff or landing-
-2000ft
67
Maximum tailwind for takeoff or landing
10 knots
68
Maximum demonstrated crosswind for takeoff or landing
30 knots
69
Minimum battery temperature at takeoff
-10° C (NiCad)
70
Maximum battery charge at takeoff
20 amps
71
ELECTRICALMaximum generator load
300 amps
72
Engine Starter operating time
30 seconds on - maximum 1 minute cooling after first and second attempt 30 minutes cooling minimum after third attempt
73
When icing conditions do not exist, the engine inlet anti-icing should not be used for more than ______ at temperatures above _______ C
When icing conditions do not exist, the engine inlet anti-icing should not be used for more than 10 seconds at temperatures above 10 degrees C
74
Hawker 800XP * Maximum ITT for Normal Takeoff, Starting, Relight .........______ * Maximum ITT for Takeoff with APU operating ..................______ * Maximum Continuous ITT ..............................................._______
Maximum ITT for Normal Takeoff, Starting, Relight - 978°C * Maximum ITT for Takeoff with APU operating - 996°C * Maximum Continuous ITT - 968°C
75
Hawker 800 * Maximum ITT for Normal Takeoff, Starting, Relight .........______ * Maximum ITT for Takeoff with APU operating ..................______ * Maximum Continuous ITT ..............................................._______
Maximum ITT for Normal Takeoff, Starting, Relight - 952°C * Maximum ITT for Takeoff with APU operating - 974°C * Maximum Continuous ITT - 924°C
76
If hydraulic pressure is reading 2,300 and you assume then that the Hydrualic system has failed beyond the PVM what is: Provided by PMV: Auxiliary HYD: GONE: Powered by Accumulators:
Provided by PMV: Normal Landing Brakes w/ Maxarest Stall ID Auxiliary HYD: LDG Gear Flaps GONE: Air Brakes Nose Wheel Steering Powered by Accumulators: Emergency Brakes T/R
77
4 Segments of the Climb 1st 2nd 3rd 4th ``` Where do they start? Where is the Landing Gear? Flaps? Power? Airspeed? ```
``` 1st: Begins at Vlof - V2 Landing Gear Down Flaps T.O. Power: T.O. Airspeed: Vlof - V2 ``` ``` 2nd: Begins at V2 - roughly 400 feet AGL Landing - Up Flaps T.O. Power: T.O. Airspeed: V2 ``` ``` 3rd Begins at level off @400 through Vt Landing - Up Flaps T.O. Power: T.O. Airspeed: V2 - 1.25Vs ``` ``` 4th Begins at level off @1.25Vs Landing - Up Flaps - Up Power: Max Continous Airspeed: V2 - 1.25Vs ```

HS125 (14 decks)

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