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HS125 > Limitations > Flashcards

Limitations Flashcards

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
Q

Maximum allowable de-fuel suction

A

11psi

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26
Q

Maximum difference in weight of the fuel in the wing tanks in flight is:

A

500 lbs

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27
Q

If the ventral tank contains fuel, commence transfer to the wings when the contents indicated for each wing has reduced to

A

3,300 LBS.

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28
Q

If the fuel quantity is less than ____ lbs. go-around should not be attempted.

A

400 lbs.

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29
Q

In the event of AUXILIARY FUEL TRANSFER FAILURE may the fight be continued?

A

Hawker 800: Land as soon as possible

Hawker 800XP: Land before airplane weight reduces to below 22,500 lbs.

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30
Q

Minimum required brake cooling time after one rejected takeoff:

A

25 minutes

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31
Q

Minimum required brake cooling time after two rejected take

A

45 minutes

32
Q

To ensure adequate pressure for normal braking, a pressure of at least how many PSI should be observed on the main hydraulic pressure gauge

A

2,300 PSI

33
Q

Is the rudder bias system a no-go item?

A

Yes

34
Q

May lift dump be used in flight?

A

No

35
Q

Where may flaps and airbrakes be used at the same time?

A

On The Ground

36
Q

Flap Extension speeds•

A

Flaps 15º ─ 220 Kts
Flaps 25º ─ 175 Kts
Flap 45º ─ 165 Kts

37
Q

Single engine flap retraction speed following engine failure on takeoff

A

Hawker 800: V2 + 9 Kts

Hawker 800XP: V2 + 10Kts

38
Q

Maximum altitude for procedural use of flaps for descent or holding:

A

15,000 ft

39
Q

How many minutes of priming and protection does the TKS system provide?

A
  • Hawker 800: 61 minutes

* Hawker 800XP: 85 minutes

40
Q

When the ANTICE LO QTY annunciator first illuminates how many minutes of priming and protection are available?

A

30 minutes

41
Q

The TKS FLUID gauge first reads empty when there are how many minutes of priming and protection available?

A

15 minutes

42
Q

Engine ANTICE should be used when in visible moisture and at or below a temperature of ____

A

10°C

43
Q

When not in icing conditions at above 10°C, the engine ANTICE must not be selected on for more than how many seconds?

A

10 seconds

44
Q

Wing/Tail ANTICE should not be used in fight when the temperature is below how many degrees?

A

-28°C

45
Q

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.

A

5 minutes
-10°C

15 minutes
-20° C

46
Q

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

A

257 Kts

8,000 ft

47
Q

Maximum ramp weight

A

Hawker 800: 27,520

Hawker 800XP: 28,120

48
Q

Maximum takeoff weight

A

Hawker 800: 27,400

Hawker 800XP: 28,000

49
Q

Maximum landing weight

A

23,350 lbs.

50
Q

Maximum zero fuel weight

A

Hawker 800: 17,520

Hawker 800XP: 18,450

51
Q

Where can the maximum weight which may be carried in the baggage compartments be determined?

A

The weight and balance manual and limitation placards on the baggage compartments.

52
Q

FLIGHT PROFILES AND MANEUVERSOn a normal takeoff, flaps are to be retracted when:

A

The airplane reaches 400ft. AGL and Vfto

53
Q

On completion of an ILS approach, speed at the threshold should be:

A

Vref

54
Q

On a non-precision approach, at the Final Approach Fix (FAF) the configuration should be:

A

Gear down
Flaps 25
Vref +20

55
Q

VMO when the ventral tank contains fuel

A

280 Kts up to 33,730

56
Q

VMO when the ventral tank is empty

A

335 Kts up to 12,000 ft

57
Q

Maximum Mach Operating Speed (MMO) .

A

.80 IMN

58
Q

Rough Air Speed (VRA/MRA)

A

230 KIAS / 0.7IMN

59
Q

Maneuvering Speed (VA)

A

196 Kias

60
Q

VLO/VLE

A

220 Kias

61
Q

Bird Strike Speed up to 8,000

A

280 Kias

62
Q

APU Starting Limitations

Honeywell GTCP 36-150 (W)

A 
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
Q

APU STARTING LIMITATIONS

Turbomach T62T-401

A 
Turbomach T62T-401
30 seconds operating
1 minute cooling
30 seconds operating
1 minute cooling
30 seconds operating
30 minutes cooling before
64
Q

Maximum permissible altitude for fight

A

FL410

65
Q

Maximum altitude for takeoff or landing

A

9,000 feet if not Cabin Hi Datum Equipped

13,000 feet if Cabin Hi Datum Equipped

66
Q

Minimum altitude for takeoff or landing-

A

-2000ft

67
Q

Maximum tailwind for takeoff or landing

A

10 knots

68
Q

Maximum demonstrated crosswind for takeoff or landing

A

30 knots

69
Q

Minimum battery temperature at takeoff

A

-10° C (NiCad)

70
Q

Maximum battery charge at takeoff

A

20 amps

71
Q

ELECTRICALMaximum generator load

A

300 amps

72
Q

Engine Starter operating time

A

30 seconds on - maximum

1 minute cooling after first and second attempt

30 minutes cooling minimum after third attempt

73
Q

When icing conditions do not exist, the engine inlet anti-icing should not be used for more than ______ at temperatures above _______ C

A

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
Q

Hawker 800XP

  • Maximum ITT for Normal Takeoff, Starting, Relight ………______
  • Maximum ITT for Takeoff with APU operating ………………______
  • Maximum Continuous ITT ……………………………………….._______
A

Maximum ITT for Normal Takeoff, Starting, Relight - 978°C

  • Maximum ITT for Takeoff with APU operating - 996°C
  • Maximum Continuous ITT - 968°C
75
Q

Hawker 800

  • Maximum ITT for Normal Takeoff, Starting, Relight ………______
  • Maximum ITT for Takeoff with APU operating ………………______
  • Maximum Continuous ITT ……………………………………….._______
A

Maximum ITT for Normal Takeoff, Starting, Relight - 952°C

  • Maximum ITT for Takeoff with APU operating - 974°C
  • Maximum Continuous ITT - 924°C
76
Q

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:

A

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
Q

4 Segments of the Climb

1st
2nd
3rd
4th

Where do they start? 
Where is the Landing Gear? 
Flaps? 
Power?
Airspeed?
A 
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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