Aircraft General & Limitations Flashcards

(41 cards)

1
Q

The 900XP’s type rating is what?

A

HS-125

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2
Q

What engines are equipped on the 900XP?

A

Two Honeywell Model TFE 731-50R-H

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3
Q

What is the general design of the 900XP?

A

Twin-turbofan engine, low-wing monoplane aircraft

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4
Q

What is the 900XP’s height?

A

17 feet 5 inches

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5
Q

What is the 900XP’s width?

A

54 feet

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6
Q

What is the 900XP’s length?

A

51 feet

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7
Q

What is the minimum turning radius of the 900XP?

A

26 feet 5.5 inches

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8
Q

How can you achieve the smallest turning radius?

A

Full tiller deflection, symmetrical idle thrust, no braking

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9
Q

Maximum Takeoff Weight

A

28,000 lbs

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10
Q

Maximum Landing Weight

A

23,350 lbs

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11
Q

VMO, VMO ventral tank

A

335 KIAS, 280 KIAS

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12
Q

MMO

A

0.80 Mach

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13
Q

Baggage Limitations

A

No external baggage; all baggage must be loaded in the interior

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14
Q

Could we use the White County airport if the taxiways were closed?

A

Yes

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15
Q

We Need 9000 lbs of Fuel Onboard - How Will it be Loaded?

A

7,500 lbs loaded in the wings (3,750 lbs per side), and 1500 lbs in the ventral tank

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16
Q

Where is the Emergency Exit, and What Type is it?

A

4th window on the right side of the fuselage - plug type door

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17
Q

N1PU Serial Number?

18
Q

Ventral Tank Fuel Restriction Before Flight?

A

Must be entirely full or entirely empty before flight

19
Q

Oil Consumption Rate

A

0.01 GPH/15 hour

20
Q

Minimum Operating Weight

21
Q

Bird Strike Normal Conditions

A

280 KIAS to 8,000 ft

22
Q

Minimum Enroute Temperature

23
Q

Garrett GTCP36-150W APU Max Gen Electrical Loads

A

Maximum Continuous Operation: 0.80; Transient Operations 1.2 < 10 seconds

24
Q

Where Are the APU Limitations Located?

A

Supplements section of the AFM

25
When Is the Inter-Compartment Door Open?
During takeoff and landing
26
Wing Fuel Quantity
1,268 gal/8,500 lbs
27
Ventral Fuel Quantity
233 gal/1,500 lbs
28
Total Fuel Quantity
1,501 gal/10,000 lbs
29
Minimum Wing Fuel Required for Fuel in Ventral Tank (To Be Loaded)
3,450 lbs per side
30
Wing Fuel Contents for Ventral Fuel Tank Transfer
3,300 lbs per side
31
Maximum Wing Fuel Imbalance (Flight, Takeoff, Landing)
500 lbs
32
Maximum Load Factor, Flaps 0
2.73G
33
Rejected Takeoff Speed
90 knots
34
What Does a Rejected Takeoff Over 90 Knots Indicated Require?
Brakes inspection
35
Minimum Altitude for Takeoff and Landing
-2,000 feet
36
Maximum Altitude for Takeoff and Landing
13,000 feet
37
The Emergency Escape Hatch Is on the _____ Side, _____ Window.
Right, fourth
38
To Receive External Power, the Ground Power Unit Must Be Plugged In to the Ground Power Receptacle on the:
Right rear fuselage
39
This Color Annunciator Indicates a Condition That Requires Immediate Crew Action:
Red
40
Electrical Heating Is Provided For:
Forward static plates, pitot heads, and windshields (all of the above)
41
When the Cabin Door Is Not in the Fully Locked Position, Microswitches Connected to the Master Warning System Illuminated the _____ Annunciator.
Yellow ENT DOOR UNLOCKED