Aircraft General & Limitations Flashcards
The 900XP’s type rating is what?
HS-125
What engines are equipped on the 900XP?
Two Honeywell Model TFE 731-50R-H
What is the general design of the 900XP?
Twin-turbofan engine, low-wing monoplane aircraft
What is the 900XP’s height?
17 feet 5 inches
What is the 900XP’s width?
54 feet
What is the 900XP’s length?
51 feet
What is the minimum turning radius of the 900XP?
26 feet 5.5 inches
How can you achieve the smallest turning radius?
Full tiller deflection, symmetrical idle thrust, no braking
Maximum Takeoff Weight
28,000 lbs
Maximum Landing Weight
23,350 lbs
VMO, VMO ventral tank
335 KIAS, 280 KIAS
MMO
0.80 Mach
Baggage Limitations
No external baggage; all baggage must be loaded in the interior
Could we use the White County airport if the taxiways were closed?
Yes
We Need 9000 lbs of Fuel Onboard - How Will it be Loaded?
7,500 lbs loaded in the wings (3,750 lbs per side), and 1500 lbs in the ventral tank
Where is the Emergency Exit, and What Type is it?
4th window on the right side of the fuselage - plug type door
N1PU Serial Number?
201
Ventral Tank Fuel Restriction Before Flight?
Must be entirely full or entirely empty before flight
Oil Consumption Rate
0.01 GPH/15 hour
Minimum Operating Weight
16,100 lbs
Bird Strike Normal Conditions
280 KIAS to 8,000 ft
Minimum Enroute Temperature
-75ºC
Garrett GTCP36-150W APU Max Gen Electrical Loads
Maximum Continuous Operation: 0.80; Transient Operations 1.2 < 10 seconds
Where Are the APU Limitations Located?
Supplements section of the AFM
When Is the Inter-Compartment Door Open?
During takeoff and landing
Wing Fuel Quantity
1,268 gal/8,500 lbs
Ventral Fuel Quantity
233 gal/1,500 lbs
Total Fuel Quantity
1,501 gal/10,000 lbs
Minimum Wing Fuel Required for Fuel in Ventral Tank (To Be Loaded)
3,450 lbs per side
Wing Fuel Contents for Ventral Fuel Tank Transfer
3,300 lbs per side
Maximum Wing Fuel Imbalance (Flight, Takeoff, Landing)
500 lbs
Maximum Load Factor, Flaps 0
2.73G
Rejected Takeoff Speed
90 knots
What Does a Rejected Takeoff Over 90 Knots Indicated Require?
Brakes inspection
Minimum Altitude for Takeoff and Landing
-2,000 feet
Maximum Altitude for Takeoff and Landing
13,000 feet
The Emergency Escape Hatch Is on the _____ Side, _____ Window.
Right, fourth
To Receive External Power, the Ground Power Unit Must Be Plugged In to the Ground Power Receptacle on the:
Right rear fuselage
This Color Annunciator Indicates a Condition That Requires Immediate Crew Action:
Red
Electrical Heating Is Provided For:
Forward static plates, pitot heads, and windshields (all of the above)
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
