Powerplant Flashcards

1
Q

Engine

A

TFE 731-50R twin spool turbofan

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2
Q

how many igniter plugs and fuel nozzles

A

2, 12

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3
Q

how much oil

A

1.65 gallons

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4
Q

what is the ignition powered by

A

PE bus

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5
Q

what do the DEECS run on

A

28vDC from PE bus
(Two of them)

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6
Q

engine shut down if N1 exceeds ____ or N2 exceeds _____

A

107% , 107.7%

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7
Q

Engine Sync

A

compares N1 or N2 of master engine (left) to right

authority range is +/- 2.5% N2 at midrange positions

inop with APR armed

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8
Q

what uncommanded slit will trigger APR

A

15% of N2

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9
Q

what type of thrust reversers

A

TR5050 bucket type

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10
Q

how are thrust reversers controlled

A

electrically through the PE bus

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11
Q

thrust reverser ion ground annunciator

A

rudder bias not inhibited

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12
Q

thrust reverser in flight indication

A

unlocked

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13
Q

N2 can spin at ____ RPM

A

30,000

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14
Q

TFE 731 spool up time

A

7 seconds

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15
Q

difference between stator and compressor

A

stators are stationary,
compressors spin

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16
Q

what’s on the accessory drive

A

Oil pump
Fuel pump (high pressure)
Starter generator
Alternator
Fuel control unit
Hydraulic pump

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17
Q

Where does the dEEC get info from

A

Engine inlet pressure
Engine inlet temperature
Interstage turbine temp
N2 and N1 speeds
Power lever angle

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18
Q

what do the DEEC inputs allow it to do

A

schedule, govern, and limit engine

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19
Q

what do the hp cocks do

A

when closed, mechanically lock thrust levers in full idle position

red fire warning light to indicate fire when in ON position

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20
Q

max thrust operating limit

21
Q

APR Automatic Power Reserve automode may activate when

A

Automode - APR activates when an uncommanded split in N2 occurs of 15% or more

22
Q

what do we operate the ignition in

23
Q

uncommanded ____ RPM drop will cause _____ to activate

A

500 rpm drop in N2 will reactivate ignition

24
Q

What measures the interstage turbine temperature

A

10 thermocouples between the high pressure turbine and first stage of the low pressure turbine

25
What oil pressure will cause the OIL 1 LO PRESS to illuminate
49 psi
26
where does the ignition system get power from
PE bus bar
27
The DEEC uses N1 or N2 for the control parameter
N1
28
can reverse thrust be used to taxi backwards
no
29
can reverse thrust be used in the air
no
30
can the engine be started with reverse thrusters deployed
no
31
when is thrust in excess of reverse idle above 50 KIAS allowed
prohibited unless emergency
32
is reverse thrust on unpaved surfaces allowed
no
33
the power plant classification on the Hawker 900xp
two-spool turbofan
34
When the aircraft is static on a standard day at sea level, each engine develops
4660 lbs of thrust
35
primary overspeed rpm-limiting device on the 731 series engine
mechanical governor in the FCU
36
Max HP rotor N2 overspeed is
102.5% for 10 seconds
37
max oil pressure for power at or above idle rpm
80 psi
38
max inter turbine temperature for engine starting
994C
39
max transient oil pressure permissible
100 psi
40
if the MWS reverser annunciator illuminates during the deploy cycle:
rudder bias not inhibited
41
to facilitate an accurate setting of climb power
CLIMB displayed in green on MFD engine display
42
the APR System is available
to any engine with an operative computer
43
DEEC ENG CMPTR switches to what during normal operation
AUTO
44
HP Cocks when closed
mechanically lock thrust levers in full idle position
45
APR does what
*MAY* allow automatic increase in engine thrust in event of engine failure
46
auto mode for APR activates
when an uncommanded split in N2 occurs of 15% or more
47
clogged oil filter
filter bypass displayed on a maintenance panel in the rear equipment bay
48
Start calls
Start (operating button) N2 (connected to starter/generator via tower shaft) (At 12% rotation without making a call HP cock up) ignition fuel flow ITT N1 Oil (at 49 PSI)
49
clogged fuel filter
ENG FUEL 1 or 2 annunciator indicates fuel filter is being blocked and bypassed