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Hawker > Engines > Flashcards

Engines Flashcards

0
Q

How much thrust does each engine produce?

A

4,660 Lbs of Thrust, static, at sea level up to 73 deg F

50R-1H engines are flat rated to a higher altitude and temp

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1
Q

What is the engine designator for the 900XP?

A

Garrett TFE731-50R-1H

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2
Q

What five components comprise the bypass section?

A 
Fan spinner support
Fan rotor assembly
Fan bypass stator
Fan duct assembly
Bypass fan support and shaft section
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3
Q

What drives the fan?

A

Low pressure N1 spool through the planetary gear section

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4
Q

How many stages are in the LP N1 spool?

A

Four

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5
Q

What two components comprise the LP N1 Spool?

A

Compressor

LP turbine

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6
Q

Describe the LP N1 spool compressor

A

Four stage, low pressure, axial flow

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7
Q

Describe the LP N1 turbine

A

Three stage, low pressure turbine

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8
Q

What does a stage consist of?

A

A paired rotor and stator

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9
Q

What does the HP N2 spool consist of?

A

Single stage centrifugal compressor

Single stage turbine

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10
Q

What drives the HP N2 spool?

A

Outer concentric shaft

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11
Q

What three components comprise the N2 compressor?

A

Impeller (rotor)
Diffuser
Compressor manifold

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12
Q

What happens when air reaches accelerating air reaches the N2 diffuser?

A

Velocity is reduced, converting kinetic energy into pressure

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13
Q

What additional component does the HP spool drive?

A

Accessory gearbox

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14
Q

How is the accessory gearbox driven?

A

Through a tower shaft and transfer gear reduction system

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15
Q

How many fuel nozzles are there in each engine?

A

12

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16
Q

What are the primary fuel nozzles used for?

A

All phases of engine operations including engine start

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17
Q

What are the two types of fuel nozzles?

A

Primary and secondary

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18
Q

What are the secondary fuel nozzles used for

A

All phases of engine operation except engine start

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19
Q

How many igniter plugs are there and what are their positions?

A

Two; six and seven o’clock

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20
Q

How many turbine wheels does the turbine contain?

A

One high pressure

Three low pressure

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21
Q

Where does gas go after leaving the turbine section?

A

Gas enters the nozzle system

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22
Q

Why are hot and cold air flows mixed through the convergent-divergent nozzle?

A

Results in more efficient use of thermal energy in hot core flow and also benefits smoke and noise reduction

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23
Q

How many thermocouples are located in the gas path between the high pressure turbine and the first stage of the low pressure turbine?

A

10

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24
Q

Where are the thermocouples located?

A

Between the high pressure stage and first low pressure turbine stage

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25
Q

What do the thermocouples do?

A

Measure the interstate turbine temp (ITT)

Send signals to the cockpit indicator and fuel computer

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26
Q

What six components does the accessory gearbox provide shaft power for?

A 
Hydraulic pump
Starter/generator 
Alternator
Fuel pump
Fuel control unit
Oil pump
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27
Q

What are the seven powerplant systems?

A 
Engine oil
Ignition
Fuel control
Power controls
Bleed air
Automatic Performance Reserve
Thrust reverser
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28
Q

What are the eight components of the engine oil system

A 
Oil tank and sight gauge
Oil pump
Oil filter and bypass valve
Air/Oil cooler and bypass valve
Fuel to oil cooler
Oil to fuel cooler
Breather pressurizing valve
Pressure and temperature transmitters and indicators
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29
Q

Where is the oil pump assembly located?

A

On the accessory drive gearbox

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30
Q

How many and what kinds of pumps does the oil pump assembly consist of?

A

One oil pressure pump

Four scavenge pumps

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31
Q

Where do the scavenge pumps collect from?

A

Planetary gear assembly and forward engine bearings
Aft engine bearings
Transfer gearbox and Mid engine bearings
Accessory drive gearbox

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32
Q

How does the oil pump assembly compensate for pressure changes due to aircraft altitude

A

Through the adjustable pressure regulator

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33
Q

Where is the oil filter located?

A

In a metal housing on the right side of the accessory drive gearbox

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34
Q

What is the capacity of the engine oil reservoir

A

1.65 US Gals

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35
Q

Where is the engine oil reservoir located?

A

On the right side of the engine fan bypass housing

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36
Q

What prevents the oil filter bypass indicator valve from actuating under cold oil conditions?

A

A thermal lockout device

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37
Q

Where is the fuel heater located?

A

On the left side of the engine

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38
Q

What does the fuel heater prevent?

A

Provides oil-to-fuel heat exchanging to prevent ice formation in the fuel system from clogging the fuel filter and other components

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39
Q

Where are the air/oil coolers located?

A

In the engine bypass duct

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40
Q

What device directs oil to or around the air/oil coolers?

A

The temperature control valve

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41
Q

What does the fuel/oil cooler do?

A

Uses aircraft fuel to maintain the oil at a constant temperature

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42
Q

What are the two components of the fuel/oil cooler?

A

Temperature control valve

Heat exchanger

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43
Q

What are the five components of the ignition system?

A 
Ignition unit
Igniter leads
Igniter plugs
ENG IGNITION switches
IGN ON annunciators
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44
Q

From where does the ignition unit receive power?

A

PE busbar

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45
Q

What are the three positions of the ignition switch?

A

OFF-AUTO-ON

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46
Q

Under what conditions should he ignition switch not be in AUTO, and what position should it be in?

A

Icing conditions; ON

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47
Q

At what point does the DEEC send an ignition request to the subject engine?

A

When N2 drops 500RPM when not commanded by the pilot through power lever movement

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48
Q

What is the approximate rate of fire for each igniter?

A

2 sparks per sec

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49
Q

From what ignition system device do the igniter plugs receive power?

A

From the ignition unit via independent high-tension leads

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50
Q

Where are the igniter plugs located?

A

On the combustion chamber

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51
Q

What are the five components of the fuel control?

A 
Fuel pump assembly
Hydromechanical Fuel Control Unit (FCU)
Digital Electronic Engine Control (DEEC)
Fuel Flow Divider Assembly
Fuel atomizers
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52
Q

What are the five components of the fuel pump assembly

A 
Booster pump element
Fuel filter
Filter bypass valve
High pressure pump element
Relief valve
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53
Q

Where is the fuel control unit located?

A

Attached to the rear of the fuel pump assembly

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54
Q

What does the fuel anti-ice valve do?

A

Mixes warm fuel from the fuel heater with the discharge flow of the booster pump to prevent icing of the fuel filter element

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55
Q

What does the fuel filter bypass do?

A

Allows fuel to bypass the filter if an excessive pressure drop across the filter occurs

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56
Q

What does the ENG # FUEL light indicate?

A

Excessive differential pressure or excessive fuel temp

Indicates ONLY a potential filter bypass

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57
Q

What event occurs if a fuel filter starts to become clogged with a differential pressure of 6-8 PSI?

A

Amber annunciator on MWS

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58
Q

What occurs if the fuel filter starts to clog with a differential pressure of 9-12 PSI?

A

The filter bypass opens to deliver fuel to the HP pump

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59
Q

What are the six components of the fuel control unit?

A 
Fuel monitoring section
Power lever input pot
Shutoff valve
Outlet pressurizing valve
Ultimate overspeed solenoid
Mechanical governor (N2)
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60
Q

What are the two modes of the mechanical governor?

A

As an overspeed governor for the HP rotor if the fuel computer is operative
As a Hydromechanical control when the fuel computer is Inop.

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61
Q

What devices operate the two FCU shutoff valves?

A

The throttle

Electronic engine computer

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62
Q

What happens if the DEEC senses an ultimate overspeed condition?

A

The DEEC closes the shutoff valve, fuel flows stops and the engine shuts down

63
Q

Where is the inlet pressure and temperature sensor located?

A

On the cowling forward of the fan inlet

64
Q

What powered the anti-icing for the inlet pressure and temperature sensor?

A

Electrical power from the PE bus bar

65
Q

What is the control parameter for the DEEC?

A

N1

66
Q

How many DEEC’s are there and where are they located?

A

2, located in therear equipment bay

67
Q

What does the DEEC control?

A

Engine acceleration and deceleration

68
Q

What are the modes of operation for each ENG CMPTR?

A

AUTO
OVRSPD PROT
(OFF)

69
Q

What powers each DEEC when in the automatic mode?

A

28VDC from the PE busbar

70
Q

What are the six inputs to each DEEC?

A 
Engine inlet pressure (PT2)
Engine inlet temperature (TT2)
Interstage turbine temp (ITT)
N2 speed
N1 speed
Power lever angle (PLA)
71
Q

The DEEC commands an engine shutdown at what N values?

A

107% N1

107.7% N2

72
Q

What happens if the DEEC malfunctions?

A

FCU switches to manual mode and the ENG # CMPTER annunciator will illuminate

73
Q

How many total CMPTER MWS annunciations are there?

A

7

74
Q

What are the two red computer annunciations?

A

ENG # COMPTER

75
Q

When does the red ENG # CMPTER annunciator illuminate?

A

During a total failure of the corresponding DEEC

76
Q

What is the memory action in the event of a red ENG # CMPTER annunciation?

A

ENG # CMPTER switch to OFF

77
Q

What happens when the ENG CMPTER switch is set to off?

A

Engine control is totally manual
Engine overspeed protection limited to the FCU mechanical governor
Ultimate overspeed protection is not available

78
Q

What does a yellow ENG # CMPTER annunciation indicate?

A

The respective DEEC has an internal fault but the the computer is still functional, to include ultimate overspeed protection

79
Q

Is any action required in flight for a yellow ENG # CMPTER annunciation?

A

No in flight action required

80
Q

What does the yellow ENG # CMPTER MM indicate?

A

A failure of the respective computer, and it had reverted to manual mode,
or:
The ENG CMPTER switch is off

81
Q

What does the ENG CMPTER OVSOD PROT mode provide?

A

Ultimate overspeed protection only

82
Q

What does a white ENG DEEC MINOR light indicate?

A

A minor fault but the computer is totally in control of the engine, ultimate overspeed protection is still available

83
Q

What does the surge bleed valve do?

A

Provides surge protection for the engine by opening the valve to allow bleed air into the bypass duct to smooth pressure through the engine to prevent compressor stalls and surges

84
Q

What device controls the surge bleed valve

A

The DEEC

85
Q

For what conditions does the DEEC normally position the surge bleed valve to open?

A

Start

Idle

86
Q

For conditions does the DEEC normally position the surge bleed valve to closed?

A

High RPM conditions

87
Q

What position is the surge bleed valve set to when the DEEC is OFF or failed?

A

1/3 open

88
Q

How does the DEEC position the surge bleed valve during transient rpm conditions?

A

DEEC modulates the surge valve in response to impending stall conditions

89
Q

Where is the fuel flow divider assembly?

A

Between the FCU and the fuel atomizers

90
Q

What does the fuel flow divider assembly do during engine start?

A

Routes fuel at a reduced rate to the primary atomizers

91
Q

How many fuel atomizers are there per engine?

A

12 duplex (primary and secondary)

92
Q

How many fuel manifolds are there per engine?

A

Two

93
Q

How does the fuel heater work?

A

Diverts a portion of engine fuel supply through fuel heater by the thermostatically operated anti-ice valve located in the fuel pump to prevent ice formation in the fuel system from clogging the fuel pump assembly fuel filter

94
Q

What does a yellow ENG # FUEL light indicate?

A

The fuel filter is blocked and is being bypassed

95
Q

What four components does the fuel flow indicating system consist of?

A

Fuel flow transmitter
Signal conditioner
Flow rate indicator
Fuel flow/fuel used indicator

96
Q

How does the fuel flow indicating system operate?

A

The transmitter is turbine-driven motor that rotates and generates an AC electric signal as fuel flows past it. From the transmitter a signal conditioner converts the AC signal to DC for the indicators

97
Q

What five components does the engine power control system consist of?

A 
Throttle levers
HP fuel cocks
Fuel control unit
DEEC
Engine synchronization
98
Q

How are the throttles connected to the FCU?

A

Mechanically through cables and a tele-flex control

99
Q

What position must the HP cock be in to allow full travel of the throttle?

A

Forward position

100
Q

What happens to the throttle when the HP cock is closed?

A

The associated throttle is locked in the IDLE position

101
Q

At what N1 setting will a warning horn go off if the gear is not down?

A

65%

102
Q

When will a warning horn sound if you are advancing the power?

A

If the air brakes are extended and gear is down

103
Q

What is the mechanical limit for power when the elevator gust lock is installed?

A

60% for both engines, though a single engine can be advanced without limit

104
Q

What two items are controlled by the HP cock

A

FCU

Hydraulic supply valve

105
Q

Closing the HP isolates the engine of what?

A

Hydraulic and fuel supplies

Removes power to the igniter unit via a microswitch in the lever

106
Q

What are the three positions of the ENG SYNC switch?

A

N1, N2, OFF

107
Q

What engines are the master and slave for synchronization?

A

Left is master

Right is slave

108
Q

What is the engine synch max authority range at mid-throttle?

A

+- 2.5% N2

109
Q

Does the engine synch have any effect at full throttle?

A

No

110
Q

What position must the ENG CMPTR switches be in IOT use engine sync?

A

Both switches must be in AUTO

111
Q

Does engine sync work when the APR is armed?

A

No

112
Q

What powers the engine sync system?

A

28VDC from the PE busbar

113
Q

What are the two bleed air ports for airplane services?

A

LP port is just aft of the last stage of axial compression
HP port is just aft of the centrifugal compressor
Dedicated engine anti-ice supply on top of the engine (900XP only)

114
Q

What four events happen when the ENG ANTICE switch is set to ON?

A

The anti-icing valve deenergizes open and HP air from the HP compressor is ducted forward to anti-ice the nacelle inlet cowl
Electric power is supplied to PT2 and TT2 sensor prove heaters
In flight, DEEC’s are reset to a schedule that incorporates raised idle rpm to compensate for the effect on thrust
The temperature provided by the A panel windscreen film is uplifted to ensure adequate anti-ice performance

115
Q

In the event of an electrical malfunction, what position does the anti-ice valve deenergize to?

A

OPEN, IOT act as a fail-safe

116
Q

DC supplies for the engine anti-ice system comes from what busbar?

A

PE

117
Q

What four services are provided with LP air, and supplementary HP air at low power settings?

A

Air conditioning
Normal pressurization
Emergency pressurization
Hydraulic reservoir pressurization

118
Q

What system is provided with LP air only?

A

Rudder bias system

119
Q

What does the APR system do?

A

Allows an automatic increase in engine performance in the event of:
a go-around during a singles-engine approach
or
an engine failure or transient fault during takeoff

120
Q

Under what conditions will there be no increase in thrust from the APRIL?

A

When N1 limited

121
Q

What powers the APR system?

A

PE busbar

122
Q

What are the two indications the APR is armed?

A

The APR ARMED switch light

On pilot MFD, a white box displaying APR ARM between N1 and ITT gauges

123
Q

What uncommanded engine split will trigger the APR activation?

A

15% N2

124
Q

What is the indication of an automatic triggering of APR?

A

Boxed green APR on MFD between N1 and ITT

125
Q

NOTE when is the only time the APR OVRD switch will illuminate in a 900XP?

A

When manually selected

126
Q

What must the ENG CMPTR be set to IOT respond to APR?

A

AUTO

127
Q

If an engine computer fails or is set to manual when APR is armed, what does the engine difference trigger become?

A

5%

128
Q

What thrust reverser system is installed on the 900XP?

A

Nordam TR5050

129
Q

Describe the thrust reverser system

A

Electromechanically controlled, hydraulically operated, target-type thrust reverser

130
Q

What are the five basic components of the thrust reverser system?

A 
Clamshell doors
Hydraulic actuators and linkages
Latches to hold doors in stowed position
Fan flaps
Thrust reverser accumulator
131
Q

What is the min psi for the thrust reverser accumulators?

A

1500 psi

132
Q

What are the three phases of reverser operation?

A

Initiation
Deployment
Stowing

133
Q

What conditions must exist for the ARM light to illuminate when the thrust reverser power switch light is depressed?

A

Weight on wheels
Throttle idle
Minimum of 400 psi hydraulic pressure

134
Q

NOTE: what is the tendency of the exhaust forces when the thrust reverser doors are deployed

A

Deploy

135
Q

NOTE: When engaged, the thrust reverser latches cannot be disengaged unless…

A

The overstow condition can be realized

136
Q

A mechanical stop is set to limit thrust when using reversers to a maximum of what?

A

65-70% N1

137
Q

What three things are inhibited when the reverser is deployed?

A

Rudder bias
Air brake warning horn
ELEV/AIL trim annunciator

138
Q

What triggers a reverser autostow?

A

If two latch position switches on the same side (inboard or outboard) indicate an unlatched condition

139
Q

How is an autostow actuated?

A

The isolation and stow valves are energized to provide stow pressure
ARM, UNLCK, and REVERSER lights illuminate
The affected throttle is moved to IDLE

140
Q

How long will an autostow procedure continue?

A

Until one of the two latches senses a latched signal

141
Q

How does the automatic throttle retard work?

A

Hydraulic pressure from the reverser system is used to force the engine fuel control mechanism toward idle when a stow signal is generated

142
Q

Where is electric power for the thrust reverser taken from?

A

PE busbar

143
Q

What is the reverser restriction for unpaved surfaces?

A

Reverse idle thrust only

144
Q

CAUTION: can the thrust reverser doors deploy without the engine operating?

A

Yes

145
Q

CAUTION: can you start the engine with the thrust reverser doors deployed?

A

The engines must not be started when the reverser doors are deployed

146
Q

CAUTION: what is required to shut the reverser doors when the engine is not operating?

A

One crew member must observe while another operates the system

147
Q

NOTE: when must thrust reversers be reduced to idle when stopping?

A

50 knots

148
Q

What are the five limitations of the thrust reversers?

A

Ground operations only
No engine starts with reverser doors open
No power backing
Idle thrust reversing only on unpaved surfaces
Full reverse minimum speed is 50 knots

149
Q

N1 takeoff operating limit

A

100%

150
Q

N1 Max continuous operating limit

A

100%

151
Q

NOTE: Thermal binding of the LP rotor can occur if engine restarts are attempted within…

A

25-45 minutes

152
Q

If engine restarts are to be attempted within 25-45 minutes of shutdown, what should be done?

A

The fan should be rotated 90 degrees by hand
Or:
A motoring cycle should be conducted

153
Q

NOTE: during an engine restart within 25-45 minutes of shutdown, start should be aborted if no N1 rotation is indicated before…

A

20% of N2

154
Q

N2 takeoff operating limit

A

100.8%

Hawker (8 decks)

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