Engine Flashcards
Max thrust continuous?
13,800 lbs
How much thrust do the engines produce?
13,800-14,200 lbs (ISA)
Describe N1 spool?
Single-stage fan
4-stage LP turbine
Describe N2 spool
10-stage compressor (gas generator)
2-stage HP turbine
How many igniters per engine?
2 per engine
How many igniters activate for engine start?
Ground…..1 igniter (switch in AUTO)
Flight……2 igniters (switch in AUTO)
What happens when the ignition switch is selected to OVRD?
Activates both igniters ON THE GROUND OR IN FLIGHT
Can the igniters be turned off during flight?
The switch may be moved to the OFF position but the FADEC disregards the command
The OFF position is used for DRY MOTORING on the ground only
What controls the engine?
A two-channel FADEC
One channel is active and the other channel remains in standby as a backup
Is only one FADEC channel used every flight?
No, they automatically alternate with each engine start
What does the cyan line on the N1 gauge represent during approach? When does it appear?
The minimum N1 for bleed requirements in icing conditions
Configured for landing less than 1200’ RA ( when anti-ice is ON)
What sources are available for engine starting?
APU
Ground Source (huffer cart or air bottle)
Opposite engine
Windmill start (in flight only)
Does the FADEC provide engine start protection?
Only on GROUND for a hot start, hung start, or no light-off
What will the FADEC automatically do in case of a start on the ground?
FADEC will not allow FF if ITT is greater than 120 degrees C
FADEC will automatically dry motor engine and introduce fuel when ITT is less than 120 degrees C
Describe the engine start sequence
1.start switch momentarily to START: 7% N2......ignition 20% N2 ......fuel flow 20% N2 +5 sec.....light off 50% N2....... Ignition off, Starter Cut-Out
2. Engine stabilizes N1.....27% ITT.....460 degrees C N2.....62% FF.......550 lbs/hour Oil pressure..... Greater than 25 psi