EMB7 Engines Flashcards
What controls engines?
Dual channel FADEC system
Describe how fuel gets to engines.
From collector tanks to engine fuel pumps. Splits into 2 streams
High pressure pump back to tanks to supply motive flow
Low pressure pump to heat exchanger to fuel filter, back to high pressure pump then to FMU (fuel metering unit) then to fuel injectors
What does the Oil system lubricate and cool?
Turbine engine main shaft bearings and accessory gear box
Where is oil quantity info displayed?
MFD
What does the starter system include?
ATS ( air turbine starter) SCV ( starter control valve) controlled by FADEC
Describe start sequence on ground.
FADEC opens SCV to allow pneumatic system to provide air to the ATS. FADEC initiates ignition at 7% N2 and fuel flow starts at 20% n2 provided ITT is 120° c or less
After lightoff , starter cutout at 50%n2 and commands FMU TO accelerate to ground idle
Ignition system
How many systems for start are energized?
Ground?
Flight?
1 on ground
2 in flight
What does ignition override do?
Both igniters on each engine are energized
Will cause sig reduction in igniter life if used frequently
Describe in flight cross bleed start.
Identical to ground start except FMU opens to provide fuel after 15 seconds even if 20% n2 is not reached
Describe windmilling start
Commanded by start stop switch Ignition at 7 % n2 Fuel flow at 7.2% N2 or 15 seconds whichever occurs first
Does FADEC provide protection for hot starts/ hung or failure to light off?
On ground yes. If no lightoff in 15 seconds after fuel flow it switches ignitions
In flight- no
When do you abort the engine start?
If no lightoff within 30 sec of fuel flow
Describe auto relight
FADEC monitors n2 and turns on both igniters and schedules relight fuel flow in event if flameout
WML icon will show next to respective engine n2 on EICAS
Inflight If engine does not relight automatically within 30 sec or n2 falls below 7.2% you should-
Consider it a failed attempt and you should terminate it manually by moving start stop switch to stop position
Auto relight on ground is terminated and fuel flow is shutoff if….
N2 falls below 52%.
The Thrust reversers are actuated and controlled by…
Actuated - Hydraulically
Controlled - Thrust lever
What prevents inadvertent thrust reverser deployment and stowing?
An interlock controlled by FADEC Consisting of 2 actuator locks and an independent cowl lock
Describe thrust reverser deployment
On ground move thrust levers to idle rev thrust Once both cowls are deployed you can command Max rev thrust by holding thrust levers in Max rev
What happens if one reverser fails while in Max rev?
Operating reverser will provide only min rev thrust unless you select just the operating thrust lever to Max rev
If thrust reverser actuates in flight what happens?
Engine thrust is limited to idle thrust
Engine control system consists of…
FADEC Thrust levers T2 N1 sensors
What does the thrust lever do?
Receives input of desired thrust setting from pilot or auto throttles
What does T2 do?
Monitors engine inlet air temp for FADEC control calculations
What does the n1 sensor do?
Provides fan speed info for FADEC and airplane vibration monitoring system
Describe FADEC
Main component of engine system It provides Engine protection Control of requested and Max N1 Control of ATTCS
FADEC has 2 identical independent channels one is the in control Channel the other is always in standby in case of active channel failure
The channels switch control on every start
Where does FADEC get it’s electrical power?
Below 50% n2 from the airplanes electrical system
Above 50% n2 from the PMA ( permanent magnet alternator)
Describe the ATTCS
Automatic takeoff thrust control system, Controlled by FADEC and is available on t/o and go around
It will provide RSV Power in event of engine failure
Displayed on EICAS as white - armed
And green - engaged. ( only when thrust levers are in TOGA
When will RSV POWER BE ACTIVATED?
ATTCS must be engaged And if one of the following occurs
N1 difference greater than 15% One engine fails during takeoff One engine fails during go around Windshear detected
Max thrust commanded by thrust levers
What is minimum flex thrust for takeoff?
75% of Max rated takeoff thrust or Climb -2 + .5 %n1 whichever is higher
What are the different idle modes?
Flight idle Approach idle Final approach idle Ground idle
When is approach idle activated?
Alt less than 15000’ In flight Flaps 1 or greater Gear down
When is final approach idle active?
Alt lower than 1200 agl Landing flaps set Gear down
Describe n2 over speed protection?
Whenever n2 reaches 102% FADEC commands an engine shutdown In the event of 3 consecutive over speed indications within 30 sec FADEC will not relight the engine
If FADEC aborts the start due to a high ITT what do you need to do?
Close the SCV by putting the start stop switch to stop
How much oil does each engine hold?
- 5 quarts
7. 2 usable
How much oil does APU hold?
4.54 quarts
What type of engines?
General Electric
CF34- 8E5 High bypass dual rotor turbofan
When will APU auto shutdown In flight
U. UNDERSPEED F. FADEC FAULT O. OVERSPEED
When will APU auto shutdown on ground
U. UNDERSPEED F. FADEC FAULT O. OVERSPEED S. SENSOR FAILURE H. HI OIL TEMP E. EGT OVERTEMP L. LOW OIL PRESSURE F. FIRE
