Engine Flashcards
Engine Ignition must be on for:
() all answers are correct
() Takeoff and Landing
() Engine Anti-Ice Operation and Heavy Rain
What is the maximum allowable EGT for Engine Start?
725ºc
What is minimum oil pressure?
13 psi
What does an Amber Arc on an Engine Limit Display indicate?
Cautionary range
On the B737-800, the APU can supply electrical power and bleed air up to a maximum altitude of ________.
10.000ft
On the B737-800, the APU can supply bleed air alone up to a maximum altitude of ________.
17.000ft
On the B737-800, the APU can supply electrical power alone up to a maximum altitude of ________.
41.000ft
With the EEC in Normal Mode, if the thrust lever is advanced to the forward stop, the EEC will ____________________________.
limit thrust to the maximum certified thrust rating for current conditions
On the engine panel on the aft overhead panel, both ON and ALTN may be in view if the EEC has __________.
automatically changed to the soft alternate mode
When the EEC is in soft alternate mode, thrust rating shortfalls and exceedances _______ occur as flight conditions change.
can
The EEC provides N1 and N2 redline overspeed protection in __________.
normal mode and alternate mode
The engines may be started with air __________.
() all answers are correct
() from the APU or ground source
() by using engine crossbleed
On the B737-800 power is removed from the start switch holding the solenoid for starter cutout at approximately what N2 speed?
56%
On the B737-800, during ground starts, the EEC monitors engine parameters to detect:
() all answers are correct
() impending hot starts and EGT start limit exceedances
() wet starts
On the B737-800, what does a flashing white box surrounding the EGT during an engine start indicate?
an impending hot start
What occurs when the Engine Start Switch is placed in the GRD position?
() all answers are correct
() the starter valve opens, the engine bleed air valve closes
() the selected igniters(s) are energized when the engine start lever is placed to IDLE
What occurs when the Engine Start Switch is placed in the CONT position?
() Ignition is provided to the selected igniters when engine is operating and engine start lever is in IDLE
What occurs when the Engine Start Switch is placed in the FLT position?
() Ignition is provided to the both igniters when engine is operating and engine start lever is in IDLE
IGN L, is powered by AC transfer bus #1 for engine #1 and AC transfer bus #2 for engine #2. IGN R is powered by _________ for either engine.
AC standby bus
What occurs when the EEC detects an engine flameout?
both engine igniters are activated
What does X-BLD START above the N2 dial indicate?
crossbleed air recommended for inflight start
The thrust revers can be deployed when either radio altimeter sense less than 10 feet altitude, or when ______________________.
the air / ground safety sensor is in the ground mode
An amber REV displayed above the N1 gages on the center instrument panel indicated ________.
the thrust reverser is moved from stowed position