Quiz 5 APU/Fire Protection Flashcards
what does the APU provide
DC electrical power
environmental bleed air
both in-ground and in flight
Was the Hawker made with the APU
no it was added later via a supplemental-type certificate
(found in the supplement section of the AFM
The APU starter/generator power the aircraft electrical system via
PS2
Where does the APU get its fuel from
The left tank through the APU fuel shutoff valve
What does the stop button on the APU panel do
initiates shut-down of the APU - this button is used to shut down the APU during all normal operation
when will the automatic ECU shutdown of the APU occur in flight or on the ground
APU fire
low oil temperature
high oil pressure
DC power interruption of the ECU
Overcurrent to the ECU
loss of EGT signal
High EGT - above red line
overspeed - in excess fo 110%
loss of speed signal
Do we monitor the APU? Why?
no - it is self-monitoring to reduce pilot workload
Starter Generator when run by APU
as generator it powers the PS2 and PE - will power PS1 if bus tie is closed
APU emergency shutoff is located in the
rear equipment bay
(limitation) maximum rpm for APU
110%
(limitation) Maximum EGT for APU
1350F
(limitation) maximum transient EGT
14000F to 15000F for 15 seconds
(limitation) what pressure altitude can you not run the APU after
30,000
(limitation) what pressure altitude can you not start the APU after
20,000
(limitation) when will you shut down the APU if the ready to load light is not illuminated
within 60 seconds