General Flashcards
Global 6000
Wing span
Length
Tail height
Wing span 94’
Length 99’ 5”
Height. 24’ 10”
Minimum pavement width for
180 degree turn
68’ landing gear
128’ wing clearance
C of G range
20% MAC to 41% MAC
Engine thrust SL to ISA + 20 C
14,750 lbs
2 main engine rotating assemblies
Single stage LP fan driven by 2 stage
LP turbine
10 Stage HP compressor driven by
2 stage HP turbine
How is engine protected from over speed
EEC recognizes N1 or N2 over speed
And closes fuel HPSOV
FADEC power source
Dedicated gen. On accessory gearbox
EEC controles idle speed to ensure
Proper operation of which services
Cowl anti ice
Cabin pressurization
Generator operation
Protection against water ingestion
Engine oil quantity
12.8 qts max
When is eng. oil quantity inaccurate
Between 5.2 and 9.0 qts
What is capacity of oil replenishment
Tank
6 qts
Which fuel shutoff valve closes after
ENGINE RUN switch off
HPSOV within the fuel metering unit
When should rotor bow be expected
Between 20 min. And 5 hours
after shutdown
When will eng. start
seq. Auto abort
On ground
Eng. Run switch OFF
N2 not >15% 120 sec.
from run switch on
Idle not achieved 120 sec.
after HPSOV open
Starter cutout not reached
within 180 sec. after start
valve open
ITT exceeding 700 C
What is
“ Quick Relight “
function
If Eng. Run switch is placed in OFF,
then returned to ON within 30 sec.
Engine will relight
Max altitude for Eng. relight
30,000’
How are thrust reversers controlled
And actuated
Controlled by EEC
Actuated by respective eng.
hydraulic system
When does APU door position appear
On status page
With
APU DOOR FAIL
msg.
When is manual operation of the
APU LCV not posible
Wing anti ice active
Left eng. pres. reg.
Valve manually opened
Right eng. pres. Reg. And cross bleed
Valve manually opened
How is emer. Shutdown
of APU
Accomplished
Batt Master OFF with no
AC power
APU DISCH handle pulled
APU SHUTOFF button
( ext. svc. panel )
APU compartment
SHUTOFF button
Slow start
Over temp
What 5 events
occur when
ENGINE FIRE DISCHARGE
handle Pulled
Fuel feed SOV closes
Hydraulic SOV closes
Bleed air SOV closes
AC VFG’s de-powered
Fire bottles armed
What 5 things occur when
APU FIRE DISCH
handle is pulled
APU fuel SOV closes
Pneumatics shut off
APU ignition shut off
APU power off
Fire bottles armed
Does pulling DISCH handle command
An immediate shutdown
No. Fire handle closes fuel feed SOV.
Engine will run a few sec. till lines empty
Immediate shutdown is via
ENGINE RUN switch
If APU fire is detected what action will occur
FADEC will command a shutdown after 5 seconds
Factory Smoke det. Locations
Fwd avionics bay
Aft avionics bay
Baggage comp.
