General

Question 1

Global 6000

Wing span
Length
Tail height

Answer 1

Wing span 94’
Length 99’ 5”
Height. 24’ 10”

Question 2

Minimum pavement width for

180 degree turn

Answer 2

68’ landing gear

128’ wing clearance

Question 3

C of G range

Answer 3

20% MAC to 41% MAC

Question 4

Engine thrust SL to ISA + 20 C

Answer 4

14,750 lbs

Question 5

2 main engine rotating assemblies

Answer 5

Single stage LP fan driven by 2 stage
LP turbine

10 Stage HP compressor driven by
2 stage HP turbine

Question 6

How is engine protected from over speed

Answer 6

EEC recognizes N1 or N2 over speed

And closes fuel HPSOV

Question 7

FADEC power source

Answer 7

Dedicated gen. On accessory gearbox

Question 8

EEC controles idle speed to ensure

Proper operation of which services

Answer 8

Cowl anti ice

Cabin pressurization

Generator operation

Protection against water ingestion

Question 9

Engine oil quantity

Answer 9

12.8 qts max

Question 10

When is eng. oil quantity inaccurate

Answer 10

Between 5.2 and 9.0 qts

Question 11

What is capacity of oil replenishment

Tank

Answer 11

6 qts

Question 12

Which fuel shutoff valve closes after

ENGINE RUN switch off

Answer 12

HPSOV within the fuel metering unit

Question 13

When should rotor bow be expected

Answer 13

Between 20 min. And 5 hours

after shutdown

Question 14

When will eng. start
seq. Auto abort
On ground

Answer 14

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

Question 15

What is
“ Quick Relight “
function

Answer 15

If Eng. Run switch is placed in OFF,
then returned to ON within 30 sec.
Engine will relight

Question 16

Max altitude for Eng. relight

Answer 16

30,000’

Question 17

How are thrust reversers controlled

And actuated

Answer 17

Controlled by EEC

Actuated by respective eng.
hydraulic system

Question 18

When does APU door position appear

On status page

Answer 18

With
APU DOOR FAIL
msg.

Question 19

When is manual operation of the

APU LCV not posible

Answer 19

Wing anti ice active

Left eng. pres. reg.
Valve manually opened

Right eng. pres. Reg. And cross bleed
Valve manually opened

Question 20

How is emer. Shutdown
of APU
Accomplished

Answer 20

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

Question 21

What 5 events
occur when
ENGINE FIRE DISCHARGE
handle Pulled

Answer 21

Fuel feed SOV closes

Hydraulic SOV closes

Bleed air SOV closes

AC VFG’s de-powered

Fire bottles armed

Question 22

What 5 things occur when
APU FIRE DISCH
handle is pulled

Answer 22

APU fuel SOV closes

Pneumatics shut off

APU ignition shut off

APU power off

Fire bottles armed

Question 23

Does pulling DISCH handle command

An immediate shutdown

Answer 23

No. Fire handle closes fuel feed SOV.
Engine will run a few sec. till lines empty

Immediate shutdown is via
ENGINE RUN switch

Question 24

If APU fire is detected what action will occur

Answer 24

FADEC will command a shutdown after 5 seconds

Question 25

Factory Smoke det. Locations

Answer 25

Fwd avionics bay

Aft avionics bay

Baggage comp.