GV Notes

Question 0

How is landing gear operated?

Answer 0

Elect cont, Hyd actuated, mech sequenced.

Question 1

How many AC gen’s

Answer 1

5 total

2 - 40 kva eng gens

1 - 20 kva HMG

1 - 40 kva APU

1 - 1 kva emerg

Question 2

How is main cabin door sealed?

Answer 2

Passively

Question 3

All doors sensored except ?

Answer 3

Nose gear pin door

Gnd service door

Ext air door

Question 4

Where are the circuit breaker is listed by bus and where they listed by alpha numeric’s

Answer 4

QRH supplemental section page 5-11 and 5-24

Question 5

Where do you find evacuation procedures?

Answer 5

Section EI-6 for planned evacuation section S – 34 for emergency evacuation

Question 6

What gust lock and flight control checks must be done prior to engine start and take off?

Answer 6

Gus lock must be disengaged prior to engine start.

ForeFlight control check must be done prior to take off.

Question 7

Why is autoignition preferred over continuous ignition?

Answer 7

This avoids inadvertence selection of fuel off when terminating continuous ignition.

Question 8

Engine fire detection indications test - 8 items

Answer 8

Loop A
Loop B
CAS - Engine Loop
CAS - Engine Fire
2 - master warning
Fuel Switch
Fire Handle

Question 9

Difference between fire detection and APU

Answer 9

Engine fire detection - 2 loop, must agree (intui?)

APU - Helium filled tube

Question 10

Which DU can be inop for dispatch?

Answer 10

DU#5

Question 11

What does EDS, ASCB, EICAS, and EFIS mean and what do they cover?

Answer 11

EDS - electronic display system - the entire avionics system

ASCB - avionics standard communication bus - ?

EICAS - electronic information crew alerting system - PFD# 3&4

EFIS - electronic flight information system - PFD# 1&2, 5&6

Question 12

How do throttles provide input to engines?

Answer 12

Fly by wire system. Electronic

Question 13

What are the auto throttle switches function on the throttles?

Answer 13

Auto throttle disconnect on front - for only disconnect. Must be used if A/T failure indicated on PFD.

Auto throttle engage/ disengage button on back - normal operation

Question 14

What are the standby instruments and their functions?

Answer 14

1. Attitude indicator - can select ILS or back course
2. Combination airspeed and altimeter
3. DG - can select VOR or NDB

Question 15

How many of each - FWC, MACD, DAU, IRU, IAC’s

Answer 15

1. FWC - 2
2. MACD - 3
3. DAU - 2
4. IRU - 3
5. IAC - 2

Question 16

Which IRU’s supply which position?

Answer 16

IRU #1 - pilot

IRU #2 - alternate

IRU #3 - copilot

Question 17

Minimum EPR for A/T engagement?

Answer 17

EPR = 1.05

Question 18

Laser track provides ?

Answer 18

Lateral Nav only.

Must enter waypoints by Lat/Long

Question 19

What happens when G/A is pressed?

Answer 19

1. A/T to G/A EPR
2. FD director mode cancel
3. Pitch to 12* (stays active until another vert mode selected)
4. Wings level
5. FMS sequences to missed approach

Note:

Question 20

What indicates mode is armed or active on PFD?

Answer 20

White - armed but not active

Green - active

Question 21

How much throttle pressure required to deactivate A/T’s

Answer 21

30 lbs of pressure.

Question 22

What are the A/T disengage methods?

Answer 22

1. Engage/Disengage Sw
2. A/T disconnect
3. Manual moving throttles - 30lbs
4. Either Engine in ALT control
5. Single engine
6. Loss of EPR signal
7. Selecting cross-side A/T computer.

Question 23

What must you do on the ground for A/T to be available?

Answer 23

Airspeed less than 50 knots
Valid V2 speed
Valid EPR target
Isolation valve closed (APU)

Question 24

Field length required is the longest of ……

Answer 24

Accelerate stop / accelerate go distance.