Systems

Question 1

ADC#1 Fail

Answer 1

Loss of Airspeed, Altitude and VSI. QRH NAP-29

Question 2

Flap Speeds

Answer 2

QRH (Performance Data) PD-2

Question 3

DC-Bus #2 Fails

Answer 3

MFD#1, PFD#2,

Question 4

IC-600#1 and IC-600#2 powered from

Answer 4

Essential DC#1 and DC#2

Question 5

nose wheel static wick

Answer 5

must be capable of touching

Question 6

ADC#1 and ADC#2

Answer 6

ADC#1: Pitot#1 and Static Ports 1 and 4

ADC#2: Pitot#2 and Static Ports 2 and 3

Question 7

Flight Data Recorder

Answer 7

Red BCN turns on FDR on ground, or FDR turns on automatically if airborne.
FDR: 25 hours solid state memory

Question 8

CVR

Answer 8

Records for 2 hours solid state memory.

CVR test; LED lights up for 1 second.

Question 9

T/O Config Check

Answer 9

Flaps, Spoiler, Trim, and Brakes

Question 10

ICAS Inhibition Logic

Answer 10

Takeoff: from V2-15 until 400’
Landing: from 200’ AGL until WOW plus 3 sec or 60 sec from passing 200’

Question 11

FLC - Flight Level Change Mode

Answer 11

Holds Speed 240 KIAS (<10,000) - 270 KIAS M0.65 (>10,000)

Question 12

Digital Audio Panel - EMRG Button

Answer 12

Ties to COM#1 on PIC side or COM#2 on SIC side

Question 13

AC BUS

Answer 13

115v 400hz, powers EGWPS/WINDSHEAR and TCAS

Question 14

GPU Connected

Answer 14

All buses powered, batteries are NOT being charged

Question 15

How many Batteries

Answer 15

Batt #1 and Batt #2 are interchangeable 24v; 44 amp hr Ni-Cads.
Batt #3 - 24v 5 amp Lead Acid (provides stabilized power for GCU)

Question 16

Fire Suppression System, Baggage Compartment

Answer 16

Two bottles: one high rate and one metering for 50 mins

Question 17

of GENs for SHED BUSES to be AUTO

Answer 17

3 or more

Question 18

4 or 5 GENs ON

Answer 18

Two isolated left and right electrical networks with all buses energized

Question 19

3 GENs ON

Answer 19

Both electrical networks interconnected (one network) through Bus Tie Contactors with all buses energized

Question 20

1 or 2 GEN’s ON

Answer 20

Both electrical networks interconnected (one network) through Bus Tie Contactors with shed buses deeergized

Question 21

Loss of all GEN’s

Answer 21

Batteries to supply the Essential Buses (in-flight condition only)

Question 22

Power Loss to Essential DC Bus

Answer 22

Emergency Lights come on

Question 23

Accessory Gearbox

Answer 23

H-ydraulic Pumps
O-il Pump
T-urbine (pneumatic starter)
F-uel Pump and Metering Unit (FPMU)
A-lternator (PMA)
G-enerators x2

Question 24

Fuel Pumps - Power Source

Answer 24

A and B pumps - Essental DC Buses

C pump - Main DC Bus

Question 25

ATTCS

Answer 25

Automatic Takeoff Thrust Control System

Question 26

Starting Engines

Answer 26

> 3 sec will abort start
RUN Position 3 sec
START Position 1 sec

Question 27

Engine Driven Hydraulic Pumps PSI

Answer 27

3000 PSI

Question 28

Electric Hydraulic Pumps PSI

Answer 28

2900 PSI +/- 200

Automatic Mode: <1600 PSI or N2 drops <56.4%

Question 29

Priority Valve

Answer 29

Hydraulic System 1: The Priority Valve will provide minimum flow to the landing gear system and give priority to the flight control services.

Question 30

Hydraulic System 1 - Liters

Answer 30

6L reservoir
1L Amber Range
<1600 PSI DC Pumps ON

Question 31

HYD SYS 1 (2) FAIL

Answer 31

ON CHECKRIDE

Question 32

Brake Overheat

Answer 32

> 420º, Temp in Amber range NO T/O

Question 33

Nose Wheel Steering

Answer 33

Electronically controlled and hydraulically operated. Pedals only 5º, steering handle only 71º, handle and pedals 76º

Question 34

Brake System: Touchdown Protection

Answer 34

Brake actuation will be allowed only after 3 seconds from the latest touchdown or after the wheels have spun-up to >50 kts.

Question 35

Brake System: Locked Wheel Protection

Answer 35

For wheel speeds below 30 kt, the locked wheel protection is deactivated and the brake system actuates without the wheel speed comparator. For wheel speeds below 10 kt, the anti-skid protection is deactivated, allowing the pilot to lock and pivot on a wheel.

Question 36

Landing Gear: Electrical Override

Answer 36

Bypasses the LGEU (Landing Gear Electronic Unit) and actuates directly the Landing Gear Electrovalve and the Nose Gear Doors Solenoid Valve.

Question 37

Landing Gear: Free-Fall Extension

Answer 37

Mechanically actuates the Free-Fall Selector Valve and unlocks 3 gear uplocks. Hydraulic fluid is sent back to reservoir.

Question 38

When Engine Fire Extinguishing Handle is pulled, what is cut off?

Answer 38

H - Hydraulics
A - Bleed Air
L - Lip Anti-Icing
F - Fuel at wing root

Question 39

Pitot/Static Tube 3 supplies

Answer 39

Total air pressure to the stby Airspeed Indicator, and static pressure to the stby Airspeed Indicator and stby Altimeter. Pitot/Static tube 3 supplies static pressure to the Cabin Pressure Acquisition Module (CPAM)

Question 40

Data Acquisition Units (DAU’s)

Answer 40

DAU#1 Left Engine and Forward Aircraft Systems
DAU#2 Right Engine and Rear Aircraft Systems
Each DAU has a Primary and Secondary channel. If a failure is detected the DAU will switch to the secondary channel.

Question 41

IC-600#1, IC-600#2 control which displays?

Answer 41

IC-600#1 - PFD#1, MFD#1, EICAS

IC-600#2- PFD#2, MFD#2

Question 42

Power source for PFD#1, MFD#1, EICAS MFD#2, PFD#2

Answer 42

PFD#1 - DC1
MFD#2 - DC2
EICAS - Essential DC Bus#1
MFD#2 - DC1
PFD#2 - DC2

Question 43

Power source for IC-600#1, IC-600#2

Answer 43

IC-600#1 - Essential DC Bus#1

IC-600#2 - DC2

Question 44

Power Source RMU-1, RMU-2, backup RMU-3

Answer 44

RMU-1 - Essential DC Bus #1
RMU-2 - Essential DC Bus #2
RMU-3 (backup) - DC Bus #2

Question 45

Turn WX on ground

Answer 45

STB x 4 < 3 sec

Question 46

Electrical System - In normal duel network, 4 generators or greater, which bus tie contactor is open?

Answer 46

Bus tie contactor #1 - (BTC 1)

Question 47

EGPWS Escape Maneuver

Answer 47

Max Thrust
Pitch Up 20 degrees
Climb to MSA

Question 48

BLD 1(2) OVTEMP

Answer 48

Associated pre-cooler downstream temperature above 305 degrees C