General

Question 1

Pilot aborts starts for:

Answer 1

1) No Oil Pressure within 20 seconds of ITT rise.
2) No N1 by 40% N2.
3) No stable GRD idle within 90 seconds of ITT rise.

Question 2

FADEC aborts starts for:

Answer 2

1) Insufficient ITT rise within 20 seconds after fuel flow.
2) ITT limit exceeded.

Question 3

TRU max current Limit?

Answer 3

100 Amps.

Question 4

Minimum battery temperature for APU Start?

Answer 4

-20C

Question 5

Minimum battery temperature for engine start?

Answer 5

-10C

Question 6

Flap setting for anti-ice Type 2, 3, or 4.

Answer 6

Flaps 1.

Question 7

Tail height.

Answer 7

21 feet.

Question 8

Aircraft width?

Answer 8

73 feet.

Question 9

Aircraft length?

Answer 9

63 feet.

Question 10

Monitored doors?

Answer 10

1) L and R Nose.
2) Passenger door.
3) Emergency exit door.
4) Baggage door.
5) Tail come access door.
6) Lav doors.

Question 11

Which electrical bus is the Cabin Door on?

Answer 11

Left Battery.

Question 12

Cabin entry door holds at closed for how many seconds?

Answer 12

10 seconds, +- 2.

Question 13

Cabin entry door “Pressure Warning” LED light means what?

Answer 13

Cabin is pressurized.

Question 14

Baggage compartment heated? Pressurized?

Answer 14

No. No.

Question 15

Battery type and amps?

Answer 15

44 amp/hr Ni-CAD.

Question 16

Engine Generator Amps?

Answer 16

300 Amps, Above FL350 275 Amps.

Question 17

APU Amps?

Answer 17

275 Amps.

Question 18

Fuel boost pumps turns on for:

Answer 18

SLAC

1) Starting engines.
2) Low Pressure sensed.
3) APU running without R engine running.
4) Crossfeed operation.

Question 19

Accessory Gearbox driven systems.

Answer 19

SOAPFH

1) Starter/Generator.
2) Oil Pump.
3) Alternator.
4) PMA (Permanent Magnet Alternator)
5) Fuel Pump.
6) Hydraulic Pump.

Question 20

Latitude Engines.

Answer 20

PW306D1, 5907 pounds of thrust.

Question 21

Service Air:

Answer 21

*Available anytime Bleed-Air source in on.

1) Cabin Recirculation Valve.
2) Enables ACM (Air Cycle Machine) low temp limit valve.

Question 22

PITOT/STATIC Heat:

Answer 22

1) Pitot
2) Static
3) Angle of Attack.

Question 23

ENG/STAB heat:

Answer 23

HIRES

1) Horizontal Stabilizer.
2) Inboard wing, (1/3).
3) RAT probes.
4) Engine Inlets.
5) Stator Vanes.

Question 24

What is powered by the hydraulic system:

Answer 24

BLTSSN

1) Brakes.
2) Landing Gear.
3) Thrust Reversers.
4) Speed Brakes.
5) Spoilers.
6) Nose wheel steering.

Question 25

Bootstrap Accumulator ensures:

Answer 25

Hydraulic pump lubrication during engine start.

Question 26

Elevator trim tabs:

Answer 26

1) Aerodynamically fairs elevator in position with the stabilizer. 2) Above Mach 0.77 helps prevent Mach tuck.

Question 27

What is a RED CAS message and it’s indicators?

Answer 27

Warning message: - Flashing Master Warning Light. - Audio Alert: Aural or (2) Chimes. - CAS message remains until resolved.

Question 28

What is a AMBER CAS message and it’s indicators?

Answer 28

Caution message: - Master Caution light. - (1) Chime. - CAS message remains until resolved.

Question 29

What is a WHITE CAS message and it’s indicators?

Answer 29

Advisory message. - CAS message flashes for 5 seconds, then steady.

Question 30

Engine Ground Idle?

Answer 30

57% N2.

Question 31

Engine Flight Idle?

Answer 31

65% N2.

Question 32

CDFA Requirements:

Answer 32

Continuous Descent Final Approach: VAST (Vertical decent, Altimeter, Straight, Temp) - Straight in Approach Minimums. - Published descent angle. - Cold correction if needed. - Local altimeter setting.

Question 33

Emergency Descent Mode Requirements:

Answer 33

- Aircraft Above 30,000 Feet. - Autopilot Engaged. - Cabin Altitude exceeds 14,500 feet.

Question 34

Flight Abort Mode Requirements:

Answer 34

- Descent is initiated. - Flight never reaches 6000 feet above takeoff field elevation. - Flight time less than 10 minutes.

Question 35

TOGA button actions when pressed:

Answer 35

- Cancels Autopilot. - Flight Director rolls wings level. - Flight Director pitches for 7.5 degrees in the air, 10.0 degrees on the ground. - Sequences the FMS for missed Approach.

Question 36

Generator cooling requirements:

Answer 36

Engine Idle with Generator load of <75 amps for 4 minutes prior to shutdown or wait 35 minutes after shutdown to start.

Question 37

Oxygen bottle size and location:

Answer 37

77 cubic feet, left nose compartment.

Question 38

Minimum Flap Maneuvering Speed

Answer 38

UP - 150 kts 1 - 145 kts 2 - 140 kts FULL - VREF+10

Question 39

RVSM Requirements

Answer 39

1 Autopilot 1 Altitude Alerting Device 1 ATC Altitude Reporting Transponder 2 Air Data Computers 2 Pitot Probe Heaters linked to ADC in use 160 kt Minimum Airspeed in RVSM Airspace

Question 40

Zero Fuel Weight

Answer 40

21,430 pounds