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112 Cards in this Set

  • Front
  • Back
  • 3rd side (hint)

Aircraft is constructed of what type of meterial?

Primarily Metal. Portion of the tail composite


The cargo Light stays on for how long?

5 min



There is a courtesy light on the main door. how does it work?
The courtesy light Consists of a dome light and stair lights. They come on automatically when the door opens and stays on for 5 minutes. The lights will turn off if the door is closed. The lights can be turned back on with the main door switch. 9-01-40 p7


What controls the AC Power outlets?
2 outlets in the cockpit and 6 in the cabin. 115vac/60hz total of 800 watts. Optional: 2 additional galley outlets and 4 additional cabin outlets. Switch in the cockpit overhead panel.
What doors are indicated on the synoptic status page?
* PAX Main Door,

* Fuel Door

* Emergency Exit,

* Cargo Door

* FWD Electronic Compartment
What are the dimensions of the aircraft?

Width: 66' 5"


Length: 68' 1"


Height: 21'2"

MAX RAMP WEIGHT

38096 LBS



MAX TAKEOFF WT

37896 lbs

MAX LDG WT

34128 LBS

Zero fuel WT

26,500 lbs

MAX FUEL WEIGHT

13, 056 LBS

When the fuel imbalance between tanks is higher than __?___ kg (__?___lb) the FUEL WING IMBALANCE CAS message is displayed on the EICAS display. AOM-3929-200 - VOLUME 1 - TITLE 9-10-50 p8

510 lbs, 220 kg

The FUEL WING IMBALANCE CASmessage is no longer displayed on the EICAS display at what ___?__ lbs of fuel?

9-10-50 P8

110 lbs

If the FUELCROSSFEED (XFEED) knob is not in the OFF position and theimbalance difference becomes lower than _____ kg (_______lb), the FUEL EQUAL-XFEED OPEN CAS message is displayed on the EICAS display. 9-10-50, p8

90 lbs, 40 kg

Fuel temperature indication turns to amber when fueltemperature reaches values below ___?__ °C (-35°F). measured inthe left fuel tank.

-37 dg C, shown on the fuel schematic in the left tank.

Fuel engine temperature indication turns to amber whentemperature reaches values below _-__?____ °C (27°F).

- 3 dg C, Shown on the schematic by the engine

When the difference between current and expected fuel quantities ishigher than ____?___ lb, the FUEL QTY MISCOMP and CHECKENGINE 1 (2) FUEL flags are displayed on the Primary Flight Display(PFD). 9-10-50, p6

440 lbs

When the difference between current and expected fuel quantities ishigher than ___?___ lb), the FUEL LEAK SUSPECTED CASmessage is displayed on the EICAS display. 9-10-50, p6

880 lbs

When the fuel quantity is below ____?___ lb, the sensor sends asignal to the warning system triggering the FUEL 1 (2) LO LEVEL CASmessage. 9-10-50, p6

550 lbs

Main landing Light power supplied by what bus?

9-01-40, p1

LH Lights- DC BUS 1


RH Lights- DC BUS 2

What Controls the APU?
APU Controlled by a dedicated ECU (Electronic Control Unit). The pneumatic power is used for engine starting and to supply bleed airto the air conditioning pack of the Environmental Control System (ECS). Primary job is to power electric.
What is lost by using the PACK BACK-UP system?

Ozone converter

When does the Main Door Pressure seal start to pressurize?
* > 6o kts
* WOW switch on ground
* No Door PAX SEAL FAIL CAS message displayed.
Emergency Ram air Door opens when?
* Both Packs fail
* Dump button pressed
The Center e-bay fans come on when? 9-02-50, P4
On the Ground 2 fans operate. In the Air, ECS Turns fans off and center e-bay cooled by cabin ventilation
The FWD e-bay fans come on when?
Two fans, but only one operates and 2nd fan for stby. they alternate running each power up. If overheat or failed fan, the 2nd fan comes on controlled by the PSC (Pheumatic System Controller)
With the pressurization control in MAN, how much UP and DN is commanded by the switch?

50 fpm up or down

The PSC (Pneumatic System Controller) controls Pack back to 24 dg C through the TCV( Trim Control Valve)

24 dg C

What altitude do you set in the ALT window during an EMERG Descent?

10,000 OR MEA, whichever is higher.

Bank Angle limit automatically reverts to 15 deg when?

25,000 ft



The Flight Director will give an aural sound when it returns to what basic mode?

Roll and Pitch

The AFGS (Autopilot Flight Director Guidance System) locks the heading when __?___ dg or less
6 dg: the wings will be commanded to 0 deg bank with a commanded 6 deg or less bank.
What are the MAX limits of the FPA (flight Path Angle)?

+ or - 9.9 degs

The EDM (Emerg Descent Mode) automatically activates when?
* AP ON (enabled)
* Airplane > 25,000 ft. (enabled)
* Activated: Depressurization event occurs(Cabin Altitude CAS message displayed (10,000 + 300)
With The EDM ( EMERG DESC Mode) Activated, how will the aircraft react?
* FD vertical mode will go to FLH
* Speed bug commanded to VMO-5kts or MMO - 0.02M
* ALT preselected to 15,000 ft
* FD lateral mode transitions to HDG and will command a 90 deg left turn
* AT(Autothrottle) will engage and goes to idle indicates(AT IDLE)
* NEAR 15,000 MSL: FD vertical mode to ASEL, FD lateral mode remains HDG, AT will Activate SPEED mode bug set to 250 kts

What are the engine thrust setting modes?

TO-1, TO-2, GA, CLB, CON, CLB, IDLE, REV. Note: do not use TO-2 as of 4/16/15

From what fuel tank does the APU receive fuel?

Right Fuel tank

The APU will shutdown in flight for what causes?

* Overspeed
* underspeed
* ECU (Electronic Control Unit) Fail
* Bleed Leak
* If an auto-shutdown condition is detected before APU start, the startattempt is inhibited and the amber LED on the top half of the STARTbutton will illuminate. It will also illuminate when an auto-shutdowncondition is detected while APU is already running.
If the APU fails to start on the synoptic, what color will the APU status light be?
AMBER; If an auto-shutdown condition is detected before APU start, the startattempt is inhibited and the amber LED on the top half of the STARTbutton will illuminate. It will also illuminate when an auto-shutdowncondition is detected while APU is already running.
What is the APU operating envelope for starting, operation and electrical power?
* Max Altitude 31,000
* Max Temp: ISA+35 degC
* SAT between -62.8 C & -11.4 C
* Bleed Air for Engine starting: 23,000
* Bleed Air for ECS up to 20,000
3 altitudes and two temps
If the APU needs oil, what is the indication on the EICAS page?

CYAN reverse video



What will cause the APU to shutdown on the ground?
* Overspeed 106%, Amber at 103%
* underspeed
* ECU internal fault
* Bleed leak
* APU Fire
* APU EGT over TEMP
* APu high oil Temp
* APU low oil Pressure
* APU starter not disengaged
* APU fuel SOV failure
VOR Approach (Green needles) requires what type of vertical mode?

FPA(Flight Path Angle)



VOR Approach (Green Needles) uses what AFCS (Automatic Flight Control System) mode for lateral tracking?

APPR

Fuel backup pumps comes on when in the AUTO mode for what reasons? 4 items

Backup pumps are activated/deactivated by the FCU for:


* Engine Start

* APU start or run

* fuel low pressure
* main pump failure
*





What is the Volts and Amps output of the main generators?

28VDC and 600Amps

During an Electrical Emergency with no generators operating, What busses are powered?

Hot Battery busses and Emergency Busses 1,2,3

Batteries are charged by what sources?
* APU Generator

* RAT Generator
* Engine Generators 1 and 2
* GPU
What busses are not power during the lose of any generator?

Shed buss 1 and 2

What are the airspeed limits for the RAT?
A/S mins for the RAT

* 140 kts minimum airspeed to operate

* If you go below 140, have to go above 170 kts to reactivate





What buss does the RAT power?

Emergency Buss 3

What altitude limits are there to start the APU?
31,000 and temp warmer than -37 deg C
What controls all of the Electrical Contactors?


ECU (Electrical Control Unit)

What functions of the Electrical system are controlled by the ECU( Electrical Control Unit)?
* Over voltage
* Under voltage
* Ripple Current
* Field Fault
* Over Current
How many Ignitors does each engine have?

One ignitor with 2 channels and 2 ignitor plugs.


Note: Alternate ignition channels are energized for automatic ground starting,but both channels are energized automatically for all other engine starts

What source is used to start the engines?
Engines need high pressure pneumatic source for engine start.
What controls the ignitors?
When in the AUTO mode, the ignitors are controlled by the FADEC
What limitations are there for Reverse thrust?
* no back up

* Must be out of reverse thrust by 40 kts
How is the oil quantity checked on the engines?
Oil can be check on the EICAS Status page 5 minutes through 30 minutes (5-30 min). Past 30 min, motor the engine. Check manually.
What controls the engine ignition during engine flame out?
The FADEC controls the ignition. Both ignitors come on when in the Auto position. 9-06-55 p3
What Electrical power runs the FADEC(ECU)?

Emerg bus 1 and 2

What are the four basic Engine idle settings?
Engine idle settings are;
* Flight Idle

* Approach Idle

* Ground Idle

* Reverse Idle
What are the three FLIGHT IDLE Schedules, depending on the bleed configuration?

* Flight idle Wing Anti-Icing (WAI) ON dual bleed;

* Flight idle WAI OFF dual bleed;
* Flight idle WAI OFF single bleed.
Approach idle is selected when the airplane is in flight, and in approachmode. Approach mode is true when?
* Airplane is in flight;

* Either main landing gear is down and locked and flap is extended;

* Altitude is lower than or equal to 16500 ft. 9-06-70 p5
When is Ground idle activated?
When the a/c is on the ground and TLA not in reverse.
When is reverse idle activated?
Reverse idle activated when the A/C is on the ground and the TLA is in the Reverse range.
What engine power settings can be selected by the crew?

– Takeoff/Go-Around (TO/GA);


– Maximum Continuous (CON);


– Climb (CLB);


– Cruise (CRZ);


– Maximum reverse - landing;


– Maximum reverse - Rejected Takeoff (RTO).


9-06-70, p 5




What is ATTCS (Automatic Takeoff Thrust Control System)?
The ATTCS function is available to provide automatic thrust increase incase One Engine Inoperative (OEI) condition is detected for takeoff orgo-around. This thrust increase is available only when the WAI is ON. 9-06-70, p8
What makes the ATTCS (Automatic Takeoff Thrust Control System) activate?
The ATTCS is triggered (ATTCS provides thrust) if it is previously armed,and any of the following conditions are true:

– N2 difference between engines is greater than 15% N2(considering OEI);


– Loss of cross-engine communication;


– Thrust lever is moved to the MAX position.


Engine 9-06-70, p8


Note: When the ATTCS is triggered, an automatic thrust increase is providedat TO/GA position, in which the corresponding RSV thrust mode isprovided (TO-1 RSV, TO-2 RSV, or GA RSV). (pack shuts down to provide more thrust)

How does the engine produce more power when the TLA is moved from TO/GA to MAX power setting?
When the thrust lever isset to the MAX position, the PACK is closed providing a slight increasein thrust independently if WAI is ON or OFF.
At what altitude does the engines change from MAX CON to climb and what is MAX CON Power?
Max CON intended to be used during OEI.

Changes from CON to CLB between 15,000 and 20,000 feet


9-06-70, p8

The AS907-3-1E engine control system provides automatic engineprotection against what items?
* Overspeed;

* Over temperature;

* Surge;

* Flameout;

* UHT(Uncontrollable High Thrust) (ground only).
What are the dry motoring duty cycle limits?
1st Motoring: Max 5 minutes then 15 min cool down.


What are the starting Duty Cycle Limits?
Starting number 1-3: max time-80 sec, no cool down

Starting number 4 and over: Max time-80 sec, Cool down-15 min

What controls the Engine?
Each engine has a FADEC with an A and B channel
What type of fire detection and/or protection does the internal storage baggage department have?
no protection but has detection (smoke detector).
What type of fire detection and/or fire protection does the exterior baggage compartment have?
Detection: 2 channel detectors for smoke. Two nozzle fire protection system with high rate and a metered rate. 9-07-60, p3
How are all of the smoke detectors tested on the aircraft?
Fire test

Cockpit test sequence: push fire test button. Two lights up top, 6 red lights on the Eicas, 5 lights on the pedestal and then go back up to the test button and a third light should be on(13 lights)

What may happen if you press the Fire Test button a SECOND TIME WITHIN 15 SECONDS during the fire test?

APU may shut down

how many fire bottles are dedicated to the APU for fire protection and which bottle is it?

One bottle, Bottle B

What is the memory item for APU FIRE?
APU SHUTOFF Button.....PUSH IN

QRH EAP7-1

With an APU FIRE detected and indicated as a CAS message, the memory item is "APU SHUTOFF Button ...PUSH IN". What happens when this button is pushed in?
APU SHUTOFF Button Pushed IN:

* Closes the fuel SOV for APU

* Closes the Bleed SOV (shutoff valve)
* The white light will illuminate
* The APU button on the Fire Protection panel will light up red( arms the B bottle)
When the APU Fire Protection button is pushed in, what happens?
PUSH IN: Discharges the fire extinguisher bottle B agent at anadequate quantity, rate and discharge distribution on the APU.The APU button light goes off and the ENG-APU FIREX BDISCH CAS message is displayed, indicating that the fireextinguisher bottle B has been discharged. NOTE: In case of pre-existing bottle failure, the APU dischargebutton will not illuminate.
With an APU FIRE detected and indicated as a CAS message, the memory item is "APU SHUTOFF Button ...PUSH IN". Before you push this button in, what lights will be illuminated in that button? (Hint: 2 lights, one white and one red)
The Red light will be illuminated. After the APU SHUTOFF Button is PUSH IN , the red and white light will be illuminated. The white light indicates that all valves are closed and RED APU Fire Protection button will be illuminated(Red)
Hint: There is a white light and a red light
What will you expect to see and hear if you have an engine fire?
* ENG 1 (2) FIRE CAS message on EICAS
* FIRE will show in the ITT display
* An Aural warning will sound
* ENG SHUTOFF button will illuminate related to the engine with the fire
* Red Master warning and Caution will illuminate.
What are the memory items for ENG 1 FIRE? Hint: 4 items
* Autothrottle.......DISENGAGE
* Eng 1 Thrust Lever..... IDLE
* ENG 1 Start/Stop knob...STOP
* ENG SHUTOFF 1 Button...PUSH
What are the memory items for ENG 2 FIRE? Hint: 4 items
* Autothrottle.......DISENGAGE

* Eng 2 Thrust Lever..... IDLE
* ENG 2 Start/Stop knob...STOP
* ENG SHUTOFF 2 Button...PUSH
What happens when you push the ENG SHUTOFF 1 (2) button?
ENG SHUTOFF button pushed:

* Closes the Fuel shutoff valve

* Closes the Bleed valve for ECS
* Closes the HYD shutoff valve
* Arms the Bottles
* the red and white light will be illuminated, white indicating the valves are closes and red indicating a fire.
Flight Control question.

REU (Remote Electronic Units) controls what Actuators?

REU-Remote Electronic Units (8)

REU's control the EHA (Electro Hydraulic Actuators)and the EMA( Electro Mechanical Actuators)

What arms the ground spoilers?

ARMED MODE: When one of the following conditions are met:


Reject takeoff condition: When the wheel speed is > 30 kt;Touchdown condition: When the WOW sensors indicate air formore than 10 seconds.


Ground Spoilers range is from 0-40 degrees.

How are the ground spoilers engaged?

The ground spoilers have to be armed first. then engaged if:


* Both TLA indicate idle position, TLA <26 deg
* WOW sensor indicates ground

When are the Ground spoilers disarmed? Hint speed

Wheel speed < 30 kts


Airspeed < 40 kts


AOM 9-08-50, PAGE 10



Landing Flaps 3 with spoiler function.


When landing with flaps 3, how do the spoilers assist during flight.

Assists the pilot to maintain the airspeed and trajectory while performinglanding with flap 3 configuration. When this function is activated, thethree pair of spoilers are commanded to 15°.


AOM 9-08-50, P11

The flaps 3 with spoiler function is activated when? (3 pair of spoilers are commanded to 15 deg)

* Flap position is equal to 3
* Both TLA position < 50 deg (the TO/GA condition not met)
* The AOA limiter function not engaged
* All spoiler panels are engagedAOM 9-08-50, P11

SPEED BRAKES: AOM 9-08-50, P10


How many spoiler panels are there on each wing?

3 each side (0 deg to 30 deg controlled by the speed brake lever)

What conditions allow the speed brakes to function? (5 flight conditions) If any of the conditions do not exist, the deployed speed brake will retract.

* All consumed data are available and valid;
* Flap lever and position is less or equal to 2;
* Airspeed is greater than 160 kt;
* TLA position is less than 55° (no takeoff/go-around condition);
* The AOA limiter function is not engaged.
Note: Spdbrake Lever disag message with be on the EICAS if just one of the above are not.met.

In the Direct Mode, what indication is there of a stall?

The Aural warning STALL, STALL will be heard repeatedly

In the Normal mode, what indication is there during a stall or approaching a stall?

A Speed Low will appear in the FMA and if the A/T are off, they will come on

In the Normal mode, describe what the Red, Amber and white markers mean on the low end of the A/S indicator. (MINIMUM SPEED CUES) AOM 90-03-30, p5

For Normal Mode (NM):These indications are computed based on Angle of Attack (AOA)

* WHITE: Indicates the stability speed (VSS); ( will vary when you turn the aircraft but the amber and red remain the same based on AOA. 1.13 Stall spd
* YELLOW: Indicates airspeed which AOA limiter functionactivates; 1.08 stall spd
* RED: Indicates airspeed which corresponds to the maximumallowable AOA. 1.03 stall

What are the MINIMUM SPEED CUES in the direct mode?

* For Direct Mode (DM)The AOA limiter function is not operative for DM, and color on theminimum speed cues indicates:
* YELLOW: Indicates an airspeed with appropriate margin to theairspeed in which the stall aural alert is triggered; 1.15 stall spd
* RED: Indicates the airspeed at which the stall aural alert istriggered. 1.10 stall spd

AOM 9-03-30, P5

When landing with flaps 3 or Full and autopilot off, how do you trim the aircraft?

Trim is commanded by the TCS switch on the control stick. Press it and release it and the pitch trim will trim at the current indicated airspeed.




How do you disconnect the autopilot? 3 ways

* Press the autopilot button on the AFCS (Automatic Flight Control System) panel.
* Press the AP/Pty button on the control stick
* Supply manual force to the stick at a rate of 0.9 deg in any axis

If the pitch pointer is red on the pitch trim indicator, what does this mean?

It means that the aircraft is not within the green trim envelope


and when you press the Takeoff button, you will hear "NO TAKEOFF-TRIM"

What altitude will you see the radio altimeter appear?

2500 feet agl



What are the position of the VHF antennas on the aircraft?

Number 1 and 3 are on top of the aircraft. #1 is the front one. #2 is under the aircraft.

What position on the ACP(Audio Control panel) does the BOOM/AUTO/MASK knob need to be in to get the O2 mask to work for communications?

AUTO

The Audio Jack control panel is located in the side box. What is the function of the Audio BACKUP button?

The AUDIO BACKUP button when pushed will recover the use of the onside radio.


note: Recover use of onside radio when full ACP functionality is notavailable, providing the ACP the capability to re-route headphone,microphone, PTT and CVR signals directly to/from an analogemergency radio.

HOW LONG CAN THE COCKPIT VOICE RECORDER RECORD CONVERSATION?

120 MIN

Where are the push to talk buttons for VHF?

* on the stick

* CCP(Cursor Control Panel)
* Glareshield


How many AHRS are there and what are they for?

3 AHRS (Attitude and Heading Reference System)


- 2 for Aircraft


- 1 for the Flight controls


Note: Ahrs 1-L PFD, Ahrs 2-Rt PFD, Arhs one is powered by Emer Bus 1 and DC Bus 1, ARHS 2 -DC BUS 2 AND DC BUS 1

How many ADSP's( Air Data SMART Probes) does the aircraft have? How many TAT probes?

4 ADSP PROBES: ADSP 1(top Left) & 3 on Left side, ADSP 2(Top RT) & 4 located on the Rt side


2 TAT Probs

test 1

test 2