Flashcards
What are the messages on the Ice test B (Ground) for the XR?
Selected no. 1 CLR ICE 1(2) CLR /I INOP 1(2) ICE DET 1(2) FAIL BLD 1(2) LOW TEMP CLR ICE 1(2) glareshield lights illuminate
Selected no. 2
Nothing
When does the high stage valve automatically opens?
Low engine thrust
Engine crossbleed start
Engine anti-ice operations
What color is the BLD 1 LOW TEMP?
Amber
Pack valve operational logic
[1L I P P / 2 E E G O]
Loss of bleed Source
Icing conditions below 24600’ pack#1(ifpack#2 is On)
Pack overload
Pack over heat
Essential power
Engine starts
Go around or takeoff:
[<1700’AGL /Engine bleeds on/ T/O-1 or higher(E-TO)]
One engine inoperative below 9700’(unless APU is used)
Lateral modes consist of
HDG - HDG HOLD & HDG SELECT
NAV - VOR NAV, LOC/BC, & NAV
APR- VOR APR,LOC/BC, & GS
BNK- LOW BANK SUBMODE
How can you cancel the Heading select mode?
Pressing heading button
Changing heading source on the pfd
Localized or back course mode has been capture.
VOR or approach capture.
Go around button.
Pressing couple button on the flight guidance.
When is the low bank mode automatically selected? Deselected?
Selected when Climbing above FL250 / deselected when descending through 24,700ft
When is VOR MODE cancelled?
- By pressing the NAV button
- selecting another lateral mode
- changing the display heading or NAV source on the PFD
- The displayed heading is invalid
- the Nav source is invalid for more than 5 seconds
- pressing the GO AROUND Button
- Placing the turn control knob out of the detent
What light should be Turner ON when taking the active taxiway
Strobe - ON
inspection - ON
Taxi - on
Pre departure duties
A - ATIS
C- Clearance
T- transponder
C- comms
H- heading
A- altitude
N- Navigation
What lights should be turned ON when take-off clearance is received?
Landing #1 - ON
Nose - ON
Landing #2 - ON
After takeoff check what do you check on the pressurization?
- Check cabin altitude remains steady
- check pressurization differential increasing
- check rate of change remains zero
What EICAS messages would you get when doing the FIRE TEST?
- Master warning + master caution lights
- ENG 1(2) FIRE
- ENG 1 (2) FIREDET FAIL
- APU FIRE
- APU FIREDET FAIL
- BAGG SMOKE
- BAGG EXT button illuminated
- both fire handles illuminated
- aural fire bell
What will happen if you hold the fire detection test button? For more than 10 a? (W/ the APU running)
It will cause an automatic APU SHUTDOWN
Alternate weather requirements
Drift down Wind alternate Ifr Breaking action Lite Takeoff alternate
What battery starts the APU on a battery assisted APU START?
Battery #2
Because battery #1 has sensitive components on it
Which door when open will cause a access door open EICAS message?
FWD Avionics
REAR electronics HATCH
Cockpit ACCS HACH
CAUTION WARNING
Stabilized approach
Speed vref between -5 to +10 kts Fully configured by 1000FT -flaps 22-45 -gear down -Engines spooled up
If GPU is plugged in but “not selected” will the ground service bus be powered?
Yes
Is cargo door pressurized?
Yes (ALL RED HANDLE DOORS ARE PRESSURIZED)
Do you need the APU to run the A/C packs?
Yes
Where is the hydraulic pump located?
On the engines accessory gear box
What is normal pressure for the hydraulic system?
2900 +- 200
When would you get a [HYD 1(2) PUMP FAIL message?
When would you get a [HYD 1(2) LO QTY] message?
Reservoir less than < 1 liter
What is the capacity of hydraulic reservoir?
6 liters
How many applications are available w/ the EMER BRAKE ACCUMULATOR?
6
What does the “ON” position for the electric hyd pump provide?
2900 PSI @1 Gal per min
Electric hydraulic pump comes ON when in the AUTO position at what point?
Pressure < 1600 PSI or n2 < 56.4%
When do you get a HYD SYS 1 (2) FAIL message?
Hydraulic pressure <1300 PSI
Max Dry motoring time?
5 minutes
When will the captain call for the after-start check
- After pushback (if required)
- After Engine start
- clear of ground personnel/equipment
- before aircraft movement
- after flaps are commended to take-off position
When should you begin the after-start flow?
Once the engines have stabilized
What flight control checks should you wait to accomplish until after the tug/tow bar has been disconnected and area is clear of personnel?
Do not complete -rudder check -engage noseheel sterring -select hydraulic pumps to AUTO -position flaps to t/o position Until tug or tow bar has been disconnected and the area is clear of personnel
Once the engines have stabilized and the tug/tow bar has been disconnected, what will the captain call for?
Flaps__, after start check
How can you identify PPG windshields?
They have horizontal bus bars
How would you identify the Sierra in windshield?
They can be identify by vertical bus bas
When should you turn the windshield heat ON w/ a PPG windshield?
During the after-start check
What selection should you make during taxi-out w/ sierracin windows?
Should be selected OFF during taxi-out UNLESS windshield fogging or icing is encountered or anticipated
Performance check is completed when?
- after the after start check
- prior to aircraft taxi
- if runway conditions or lox changes and it affects t/o performance, then the performance then the perf check must repeat
- Captain will call for performance check
What’s controlled by the FADEC?
- Fuel flow
- Compressor variable geometry
- Certain pneumatic functions during engine start, takeoff, and anti-icing.
Max %N1?
At what N1 speed will the FADEC command an automatic shutdown ?
100% - 105% N1
Max N2? At what speed will the FADEC command an automatic shutdown?
- 4% N2
105. 6% N2 & Below 54% N2
Accessory gear box (AGB) Components
- Fuel pump metering unit (FPMU)
- 2 DC electrical Generators
- Hydraulic Pump
- Oil Pump
- Air turbine starter (ATS)
- Permanent Magnetic alternator
How can we start the engine?
3 ways
Engine crossbleed
APU BLEED
Ground air supply source
FADEC commands MAX reverse works when?
-On the ground
-associated thrust reverser is requiring reverse thrust
-associated thrust reverser is deployed
-either condition exists:
1.both main landing gear indicate WOW
2.wheel speeds >25knts
Or 1. All 3 landing gear indicate weight on wheels (wow)
System inhibition stick pusher
- On the ground (except during the test)
- below .5G
- if the quick disconnect button is kept pressed.
- below 200ft AGL. (Reverts to 10s after takeoff if the radio altimeter have fail)
- if either SPS cutout button has been pressed (released or, unlatched button position)
- above 200KIAS
- if at least one SPS channel is inoperative.
when will the engine hydraulic shutoff valve close ?
It will close when
- the respective fire handle is pulled
- the guarded “ENG PUMP shutoff” button is pressed
Hydraulic system no. 1
AILERON RUDDER (half) SPLR INBD BRAKE OUTBD THRUST REVR 1 LDG GEAR Nose wheel STEERING
[you can also check on the poster]
Hydraulic system no.2
AILERON RUDDER (half) SPLR OUTBOARD BRAKE INBD THRUST REVR 2 BRAKE EMERG. parking [you can also read on the poster]
How is the latched fuel shutoff valve control?
The fuel shutoff valve is automatically controlled by the start/stop selector.
Pressing the APU EXTG Extingushing button will:
- Command FADEC shutdown of APU
- closes the APU fuel SOV
- discharges the fire extinguisher bottle into APU compartment
Baggage detection.
Baggage protection
Two smoke/heat detectors deactive the baggage compartment fan and causes a BAGG EXTG button to illuminate. A BAGG SMOKE message EICAS is presented.
Two fire extinguishing bottles installed. One instantaneously fills the baggage compartment. One metering rate discharge bottle provides extinguishing agent for 50minutes.
Engine fire protection is on what bus?
HOT battery bus
We have the ability to discharge the engine fire bottles on a depowered airplane.
All other fire protection requires the aircraft to be powered
How can we manually close the fuel shutoff valve?
The only way to manually close the fuel shutoff valve is when the engine fire handle is pulled.
When is the ground service bus powered? What is available when lights when using the ground service bus?
The ground service bus will be powered when a GPU is powered, plugged into the aircraft, but not selected and the batteries are off.
- Passenger cabin light
- Lavoratory lights
- Galley lights
- Courtesy lights
- cockpit dome lights
- Baggage/service compartment lights
Difference between Bleed 1? Bleed 2?
Bleed 1 Pressurization Wing 1 A/I STAB A/1 STARTER 1
Bleed 2
Pressurization
WING 2 A/I
STARTER 2
PNEUMATICS panel power sources
Everything below packs is essential XBLEED BLEED 1 APU BLD BLEED 2
Pack above:
PACKS 1 AND 2 DC
GASPER DC
RECIRC shed
what is lost ADC failure?
Airspeed
Altitude
Vertical speed
Autopilot defaults to basic pitch mode
What is lost on a AHRS Failure?
- Attitude
- Heading (PFD)
- Heading (MFD) if MAP mode
- autopilot may not function
What is MAG? MAG 1 MAG2
When there is a AHRS reversion and we are using the other side information for the Heading information
Reduced vertical separation mínimum ( RVSM )
Space aircraft between 2000-1000 FT.
FL 290 - FL 410
MEL Affecting fly below FL290
Holding
Reduce 3Min prior to holding fix.
Clean configuration. Time: 1 min at 14 and 1.5min above 14.
Min speed never less than 200kias in icing.
Max: standard.
-MHA TO 6 200
-6 TO 14 230
-14 ABove 265
CDR Coded departure routes
CDR are a combination of coded air traffic routes and refined coordination procedures designed to mitigate potential adverse delays during periods of severe weather or higher than normal traffic volume
CFIT controlled flight into terrain, EGPWS warning occurs
- Disconnect autopilot and set max thrust
- rolls wings level unless a turn is required
- rotate the aircraft to increase pitch attitude 20*up
- mantain configuration
Max xwind
30 knots
IMC
1000’ 3 miles
Two engine departure
-VMC allowed below 1000’ delayed until 400’AFE
-IMC delayed until 1000’
SID when procedure indicates. Altitude not published not below 400’
