SYSTEMS VALIDATION REVIEW 2020 Flashcards
If Display Unit 2 and/or 4 are configured as PFDs set Reversionary panel knob to __________
MFD then AUTO
Can a DC GPU be used to replace BATT 1 & 2 for APU starting?
NO, DC GPU
ONLY
provides power to the APU START BUS
What is the procedure for abnormal start/no starter cutout?
QRC memory item for abnormal start, then QRH, Non
-annunciated procedures
If no starter cutout, proceed to QRH (Is annunciated)
APU shutdown sequence.
The cool down period is 1 minute. EICAS message APU SHUTTING DOWN Followed by spool down. If
the APU knob is turned back to on during the 60
seconds, the shutdown sequence is canceled
When can the after start check be deferred?
SOPM 4
-
5.3
If deicing/anti - icing is required. Delay until post deicing/anti - ice procedure XPDR as necessary
Safety and Power Up Checklist:
A silent READ and DO completed by either CA or FO
- Two ways to confirm power transfer?
Electrical synoptic page or 30 seconds after
When not to S.E. taxi:
SOPM 4
-
6.3
Ramp/Taxiway surface contamination
Maneuvering room in the ramp/gate area is marginal
Taxi time to/from a runway is expected to be less than 5 minutes
Airport
-
specific regulations prohibit S.E. taxi
Risk of injury to personnel or damage to equipment
- ## What page is required for a XBLEED start?
Status page to see duct pressure
40 to 45 psi
What wil l happen with the start/stop selectors? AOM V2 14 - 06 - 20 P2
FADEC will automatically switch to the other igniter if no light off is detected within 15s after
initiation of fuel flow. The start should be aborted if no light off is detected within 30 s after
initiation
of fuel flow.
Operational differences with carbon brakes.
SOPM 4
-
6.3
During taxi, minimize the duration of each brake application when practical by using shorter
applications with higher pressure on the pedals.
Avoid using brakes asymmetrically
What indications should the FMA have upon being issued line up and wait? AOM V2 14 - 09
FMA will have from left to right: TO armed for the AT, ROLL as the
active lateral mode, and TO as the
active vertical mode
ATTCS will command RSV thr ust when it is engaged, thrust levers are at TOGA position and one of the following conditions occurs: AOM V2 14 - 06 - 03 P3
Difference between N1 is greater than 15%
One engine failure during takeoff
One engine failure during GA
Windshear detection
In the AUTO position the HYD SYS logic activated the PTU if the engine 2 or EDP 2 fails. The PTU
will
be automatically started when all the following conditions are met:
Flaps not set to zero, or Landing gear not up and locked
EDP 1 Not failed
HYD reservoir 2 quantity above 12%
Can LNAV be armed on the ground?
SOPM 4
-
8.3
Yes
it will be engaged at 200 AGL
When should the pilot consider using the Downlock release button? AOM V2 14 - 13 - 15 P1
To prevent structural damage to the airplane the landing gear must be retracted only in the case of
an emergency that requires climb performance improvement
What is the A - I WING VLV OPEN message after take off? AOM V2 14 - 12 - 15 P1
ice (SAI IBIT) 10 mins after takeoff or at 10,000ft AGL whichever occurs first. The duration
is 60 seconds, but can be finished earlier if all
slat temperature sensors have increased 10F
When should the flaps be retracted climbing out?
SOPM 4
-
8.4
Flaps should be
retracted using the F
-
BUG
Root EICAS messages. (MSG. that come up that may cause other EICAS msgs. ) AOM V2 14 - 15 - 10 P3
If more than one root message is displayed at the same time or displayed together with a WARNING
message, the priority order to be evaluated is:
WARNING messages
ELECTRICAL BUSSES and then
MAU (Modular Avionics Unit)
What ADS reversionary logic does the F.O. system follow? AOM V2 14 - 09 - 10 P4
Normal is ADS 2 1st Reversion is ADS 3 2nd Reversion is ADS 1
Is it possible to get a FUEL LO LEVEL warning with fuel in the tanks? AOM V2 14 - 10 - 10 P10
Yes. If any
scavenge pump stops transferring to the collector box. The fuel contained in the collector
box flows out so that the fuel level inside the collector box and the rest of the tank reach the same
level or High pitch or High bank angle.
If a cruise altitude of FL380 is entered into the FMS, but the aircraft is cruising at a lower level, what is happening? AOM V2 14 - 02 - 20 P4
FMS cruise level set below FL370 7.8PSI is scheduled
FMS cruise level or airplane actually above FL370 pressure differential becomes 8.4 PSI
During ALT mode, how is speed controlled?
SPDt
Speed on Thrust
What happens when the DUMP button is pushed while in manual mode? AOM V2 14 - 02 - 20 P5
The Dump
function is not available in manual mode. However if the associated pushbutton is pushed
in, both RECIRC fan and PACKs are turned off
Which fuel pumps will be powered during an electrical emergency (RAT deployed)? AOM V2 14 - 05 - 10 P3; AOM V2 14 - 05 - 35 P1 6
AC Fuel pump 2A and the DC fuel pump will be available
During a dual engine failure why does the QRH direct the pilot to select Fuel
XFeed selector to LOW 1?
See question above…Fuel pumps AC 2 A and the DC fuel pump. Only 2 pumps going off one tank.
What is VB at FL 210? SOPM 2 - 3.3 V B
(10,000 and above) 270/ .76 M (whichever is lower)
If
the aircraft is cruising at FL250, with 12,000 set in the altitude selector, and
the pilot presses DESCEND now, what will happen?
The plane will command a 1000 FPM descent until intercepting the PATH
What information can the pilot get from GREEN DOT on the airspeed tape? AOM V2 14 - 09 - 05 P3
Indicates the driftdown speed when Slat/Flap is UP and the ideal Slat/Flap extension speed for the
current airplane weight
How long will batteries 1&2 provide power on their own? AOM V2 14 - 05 - 15 P2
In an ELECTRICA
L EMERGENCY, batteries are capable to supply airplane essential systems for at
least 10 min, even if the RAT is failed.
What are pilot considerations when STALL PROT ICE SPEED is displayed on EICAS? SOPM 4 - 12.7, QRH
Anytime the EICAS message STALL PROT
ICE SPEEDS is displayed during the approach in normal or
abnormal conditions, the speeds must be adjusted using the ICE ACCRETION table regardless of the
icing condition on landing.
How is VAP calculated? SOPM 4 - 12.7
Target approach speed is VAP
, which is VREF+wind correction
How can the back up radio be accessed?
Via MCDU 2. Go to Menu, then LSK4L. Pick the three step answer for the test
Which mode from the choices below use SPDE
?
FLCH uses speed on elevator
The Magenta course will change
over to LOC when using preview needles upon
capture. T/F
True
Allowances for minor fluctuations on final.
SOPM 4
-
12.7
Below 1000 but Above 500 HAT VMC or IMC:
PM will state deviation, PF will state “correcting” and make proper adjustment. If deviation
is not
corrected, missed approach is mandatory
IMC below at or below 500:
Should any unstabilized condition or EGPWS warning occur, missed approach is mandatory
When shooting a VOR approach with vertical guidance .... SOPM 4 - 12.19
When using an MDA for approach minimums, add 50 ft to the MDA (DMDA). Can use DA when published.
Can FMS Speeds be used during an engine failure?
SOPM 2
-
4.6
The use of FMS Speed Mode is prohibited in the event of an engine failure
You can use FMS Speed Modes during engine failure.
What are minimum and emergency fuel quantities?
SOPM 4
-
10.3
MIN 2250 lbs
Emergency: 1500 lbs
Which of the following are false?
Flaps 4 (It cannot be used for landing T.O. only)
When does GA become active on the engine instruments?
GA will be annunciated at gear down
What are the conditions to deploy ground spoilers?
The instructor answer was to choose answers A and B
1 Weight on Wheels
- Wheel speed 45kt. or airspeed above 60kt
- TLA below 26 degrees
After Landing sequence is…
Performed by the FO silently without verification
When shutting down an engine are there any considerations for taxi?
Taxi straight ahead
When parking at the gate you notice your brakes are hot, what can you do?
After the chocks are in, brakes can be released
To set the parking brake, first step on the pedals. T/F
FALSE
When establishing power how long do we wait before shutting down the
engines?
Wait 10 seconds after GPU or APU is established
Actually check electric synoptic page or
wait 30 sec after N2 stabilizes.
During your flight, you left the GPU button selected in. Will AC BUS 2 be powered by the GPU?
NO! Both busses will be powered by IDG1, until the GPU button is cycled
When can the post flight inspection be waived?
The correct answer is if the next crew meets you at the plane
