Overhead Panel Flashcards

1
Q

What does the DC service switch power

A

Lights; (NAV, Beacon, Service, Boarding,
Toilet, Galley Dome)

W/no AC PWR, SERV BUS is powered by APU BATT BUS via Service Bus contactor

  • SERVICE CONFIGURATION message appears on DC Synoptic page
  • Service Bus contactor not represented on DC Synoptic page
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2
Q

What lights will illuminate with the Battery Master on

A
AC ESS XFER
"INOP" L/R boost pump switch lights
"Fault" portion PRESS CONT switchlights
"OFF" portion L/R PACK switch lights
MACH TRIM switch light
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3
Q

Regarding the AC switchlight, what does AVAIL mean

A

System has correct volts, frequency, phase

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4
Q

IDG swithlight, what does the FAULT/DISC portion indicate

A

IDG has low oil pressure, or high oil temp

DISC; associated IDG is disconnected

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5
Q

AC ESS XFER light indicate

A

AC Bus 1 is not powering the AC ESS Bus

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6
Q

When should a Generator be reset

A

When directed to by QRH

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7
Q

AUTO XFER FAIL switch light indicates

A

GCU (GEN CONTROL UNIT), detected bus fault or
GEN overcurrent
Affected GEN taken offline
GCU ihibits auto transfer on affected side
Associated AC Bus can’t be powered by APU or offside

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8
Q

What is associate with successful FIRE TEST

A
FIRE SYS OK
LH/RH ENG and APU FIRE PUSH
LH/RH, APU BOTTLE Armed push to discharge
Both MASTER WARNING
FWD/AFT CARGO SMOKE push to discharge
Cargo BOTTLE ARMED push to discharge 
lights illuminate
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9
Q

What is the function of the L/R HYD SOV

guarded switchlight

A

Stops flow of Hydraulic fluid to associated (EGP)

Engine Driven Pump

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10
Q

L/R Boost Pumps, what does the INOP/ON portion indicate

A

Pump outlet psi is to low,

Pump outlet psi is satisfactory

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11
Q

What does the FAIL portion of the Gravity Crossflow

indicate

A

Gravity crossflow valve not in commanded position

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12
Q

L/R Crossflow switchlights, what does FAIL/ON indicate

A

Respected Crossflow SOV is not in
Commanded position

ON crossflow pump energized, fuel directed to
low tank

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13
Q

XFLOW AUTO OVERRIDE switchlight IN/ON

A

Pressed in arms crossflow pump for manual use

Pressed out pump is disarmed for manual use and
auto Crossflow is available (Switch not illuminated)

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14
Q

Wing A.I. Cross Bleed rotary switch

A

From Left, Right anti-ice valve is closed and bleed is is drawn from the L. ENG for both wings

From Right, Left anti-ice valve is closed and bleed air is drawn from the R. ENG for both wings

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15
Q

Bleed Valve Rotary Switch

A

AUTO - Automatic Operation of the Bleed valves
CLSD - Closes valves
Manual - Allows for manual operation of valves
controlled by ACSC ISOL toggle switch

CLSD - allows valve to open automatically when
APU LCV is opened during crossbleed starts
and cycle open/closed during auto transfer of bleeds
between APU and ENGs.

OPEN - allows for manual operation of valve in conjunction with BLEED VALVE rotary switch.

BOTH ENG - L/R bleed valve is open if both are capable of supplying bleed air, APU LCV is closed.

L or R ENG selected; selected ENG is supplying bleed
air if able, and the APU LCV is closed.

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16
Q

APU PWR FUEL Switch

A
Pressed, ECU is powered:
            APU BITE status message
            APU SOV OPEN status message
            Air inlet door opens
            APU RPM/EGT displayed on EICAS status page
            Fuel pump comes on
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17
Q

PUMP FAIL illuminates

A

APU Pump failed

18
Q

SOV FAIL illuminates

A

APU SOV not in commanded position

19
Q

APU START/STOP Switch

A
Ignition activates
Starter motor energized
Fuel Shutoff valve opens
Start switch illuminates
APU START message is displayed
20
Q

L/R ENG START switchlight

A

Pressed in, isolation valve opens
Associated starter valve opens
START switchlight illuminates
L or R ENGINE STARTER status message displayed

21
Q

STOP switchlight

A

Discontinues start sequence by closing ATS,

Air Turbine Starter

22
Q

CONT. Ignition switchlight

A

Engages continuous ignition

23
Q

Hydraulic Toggle Switches

A

1 (1B): Auto, allows 1B to operate when perspective bus is powered and 1 GEN is online and Flaps out of zero.
ON, allows pump to operate when perspective bus is powered and 1 GEN is online regardless of Flap position.
OFF, pump is off

3A: ON, allows operation of AC Motor Pump 3A
OFF, pump os off
3B/2: “Same as 1B”

24
Q

LDG ELEV control knob

A

Pre-selects a landing elevation

25
Q

MAN ALT control switch

A

Manual - control of cabin pressure
UP/DN - commands climb/descent
HOLD - holds selecte altitude

26
Q

EMER DEPRESS guard switch

A

Pressed, DC motor will open outflow valve and depressurize the aiplane

27
Q

PRESS CONTROL switchlight

A

Pressed allows outflow valve to manually operate with
MAN RATE toggle and rotary switch
(MAN portion of switch illums)

Fault portion illumiates, Both pressuritaion controlers have failed

28
Q

MAN RATE rotary switch

A

When Manual Mode selected, controls rate of change in cabin altitude

29
Q

PACK switches L/R

A

L/R pressed supplies air to the flight deck and main cabin perspectively through the mixing manifold.

FAULT portion:
indicates over temp or over pressure condition
OFF portion:
means just that

30
Q

RECIRC toggle switch

A

ON: energizes both recirculation fans

OFF: means just that

31
Q

RAM AIR guarded switch

A

OPEN: allows air from the ram air scoop into the mixing manifold, provides vetilation to the aircraft
(Switchlight Illuminates)

32
Q

L and R MAN switches

A

Allows Manual control of airflow through the PACK by directed actuation of the temperature control valve

33
Q

HOT/COLD toggle switch

A

Controls temperature when in manual mode

34
Q

CKPT and CABIN rheostat control knobs

A

Allows auto temp control through ACSC mixing hot/cold air

allows pre-selected temperature for the aircraft flight deck and cabin

35
Q

CARGO switch (3 positions)

A
  1. OFF: Closes intake and exhaust SOVs to seal AFT cargo bay
  2. AIR: SOVs open to allow recirculated or conditioned air in AFT cargo bay
  3. COND AIR: Provides automatic temperature control of AFT cargo bay using electric heater.
36
Q

WING toggle switch

A

ON: (AILC) Anti-ice leak detection controller modulates the wing anti-icing vavles

White N2 arc appears 0-77%

37
Q

COWL LH/RH toggle switches

A

Allows cowl anti-ice SOVs to open provideing bleed air into leading edges of cowls via piccolo tube

38
Q

ICE DET TEST switchlight

A

Provides 3 separate functions
-Tests Ice Detectors circuitry and probes
-Tests Probes and sensor heaters
-Switch will illuminate w/wing or cowls ice off along
w/ICE caution message

39
Q

WSHLD LH and RH toggle switches

A

Low: All 4 panels are heated to 24C
High: Windshields are heated to 41
C

40
Q

WSLD TEST button

A

Initiates a self test of windshield heating system.

L/R WSHLD HEAT and L/R WINDOW HEAT caution message is Good Test.

41
Q

PROBES toggles switches

A

ON: On ground w/AC power, TAT and probe bases are off

Static and AOA are heated

Pitot heads are heated