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Tech Q's (FCOM 2) > TECH DECK > Flashcards

TECH DECK Flashcards

1
Q

REfer to the RF indication to the right of the Hydraulic system quantity indication.
This indication is displayed.

A

Only when the hydraulic is below 76% in either system A or B and the aircraft is on the ground with both Engines shut down.
Or after Landing with flaps up during Taxi.

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2
Q

Cargo compartment
Smoke detection system
Powered by?

A

DC Bus 1 and DC Bus 2

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3
Q

During normal ops

Hydraulic quantity indications vary

A

By Raising or Lowering the Land Gear and Lead edge devices

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4
Q

Once Activated, the APU DC operated fuel pump operates automatically UNTIL

A

an AC fuel pump pressurises the manifold

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5
Q

Amber Display Source annunciation bellow SPEED TAPE indicates

A

A single DEU has been manually or automatically selected to all six display units

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6
Q

Which of these is indicated by the HYDRAULIC BRAKE pressure indicator

A

MAXIMUM pressure 3500psi in white

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7
Q

The flaps/spats ELECTRONIC unit (FSEU) provides

A

Protection for LE devices and TE flaps if two or more LE Flaps or LE slats move from commanded position.

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8
Q

Zone TEMP maker light illumination for CONT CAB indicates

A

Both a duct temp overheat, or a failure of both temperature controllers.

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9
Q

If all TEMP ZONE SELECTORS are positioned OFF

A

the LEFT PACK maintains 24 DEG, RIGHT PACK 18 DEG

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10
Q

If the Autopilot ALT HOLT mode is manually overridden with the control column pressure, which of the following occurs

A

The autopilot changes to CWS P and returns to ALT HOLD if the control pressure is released within 250ft of the elected ALT.

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11
Q

ILL of FAULT light with the over heat detector in NORMAL indicates

A

Both detector loops for and engine have FAILED

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12
Q

Predictive windshear warnings

A

will activate up to 1.5 NM ahead of the AC

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13
Q

In addition to HYD sys A and B, the rudder can be powered by the STBY HYD sys through the

A

STBY rudder PCU

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14
Q

Normal Brake SYS Powered by HYD

A

SYS A

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15
Q

Auto brake uses HYD SYS

A

SYS B

Only operates when normal brake system is operating

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16
Q

Landing AUTOBRAKE setting may be selected after touchdown

A

Prior to decelerating through 30 KTS groundspeed

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17
Q

When is the ENGINE ANTI-ICE turned on if icing conditions exist on the Ground

A

As part of the AFTER START checks.

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18
Q

What could cause the AMBER anti SKID light to ILLUMINATE

A

FAULT in the PARK BRAKE system

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19
Q

MIN in flight tank FUEL TEMP is

A

3 Degrees Above fuel freezing point or -43 DEG, whichever is higher .

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20
Q

The Air/ Ground system receives Logic signals from

A

SIX Sensors, TWO on Each Landing Gear.

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21
Q

Source of ELEC power for the Engine Fuel shutoff valve

A

The Battery Bus

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22
Q

Manual IRS entry of present position or magnetic heading are normally accomplished on the

A

POS INIT page or ISDU

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23
Q

The Amber LOW PRESSURE light for SYS B HYD pump illuminates what are the other indications

A

MASTER CAUTION, and HYD annunciation lights illuminate

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24
Q

*The Red Landing GEAR indication lights are illuminated under which of the following conditions

A

Both: Landing Gear is in disagreement with the landing gear lever position
and the Landing Gear is not down and locked (With either or both thrust levers retarded to idle, and below 800ft AGL.

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25
Q

on GRD,
BATT SWITCH OFF
STBY POWER SWITCH on BATT

Switched hot bat bus IS ?

A

NOT POWERED

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26
Q

If ON DC on the LEFT IRS comes on steady

it MEANS

A

Related IRS is operating on
DC POWER from
SWITCHED HOT BATTERY BUS

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27
Q

FCCs

Number of ?

A

2

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28
Q

After normal T/O. the commanded pitch command is ?

A

V2 + 20

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29
Q

Right IRS is electrically powered from

A

Normally AC transfer Bus 2
In an Emergency from the switched Hot bat bus
MAX 5 MINS

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30
Q

The ENG start Switch OFF,

Austomatic Ignition will occur

A

if N2 is between 57% and 50%

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31
Q

With AUTOBRAKE select switch to RTO,

Autobraking is initiated when?

A

Wheel spin 90 KTSor more from thrust levers at IDLE

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32
Q

With MFD system, in SYS

The LOWER DU shows

A

Hydraulic Pressure and quantity only

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33
Q

If Landing is Made with the RTO selected

A

AUTO BRAKE DISARM light illuminates for 2 seconds after touchdown

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34
Q

In AUTO, the FASTEN SEAT BELTS and return to seats signs

A

ILLUMINATES when the FLAP and GEAR are extended

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35
Q

MAX ZERO FUEL WEIGHT

A

(61,688 KG)

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36
Q

MAX LAND WEIGHT

A

(65,317 KG)

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37
Q

DEU 1

A

CAPTAINS

(Capt 28V DC STBY BUS) supplies data to the captains outboard, inboard and upper DUs

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38
Q

DEU 2

A

(F/O 28vV DC BUS 2 ) supplies dRa to the F/Os outboard inboard and lower DUs

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39
Q

GPWS (LOOKS OUT FOR )

A 
WINDSHEAR 
TERRAIN 
OBSTACLES 
GLIDE SLOP DEV
CONFIG ALERTS
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40
Q

SINGLE CHANNEL FAULTS

A

PSEU
AUTO SLATS
MACH TRIM
SPEED TRIM

41
Q

Overspeed Clacker receives Aural warnings from

A

ADIRUs

42
Q

Speed clacker can be operated in ON Ground or in AIR

A

ON ground only

43
Q

ADIRU provides

A

P osition
A ttitude
A ltitude
S speed

44
Q

TCAS Resolution Advisory generated when

A

The conflicting AC is 25 seconds fro the point of closest approach

45
Q

Fuel for APU supplied

A

Left side of fuel manifold

46
Q

If NOSE GEAR steering lockout pin is not installed for pushback and towing

A

SYSTEM A HYDRAULIC PUMPS must be switched off

47
Q

TO RECIEVE NAV and ADF voice and range audio

A

Set the filter to BOTH

48
Q

During VNAV path decent and below the speed restriction altitude
The FMC alerting message OVERSPEED DISCONNECT means

A

VNAV has disengaged because airspeed has exceeded FMC target speed by more than 15KTS

49
Q

Autopilot Trim & MAIN Stabiliser Trim use

A

Single ELECTRIC TRIM MOTOR

50
Q

EGT Display, both box and dial, TURN RED and the EEC automatically turns off IGNITION and shutoff fuel to the ENGINE if

A

The EGT EXCEEDS the starting limit during GROUND starts

51
Q

No 1 DRIVE light ILLuminates AMBER. This is directly caused by

A

LOW OIL pressure in the IDG

52
Q

With the Loss of HYD System B (System A operating Normally)

A

Main and STBY Yaw damper functions are lost

53
Q

PTU provides alt source of power for the Autoslat System if

A

A loss of Hydraulic System B is sensed

54
Q

APU MAINT Light means

A

APU can be operated

55
Q

If thrust lever (s) are advanced after Touchdown

A

After 3 Seconds in the advanced position,

AUTOBRAKE DISARM LIGHT WILL ILLUMINATE

56
Q

Predictive Wind shear alerts

A

Below 1200FT Rad alt

57
Q

During flight with HYD system B inoperative (No Fluid in System B)

A

The STBY HYD System operates the leading edge slats and leading edge flaps to fully extend position only

58
Q

To climb to FL280 in the shortest distance, MAX ANGLE should be selected on page?

A

CLB

59
Q

PROXIMITY TRAFFIC SYMBOl

A

WHITE SOLID DIAMOND

60
Q

Accessory Gearbox receives info from

A

N2 Rotor

61
Q

BLEED TRIP OFF LIGHT

A

INDICATES excessive bleed air pressure or Temp

62
Q

FMC Advisory message BUFFET ALERT Indicates

A

Current Conditions results in MANOEUVERING MARGIN less than Specified.

63
Q

During primary Charge CYCLE

BAT CAN BE AS HIGH AS

A

30 VOLTS

64
Q

When Does RAD ALT display a DIGITAL readout

A

Between 2500ft and 1000ft AGL

65
Q

LOW PRESSURE LIGHT Main tank indicate?

A

Low fuel pump OUTPUT pressure

66
Q

Bleed trip off light, What valve has automatically closed

A

ENGINE BLEED AIR VALVE

67
Q

HYdraulic Pressure from System B will be used to retract the landing GEAR

A

After failure of No1 Engine with the Landing Gear still down and the Landing gear lever is positioned up.

68
Q

Antenne Switiching from TAIL ANTENNA to NOSE ANTENNA OCCURS when

A

LOC frequency is selected and VOR/LOC is armed and ENGAGED

69
Q

RAM AIR SYSTEM DEFLECTOR DOORS

A

EXTEND on the GROUND only

70
Q

AC not certified above

A

82N and 82S

71
Q

AFTER FMC CDU preflight , Flight crew notices the ACTIVE NAV DATA BASE is expired, must be changed,
WHAT will route page look like after NAV DATAbase change

A

BLACK, Requiring RELOADING.

72
Q

TOGA Switch pressed, once bellow 2000FT RA
AUTOMATIC GO AROUND
FLARE ARMED
ILS Channel APP

A

Auto throttles advance thrust levers to

REDUCED go around N1

73
Q

WHeel spinnup not detected on Landing
With the speed brake armed the flight spoilers will rep
Automatically when

A

When the Air/Ground senses the ground

any strut compresses

74
Q

If the Fault light on IRS mode SELECTOR UNIT ILLUMINATES

Indicates

A

A system Fault affecting the respective IRS ATT and /or NAV mode has been detected

75
Q

Power source for FIRE EXTINGUISHING

A

the HOT BATT BUS

76
Q

DOTTED RED AREAS

TERAIN DISPLAY

A

Terrain more than 2,000ft above the airplane ALT (BARO)

77
Q

Which statement is true regarding AILERON TRIM

A

If the autopilot is engaged

The amount of trim is not indicated on the scale.

78
Q

ALL WINDOW HEATS SELECTED ON
The Green window heat ON extinguishes
WHY

A

System is at Correct TEMP.

79
Q

MIN EQUIP for RAs to be GENERATED

A

The other AC needs a MODE C Transponder

80
Q

When the manual gear extension access door is open

A

Manual landing gear extension may be accomplished with the Landing gear handle in the up position

81
Q

WITH ENGINE START switches OFF, Automatic IGNITION will occur

A

IF N2 is between 57% and 50%

82
Q 
During preflight
procedure the trim air
switch is left in the OFF
position and only one
pack is selected ON for
airconditioning. What is
the correct
consequence?
A 
With the TRIM AIR
selected OFF, the pack
attempts to produce an
air temperature to
satisfy the average
temperature demands
of all three zones.
83
Q

An overheat condition causes the pack valve

in the cooling cycle:

A

to close and the PACK

light to illuminate

84
Q 
On the GROUND, with
both pack switches set
to HIGH and both
RECIRC FANs selected
to AUTO:
A

the left recirculation

fan will shut down

85
Q 
With pack switches set
to AUTO, if one pack
fails, when does the
remaining pack provide
high air flow
A

In Flight (With Flaps UP)

86
Q 
The controller programs
the cabin to land
slightly pressurized.
After landing to
depressurize the
aircraft
A

while taxiing in, the
controller slowly drives
the outflow valve fully
open

87
Q

If all Temperature Zone
Selectors are positioned
OFF:

A

the left pack maintains 75degF,
the right 65degF

LEFT 24DEG RIGHT PACK 18 DEG C

88
Q 
When pressing Master
Caution Recall the
CONT CAB amber ZONE
TEMP light illuminates.
What is correct?
A 
Due to failure of the
primary flight deck
temperature control,
automatic switching to
the backup system has
occurred.
89
Q

What indications can be reset with TRIP RESET (Button)

A

ZONE TEMP (Duct overheat) , PACK, BLEED TRIP OFF

90
Q 
The wing-body
overheat light comes
on. What is the related
master caution
warning?
A

AIR CON

91
Q

ENGINE BLEED AIR VALVE

A

PRessure Regulator & SHUTTOFF VALVE

92
Q

The bleed air pressure
indicator has L and R
pointers. These
pointers:

A

may indicate a L/R
duct pressure difference
which is considered
normal as long as there is sufficient air for cabin pressurisation

93
Q

may indicate a L/R
duct pressure difference
which is considered
normal as long as there

A

the high stage valve
modulates open to
maintain adequate
bleed air pressure

94
Q

From where does the
Cabin Auto Controller
get its inputs?

A

From the ADIRUs.

95
Q

In MANUAL
pressurization mode the
outflow valve is driven
by?

A

a motor supplied from

DC standby bus

96
Q

The cabin begins to

pressurize:

A

ON the ground at high power settings

97
Q

During flight with Hyd SYS B inop (No FLUID in system B)

A

The STBY hid system operates the leading edge slats and leading edge flaps to fully extended position only

98
Q

During BAT START EEC start to operate

A

15% N2

99
Q

What is the position of the isolation Valve when the Isolation is set to AUTO

A

Open when any bleed air switch or air conditioning pack switch is positioned off

Tech Q's (FCOM 2) (3 decks)

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