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145 Cards in this Set
- Front
- Back
- 3rd side (hint)
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What turns on emergency lighting system |
loss of DC power DC bus 4 |
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With a main Cargo fire armed the main deck fire switch does what |
enables maindeck fire suppression by turning off all airflow to the main deck and all airflow and heat into the lower cargo compartments including: turns off two packs remaining pack goes to low flow for upper deck configures equipment cooling to close loop closes master trim air valve |
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What is the wingspan of a B747 400 |
211'5" |
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When are landing lights at the Max intensity |
landing Gear lever down |
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what is the purpose of the flight deck access lights |
To gain access to flight deck powered by ground handling bus |
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After positioning the fuel jettison selector A or B
where does the fuel to remain valve display |
Replaces fuel temp on primary EICAS |
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What is the advantage of selecting LWR on the beacon light switch |
Upper lights wont flash distract during low visibility |
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What is a turning radius with body gear steering armed |
Minimum runway web for 180 turn is 153 feet |
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Where is Emergency equipment located on the BCF |
OK just Ford of the left upper deck door |
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what ND mode will weather radar not be displayed |
Plan
VOR Center
approach center |
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Bleed air is used in what systems |
paws had salt Pressurization Air Conditioning water tank pressurization smoke detection hydraulic reservoir pressure aft cargo heat Demand pumps 1 & 4 PE all Engine start Anti ice Nacelles and Wing Leading edge flaps Thrust reverser's |
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Can apu provide bleed air in flight |
Yes of the 15,000 Feet |
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Turning a bleed air switch off does what |
Closes: engine bleed air valve pressurization regulating valve High pressure valve |
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If switch is off is Nacelle anti ice switch still available |
Yes unless PRV failed closed PRV closed automatically as a result of a bleed air overheat Engine start valve has not closed HP Valve failed open |
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Yes bleed air switch is off is thrust reverser still available |
Yes unless PRV/HP failed closed PRV clothes because of overheats Engine start valve not close |
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What will illuminate a Hydraulic SYS fault light |
bleed air overheats bleed air over pressure HP bleed valve open when command closed PRV open when command closed |
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with the SYS fault light illuminated is reversing available on landing |
yes unless light is on due to an overheat |
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What unit is the bleed air system reduces bleed air temperature |
Fan air precooler |
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With an L duct 0VT what systems are no longer available |
wing anti-ice left Number one hydraulic demand pump (both on Pratts) Pack one hydraulic reservoir pressure systems one and two leading edge flaps will work and slow secondary mode only Turn additional packs off if necessary due to draw on #3 #4 |
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APU bleed air supplied to which duct |
Center section of bleeder duct |
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How can I isolate the number 1DCIR |
de selects the number 4 Bus Tie switch |
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What areas receive anti-ice protection |
Engine nacelles Wings windshield Probe 2, Pitot static 4 , TAT 2 |
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Under what conditions is Nacelle at the ice required on |
When the OAT on the ground or TAT in flight is 10° C or below and visible moisture Clouds fog with visibility less than one statue mile rain snow ice crystals ramp taxi runways with snow iced slush and standing water |
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Are the TAT probes heated and when |
Yes in-flight only |
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What indications do we have that NAC anti ICE is on and wings on |
NAI displayed to the left of the vertical N1 WAI at the bottom of the N1 displays between #1 or #3 |
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What section of the wing is anti iced |
The outer and mid span sections of the leading edge |
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At flaps 5. what portion of the leading edge is being the iced with WAI on |
Leading edge anti-ice is ineffective with flaps extended |
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Which windows are provided anti-ice and anti-fog protection |
all Flight deck windows are electrically heated
The Forward windows have both exterior service and the ice and anterior surface antifog The side windows have interior service antifog only |
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when is anti-fog available to the windows |
Anytime aircraft is powered |
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How do I reset the windshield heat control fault |
Pull circuit breaker wait 10 seconds then back on |
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what is the purpose of the OBS audio system switch on the overhead panel |
If captain or FOs Audio control panel is an app allows there audio to be controlled with the observers ACP |
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I just sat in the LAX the number 4 hydraulic quantity goes to zero what systems will be affected for approach and landing |
inbiard TE flaps right Outboard elevator inboard spoilers number 5,6,7,8 normal brakes including auto breaks Wing gear actuator |
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the number 4 hydraulic quantity goes to zero what systems will be affected for approach and landing |
inbiard TE flaps right Outboard elevator inboard spoilers number 5,6,7,8 normal brakes including auto breaks Wing gear actuator |
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the number four hydraulic quantity goes to zero what systems will be affected for approach and landing |
inbiard TE flaps right Outboard elevator inboard spoilers number 5,6,7,8 normal brakes including auto breaks Wing gear actuator |
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How can you monitor for the inner marker signal during cat 2 approach |
On audio control panel select marker and push -volume knob |
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How can we tune data on C VHF |
Dial above 136 or below 118 on the big knob and select transfer |
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how is the oxygen mask microphone operation verified during preflight |
Select the flights microphone on the audio control panel speaker on select push to test an O2 panel along with Emergency knob simultaneously press the push to talk button glareshield yoke audio control panel
On certain aircraft you must also select oxygen on Audio control panel and turn back to boom afterwards |
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What should be seen when pushing the Cockpit voice recorder test button |
Pulsating indication on meter |
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How many push to talk switches are in the cockpit |
7 to 10 depending on aircraft |
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Selecting the SERV Interphone switch to on does what |
Connects gown crew stations around the aircraft to flight intercom |
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What does IDG stand for |
Integrated Drive generator |
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What turns on and IDG drive light ? |
hi oil temperature Low oil pressure Uncorrectable frequency fault |
Hot lop UFF |
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The Amber line on the N1 indicator represents what |
N1 overboost limits EEC in normal The red line indicates max N1 over speed limit |
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What buses are Powered with one and two external power available but not on |
ground handling bus main deck cargo handling bus |
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what bus normally powers the service bus is there an alternative means to power the bus |
AC bus number 1 is normal source Service bus can be powered by Ground handling bus by pushing the 1L door ground service switch |
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The altitude Range Ark Green Ark Banana displays what information |
shows were MCP altitude will be reached based on current vertical speed and ground speed |
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with the loss of the number three AC bus the AP standby bus is power from which source |
AC number one via Captain transfer bus AP hot bad bus via inverter if both AC three and AC one fail |
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How can I isolate the number 1DCIR |
de selects the number 4 Bus. switch |
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what will power the main deck cargo handling bus with number two external available and number two AP generator available |
Number 2 external power |
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what is the minimum oil quantity for dispatch |
16 quarts |
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If the EGT limit is exceeded what is indicated and on takeoff |
start limit redline EGT vertical indicator max continuous limit Amber line EGT vertical indicator take off limit red line EGT vertical indicator
on take off and go rounds colors changes are inhibited for five minutes after TOGA is pushed |
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The Amber line on the N1 indicator represents watch |
N1 overboost limits EEC in normal The red line indicates max N1 over speed limit |
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What areas receive anti-ice protection |
Engine nacelles Leading edges Wings windshield Probe 2, Pitot static 4 , TAT 2 |
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when will standby ignition turn on if the switch is in normal |
loss of AC power Standby ignition just insures a standby power source to the igniter
does not turn on igniters |
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When will continuous ignition come on automatically |
normal single igniter Nacelle anti ice selected on flaps out of up and to below 50% during ground engine startnormally dual ignighter Engine flameouts in flight start |
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What protection are provided by the EEC |
Overspeed and overboost |
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When is approach idle active |
Nacelle anti ice on flaps in landing position Continuous ignition switch selected on |
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With APU running. turning off the APU selector does what |
Closes APU bleed air isolation valve initiate normal shut down 60 second cool down cycle resets auto shut down fault logic Except when shut down due to APU bleed Duct leak |
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what are the five thrust references selected from the CDU |
Takeoff climb cruise continuous go around |
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How many fire bottles are in the BCF |
11, 2 per wing (4) six cargo on the BCF and 1 APU |
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after a fire test pass what two systems are no longer being monitored by the aircraft |
wheel wells
Leading edge duct |
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With the engine fuel switch running can the fire switch be pulled |
Yes The fire switch is locked with fuel control switch and run but will unlock by
pressing the mechanical release switch
A fire warning signal actual or a test |
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Pulling the number one engine fire switch does What |
closes bleed air valve Arms the squib closest hydraulic shut off valve depressurize is the hydraulic pump closes engines and spar fuel valves Trips generator field |
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With a main Cargo fire armed the main deck fire switch does what |
enables maindeck fire suppression by turning off all airflow to the main deck and all airflow and heat into the lower cargo compartments including: turns off two packs remaining pack goes to low flow for upper deck configures equipment cooling to close loop closes master trim air valve |
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with a lower forward cargo fire pressing the cargo fire discharge switch does what ? how many minutes of protection is provided |
discharges two bottles immediately
remaining 2 to 4 bottles tail dependent begin to meter flow after 30 minutes or upon landing whichever occurs first
Gives 334 minutes of protection 180 minutes on the ERS |
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Are engine fire loops an "and"
or
"or" logic system |
and
but refers to or when configured for single loop operation due to a fault |
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what fire protection do we have in the wheel well |
none |
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How many overheat loops are installed for the APU |
none just fire warning |
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Where is the APU ground control panel located |
Right body gear wheel well |
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The stabilizer is powered from what hydraulic systems |
Two and three |
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What is the auto position of the stab trim auto cut out switch for |
Allows auto cut out if unscheduled stab trim is detected |
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When are the stab trim switches are the control wheel inhibited |
Multiple auto pilot engaged |
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When do outboard ailerons unlock |
flaps out of up or airspeed below 232 knots
Ailerons lock with flaps up and air speed above 238 |
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with the speed break in arm when do the speed brakes deploy on landing
When not armed |
Armed thrust level one and three close maingear touchdown switch
not armed thrust levers one and three closed Maingear touchdown switch Reverse levers two or four pulled to reverse idle
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What flat protection is provided in secondary mode |
TEF asymmetry only Not flap load relief |
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what will occur if the trailing edge flap group is in the secondary mode with hydraulic pressure available |
Leading edge flaps stay in secondary mode until reaching selected position
trailing edge flaps In secondary mode due to loss of hydraulic pressure they will switch back to primary mode as soon as hydraulic pressure is restored but since the question said that they were in secondary mode with hydraulic pressure available it must have been some other fault so trailing edge flaps will be driven electrically instead of hydraulically much slower tell remain in secondary mode until fully retracted |
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In the alternate control mode how is flap extension sequenced |
Extend all flaps simultaneously to a maximum of flaps 25 alternate control mode flap retraction Trailing edge flaps fully up then Leading edge flaps up |
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on landing why does the flat position indicator change from green to magenta |
Juju in board and midspan LEF retracting when reverse thrust is commanded |
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what is the maximum altitude for extension |
Flight level 200 |
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When the pitch limit indicator displayed on the PFD and what is its purpose |
displayed when flaps out of up
Purpose stick shaker activation points |
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What is the input sources for the command speed displays on the PFD |
Speed set on mold control panel when window is open
FMC computer speed when window is blank |
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what identifies the active waypoint on the ND |
magenta star |
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The altitude range arc, green arc, displays what information Banana |
indicates where MCP altitude will be reached based on current vertical speed and ground speed |
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The altitude Range Ark Green Ark Banana displays what information |
Educates were MCP altitude will be reached based on current vertical speed and ground speed |
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What does WXR button do |
Powers the radar transceivers selected on the center consul weather radar control panel displays radar returns and respective ND |
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What does the STA button do |
displays VOR's according to range
Less or equal to 40 nautical miles high and low VORs
Greater than or equal to 80 miles high VOR's only |
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What does the WPT button do |
Displays waypoints when Range selector is 40 nautical miles or less |
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What does the AARPT button do |
in map and map center modes displays airports in range |
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What does ARPT button do |
Displays airports in all ranges |
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What does the data button do |
Displays FMC ETA and any altitude constricts at each waypoint |
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What does the POS button do |
Displays navigational inputs
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What items will activate the takeoff configuration warning |
N1 at 70% in any of the below parking brakes set body gear steering not centered stab trim not in Green band Flaps not in planed to take off position speed break not stowed Wrong runway programmed into FMS |
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What three things will illuminate the hydraulic sys fault light |
Low system pressure low system quantity excessive temperature |
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what ND mode will weather radar not be displayed |
Plan
VOR Center
approach center |
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What indicates a route modification on the ND |
A white dashed line |
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The standby horizon is powered from what source |
Main battery bus |
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What will illuminate a bleed air SYS fault light |
bleed air overheats bleed air over pressure HP bleed valve open when command closed PRV open when command closed |
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what is a max amount of fuel we can carry in pounds with a fuel density of 6.7 pounds per gallon |
359,414 pounds |
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What does a TCAD advisory traffic traffic mean |
A traffic advisory another aircraft is predicted to penetrate a safety bubble around your aircraft within 25 to 45 seconds
A resolution authority means conflict within 20 to 30 seconds with a smaller safety bubble crew action is required |
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What switch turns off TCAS advisory on the ND |
TFC button on the EFIS control panel |
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what is the maximum wind limit for operating the main cabin door |
40 knots operating 65 knots fully open |
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What is the maximum tailwind for a landing |
15 knots |
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What will turn on the number 4 demand pump if the switch is an auto |
Fuel console switch selected off low working pressure
flaps in transit on the ground
flaps out of up in flights |
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What is the maximum cross component for a dry runway
landing |
40 knots 36 knots |
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Max depth of slush for takeoff |
.5 inches |
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What is the max landing weight for an ERF |
653,000 pounds |
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What is the minimum crew oxygen dispatch pressure |
1400 pounds |
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What is the minimum TCH |
40 feet |
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What is the maximum N1 |
117. 5% GE
111.4% P&W
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Max engine start EGT |
750°C GE
535°C P&W |
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What is the difference between total fuel and calculator fuel |
Total fuel is what the fuel quantity system is reading in the tanks
Calculated fuel is calculation of the fuel that should remain based on how much the engines have used |
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What is the max fuel in balance between tank 1&4 and 2&3 |
3000. 1-4 6000. 2-3 |
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Does the flow bar disappear in the number two and three cross feed valve switches when the flaps are selected to the take off position |
No the flow bar in the inboard cost me switch just mean that the valves control by system logic not necessarily that it is open |
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After positioning the fuel jettison selector A or B
where does the fuel to remain valve display |
Replaces fuel temp on primary EICAS |
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What's activated how long will the scavenge pumps operate |
120 minutes or until low pressure is sensed by the pump |
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What three things will illuminate the sys fault light |
Low system pressure low system quantity excessive temperature |
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What will turn on the number 4 demand pump if the switch is an auto |
Fuel console switch selected off low EDP pressure
flaps in transit on the ground
flaps out of up in flights |
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I just sat in the LAX the number for hydraulic quantity goes to zero what systems will be affected for approach and landing |
inbiard TE flaps right Outboard elevator inboard spoilers number 5,6,7,8 normal brakes including auto breaks Wing gear actuator |
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With the loss of systems two and three why is there a speed additive for the approach |
Loss of Stab trim the elevator feel is an a degraded mode with inputs only from mechanical Springs |
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With the loss of number one hydraulic what system will be effective for approach landing |
Inboard TE flaps left Outboard elevator alternate break source one of two nose body gear actuating nose body gear steering center auto pilot |
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on landing the brakes source light illuminates |
Loss of normal and alternate brakes systems 4 , 1. and 2 |
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How are the demand pumps powered |
GE one and four pneumatic , two and three electrical
P&W all are pneumatic |
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The auxiliary hydraulic pumps are powered from what source |
Ground handling bus |
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with The number 4 Auxiliary bus on and providing pressure will the hydraulic sys fault light be on or off |
Off |
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What is the minimum hydraulic quantity for dispatch where do you read that value |
.080 on the STAT page of the lower EICAS |
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How many tires we have a water the numerical order |
18 count clock wise Zs |
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Selecting value three on the auto brake selector does what ? from which source does Autobrake system receive to acceleration inputs |
Maintains a fixed deceleration rate so it will ease off the brakes when other deceleration factors such as speed breaks or thrust reversers kick in
The IRS specifically the captains selected IRU |
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What does the EICAS message gear tilt mean |
Main gear trucks not in full tilt position after takeoff |
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How do we alternately extend the gear where are the switch is located |
Two alternate Nose/ Body and Wing gear switches pushed on Lower Landing gear panel to the right of the gear lever |
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you have a real well fire what speed should you be at before extending the gear |
270 knots or 0. 82 mach |
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On take off roll when does RTO arm. what kind of breaking is provided |
85 knots
Max breaking |
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What does a white hash box displayed on the expanded gear position indicate |
Gear in transit |
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How long does the gear up indication remain on the EICAS |
10 seconds |
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At what speed does the body gear steering disarm |
greater than 20 knots on takeoff roll arms less than 15 knots on landing roll or rejected landing |
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What does the brake torque limiting system do |
prevents excessive torque to prevent landing gear damage |
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What are the three levels of EICAS alerting |
Warning caution and advisory three types of messages alert memo Status |
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Can a warning EICAS message be canceled |
No neither can a memo |
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When are the fire bell and master warning lights Inhibited |
From V1 until 400 feet AFE or 25 seconds after V1 |
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What items will activate the takeoff configuration warning |
N1 at 70% in any of the below parking brakes set body gear steering not centered stab trim not in Green band Flaps not in planed to take off position speed break not stowed Wrong runway programmed into FMS |
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When is the predicted wind sheer activated |
Vr through 1500 feet AGL |
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In what phase of flight will you get a GPWS don't sink warning |
Altitude loss of flaps and or gear up after take off or go around |
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What is the purpose of the event record switch how many events can be recorded |
Records currently displayed Engine parameters and additional maintenance info of the five events may be recorded a sixth record will record over the first the system also automatically records out of limit parameters |
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What is a status message |
And the kids equipment thoughts requiring MEL reference prior to dispatch |
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And NAV mode the IRS provides what information |
Hat swap
heading altitude track speeds winds acceleration position |
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What does the depressurization discharge switch do for the main cabin deck |
Initiates a controlled cabin depressation |
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