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240 Cards in this Set
- Front
- Back
|
What type of cargo may be carried in the AFT cargo compartment that may NOT be carried
in the FWD cargo compartment? |
Live cargo
Ref: CR7/9 OM 11-7.4, FOM 7-1.9 |
|
|
What is the radar hazard area?
|
2 feet
Ref: CR7/9 OM 11-1.9 |
|
|
What is the minimum pavement for a 180 degree turn for the CR7/CR9?
|
CR7: 75 feet
CR9: 80 feet &1 inch Ref: CR7/9 OM 11-1.6 & 1.7 |
|
|
How many PBEs are required for dispatch?
|
4, one for each Fire Extinguisher.
Ref: CR7/9 OM 7.2.6 & 7-2.7 |
|
|
What test requires coordination between the Flight Attendant and Cockpit Crew during the
interior inspection? |
The testing of the lavatory smoke detectors requires verification by a cockpit crewmember that the
“SMOKE FWD/AFT LAV” EICAS message is displayed. Ref: CR7/9 OM 2-3.1 |
|
|
What precaution must be taken before turning the NWS switch ON during the After Start
Checklist? |
Be sure that the tow bar and/or chocks have been removed and ground crew clear.
Ref: CR7/9 OM 2-6.1 |
|
|
If one of the STALL PTCT PUSHER switches is selected OFF will the stall pusher be
operational? |
No.
Ref: CR7/9 OM 11-9.9 |
|
|
How can the stick pusher be stopped?
|
By pressing and holding the AP/SP DISC switch on the pilot or copilot control wheel, or by
selecting either of the STALL PTCT PUSHER switches OFF. Ref: CR7/9 OM 11-9.9 |
|
|
May you depart with one of the STALL PTCT PUSHER switches off?
|
No
Ref: CR7/9 OM 1-7.3 |
|
|
Can cross side NAV data be displayed on the PFD and MFD?
|
Yes, by rotating the NAV SOURCE knob on the DCP.
Ref: CR7/9 OM 11-10.4, .5, .6 |
|
|
How is TCAS information displayed on the MFD?
|
The TFC button on the DCP is used to select the TCAS page. As long as the FMS MAP range is
currently selected to a range of 40NM or less, the TCAS information will be overlaid on the FMS MAP page, and larger ranges can be subsequently selected. If the current FMS MAP range is greater than 40nm, the TCAS MFD page will be presented. Ref: CR7/9 OM 11-17.7 |
|
|
How is EGPWS terrain information displayed on the MFD?
|
Automatically if encountered, or overlaid if selected.
Ref: CR7/9 OM 11-17.3 |
|
|
How is the EGPWS display removed from the MFD?
|
Pushing the TERR/WX pushbutton on the DCP, or inhibit the EGPWS by selecting the TERRAIN
OFF switchlight on the GND PROX Panel. Ref: CR7/9 OM 11-17.5 |
|
|
When the RA TEST button is pressed what should the radar altitude read?
|
50 feet.
Ref: CR7/9 OM 2-3.2 |
|
|
What is the function of the EICAS position on the Display Reversionary Panel?
|
To display ED2 information on the MFD.
Ref: CR7/9 OM 11-10.6 |
|
|
What does the response “TESTED” in reference to SIDE PANEL... on the Originating Check
indicate? |
The Display Reversionary Panel has been selected to PFD and EICAS to check for proper display,
and then returned to NORM, the RA test push button on the Air Data Reference Panel has been pressed to check that 50 feet is displayed on the PFD, and the center of the Baro knob has been pressed to ensure 29.92 is set on the altimeter, stall protection switch, clock, and wiper switch, etc. Ref: CR7/9 OM 2-3.1 & 3.2 |
|
|
To what figure should the MDA be set with a DA of 512 feet on a CAT I precision approach?
|
520 feet. MDAs are in 10-foot increments for precision approaches.
Ref: CR7/9 OM 1-7.5 |
|
|
What are the primary sources of AC power?
|
Two engine and one APU driven generators
Ref: CR7/9 OM 11-6.1 |
|
|
What is the normal source of DC power?
|
Four Transformer Rectifier Units (TRUs) rated at 120 amps each.
Ref: CR7/9 OM 11-6.1 & 6.6 |
|
|
How many batteries are installed and where are they located?
|
Two nicad batteries, one located in the aft equipment bay (APU), and the other located in the nose
compartment with the TRUs (Main). Ref: CR7/9 OM 11-6.1 & 6.8 |
|
|
What are the individual components that make up an IDG (integrated drive generator)?
|
A constant speed drive and an electrical generator.
Ref: CR7/9 OM 11-6.2 |
|
|
When will a generator automatically shut down?
|
If an over temperature or over torque condition occurs.
Ref: CR7/9 OM 11-6.2 |
|
|
Under what conditions will a GCU remove it’s associated generator from the bus system?
|
Over or under voltage, over or under frequency, generator or bus overcurrent, or generator phase
out of sequence. Ref: CR7/9 OM 11-6.3 |
|
|
How can an IDG be manually disconnected from its engine?
|
By pressing the IDG DISC switch on the Electrical Services Panel.
Ref: CR7/9 OM 11-6.2 |
|
|
Once disconnected, can the IDG be reconnected in flight?
|
No.
Ref: CR7/9 OM 11-6.2 |
|
|
What does a green AVAIL light illuminated on the AC External switchlight indicate?
|
Power is connected and is of correct phase, voltage, and frequency.
Ref: CR7/9 OM 11-6.3 |
|
|
What is the function of the AC ESS XFER switchlight?
|
To manually transfer or to indicate the AC ESS BUS is looking for power from an alternate source.
Ref: CR7/9 OM 11-6.4 |
|
|
When will power to the AC Essential Bus automatically switch from AC Bus 1 to AC Bus 2?
|
When AC Bus 1 is not powered.
Ref: CR7/9 OM 11-6.4 |
|
|
What does the FAIL light illuminated in an AUTO XFER switchlight along with the amber
EICAS message AUTO XFER FAIL indicate? |
A bus fault or generator overcurrent condition.
Ref: CR7/9 OM 11-6.8 |
|
|
What is power source priority for AC Bus 1, AC Bus 2?
|
AC Bus 1 - GEN 1, APU, GEN 2, External Power.
AC Bus 2 - GEN 2, APU, GEN 1, External Power. Ref: CR7/9 OM 11-6.4 |
|
|
How can AUTO XFER be manually inhibited?
|
By pushing the AUTO XFER switchlight on the electrical services panel.
Ref: CR7 OM 11-6.8 |
|
|
What controls the operation of the DC TIE CONTACTORS?
|
Automatically controlled by the two DCPCs (DC power centers).
Ref: CR7/9 OM 11-6.8 |
|
|
What is the ExpressJet policy on crewmembers resetting cockpit electrical Circuit Breakers
in flight? |
A circuit breaker must not be reset or cycled (i.e., opened or closed) unless doing so is consistent
with explicit procedures specified in the OM/QRH or unless, in the judgment of the PIC that resetting or cycling of the circuit breaker is necessary for the safe completion of the flight. Ref: CR7/9 OM 1-7.3 |
|
|
If AC external power is to be utilized, explain how AC power is properly established?
|
If the green AVAIL light is illuminated, press the external AC switchlight to supply the electrical
system. Ref: CR7/9 OM 11-6.3 |
|
|
What areas are protected by the fire and/or overheat protection system?
|
Engines, APU, main landing gear bay and bleed ducts
Ref: CR7/9 OM 11-8.1 |
|
|
What are the benefits of the dual detection loop system?
|
Redundancy and Dispatchability
Ref: CR7/9 OM 11-8.1 |
|
|
How many Firex bottles are provided for engine fire extinguishing?
|
2 Halon bottles.
Ref: CR7/9 OM 11-8.1 |
|
|
How many Firex bottles are provided for APU fire extinguishing?
|
1 Halon bottle.
Ref: CR7/9 OM 11-8.1 |
|
|
When will APU fire extinguishing activate automatically?
|
On the ground in the event of an APU fire.
Ref: CR7/9 OM 11-8.1 |
|
|
After pressing the FIRE DETECTION/FIREX MONITOR test switch what is the indication of a
successful test? |
A “FIRE SYS OK” advisory msg is displayed.
Ref: CR7/9 OM 11-8.3 |
|
|
What are the aural and visual indications of a successful APU Fire Warning test prior to
APU start? |
A “FIRE SYS OK” advisory msg is displayed.
Ref: CR7/9 OM 2-3.3 & 11-8.3 |
|
|
What are the aural and visual indications of a successful Fire protection test during the
Originating Check? |
A “FIRE SYS OK” advisory msg is displayed.
Ref: CR7/9 OM 2-3.3 |
|
|
How many smoke detectors are in the cargo compartment?
|
3 in the forward cargo compartment and 2 in the aft cargo compartment
Ref: CR7/9 OM 11-8.2 |
|
|
Which areas are protected by the dual loop system?
|
Engines, APU, and Bleed Ducts
Ref: CR7/9 OM 11-8.1 |
|
|
What powers the fuel system ejector pumps (transfer, scavenge, main)?
|
Motive Flow
Ref: CR7/9 OM 11-11.2 |
|
|
What does selecting either of the fuel boost pump switch lights on cause?
|
Arms both boost pumps, and if a low fuel feed pressure is detected, both pumps turn on
Ref: CR7/9 OM 11-11.6 |
|
|
How can fuel be manually transferred from the left wing tank to the right wing tank?
|
Normal crossflow is automatic, but manual crossflow is accomplished by selecting the XFLOW
AUTO OVERRIDE to MAN, then selecting the wing you wish to send fuel to (R XFLOW). Fuel can also be balanced in flight using the GRAVITY XFLOW valve. Ref: CR7/9 OM 11-11.4 |
|
|
When is automatic fuel transfer initiated (wing tank to wing tank)?
|
When a 200-lb. imbalance exists.
Ref: CR7/9 OM 11-11.4 |
|
|
How is fuel heated?
|
Engine oil to fuel heat exchangers.
Ref: CR7/9 OM 11-11.3 |
|
|
In flight, if low pressure is detected in the left engine feed line, which boost pump ON light
will illuminate? |
Both boost pump lights will illuminate if they are both selected ON
Ref: CR7/9 OM 11-11.6 |
|
|
On the ground, if low pressure is detected in the left engine feed line, which boost pump
ON light will illuminate? |
Both, if both are selected ON.
Ref: CR7/9 OM 11-11.6 |
|
|
How is fuel transferred from the center tank to the wing tanks?
|
Through motive flow (transfer ejectors).
Ref: CR7/9 OM 11-11.2 & 11.3 |
|
|
Why are both fuel boost pumps selected off for single engine taxi?
|
To prevent a fuel imbalance
Ref: CR7/9 OM 1-4.13 |
|
|
An Amber FUEL IMBALANCE caution message is displayed when?
|
When the fuel imbalance exceeds 800 lbs.
Ref: CR7/9 OM 11-11.7 |
|
|
Where is engine fuel feed temperature displayed?
|
On the FUEL synoptic page.
Ref: CR7/9 OM 11-11.1 |
|
|
Where is bulk fuel temperature displayed?
|
On the FUEL synoptic page.
Ref: CR7/9 OM 11-11.1 |
|
|
Are the fuel check valves that are checked during the first flight of the day checks depicted
on the FUEL synoptic page? |
No.
Ref: CR7/9 OM 11-11.1 |
|
|
How does fuel get to the APU?
|
The APU fuel pump feeds fuel from the left wing tank.
Ref: CR7/9 OM 11-11.1 |
|
|
The pneumatic system can receive pressurized air from what sources?
|
The 6th or 10th stage bleed air, APU, and external ground air.
Ref: CR7/9 OM 11-19.1 |
|
|
How is the distribution of bleed air managed?
|
Automatically controlled by the two ACSCs when in auto, and can be manually controlled using the
BLEED AIR control panel. Ref: CR7/9 OM 11-19.1 |
|
|
What determines whether 6th or 10th stage bleed air is used?
|
The ACSC automatically determines which bleed air source is to be used based on system
demand. Ref: CR7/9 OM 11-19.2 |
|
|
When are the bleed valves selected to manual?
|
When the QRH or OM calls for it.
Ref: CR7/9 OM 11-19.2 |
|
|
Can the APU supply the bleed air to the anti ice system?
|
No.
Ref: CR7/9 OM 11-19 |
|
|
With the bleed valves selected closed can external air be used?
|
Yes.
Ref: CR7/9 OM 11-19.2 |
|
|
With the bleed valves selected to AUTO, will selecting the bleed source to R ENG change
the bleed source? |
No, the bleed source rotary switch is only operable when the bleed valves switch is selected to
MANUAL. Ref: CR7/9 OM 11-19.3 |
|
|
What actions are initiated on the pneumatic system by selecting the START pushbutton?
|
The isolation valve OPENS, the pack valves CLOSE, the associated start valve OPENS, and the
engine air turbine starter (ATS) is engaged. Ref: CR7/9 OM 11-19.2 |
|
|
With the APU operating what parameters must be met for the automatic switching from
APU bleed air to engine bleed air after takeoff? |
Gear up, flaps 20° or less and the thrust levers reduced from the TOGA detent.
Ref: CR7/9 OM 11-19.3 |
|
|
On approach, with the APU operating what other parameters must be met for automatic
switching of the bleed air from the engines back to the APU? |
Flaps>20° or gear down.
Ref: CR7/9 OM 11-19.3 |
|
|
With the BLEED VALVES selected to MANUAL, can the APU supply the anti ice system?
|
No, in MANUAL mode with the APU as the bleed source, selection of wing or cowl anti ice will
cause the APU LCV to close, but will not open the engine bleed valves. Ref: CR7/9 OM 11-19.3 |
|
|
What is the primary function of the APU?
|
To provide AC electrical power
Ref: CR7/9 OM 11-3.1 |
|
|
What is the secondary function of the APU?
|
To supply pneumatic power to the engine air turbine starters (ATS) and for air conditioning packs.
Ref: CR7/9 OM 11-3.1 |
|
|
What DC voltage is required to start the APU from battery power?
|
22 Volts from main and APU batteries
Ref: CR7/9 OM 2-2.3 CR7/9 OM 11-3.2 |
|
|
How is the APU fuel feed SOV opened?
|
It opens when the APU PWR FUEL switchlight is pressed in (on).
Ref: CR7/9 OM 11-3.2 |
|
|
Under what conditions will the APU SOV close automatically?
|
If a fire is detected, the ECU will close the SOV
Ref: CR7/9 OM 11-3.1 |
|
|
What does the amber PUMP FAIL light illuminating in the APU PWR FUEL switchlight
indicate? |
APU pump has failed.
Ref: CR7/9 OM 11-3.5 |
|
|
What does the amber SOV FAIL light illuminating in the APU PWR FUEL switchlight
indicate? |
Indicates failed APU fuel feed SOV.
Ref: CR7/9 OM 11-3.5 |
|
|
What does the white START light illuminating in the APU PWR FUEL switchlight indicate?
|
APU starter motor is engaged.
Ref: CR7/9 OM 11-3.5 |
|
|
What does the green AVAIL light illuminating in the APU PWR FUEL switchlight indicate?
|
APU is available for electrical loading.
Ref: CR7/9 OM 11-3.5 |
|
|
What indications are you looking for when the START/STOP switch is pressed for APU
start? |
Amber START light in switch illuminates, APU START status message appears, and prior to 60%
RPM, START light and status message go out. Ref: CR7/9 OM 11-3.2 |
|
|
What 4 indications are you looking for when the APU PWR FUEL switch is pushed?
|
APU IN BITE status message, APU SOV OPEN status message, APU gauges appear and APU
door opens. Ref: CR7/9 OM 11-3.2 |
|
|
During APU start at what RPM should the white Status APU START and the START light in
the START/STOP switch/light go out? |
Before 60%.
Ref: CR7/9 OM 11-3.2 |
|
|
Can the APU supply bleed air to the packs during the climb phase of flight?
|
Only with the BLEED SOURCE switch selected to APU and the BLEED VALVE selector switched
to MANUAL, up to 25,000 feet. Ref: CR7/9 OM 1-4.16 & 4.17, CR7/9 OM 11-19.2 & .3 |
|
|
What are the APU starter limits?
|
Three starts in one hour with 2 minutes between starts.
Ref: CR7/9 OM 1-4.15 |
|
|
What is the maximum altitude for the APU to be used for engine starting?
|
21,000 feet Note: This is good to know but is not a memory item. It is a system limitation that
appears in QRH checklist. There is no procedure to start an engine in flight from memory. Ref: CR7/9 OM 1-4.17 CR7 & CR9 QRH Vol 2, ABNORM 1-4 |
|
|
What type of fire protection does the APU have?
|
Dual loop detection with one bottle for extinguishing.
Ref: CR7/9 OM 11-8.1 |
|
|
What is initiated by pressing the START switchlight on the START/IGNITION panel?
|
The isolation valve opens, FADEC opens the starter valve on the associated engine to allow
pressure from the bleed air manifold to engage the air turbine starter, white light illuminates in the associated START switchlight, L or R ENGINE START status message is posted. Ref: CR7/9 OM 11-20.14 |
|
|
What is initiated by advancing the associated power lever during the start sequence?
|
The FADEC turns on the ignition, introduces fuel, monitors for engine lightoff, and controls engine
acceleration. Ref: CR7/9 OM 11-20.14 |
|
|
Is AC electrical power required for engine starting?
|
No.
Ref: CR7/9 OM 11-20.14 |
|
|
When starting with DC power only, which engine is started first?
|
The right engine should be started first.
Ref: CR7 & CR9 QRH Vol 1, SUPP-4 |
|
|
Above what RPM may the starter not be engaged?
|
45% N2
Ref: CR7/9 OM 1-4.7 |
|
|
For what conditions will the FADEC auto abort during start?
|
On the ground, FADEC will abort an engine start for a HOT or HUNG start.
Ref: CR7/9 OM 11-20.15 |
|
|
Under what conditions will both ignition systems be activated?
|
Activated by FADEC when the Stall Warning Computer senses the trip points have been
exceeded, when starting an engine in flight, when continuous ignition is selected and during flameout. Ref: CR7/9 OM 11-20.15 & 20.16 |
|
|
How are the primary flight controls actuated?
|
Hydraulic power.
Ref: CR7/9 OM 11-12.1 |
|
|
The rudder system is powered by which hydraulic system?
|
All three systems.
Ref: CR7/9 OM 11-12.1 & 12.3 |
|
|
How many hydraulic systems are on the CR7/CR9?
|
3
Ref: CR7/9 OM 11-12.1 |
|
|
Which of the hydraulic systems have engine driven pumps as well as electric pumps?
|
Systems 1 and 2
Ref: CR7/9 OM 11-12.1 |
|
|
What does the AUTO position on the HYD 1, 2 and 3B do?
|
Causes the B pumps to operate when their respective bus is powered and the flaps are not at 0°
Ref: CR7/9 OM 11-12.2 |
|
|
Do the B pumps activate automatically after an engine failure?
|
No
Ref: CR7/9 OM 11-12.2 |
|
|
How many hydraulic pumps are lost following and engine failure?
|
Only the engine driven pump
Ref: CR7/9 OM 11-12.2 |
|
|
Which ACMP runs continuously during normal operations?
|
3A
Ref: CR7/9 OM 11-12.3 |
|
|
How is hydraulic system fluid cooled?
|
Systems 1 & 2 are cooled by a ram-air/oil heat exchanger and system 3 hydraulic pumps are
located in the wheel well area and do not require dedicated cooling. Ref: CR7/9 OM 11-12.2 & 12.3 |
|
|
With all AC busses powered and pumps 1B and 2B selected to the AUTO position, when
will the pumps operate? |
When the flaps are out of the 0 position.
Ref: CR7/9 OM 11-12.2 |
|
|
Which hydraulic pump automatically operates from the ADG Bus during ADG deployment?
|
Pump 3B.
Ref: CR7/9 OM 11-12.3 |
|
|
How does the crew know there is adequate hydraulic fluid quantity?
|
By checking the HYD synoptic page and verifying fluid quantities are green.
Ref: CR7/9 OM 11-12 |
|
|
What are the Normal Hydraulic quantities?
|
Green quantity indications.
Ref: CR7/9 OM 11-12, CR7/9 OM 2-3.4 |
|
|
If the left engine fails or is shutdown, which hydraulic pump(s) will be unavailable?
|
The left engine EDP.
Ref: CR7/9 OM 11-12 |
|
|
What is the purpose of the HYD SOV switchlights on the overhead panel?
|
To close the respective hydraulic SOV without the need to shutdown the engine.
Ref: CR7/9 OM 11-12.4 |
|
|
What does the EICAS caution message “ELT ON” mean?
|
ELT is transmitting
Ref: CR7/9 OM 11-4.4 |
|
|
What is the correct position for the ELT switch?
|
Arm/Reset
Ref: CR7/9 OM 11-4.4 |
|
|
When will passenger oxygen automatically deploy?
|
Cabin altitude >14,000 feet
Ref: CR7/9 OM 7-2.15 |
|
|
What is the function of the N/100% selector on the crew O2 mask?
|
To select either a mixture of ambient air with oxygen or 100% oxygen.
Ref: CR7 OM 7-2.17 |
|
|
How is oxygen supplied to the passengers?
|
Chemical oxygen generators mounted in overhead compartments.
Ref: CR7/9 OM 7-2.15 |
|
|
At what cabin altitude does the amber CABIN ALT caution activate?
|
Greater than 8,500 feet, but less than 10,000 feet.
Ref: CR7/9 OM 11-7.5 |
|
|
At what cabin altitude does the red CABIN ALT warning activate?
|
Greater than 10,000 feet.
Ref: CR7/9 OM 11-7.5 |
|
|
How is cabin pressurization maintained?
|
Cabin pressurization is maintained by regulating the amount of air leaked overboard through an
outflow valve. Ref: CR7/9 OM 11-7.4 |
|
|
What does the LDG ELEV knob on the pressurization control panel do?
|
Sets the landing elevation on the status page
Ref: CR7/9 OM 11-7.4 |
|
|
What happens when EMER DEPR switchlight is pressed in (on)?
|
Pressing the EMER DEPR switchlight causes the Cabin Pressure Controller to drive the outflow
valves fully open, climbing the cabin to 14,500+/- 500 feet or ambient if lower. Ref: CR7/9 OM 11-7.4 |
|
|
What does pressing the PRESS CONTROL switchlight twice do?
|
Switches Pressure Controllers.
Ref: CR7/9 OM 11-7.5 |
|
|
Flying at FL 200, the EMER DEPRESS switch/light is pressed, what pressure altitude should
the cabin reach? |
14,500 +/- 500 feet.
Ref: CR7/9 OM 11-7.5 |
|
|
Where is the unpressurized takeoff procedure found?
|
CR7 & CR9 QRH VOL 1
Ref: CR7 & CR9 QRH VOL 1, SUPP-6 |
|
|
Where is the unpressurized landing procedure found?
|
CR7 & CR9 QRH VOL 1
Ref: CR7 & CR9 QRH SUPP-6 |
|
|
When might you be required to perform an unpressurized takeoff?
|
APU deferred and anytime directed by the takeoff data
Ref: CR7/9 OM 6-1.1 & 1.2 CR7/9 OM 3-3.1 & 3-4.3 |
|
|
What is the maximum cabin pressure differential for opening the cabin door at the gate?
|
The cabin must be completely depressurized prior to opening any of the airplane doors.
Ref: CR7/9 OM 1-7.1 |
|
|
How many motors are available to activate the outflow valve?
|
Three DC motors.
Ref: CR7/9 OM 11-7.4 |
|
|
During a cargo overheat condition, what does the AIR position of the CARGO switch
provide? |
Selecting AIR removes power from the over-temp circuit and removes the EICAS message.
Ref: CR7/9 OM 11-7.4 |
|
|
What does the COND AIR position of the CARGO switch provide?
|
Recirculated cabin exhaust air mixed with fresh air warmed by a thermal heater to the cargo bay
area. Ref: CR7/9 OM 11-7.4 |
|
|
When is COND AIR required to be used in the CARGO compartment?
|
When live cargo is carried.
Ref: CR7/9 OM 11-7.4 |
|
|
May live cargo be carried in the FWD cargo compartment?
|
No, only the aft cargo compartment is ventilated.
Ref: CR7/9 OM 11-7.4 FOM 7-1.19 |
|
|
Why does the “CARGO OVERHEAT” abnormal procedure have you select the AIR position?
|
Overheat protection is only provided in COND AIR, power for the over-temperature circuit is
removed when in AIR. Ref: CR7/9 OM 11-7.4 |
|
|
When would the Ram Air switch be used?
|
During unpressurized flight, or when QRH directed.
Ref: CR7/9 OM 11-7.1 |
|
|
What happens to the pack during a “PACK TEMP” condition?
|
The affected pack turns off.
Ref: CR7/9 OM 11-7.2 |
|
|
How are the pack heat exchangers cooled?
|
By air from the ram air scoop.
Ref: CR7/9 OM 11-7.1 |
|
|
How does the Anti Ice Leak detection Controller (AILC) maintain wing anti icing with the
slats extended? |
Two separate temperatures are used. With slats extended, wing anti-ice valves are modulated to
maintain a higher temperature. Ref: CR7/9 OM 11-13.1 |
|
|
Does the power have to be maintained above the white arcs on the N2 gauge when using
wing anti ice? |
No, the white arc is generated by the anti ice switch position and is a reminder that for OPTIMUM
anti icing the N2 core speed should be kept at a higher rpm. Ref: CR7/9 OM 11-13.4 |
|
|
How can the left engine provide bleed air to the right wing?
|
By using the WING A/I CROSS BLEED switch on the bleed air panel.
Ref: CR7/9 OM 11-13.1 |
|
|
What does the WING OVHT EICAS message mean?
|
Indicates an overheat condition in either the left or right wing anti-ice duct.
Ref: CR7/9 OM 11-13.2 |
|
|
Wing anti ice valves fail to the closed position, what position do the cowl valves fail?
|
Open. The cowl anti ice valves require air pressure and electrical power to close.
Ref: CR7/9 OM 11-13.3 |
|
|
Is there bleed leak detection in the aft equipment bay?
|
Yes, the two channel Anti Ice Leak detection Controller monitors the dual loop system in the
equipment bay. Ref: CR7/9 OM 11-13.1 |
|
|
With a probe heater switch in the OFF position, will the probe be heated in flight?
|
Yes, the Air Data Sensor Heater Controllers (ADSHCs) heat all probes in flight regardless of switch
position. Ref: CR7/9 OM 11-13.3 |
|
|
What besides the beacon is turned on with the Beacon switch while on the ground?
|
The FDR.
Ref: CR7/9 OM 11-16.1 |
|
|
Where are the Recog/Taxi lights located?
|
In the wing roots.
Ref: CR7/9 OM 11-16.2 |
|
|
Which external lights must be on for all night taxi operations?
|
NAV, BEACON, RECOG/TAXI and WING INSP lights.
Ref: CR7/9 OM 3-4.3 |
|
|
Why is the Cockpit Dome light turned off on the Shut Down Check?
|
It is possible to leave the dome light on and discharge the battery.
Ref: CR7/9 OM 11-6.2 |
|
|
What does the AUTO position of the PASS SIGNS switches provide?
|
If cabin altitude exceeds 10,000 feet, the NO SMOKING and SEAT BELTS signs illuminate. If the
landing gear is extended, or if the flaps are greater than 0°, the SEAT BELTS sign illuminates. Ref: CR7/9 OM 11-16.4 |
|
|
What is the position of the Emergency Lights switch in normal operation?
|
ARM
Ref: CR7/9 OM 2-4.4 |
|
|
With the Emergency Lights switch in the ARM position, when would the Emergency lights
activate? |
Loss of power to the DC or AC Essential Buses.
Ref: CR7/9 OM 11-16.5 |
|
|
How long will the emergency lights provide illumination?
|
Approximately 15 minutes of lighting
Ref: CR7/9 OM 11-16.5 |
|
|
How are the floor track lights powered?
|
Photo luminescent strips absorb light energy and will glow in the dark.
Ref: CR7/9 OM 7-2.19 |
|
|
What functions do the LH/RH ENG FIRE PUSH switchlights perform when pressed in?
|
Arms squibs on both engine bottles, fuel, hydraulic, and bleed-air SOVs closed on affected engine,
affected engine-driven generator shuts down. Ref: CR7/9 OM 11-8.3 |
|
|
Pushing the APU Fire PUSH switch, on the glareshield, performs what functions?
|
·Bottle squib is armed, green bottle light illuminates
·APU Fuel shutoff valve closes ·APU fire relay is energized to shutdown APU by closing a fuel solenoid valve ·APU LCV closes ·APU generator is tripped Ref: CR7/9 OM 11-8.4 |
|
|
What warnings are provided to warn the pilot of approaching stall?
|
Aural, visual, and tactile (stick shaker). If no corrective action is taken, the stick pusher is
activated. Ref: CR7/9 OM 11-9.8 |
|
|
How is the stall warning system tested?
|
Captain & First Officer STALL PTCT switches - ON. STALL switchlight - Press momentarily:
CONT IGNITION status message illuminated. Stick Shakers - ON. Stick Pusher - ON. STALL switchlights (2) - Illuminated. STALL switchlights (2) - Extinguish. Stick Shakers/Pushers - OFF. CONT IGNITION message - Extinguish. Ref: CR7/9 OM 2-3.5 |
|
|
What aural messages should be heard during the EGPWS test?
|
“GLIDE SLOPE...PULL UP...TERRAIN…WINDSHEAR”.
Ref: CR7/9 OM 2-3.5 |
|
|
How is a Windshear Alert provided to the flight crew?
|
By amber Windshear caption on the PFD and the AMI indicators.
Ref: CR7/9 OM 5-1.6 |
|
|
How is a Windshear Warning provided to the flight crew?
|
By a red Windshear caption on the PFD, AMI indicators, flight director guidance, and an audio
warning “WINDSHEAR”. Ref: CR7/9 OM 5-1.6 |
|
|
Is Windshear escape guidance provided?
|
Windshear escape guidance is provided for decreasing performance shears only.
Ref: CR7/9 OM 5-1.6 |
|
|
Is the proper Pilot reaction to Windshear alerts to follow the Flight Director Command Bars
or to follow the AMI indicators? |
Follow the flight director command bars but, the flight director command bars will provide you
windshear escape guidance only for decreasing performance shears. Ref: CR7/9 OM 5-1.6 |
|
|
What is the purpose of the ROLL SEL switchlight on the glareshield panel?
|
The amber ROLL SEL portion illuminates after the ROLL DISC handle has been pulled, giving
cross side spoileron control. The pilot with the operating aileron then presses the ROLL SEL switchlight to signal the SSCU to give control of both spoilerons to his control column. The PLT/CPLT part of the switchlight illuminates to indicate which pilot has selected control. Ref: CR7/9 OM 11-9.2 |
|
|
During a jammed aileron condition what does the amber ROLL SEL light in the ROLL SEL
switch come on to indicate? |
The roll disconnect handle has been pulled and that the ROLL SEL switch on the unjammed side
must be pressed to transfer the spoileron control to the operable side. Ref: CR7/9 OM 11-9.2 |
|
|
Does the ROLL SEL switch have to be selected for the operable aileron circuit after an
aileron PCU runaway? |
No. PLT ROLL or CPLT ROLL has been automatically selected for spoileron control.
Ref: CR7/9 OM 11-9.2 |
|
|
What guidance does the Flight Director provide in Takeoff mode?
|
Optimized pitch attitude referenced to V speeds (V2 and VR ratio) and flap setting. Lateral
Guidance -Weight off wheels heading hold with 5 Angle of Bank authority. Ref: CR7/9 OM 11-2.2 |
|
|
When is SPEED mode selected on takeoff?
|
When the aircraft accelerates to V2+15 KIAS.
Ref: CR7/9 OM 3-5.1 |
|
|
When should APPR mode be selected when being vectored for an ILS approach?
|
When cleared for the instrument approach.
Ref: CR7/9 OM 3-7.3 CR7/9 OM 10-5.4 |
|
|
How can you center the Heading Bug on the FCP?
|
Pushing the center of the heading knob aligns the heading bug to the current aircraft heading.
Ref: CR7/9 OM 11-2.3 |
|
|
Pushing the button on the FCP SPD knob performs what function?
|
Changes the FCC speed reference from IAS to MACH commands.
Ref: CR7/9 OM 11-2.3 |
|
|
Pushing the button in the FCP CRS knob performs what function?
|
Centers the HSI needle TO the tuned VOR station.
Ref: CR7/9 OM 11-2.3 |
|
|
What is the function of the B/C button on the FCP?
|
Arms the Back course Mode to track the received LOC course reciprocal.
Ref: CR7/9 OM 11-2.3 |
|
|
Selecting APPR mode enables what?
|
Commands LOC and GS capture and tracking and clears TURB and ½ Bank. Also provides more
precise tracking and activates both Flight Directors. Ref: CR7/9 OM 11-2.3 |
|
|
What is the function of the XFR switch?
|
Selects the active flight director, which will follow guidance commands from the selected side flight
control computer. Ref: CR7/9 OM 11-2.3 |
|
|
What is the primary means to turn OFF the Autopilot?
|
Either AP DISC button on the control wheel.
Ref: CR7/9 OM 11-2.4 |
|
|
What are the manual methods used to turn OFF the Autopilot?
|
·Either AP DISC button on the control wheel (normal)
·Activating the Stab trim ·AP pushbutton on FCP panel ·AP DISC on the FCP panel ·Either TOGA pushbutton ·YD DISC button Ref: CR7/9 OM 11-2.4 |
|
|
What does the Airspeed Trend Vector indicate?
|
Predicts where the IAS will be in ten seconds.
Ref: CR7/9 OM 11-10.2 |
|
|
How is the stall speed displayed to the pilots?
|
By the Low Speed Cue (red/black checkerboard).
Ref: CR7/9 OM 11-10.2 |
|
|
If the pilot’s PFD CRT fails, how can the PFD be displayed on the MFD?
|
By selecting PFD 1 on the pilot‟s Display Reversionary Panel.
Ref: CR7/9 OM 11-10.6 |
|
|
What is meant by the response “As Required” to the “CVR CIRCUIT BREAKER” query on
the shutdown checklist to the line? |
If a possible NTSB Reportable Incident, as defined in the FOM, has occurred, pull the CVR circuit
breaker (CBP-2 V-7), and state “Pulled” otherwise state “Normal.” Ref: CR7/9 OM 2-16.2 |
|
|
In the event the Primary EICAS CRT (ED1) fails how is the information then displayed?
|
Automatically on ED2.
Ref: CR7/9 OM 11-14.2 |
|
|
How can the information normally displayed on ED2 be seen?
|
By changing the selector knob on the Display Control Panel to EICAS, the status and synoptic
pages are shown on the associated MFD Ref: CR7/9 OM 11-14.2 |
|
|
What happens and what can be done if ED1 fails?
|
If ED1 fails, the primary page is automatically displayed on ED2 and the ECP is deactivated. This
ensures that the engine instruments and CAS messages are always in view. Failure of ED2 also deactivates the ECP. Changing the selector knob to EICAS on either DRP will make the status and synoptic pages available on that MFD. If either ED1 or ED2 has failed, the ECP is deactivated. To reactivate the ECP, the selector on the Source Selector Panel must be moved to ED1 or ED2 – whichever CRT has not failed. If ED1 fails, all EICAS pages are available on ED2 after the selector on the Source Selector Panel is moved to ED2. If operating with a single ED and the Source Select Panel selected to allow ECP usage, a new Warning or Caution message will cause the ED to switch back to the primary page Selecting ED2 on the source selector panel will reactivate the ECP Ref: CR7/9 OM 11-14.11 |
|
|
What does the aural warning “CONFIG TRIM” indicate on takeoff?
|
The horizontal stabilizer, rudder or aileron trim is outside the takeoff (green) range.
Ref: CR7/9 OM 11-9.8 |
|
|
What are the four levels of CAS messages?
|
·Warning
·Caution ·Advisory ·Status Ref: CR7/9 OM 11-14.5How are CAS Warnings indicated? ·Triple Chime ·Flashing Warning lights ·Red light on the faulted switch or red EICAS indication ·Sometimes an aural tone ·Sometimes a voice message Ref: CR7/9 OM 11-14.6 |
|
|
If the ECP fails, what four buttons remain active?
|
The PRI, STAT, CAS, and STEP buttons bypass the microprocessor, and should function even if
the ECP has failed. Ref: CR7/9 OM 11-14.3 |
|
|
Pushing the CAS Pushbutton on the EICAS Control Panel (ECP), performs what function?
|
Will „box‟ the caution messages and display a MSGS icon, pushing again will display all caution
messages. Ref: CR7/9 OM 11-14.6 |
|
|
What is used to lower the landing gear if there is a failure in the gear control circuitry or
HYD system 3? |
By pulling the landing gear manual release handle, the uplocks are released, the nose strut is
pulled into place by drag assisted by hydraulic actuator (Hyd Sys 2). The main gear partially freefalls, then is assisted to the down and locked position by the MLG auxiliary actuators. Ref: CR7/9 OM 11-15.4 |
|
|
Can the landing gear warning horn be muted?
|
Yes, under some conditions.
Ref: CR7/9 OM 11-15.8 |
|
|
How do you perform an Anti-Skid test?
|
The ASCU (ANTI SKID CONTROL UNIT) does an automatic continuous self test and an initial
start-up self test, however on the first flight of the day it is turned OFF and re-ARMED manually to verify Anti-skid messages. Ref: CR7/9 OM 2-3.6 |
|
|
At what brake temperature readout do the units turn white?
|
They are white from 07.
Ref: CR7/9 OM 11-15.7 |
|
|
At what brake temperature readout do the units turn red?
|
They are red from 15.
Ref: CR7/9 OM 11-15.7 |
|
|
Upon entering the cockpit you notice a BTMS indication of 1, but the boxes are red. What
action do you take? |
Call maintenance because an overheat of at least 15 has occurred.
Ref: CR7/9 OM 11-15.7 |
|
|
What is the difference between a Huffer and a bottle, used for air starting?
|
A bottle is a large cylinder containing a charge of high pressure air. A Huffer is a self contained
high pressure air generation source. It has an engine and air pump but no storage. Ref: CR7/9 OM 4-1.2 |
|
|
Can you operate the air conditioning from a bottle?
|
No.
Ref: CR7/9 OM 4-1.2 OM 2-2,5 |
|
|
What is a Crossbleed start?
|
Starting an engine using bleed air from the running engine.
Ref: CR7/9 OM 4-1.2 |
|
|
What are the necessary precautions when performing a Cross Bleed Start?
|
·Position aircraft away from congested areas.
·Never perform a crossbleed start at the gate. ·Advise ATC you will be performing a Crossbleed start. ·It may be necessary to move the aircraft to a start up pad. ·The PIC could be responsible for damages caused by jet blast. Ref: CR7/9 OM 4-1.2 |
|
|
What detents are provided for the thrust levers?
|
SHUT OFF, IDLE, CLIMB, TOGA, AND MAX POWER.
Ref: CR7 OM 11-20.8 |
|
|
What is the indication the starter has cutout?
|
At approximately 50% N2 L(R)AUTOIGNITION and L(R) ENGINE START messages extinguish.
Ref: CR7/9 OM 11-20.15 |
|
|
What powers the FADEC?
|
Below 50% N2 the aircraft electrical system powers the FADEC. Above 50% N2 an alternator on
the accessory gearbox powers the FADEC. Ref: CR7/9 OM 11-20.4 |
|
|
The loss of an engine on takeoff will cause FADEC to increase power to what setting?
|
APR, when the thrust levers are in the TOGA detent.
Ref: CR7/9 OM 11-20.5 |
|
|
How many channels does each FADEC have?
|
Two, one normally in command and the other in standby.
Ref: CR7/9 OM 11-20.4 |
|
|
How is MCT selected?
|
When the CLIMB detent is selected and an engine fails, MCT is set on the operating engine.
Ref: CR7/9 OM 11-20.6 |
|
|
You aborted the engine start because you noticed a rapidly rising ITT. Must maintenance
be notified? |
Maintenance must be notified if the ITT exceeded 815, or if a HOT Icon appeared, or if a
malfunction is suspected. Ref: CR7/9 OM 3-4.2 |
|
|
Describe the proper procedure for setting takeoff power.
|
The PF will press the TOGA switch, advance the thrust levers to approximately 75% N1, allow the
engines to spool up together and the ITT to stabilize, then advance the thrust levers to the TOGA detent. The PF will then call “Set Power”. The PM then verifies the thrust levers are in the TOGA detent, and actual N1 agrees with N1 digital reference and N1 caret. PM then states “Power Set”. Ref: CR7/9 OM 3-5.1 |
|
|
Which engine ignition system(s) are supplied continuous ignition with the CONT
switch/light? |
Both
Ref: CR7/9 OM 11-20.15 |
|
|
Which ignition system does the DC Battery Bus power?
|
B
Ref: CR7/9 OM 11-20.16 |
|
|
When does continuous ignition come on automatically?
|
FADEC will activate continuous ignition based upon angle-of-attack data from the stall warning
computer. Ref: CR7/9 OM 11-20.16 |
|
|
What powers the Thrust reversers?
|
Hydraulic systems 1 and 2.
Ref: CR7/9 OM 11-20.16 |
|
|
Pushing the TOGA button(s) before takeoff, performs what function?
|
Activates the Vertical and Lateral Takeoff (TO/TO) modes, also provides a runway update to the
FMS. Ref: CR7/9 OM 11-20.8 & 9 11-2.2 & 2.3 |
|
|
Pushing TOGA for a Go-Around provides what FD guidance?
|
Current heading hold with 5 Angle of Bank authority and 8 pitch.
Ref: CR7/9 OM 11-2.2 |
|
|
What is the function of the pitch and roll disconnect handles?
|
To disconnect control wheels in case of a jammed elevator or aileron.
Ref: CR7/9 OM 11-9.2 |
|
|
What does the white status message FLAPS HALF SPEED indicate?
|
Reduced flaps deployment and retraction rate.
Ref: CR7/9 OM 11-9.6 |
|
|
What conditions must be met for GLD automatic arming?
|
GLD switch - AUTO, and L & R thrust lever TOGA.
Ref: CR7/9 OM 11-9.7 |
|
|
What conditions must be met for GLD deployment?
|
GLD switch - AUTO,
L & R thrust levers - IDLE, and 2 of the 3: L or R MLG WOW, radio altitude < 10 feet, wheel spin up speed >16 knots. Ref: CR7/9 OM 11-9.7 |
|
|
What is APR?
|
Automatic Performance Reserve.
Ref: CR7/9 OM P-5 CR7/9 OM 11-20.6 |
|
|
What does APR provide?
|
An automatic power increase on the operating engine in the event of an engine failure, during
takeoff or go-around. Ref: CR7/9 OM 11-20.6 |
|
|
How is the APR system armed?
|
The APR feature is armed automatically for takeoff or go-around.
Ref: CR7/9 OM 11-20.6 |
|
|
What is the function of the VOICE/BOTH switch on the audio control panels?
|
Voice position: Station IDs are filtered out allowing only voice signals to be heard. Both position:
Station IDs and voice signals are audible. Ref: CR7/9 OM 11-4.1 |
|
|
What is the function of the EMER position of the Emergency/Normal switch on the Audio
Control Panels? |
Pilot: Two-way communication on VHF 1, audio on NAV1 and aural warnings. Copilot: Two-way
communication on VHF2, audio on NAV2 and aural warnings. Ref: CR7/9 OM 11-4.1 |
|
|
In the event RTU 2 fails how can the # 2 radios be tuned?
|
Press RTU 2 INHB switchlight on the back-up tuning unit and the ½ pushbutton on RTU 1, the
Radio page on the FMS can also be used. Ref: CR7/9 OM 11-4.3 |
|
|
In the event RTU 1 fails how can the # 1 radios be tuned?
|
Press RTU 1 INHB switch/light on the backup tuning unit and the ½ pushbutton on RTU 2, the
Radio page on the FMS can also be used. Ref: CR7/9 OM 11-4.3 |
|
|
The CR9 Radio Tuning Units provide what additional feature not found on the CR7?
|
They provide centralized control and display for the HF radios.
CR7/9 OM 11-4.4 |
|
|
What are the normal TCAS selections?
|
AUTO, ON (traffic), REL, and NORM.
Ref: CR7/9 OM 2-3.7 |
|
|
What is the function of the XFR switch on the Radar Control Panel?
|
It transfers control of the WX radar display range to pilot‟s or copilot‟s display control panel.
Ref: CR7/9 OM 11-17.10 |
|
|
For what is the GCS (Ground Clutter Suppression) function used?
|
It decreases the intensity of ground returns in order to allow precipitation returns to be assessed
more accurately. Ref: CR7/9 OM 11-17.9 |
|
|
Is there a requirement to monitor a company frequency enroute?
|
Yes
Ref: FOM 2-4.4 |
|
|
Where do you find the proper radio frequency to monitor during flight?
|
Communication maps for Delta Radio (COMM-1), ASA DTMF (COMM-2) and ARINC ( ARINC-1 or
ARINC-5 for Mexico) are located in the ENROUTE section of the Jeppesen manual. Ref: FOM 2-4.4 |
|
|
What is the function of MACH trim?
|
The Mach trim system automatically adjusts the stabilizer trim as the aerodynamic center of
pressure moves rearward above Mach .4. Ref: CR7/9 OM 11-9.5 |
|
|
What is the priority of the stabilizer trim system?
|
·Pilot manual trim
·Co-pilot manual trim ·Autopilot trim ·Auto trim ·Mach trim Ref: CR7/9 OM 11-9.5 |
|
|
What does it mean when a DISPLAY COOL caution message is displayed in flight?
|
It indicates a low airflow condition.
Ref: CR7/9 OM 11-7.6 |
|
|
What can be done to extinguish a DISPLAY COOL message that is posted in flight?
|
Follow QRH procedure – use alternate fan STBY setting for cockpit air.
Ref: CR7/9 OM 11-7.6 |
|
|
What is the function of the NORM position for the DISPLY FAN on the AVIONICS COOLING
panel? |
Two fans are provided for CRT cooling. One fan is primary in-flight with another for ground
operations. Ref: CR7/9 OM 11-7.6 |
|
|
What is checked on the Aileron and Rudder Trim panel during the Originating Check?
|
Verify free movement in both directions, and then set to center.
Ref: CR7/9 OM 2-3.7 |
|
|
What happens if you press the DISC button on the yaw damper control panel?
|
Both yaw dampers will disconnect.
Ref: CR7/9 OM 11-9.3 |
|
|
Will the autopilot engage with the amber “YAW DAMPER” message posted?
|
No, at least one yaw damper must be engaged for the autopilot to engage.
Ref: CR7/9 OM 11-9.3 |
|
|
What does the 1/2 selection on the ATTD/HDG, AIR DATA, and DISP CONT switch and
ED1/ED2 on the EICAS do? |
In the event of an AHRS, ADC, EICAS or DCP failure, an alternate source for the disabled system
can be selected. Ref: CR7/9 OM 11-10.7 |
|
|
When will the ADG automatically deploy?
|
During a complete AC power failure.
Ref: CR7/9 OM 11-6.5 |
|
|
What is the function of the PWR TXFER OVERRIDE switch?
|
When pressed it switches the AC ESS bus back to AC BUS 1 or 2 if normal AC power is restored
after ADG deployment. Ref: CR7/9 OM 11-6.5 |
|
|
The EMER FLAP switch will override the SLAT/FLAP lever and set the slats and flaps to
what setting? |
Slats 25 and Flaps 20
Ref: CR7/9 OM 11-9.6 |
|
|
Can the EMER FLAP switch cause the flaps to extend at any speed?
|
No, it is inhibited above 230 knots.
Ref: CR7/9 OM 11-9.6 & 7 |
|
|
How many water systems are installed in the aircraft?
|
Two.
Ref: CR7/9 OM 11-22.1 |
|
|
Where are the water systems serviced?
|
Right side fuselage, one aft, one fwd.
Ref: CR7/9 OM 11-22.1 |
|
|
Where are the controls for the water systems?
|
The potable water control located in the forward galley.
Ref: CR7/9 OM 11-22.1 |
|
|
Are the water drain line(s) and drain mast(s) heated?
|
Yes.
Ref: CR7/9 OM 11-22.1 |
