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RJET E-170 Validation Guide > Originating & Receiving Checklist > Flashcards

Originating & Receiving Checklist Flashcards

1
Q

MCDU… SET

What are you setting/checking?

A
  • Verifying the NAV Database currency.
  • Initialize the FMS position on both FMSs.
  • Check all the electronic circuit breakers are in or MEL’d.
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2
Q

DVDR Control Panel … TESTED

What are you checking for when you press the test button?

A

Honeywell DVDR: Press the DVDR Test button and verify no fail messages displayed on EICAS.
Universal DVDR: Press and hold the TEST for 2 seconds. Verify no fail messages displayed on EICAS and observe the following test results:
The FDR 1 and CVR 1 PASS/FAIL lights flash for 10 seconds. After 10 seconds the FDR 1 and CVR 1 PASS/FAIL lights illuminate steady green, indicating the completion of a successful test.
After DVDR 1 test finishes, the DVDR 2 test will automatically start. Verify the following results:
The FDR 2 and CVR 2 PASS/FAIL lights flash for 10 seconds. After 10 seconds the FDR 2 and CVR 2 PASS/FAIL

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3
Q

DVDR Control Panel … TESTED

When does the DVDR normally begin recording?

A

After the first engine is started

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4
Q

DVDR Control Panel … TESTED

When does the DVDR turn off?

A

Weight on wheels and engine not running

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5
Q

ELECTRICAL PANEL … SET

What happens when the IDG sector knob is in AUTO?

A

AUTO – closes the IDG contactor and allows the automatic operation of the electrical system.

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6
Q

ELECTRICAL PANEL … SET

What happens when the IDG sector knob is in OFF?

A

OFF – opens the IDG contactor isolating the IDG from the respective AC BUS.

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7
Q

ELECTRICAL PANEL … SET

What happens when the IDG sector knob is in DISC?

A

DISC – must be held in this position for one second to mechanically disconnect the IDG.

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8
Q

ELECTRICAL PANEL … SET

Can the IDG generator be reconnected in flight?

A

No

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9
Q

What indication would you get with an IDG low oil pressure or high oil temperature?

A

An amber LED next to the associated IDG switch and an associated EICAS IDG 1 (2) oil illuminates.

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10
Q

ELECTRICAL PANEL … SET

What happens when the AC BUS TIE switch is in AUTO or 1 (2) OPEN?

A

AUTO – allows automatic operation of the electrical system.

1(2) OPEN – isolates the respective AC BUS.

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11
Q

ELECTRICAL PANEL … SET

What happens when the TRU 1(2), and TRU ESS Switches are in AUTO?

A

AUTO allows automatic operation of the electrical system.

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12
Q

ELECTRICAL PANEL … SET

What happens with the BATT 1 switch ON or OFF?

A

On: The battery is connected to the DC ESS BUS 1.
Off: The battery supplies power to the HOT BATT BUS.

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13
Q

ELECTRICAL PANEL … SET

What happens when the DC BUS TIES switch is in AUTO or OFF?

A

AUTO: Allows automatic operation of the electrical system.
OFF: Opens all BUSS TIE contactors.

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14
Q

ELECTRICAL PANEL … SET

What happens when the BATT 2 switch is in AUTO or OFF?

A

AUTO: Allows automatic operation of the electrical system.
OFF: The battery supplies power to the HOT BATT BUS 2

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15
Q

ELECTRICAL PANEL … SET

Why is there an AUTO position on BATT 2?

A

BATT 2 supplies the APU START BUS during APU starting.

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16
Q

ELECTRICAL PANEL … SET

Is BATT 1 necessary to start the APU?

A

Yes, BATT 1 powers the APU FADEC

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17
Q

COCKPIT LIGHTS PANEL … AS REQD

What are you checking for when you push the ANNUNCIATOR TEST Button?

A

The lamp integrity of all striped bars and caption indications on the main and overhead panel, and control pedestal.

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18
Q

FUEL PANEL … CHECKED

What is the max permissible fuel imbalance between left and rain main tanks?

A

794 lbs

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19
Q

FUEL PANEL … CHECKED

What is the limitation associated with the XFEED Selector?

A

XFEED Selector must be OFF for takeoff and landing

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20
Q

FUEL PANEL … CHECKED

How would you correct a fuel imbalance?

A

Position the XFEED Selector knob to the low side tank with LOW 1 (2) as required.

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21
Q

FUEL PANEL … CHECKED

What happens when the Crossfeed Selector knob is positioned in LOW l?

A

It opens the Crossfeed valve and automatically activates the right AC fuel pump
(AC PUMP 2), supplying fuel from the right wing tank to both engines.

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22
Q

FUEL PANEL … CHECKED

What is the purpose of the DC Fuel Pump?

A

It provides pressurized fuel for normal APU operation and engine start, when AC power or the AC fuel pump is not available.

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23
Q

FUEL PANEL … CHECKED

What happens when the AC PUMP 1 (2) selector knob is in AUTO?

A

Automatically operates the associated AC fuel pump according to system ‘s logic.

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24
Q

FUEL PANEL … CHECKED

What is the purpose of the AC Fuel Pump?

A

It is a backup pump, supplying fuel to the engine in the event of an ejector pump failure or during engine start

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25
Q

PASSENGER SIGNS PANEL … SET

When do the emergency light automatically come on?

A

Automatically illuminates all emergency light if the DC buses lose electrical power

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26
Q

PASSENGER SIGNS PANEL … SET

How long will the batteries supply emergency power to the ELPU’s?

A

Approx. 10 mins

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27
Q

FIRE EXTINGUISHER PANEL … CHECKED
What indications are you looking for on the Lights on overhead panel when you press & hold the Fire Detection TEST button?

A
  1. # I Engine Fire Extinguishing handle
  2. # 2 Engine Fire Extinguishing handle
  3. FIRE EXTINGUISHER CARGO SMOKE FWD pushbutton
  4. FIRE EXTINGUISHER CARGO SMOKE AFT pushbutton
  5. FIRE EXTINGUISHER APU pushbutton
  6. APU CONTROL EMER STOP pushbutton (upper half)
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28
Q

FIRE EXTINGUISHER PANEL … CHECKED

What EICAS messages are you looking for when you press & hold the Fire Detection TEST button?

A
  1. ENG 1 FIRE
  2. ENG 2 FIRE
  3. APU FIRE
  4. CARGO FWD SMOKE
  5. CARGO AFT SMOKE
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29
Q

FIRE EXTINGUISHER PANEL … CHECKED

What Lights on main instrument panel s are you looking for when you press & hold the Fire Detection TEST button?

A
  1. Left and right FIRE warning icon on ITT EICAS indicators

2. 2 Master Warning Lights (Red)

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30
Q

FIRE EXTINGUISHER PANEL … CHECKED

What aural warnings are you listening for when you press & hold the Fire Detection TEST button?

A
  1. Continuous bell and triple chime, silence by pressing either master WARN lights
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31
Q

WINDSHIELD WIPER … OFF

What is the max windshield wiper operation speed?

A

250 KIAS

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32
Q

HYDRAULIC PANEL … SET

What happens when you push the SYS 1 and SYS 2 ENGINE PUMP SHUTOFF guarded buttons?

A

Closes the hydraulic SOV, isolating the respective engine driven pump (EDP).

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33
Q

HYDRAULIC PANEL … SET

What is the purpose of the PTU?

A

The PTU uses system 1 hydraulic pressure and system 2 hydraulic fluid to provide additional power to retract the landing gear.

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34
Q

HYDRAULIC PANEL … SET

When will the PTU operate automatically?

A

With the PTU control knob in auto, during takeoff or landing if the #2 engine driven hydraulic pump or #2 engine fails.
Flaps not set to 0 OR landing gear is not up and locked and
EDP 1 not failed and
Hydraulic reservoir 2 quantity above 12%

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35
Q

HYDRAULIC PANEL … SET

What is the purpose of ELEC PUMP A and ELEC PUMP B?

A

ELEC PUMP A (B) is used as a backup for the respective Engine Driven Pump (EDP).

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36
Q

HYDRAULIC PANEL … SET

What happens when the SYS 1 ELEC PUMP selector knob is in AUTO?

A

Activates the electric pump whenever the EDP pump fails
In flight, flaps are selected to any position other than 0
On the ground, flaps are selected to any position greater than 0 and
Thrust levers set to takeoff thrust OR
Groundspeed is greater than 50 Kts.

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37
Q

HYDRAULIC PANEL … SET

A

On the ground, after starting engine number 1, releasing the-parking brake will
automatically activate electric pump 2 to allow single engine taxi. It will turn off 6 minutes after the parking brake has been applied.

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38
Q

HYDRAULIC PANEL … SET

What is the primary hydraulic source for hydraulic system 3?

A

SYS 3 ELEC PUMP A.

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39
Q

HYDRAULIC PANEL … SET

What is the purpose of SYS 3 ELEC PUMP B and what happens when the selector switch is in AUTO?

A

Backs up SYS 3 ELEC PUMP A. In AUTO, SYS ELEC PUMP B will come on when SYS ELEC PUMP A fails.

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40
Q

HYDRAULIC PANEL … SET

How would you be alerted to a hydraulic low quantity or over temperature?

A

On the EICAS display and confirmed on the hydraulic synoptic page on the MFD.

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41
Q

PRESSURIZATION PANEL … SET

Why do we put the CABIN ALT selector knob in the STOP position?

A

Normal operating position, allows automatic operation of the system.

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42
Q

PRESSURIZATION PANEL … SET

What are the DOWN/UP positions used for on the CABIN ALT selector knob?

A

Manually closes/opens the outflow valve to decrease/increase cabin altitude.

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43
Q

PRESSURIZATION PANEL … SET

What must you do to manually control the cabin altitude?

A

The pressurization MODE selector knob must be in MAN. When in manual mode, both CPCS controllers revert to standby, but only one channel performs the manual operation. The channel selection is automatic.
With the pressurization system in manual mode, the pilot is responsible for opening and closing the outflow valve to maintain the desired cabin altitude (reference the QRH for the schedule).
In manual mode, there is no automatic cabin depressurization on the ground (after landing).

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44
Q

PRESSURIZATION PANEL … SET

What is the LFE CTRL selector position on the pressurization MODE selector knob used for?

A

Allows manual input of the landing field elevation.

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45
Q

PRESSURIZATION PANEL … SET

Is the pressurization system still in the AUTO mode when LFE is entered manually?

A

Yes

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46
Q

PRESSURIZATION PANEL … SET

How would you manually control the LFE?

A

With the LFE selection knob momentary selected to the DOWN/UP position will decreases/increase the LFE in 100 ft. increments.

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47
Q

PRESSURIZATION PANEL … SET

What happens when you press the DUMP pushbutton?

A

In the AUTO mode, provides rapid depressurization of the cabin at 2000 fpm up to 12,400 feet.
Shuts off the recirculation fans and the packs

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48
Q

PRESSURIZATION PANEL … SET

What does the cyan “M” indicated on the EICAS?

A

A cyan “M” in front of the altitude readout indicates manual input of the landing field elevation.

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49
Q

PRESSURIZATION PANEL … SET

How can you determine the position of the outflow valve?

A

There is a pointer on the outflow valve position indicator on the environmental control system (ECS) synoptic page on the MFD.

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50
Q

WINDSHIELD HEAT … In

What happens to the WINDSHIELD HEAT when you have a single power source?

A

On the ground, the windshield heating is inhibited. In flight, only the left windshield heat is powered, or the right windshield heat is powered if the left has failed.

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51
Q

ICE PROTECTION PANEL … SET

At what temperature are we considered in icing conditions?

A

10C OAT on ground/takeoff

10C TAT in flight

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52
Q

ICE PROTECTION PANEL … SET

When must engine anti-ice be on?

A

During all flight and ground operations when icing conditions exist or when ICE is
annunciated by the ice detection system.

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53
Q

ICE PROTECTION PANEL … SET

How many ice detectors is the airplane equipped with?

A

2

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54
Q

ICE PROTECTION PANEL … SET

What would happen with the failure of one ice detector?

A

If the remaining detector senses an icing condition, the system automatically activates the ENGINE and WING anti-ice system.

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55
Q

ICE PROTECTION PANEL … SET

When the ice detectors automatically activate the engine and wing how long will the ice detectors remain activated?

A

For 5 minutes after the detector is no longer sensing an icing condition.

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56
Q

ICE PROTECTION PANEL … SET

What happens when the ICE PROTECTION MODE selector knob is in AUTO?

A

Allows the automatic operation of the engine anti-ice system.

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57
Q

ICE PROTECTION PANEL … SET

How can you override the system logic and turn the anti ice system on?

A

Select the ICE PROTECTION selector knob to on.

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58
Q

ICE PROTECTION PANEL … SET

What happens when you select the WINDSHIELD WIPER selector knob to timer?

A

The windshield wipers operate on a 7 second intermittent operation.

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59
Q

ICE PROTECTION PANEL … SET

What happens to the engine bleed valve with the loss of electrical power?

A

The engine bleed valve is fail-safe open.

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60
Q

ICE PROTECTION PANEL … SET

What control surfaces are heated by the wing anti- ice system?

A

The 3 outboard leading edge slats on each wing.

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61
Q

ICE PROTECTION PANEL … SET

What happens in the event of a bleed air source failure?

A

The system automatically opens the crossfeed valve supplying airflow from one engine bleed to the opposite wing anti-ice.

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62
Q

ICE PROTECTION PANEL … SET

Are the AIR DATA SMART PROBE and TAT probes heated?

A

Yes, whenever either engine is running

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63
Q

ICE PROTECTION PANEL … SET

What happens if you operate the windshield wiper system on a dry windshield?

A

They will stop and remain inoperative until the wiper control is set to OFF.

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64
Q

ICE PROTECTION PANEL … SET

How would you configure the ENGINE and WING anti-ice system for automatic operation?

A

The ENGINE 1 (2) ICE PROTECTION push buttons must be in.

OFF, ENG, or ALL must be selected on the MCDU TO DATASET Menu.

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65
Q

ICE PROTECTION PANEL … SET

What happens when ALL is selected in the REF ALL line in the MCDU and the ice protection selector knob is in AUTO?

A

The engine anti-ice valves are commanded open after the completion of the engine start and the wing anti-ice valve are commanded open with wheel speed above 40 kts. The EICAS status message END TDS REF A-I ALL will be displayed to confirm the MCDU selection.

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66
Q

ICE PROTECTION PANEL … SET

When do we use the Ice Protection Test selector knob?

A

The TEST function is a maintenance procedure.

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67
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What is the DUMP pushbutton used for?

A

The DUMP function is used for emergency evacuation, smoke evacuation, and fast cabin de-pressurization.

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68
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What happens to the Recirculation Fans when the DUMP button is pushed, or smoke is detected in the recirculation bay?

A

25 September 1, 2014

The Recirculation Fans are commanded to off

69
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What happens when the PACK 1 (2) pushbutton switch is in?

A

Allows automatic operation of the pack valve by the AMS controller.

70
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

Is a single pack capable of maintaining adequate cabin/cargo pressurization and temperature?

A

Yes

71
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What is the maximum cruise altitude with only 1 pack operating?

A

FL 310

72
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What happens when the XBLEED pushbutton is in?

A

Allows automatic operation of the crossbleed valve by the AMS controller

73
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET
What happens when one side provides manifold pressure and there is not a bleed air source on the opposite side when the XFEED pushbutton is in?

A

The crossbleed valve is commanded open.

74
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What happens when the BLEED 1 (2) pushbutton is in?

A

Allows automatic operation of the bleed valve by the AMS controller.

75
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What happens when the BLEED APU pushbutton is in?

A

Allows automatic operation of the APU bleed valve by the AMS controller.

76
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

Can engine bleed air flow to the APU when the engine is running?

A

No. The APU check valve will prevent engine bleed airflow to the APU.

77
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET
When the engine and APU bleed are available simultaneously and the airplane is on the ground, or the opposite engine bleed pressure is below the minimum for engine start, which has priority?

A

The APU bleed supply

78
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

Can the APU bleed be used for the anti ice system?

A

No

79
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What protects the bleed system from an overheat condition?

A

The overheat detection system

80
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

When is the Emergency Ram Air Valve commanded to open?

A

Anytime the airplane is in flight and both air conditioning packs commanded or failed OFF and the airplanes altitude is less than 25,000 feet.

81
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

How many channels does the Cabin Pressure Controller have?

A

The CPC has 2 independent automatic channels that alternate after each flight

82
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What prevents the cabin from negative pressure?

A

The negative pressure relief valve (NPRV).

83
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

Does the positive pressure relief valve require electrical power to operate?

A

No

84
Q

AIR CONDITIONING/PNEUMATIC PANEL … SET

What happens to the Landing Field Elevation (LFE) in the ABORT mode?

A

During the ABORT mode the cabin pressure is scheduled back to the takeoff altitude.

85
Q

PASSENGER OXYGEN … SET

What happens with the PASSENGER OXYGEN selector knob in AUTO?

A

Enables the automatic deployment of the passenger oxygen masks when the cabin pressure altitude is above 14,000 feet.

86
Q

PASSENGER OXYGEN … SET

What happens with the PASSENGER OXYGEN selector knob in OVRD?

A

It deploys the passenger oxygen masks regardless of cabin altitude.

87
Q

PASSENGER OXYGEN … SET

What is indicated when the MASK DEPLOYED light is on?

A

The passenger and flight attendant oxygen masks have been deployed

88
Q

PASSENGER OXYGEN … SET

Where would you find the oxygen system parameters and indications?

A

On the Status Page and the EICAS displays.

89
Q

PASSENGER OXYGEN … SET

How is passenger oxygen supplied?

A

Chemical oxygen generators

90
Q

PASSENGER OXYGEN … SET

How long will the passenger oxygen system provide a supply of oxygen?

A

Approximately 12 mins

91
Q

Standby compass … checked

Are there any times when the mag compass indication in invalid?

A

When transmitting on VHF #1

92
Q

Standby compass … checked

What are you checking for?

A

Cross check heading against pilot and copilot HSIs on the PFD/MFD

93
Q

Guidance Panel … Set

What is the minimum height for autopilot engagement?

A

400 ft

94
Q

Guidance Panel … Set

What is the minimum height for a couples ILS approach

A

50 feet

95
Q

Guidance Panel … Set

What does the SRC button do?

A

It alternates the Captain or FO AFCS side as the data source

96
Q

Guidance Panel … Set

What does the green arrow on the FMA indicate?

A

The elected AFCS source

97
Q

DISPLAY CONTROLLER UNIT … SET

What are you setting?

A

The current airport altimeter

98
Q

REVERSIONARY PANEL … Set

What happens with the DISPLAYS selector in AUTO?

A

Automatically reverts the MFD in case of display failure

99
Q

What indication would you get when you push the SENSORS ADS or IRS pushbutton?

A

A white striped bar illuminates on the button

100
Q

PFD … Checked

What are some of the items you are checking on the PFD?

A
  1. Airspeed tape – no speeds
  2. EADI – level and no flags
  3. Altitude tape – within limits (+/- 75 feet)
  4. VSI – zero
  5. EHSI and compass – same headings and no flags.
101
Q

MFD … checked

What are you checking for?

A

Looking for green indications (no amber)

  1. Hydraulic page check
    a. Fluid quantity
    b. Hyd pressure
  2. Status page check
    a. Hydraulic brake accumulator pressures
    b. Oil quantities
    c. Oxygen quantity (green, cyan, or amber)
102
Q

MFD … Checked
What is the max altimeter altitude difference in flight?
-

A

Aircraft Altitude Max Diff
-2000 up to 10,000 / 50 feet
10,000 up to 20,000 / 120 feet
20,000 up to 41,000 / 180 feet

103
Q

IESS … Checked and Set

What does the IESS do?

A

Displays Attitude (pitch and roll), altitude, and indicated airspeed.

104
Q

IESS … Checked and set

When is the IESS powered?

A

When the batteries are switched to AUTO

105
Q

IESS … Checked and set

How is the IESS powered in an emergency

A

The IESS is powered by the RAT or by the batteries

106
Q

What types of approaches are not authorized using the IESS?

A

LOC backcourse

107
Q

Auto brakes … Checked & Set

How do you check the Autobrakes?

A

Verify the AUTOBRAKES on the EICAS shows OFF

108
Q

Auto brakes … Checked & Set

What conditions must be met for the Autobrakes to engage during a rejected takeoff?

A

Thrust levers Idle or REV.
Wheel speed above 60 kts.
Brake pedals not pressed

109
Q

Auto brakes … Checked & Set

How are the autobrakes disarmed?

A

Selector set to OFF
Pedal brake pressure is applied
Brake control system failure is detected
Either thrust lever is advanced beyond idle during autobrake application

110
Q

GND PROX TERR INHIB … Out

What is the GND PROX TERR INHIB switch used for?

A

Momentary pushbutton annunciator used to manually cancel glideslope alerts. Illuminates when pressed any time below 2,000 ft. nominal radar altitude and is automatically reset (light off) by climbing above 2,000 ft. or descending below 30 ft.
Used to inhibit unwanted terrain alerts in airports not covered by the EGPWS database.

111
Q

Parking Brake Light … Checked

How do you know that the parking brake is set?

A

An “ON” light illuminates on the EMERG PRKG BRAKE light.

112
Q

Parking Brake Light … Checked
How many full brake applications are available with the EMER/PRKG brake
accumulator?

A

6

113
Q

Clock … Set

What is indicated when the clock displays dashes (—-)?

A

No GPS signal is detected

114
Q

Landing gear lever … DN

What does a red icon indicate on the landing gear position indicator?

A

A discrepancy between the landing gear lever position, and the respective landing gear position.

115
Q

Landing gear lever … DN

How do you engage the nose wheel steering system?

A

The nose wheel steering handle must be pushed down to engage the system.

116
Q

Landing gear lever … DN

What are the 3 landing gear extension modes?

A

Normal
Electrical override
Alternate

117
Q

Landing gear lever … DN

When would you use the Electrical Override switch?

A

When the normal extension mode fails, the electrical override system bypasses the PSEM, and energizes the landing gear selector valve allowing extension.

118
Q

Landing gear lever … DN

When would you use the Alternate Gear extension procedure?

A

The Alternate Extension procedure would be used in the event of a failure of the electric and hydraulic systems.

119
Q

Landing gear lever … DN

When would you get the aural warning “LANDING GEAR?

A

Below 700 ‘ AGL RA with the flap lever in any position, or with the flap lever in the landing position (5 or FULL) regardless of the RA.

120
Q

Landing gear lever … DN

What disengages the rudder pedal steering?

A

The activation of the nose wheel steering.

121
Q

Landing gear lever … DN

Which steering mode is used for high-speed control?

A

The rudder pedal steering mode.

122
Q

Landing gear lever … DN

When is handwheel steering mode activated?

A

Used for low speed contol.
During taxiing, an extended steering range greater than that provided via rudder pedals are available through the pilot’s tiller. Activation of the tiller disengages pedal steering.

123
Q

Landing gear lever … DN

When is locked wheel protection deactivated?

A

When the faster wheel speed is below 30 knots.

124
Q

When is the Anti Skid system deactivated?

A

When the wheel speed is below 10 knots.

125
Q

What is maximum gear extension, VLO, gear extended VLE, and gear retraction VLO Speeds on the 170/175?

A

25 KIAS

126
Q

What is the max operating speed

A

VMO

127
Q

What is the max operation Mach number

A

.82M

128
Q

What is turbulent air airspeed (below 10,000ft)

A

250KIAS

129
Q

What is turbulent air airspeed above 10K’?

A

270 KIAS / .70M

130
Q

When is the GRD PROX INHIB switch used?

A

To manually cancel glideslope alerts anytime below 2000 feet and will automatically be reset by climbing above 2000 feet or descending below 30 feet.

131
Q

LG WRN INHIB … OUT

When is this switch used?

A

To inhibit landing gear warning in the event of a dual radio altimeter failure

132
Q

LG WRN INHIB … OUT

What is the indication that the button has been pressed?

A

A white striped bar illuminates

133
Q

FLIGHT CONTROLS MODE … Checked

What are the two modes?

A

Normal and Direct

134
Q

FLIGHT CONTROLS MODE … Checked

What happens when the FLIGHT CONTROL MODE button is pushed?

A

The associated system goes into the direct mode

135
Q

FLIGHT CONTROLS MODE … Checked

When all systems on board are operating normally, what will be the flight control mode?

A

Normal

136
Q

FLIGHT CONTROLS MODE … Checked

What are some examples of NORMAL MODE functions?

A

Elevator control law scheduling with airspeed
Auto-thrust compensation with elevator
Mach trim and autopilot trim functions in AFCS
Angle-of Attack (AOA) limiting with elevator offset
Rudder airspeed gain scheduling and stroke limiting
Yaw damper and turn coordination via AFCS
Rudder flight authority
Roll spoiler scheduling with airspeed and speedbrake deployment
Automatic spoiler deployment at high Mach number
Configuration change compensation with Horizontal Stabilizer

137
Q

STALL WARNING … Checked

What happens when the STALL WARNING cutout button is pushed?

A

Cuts out the associated shaker channel

138
Q

STALL WARNING … Checked

How would you be alerted to an AOA limit failure?

A

An EICAS message

139
Q

STALL WARNING … Checked

What happens when the stick shaker is activated?

A

Control column authority is limited in the nose up direction

140
Q

POWERPLANT PANEL … Checked

What are the starter cranking lists on the ground?

A

a. 1st and 2nd Start – 90 Seconds ON, 10 Seconds OFF

b. 3rd to 5th Start – 90 Seconds ON, 5 Minutes OFF

141
Q

POWERPLANT PANEL … Checked

What controls engine starting and provides hung start, hot start, and no light off protection?

A

The FADEC

142
Q

POWERPLANT PANEL … Checked

How is the FADEC powered?

A

The FADEC has its own alternator above approximately 50% N2 backed up by the airplanes electrical system.

143
Q

POWERPLANT PANEL … Checked

How many channels does the FADEC computer have?

A

2, one channel is always active, while the other is an automatic backup.

144
Q

POWERPLANT PANEL … Checked

How is the ATTCS system controlled?

A

The FADEC

145
Q

POWERPLANT PANEL … Checked

If the ATTCS is selected off for takeoff, will it be available for go-around?

A

Yes, it will be armed automatically during the go-around mode.

146
Q

POWERPLANT PANEL … Checked

What is a Flexible Thrust take-off?

A

A reduced thrust take-off based on an assumed temperature.

147
Q

POWERPLANT PANEL … Checked

How are engine thrust ratings controlled?

A

By the FADEC

148
Q

POWERPLANT PANEL … Checked

How long is the Go around mode limited to in the go-around phase?

A

5 mins

149
Q

POWERPLANT PANEL … Checked

The FADEC has four idle modes, what are they?

A

Flight, Approach, Final Approach, and Ground.

150
Q

POWERPLANT PANEL … Checked

Where would you set the TO thrust rate mode and TO temperature?

A

The T/O DATASET MENU on the MCDU.

151
Q

EICAS FULL … OUT

What happens when the EICAS FULL Pushbutton is pushed in?

A

The automatic EICAS de-clutter logic is inhibited

152
Q

EICAS FULL … OUT

What are the EICAS Engine Limit Display Markings?

A

Red - Maximum and Minimum Limitations
Amber – Caution Range
Green – Normal Operating Range

153
Q

Speed Brake Lever … 0

During ground operations, which spoiler panels function as ground spoilers?

A

The ground spoiler function commands all ten ground spoilers at full rate.

154
Q

Speed Brake Lever … 0

When does full Multi-function spoiler extension occur?

A
  1. Weight on wheels on ground.
  2. Main wheel speed is above 45 Kts or airspeed is above 60 KIAS.
  3. Thrust Lever Angle (TLA) below 26 degrees.
155
Q

Speed Brake Lever … 0

What will happen if the speed brakes are extended during approach?

A

The speed brakes will automatically retract upon selection of Flap/Slat 2 or airspeed is below 180 kts. or thrust levers advanced beyond 70 degrees TLA.

156
Q

Speed Brake Lever 0

When will the speed brakes automatically retract during a go-around maneuver?

A

When the Thrust Lever Angle (TLA) is advanced beyond 70 degrees.

157
Q

Speed Brake Lever … 0

Are speed brakes available in the direct mode?

A

No – they are controlled by the FCM

158
Q

Speed Brake Lever … 0

What indication on the EICAS would indicate the speed brakes are open?

A

A white SPDBRK annunciation

159
Q

Thrust Levers … IDLE

The application of maximum reverse thrust is not permitted below what airspeed?

A

60 KIAS

160
Q

Thrust Levers … IDLE

What are the other 4 limitations associated with the thrust reversers?

A

Approved for ground use only
Intended for use during full stop landings
Do not attempt a go-around maneuver after deployment of the thrust reversers
Power back operations using thrust reversers are prohibited

161
Q

RAT MANUAL DEPLOY … Stowed

What will cause the RAT to extend Automatically?

A

Whenever AC ESS BUS loses power.

162
Q

RAT MANUAL DEPLOY … StowedWill the emergency generator supply power immediately after automatic RAT deployment?

A

No, there is an 8 second delay during which time the batteries supply power to the DC ESS BUSES and the STANDBY AC BUS.

163
Q

RAT MANUAL DEPLOY … Stowed

What is the minimum speed required to ensure RAT operation?

A

130 knots

164
Q

RAT MANUAL DEPLOY … Stowed

Is there and altitude restriction for operation of the RAT?

A

No

165
Q

RAT MANUAL DEPLOY … Stowed

How would you deploy the RAT in case of an automatic deployment failure?

A

Use the RAT manual deploy handle.

166
Q

O2 & Interphone … Checked

How do you check the O2 and Interphone?

A 
Control Wheel Com switch to MIC HOT
Regulator Control Knob to 100%
Press and hold the TEST/RESET Button
Yellow indicator blinks (short illumination)
Audible Pressure sound through the cockpit speakers
Release the TEST/RESET Button
Regulator Control Knob to EMER
REPUBLIC AIRLINES
KNOWLEDGE VALIDATION GUIDE
36 September 1, 2014
Press and hold the TEST/RESET Button
Yellow indicator illuminates as long as TEST/RESET Button is pressed
Release the TEST/RESET Button
Regulator Control Knob back to 100%
167
Q

How is cockpit crew oxygen supplied?

A

By a single high-pressure bottle.

168
Q

Where is the oxygen over pressure blow out disk located?

A

To the right of the forward cargo compartment door.

RJET E-170 Validation Guide (7 decks)

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