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ERJ QRC (Memory Items) > ERJ 175 Quick Reference Card (QRC) > Flashcards

ERJ 175 Quick Reference Card (QRC) Flashcards

Memory Items

1
Q

V1 Cut

Engine fail after takeoff

A

QRC
ENGINE FIRE, SEVERE DAMAGE, OR SEPARATION - check list

AUTO THROTTLE………………… DISENGAGE
Affected Engine
THRUST LEVER 1(2) …………………….IDLE
START/STOP SELECTOR 1(2) ……….STOP
FIRE EXT HANDLE 1(2)………………….PULL

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2
Q

DUEL ENGINE FIRE

A

QRC
DUEL ENGINE FIRE - checklist

AIRSPEED…………………………………….. 250 KTS
RAT MANUAL DEPLOY LEVER…….. PULL

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3
Q

EMERGENCY EVACUATION

A

QRC
Emergency Evacuation - Checklist

EMERGENCY PARKING BRAKE………….. ON
THRUST LEVERS…………………………………IDLE
START/STOP SELECTORS………………….STOP
FIRE EXT HANDLES-PULL & ROTATE (1L&2R)
APU EMERGENCY STOP BUTTON (PUSH IN)
APU FIRE EXT BUTTON……………….PUSH IN
PRESSURIZATION DUMP……………..PUSH IN
EMERGENCY EVACUATION……….ANNOUNCE
ATC (FO)…………………………………………….NOTIFY
BATTERIES…………………………………………….OFF

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4
Q

Cabin Altitude High (memory)

A

QRC - memory item
Cabin Altitude High - Checklist
OXYGEN MASKS …………………….DON 100%
CERW COMMUNICATIONS…….ESTABLISH

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5
Q

EMERGENCY DESCENT

A

QRC
Emergency Descent - Checklist

FASTEN SEAT BELT SIGNS…………ON
ALTITUDE…………………….10,000 OR MEA (WHICHEVER IS HIGHER)
FLCH…………………………………………SELECT
THRUST LEVERS………………………IDLE
SPEED BRAKE…………………………..FULL OPEN
AIRSPEED…………………………MAX APROPRIATE
TRANSPONDER (FO)…………………7700
ATC (FO)……………………………………..NOTIFY
PA (FO)………………ATTN FLIGHT ATTENDANTS
EMERGENCY DESCENT
PA(FO) ………………ATTN FLIGHT ATTENDANTS
WE HAVE REACHED A SAFE ALTITUDE IT IS SAFE TO REMOVE OXYGEN MASKS

QRH EAP2-1

CABIN ALTITUDE HI
EICAS Indication: Cabin Altitude indication in red. Aural Warning: CABIN

Crew Oxy Masks……………………………. DON, 100% Crew Communication……………………… ESTABLISH Altitude…………………………………………. 10000 ft or MEA,
WHICHEVER IS HIGHER
Thrust Levers………………………………… IDLE
SPEEDBRAKE Lever…………………….. FULL OPEN Airspeed……………………………………….. MAX/ APPROPRIATE Transponder…………………………………. 7700 ATC……………………………………………… NOTIFY

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6
Q

ENGINE ABNORMAL START (memory)

A

QRC - memory item
Engine Abnormal Start - checklist
START/STOP SELECTOR……….STOP

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7
Q

APU FIRE

A

QRC
APU Fire Checklist

APU EMERGENCY STOP BUTTON..PUSH IN

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8
Q

CARGO COMPARTMENT FIRE

A

QRC
Cargo Compartment Fire - checklist

CAUTION - Do not discharge cargo fire extinguisher on the ground with the cargo door open.

ASSOCIATED CARGO
FIRE EXTINGUISHING BUTTON…….PUSH

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9
Q

CRG FWD (AFT) SMOKE

A

QRC

CRG FWD(AFT) SMOKE - Checklist

CAUTION - Do not discharge cargo fire extinguisher on the ground with the cargo door open.

ASSOCIATED CARGO
FIRE EXTINGUISHING BUTTON…….PUSH

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10
Q

SMOKE EVACUATION (memory)

A

QRC - Memory Item

Smoke Evacuation - checklist

OXYGEN MASKS………..DON EMERGENCY
CREW COMMUNICATION….. ESTABLISH
PRESSURIZATION DUMP………..PUSH IN

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11
Q

SMOKE / FIRE / FUMES (memory)

On descent, you smell a strong burning smell that isn’t dissipating. What’s the first thing you would do? (Smoke/fire/fumes memory items.

A

QRC - memory item
Smoke / Fire / Fumes - checklist
OXYGEN MASKS……………………DON 100%
CREW COMMUNICATION…… ESTABLISH

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12
Q

BATT 1 (2) OVERTEMP (memory)

What do you do?
How do you verify that this action was effective?

A

QRC - Memory Item - (QRH EAP 5-1)

BATT 1(2) OVERTEMP checklist

ASSOCIATED BATTERY …………OFF

Check MFD - Electric Systems Synoptic Page

(QRH EAP 5-1)
BATT 1 (2) OVERTEMP
Associated BATT Knob........................ OFF 
NOTE: 
Do not start the APU.
END
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13
Q

Elevator Jammed.

What if it was the elevator pitch that was jammed?

A

QRC - Memory Item

JAMMED CONTROL COLUMN - PITCH - check list

ELEVATOR DISCONNECT HANDLE….PULL

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14
Q

Ailerons Jammed.

You’re flying at cruise when the auto pilot disconnects. After taking the controls, you realize that the aileron controls are jammed. What do you do?

A

QRC - memory items

JAMMED CONTROL WHEEL - roll checklist

AILERON DISCONNECT HANDLE…….PULL

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15
Q

PITCH TRIM RUNAWAY (memory)

A

QRC
Pitch Trim Runaway - checklist

A/P DISC BUTTON……………………………..PRESS AND HOLD
PITCH TRIM SYS 1 and 2 CUTOUT BUTTONS…….PUSH IN

QRH NAP 1-15

PITCH TRIM RUNAWAY
AP/TRIM DISC Button………………………. RELEASE
WARNING: DO NOT OPEN THE SPEEDBRAKE.
NOTE: Continuous turns helps to alleviate excessive pitch up tendencies.
Prepare to overcome unwanted pitch change:
Pitch Trim SYS 1 CUTOUT Button……. PUSH OUT PITCH TRIM Switch………………………… ACTUATE

AP/TRIM DISC Button……………………. PRESS AND HOLD Pitch Trim SYS 1 and SYS 2
CUTOUT Buttons………………………….. PUSH IN
PITCH TRIM NORMAL?
Yes

No
NOTE: Manual trim command through Pitch Trim Switches is available with at least one functional HS-ACE channel. With one HS-ACE channel available expect the following differences on the pitch trim indication on EICAS:
– Pitch trim readout display showing amber dashes.
– Pitch trim scale without the solid green pointer.
END

Pitch Trim SYS 1 CUTOUT Button……… PUSH IN Pitch Trim SYS 2 CUTOUT Button……… PUSH OUT

NOTE: Manual trim command through PITCH TRIM Switches is available with at least one functional HS-ACE channel.
With one HS-ACE channel available expect the following differences on the pitch trim indication on EICAS:
– Pitch trim readout display showing amber dashes.
– Pitch trim scale without the solid green pointer.
END

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16
Q

ROLL (YAW) TRIM RUNAWAY (memory)

You’re flying in Cruise when the auto pilot disconnects and the airplane starts yawing and banking to the right. You see on the EICAS that the YAW trim is deflecting to the right. What do you do?

What if it was the aileron trim?

A

QRC - Memory Item

ROLL (YAW) TRIM RUNAWAY - checklist

A/P DISC BUTTON…………PRESS AND HOLD

QRC - memory items

JAMMED CONTROL WHEEL - roll checklist

AILERON DISCONNECT HANDLE…….PULL

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17
Q

STEERING RUNAWAY (memory)

A

QRC - memory item
Steering runaway checklist

STEER DISC SWITCH…………….PRESS
Steer the airplane using differential braking and rudder.

QRH
STEER FAIL
EMERGENCY/PARKING BRAKE Lever……………………………………………… SET
Steer DISENGAGE Switch………………… PRESS AND HOLD NOSEWHEEL STEERING Handle……… PRESS AND RELEASE Steer DISENGAGE Switch………………… RELEASE
If the message persists, accomplish the following CB reset procedure:
CAUTION: MAKE SURE THAT THE INTEGRATED PITOT/ STATIC/AOA SENSORS, TAT SENSORS, ICE DETECTORS AND STATIC PORTS HAVE NO COVERS ON THEM BEFORE ACCOMPLISHING THIS PROCEDURE. THESE COMPONENTS CAN BECOME HOT DURING THIS PROCEDURE DAMAGING THEM.
NOTE: – Refer to the MAU SAFETY PROCEDURES before accomplishing this procedure.
– Crosscheck flap setting after the reset on MCDU’s Takeoff page 2/3.
Open the following CB, after approximately 3 s, reset them: RHCBP…………………………………………… MAU 2 PWR 1
END

18
Q

Duel EFB Failure

A

QRC
Duel EFB Failure - Checklist
DISPATCH …………………..NOTIFY
ATC……………………………….NOTIFY
FMS………………………………PROGRAM

19
Q

Where is the the SMOKE EVACUATION memory item found in the QRH?

A

SMOKE Section QRH S1-2

SMOKE EVACUATION
Crew Oxy Masks………….. DON, EMER
Crew Communication….. ESTABLISH
DUMP Button…………………PUSH IN

LAND AT THE NEAREST SUITABLE AIRPORT.
Cockpit Door……………….. CLOSE Cabin
Rate………………………………. VERIFY
CABIN RATE IS LESS THAN 1000 FT/MIN?
Yes

Pressurization MODE Selector……………………. MAN
No

PACK 1 Button.............. PUSH OUT 
PACK 2 Button.............. PUSH OUT 
RECIRC Button ............ PUSH OUT
FSTN BELTS Switch...... ON 
Altitude........................... 10000 ft OR MEA, WHICHEVER IS HIGHER
Thrust Levers................. IDLE 
SPEEDBRAKE Lever..... FULL OPEN 
Airspeed......................... MAX/
APPROPRIATE Transponder................... 7700
20
Q

Where is the Battery Temperature read?

27.1 NG IAS Pilot Guide Ch.7

A

(MFD) Electrical Systems Synoptic Page

21
Q

When will FADEC abort an engine start?
AOM pg 218

When is a manual abort on engine start required?

A

hot start,
hot re-start
hung start

Manual Abort Required

1) No Oil pressure in 10 seconds at N2 increases
2) Oil stabilizes below limits
3) Tailwind - No N1 indication before N2 @50%
4) No ITT reading within 30 seconds
5) ITT exceed hot start limits 815º (hot start)
6) N1 or N2 fail to accelerate to stable idle -speeds - (hung start)
7) starter malfunction occurs

22
Q 
After disconnecting the Ailerons, what controls remain usable on the "free side"?
pg 39 (Flight Controls / Stall Protection)
A

PF controls ailerons on his side.

and remaining flight controls.

23
Q

You’re flying in cruise when the autopilot disconnects and the airplane begins to pitch up, in spite of nose-down control pressure. What do you do? (Pitch Trim Runaway)

A

QRC - Memory Item
A/P DISC BUTTON………………..PRESS AND HOLD
PITCH TRIM SYS 1 and 2
CUTOUT BUTTONS……………..PUSH IN

QRH NAP 1-15
ABNORMAL CHECKLIST
NORMAL CHECKLIST

24
Q

Give another example of why it is alway important to view the appropriate synoptic page(s) when troubleshooting a problem?

A

Fuel balance…

25
Q

How would you alleviate excessive pitch up tendencies with a PITCH TRIM RUNAWAY?

A

QRC (Memory Item)
PITCH TRIM RUNAWAY
A/P DISC BUTTON………………….PRESS AND HOLD
PITCH TRIM SYS 1 and 2
CUTOUT BUTTONS………………..PUSH IN

QRH Non-Annunciated
Continuous turns (Note QRH)
26
Q

True / False: JAMMED CONTROL WHEEL - ROLL MI

Cross wind component greater than 10 its must be avoided.

A 
True:
QRH Non Annunciated 
JAMMED CONTROL WHEEL (ROLL)
CAUTION NOTE: 
During Landing a crosswind component greater than 10 kts must be avoided.
27
Q

When powering-up the aircraft, what minimum voltage is required?

A

22.5 Volts

28
Q

When would you need to perform the the SOPM (battery) Charging procedures?

A

21 - 22.5 Volts
Recharge through any AC source (including engines during taxi)
>= 0ºC …………………….30 min
> = -5º and < 0º ………..35 min
>= -10 and < -5º………….40 min
< -10º…………………………..50 min
< 21 Volts - Report IAW SP3100 - Do not depart.

29
Q

After the EICAS is powered, how long must we wait before APU start? SOPM pg31

A

30 Seconds

30
Q

How long can you leave the aircraft with the APU powered? SOPM pg31

A

5 minutes

31
Q

You’re starting an engine and notice the the ITT is rapidly rising toward the ITT redline. What temperature is redline, and what do you do?

A

(QRC) (AOM CH2-40, SOPM CH2), (AOM CH2-40), (QRH NAP 1-6)

QRC
ENGINE ABNORMAL START
AFFECTED ENGINE
START STOP SELECTOR ……………………………STOP

(AOM CH2-40) or SOPM 137 of 333
MAX TEMP - 815 deg C

QRH NAP 1-6

EMERGENCY EVACUATION
Emergency/Parking Brake……………ON
Thrust Levers………………………………… IDLE
Engine 1 and 2 START/STOP Selectors………………………………………. STOP
Engine 1 and 2 FIRE EXTINGUISHER Handles……………………………………….. PULL AND ROTATE (1-L
and 2-R) APU EMER STOP Button……PUSH IN
Fire Extinguisher APU Button…………PUSH
DUMP Button………………………………… PUSH IN ATC……………………………………………… NOTIFY
Emergency Evacuation…………………ANNOUNCE
BATT 1 and BATT 2 Knobs…………….. OFF

32
Q

Where is the battery temperature read?
Give another example of why it is always important to view the appropriate synoptic page(s) when trouble shooting a problem.

A

(27.1 NG IAS Pilot Guide Ch 7-56) 398 of 1019

MFD - Electrical System Synoptic Page

If you are trouble shooting EICAS messages, or non annunciated failures, the associated synoptic page that relates to the issue, might provide SA on where the system sensors identify an issue(s).
example - FUEL cross feed or SOV
Hydraulic System Pressure

33
Q

What CAUTION Message with populate when the Associated Battery is selected off?

A

(AOM2 14-05-45)

CAUTION - BATT 1 (2) OFF - Associated Battery is isolated from the electrical network.

34
Q

What action does the SOPM require when the cabin altitude reaches 14,500’ on an emergency descent?
SOPM Ch.5.1.7 and QRH EAP 2-1

A

SOPM ch. 5.1.7

When the cabin reaches 14,500 ft or above,

set MASKS DEPLOY knob to OVRD immediately

QRH EAP2-1

CABIN ALTITUDE HI
EICAS Indication: Cabin Altitude indication in red. Aural Warning: CABIN

Crew Oxy Masks……………………………. DON, 100% Crew Communication…………………………….. ESTABLISH Altitude…………………………………………. 10000 ft or MEA,
WHICHEVER IS HIGHER
Thrust Levers………………………………… IDLE
SPEEDBRAKE Lever…………………….. FULL OPEN Airspeed……………………………………….. MAX/ APPROPRIATE Transponder…………………………………. 7700 ATC……………………………………………… NOTIFY

35
Q

How must the MFD be configured for an emergency descent? SOPM 5.1.7

A

SOPM 5.1.7
The flight profile must be monitored and TERRAIN set on MFD, At 1,000 ft to MEA or 10,000 ft MSL, close the speed brakes and reduce to an appropriate speed.

36
Q

Is the PITCH TRIM RUNAWAY addressed by the QRC? In What Section of the QRH is it located?

A

QRC
Pitch Trim Runaway - checklist

A/P DISC BUTTON……. PRESS AND HOLD
PITCH TRIM SYS 1 and 2 CUTOUT BUTTONS…………………….PUSH IN

QRH NAP 1-15

PITCH TRIM RUNAWAY
AP/TRIM DISC Button………………………. RELEASE
WARNING: DO NOT OPEN THE SPEED BRAKE.

NOTE: Continuous turns helps to alleviate excessive pitch up tendencies.

Prepare to overcome unwanted pitch change:
Pitch Trim SYS 1 CUTOUT Button……. PUSH OUT PITCH TRIM Switch………………………… ACTUATE

AP/TRIM DISC Button……………………. PRESS AND HOLD Pitch Trim SYS 1 and SYS 2
CUTOUT Buttons………………………….. PUSH IN
PITCH TRIM NORMAL?
Yes

No
NOTE: Manual trim command through Pitch Trim Switches is available with at least one functional HS-ACE channel. With one HS-ACE channel available expect the following differences on the pitch trim indication on EICAS:
– Pitch trim readout display showing amber dashes.
– Pitch trim scale without the solid green pointer.
END

Pitch Trim SYS 1 CUTOUT Button……… PUSH IN Pitch Trim SYS 2 CUTOUT Button……… PUSH OUT

NOTE: Manual trim command through PITCH TRIM Switches is available with at least one functional HS-ACE channel.
With one HS-ACE channel available expect the following differences on the pitch trim indication on EICAS:
– Pitch trim readout display showing amber dashes.
– Pitch trim scale without the solid green pointer.
END

37
Q

How would you alleviate excessive pitch up tendencies with PITCH TRIM RUNAWAY?

A

QRH NAP 1-15

NOTE: Continuous turns helps to alleviate excessive pitch up tendencies.

38
Q

What happens to pitch rates and authority after the completion of the JAMMED CONTROL COLUMN- (PITCH)

A

QRH: NAP 1-12
Note: Expect lower pitch rates and authority

JAMMED CONTROL COLUMN (PITCH)
ELEVATOR DISCONNECT Handle….. PULL
Unrestricted Control Column……………… IDENTIFY
Maximum Airspeed…………………………… CURRENT OR 175 KIAS,WHICHEVER IS HIGHER

Unrestricted Control Column ……….. IDENTIFY
Max airspeed………………current or 175 kts whichever is higher

Note: Expect lower pitch rates and authority

Relevant Inoperative Items
AOA Limit
Autopilot

Avoid Side Slipping the airplane

Note: Stick Shaker remains operative

Landing Configuration
Slat/Flap ………………5

Set Vref = Vref full + 15 kts

Caution: Multiply the fuel flaps unfactored landing distance by 1.40 (DRY)

If a go-around is required
Slat/Flap………………….4
Airspeed………………….Vref full +15 KIAS (limited to 175 KIAS)

39
Q

In the QRH, what is the difference between a
BATT 1-2 OFF procedure, and a
BATT 1 OFF or BATT 2 OFF procedure?
What is the potential pit-fall if the wrong procedure is completed?

A

1-2 OFF Emergency - APU start not possible.
Warning Message -

1 (2) Caution Message - QRH
Unnecessary Emergency Landing.

40
Q

What does the oxygen discharge indicator look like in its normal condition?

A

Oxygen Discharge Indicator ………………….GREEN DISC

41
Q

MINIMUM / EMERGENCY FUEL TABLE
MINIMUM ……………..
EMERGENCY…………..

A

MINIMUM / EMERGENCY FUEL TABLE
MINIMUM………….. 2,250 LB - 45 Min
EMERGENCY……… 1,500 LB - 30 Min

42
Q

UPSETS

  • Pitch attitude…….
  • Pitch attitude …….
  • Bank angle…….
  • Flight within the above parameters, ……
A

UPSETS

  • Pitch attitude greater than 25 degrees nose up;
  • Pitch attitude greater than 10 degrees nose down;
  • Bank angle greater than 45 degrees; or
  • Flight within the above parameters, but at an airspeed inappropriate for the conditions.

ERJ QRC (Memory Items) (8 decks)

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