Knowledge Validation Flashcards

1
Q

What is the minimum voltage for batteries 1 and 2 before start

A

22.5 V

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2
Q

What is the procedure if battery voltage is less than 21.0?

A

Write it up in the EAML as a mechanical irregularity.
DO NOT DEPART.

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3
Q

The E-PBIT is automatically peformed when an initial AC source is introduced. What actions will interrupt the test?

A

Any hydraulic pump in running.
The Flight Control Mode Panel switches are cycled.
The AC power supply is interrupted.

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4
Q

If AC power is lost, what is the procedure for reestablishing AC power?

A

Power down must be accomplished using the shutdown and leaving the airplane checklist.
Established flows, checklists, and procedures must be used to re-establish power to the aircraft.

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5
Q

BATT 1 Overtemp message populates on the EICAS with an associated triple chime and Master Warning Light, what do you do?

A

Memory Item
Battery 1 OFF
QRC
QRH
Enter Mechanical Irregularity in the EAML.
Call Maintenance Control

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6
Q

What is the Min Hydraulic Reservior Temp for engine start?

A
  • 18 Deg C
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7
Q

What is the Max Fuel capacity?

A

20,935 lbs

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8
Q

During fueling operations, a FUEL IMBALANCE caution message is presented on the EICAS, what is the Max fuel imbalance ?

A

794 lbs

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9
Q

What is the Max temperature for APU start –

A

ISA +35

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10
Q

What time period must elapse after the EICAS is energized prior to starting the APU

A

Wait 30 seconds

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11
Q

An APU FUEL SOV FAIL Caution message is displayed after the EICAS is fully energized, what do you do

A

APU Switch ON
Wait 2 seconds
APU Switch OFF
If this clears the message, it is considered a nuisance message and no write up is necessary.

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12
Q

Is it permissible to simultaneously use the APU bleed and HP cart

A

Simultaneous use of the APU bleed and the HP cart is prohibited.

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13
Q

When should the TO DATA SET MENU on the MCDU be set to ENG –

A

Between 5 deg C and 10 deg C with visible moisture, possibility of encountering visible moisture up to 1700 ft, and on contaminated ramps, taxiways, and runways where surface snow, ice, standing water or slush may be ingested, or freeze on engines, nacelles or engine sensor probes.

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14
Q

When should the TO DATA SET MENU on the MCDU be set to ALL

A

For the same above conditions when the OAT is 4 deg C and below.

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15
Q

What is the SOPM definition of “visible moisture”

A

Such as clouds, fog with visibility of one mile or less, rain, snow, sleet, ice crystals.

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16
Q

What are the Starter Cranking Limits on the ground

A

90 seconds on, 10 seconds off for starts 1 through 2.
Followed by 90 seconds on, 5 minutes off for starts 3 through 5.

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17
Q

What are the Dry Motoring Cycle Limits

A

90 seconds ON, 5 minutes OFF for first start.
Followed by 30 seconds ON, 5 minutes OFF for 2 through 5 attempts.

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18
Q

During engine start you experience a hung start, what are the indications and what action do you take

A

N1 or N2 failing to accelerate to stable idle speed.

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19
Q

What other conditions require aborting a start

A

OIL
No positive oil pressure within 10 seconds after N2 increase. Oil pressure stabilizes below engine limits.

ITT
No ITT indication within 30 seconds
ITT Exceeds start limit 815 deg C.

N1/ N2
N1 or N2 fail to accelerate and stabilize at idle speed. HUNG START
With a tail wind, when a positive N1 is not indicated prior to starter cutout 50% N2.

An intermittent electrical or pneumatic or starter malfunction occurs before the starter cutout.

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20
Q

At idle engine thrust, the engine exhaust danger area can extend to approximately 90 feet behind the aircraft with a jet blast velocity reaching

A

greater than 65 mph

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21
Q

A NOTAM prohibits taxiway usage to aircraft with a wing span of greater than 100 ft, what is the wing span of the ERJ 175

A

Wingspan 93 ft 11 inches

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22
Q

What are the Max taxi speeds on dry surface conditions (straight/turns)

A

Straight - Dry - 30 kts
Turns - Dry 10 kts

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23
Q

What are the Max taxi speeds on wet or contaminated surface conditions (straight/turns)

A

Straight - Wet or Contaminated - 10 kts
Turns 5 kts

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24
Q

If the nosewheel deflects partially or fully uncommanded, what is the memory item –

A

Memory Item:
Nose Wheel Steering Disconnect Switch - Press
Steer the aircraft using differential braking and rudder.

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25
When is the use of FLEX Thrust for takeoff prohibited? Name all three conditions
Takeoff on contaminated Runway Reported or Forecaset Windshear When a special departure procedure specifies full thrust for takeoff.
26
What is the memory item if the nosewheel deflects partially or fully uncommanded?
Memory Item: Nose Wheel Steering Disconnect Switch - Press Steer the aircraft using differential braking and rudder.
27
When is the use of FLEX Thrust prohibited for takeoff? Name all three conditions.
Takeoff on contaminated Runway Reported or Forecaset Windshear When a special departure procedure specifies full thrust for takeoff.
28
What is the Max Takeoff Weight for the ERJ 175LL and LR?
ERJ 175 LL = 85,098 ERJ 175 LR = 85,517
29
At what crosswind velocity are static takeoffs not recommended and why?
crosswind greater than 25 kts due to possibility of compressor stall.
30
What is the maximum crosswind limit for takeoff on a dry runway?
Take Off: 38 KTS Landing: 38 KTS
31
What is the maximum crosswind component for takeoff on a runway contaminated with compacted snow?
Take Off: 20 KTS Landing: 20 KTS
32
The landing gear must be retracted by what Vspeed? V le ret
250 kts
33
During takeoff the airplane pitches up un-commanded and a trim runaway is suspected. What is the memory item?
Memory Item: Auto Pilot Disconnect Press and Hold Pitch Trim Disconnect 1 and 2 Press
34
Crews should not manually select CLB 1 unless...
Directed by Departure Procedure or Operationally needed for safety of flight.
35
During Climb, traffic preceding you reports moderate turbulence ahead at 7000 ft. What speed would be appropriate to fly?
250 kts
36
Describe the ROLL trim runaway, what is the memory item?
AutoPilot Disconnect - Press and Hold Proceed with NAP Procedure
37
The Roll Axis is jammed. What is the memory item?
Aileron Disconnect Handle ---- PULL Proceed with NAP procedure
38
What if the pitch axis is jammed? What is the memory item?
Elevator Disconnect Handle --- PULL
39
What is the max altitude for the APU bleed use?
15,000 ft
40
What is the max operational altitude of the ERJ 175?
FL 410
41
With the IDG OFF BUS EICAS message, the QRH says APU as required. If you choose to start the APU at cruise, what altitude do you have to be below?
30,000 ft - max APU start altitude
42
The left Pack fails in cruise at FL330. The issue is not resolved by the QRH procedure. What is the max altitude under this condition?
FL 310 - Max Single Pack Ops
43
Icing conditions exist in flight when in visible moisture and what temperature?
10 degrees C and below to -40 DEG C
44
The EICAS shows a CABIN ALT HIGH message. What do you do?
Oxygen Masks: DON 100% Crew Communication Establish
45
What if instead of the above message, you had strong FUMES in the flight deck, maybe an electrical smell?
Oxygen Masks: DON 100% Crew Communication Establish
46
If Smoke filled the flight deck, what would you do?
Oxygen Masks: DON EMERGENCY Crew Communication Establish Pressurization DUMP: Push In
47
During descent you encounter moderate turbulence through FL 280. What speed would be appropriate?
270 KTS
48
What is the Max altitude permitted to fly with flaps slats extended?
20,000 ft.
49
The descent is conducted in light rain, what is the max wiper speed?
250 Kts
50
Is it permissible to utilize the LP minimums for a straight in approach?
NO LP Minima are NOT authorized.
51
CAT II minimums limitations regarding DA.
RA NOT AUTH minima are NOT authorized.
52
If conducting a Flaps Full approach, what is the go around flap setting?
Flaps 4
53
What is the stabilized approach criteria at 1000 HAT for a straight in approach?
At 1,000 ft HAT / RA: IAP at 1000’ HAT 1. Final landing configuration 2. BEFORE LANDING CHECKLIST Complete 3. Airspeed within +15 and -5 kts of VAP 4. On lateral profile (Visual +/- 10 deg Centerline) 5. On vertical profile or correcting with minor bracketing maneuvers (Visual On Glide Path) Visual: Sink Rate no greater than 1000 fpm. PM announce deviations: Airspeed or Sinkrate
54
What is the stabilized approach criteria at 500 ft HAT for a straight in approach?
Airspeed within the bug with adjustments for gust factor. Thrust Levers above Idle. Except for momentary airspeed and descent fluctuations, any unstable condition or any EGPWS notification below 500 HAT requires a missed approach. "UNSTABLE GO AROUND"
55
What is the max landing weight?
74,957 lbs
56
What is the min runway width for landing?
100 ft 80 ft cleared
57
RCCs of 3 are reported. What is the max crosswind component for landing?
15 Kts
58
Is it permissible to land with a FUEL IMBALANCE EICAS message? If so, under what conditions?
It is permissible to takeoff and land with a FUEL IMBALANCE EICAS message as long as the actual imbalance does not exceed 794 lbs.
59
What is required to move the thrust levers into the forward thrust range after using reverse thrust?
After selecting reverse thrust, do not move the thrust levers into the forward thrust range until the REV icon on the EICAS is shown in amber or green.
60
Height of Rudder / Vertical Stabilizer
32 ft 4 inches
61
If landing below -40 deg C, what is the crew required to accomplish prior to Flight View Closeout?
Write up in EAML.
62
794
63
What is the Minimum temperature for APU Start?
-54 dec C
64
Wet Runway Definition
A runway is wet when it is neither dry nor contaminated. Wet when more than 25% of the surface area is covered by any visible dampness or water 1/8th inch or less in depth.
65
Contaminated Runway Definition
Contaminated when more than 25% of the surface area is covered more than 1/8th inch water or equivalent in slush, wet snow, dry snow, or any depth of ice or compacted snow.
66
FADEC automatically aborts the start for the following:
HOT START Hung START based on acceleration rate. No Light Off 15 seconds Ignition A then 15 seconds for Ignition B.
67
FADEC automatically aborts for hot start when the temperature is within. ----- degrees of the limit?
10 deg C
68
Stabilized Approach Criteria 1500 ft
IAP: By 1,500 ft HAT / RA or the FAF, whichever occurs FIRST: 1. Landing gear down 2. Flap 3 3. Airspeed no greater than 180 KIAS Visual Approach: By 1500 ft HAT: 1. Landing gear down 2. Flap 3 3. Airspeed no greater than 180 KIAS
69
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