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RYAN E175 GROUND SCHOOL > Safety and Power up Checklist > Flashcards

Safety and Power up Checklist Flashcards

1
Q

When must the Safety and Power up checklist be performed?

A

First Flight of Day (FFOD)

or

when a power down was required

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2
Q

When recieving an aircraft already powerd up you must?

A

verify compliance with all items and perform

Fire Extinguisher panel check

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3
Q

What flight deck emergency equipment items should be checked during safety and power up checklist?

A

DOOR WAY -

  1. (1) PBE check seal integrity
  2. (1) Halon fire extinguisher pressure green, pin installed
  3. 1 crash axe

CAPTAINS SIDE

  1. FLASHLIGHT LED FLASHING
  2. LIFE VEST SEAT BACK POCKET
  3. JUMPSEAT LIFE VEST SEAT BACK POCKET
  4. CIRCUIT BREAKERS CLOSED OR COLLARED
  5. ESCAPE ROPE CHECK

FIRST OFFICERS SIDE

  1. FLASHLIGHT LED FLASHING
  2. CIRCUIT BREAKERS CLOSED OR COLLARD
  3. LIFE VEST (1) IN SEAT BACK POCKET
  4. ESCAPE ROPE CHECK
  5. LANDING GEAR AND RAT PINS ONBOARD

OBSERVER SEAT

  1. OBERVER SEAT SECURE
  2. OBSERVER o2 CHECKED
  3. OBSERVER HEADSET CONDTION
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4
Q

Where are the required documents and equipment found?

A

Flight deck documents/equipment list,

EFB company manuals application

When a document or equipment is missing the PIC must obtain a replacement.

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5
Q

After power up and IESS intialization, how long must the aircraft remain unmoved.

A

90 seconds

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6
Q

Intial power up, BATT 1 on / BATT 2 auto. more than displays 2 and 3 are available. What must be done?

A

call MX. no dispatch

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7
Q

What display and page are the battery voltages checked?

A

MFD/ Status

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8
Q

Battery voltage between 21.0v and 22.5v

A

Use SOPM Table for charging time by tempature

recharge batteries prior to takeoff through any AC source (includes engines during taxi)

Battery temp > = 0* c 30 min charge

Battery temp > = -5c and < 0*c 35 min charge

Battery temp > = -10c and < 5*c 40 min charge

Battery temp, < -10c 50 min charge

voltage below 21.v report ireggularity Do not Depart

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9
Q

What should be verified before pushing the test button on the fire extinguisher panel?

A

no fire protection fail messages on EICAS

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10
Q

What indications are present/checked during the fire extinguisher panel test?

A

6 Lights on overhead panel

5 EICAS Messages

2 ITT FIRE Warnings

2 MASTER WARNINGS

2 AURAL Alerts - Triple Chime and fire bell

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11
Q

To avoid Battery Depletion?

A

Establish AC power ASAP

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12
Q

When Display units 2 and or 4 are configured as PFDs.

How do you set 2 and 4 back to MFD.s?

A

Use the Revisionary panel selector

set respective knob to MFD then to Auto.

After 8 secs the affected display config returns to MFD display.

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13
Q

When are the NAV and LOGO lights turned on?

A

NAV after power is established, LOGO after power established at night.and also all operations under FL180 at night.

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14
Q

When is the APU started?

A

10 min prior to pushback

unless required for passenger comfort

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15
Q

To allow flight control built in test (PBIT) to complete, How long after power up can any hydraulic pump be turned on?

A

3 minutes

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16
Q

If Electrical PBIT is interrupted what message appears?

A

FLIGHT CONTROL NO DISPATCH

CAUTION MESSAGE IN EICAS

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17
Q

How do you clear a

FLIGHT CONTROL NO DISPATCH

EICAS CAUTION MESSAGE

A

Power down the airplane, wait at least one min

then power up

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18
Q

Before selecting ground power (pushing the GPU button in) What is done?

A

Verify,

Available light,

on GPU button is illuminated

19
Q

What do you do to the GPU Button if Ground power is not available?

A

Verify

GPU BUTTON

OUT

20
Q

If AC power is lost, what is accomplished?

A
  1. shut down via leaving the Airplane checklist
  2. re-power via Safety and power up checklist
21
Q

Prior to APU start, what positions should BAT 1(2) be in

A

BAT 1 - on / BAT 2 Auto

22
Q

How do you transfer AC power source from External to APU?

A
  1. APU GEN Button IN
  2. GPU switch/light AVAIL
  3. GPU Button OUT
23
Q

How is AC power transferred from APU to gound power (EXternal)?

A

GPU switch/light AVAIL illuminated,

GPU button IN

APU shutdown.

24
Q

What will improve cockpit and cabin cooling on ground?

A
  1. AIR COND RECIRC IN
  2. TEMP CONTROLLERS COLD
  3. DOORS AND WINDOWS CLOSED
  4. PASSENGER CABIN GASPERS OPEN
  5. WINDOW SHADES CLOSED EXPOSED SIDE
25
Q

What will/may happen if the PACKS and ground air are used simultaneously?

A

AIR conditioned pressure may become excessive.

26
Q

(PBIT) consists of two different tests?

A

Electrical (E-BIT)

Hydraulic (H-BIT)

27
Q

When is the E-PBIT automatically performed.

A
  1. Automatically after power up by intial AC source
  2. takes plus or minus 3 minutes to complete
28
Q

What will interrupt the “E-PBIT” test

A

3x3

  1. any hydraulic pump running,
  2. Flight control mode panel switches are cycled,
  3. AC power interruption
29
Q

What is displayed if the EBIT test is inturrupted?

A

FLIGHT CONTROL NO DISPATCH

EICAS MESSAGE

30
Q

When PBIT is in process, What EICAS is displayed?

A

FLT CTRL TEST IN PROG

31
Q

When is the H-PBIT test performed.?

A

All three hydraulic systems are pressurized.

Hydaulic systems are pressurized in order 3,1,2

32
Q

What will interrupt the “H-BIT” test?

A

1x1

Movement of any flight control surface

33
Q

What does the FLT CTRL BIT EXPIRED, EICAS message mean?

A

If the last successful PBIT test was more than 50 hrs old.

34
Q

Where can the elapsed time between PBITs be found (display/page)

A

FLT CTRL synoptic page

35
Q

FLT CTRL BIT EXPIRED message remains after completion of

E-BIT Or E-BIT is intrurrputed. About to expire or Expired.

What should flight crew do?

A
  1. Power Down using Leaving the Airplane Checklist
  2. Wait a min of 1 minute
  3. Power up using Safety and Power up Checklist
  4. Wait 3 min for E-BIT to run
  5. Perform H-BIT if required
36
Q

FLT CTRL BIT EXPIRED

message remains after completion of

H-BIT Or H-BIT is intrurrputed. About to expire or Expired.

what should flight crew do?

A

Perfom appropriate PBIT as outlined on 4-1-12 of he ERJ SOPM

  1. Do not move any flight controls
  2. Confirm STEER OFF EICAS message illuminated

IF STEER OFF not illuminated Press steer disengage switch

If STEER OFF is illuminated Procced to step 3

  1. Select HYD Synoptic page confirm all three hydraulic systems below 250psi and reservoir temp above +10c
  2. Turn Electrical hydraulic pumps 1,2,3a, on
  3. wait 60 sec
  4. VERIFY FLT CTRL BIT EXPIRED message extinguishes
  5. Turn Electrical HYD pumps 1, 2 to auto, 3A, off
37
Q

When must the hydraulic systems warm-up procedure be accomplished?

A

Before starting the engines when the reservoir temperatures are below -18*c

38
Q

How do you accomplish the HYDRAULIC SYSTEMS WARM-UP

A

Use QRH or SOPM?

39
Q

What would cause an airspeed to be displayed on the PFD following (usually the first) power up?

A

Frozen moisture inside the ADSPs

40
Q

What EICAS messages will/could be associated with an erroneous airspeed on the PFD on the ground?

A

ANY OR ALL

  1. AFCS FAULT
  2. AT FAIL
  3. AP FAIL
  4. FD FAIL
  5. YD FAIL
  6. APPR 2 NOT AVAIL
  7. ADS messages on EICAS
41
Q

When must the Air Data Smart Probe (ADSP) heater procedure be accomplished?

A

First flight of the day (FFOD)

OATs below -18*c (0*f)

  1. ADSP heat ON
  2. PBIT COMPLETED (3min to complete)
  3. Verify clock on Flight Control Synoptic page resets to 50 hours
  4. IF PBIT does not run or PBIT countdown clock fails to reset
  5. After any ice in smart probes has had a chance to melt power down, wait 1 min, power up using normal procedure
  6. Flight Control PBIT should run properly

VERIFY

  1. no airspeed data is displayed on both PFDs
  2. all EICAS messages cleared
  3. ADSP Heat OFF
42
Q

If ADSP heater procedure does not clear spurious AFCS

(PFD) and ADS EICAS messages, what must be done?

A

call MX control

43
Q

When a RAM AIR FAULT advisory message remains for more than one minute after power up.

What is the clearing procedure?

A
  1. PACK 1 and PACK 2 PUSH OUT wait 5 secs
  2. PACK 1 and PACK 2 PUSH IN
  3. Fault message is considered nuisance no further action if message clears
  4. Message does not clear. Considered actual RAM AIR failure
  5. report to maint.

RYAN E175 GROUND SCHOOL (21 decks)

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