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Phenom > EMB 505 Quick Study > Flashcards

EMB 505 Quick Study Flashcards

1
Q

45 Minute IFR RESERVE

A

1121

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2
Q

Release

A

1880

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3
Q

Hot spare

A

3400

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4
Q

Emergency Fuel

A

759

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5
Q

Runway Dry Length

A

3500
Ops review if less than 4000
Wet/contaminated less than 5500
DAAP less than 4500

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6
Q

Crosswind

A

T/O
static 18
rolling 25
Landing 28
>=150 15
<150 10
Tailwind 10

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7
Q

RVSM

A

Autopilot
Alerter
Transponder
ADC x2
Pitot Heat x2

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8
Q

Max Ramp

A

18497

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9
Q

Max TO

A

18387

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10
Q

Max Landing

A

17042

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11
Q

ZFW

A

14220

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12
Q

Max Alt

A

45000

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13
Q

Flaps Max Alt

A

18000

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14
Q

OEI Icing Max Alt

A

15000

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15
Q

Max alt start TO land

A

14000

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16
Q

T/O Land in ice max Alt

A

10000

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17
Q

Min Alt

A

-1000

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18
Q

VMO

A

320

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19
Q

MMO

A

.78

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20
Q

VRA MRA

A

232/.65

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21
Q

VA

A

205

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22
Q

VLO

A

250

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23
Q

Max tire speed

A

182

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24
Q

Flaps speeds

A

180 170 160

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25
Q

Icing speeds

A

Inhibited 165
Uninhibited 150
YD off 180

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26
Q

Max diff

A

9.4

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27
Q

Max diff overpressure

A

9.6

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28
Q

Negative diff pressure

A

-0.3

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29
Q

Max diff TO/Land

A

0.2

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30
Q

How many pax O2 masks

A

7+1=8

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31
Q

Autopilot

A

TO 600/1000
Land 195/220

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32
Q

Min V battery start

A

24

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33
Q

Min GPU V to charge

A

27

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34
Q

Max amps Gen

A

390 in flight
330 on ground

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35
Q

Fuel Max

A

5401 total
220 imbalance

36
Q

Min temp to run icing system

A

landing -38C
Below 16 -40
Above 16 -45

37
Q

No autopilot

A

Ice aft of protected area
Unusual trim inputs or autopilot warnings

38
Q

Brake temp

A

20 minutes after RTO

39
Q

Approach Category

A

B unless approach speed is >120

40
Q

Baro VNAV

A

N/A above 5000

41
Q

Max thrust

A

10 minutes

42
Q

TO thrust

A

5 minutes

43
Q

MCT

A

5 minutes in level flight

44
Q

Ground Idle

A

N2
51.2 or 55.1 OEI

45
Q

Transient power

A

102 N1
103 N2
765C
20 sec

46
Q

Oil transient

A

0-20 for 20 sec
20-270 for 400 sec

47
Q

Starter cool down

A

1
1
15
30

48
Q

Evacuation

A

Thrust LP
Brakes LP
Eng stop LP
Fire shutoff LP
Press man. RP
Dump press RP

49
Q

Start Malfunction

A

Engine Stop

50
Q

Dual engine failure

A

Thrust idle
O2 masks Don
Crew comm establish

51
Q

Inadvertent pusher activation

A

Quick disconnect press and hold

52
Q

Smoke fire fume

A

O2 masks and goggles Don Emer
ADV close
Crew comm establish

53
Q

Smoke evacuation

A

O2 masks and goggles Don Emer
ADV close
Crew comm establish

54
Q

Cabin Alt Emer descent

A

O2 masks don 100%
Crew comm establish

55
Q

Dimensions

A

17’ tall
52 wide
53 long

56
Q

Main door

A

8 pins
Monitored
Vent flap makes it hard to open pressurized

57
Q

ELEC EMER button

A

Connects batt 1&2 directly to the emergency bus

58
Q

Battery Colors

A

Green 27-29
Yellow 10-27
Red 0, >40, loss of monitoring

59
Q

Batteries

A

24 VDC
Lead acid
45 minutes maximum for dual Gen fail
1-34 ah
2-36 ah

60
Q

Beacon

A

Eng start/stop in run position

61
Q

Golden CAS

A

Root cause of other messages

62
Q

Takeoff config warn

A

Flaps
Brakes
Pitch trim
Spoilers

63
Q

Stall inhibit

A

On the ground
Quick disconnect button
Above 205 KIAS
One channel inop

64
Q

Electric boost pump

A

Start
crossfeed
backup for primary ejector pump

65
Q

Crossfeed

A

Off for takeoff and landing
220 imbalance

66
Q

Engine

A

PW535E
3360 lbs thrust

67
Q

Ignition

A

Channel
A Emer bus
B DC Bus 2

1 igniter on ground
2 in the air

68
Q

Start abort

A

Hot
Hung 60 sec
No light off 10 sec

69
Q

FADEC

A

PMA powered

70
Q

ATR

A

N1 difference >20
Loss of comm between engines
Closes ECS valve when triggered
10 minute limit

71
Q

TT0 probe

A

Two temp sensors per body in each engine

Electrically heated below 10 on the ground and 15 in the air or engine heat on

72
Q

Cabin altitude high warning

A

10000 normally
11500 if in High Field mode
14200 if in even higher field mode
Climb above 25000 to cancel high field mode

High field is above 9600 Field Elevation

73
Q

Hydraulic Systems

A

Gear
Spoilers
Brakes
Pusher
SLRB

74
Q

NWS

A

20 degrees
43 degrees with brakes

75
Q

Brakes

A

Locked wheel
Anti skid
Touchdown protection
Gear retract braking
Initiated built in test

76
Q

Emer Braking

A

6 applications
No antinskid

77
Q

Pitch trim

A

3 second cutout
Trim trim trim at 4 seconds or half switch for 1 seconds
7 seconds to PTRIM Fail

78
Q

Backup Pitch trim

A

4 seconds trim trim trim
10 seconds inop and fail

79
Q

Roll and yaw trim

A

3 second timer

80
Q

Ventral rudder

A

Centers on ground
Dutch roll damp above 60 kts
Streamline if YD engaged

81
Q

Spring loaded rudder boost

A

Thrust asymmetry activated
Deactivated below 50 kts

82
Q

Speed brakes

A

Close if
flaps commanded open
Airspeed less than 125
TLAs > max crz

83
Q

Ground spoilers

A

Wow> 10 sec
3 out of 4 WOW on ground
2 WOW on one side indicate wheel spinning above 50 KTS
Retract when wheel spin <45 detected

84
Q

CVR

A

120 minutes
Starts with avionics power on
Test after 60 seconds from power on

85
Q

Static wicks

A

14

86
Q

IESI (backup instrument)

A

Power from EMER bus or DC bus 1

Phenom (1 decks)

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