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
Icing speeds
Inhibited 165 Uninhibited 150 YD off 180
26
Max diff
9.4
27
Max diff overpressure
9.6
28
Negative diff pressure
-0.3
29
Max diff TO/Land
0.2
30
How many pax O2 masks
7+1=8
31
Autopilot
TO 600/1000 Land 195/220
32
Min V battery start
24
33
Min GPU V to charge
27
34
Max amps Gen
390 in flight 330 on ground
35
Fuel Max
5401 total 220 imbalance
36
Min temp to run icing system
landing -38C Below 16 -40 Above 16 -45
37
No autopilot
Ice aft of protected area Unusual trim inputs or autopilot warnings
38
Brake temp
20 minutes after RTO
39
Approach Category
B unless approach speed is >120
40
Baro VNAV
N/A above 5000
41
Max thrust
10 minutes
42
TO thrust
5 minutes
43
MCT
5 minutes in level flight
44
Ground Idle
N2 51.2 or 55.1 OEI
45
Transient power
102 N1 103 N2 765C 20 sec
46
Oil transient
0-20 for 20 sec 20-270 for 400 sec
47
Starter cool down
1 1 15 30
48
Evacuation
Thrust LP Brakes LP Eng stop LP Fire shutoff LP Press man. RP Dump press RP
49
Start Malfunction
Engine Stop
50
Dual engine failure
Thrust idle O2 masks Don Crew comm establish
51
Inadvertent pusher activation
Quick disconnect press and hold
52
Smoke fire fume
O2 masks and goggles Don Emer ADV close Crew comm establish
53
Smoke evacuation
O2 masks and goggles Don Emer ADV close Crew comm establish
54
Cabin Alt Emer descent
O2 masks don 100% Crew comm establish
55
Dimensions
17’ tall 52 wide 53 long
56
Main door
8 pins Monitored Vent flap makes it hard to open pressurized
57
ELEC EMER button
Connects batt 1&2 directly to the emergency bus
58
Battery Colors
Green 27-29 Yellow 10-27 Red 0, >40, loss of monitoring
59
Batteries
24 VDC Lead acid 45 minutes maximum for dual Gen fail 1-34 ah 2-36 ah
60
Beacon
Eng start/stop in run position
61
Golden CAS
Root cause of other messages
62
Takeoff config warn
Flaps Brakes Pitch trim Spoilers
63
Stall inhibit
On the ground Quick disconnect button Above 205 KIAS One channel inop
64
Electric boost pump
Start crossfeed backup for primary ejector pump
65
Crossfeed
Off for takeoff and landing 220 imbalance
66
Engine
PW535E 3360 lbs thrust
67
Ignition
Channel A Emer bus B DC Bus 2 1 igniter on ground 2 in the air
68
Start abort
Hot Hung 60 sec No light off 10 sec
69
FADEC
PMA powered
70
ATR
N1 difference >20 Loss of comm between engines Closes ECS valve when triggered 10 minute limit
71
TT0 probe
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
Cabin altitude high warning
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
Hydraulic Systems
Gear Spoilers Brakes Pusher SLRB
74
NWS
20 degrees 43 degrees with brakes
75
Brakes
Locked wheel Anti skid Touchdown protection Gear retract braking Initiated built in test
76
Emer Braking
6 applications No antinskid
77
Pitch trim
3 second cutout Trim trim trim at 4 seconds or half switch for 1 seconds 7 seconds to PTRIM Fail
78
Backup Pitch trim
4 seconds trim trim trim 10 seconds inop and fail
79
Roll and yaw trim
3 second timer
80
Ventral rudder
Centers on ground Dutch roll damp above 60 kts Streamline if YD engaged
81
Spring loaded rudder boost
Thrust asymmetry activated Deactivated below 50 kts
82
Speed brakes
Close if flaps commanded open Airspeed less than 125 TLAs > max crz
83
Ground spoilers
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
CVR
120 minutes Starts with avionics power on Test after 60 seconds from power on
85
Static wicks
14
86
IESI (backup instrument)
Power from EMER bus or DC bus 1