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SF50 > SF50 > Flashcards

SF50 Flashcards

1
Q

Vo

A

150 KIAS

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2
Q

Scoreboard is …

A

KING!

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3
Q

Sterile cockpit in …

A

critical phases of flight (10k)

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4
Q

Flaps Up G Limits

A

+3.6g, -1.44g

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5
Q

Flaps 50% G Limits

A

+2g, 0g

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6
Q

Flaps 100% G Limits

A

2g, 0g

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7
Q

Takeoff Temp Limits

A

+50C, -40C

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8
Q

General Operating

A

50C, -63C (FL 310)

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9
Q

Fuselage Design / Construction

A

Carbon fiber, one piece pressure vessel

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10
Q

Wings Design / Construction

A

Carbon fiber, two main spars, wet wing, aluminum flight controls

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11
Q

Landing Gear

A

Tricycle gear, aluminum

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12
Q

Engine Mount

A

Pylon

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13
Q

Engine Type

A

Williams FJ33-5A

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14
Q

Engine Thrust

A

1846 lbs

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15
Q

Engine Nacelle

A

Fiberglass cover

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16
Q

Engine Pylon

A

Raised mount

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17
Q

Nav lights controlled by

A

Bat 1

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18
Q

Landing Light Switch

A

Leave on 24/7

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19
Q

Wingtip Lights Pattern

A

Alternates in flashing patter at 500ft AGL

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20
Q

Hot Bus Battery

A

Bat 1

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21
Q

Main Cabin Door

A

Clamshell; pressure vessel

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22
Q

Preferred Exit In Water

A

Egress door

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23
Q

Required Seats To Fly

A

Seats 1 & 2

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24
Q

When 6 and 7 Are Occupied, Where is Seat 4

A

Fully aft

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25
Q

Baggage Weight Limit

A

300 lbs

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26
Q

X-Tend Weight Limit

A

40 lbs (implies 260 for main)

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27
Q

Control Summary

A

Manual for pitch, roll, and yaw. Forces transmitted via cables, pulleys, bellcranks, pushrods

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28
Q

Left Aileron Tab

A

Trim Tab

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29
Q

Right Aileron Tab

A

Balance Tab

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30
Q

Two Yaw Systems

A

Yaw SAS and Yaw Damper

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31
Q

Yaw Damper Purpose & Engagement

A

Turn Coordinator; 200 AGL

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32
Q

Yaw SAS Purpose & Engagement

A

Reduce dutch roll (longitudinal stability); weight on wheels sensor

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33
Q

100% Flaps Crosswind

A

16 knots

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34
Q

50% Flaps Crosswind

A

18 knots

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35
Q

0% Flaps Crosswind

A

Not demonstrated

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36
Q

Trim Runaway Indication

A

CAS Warning, Trim Indicator

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37
Q

Trim Runaway Memory

A

Hold; AP disconnect; control; A3; AP release

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38
Q

Type of flaps

A

Fowler (travel aft and down); no need for slots because we’re not producing as much drag

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39
Q

Deflection for 50% flaps and 100% flaps

A

50% - 15 degrees; 100% - 40 degrees

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40
Q

Only Approved TO Flaps

A

50%

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41
Q

Flaps Actuation

A

Single piece torque tube; electro-mechanical actuator

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42
Q

Vfe 100%

A

150 KIAS

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43
Q

Max Flap in Icing

A

50%

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44
Q

Vfe 50%

A

190 KIAS

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45
Q

Terminal Area Speed (AT) Speed

A

180 KIAS

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46
Q

50% Flaps Speed (AT) Speed

A

140 KIAS

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47
Q

100% Flaps Speed (AT) Speed

A

95 KIAS

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48
Q

Climb (AT) Speed

A

165 KIAS

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49
Q

Cruise (AT) Speed

A

245 KIAS / 0.525

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50
Q

Holds (AT) Speed

A

160 KIAS

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51
Q

Avionics

A

2 GIAS/IAUs, 2 ADCs, 2 ADHRS, 3 GRCs, MFD, PFD, GMA36, GFC 700 w/ 707 Mode Controller

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52
Q

Changeover Point to Mach

A

18,300 ft

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53
Q

RAGL Height

A

2500

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54
Q

Reminder: Switch NAV Modes As Needed

A

Magenta vs green

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55
Q

How to get runway remaining

A

Surfacewatch! (Lower left PFD)

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56
Q

VNAV Acronym

A

Build, Bug (lowest cleared), Button, Brief It

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57
Q

VNAV Traps

A

Changing runway blows up Creates; VS down if above;

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58
Q

GIA Failure Indication

A

No CAS; Christmas Tree

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59
Q

Action For Any Miscompare

A

Display Backup

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60
Q

“Join the locailizer”

A

NAV

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61
Q

“Cleared … “ button

A

APR

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62
Q

FLC Descent (engine fire)

A

AT Man first

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63
Q

Missed / Go Around Trap

A

Call Tower with Go Around

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64
Q

Trick for GoAround FLC

A

Wait until 165 to hit FLC

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65
Q

ESP Armed

A

> 200ft

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66
Q

ESP Roll

A

At 45 degrees, rolls to 30 degrees

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67
Q

ESP Pitch

A

At Vmo + 6 KIAS, pitch up

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68
Q

LVL vs Autolevel

A

Normal button vs exceeding normal flight envelope for 50% of the last 40 seconds.

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69
Q

Safe Return automatically activates?

A

Autolevel for 1 minute
Passing 15,000 ft in EDM mode
Button

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70
Q

Emergency Descent Mode Activates

A

1) AP on 2) PA > 14,900 ft 3) Cabin pressure >15,000 4) Cabin Dump switch not pressed

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71
Q

Emergency Descent Mode goes to

A

14,000 ft

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72
Q

How to deactivate EDM mode

A

AP DISC; cabin dump

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73
Q

CAPS mode

A

Pitch up, reduce thrust to idle, wings level. No deceleration in 8 seconds, will deploy. After 30 seconds, will deploy. <135

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74
Q

RVSM Airspace

A

FL 290

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75
Q

AFCS Limitations - Min Speeds and Max

A

Up - 105 KIAS; 50% - 95 KIAS; 100%.- 85 KIAS. Max - Vmo Mmo

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76
Q

AFCS AGL

A

1000 visual; 400 non-precision; 200 precision

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77
Q

AFCS Required

A

RVSM

78
Q

CAS - STALL WARNING

A

Reduce AOA (-10 degrees); Thrust TO; recover (5 degrees)

79
Q

PLI

A

Pitch Limit Indicator

80
Q

Stall Procedure

A

Recover, Start A Climb, Clean Up, Level Off

81
Q

Stick Pusher Inhibits

A

1) Below 500 AGL 2) Above 160 KIAS 3) 35 seconds after takeoff 4) On the ground

82
Q

FALSE AOA

A

High AOA but … airspeed is high enough

83
Q

Auto Fuel Switch

A

Every 2 gallons

84
Q

Fuel Low Yellow Threshold

A

<25 gal in either, or <50 total

85
Q

Fuel Low Red

A

<5 gal on either, or <25 gal

86
Q

Fuel Imbalance Limits

A

15 gal for advisory; 50 gal roll control

87
Q

Fuel Types

A

Jet A, Jet A-1, JP-8

88
Q

Min / Max Fuel Temp

A

-40C / 50C

89
Q

When fueling, max imbalance

A

75 gallons

90
Q

GEN 1 Volt / Amp

A

27.8V / 270

91
Q

GEN 2 Volt / Amp

A

28.7V / 76

92
Q

BAT 1 & 2 … Volt / Amp

A

26.4V / 17 amp hour

93
Q

BAT 1 / BAT 2 Location

A

Under floor in baggage; Nose

94
Q

EMER Power from BAT 1

A

60 min

95
Q

Ground Power

A

28 volts; 1000 amps

96
Q

How many ciruit breaker panels?

A

5 … 2 cabin, 1 nose, 2 baggage

97
Q

N1 / N2 RPM

A

22k rpm / 50k rpm

98
Q

Full Line Oil

A

2.2 qts

99
Q

Idle N2 %

A

53%

100
Q

Compressor stall vs surge

A

local disruption vs reversal

101
Q

FADEC airstart attempts

A

3 lights

102
Q

Gear handle down does what to igniters?

A

One ignitor fires

103
Q

FADEC Switch When?

A

When N2 Drops Below 24%

104
Q

Jet Stages

A

Suck, squeeze, bang, blow; compression, combustion, expansion, exhaust

105
Q

4 Things Powered By Gear Box

A

FCU, Gen 1, Gen2, Oil Pump

106
Q

Powerplant

A

FJ33-5A, medium bypass, FADEC controlled

107
Q

Engine Thrust

A

1846 lbs

108
Q

Types N1 compressor

A

Axial, 3 stage

109
Q

Two types of oil

A

Mobile Jet II or Mobile 254

110
Q

Bleed Ports Use

A

(1) IPS (2) ECS

111
Q

Probes

A

PT2; TT2

112
Q

FADEC adjusts based on

A

Thrust, ambient air, engine condition

113
Q

FADEC powered by

A

PMA at N2 > 50%

114
Q

Min Oil Temp

A

40C

114
Q

WOW Sensor

A

(1) Ground idle (2) Gear Retraction (3) Ground Fan (4) Outflow Valves (5) Probe Heat (6) Yaw SAS (7) Flight timer (8) Radar (9) Airport Diagram

115
Q

Max Crosswind For Start

A

25 kts

116
Q

Max Tailwind For Start

A

15 kts

117
Q

Titanium Firewall Specs

A

2000 degrees for 15 minutes

118
Q

Fuel Ack Switch Actions

A

1) FSV 2) Aural 3) Arms Halon

119
Q

Thrust Cheats

A

25% = 140 kts clean
30% = GP/GS Full Config
45% = MDA level off

120
Q

What holds gear in place?

A

Over Center Locking Links

121
Q

Main Gear Description

A

Trailing Link, Oleo Strut, Berringer Brakes

122
Q

Nose Gear Description

A

Free castering. oleo strut, self centering

123
Q

Landing Gear Description

A

Tricycle, Retractible, Hydraulically Powered

124
Q

Gear Travel

A

8 seconds

125
Q

Gear Up Speed

A

150 KIAS

126
Q

Gear Down Speed

A

210 KIAS

127
Q

Landing Gear Takes How Long To Show CAS

A

30 sec

128
Q

Landing Gear Limitation

A

8 cycles per 30 minutes
Minimum 10 seconds rest

129
Q

High Energy Event Limitation

A

30 minute cool down. (Flaps up, ice landing, HDA)

130
Q

Probe Heat Limitations

A

Max five min on ground if above 5C

131
Q

What turns on with Engine IPS

A

Bleed air to d ring; PT2TT2

132
Q

Engine IPS When?

A

Below 5C and visible moisture. OR, first signs of ice.

133
Q

Engine IPS Limitations

A

Max Temp 10C; engine must be running

134
Q

IPS Boot Cycles

A

6 tail, 6 bottom, 6 top; 42 second dwell

135
Q

When Boot On?

A

First sign of ice.

136
Q

Boot Limitations

A

Non-RVSM; min -40; not for T/O; STALL SPEED HIGH (Vref 5-10 kt higher, max 50% flaps … Vref = 1.5 Vso)

137
Q

Windshield IPS Cycles

A

1 pump 4 sec / min; 1 pump 4 sec; 2 pumps on demand

138
Q

Windshield IPS When?

A

When leading edges start to accumulate?

139
Q

Windshield IPS Limitations

A

Off 2 min before landing, min temp 30C, not on TO, max 3 gallons (27 lbs), min 1 gal dispatch

140
Q

Windshield IPS duration

A

270 min on NORM; 135 min on HIGH

141
Q

Windshield IPS MAX

A

50% duty cycle up to 10 seconds

142
Q

What controls the PRSOV?

A

Bleed/Fresh Air

143
Q

Warm Air Config

A

TCV Closed. FCV High Flow

143
Q

How do you get pressurized air into cabin?

A

N2 Bleed Port, through PRSOV, through heat exchanger, through FCV, to pressure vessel (defog and cabin plenums); two outflow valves, one CPCS controller (pneumatic), and two static ports

144
Q

Cool Air Config

A

TCV Open, FCV Low Flow

145
Q

Location of temperature sensors for ECS

A

Copilot speaker, above seat 4

146
Q

AC System

A

Compressor, scoop (fan on ground), and NLG (nose gear); refrigerant to pressure vessel; two evaporators driven by cabin fan (foot intake and vent output)

147
Q

Fresh Air Path

A

Check valve needs no bleed air pressure and no pressure vessel pressure in order to pass the check valve

148
Q

N2 Compressor Type

A

Centrifugal

149
Q

Max Differential

A

7.1psi

150
Q

Cabin Dump Actions

A

Disables CPCS and opens outflow valves; can be reactivated by pressing dump a second time; activating disables Emer Descent

151
Q

Full cold / full hot target

A

65-85%

152
Q

ECS Disable

A

AC Off, Defog Selected, TCV Full Open, FCV To Low

153
Q

Target CPCS Pressure Change

A

600 fpm change; scaling to LFE by 1500 AGL

154
Q

High Field Elevation Indication

A

After T/O, will pressurize to 8k ft. When landing, takes above 8k below 23500

155
Q

CAS Message / Synoptic

A

Open appropriate synoptic

156
Q

Ramp Weight

A

6,040 lbs

157
Q

MTOW

A

6,000 lbs

158
Q

Landing Weight

A

5,550 lbs

159
Q

Zero Fuel

A

4,900 lbs

160
Q

Baggage

A

300 lbs (40 lbs xtend)

161
Q

Pressure Altitude Math

A

29.92 minus Current = X * 1000

162
Q

Performance Charts - Remember

A

Pressure Altitude Conversion!

163
Q

Takeoff Grey Cells vs Landing Grey Cells

A

Not Demonstrated vs Not Possible (balked landing)

164
Q

MEL Location

A

Has to be on the aircraft.

165
Q

NEF Defn

A

Non Essential Furnishings

166
Q

MEL Procedure

A

Identify, consult, comply, log, keep limitations in mind

167
Q

CAPS Threshold

A

135 IAS / 145 TAS

168
Q

CAPS Submode

A

1) Idle 2) Level 3) Pitch Up

169
Q

Two G Forces CAPS Components

A

Disreef Ring; Snubline

170
Q

Immediate CAPS pull

A

Loss of Control, Midair, Disorientation, 600-2000

171
Q

EDM will level where?

A

14k

171
Q

GPS For Dispatch? (Outage)

A

Required

172
Q

DeIce Fluid

A

Type 1 (Not Type 4)

172
Q

Gallons between MTOW and MLW

A

67 gal

173
Q

Passenger Briefing

A

Buckle Up, Egress, Smoking, Fire Ext, O2, Safe Return, CAPS

174
Q

140 kts Clean (Thrust)

A

25%

175
Q

O2 Requirements

A

10 minutes for every pax above FL250

176
Q

MAch Formula

A

True Airspeed / Speed of Sound

177
Q

Vmo

A

250 KIAS

178
Q

Mmo

A

0.53

179
Q

When does Mach change?

A

18,300

180
Q

CAT Stronger On

A

North Side of Jet Stream

181
Q

Four Types of Hypoxia

A

Hypoxic, Hypemic, Stagnant, Histotoxi

182
Q

O2 Auto Deploy

A

15,000

183
Q

O2 System

A

Master (PRSOV), Burst Disc, Outlets, PAX (6) Deploy

184
Q

STAR Clearance

A

Need to hear “VIA” to follow altitude

185
Q

Missed Approach Sequence

A

Click, Clean, Configure, Clean, Communicate

186
Q

RVSM Requirements

A

(1) Alt Reporting Transponder (2) Independent Primary Altimeters (1) Autopilot (1) Alt Alerting system

187
Q
A

SF50 (3 decks)

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