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
Baggage Weight Limit
300 lbs
26
X-Tend Weight Limit
40 lbs (implies 260 for main)
27
Control Summary
Manual for pitch, roll, and yaw. Forces transmitted via cables, pulleys, bellcranks, pushrods
28
Left Aileron Tab
Trim Tab
29
Right Aileron Tab
Balance Tab
30
Two Yaw Systems
Yaw SAS and Yaw Damper
31
Yaw Damper Purpose & Engagement
Turn Coordinator; 200 AGL
32
Yaw SAS Purpose & Engagement
Reduce dutch roll (longitudinal stability); weight on wheels sensor
33
100% Flaps Crosswind
16 knots
34
50% Flaps Crosswind
18 knots
35
0% Flaps Crosswind
Not demonstrated
36
Trim Runaway Indication
CAS Warning, Trim Indicator
37
Trim Runaway Memory
Hold; AP disconnect; control; A3; AP release
38
Type of flaps
Fowler (travel aft and down); no need for slots because we're not producing as much drag
39
Deflection for 50% flaps and 100% flaps
50% - 15 degrees; 100% - 40 degrees
40
Only Approved TO Flaps
50%
41
Flaps Actuation
Single piece torque tube; electro-mechanical actuator
42
Vfe 100%
150 KIAS
43
Max Flap in Icing
50%
44
Vfe 50%
190 KIAS
45
Terminal Area Speed (AT) Speed
180 KIAS
46
50% Flaps Speed (AT) Speed
140 KIAS
47
100% Flaps Speed (AT) Speed
95 KIAS
48
Climb (AT) Speed
165 KIAS
49
Cruise (AT) Speed
245 KIAS / 0.525
50
Holds (AT) Speed
160 KIAS
51
Avionics
2 GIAS/IAUs, 2 ADCs, 2 ADHRS, 3 GRCs, MFD, PFD, GMA36, GFC 700 w/ 707 Mode Controller
52
Changeover Point to Mach
18,300 ft
53
RAGL Height
2500
54
Reminder: Switch NAV Modes As Needed
Magenta vs green
55
How to get runway remaining
Surfacewatch! (Lower left PFD)
56
VNAV Acronym
Build, Bug (lowest cleared), Button, Brief It
57
VNAV Traps
Changing runway blows up Creates; VS down if above;
58
GIA Failure Indication
No CAS; Christmas Tree
59
Action For Any Miscompare
Display Backup
60
"Join the locailizer"
NAV
61
"Cleared ... " button
APR
62
FLC Descent (engine fire)
AT Man first
63
Missed / Go Around Trap
Call Tower with Go Around
64
Trick for GoAround FLC
Wait until 165 to hit FLC
65
ESP Armed
>200ft
66
ESP Roll
At 45 degrees, rolls to 30 degrees
67
ESP Pitch
At Vmo + 6 KIAS, pitch up
68
LVL vs Autolevel
Normal button vs exceeding normal flight envelope for 50% of the last 40 seconds.
69
Safe Return automatically activates?
Autolevel for 1 minute Passing 15,000 ft in EDM mode Button
70
Emergency Descent Mode Activates
1) AP on 2) PA > 14,900 ft 3) Cabin pressure >15,000 4) Cabin Dump switch not pressed
71
Emergency Descent Mode goes to
14,000 ft
72
How to deactivate EDM mode
AP DISC; cabin dump
73
CAPS mode
Pitch up, reduce thrust to idle, wings level. No deceleration in 8 seconds, will deploy. After 30 seconds, will deploy. <135
74
RVSM Airspace
FL 290
75
AFCS Limitations - Min Speeds and Max
Up - 105 KIAS; 50% - 95 KIAS; 100%.- 85 KIAS. Max - Vmo Mmo
76
AFCS AGL
1000 visual; 400 non-precision; 200 precision
77
AFCS Required
RVSM
78
CAS - STALL WARNING
Reduce AOA (-10 degrees); Thrust TO; recover (5 degrees)
79
PLI
Pitch Limit Indicator
80
Stall Procedure
Recover, Start A Climb, Clean Up, Level Off
81
Stick Pusher Inhibits
1) Below 500 AGL 2) Above 160 KIAS 3) 35 seconds after takeoff 4) On the ground
82
FALSE AOA
High AOA but ... airspeed is high enough
83
Auto Fuel Switch
Every 2 gallons
84
Fuel Low Yellow Threshold
<25 gal in either, or <50 total
85
Fuel Low Red
<5 gal on either, or <25 gal
86
Fuel Imbalance Limits
15 gal for advisory; 50 gal roll control
87
Fuel Types
Jet A, Jet A-1, JP-8
88
Min / Max Fuel Temp
-40C / 50C
89
When fueling, max imbalance
75 gallons
90
GEN 1 Volt / Amp
27.8V / 270
91
GEN 2 Volt / Amp
28.7V / 76
92
BAT 1 & 2 ... Volt / Amp
26.4V / 17 amp hour
93
BAT 1 / BAT 2 Location
Under floor in baggage; Nose
94
EMER Power from BAT 1
60 min
95
Ground Power
28 volts; 1000 amps
96
How many ciruit breaker panels?
5 ... 2 cabin, 1 nose, 2 baggage
97
N1 / N2 RPM
22k rpm / 50k rpm
98
Full Line Oil
2.2 qts
99
Idle N2 %
53%
100
Compressor stall vs surge
local disruption vs reversal
101
FADEC airstart attempts
3 lights
102
Gear handle down does what to igniters?
One ignitor fires
103
FADEC Switch When?
When N2 Drops Below 24%
104
Jet Stages
Suck, squeeze, bang, blow; compression, combustion, expansion, exhaust
105
4 Things Powered By Gear Box
FCU, Gen 1, Gen2, Oil Pump
106
Powerplant
FJ33-5A, medium bypass, FADEC controlled
107
Engine Thrust
1846 lbs
108
Types N1 compressor
Axial, 3 stage
109
Two types of oil
Mobile Jet II or Mobile 254
110
Bleed Ports Use
(1) IPS (2) ECS
111
Probes
PT2; TT2
112
FADEC adjusts based on
Thrust, ambient air, engine condition
113
FADEC powered by
PMA at N2 > 50%
114
Min Oil Temp
40C
114
WOW Sensor
(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
Max Crosswind For Start
25 kts
116
Max Tailwind For Start
15 kts
117
Titanium Firewall Specs
2000 degrees for 15 minutes
118
Fuel Ack Switch Actions
1) FSV 2) Aural 3) Arms Halon
119
Thrust Cheats
25% = 140 kts clean 30% = GP/GS Full Config 45% = MDA level off
120
What holds gear in place?
Over Center Locking Links
121
Main Gear Description
Trailing Link, Oleo Strut, Berringer Brakes
122
Nose Gear Description
Free castering. oleo strut, self centering
123
Landing Gear Description
Tricycle, Retractible, Hydraulically Powered
124
Gear Travel
8 seconds
125
Gear Up Speed
150 KIAS
126
Gear Down Speed
210 KIAS
127
Landing Gear Takes How Long To Show CAS
30 sec
128
Landing Gear Limitation
8 cycles per 30 minutes Minimum 10 seconds rest
129
High Energy Event Limitation
30 minute cool down. (Flaps up, ice landing, HDA)
130
Probe Heat Limitations
Max five min on ground if above 5C
131
What turns on with Engine IPS
Bleed air to d ring; PT2TT2
132
Engine IPS When?
Below 5C and visible moisture. OR, first signs of ice.
133
Engine IPS Limitations
Max Temp 10C; engine must be running
134
IPS Boot Cycles
6 tail, 6 bottom, 6 top; 42 second dwell
135
When Boot On?
First sign of ice.
136
Boot Limitations
Non-RVSM; min -40; not for T/O; STALL SPEED HIGH (Vref 5-10 kt higher, max 50% flaps ... Vref = 1.5 Vso)
137
Windshield IPS Cycles
1 pump 4 sec / min; 1 pump 4 sec; 2 pumps on demand
138
Windshield IPS When?
When leading edges start to accumulate?
139
Windshield IPS Limitations
Off 2 min before landing, min temp 30C, not on TO, max 3 gallons (27 lbs), min 1 gal dispatch
140
Windshield IPS duration
270 min on NORM; 135 min on HIGH
141
Windshield IPS MAX
50% duty cycle up to 10 seconds
142
What controls the PRSOV?
Bleed/Fresh Air
143
Warm Air Config
TCV Closed. FCV High Flow
143
How do you get pressurized air into cabin?
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
Cool Air Config
TCV Open, FCV Low Flow
145
Location of temperature sensors for ECS
Copilot speaker, above seat 4
146
AC System
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
Fresh Air Path
Check valve needs no bleed air pressure and no pressure vessel pressure in order to pass the check valve
148
N2 Compressor Type
Centrifugal
149
Max Differential
7.1psi
150
Cabin Dump Actions
Disables CPCS and opens outflow valves; can be reactivated by pressing dump a second time; activating disables Emer Descent
151
Full cold / full hot target
65-85%
152
ECS Disable
AC Off, Defog Selected, TCV Full Open, FCV To Low
153
Target CPCS Pressure Change
600 fpm change; scaling to LFE by 1500 AGL
154
High Field Elevation Indication
After T/O, will pressurize to 8k ft. When landing, takes above 8k below 23500
155
CAS Message / Synoptic
Open appropriate synoptic
156
Ramp Weight
6,040 lbs
157
MTOW
6,000 lbs
158
Landing Weight
5,550 lbs
159
Zero Fuel
4,900 lbs
160
Baggage
300 lbs (40 lbs xtend)
161
Pressure Altitude Math
29.92 minus Current = X * 1000
162
Performance Charts - Remember
Pressure Altitude Conversion!
163
Takeoff Grey Cells vs Landing Grey Cells
Not Demonstrated vs Not Possible (balked landing)
164
MEL Location
Has to be on the aircraft.
165
NEF Defn
Non Essential Furnishings
166
MEL Procedure
Identify, consult, comply, log, keep limitations in mind
167
CAPS Threshold
135 IAS / 145 TAS
168
CAPS Submode
1) Idle 2) Level 3) Pitch Up
169
Two G Forces CAPS Components
Disreef Ring; Snubline
170
Immediate CAPS pull
Loss of Control, Midair, Disorientation, 600-2000
171
EDM will level where?
14k
171
GPS For Dispatch? (Outage)
Required
172
DeIce Fluid
Type 1 (Not Type 4)
172
Gallons between MTOW and MLW
67 gal
173
Passenger Briefing
Buckle Up, Egress, Smoking, Fire Ext, O2, Safe Return, CAPS
174
140 kts Clean (Thrust)
25%
175
O2 Requirements
10 minutes for every pax above FL250
176
MAch Formula
True Airspeed / Speed of Sound
177
Vmo
250 KIAS
178
Mmo
0.53
179
When does Mach change?
18,300
180
CAT Stronger On
North Side of Jet Stream
181
Four Types of Hypoxia
Hypoxic, Hypemic, Stagnant, Histotoxi
182
O2 Auto Deploy
15,000
183
O2 System
Master (PRSOV), Burst Disc, Outlets, PAX (6) Deploy
184
STAR Clearance
Need to hear "VIA" to follow altitude
185
Missed Approach Sequence
Click, Clean, Configure, Clean, Communicate
186
RVSM Requirements
(1) Alt Reporting Transponder (2) Independent Primary Altimeters (1) Autopilot (1) Alt Alerting system
187