SF50 Flashcards
Vo
150 KIAS
Scoreboard is …
KING!
Sterile cockpit in …
critical phases of flight (10k)
Flaps Up G Limits
+3.6g, -1.44g
Flaps 50% G Limits
+2g, 0g
Flaps 100% G Limits
2g, 0g
Takeoff Temp Limits
+50C, -40C
General Operating
50C, -63C (FL 310)
Fuselage Design / Construction
Carbon fiber, one piece pressure vessel
Wings Design / Construction
Carbon fiber, two main spars, wet wing, aluminum flight controls
Landing Gear
Tricycle gear, aluminum
Engine Mount
Pylon
Engine Type
Williams FJ33-5A
Engine Thrust
1846 lbs
Engine Nacelle
Fiberglass cover
Engine Pylon
Raised mount
Nav lights controlled by
Bat 1
Landing Light Switch
Leave on 24/7
Wingtip Lights Pattern
Alternates in flashing patter at 500ft AGL
Hot Bus Battery
Bat 1
Main Cabin Door
Clamshell; pressure vessel
Preferred Exit In Water
Egress door
Required Seats To Fly
Seats 1 & 2
When 6 and 7 Are Occupied, Where is Seat 4
Fully aft
Baggage Weight Limit
300 lbs
X-Tend Weight Limit
40 lbs (implies 260 for main)
Control Summary
Manual for pitch, roll, and yaw. Forces transmitted via cables, pulleys, bellcranks, pushrods
Left Aileron Tab
Trim Tab
Right Aileron Tab
Balance Tab
Two Yaw Systems
Yaw SAS and Yaw Damper
Yaw Damper Purpose & Engagement
Turn Coordinator; 200 AGL
Yaw SAS Purpose & Engagement
Reduce dutch roll (longitudinal stability); weight on wheels sensor
100% Flaps Crosswind
16 knots
50% Flaps Crosswind
18 knots
0% Flaps Crosswind
Not demonstrated
Trim Runaway Indication
CAS Warning, Trim Indicator
Trim Runaway Memory
Hold; AP disconnect; control; A3; AP release
Type of flaps
Fowler (travel aft and down); no need for slots because we’re not producing as much drag
Deflection for 50% flaps and 100% flaps
50% - 15 degrees; 100% - 40 degrees
Only Approved TO Flaps
50%
Flaps Actuation
Single piece torque tube; electro-mechanical actuator
Vfe 100%
150 KIAS
Max Flap in Icing
50%
Vfe 50%
190 KIAS
Terminal Area Speed (AT) Speed
180 KIAS
50% Flaps Speed (AT) Speed
140 KIAS
100% Flaps Speed (AT) Speed
95 KIAS
Climb (AT) Speed
165 KIAS
Cruise (AT) Speed
245 KIAS / 0.525
Holds (AT) Speed
160 KIAS
Avionics
2 GIAS/IAUs, 2 ADCs, 2 ADHRS, 3 GRCs, MFD, PFD, GMA36, GFC 700 w/ 707 Mode Controller
Changeover Point to Mach
18,300 ft
RAGL Height
2500
Reminder: Switch NAV Modes As Needed
Magenta vs green
How to get runway remaining
Surfacewatch! (Lower left PFD)
VNAV Acronym
Build, Bug (lowest cleared), Button, Brief It
VNAV Traps
Changing runway blows up Creates; VS down if above;
GIA Failure Indication
No CAS; Christmas Tree
Action For Any Miscompare
Display Backup
“Join the locailizer”
NAV
“Cleared … “ button
APR
FLC Descent (engine fire)
AT Man first
Missed / Go Around Trap
Call Tower with Go Around
Trick for GoAround FLC
Wait until 165 to hit FLC
ESP Armed
> 200ft
ESP Roll
At 45 degrees, rolls to 30 degrees
ESP Pitch
At Vmo + 6 KIAS, pitch up
LVL vs Autolevel
Normal button vs exceeding normal flight envelope for 50% of the last 40 seconds.
Safe Return automatically activates?
Autolevel for 1 minute
Passing 15,000 ft in EDM mode
Button
Emergency Descent Mode Activates
1) AP on 2) PA > 14,900 ft 3) Cabin pressure >15,000 4) Cabin Dump switch not pressed
Emergency Descent Mode goes to
14,000 ft
How to deactivate EDM mode
AP DISC; cabin dump
CAPS mode
Pitch up, reduce thrust to idle, wings level. No deceleration in 8 seconds, will deploy. After 30 seconds, will deploy. <135
RVSM Airspace
FL 290
AFCS Limitations - Min Speeds and Max
Up - 105 KIAS; 50% - 95 KIAS; 100%.- 85 KIAS. Max - Vmo Mmo
AFCS AGL
1000 visual; 400 non-precision; 200 precision
AFCS Required
RVSM
CAS - STALL WARNING
Reduce AOA (-10 degrees); Thrust TO; recover (5 degrees)
PLI
Pitch Limit Indicator
Stall Procedure
Recover, Start A Climb, Clean Up, Level Off
Stick Pusher Inhibits
1) Below 500 AGL 2) Above 160 KIAS 3) 35 seconds after takeoff 4) On the ground
FALSE AOA
High AOA but … airspeed is high enough
Auto Fuel Switch
Every 2 gallons
Fuel Low Yellow Threshold
<25 gal in either, or <50 total
Fuel Low Red
<5 gal on either, or <25 gal
Fuel Imbalance Limits
15 gal for advisory; 50 gal roll control
Fuel Types
Jet A, Jet A-1, JP-8
Min / Max Fuel Temp
-40C / 50C
When fueling, max imbalance
75 gallons
GEN 1 Volt / Amp
27.8V / 270
GEN 2 Volt / Amp
28.7V / 76
BAT 1 & 2 … Volt / Amp
26.4V / 17 amp hour
BAT 1 / BAT 2 Location
Under floor in baggage; Nose
EMER Power from BAT 1
60 min
Ground Power
28 volts; 1000 amps
How many ciruit breaker panels?
5 … 2 cabin, 1 nose, 2 baggage
N1 / N2 RPM
22k rpm / 50k rpm
Full Line Oil
2.2 qts
Idle N2 %
53%
Compressor stall vs surge
local disruption vs reversal
FADEC airstart attempts
3 lights
Gear handle down does what to igniters?
One ignitor fires
FADEC Switch When?
When N2 Drops Below 24%
Jet Stages
Suck, squeeze, bang, blow; compression, combustion, expansion, exhaust
4 Things Powered By Gear Box
FCU, Gen 1, Gen2, Oil Pump
Powerplant
FJ33-5A, medium bypass, FADEC controlled
Engine Thrust
1846 lbs
Types N1 compressor
Axial, 3 stage
Two types of oil
Mobile Jet II or Mobile 254
Bleed Ports Use
(1) IPS (2) ECS
Probes
PT2; TT2
FADEC adjusts based on
Thrust, ambient air, engine condition
FADEC powered by
PMA at N2 > 50%
Min Oil Temp
40C
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
Max Crosswind For Start
25 kts
Max Tailwind For Start
15 kts
Titanium Firewall Specs
2000 degrees for 15 minutes
Fuel Ack Switch Actions
1) FSV 2) Aural 3) Arms Halon
Thrust Cheats
25% = 140 kts clean
30% = GP/GS Full Config
45% = MDA level off
What holds gear in place?
Over Center Locking Links
Main Gear Description
Trailing Link, Oleo Strut, Berringer Brakes
Nose Gear Description
Free castering. oleo strut, self centering
Landing Gear Description
Tricycle, Retractible, Hydraulically Powered
Gear Travel
8 seconds
Gear Up Speed
150 KIAS
Gear Down Speed
210 KIAS
Landing Gear Takes How Long To Show CAS
30 sec
Landing Gear Limitation
8 cycles per 30 minutes
Minimum 10 seconds rest
High Energy Event Limitation
30 minute cool down. (Flaps up, ice landing, HDA)
Probe Heat Limitations
Max five min on ground if above 5C
What turns on with Engine IPS
Bleed air to d ring; PT2TT2
Engine IPS When?
Below 5C and visible moisture. OR, first signs of ice.
Engine IPS Limitations
Max Temp 10C; engine must be running
IPS Boot Cycles
6 tail, 6 bottom, 6 top; 42 second dwell
When Boot On?
First sign of ice.
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)
Windshield IPS Cycles
1 pump 4 sec / min; 1 pump 4 sec; 2 pumps on demand
Windshield IPS When?
When leading edges start to accumulate?
Windshield IPS Limitations
Off 2 min before landing, min temp 30C, not on TO, max 3 gallons (27 lbs), min 1 gal dispatch
Windshield IPS duration
270 min on NORM; 135 min on HIGH
Windshield IPS MAX
50% duty cycle up to 10 seconds
What controls the PRSOV?
Bleed/Fresh Air
Warm Air Config
TCV Closed. FCV High Flow
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
Cool Air Config
TCV Open, FCV Low Flow
Location of temperature sensors for ECS
Copilot speaker, above seat 4
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)
Fresh Air Path
Check valve needs no bleed air pressure and no pressure vessel pressure in order to pass the check valve
N2 Compressor Type
Centrifugal
Max Differential
7.1psi
Cabin Dump Actions
Disables CPCS and opens outflow valves; can be reactivated by pressing dump a second time; activating disables Emer Descent
Full cold / full hot target
65-85%
ECS Disable
AC Off, Defog Selected, TCV Full Open, FCV To Low
Target CPCS Pressure Change
600 fpm change; scaling to LFE by 1500 AGL
High Field Elevation Indication
After T/O, will pressurize to 8k ft. When landing, takes above 8k below 23500
CAS Message / Synoptic
Open appropriate synoptic
Ramp Weight
6,040 lbs
MTOW
6,000 lbs
Landing Weight
5,550 lbs
Zero Fuel
4,900 lbs
Baggage
300 lbs (40 lbs xtend)
Pressure Altitude Math
29.92 minus Current = X * 1000
Performance Charts - Remember
Pressure Altitude Conversion!
Takeoff Grey Cells vs Landing Grey Cells
Not Demonstrated vs Not Possible (balked landing)
MEL Location
Has to be on the aircraft.
NEF Defn
Non Essential Furnishings
MEL Procedure
Identify, consult, comply, log, keep limitations in mind
CAPS Threshold
135 IAS / 145 TAS
CAPS Submode
1) Idle 2) Level 3) Pitch Up
Two G Forces CAPS Components
Disreef Ring; Snubline
Immediate CAPS pull
Loss of Control, Midair, Disorientation, 600-2000
EDM will level where?
14k
GPS For Dispatch? (Outage)
Required
DeIce Fluid
Type 1 (Not Type 4)
Gallons between MTOW and MLW
67 gal
Passenger Briefing
Buckle Up, Egress, Smoking, Fire Ext, O2, Safe Return, CAPS
140 kts Clean (Thrust)
25%
O2 Requirements
10 minutes for every pax above FL250
MAch Formula
True Airspeed / Speed of Sound
Vmo
250 KIAS
Mmo
0.53
When does Mach change?
18,300
CAT Stronger On
North Side of Jet Stream
Four Types of Hypoxia
Hypoxic, Hypemic, Stagnant, Histotoxi
O2 Auto Deploy
15,000
O2 System
Master (PRSOV), Burst Disc, Outlets, PAX (6) Deploy
STAR Clearance
Need to hear “VIA” to follow altitude
Missed Approach Sequence
Click, Clean, Configure, Clean, Communicate
RVSM Requirements
(1) Alt Reporting Transponder (2) Independent Primary Altimeters (1) Autopilot (1) Alt Alerting system
