SF-50 G1 Memory Items
Type of engine
Williams FJ33-5A
Minimum dispatch quantity for icing protection fluid
1 gallon
Maximum tailwind component for landing
10 knots
Maximum duty cycle for windshield ice protection system
10 seconds on, 10 seconds off
Maximum airport elevation, T/O and landing
10,000 feet MSL
A/P disconnect altitude for visual approach
1000 feet AGL
Minimum airspeed for flaps 0%, A/P engaged
105 KIAS
KIAS for engine inflight air start below 18,000 feet MSL
120-200 KIAS
Maximum allowable fuel imbalance
15 gallons
Maximum tailwind for engine start
15 knots
Vfe for Flaps 100%
150 KIAS
Vlo for gear retraction
150 KIAS
Vo (knots)
150 KIAS
Flaps 100% maximum demonstrated crosswind component
16 knots
Minimum airspeed in icing conditions
160 KIAS
Flaps 50% maximum demonstrated crosswind component
18 knots
Maximum rated thrust at MSL
1846 lbs
Vfe for Flaps 50%
190 KIAS
Quarts of oil to the full line
2.2 quarts
Vle
210 KIAS
Vlo for gear extension
210 KIAS
Minimum voltage for battery 1 start
23.5V
Maximum crosswind for engine start
25 knots
Vmo (knots)
250 KIAS
Generator 1 Volts and Amps
27.8V and 270A
Generator 2 Volts and Amps
28.7V and 72A
EPU volts and amps requirement
28V and 800-1000A
Total usable fuel
296 gallons
Total usable icing protection fluid
3 gallons
Maximum oil capacity
3 quarts
Minimum cool down time after high energy event
30 minutes
Minimum wait time after third start attempt
30 minutes
Minimum wait time between first and second start attempts
30 seconds
Starter time limit for each attempted start
30 seconds
Max aft baggage compartment (lbs)
300
Max Cargo X-tend compartment (lbs)
40
Minimum altitude for A/P engangement
400 feet AGL
Max zero fuel weight (lbs)
4900
Maximum duration for T/O thrust
5 minutes
Maximum time allowed for Probe Heat during ground operations
5 minutes
Minimum wait time between second and third start attempts
5 minutes
When should conduct a tactile inspection of Wing/Stabilizer ice protection system
5 minutes before departure
Approved flap configuration for landing
50% and 100%. 0% for abnormal operations
Maximum fuel temperature
50C/122F
Maximum temperature allowed for T/O
50C/122F
Max. landing weight (lbs)
5550
Maximum cabin pressure differential
6.4 psid
Max. takeoff weight (lbs)
6000
Max. ramp weight (lbs)
6040
Maximum fuel imbalance during fueling operations
75 gallons
Full gear cycle limitation (UP, DN, UP or DN, UP, DN)
8 cycles within 30 minutes, 10 second rest between cycles
Minimum airspeed for flaps 100%, A/P engaged
85 KIAS
Minimum airspeed for flaps 50%, A/P engaged
95 KIAS
Cabin altitude where passenger oxygen is unavailable
Below 10,000 feet
Approved flap configuration for T/O
Flaps 50%
Maximum flap deflection in icing conditions
Flaps 50%
Max operating altitude
G1 - FL280
Types of approved fuels
Jet A, Jet A-1, JP-8 (6.76 lbs/gallon)
Types of approved engine oil
Mobile Jet II, Mobile 254
Minimum altitude for A/P disconnect on instrument approach
Published approach minimums
Minimum airport elevation, T/O and landing
-1000 feet MSL
Minimum temperature for battery 1 start
-18C/0F
Minimum temperature for windshield ice protection system
-34C/-30F
Minimum fuel temperature
-40C/F
Minimum landing gear temperature
-40C/F
Minimum oil temperature
-40C/F
Minimum temperature allowed for T/O
-40C/F
Minimum temperature for EPU start
-40C/F
Minimum temperature for Wing/Stabilizer ice protection system
-40C/F
Minimum operating temperature at FL200
-54C/-65F
Minimum operating temperature at FL280
-61C/-77F
Mmo (Mach)
0.53 mach
