SF-50 G1 Memory Items

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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


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