SF50 Facts Memory Items Flashcards by Amit Patel | Brainscape

Q

Max ramp weight

A

6040 lbs

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Q

Max takeoff weight

A

6000 lbs

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Q

Max landing weight

A

5550 lbs

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Q

Max zero fuel weight

A

4900 lbs

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Q

Max baggage

A

300 lbs

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Q

Max Cargo x-tend

A

40 lbs

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Q

Min oil temp

A

-40C

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Q

Min temp start

A

-40C

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Q

EPU requirements

A

28V + 800-1000amps

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Q

Max tailwind for start

A

15 kts

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Q

Max crosswind for start

A

25 kts

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Q

Inflight air start

A

120-200 KIAS and 18000 ft

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Q

Seconds per attempted start

A

30

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Q

Time off after each attempted start

A

1st attempt - 30 seconds
2nd attempt - 5 minutes
3rd attempt - 30 minutes

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Q

What do you do after a failed start?

A

External check

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Q

Type of fuels and weight

A

Jet-A
Jet A-1
JP-8

6.76 lbs/gal

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Q

Usable fuel

A

296 gal

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Q

Max allowable fuel imbalance

A

15 gal

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Q

Min fuel temp

A

-40 C

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Q

Max fuel temp

A

50 C

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Q

Engine Model and THRUST

A

Williams FJ33-5A

1846 lbs of thrust

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Q

Engine oil types

A

Mobile Jet II
Mobile 254

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Q

Total oil quantity

A

3 qts

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Q

Oil to full line

A

2.2 qts

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Q

Max tailwind for landing

A

10 knots

Q

Max crosswind Flaps 50% landing

A

18 knots

Q

Max crosswind 100% flaps landing

A

16 knots

Q

Max airport elevation

A

10000 feet

Q

Min airport elevation

A

-1000 ft

Q

Min takeoff temp

A

-40 C

Q

Max takeoff temp

A

50 C

Q

Only approved flap setting for takeoff

A

50%

Q

Vmo

A

250 KIAS

Q

Mmo

A

Mach .53

Q

Vo

A

150 KIAS

Q

Max duration of takeoff thrust

A

5 min

Q

Max operating altitude

A

FL310

Q

Min operating temp @ FL310

A

-63 C

Q

Min operating temp at FL200

A

-54 C

Q

Cool down time after high energy landing event

A

30 min

Q

VFE_50%

A

190 KIAS

Q

VFE_100%

A

150 KIAS

Q

VLO_EXTEND

A

210 KIAS

Q

VLO_RETRACT

A

150 KIAS

Q

VLE

A

210 KIAS

Q

Max cabin pressure differential

A

7.1 psi

Q

Min speed with flaps 100%

A

85 KIAS

Q

Min speed with flaps 50%

A

95 KIAS

Q

Min speed with flaps UP

A

105 KIAS

Q

Min autopilot engagement altitude

A

400’

Q

Disconnect altitude for visual approach

A

1000’

Q

Min disconnect altitude for IAP

A

Minimums

Q

Max usable IPS fluid

A

3.0 gal

Q

Minimum IPS fluid dispatch quantity

A

1.0 gal

Q

Min windshield IPS temp

A

-30 C

Q

Minimum wing/stab IPS temp

A

-40 C

Q

Min airspeed in icing

A

160 KIAS

Q

Max flaps deflection in icing

A

50%

Q

Max duty cycle for windshield IPS

A

10 sec on/10 sec off

Q

Icing tactile inspection timing

A

5 minutes prior to departure

Q

Max continuous probe heat on ground

A

5 min