Limitations Flashcards by Alexander Rodriguez | Brainscape

Q

Max Ramp Weight (MRW)

A

18,497 lbs

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Q

Max Takeoff Weight (MTOW)

A

18,387 lbs

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Q

Max Landing Weight (MLW)

A

17,042 lbs

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Q

Max Zero Fuel Weight (MZFW)

A

14,220 lbs

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Q

vLO

A

250 KIAS

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Q

vLE

A

250 KIAS

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Q

Takeoff vMC

A

97 KIAS

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Q

Landing vMC (no icing conditions)

A

91 KIAS

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Q

Landing vMC (icing conditions)

A

95 KIAS

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Q

Mmo

A

.78 Mach

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Q

vO

A

205 KIAS

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Q

vFE

A

180 flaps 1
170 flaps 2/3
160 flaps full

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Q

Max tire speed

A

182kt

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Q

Min Mach for SAT -66c/-70c

A

.67M

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Q

Min battery volt for start

A

24v

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Q

Min GPU volt for battery charge

A

27v

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Q

Generator load on the ground

A

330A each

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Q

Generator load in flight

A

390A each

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Q

Max USABLE fuel

A

5,352 lbs

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Q

Max usable fuel PER tank

A

2,676 lbs / 399gal

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Q

Unusable fuel per tank

A

25lbs

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Q

Max fuel imbalance

A

220lbs

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Q

Min fuel temp

A

-37c

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Q

Max fuel temp GROUND

A

52c

Q

Max fuel temp inFLIGHT

A

80c

Q

Xfeed operation

A

Off for T/L

Q

Inop jet pump, unusable fuel increases to…

A

45lbs per tank

Q

Max differential pressure

A

9.4 psid

Q

Max differential OVER pressure

A

9.6 psid

Q

Max differential T/L

A

0.2 psid

Q

Max negative differential

A

0.3 psid

Q

Max T/O & Landing Press Alt in icing conditions

A

10,000 ft

Q

Max cruise alt OEI in icing conditions

A

15,000 ft

Q

Min temp for landing in icing conditions

A

-38c

Q

Min airspeed WHSAIS inhibited or armed

A

165 Kias

Q

Min airspeed WHSAIS Un-inhibited

A

150 kias

Q

Starter limits

A

1…….1min
2……..1min
3……..15min
4……..30min

Q

Min ground idle N2

A

55.1%

Q

Forward baggage compartment max weight

A

110lbs

Q

Aft baggage compartment max weight

A

463lbs

Q

AP minimum engagement height dual and single engine

A

600ft

1000ft Single engine

Q

AP minimum use height dual and single engine?

A

195 ft agl

220 ft agl SE

Q

Max cruise alt

A

45,000 ft

Q

Max alt for flaps extended

A

18,000ft

Q

Max alt for takeoff and landing

A

14,000 ft PA

Q

Max load factor flaps 0

A

3.00 g

Q

Max load factor with flaps

A

2.00g

Q

Runway slope limits

A

+2%, -2%

Q

Max tailwind

A

10kts

Q

Max crosswind for static TO

A

18 kts LIMITING

Q

Min temp for TO/landing

A

-40c

Q

Max ISA deviation

A

ISA + 35c

Q

Max airspeed in icing if YD off

A

180 KIAS

Q

Max demonstrated crosswind for takeoff

A

25kts

Q

Max demonstrated crosswind for landing

A

28kts

Q

Are the demonstrated crosswinds limiting?

A

No

Q

Turbulence penetration speed

A

232 kts or .65mach

Q

Normal climb

A

225 KIAS to . 60mach

(.67 mach if it’s SAT -65°)