AC Limits Flashcards by Audrey Marquis

Vyse

(def&speed)

128 kts (decrease 2kts / 5,000’)

One-engine INOP best RATE of climb

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Vxse

(def&speed)

122 kts

One-engine INOP best ANGLE of climb

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Venr

(def&speed)

123 kts

One-engine INOP best EN-ROUTE climb

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Vmca

(F.UP & F17)

92 kts
92 kts

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Emergency descents

(best rate & range)

Rate : 180 kts
Range : 140 kts

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Stall speed - Flaps UP

102 kts

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Stall speed - Flaps 17

91 kts

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Stall speed - Flaps 35

84 kts

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(def&speed)

178 kts

Manoeuvering : Full deflection of any flight control surface

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Vfe - Flaps 17

188 kts

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Vfe - Flaps 35

154

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Vle & Vlo

180 kts

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Vmo & Mmo

0’ - 13,200’ = 248 kts
13,200’ - FL250 = 248>195*

* 0.48 Mach

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Min N1 - 0%-75% electrical load

65% N1

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Min N1 - 75%-100% electrical load

72% N1

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GPU limits

(Volts & Amps)

28.0-28.4 Volts
1,000 amps (momentary)
300 amps (continuous)

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Starter limit - Restart following normal start

3 minutes cool-down

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Starter limit - Aborted start

(seq) 30 sec (seq) 60 sec (seq) 5 minutes

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Starter limit - Aborted start

(seq) 30 sec (seq) 60 sec (seq) 5 minutes

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Starter limit - Dry motoring run

5 minutes cool-down

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Reduced power take-offs

(3) Requirements

1) Rwy not wet or contaminated wt snow, sluch or ice
2) Flaps 17
3) Periodic check of static take-off power (25 hours <> 25 take-off)

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Cabin pressure - Max differential

5.1 PSI

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Usable fuel qty

4,484 lbs

Main tanks capacity

1,621 lbs

Aux tanks capacity

621 lbs

Fuel imbalance

200 lbs

Fuel yellow arc

363 lbs (FUEL QTY annunc : 324) | * no take-off allowed

Approved engine fuels

Jet-A Jet A-1 Jet B* JP-4* JP-5 JP-8 | * Operation prohibited > 8,000' if either standby pump inop

Max ramp weight

17,230 lbs

MTOW

17,120 lbs

MLW

16,765 lbs

MZFW

15,165 lbs | * 15,700 wt. STC

Cargo compartment capacity - FORWARD

1,000 lbs (700 if cargo config)

Cargo compartment capacity - AFT

630 lbs

Cabin floor loading

100 lb/sq ft

Load factor - Flaps UP

3.00 pos 1.20 neg

Load factor - Flaps 17&35

2.00 pos 0.00 neg

Landing gear cycle limit

1) Max 3 consecutive cycles, wt. 2 minutes cool-down 2) Then 5 min cool-down unlimited

Propeller RPM - Prohibited range (ground)

400-950 RPM 1,250-1,395 RPM

Aviation gasoline | (4) Limitations

1) Max 150 between engine overhauls 2) Prohibited above 18,000' 3) Standby pumps ON for take-off & landing 4) Prohibited if either standby pump inop

Max. airspeed - Windshield anti-ice effectivness

223 kts

Min. temp - Deicing boots

(-) 40 deg

Min. airspeed - Level flight in icing

160 kts

Engine anti-ice operation recommended temps

+5 deg, and below

Propeller deice - Limit

One cycle per propeller at temp above +10 deg

Max. OAT limit

ISA + 37 deg ## Footnote 52 at ISA a 0'ASL

Exhaust heating of windows - Prevention (3)

1) Reverse max 10 sec 2) No ground fine when OAT above 38 deg 3) No ground ops wt props feathered unless : _a) GPU start _b) Prop AFX checks _c) Airframe deicing, providing that : ___i) OAT below +5 deg ___ii) Max 3 minutes

Cracked windshield - Ops limits (5)

1) Max 25 hours 2) Inner ply intact 3) Visibility not impaired 4) Windshield wipers use ok 5) Windshield anti-ice ok

Propeller rotational overspeed limits (3)

1700 RPM : Max. continuous (failure of primary governor) 1802 RPM : Torque limit 35,38 ft-lb (failure of overspeed governor) 1870 RPM : Max. 20 seconds

Wardrobe weight limits (&pole)

Total : 250 lbs Pole : 100 lbs

Max. demonstrated crosswind

22 kts

Vx (def & speed)

two-engine best ANGLE of climb 122 kts

Vy (def&speed)

two-engine best RATE of climb 138 kts, decrease 2 kts / 5,000'

Vb (turbulent air)

170 kts

Vsse (def&speed)

Intentional one-engine inop speed 105 kts

Cruise climb speed

0'-10,000' = 160 kts 10-15,000' = 150 kts 15-20,000' = 140 kts 20-25,000' = 130 kts