AC Limits Flashcards

1
Q

Vyse

(def&speed)

A

128 kts (decrease 2kts / 5,000’)

One-engine INOP best RATE of climb

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2
Q

Vxse

(def&speed)

A

122 kts

One-engine INOP best ANGLE of climb

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3
Q

Venr

(def&speed)

A

123 kts

One-engine INOP best EN-ROUTE climb

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4
Q

Vmca

(F.UP & F17)

A

92 kts
92 kts

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5
Q

Emergency descents

(best rate & range)

A

Rate : 180 kts
Range : 140 kts

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6
Q

Stall speed - Flaps UP

A

102 kts

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7
Q

Stall speed - Flaps 17

A

91 kts

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8
Q

Stall speed - Flaps 35

A

84 kts

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9
Q

Va

(def&speed)

A

178 kts

Manoeuvering : Full deflection of any flight control surface

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10
Q

Vfe - Flaps 17

A

188 kts

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11
Q

Vfe - Flaps 35

A

154

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12
Q

Vle & Vlo

A

180 kts

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13
Q

Vmo & Mmo

A

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

* 0.48 Mach

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14
Q

Min N1 - 0%-75% electrical load

A

65% N1

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15
Q

Min N1 - 75%-100% electrical load

A

72% N1

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16
Q

GPU limits

(Volts & Amps)

A

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

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17
Q

Starter limit - Restart following normal start

A

3 minutes cool-down

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18
Q

Starter limit - Aborted start

A

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

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19
Q

Starter limit - Aborted start

A

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

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20
Q

Starter limit - Dry motoring run

A

5 minutes cool-down

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21
Q

Reduced power take-offs

(3) Requirements

A

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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22
Q

Cabin pressure - Max differential

A

5.1 PSI

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23
Q

Usable fuel qty

A

4,484 lbs

24
Q

Main tanks capacity

A

1,621 lbs

25
Q

Aux tanks capacity

A

621 lbs

26
Q

Fuel imbalance

A

200 lbs

27
Q

Fuel yellow arc

A

363 lbs
(FUEL QTY annunc : 324)

* no take-off allowed

28
Q

Approved engine fuels

A

Jet-A
Jet A-1
Jet B*
JP-4*
JP-5
JP-8

* Operation prohibited > 8,000’ if either standby pump inop

29
Q

Max ramp weight

A

17,230 lbs

30
Q

MTOW

A

17,120 lbs

31
Q

MLW

A

16,765 lbs

32
Q

MZFW

A

15,165 lbs

* 15,700 wt. STC

33
Q

Cargo compartment capacity - FORWARD

A

1,000 lbs
(700 if cargo config)

34
Q

Cargo compartment capacity - AFT

A

630 lbs

35
Q

Cabin floor loading

A

100 lb/sq ft

36
Q

Load factor - Flaps UP

A

3.00 pos
1.20 neg

37
Q

Load factor - Flaps 17&35

A

2.00 pos
0.00 neg

38
Q

Landing gear cycle limit

A

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

39
Q

Propeller RPM - Prohibited range (ground)

A

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

40
Q

Aviation gasoline

(4) Limitations

A

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

41
Q

Max. airspeed - Windshield anti-ice effectivness

A

223 kts

42
Q

Min. temp - Deicing boots

A

(-) 40 deg

43
Q

Min. airspeed - Level flight in icing

A

160 kts

44
Q

Engine anti-ice operation recommended temps

A

+5 deg, and below

45
Q

Propeller deice - Limit

A

One cycle per propeller at temp above +10 deg

46
Q

Max. OAT limit

A

ISA + 37 deg

52 at ISA a 0’ASL

47
Q

Exhaust heating of windows - Prevention (3)

A

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

48
Q

Cracked windshield - Ops limits (5)

A

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

49
Q

Propeller rotational overspeed limits (3)

A

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

50
Q

Wardrobe weight limits (&pole)

A

Total : 250 lbs
Pole : 100 lbs

51
Q

Max. demonstrated crosswind

A

22 kts

52
Q

Vx (def & speed)

A

two-engine best ANGLE of climb
122 kts

53
Q

Vy (def&speed)

A

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

54
Q

Vb (turbulent air)

A

170 kts

55
Q

Vsse (def&speed)

A

Intentional one-engine inop speed
105 kts

56
Q

Cruise climb speed

A

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