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CASA 212 Erickson > Operating Limitations > Flashcards

Operating Limitations Flashcards

1
Q

Maximum Ramp Weight

A

17,086 lbs

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2
Q

Maximum Takeoff Weight

A

16,976 lbs

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3
Q

Maximum Landing Weight

A

16,424 lbs

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4
Q

Maximum Zero Fuel Weight

A

15,653 lbs

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5
Q

Minimum Flight Weight

A

9,481 lbs

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6
Q

Maximum Continuous EGT

A

650°

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7
Q

Maximum Continuous Torque

A

100%

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8
Q

Maximum Takeoff Torque

A

104.4% for 5 minutes

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9
Q

Takeoff and Maximum Continuous RPM

A

100%

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10
Q

Maximum Cruise RPM

A

98.0%

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11
Q

Normal Cruise RPM

A

96.1%

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12
Q

Minimum In-Flight Cruise RPM

A

96.0%

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13
Q

Maximum Continuous Overspeed RPM

A

101.0%

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14
Q

Maximum Transient Overspeed RPM - 5 minutes

A

101.5%

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15
Q

Maximum Transient Overspeed RPM - 30 seconds

A

105.5%

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16
Q

Maximum Transient Overspeed RPM - 5 seconds

A

106.0%

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17
Q

Never Exceed Overspeed RPM

A

Greater than 106.0%

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18
Q

Landing Reverse Minimum RPM

A

93.0%

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19
Q

Static Reverse Minimum RPM

A

94.5%

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20
Q

Propeller Windmilling Limit 0% - 5%

A

No Limit

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21
Q

Propeller Windmilling Limit 5% - 10%

A

30 minutes

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22
Q

Propeller Windmilling Limit 10% - 18%

A

5 minutes

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23
Q

Propeller Windmilling Limit 18% - 28%

A

Prohibited

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24
Q

Propeller Windmilling Limit 28% - 100%

A

1 minutes

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25
Q

Maximum Starting EGT

A

770º for 1 second

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26
Q

Initial Takeoff EGT Limit

A

650º with APR System Operative

for 5 minutes

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27
Q

Takeoff APR ON EGT Limit

A

650º (now a corrected value via 26º bias reduction)

for 5 minutes from application of takeoff power

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28
Q

Maximum Continuous

A

650º

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29
Q

Takeoff, Climb, Cruise with APR or SRL Inoperative EGT Limit

A

Per Section 3 “Abnormal Procedures”

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30
Q

Minimum Temperature Ground Start

A

-40º

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31
Q

Engine Light-Off Time Limits

A

(from 10% RPM to Light-Off)
GND: 10 seconds (Auto-Start), 5 seconds (if PRIME used)
AIR: 15 seconds

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32
Q

Ignition System Limits (Manual Ignition Switch)

A

i) 1 minute ON . . . 1 minute OFF
ii) 2 minutes ON . . . 2 minutes OFF
(a further 2 minutes ON . . . 23 minutes OFF)
iii) 5 minutes ON . . . 55 minutes OFF

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33
Q

Total Useable Fuel Capacity

A

528 gal (3432 lbs)

34
Q

Total Unusable Fuel

A

10 gal

35
Q

“Inboards Only”

A

370 gal (2406 lbs) - approximately 3.5 hours of flying - ish

36
Q

Outboard Fuel Capacity

A

158 gal (79 gal each) - 1026 lbs

37
Q

Fueling Procedure (Overwing)

A

inboards first, then outboards

38
Q

Pressure Refueling Maximum PSI

A

55 psig

39
Q

Fuel Asymmetry

A

No Limitation

40
Q

Minimum Fuel Pressure Warning Range

A

3.5 to 7.0 psig

41
Q

Unfeathering Pump Duty Cycle

A

1 minute ON . . . 3 minutes OFF

42
Q

Negative Torque Sensing (NTS) Required…

A

for ALL takeoffs

43
Q

Movement of the Power Lever aft of Flight Idle in flight…

A

Prohibited

44
Q

Engine Oil Tank Capacity

A

7.25 quarts

45
Q

Engine Oil Tank Usable Capacity

A

5.25 quarts

46
Q

Maximum Permissible Oil Consumption

A

1 quart per every 12 hours per engine

47
Q

Oil Quantity when dipstick indicates FULL

A

6.2 quarts

48
Q

Oil Quantity when dipstick indicates ADD OIL

A

5.0 quarts

49
Q

Oil Servicing Technique

A

rotate propeller for 10 seconds or 100 revolutions to scavenge oil from sump into oil tank

50
Q

Minimum Oil Temperature for Starting

A

-40º

51
Q

Maximum Oil Temperature at 86% TQ or less (continuous)

A

110ºC

52
Q

Maximum Oil Temperature for Ground Operations (continuous)

A

110ºC

53
Q

Maximum Oil Temperature above 86% TQ (continuous)

A

79ºC

54
Q

Minimum Oil Temperature for Air Start

A

4ºC

55
Q

Minimum Oil Pressure Ground Operations

A

40 psig

56
Q

Vmo

A

200 KIAS

57
Q

Va

A

146 KIAS

58
Q

Vfe Takeoff (25%)

A

135 KIAS

59
Q

Vfe Approach (37.5%)

A

130 KIAS

60
Q

Vfe Landing (100%)

A

115 KIAS

61
Q

Vmca

A

85 KCAS

62
Q

Vmcg

A

85 KCAS

63
Q

Maximum Demonstrated Crosswind

A

20 kts

64
Q

Maximum Reverse Forward Speed

A

90 KIAS

65
Q

Maximum Cargo Door Operating Speed

A

170 KIAS

66
Q

Maximum Tire Speed

A

120 mph or 160 mph (dependent on tire part number)

67
Q

Load Factor Flaps UP

A

+3.0 to -1.2

68
Q

Load Factor Flaps LANDING

A

+2.0 to 0.0

69
Q

Maximum Operating Altitude

A

25,000’

70
Q

Maximum Altitude for Air Start

A

20,000’

71
Q

Minimum Allowable De-Ice Boot Pressure

A

17 psig

72
Q

Propeller De-Icing System must be switched on…

A

when flying in visible moisture below 5ºC

73
Q

Engine Inlet Anti-Icing should be used…

A

in flight continuously during expected icing conditions

74
Q

If ice has accumulated, de-ice engines…

A

one at a time

75
Q

Engine Inlet Anti-Icing should NOT be used…

A

when icing conditions do not exist, at OAT above 5ºC, for longer than 10 seconds

76
Q

Maximum Pitot Tube Ground Operating Duration

A

60 seconds

77
Q

Hydraulic Motor Duty Cycle Limits

A

25 minutes ON . . . 15 minutes OFF

78
Q

Maximum Permissible Starter-Generator Load

A

300 amps

79
Q

Starter-Generator Duty Cycle Limits

A

30 seconds ON . . . 1 minute OFF
30 seconds ON . . . 1 minute OFF
30 seconds ON . . . 15 minutes OFF

80
Q

Maximum Landing Light Ground Operating Time Limit

A

5 minutes ON . . . 5 minutes OFF

81
Q

AC/DC Inverter Operating Limits

A

Normal: 450 VA
Transient: 600 VA for 1 minute

CASA 212 Erickson (8 decks)

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