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P2 Evaluation Sequence questions > ACAT.05 Limits > Flashcards

ACAT.05 Limits Flashcards

1
Q

Minimum Flight crew:

A

1 Rated pilot

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2
Q

Maximum number of occupants in the aircraft:

A

11

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3
Q

Maximum gross weight:

A

3585 kg

7905 lbs

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4
Q

Minimum gross mass:

A

1750 kg

3858 lbs

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5
Q

Loading limits:

A

600 kg/m^2

123 lb/ft2

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6
Q

Tie-down ring limits:

A

70 kg

152 lbs

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7
Q

Lateral center of gravity limits:

<3000kg:

>3000kg:

A

<3000kg: 100mm

>3000kg: 80mm

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8
Q

Airspeed limitations:

VNE for OEI

VNE for steady autorotation

A

VNE for OEI operations under all conditions is 110kts or as shown in the VNE table, whichever is less

VNE for steady autorotation under all conditions is 90kts or as shown in the VNE table, whichever is less

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9
Q

Altitude limitations:

A

Max operation altitude: 18.000 ft PA

Maximum operation altitude for hove IGE / takeoff and landing: 18.000 ft DA or 18.000 ft PA, whichever is less

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10
Q

Environmental operation conditions

(in Heavy smoke etc:)

A

Flight is restricted to 30 minutes with NACA inlets closed.

If CPDS OHVT caution comes on during the 30 minutes, proceed according to CPDS OVHT caution indication (another 30 minutes).

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11
Q

Ambient air temperature limits:

1 - Minimum air temp with cold weather kit:

2 - Minimum air temp without cold weather kit:

3 - Minimum air temp with bleed air heating defective:

4 - Maximum air temp:

A

1: -45C
2: -30C
3: +10C
4: ISA + 35 C (Max 50C)

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12
Q

Battery temperature limits:

A

For engine start-up at outside air temperatures below -20C using the A/C battery, the ac battery shall be preheated to at least -20C.

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13
Q

Rotor RPM limitations:

A
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15
Q

Engine oil pressure limits

Minimum

Caution range

Continous operation

Maximum continous

A

Minimum: 1.3 bar

Caution range: 1.3 - 1.5 bar

Continous operation: 1.5 - 5 bar

Maximum continous: 5 bar

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16
Q

Engine starter/generator energize times

A
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17
Q

Engine ventilation limits:

A
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18
Q

Engine oil temperature

Minimum for starting:

Oil viscosity 3 cSt and 3.9 cSt .

Oil viscosity 5 cSt

Minimum for power application:

Oil viscosity 3 cSt and 3.9 cSt

Oil viscosity 5 cSt

Maximum operating temperature:

A

Minimum for starting:

3 cSt and 3.9 cSt: -45C

5 cSt: -40C

Minimum for power application:

3 cSt and 3.9 cS: -10C

5 cSt: 0C

Maximum operating temperature: 115C

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21
Q

Max continous load pr generator:

A

200 A

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22
Q

Total max continous load with both generators:

A

360 A

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23
Q

DC system/generator normal operating range:

A

Voltage: 28.5 +/- 0.3 V

Current: 0A - 200 A

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24
Q

Main transmission oil pressure limits:

Minimum

Caution range

Continuous opration

Maximum

A

Minimum: 1 bar

Caution range: 1.0 - 1.5 bar

Continuous opration: 1.5 - 5 bar

Maximum: 5 bar

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25
Q

Main transmission oil temperature:

Continuous operation

Maximum

A

Continuous operation: -10C - 105C

Maximum: 105C

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26
Q

1 System:

Hydraulic system fluid quantities:

A

1 System: 1.0L

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27
Q

Main rotor mast moment limits indicaitons (linear scale)

A
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28
Q

Main rotor mast moment limits (circular scale)

  • Showed when
A

Showed when Nro is avbove 70%

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29
Q

Prohibited flight maneuvers:

A

Aerobatic maneuvers

Intentional full autorotation landings

Flight into icing condition. In case that icing condition are entered unexpectedly, the icing zone shall be left in the quickest possible way.

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30
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - Max. TOT starting

FLI - 8.5

Time - N/A

Torque - N/A

TOT - 785C

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31
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - TOT starting transient

FLI - 11

Time - 5sec

Torque - N/A

TOT - 865C

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32
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - TOT starting range

FLI - N/A

Time - N/A

Torque - N/A

TOT - N/A

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33
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - AEO takeoff power range; max. 5 min

FLI - 8.5

Time - 5min

Torque - 71%

TOT - 845C

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34
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - OEI max. continuous power

FLI - 11

Time - N/A

Torque - 91.5%

TOT - 845C

35
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - AEO max. takeoff power

FLI - 10

Time - 5 min

Torque - 88%

TOT - 845C

36
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - OEI 2.5 min. power

FLI - 12

Time - 2.5 min

Torque - 125%

TOT - 885C

37
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - OEI transient; max. 12 sec.

FLI - 14

Time - 12 sec

Torque - 140%

TOT - N/A

38
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - AEO transient; max. 12 sec.

FLI - 10.5

Time - 12 sec

Torque - 97%

TOT - N/A

39
Q

Rotor starting/stopping in high wind:

A

Max 50kts from all HORIZONTAL directions

40
Q

Hover turns:

With gross mass <3200 kg

With gross mass >3200 kg

A

With gross mass <3200 kg - Max 45*/s (8 seconds for a 360* turn)

With gross mass >3200 kg - Max 30*/s (12 seconds for a 360* turn)

43
Q

Slope operation limits:

Left

Right

Up

Down

A

Left - max. 11*

Right - max. 6*

Up - max. 8*

Down - max. 8*

44
Q

Minimum Flight crew:

A

1 Rated pilot

45
Q

Maximum number of occupants in the aircraft:

A

11

46
Q

Maximum gross weight:

A

3585 kg

7905 lbs

47
Q

Minimum gross mass:

A

1750 kg

3858 lbs

48
Q

Loading limits:

A

600 kg/m^2

123 lb/ft2

49
Q

Tie-down ring limits:

A

70 kg

152 lbs

50
Q

Lateral center of gravity limits:

<3000kg:

>3000kg:

A

<3000kg: 100mm

>3000kg: 80mm

51
Q

Airspeed limitations:

VNE for OEI

VNE for steady autorotation

A

VNE for OEI operations under all conditions is 110kts or as shown in the VNE table, whichever is less

VNE for steady autorotation under all conditions is 90kts or as shown in the VNE table, whichever is less

52
Q

Altitude limitations:

A

Max operation altitude: 18.000 ft PA

Maximum operation altitude for hove IGE / takeoff and landing: 18.000 ft DA or 18.000 ft PA, whichever is less

53
Q

Environmental operation conditions

(in Heavy smoke etc:)

A

Flight is restricted to 30 minutes with NACA inlets closed.

If CPDS OHVT caution comes on during the 30 minutes, proceed according to CPDS OVHT caution indication (another 30 minutes).

54
Q

Ambient air temperature limits:

1 - Minimum air temp with cold weather kit:

2 - Minimum air temp without cold weather kit:

3 - Minimum air temp with bleed air heating defective:

4 - Maximum air temp:

A

1: -45C
2: -30C
3: +10C
4: ISA + 35 C (Max 50C)

55
Q

Battery temperature limits:

A

For engine start-up at outside air temperatures below -20C using the A/C battery, the ac battery shall be preheated to at least -20C.

56
Q

Rotor RPM limitations:

A
58
Q

Engine oil pressure limits

Minimum

Caution range

Continous operation

Maximum continous

A

Minimum: 1.3 bar

Caution range: 1.3 - 1.5 bar

Continous operation: 1.5 - 5 bar

Maximum continous: 5 bar

59
Q

Engine starter/generator energize times

A
60
Q

Engine ventilation limits:

A
61
Q

Engine oil temperature

Minimum for starting:

Oil viscosity 3 cSt and 3.9 cSt .

Oil viscosity 5 cSt

Minimum for power application:

Oil viscosity 3 cSt and 3.9 cSt

Oil viscosity 5 cSt

Maximum operating temperature:

A

Minimum for starting:

3 cSt and 3.9 cSt: -45C

5 cSt: -40C

Minimum for power application:

3 cSt and 3.9 cS: -10C

5 cSt: 0C

Maximum operating temperature: 115C

64
Q

Max continous load pr generator:

A

200 A

65
Q

Total max continous load with both generators:

A

360 A

66
Q

DC system/generator normal operating range:

A

Voltage: 28.5 +/- 0.3 V

Current: 0A - 200 A

67
Q

Main transmission oil pressure limits:

Minimum

Caution range

Continuous opration

Maximum

A

Minimum: 1 bar

Caution range: 1.0 - 1.5 bar

Continuous opration: 1.5 - 5 bar

Maximum: 5 bar

68
Q

Main transmission oil temperature:

Continuous operation

Maximum

A

Continuous operation: -10C - 105C

Maximum: 105C

69
Q

1 System:

Hydraulic system fluid quantities:

A

1 System: 1.0L

70
Q

Main rotor mast moment limits indicaitons (linear scale)

A
71
Q

Main rotor mast moment limits (circular scale)

  • Showed when
A

Showed when Nro is avbove 70%

72
Q

Prohibited flight maneuvers:

A

Aerobatic maneuvers

Intentional full autorotation landings

Flight into icing condition. In case that icing condition are entered unexpectedly, the icing zone shall be left in the quickest possible way.

73
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - Max. TOT starting

FLI - 8.5

Time - N/A

Torque - N/A

TOT - 785C

74
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - TOT starting transient

FLI - 11

Time - 5sec

Torque - N/A

TOT - 865C

75
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - TOT starting range

FLI - N/A

Time - N/A

Torque - N/A

TOT - N/A

76
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - AEO takeoff power range; max. 5 min

FLI - 8.5

Time - 5min

Torque - 71%

TOT - 845C

77
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - OEI max. continuous power

FLI - 11

Time - N/A

Torque - 91.5%

TOT - 845C

78
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - AEO max. takeoff power

FLI - 10

Time - 5 min

Torque - 88%

TOT - 845C

79
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - OEI 2.5 min. power

FLI - 12

Time - 2.5 min

Torque - 125%

TOT - 885C

80
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - OEI transient; max. 12 sec.

FLI - 14

Time - 12 sec

Torque - 140%

TOT - N/A

81
Q

Describe Name, FLI, Time, Torque and TOT of the figure below

A

Name - AEO transient; max. 12 sec.

FLI - 10.5

Time - 12 sec

Torque - 97%

TOT - N/A

82
Q

Rotor starting/stopping in high wind:

A

Max 50kts from all HORIZONTAL directions

83
Q

Hover turns:

With gross mass <3200 kg

With gross mass >3200 kg

A

With gross mass <3200 kg - Max 45*/s (8 seconds for a 360* turn)

With gross mass >3200 kg - Max 30*/s (12 seconds for a 360* turn)

86
Q

Slope operation limits:

Left

Right

Up

Down

A

Left - max. 11*

Right - max. 6*

Up - max. 8*

Down - max. 8*

P2 Evaluation Sequence questions (8 decks)

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