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
Main rotor mast moment limits (circular scale) - Showed when
Showed when Nro is avbove 70%
29
Prohibited flight maneuvers:
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.
30
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - Max. TOT starting FLI - 8.5 Time - N/A Torque - N/A TOT - 785C
31
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - TOT starting transient FLI - 11 Time - 5sec Torque - N/A TOT - 865C
32
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - TOT starting range FLI - N/A Time - N/A Torque - N/A TOT - N/A
33
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - AEO takeoff power range; max. 5 min FLI - 8.5 Time - 5min Torque - 71% TOT - 845C
34
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - OEI max. continuous power FLI - 11 Time - N/A Torque - 91.5% TOT - 845C
35
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - AEO max. takeoff power FLI - 10 Time - 5 min Torque - 88% TOT - 845C
36
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - OEI 2.5 min. power FLI - 12 Time - 2.5 min Torque - 125% TOT - 885C
37
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - OEI transient; max. 12 sec. FLI - 14 Time - 12 sec Torque - 140% TOT - N/A
38
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - AEO transient; max. 12 sec. FLI - 10.5 Time - 12 sec Torque - 97% TOT - N/A
39
Rotor starting/stopping in high wind:
Max 50kts from all HORIZONTAL directions
40
Hover turns: With gross mass \<3200 kg With gross mass \>3200 kg
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
Slope operation limits: Left Right Up Down
Left - max. 11\* Right - max. 6\* Up - max. 8\* Down - max. 8\*
44
Minimum Flight crew:
1 Rated pilot
45
Maximum number of occupants in the aircraft:
11
46
Maximum gross weight:
3585 kg 7905 lbs
47
Minimum gross mass:
1750 kg 3858 lbs
48
Loading limits:
600 kg/m^2 123 lb/ft2
49
Tie-down ring limits:
70 kg 152 lbs
50
Lateral center of gravity limits: \<3000kg: \>3000kg:
\<3000kg: 100mm \>3000kg: 80mm
51
Airspeed limitations: VNE for OEI VNE for steady autorotation
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
Altitude limitations:
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
Environmental operation conditions (in Heavy smoke etc:)
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
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:
1: -45C 2: -30C 3: +10C 4: ISA + 35 C (Max 50C)
55
Battery temperature limits:
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
Rotor RPM limitations:
58
Engine oil pressure limits Minimum Caution range Continous operation Maximum continous
Minimum: 1.3 bar Caution range: 1.3 - 1.5 bar Continous operation: 1.5 - 5 bar Maximum continous: 5 bar
59
Engine starter/generator energize times
60
Engine ventilation limits:
61
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:
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
Max continous load pr generator:
200 A
65
Total max continous load with both generators:
360 A
66
DC system/generator normal operating range:
Voltage: 28.5 +/- 0.3 V Current: 0A - 200 A
67
Main transmission oil pressure limits: Minimum Caution range Continuous opration Maximum
Minimum: 1 bar Caution range: 1.0 - 1.5 bar Continuous opration: 1.5 - 5 bar Maximum: 5 bar
68
Main transmission oil temperature: Continuous operation Maximum
Continuous operation: -10C - 105C Maximum: 105C
69
Hydraulic system fluid quantities: #1 System: #2 System:
#1 System: 1.0L #2 System: 1.2L
70
Main rotor mast moment limits indicaitons (linear scale)
71
Main rotor mast moment limits (circular scale) - Showed when
Showed when Nro is avbove 70%
72
Prohibited flight maneuvers:
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
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - Max. TOT starting FLI - 8.5 Time - N/A Torque - N/A TOT - 785C
74
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - TOT starting transient FLI - 11 Time - 5sec Torque - N/A TOT - 865C
75
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - TOT starting range FLI - N/A Time - N/A Torque - N/A TOT - N/A
76
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - AEO takeoff power range; max. 5 min FLI - 8.5 Time - 5min Torque - 71% TOT - 845C
77
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - OEI max. continuous power FLI - 11 Time - N/A Torque - 91.5% TOT - 845C
78
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - AEO max. takeoff power FLI - 10 Time - 5 min Torque - 88% TOT - 845C
79
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - OEI 2.5 min. power FLI - 12 Time - 2.5 min Torque - 125% TOT - 885C
80
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - OEI transient; max. 12 sec. FLI - 14 Time - 12 sec Torque - 140% TOT - N/A
81
Describe Name, FLI, Time, Torque and TOT of the figure below
Name - AEO transient; max. 12 sec. FLI - 10.5 Time - 12 sec Torque - 97% TOT - N/A
82
Rotor starting/stopping in high wind:
Max 50kts from all HORIZONTAL directions
83
Hover turns: With gross mass \<3200 kg With gross mass \>3200 kg
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
Slope operation limits: Left Right Up Down
Left - max. 11\* Right - max. 6\* Up - max. 8\* Down - max. 8\*