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PPC Study > AS350 B2 > Flashcards

AS350 B2 Flashcards

1
Q

MGW

A

4961 lbs

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2
Q

Lateral CG Limits

A

Left 7.08 inches
Right 5.51 inches

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3
Q

Longitudinal CG Limits

A

124.8 in to 137.8 in, weight dependent

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4
Q

VNE

A

155kts
Reduce by 3kts/1000’

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5
Q

VNE below -30

A

Subtract 10 kts

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6
Q

VNE Power Off

A

125kts
Reduce by 3kts/1000’

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7
Q

VNE Power Off below -20

A

Reduce by 20kts, not below 65kts

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8
Q

VNE Doors Off

A

110kts or 100kts or VNE depending on configuration

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9
Q

Max Pressure Altitude

A

20k

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10
Q

Min Temperature

A

-40

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11
Q

Maximum Operating Temperature

A

50

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12
Q

Flight in Falling Snow Limits with FDC Filter

A

1/2 mile vis no time limit

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13
Q

Main Rotor Power On on ground

A

380 +/- 5 rpm

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14
Q

Main Rotor Power On in Flight

A

390 +4, -5 rpm

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15
Q

Main Rotor Power Off

A

320-430 rpm

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16
Q

Warning Horn

A

Main Rotor:
Below 360 continuous
Above 410 intermittent

Hydraulic pressure below 30 Bar

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17
Q

Rotor Brake

A

Max 170 RPM (high winds)
140 normal
5 min between braking

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18
Q

Torque A/S less than 40kts

A

100%

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19
Q

Torque A/S Less than 40kts Transient

A

107% for 10s

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20
Q

Torque A/S 40kts plus

A

94%

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21
Q

NG Transient

A

+6, less than 5s

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22
Q

NG 5 Min T/O

A

0

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23
Q

NG 5 Min Takeoff P2 Bleed

A

-.6

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24
Q

NG Max Continuous

A

-3.5

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25
Q

T4 Max During Start

A

795

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26
Q

T4 Transient During Start

A

865 5s

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27
Q

Max t4 Takeoff

A

845

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28
Q

MCP T4

A

795

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29
Q

Free Turbine (N2) MCP

A

417 rpm

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30
Q

Free Turbine Transient

A

5 Seconds 330 min, 463 max

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31
Q

Emergency Gasoline Use 4 parts

A

Max 25 hrs between engine overhauls
Add 2% mineral oil if possible
Max 1500’PA
Max fuel temp 30C

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32
Q

Oil Pressure Min above 85% NG

A

1.8 bar

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33
Q

Oil Pressure Min between 70 and 85% NG

A

1.3 bar

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34
Q

Max Oil Pressure outside start sequence

A

5 bar

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35
Q

Oil Temp

A

0-115C

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36
Q

Normal Voltage

A

26-29 V

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37
Q

Max Voltage

A

31.5

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38
Q

Max Current

A

150Amp

39
Q

Nose Up Slope

A

10

40
Q

Nose Down Slope

A

6

41
Q

Sideways slope

A

8

42
Q

MR diameter

A

35ft

43
Q

Overall Length

A

42.45ft

44
Q

Max Climb

A

55kts

45
Q

Heating and Demisting T4 Check

A

Above OAT 10C

46
Q

Fuel Capacity

A

143 Gallons

47
Q

Usable fuel Low Fuel Light

A

15.8G
18 min

48
Q

Unusable Fuel

A

.33G

49
Q

Hydraulic Failure Speed

A

40-60kias
Banks less than 30 degrees

50
Q

Max Sling load

A

2557lbs

51
Q

Max External GW

A

5512lbs

52
Q

VNE External Load

A

80kts

53
Q

Cabin Floor Rear Limit

A

682lbs

54
Q

Cabin floor LH Limit

A

330lbs

55
Q

Rear Hold Limit

A

176lbs

56
Q

LH Hold Limit

A

264 lbs

57
Q

RH Hold Limit

A

220lbs

58
Q

Auto Speed

A

65kts

59
Q

Normal Relight Cieling

A

13k

60
Q

TR Control Failure Speed

A

70kts

61
Q

Fin Control Speed

A

20kts

62
Q

Utility Basket VNE Auto

A

100kts

63
Q

VNE Cargo Mirror

A

145kts

64
Q

High Engine Oil Temp Speed

A

80kts

65
Q

NG Failure below 15C

A

730C T4

66
Q

NG Failure above 15C

A

T4 750C

67
Q

Min Voltage Gen Failure

A

22V

68
Q

Door Light Speed

A

70kts

69
Q

Fuel Pressure Altitude both pumps faulty

A

5000’

70
Q

4 Items that must remain on when flying on battery only

A

Battery, Fuel Pump, VHF, Radio Nav

71
Q

Large drop in fuel flow #s

A

Ng stable below 70%
Get up to 70%
Increase collective 350rpm
Increase fuel flow 380rpm
Level flight

72
Q

Fuel P (Amber)

A

Fuel Pressure
Lower than .2 Bar

Check Pressure, If Normal (One Pump Faulty) Continue Flight
If Zero, Both pumps faulty, Continue Flight Below 5000’

73
Q

F Filt (Amber)

A

Fuel Filter Clogging

Reduce Power, If light goes out: continue

If Light remains on: Land ASAPoss

74
Q

CHIP MGB

A

Main Rotor Gearbox Chip

Land as soon as possible
Reduce Power
Monitor Main Gearbox Temp and Pressure Lights

75
Q

CHIP TGB

A

Tail Rotor Gearbox Chip

Continue Flight, avoid prolonged hovering

76
Q

ENG Chip

A

Engine Chip

Land As Soon As Possible
Take off prohibited until MX

77
Q

PITOT

A

Check Push button
Monitor ASI

78
Q

DOORS

A

Slow down to 70kts
Land as soon as practical, use a low rate of descent

79
Q

FUEL

A

Fuel Level Low

15.8 Gal (18 Min @ MCP)
Avoid Large attitude changes

80
Q

HORN

A

Horn not set
Check button

81
Q

BATT

A

Battery isolated from DC Network

Check button on: Switch on and continue flight
If already on, monitor voltage and land ASAPrac

82
Q

GEN

A

Generator Failure or Over Voltage
Check Voltage and Gen button
Reset Gen
Shed electrical load: 22V Minimum. Batt, Boost Pumps, and VHF Reqd
Land ASAPrac

83
Q

Eng P

A

Engine Oil Pressure
Reduce Power
Check Torque
Low Reading: Shut Down Eng
Normal Reading: Land Immediately
If Both Gauges Correct: Land ASAPoss

84
Q

MGB P

A

Main Gearbox Oil Press

Land ASAPoss, Reduce Power

85
Q

HYD (HIGE, Takeoff, Final)

A

Land normally within 30s
Fuel Idle
Collective Locked
Shutdown

86
Q

HYD (In Flight)

A

Establish Level 40-60kts
Cutoff Switch Off
Land ASAPoss
Flat approach into wind
Running landing @ 10kts
Idle and lock collective
Shutdown

87
Q

Fuel Pressure Guage Failure

A

Confirm with FUEL P or F FILT light, if gauge faulty continue flight

88
Q

Low Eng Oil Pressure (Below 1.8 bar when above 85% NG)

A

Test ENG P Light and cross reference Torque
If all low - auto
Otherwise Land ASAPoss

89
Q

Eng Oil Temp High

A

In Hover - Land, stop, check cooler fan
Landing impossible - Increase speed 80kts, reduce power, if temp does not reduce land ASAPoss

90
Q

NG Gauge Failure Below 15C

A

T4 Limit 730C

91
Q

NG Guage Failure above 15C

A

T4 Limit 750

92
Q

Torque meter Failure

A

Limit NG as per chart

93
Q

T4 Failure

A

Comply with NG Limits
Do not start

94
Q

Oil cooler on

A

77C

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