POH R44 Incl Emergency Checks Flashcards

1
Q

Power Fail 8’ - 500’ & Above
AR

A

1) Lower Collective
2) Glide 70kts
3) Adjust Collective 97-108% RPM
4) Ldg Spot
(Restart - for >500’)
(If not- Sw off unnecessary sw & Fuel Valve - for >500’)
40’ Flare
8’ Forward Cyclic Level Ship -
Raise Collective just before TD - (For <8’. Yaw & Settle then)

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2
Q

Engine Fire During Start

A

Crank & try start
If Starts run 60-70% for short time
Fuel Mix Off
Fuel Valve Off
Battery Off
Brake if time
Exit

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3
Q

Engine Fire in Flight

A

** Enter AR **
** Cabin heat off if time, Vent on **

If Engine Running -
Norm Ldg,
Mix Off
Fuel Valve Off

If Eng Stopped-
Fuel Valve Off
AR

Batt Off
Brake if time
Exit

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4
Q

Electrical Fire in Flight

A

** Batt & Alt Off **
Open vents
Land Immediately

Fuel - Mix & Valve Off
Brake if time
Exit

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5
Q

Tacho Fail

A

Use remaining tacho to monitor RPM
Allow governor to control RPM
Land as soon as practical

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6
Q

Oil Warning

A

Indicates loss eng power or oil P
Check gauges
If P Loss confirmed
Land Immediately

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7
Q

MR Temp

A

Indicates excessive T Main Rotor

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8
Q

MR Chip

A

Metallic particles in MR gearbox

If external indications. Land as soon as practical

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9
Q

TR Chip

A

Metallic particles in Tail Rotor
If external indications. Land as soon as practical

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10
Q

Low Fuel

A

10 mins left

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11
Q

Clutch

A

Briefly is ok
>10s
Pull clutch cb
Land as soon as practical
Other indications- reduce power, land immediately

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12
Q

ALT

A

Turn off nonessential
Turn Alt sw off & on
If lt stays on, land as soon as practical Other indications

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13
Q

Starter on

A

Pull mix & Master sw off

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14
Q

Full throttle

A

Lower collective to ext

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15
Q

Low RPM

A

Roll throttle on
Lower collective
Aft cyclic

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16
Q

Limitations
Instruments
Red
Red Hatch
Yellow

A

Red Operating Limit
Red Hatch Power off Vne
Yellow Precautionary or Special Proc Range

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17
Q

Vne

A

2,200lbs TOGW and Below 130
Over 2,200lbs 120
Autorotation 70

For Vne reductions see placard

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18
Q

Max Speed if Power Above MCP
Or if Doors are removed

A

100kias

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19
Q

Rotor Speed
Power On

A

101-102%

(R44s showing green arc 99-102%, can do 99%

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20
Q

Rotor Speed
Power Off

A

90-108%
Transient at lower ok

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21
Q

Power Plant
Engine speed %
Max
Max Transient

A

102%
105%
(Works PT 2 to 5)

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22
Q

Power Plant
Cylinder Head Max T
Oil T max

A

260C (Too sexy head)
118C (oily legs w snake)

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23
Q

Power Plant
Oil Q

A

7-9USQ

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24
Q

Weight Limits
Max Gross
Min Gross

A

2,400lbs
1,550lb

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25
Q

Weight
Max per seat
Baggage

A

300lb
50lb

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26
Q

C of C
Datum position

A

100” forward of main rotor shaft

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27
Q

Weights
Min for solo pilot

A

150lb

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28
Q

Max Operating Alt

A

Density Alt 14,000’
AGL 9,000’ to allow landing in 5 minutes in case of fire

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29
Q

Fuel Used at School

A

100LL Blue
Avgas

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30
Q

Fuel Capacity Useable/Total
With Bladders
Main
Aux
Total

A

29.5USG +1
17USG + .2
46.5

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31
Q

Carb Icing
Yellow Arc
Practical

A

-19C to +3C (3mins past 7pm yellow time)
-4C to +30C if Dew Pt & Temp within 15C

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32
Q

Definition
CAT
CHT

A

Carburetor Air T
Cylinder Head T

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33
Q

Balance
Moment=

A

Weight of item multiplied by its arm

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34
Q

Balance Definition
Standard Empty Weight
Basic Empty Weight

A

Standard- Heli Including unusable fuel, fluids, full Oil (Standard out of the box!)
Basic- Standard Empty Weight plus installed operational equipment (basic as customer wanted!)

35
Q

Temperature
F=

A

F= 9/5 (C) + 32

36
Q

Immediately After Start memory

A

Starter Light Out
Oil Pressure in 30s in Green
All Switches On
Clutch and Stopwatch
Engine 50-60%
Blades turn (5s… ish)

37
Q

Radio Frequencies CYND

A

Gatineau Ground Advisory 122.6
Gatineau Radio 122.3
Traffic Advisory 126.7

38
Q

Dim
Length Heli

A

459”

39
Q

Dim
Total Height

A

129”

40
Q

Dim
Radius Blade

A

198”

41
Q

Voltage R44

A

28V

42
Q

Hover Checks

A

Skids Free
Controls Working
CofG ok
Warning Lights Out
Gauges in the Green
MaP

43
Q

Engine

A

Lycoming 540 F1 B1
6 Cylinder Horizontally Opposed
Direct Drive, Air Cooled
Carbureted, Normally Aspirated
260BHP at 2800rpm

44
Q

Fuel Flow
Ticks Main & Aux
Endurance & Reserves Min

A

15USG/hr
Main Ticks every 30 minutes
Aux Tank Ticks every 15min
Endurance 3 hours
20 mins needed for Reserve

45
Q

Vy
V Max Range
V Autorotation

A

55
100
70

46
Q

Dimensions
Width (skids)

A

86”

47
Q

BHP De-Rated

A

225 TOP
205 Max Con

48
Q

Max Weight

A

2,400lb

49
Q

Oil Used in School

A

W15W-50

50
Q

Before Liftoff (7)

A

Doors & s/b
Governor & Hydraulics
RPM
W Lts Gauges Green
Nav / Ldg Lts
Carb Heat Closed
Area & Traffic

51
Q

After Take Off (4)
500’ AGL
Standard checks

A

MaP
Warning Lights
Gauges
Carb Heat
Traffic & Area

52
Q

On Takeoff to Accelerate

A

Traffic & Area
Airspeed Alive 45kts
Altimeter Alive Positive Climb

53
Q

Approach

A

W Lights out Gauges Green
Nav / Landing lights
Carb H, Traffic & Area

54
Q

Before Liftoff (7)

A

Doors & s/b
Governor & Hydraulics
RPM
W Lts Gauges Green
Nav / Ldg Lts
Carb Heat Closed
Area & Traffic

55
Q

Minimum Rate of Descent

A

*airspeed 55 KIAS (t flat top in rate)
*rotor RPM 90%
*minimum rate of descent is about 1350 ft per minute
Ratio 4:1 or 1 nm per 1500 ft AGL

97% below 500’

56
Q

Maximum Glide Configuration

A

*airspeed 90 KIAS
*rotor RPM 90%
*best glide ratio 4.7:1
1 nm per 1300 ft AGL

Minimum 97% below 500’

57
Q

Stuck Pedal

A

Stabilizer Works at 70kts
At 60kts identify power to maintain S&L flight
>17” MaP - Left yaw - use collective to yaw
On landing control yaw with collective
If left yaw- raise collective
Pump collective to lose height
Yaw right - throttle off
Yaw left - pump

58
Q

Mayday call format

A

M M M
Ident 3
Nature
Intentions
T- Position- Location, Alt, Speed, Direction, AND Souls Onboard
Ident
1

59
Q

How many feet in a Mile?

A

1 mile is 5,280’

60
Q

How many feet in a nm

A

6,076’

61
Q

How many feet in a nm

A

6,076’

62
Q

Rotor Diameter

A

33’

63
Q

Engine Cooling

A

Direct Drive Squirrel Cage Blower

64
Q

ISA

A

29.92” of mercury
SL 15C
1.98C/1000’

65
Q

Density Altitude

A

Pressure Alt corrected for T

66
Q

Pressure Altitude

A

Alt indicated when 29.92” set

67
Q

Where MaP measured at

A

Engine Intake Manifold

68
Q

TOP means
& Time

A

Take Off Power
5 minutes

69
Q

Critical Altitude

A

Alt at which full throttle produces max allowable power (MCP or TOP)

70
Q

Mayday

A

Grave & imminent danger

Life threatening & Imm assist required

A situation where safety is being threatened by grave and imminent danger and requires immediate assistance.

71
Q

Pan

A

Threat to safety but not require Imm assist

A situation where the safety of an aircraft or other vehicle, or of some person on board or within sight is threatened, but does not require immediate assistance.

72
Q

1nm cf sm

A

1nm = 1sm + 15%

73
Q

Do not exceed …. Except in smooth air

A

110

74
Q

Indications of an Engine Failure

A

Change in noise
Nose Left Yaw
Oil pressure light
Decreasing engine RPM

75
Q

Indication of Drive System Failure

A

Unusual noise or vibration
Nose right or left yaw
Decreasing rotor RPM while Engine RPM is increasing

76
Q

Water landing power off

A

If time permits unlatch doors
Lateral cyclic to stop rotors

77
Q

Water Landing power on

A

Hover
Unlatch doors
Passengers exit
Move
Sw battery off
Roll throttle off overtravel spring
Level & full collective as contact water
Lateral cyclic stop rotors

78
Q

Loss Tail Rotor in Forward Flight

A

AR
>=70
Select landing site, roll throttle off into overtravel spring
AR landing
If no landing site- may be ok 70 for controlled flight, however prior reduce speed, enter full AR

79
Q

Loss Tail Rotor in Hover

A

Imm roll Throttle off into overtravel spring
Settle
Raise collective just before t/d

80
Q

Headset fail

A

No Low RPM Horn
LaSaP

81
Q

What’s lost if battery & Alternator off

A

Governor & Low RPM Horn

82
Q

Hydraulic sys fail

A

Verify sw on
If not restored, sw off
Lasapractical

83
Q

Governor Fail

A

Grip throttle firmly & sw off governor

84
Q

What’s Low RPM light mean

A

Indicates rotor speed below 97%
Imm lower collective
Roll throttle on
& in forward flight aft cyclic