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Helicopters > 407 135 Chekride > Flashcards

407 135 Chekride Flashcards

1
Q

Run-On Landing Definition

A

Forward ground travel of greater than 3 feet

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2
Q

Passenger Deck Loading Limit

A

75 PPSI

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3
Q

Cargo Deck Loading Limit

A

86 PPSI

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4
Q

What is the minimum pilot weight?

A

170

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5
Q

Who set the minimum pilot weight, and why?

A

RLC, So we can do selective loading

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6
Q

Which Fadec Version are we on?

A

5.4

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7
Q

Maximum approved weight?

A

5250

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8
Q

Minimum gross weight?

A

2650

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9
Q

Basic VNe

A

140KIAS

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10
Q

VNe at takeoff Power

A

100

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11
Q

AutoRotation VNe

A

100

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12
Q

Maximum speed for Sideward or Rearward flight

A

35 KIAS

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13
Q

Max Operating alt

A

<5000lbs, 20k
>5000lbs 11k

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14
Q

Max Rate of Climb

A

2000FPM

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15
Q

Slope Limitations

A

10 degrees sideways
10 degreees nose up
5 degrees nose down

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16
Q

When is engine anti ice required?

A

5c with visible moisture

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17
Q

Generator Continous OP Range

A

0 -180 amps

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18
Q

Generator Max continuous Amps

A

180 amps

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19
Q

Generator Transient Ranges ( 2 )

A

180 - 300 amps 2 MINUTES
300 - 400 400 amps 5 SECONDS

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20
Q

Powerplant Type

A

Rolls Royce 250 - C47B

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21
Q

What is Ng

A

Gas Producer, Brings air into Engine

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22
Q

Ng Continuous limits

A

63 - 105%

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23
Q

Ng Max Continuous

A

105%

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24
Q

Ng Transient Limit

A

105.1 - 106.5 % 10 Seconds

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25
Q

What is Np

A

Power Turbine, Supplies power to the rotor

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26
Q

Np Avoid Section

A

68.4 - 87.1%

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27
Q

Np Continuous operations

A

99 - 100%

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28
Q

Np Max Transient

A

102.1 - 107.3% 15 Seconds

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29
Q

MGT Continous

A

100 - 727c

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30
Q

MGT Take Off

A

727 - 779c

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31
Q

MGT Transient

A

780 - 905c 12 seconds

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32
Q

MGT On Start

A

843 - 927, 10 Seconds

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33
Q

Torque Continous

A

0 - 93.5

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34
Q

Torque Take off

A

93.5 - 100%

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35
Q

Torque Transient

A

105% 5 Seconds

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36
Q

Fuel Pressure

A

8 - 25 PSI

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37
Q

Engine Oil Pressure on Start

A

50 PSI below 79% Ng

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38
Q

Oil Pressure Required at 79 - 94% Ng

A

90 PSI

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39
Q

Oil Pressure Required at 94% +

A

115 PSI

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40
Q

Maximum Oil Pressure ( 2 )

A

130 PSI
200 PSI on Cold Starts

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41
Q

Oil Temp

A

0 - 107 c

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42
Q

How to bring Oil Temp Down if in Hover

A

Turn into wind, or take off

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43
Q

Transmission Oil Temp

A

15 - 110c

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44
Q

Transmission Oil Pressure

A

40 - 70 PSI

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45
Q

Minimum Transmission Oil Pressure

A

30 PSI

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46
Q

Rotor RPM, On and OFF

A

On - 99 - 100%
Off - 85 - 107%

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47
Q

When to apply rotor brake?

A

40%

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48
Q

Max Fuel

A

127 Gallons, 850 lbs

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49
Q

Minimum Fuel reserve

A

<20 KTS .5 175 lbs
>20 KTS .75 260 lbs

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50
Q

How do you calculate how much cargo you can hold?

A

1 lb per lb over 170 in front seats, 1lb per 2lbs in mid

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51
Q

What is the weight on Skids for?

A

ADS-b Out
Flight Timer
Cyclic Centering

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52
Q

Define Land as Soon as Practical

A

Landing site and Flight duration are at the pilots discretion. Flight beyond the nearest approved landing area is not recommended

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53
Q

Define Land as soon as Possible

A

Land with out delay to the nearest suitable area where a safe landing can be made

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54
Q

Engine Out Procedure and indication

A

Left Yaw, beeping horn at 55%Ng, Nr
Low collective, maintain Nr between 85 - 107% Preferably above 90%

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55
Q

Engine Underspeed

A

No cation or warming lights
Adjust collective to Cruise, switch to Manual
Land as soon as PRACTICAL

56
Q

Engine Overspeed

A

Increase in Nr, Ng, Np, TRQ
Retard Throttle, Stablize, Fadec Manual
If unable to control engine off, autorotate

57
Q

Engine Compressor Stall

A

Engine Pops and Bangs, High or erratic MGT TRQ Oscillations
Reduce Power, Check for normal conditions
Bleed air systems on
If you decide to continue, Land as soon as Practical
Otherwise enter auto, engine off

58
Q

Engine Hot start

A

Rapidly increase MGT
Cuttoff Throttle at rapid increase nearing 850c

59
Q

Engine Oil Pressure Low, High

A

Engine oil pressure below mins
Below minimum, Land as soon as POSSIBLE
Above Minimums, Monitor, Land as soon as PRACTICAL

60
Q

Engine Oil Temp High

A

Land as soon as Practical

61
Q

Drive Shaft Failure

A

Left Yaw, Rapid Decrease in Nr, Rapid Increase in NP, Low Rotor Horn
Autorotate

62
Q

Fadec Fail

A

Indications: Fadec FAIL, Fadec Manual, Fadec Man Light, “Bing Bong”
Raise Throttle to Cruise, Stabalize RPM, Press Fadec Man, Land as soon as PRACTICAL

63
Q

Fire on ground

A

Throttle off, Fuel off, Gen off, Bat off Rotor Brake on, Leave

64
Q

Engine Fire in flight

A

Enter Autorotation, Throttle off, Fuel Valve off, Batt off after Landing

65
Q

Cabin Smoke

A

Start Descent, Open Vents, Turn Off heat
If source is found and extinguished, land as soon as Practical
If fire isnt extinguished , land as soon as POSSIBLE

66
Q

Loss of tail rotor in flight

A

Roll throttle to idle, Immediatly enter autorotation, Maintain minimum 55 KIAS, A run on style landing with nose high is prefered, cut off throttle before decreasing speed

67
Q

Loss of tail rotor in Hover

A

Cut off Throttle, hover auto

68
Q

Fixed pitch Failure

A

Pedals are unable to move
In Flight Left Pedal: A slow, high powered, almost vertical approach may be required
In Flight right pedal: A Run on may be required with a nose high attitude, cut off throttle if right Yaw is excessive

69
Q

Hydraulic Failure

A

Hydraulic Cation Light, Grinding noise, Increase Control requirements
Reduce Speed to 70 - 100KIAS, Hydraulic Circuit Breaker out, if Restored, Land as soon as Practical, If Not restored, push in and switch off, land as soon as practical

70
Q

Flight Control Actuator/ Hard Over

A

Uncommanded Control movements “ Trying to Kill you”
Turn Off hydraulic switch, 70 to 100 KIAS, Land as soon as POSSIBLE

71
Q

Generator Failure

A

“Gen Fail” Light illuminated
Amps 0
Voltmeter ~ 24
Verify Generrator Circuit Breakers in
Gen Switch - Reset
If not restored, Land as soon as PRACTICAL, about 20 minutes, Turn as much as you can off except transponder and radio and battery, and left boost pump

72
Q

Excessive Load

A

Amps indicate high, smoke or fumes
Batt and Gen off, leave at least left boost on

73
Q

Starter Light in Flight

A

Pull starter circuit breaker to renable Generator, Land as soon as PRACTICAL

74
Q

Engine out Light

A

When Ng below 55%

75
Q

Fadec Fail ( Startup)

A

Serious Malfunction, Cut Throttle

76
Q

Fadec Fail ( In Flight )

A

“Bing Bong”, Serious Malfunction, will switch to manual mode automatically, Raise Collective to Cruise Power and watch RPM, Land as Soon as Practical
“ Cat 1 Fail”

77
Q

Fadec Degraded ( In Flight )

A

Probably using alternate ECU, Nr and Np possible lag, FLy conservatively, MX prior to next flight
“Cat 2 Fail”

78
Q

Fadec Degraded ( ShutDown )

A

at 9.5 Ng, A minor Fault was detected, have MX look over before next flight

79
Q

Fadec fault

A

PMA, MGT, NP, or Ng cicuit may not be functioning, Restart light may also come on
Land as soon as Practical
“Cat 3 Fail”

80
Q

RPM Light

A

Nr below 95%, With audio
With out Audio, Nr above 107%

81
Q

Xmsn Oil Pressure light

A

Below Mins, Reduce Power, Verify with guage, Land as soon as POSSIBLE

82
Q

XMSN Oil Temp light

A

Reduce power, verify with guage, Land as soon as Practical

83
Q

Auto Relight

A

Ignitor Circuit is running

84
Q

Baggage Door Light

A

Baggage Door not Closed, PRACTICAL

85
Q

Battery RLY

A

Has malfunctioned to On Position with battery off
If battery hot, land as soon as Possible, gen off
If it fails off, You may loos all gauges below 55% Ng

86
Q

Check Instrument

A

An exceedance is about to happen or has happens on the TQ, MGT Ng

87
Q

Cyclic Centering

A

Cyclic isnt Centered, on ground

88
Q

Engine Anti Ice

A

Engine Anti Ice On

89
Q

Engine Chip

A

Possible metal in Engine Oil, Land as soon as Possible

90
Q

Fuel Filter Light

A

AirFrame Fuel Filter in impending ByPass, Land as soon as Practical MX

90
Q

Fuel Low

A

100lbs in Rear Tank

91
Q

R/Fuel Boost light

A

Failed, Descend below 8k DA As soon as PRACTICAL

92
Q

L and R/Fuel Boost

A

Both have Failed, Below 8k, Land as soon as PRACTICAL

93
Q

Fuel Valve Light

A

Fuel Valve is in a different position than switch is. You probably just switched it on or off

94
Q

L/Fuel XFR

A

Failed, As Practical

95
Q

R/Fuel XFR

A

Failed, As Practical

96
Q

L & R Fuel XFR

A

Up to 151 lbs can be trapped, Land as soon as Practical

97
Q

Pedal Stop

A

Pedal Rrestrictor Control unit has failed, Vne 60 KIAS, Land as soon as PRACTICAL

98
Q

Restart Fault

A

Fadec ECU has detected a fault, Will not allow engine to be restarted in Auto, Land as accordingly since start wont be possible
When decreasing, throttle PMA may go offline, below 85%

99
Q

T/R and XMSN Chip

A

Metal Particals, Land as soon as Possible

100
Q

9 Sensors in ECU

A

Ng Monopole
Np Monopole
Nr Monopole
TMOP, TRQ meter oil pressure, separate from what supplys gauge
MGT
Ambient Pressure (p1)
Compressor Inlet Temp (CIT)
PLA Power Lever Angle ( Throttle, on HMU)
Collective pitch ( CP ) ( Under Passenger seat)

101
Q

Type of Rotor System

A

4 Bladed soft in plane flex beam rotor system, closest to Fully Articulated. Elastomeric bearings vs dampers
35’ Rotor

102
Q

EOC Level 1 Requirements

A

No additional requirements than typical release

103
Q

EOC Level 2 Requirements

A

Ops Supervisor required to individually release before unstrapping, Aircraft required to be secured

104
Q

EOC Level 3 Requirement

A

Only Director of Ops Can Release

105
Q

Can Cargo be stored with passengers?

A

Only if it is secured with seat belts, not above passengers

106
Q

Why don’t we have to do W&B

A

Selective loading if pilot is 170

107
Q

How do you know you have everything in the aircraft?

A

Aircraft Inventory at beginning of hitch
Airworthiness, Registration, RFM, Aircraft Logbook, MEL, Checklist, Passenger Briefing Card, Tool Kit

108
Q

Crew Currency/Recency

A

C.B.T’s, Annual Check ride, 30 - 60 - 90 Report, 3 T.O. with in 90 days

109
Q

Hazmat Info

A

Make sure Shippers declaration was stamped by RLC or that you have verified it is correct off shore, you can fill out the pilots declaration if needed

110
Q

Approved Weather Sources ( 5 )

A

National Wx Service
A source approved by Nation Wx Services
Foreflight
Aviation Sentry
Fltplan.com

111
Q

VFR Requirements & RLC Minimums

A

Reference to the ground
Not less than 300 feet
RLC Minimums 500 and 3 Miles

112
Q

RLC Wind Limits

A

40 KTS or Gusting 15 Kts

113
Q

Cold Wx Operations and engine rinse

A

Cold wx starts at 40f, no rinse at or below 35f

114
Q

Fuel minimums

A

30 mins if below 20 knts
45 mins above 20 knts

115
Q

Above 30 knots and greater than 60 degree crosswind, what must be done during loading

A

Keep RPM at 100%

116
Q

Run and Hold Policy

A

If a customer wants you to stay running, less than 15 minutes, no charge. Longer add the time to the FSO

117
Q

135 Flight times

A

500 per quarter
800 per two consecutive quarter
1400 per year
8 hours per day
14 hours duty days
If you exceeded, by less than 30 minutes 11 hours, 12, 16

118
Q

Down Time

A

30 minutes before sunset or 30 minutes before 1930

119
Q

Alcohol Policy

A

None within 12 hours of duty time

120
Q

What items are required to be in the Pilots Possession?

A

Pilot Certificate
ID
Medical
Flashlight
EFB: Current Charts, General Operating Manual

121
Q

When is customs documentation Required?

A

Bringing People to or from a not anchored platform or vessel

122
Q

Can we fly into Warning areas?

A

Yes, but contact controlling agency to determine activity

123
Q

How much weight can you put on blades and how far pull down?

A

60lbs and 24” from drooping bladesf

124
Q

What is our Squawk Code?

A

4304

125
Q

When does the low fuel light come on?

A

100lbs

126
Q

What is the fuel burn?

A

350lb/hour or ~6 lb/min

127
Q

What type of Rotor system do we have?

A

4 Bladed, soft in plane, glass epoxy yolk. Uses elastomeric bearing instead of dampers

128
Q

Which two systems fail on?

A

Hydraulic and Engine anti-Ice

129
Q

What electronics will work with the battery turned off?

A

Left Boost Pump and Left Xfer Pump

130
Q

Getting a Fuel Sump and filter sump switch positions

A

Fuel Sump: Bat On, Fuel valve closed, boost & Xfer OFF
Filter Sump: Bat On, Fuel Valve On, Boost and Xfer ON

131
Q

TURN ON TCAS

A

TURN ON TCAS

132
Q

What Voltage does FADEC abort start?

A

10.5 Volts

133
Q

Required Voltage for start

A

24 volts

134
Q

When does PMA power FADEC and what is it?

A

85%, Permanent Magnetic Alternator, powers FADEC

135
Q

What lights are on after the BIT Test

A

LFuel Boost, L/Fuel Xfer, R/Fuel Boost, R/Fuel Xfer, Gen Fail, XMSN oil Press, HYD System, Engine out, RPM

136
Q
A

Helicopters (3 decks)

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