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Archive > 1H-65D-1 14March2016 > Flashcards

1H-65D-1 14March2016 Flashcards

1
Q

<p>What system provides VOR/ILS with vertical runway deviation?</p>

A

<p>Glideslope

1H-65D-1
Page 1-D-20</p>

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2
Q

<p>What system provides VOR/ILS with lateral runway deviation?</p>

A

<p>Localizer

1H-65D-1
Page 1-D-20</p>

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3
Q

<p>What channels do you use when doing TACAN Air to Air?</p>

A

<p>Y-Channels

1H-65D-1
Page 1-D-21</p>

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4
Q

<p>When will your Glideslope and/or Localizer Flags come into view?</p>

A

<p>When a localizer frequency is selected and received but there is a loss of signal strength or validity from glideslope or localizer.

1H-65D-1
Page 1-D-12</p>

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5
Q

<p>What form is used for Recommendation for change of a flight publications?</p>

A

<p>AF-847

1H-65D-1
Page xxxi</p>

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6
Q

<p>What channels do you use when doing TACAN Air to Ground?</p>

A

<p>X-Channel

1H-65D-1
Page 1-D-21</p>

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7
Q

<p>what is the maximum unrestricted gross weight of the MH-65D?</p>

A

<p>8,900 pounds

1H-65D-1
Page 1-A-2</p>

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8
Q

Restricted operations for the MH-65 many be done at what weight?

A

9,480 pounds

1H-65D-1
Page 1-A-2

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9
Q

<p>How are airframe components (such as engines and generators) labelled?</p>

A

<p>#1 left side and #2 right side

1H-65D-1
Page 1-A-2</p>

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10
Q

<p>How are avionics components labeled on the MH-65D?</p>

A

<p>#1 ride side and #2 left side

1H-65D-1
Page 1-A-2</p>

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11
Q

How is the WCA panel powered in the MH-65D?

A

Each light bulb in the individual indicator modules are powered by separate nonshed 28DC buses

1H-65D-1
Page 1-A-6

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12
Q

<p>What does the BRIGHT/DIM button on the WCA panel do?</p>

A

<p>Controls the intensity of both light bulbs

1H-65D-1
Page 1-A-6</p>

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13
Q

<p>When does the Master WARNING light come on?</p>

A

<p>After pressing the WCA TEST button or when a warning light on the WCA panel illuminates

1H-65D-1
Page 1-A-6</p>

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14
Q

<p>What is used to limit the compressive load to the occupant's spine during G-loading?</p>

A

<p>Variable Load Energy Absorber build into the P, CP, FM seat

1H-65D-1
Page 1-A-8</p>

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15
Q

<p>Who can authorize removal of safety belts?</p>

A

<p>Pilot-in-Command (PIC)

1H-65D-1
Page 1-A-8</p>

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16
Q

<p>What is used to adjust the left and right movements of the RS seat?</p>

A

<p>Forward left handle under the seat

1H-65D-1
Page 1-A-8</p>

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17
Q

<p>Where must the RS seat be to be showed?</p>

A

<p>Full left

1H-65D-1
Page 1-A-8</p>

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18
Q

<p>What is the point of the gunner's belt?</p>

A

<p>It act as an edge limiting device

1H-65D-1
Page 1-A-8</p>

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19
Q

<p>What is the best way to prevent inadvertent release of the latch mechanism on the Gunner's Belt?</p>

A

<p>Wearing it snug

1H-65D-1
Page 1-A-8</p>

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20
Q

<p>How long should the gunners belt be?</p>

A

<p>No longer then the point to prevent the aircrew member from proceeding past the edge of the door frame

1H-65D-1
Page 1-A-8</p>

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21
Q

<p>How is the gunner's belt worn?</p>

A

<p>With the leather flap on the wearer's left to facilitate a right-hand release

1H-65D-1
Page 1-A-8</p>

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22
Q

<p>What is the cabin area designed to accommodate for cargo?</p>

A

<p>Two pallets of 32 by 48 inches

1H-65D-1
Page 1-A-8</p>

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23
Q

<p>How many tie down rings are in the cabin floor?</p>

A

<p>24

1H-65D-1
Page 1-A-9</p>

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24
Q

<p>How any tie down rings are in the baggage compartment?</p>

A

<p>4

1H-65D-1
Page 1-A-9</p>

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25
Q

<p>How are the three hinged doors jettisoned?</p>

A

<p>Raising and pulling aft on the jettison handle and pushing outward on the door

1H-65D-1
Page 1-A-9</p>

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26
Q

<p>What is the minimum door opening for the baggage compartment?</p>

A

<p>19 inches high by 28 inches long

1H-65D-1
Page 1-A-10</p>

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27
Q

<p>What are the emergency flotation filled with?</p>

A

<p>Helium

1H-65D-1
Page 1-A-10</p>

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28
Q

<p>How is the emergency flotation system powered?</p>

A

<p>Directly from the #1 and #2 main DC buses

1H-65D-1
Page 1-A-10</p>

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29
Q

<p>Besides floats where is additional buoyancy provided? </p>

A

<p>Water tight compartments which is the sealed trail boom and sealed fuel tank cavities

1H-65D-1
Page 1-A-10</p>

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30
Q

<p>In light seas how long will the floats keep the MH-65 afloat? </p>

A

<p>4 minutes

1H-65D-1
Page 1-D-10</p>

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31
Q

<p>In light seas how low in the water will the floats keep the MH-65D?</p>

A

<p>Waterline below the cabin floor

1H-65D-1
Page 1-D-10</p>

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32
Q

<p>What does the 1 and 2 light on the float capsule tell the crew?</p>

A

<p>Power is available to that side of the float system

1H-65D-1
Page 1-D-10 </p>

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33
Q

<p>How long does it take for the floats to shape? </p>

A

<p>Less the 2.5 seconds

1H-65D-1
Page 1-D-11</p>

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34
Q

<p>How long does it take for the float cylinders to completely discharge? </p>

A

<p>Less then 4 seconds

1H-65D-1
Page 1-D-11</p>

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35
Q

<p>Where is the portable fire extinguisher located at/</p>

A

<p>Back of the pilots seat

1H-65D-1
Page 1-D-12</p>

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36
Q

<p>How much Halon is in the portable fire extinguisher?</p>

A

<p>2.5 pounds

1H-65D-1
Page 1-D-12</p>

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37
Q

<p>What is the Halon pressured with in the portable fire extinguisher?</p>

A

<p>Nitrogen

1H-65D-1
Page 1-D-12</p>

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38
Q

<p>What is the portable fire extinguisher pressured to? </p>

A

<p>125 PSI

1H-65D-1
Page 1-D-12</p>

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39
Q

<p>What is the duration of the operation of the portable fire extinguisher?</p>

A

<p>10 seconds

1H-65D-1
Page 1-D-12</p>

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40
Q

<p>What is the horizontal range of the portable fire extinguisher? </p>

A

<p>Between 9 and 15 feet

1H-65D-1
Page 1-A-12</p>

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41
Q

<p>Where are the two first aid kits located?</p>

A

<p>Front left side of the 9 degree frame and in the baggage compartment door

1H-65D-1
Page 1-A-12</p>

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42
Q

<p>How many people can the life raft hold?

| </p>

A

<p>6 people

1H-65D-1
Page 1-A-12</p>

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43
Q

<p>Where is the underwater acoustic beacon located?</p>

A

<p>On the Voice and Flight Data Recorder

1H-65D-1
Page 1-A-12</p>

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44
Q

<p>What is used to adjust the reclining back of the RS seat? </p>

A

<p>Left aft handle

1H-65D-1
Page 1-A-8</p>

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45
Q

<p>How do you jettison the baggage compartment door?</p>

A

<p>Can not be

1H-65D-1
Page 1-A-10</p>

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46
Q

<p>What is in the portable fire extinguished that is used to put out the fire?</p>

A

<p>Halon

1H-65D-1
Page 1-A-12</p>

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47
Q

<p>What activates the Underwater acoustic Beacon (UAB)?</p>

A

<p>water activated

1H-65D-1
Page 1-A-12</p>

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48
Q

<p>What frequency does the Underwater Acoustic beacon transmit on? </p>

A

<p>37.5 kHz

1H-65D-1
Page 1-A-12</p>

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49
Q

<p>How long will the Underwater Acoustic Beacon run for? </p>

A

<p>30 days

1H-65D-1
Page 1-A-12</p>

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50
Q

<p>What is the detection range of the Underwater Acoustic Beacon?</p>

A

<p>2,000 to 4,000 yards

1H-65D-1
Page 1-A-12</p>

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51
Q

<p>What is the Underwater Acoustic Beacon powered by?</p>

A

<p>9 volt battery

1H-65D-1
Page 1-A-12</p>

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52
Q

<p>How can the ELT be tracked?</p>

A

<p>Via satellites on the 406 MHz

1H-65D-1
Page 1-A-12</p>

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53
Q

<p>How does the ELT get it position?</p>

A

<p>Off the pilot's EGI

1H-65D-1
Page 1-A-12</p>

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54
Q

<p>What is the shelf life of the ELT battery?</p>

A

<p>5 years

1H-65D-1
Page 1-A-12</p>

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55
Q

<p>How long will the ELT last when active?</p>

A

<p>24 Hours using 406 MHz and 48 hours using 121.5 and 243 MHz

1H-65D-1
Page 1-A-12</p>

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56
Q

<p>What position does the ELT transmit with out a working signal from the pilot's GPS?</p>

A

<p>The last position stored prior to the pilot's GPS becoming inoperative

1H-65D-1
Page 1-A-12</p>

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57
Q

<p>The ELT system remote control switch is located where? </p>

A

IFF/COMM control panel

1H-65D-1
Page 1-A-12

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58
Q

<p>How long must the ELT test switch be held in RESET to rest the ELT?</p>

A

<p>5 second

1H-65D-1
Page 1-A-13</p>

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59
Q

<p>The ELT G-switch activates when how many Gs?</p>

A

<p>2.6 Gs

1H-65D-1
Page 1-A-13</p>

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60
Q

<p>How many ways to active the ELT?</p>

A

<p>3

1H-65D-1
Page 1-A-13</p>

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61
Q

<p>What are the three ways to activate the ELT switch?</p>

A

<p>IFF/COMM panel, ELT, and G-switch

1H-65D-1
Page 1-A-13</p>

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62
Q

<p>What are and how many the engines on the MH-65D?</p>

A

<p>Two Turbomeca Arriel 2C2-CG

1H-65D-1
Page 1-B-2</p>

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63
Q

<p>What is the power the MH-65D engine can make for dual engine operation?</p>

A

<p>712 SHP derated by the DECU from 853 SHP

1H-65D-1
Page 1-B-2</p>

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64
Q

<p>How much power can the MH-65D engine make for single-engine operation?</p>

A

<p>1,005 shaft horsepower (SHP) derated by the DECU from 1,053

1H-65D-1
Page 1-B-2</p>

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65
Q

<p>What is 100% MGB torque?</p>

A

<p>1,294 SHP

1H-65D-1
Page 1-B-2</p>

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66
Q

<p>How many sections are there in the Arriel 2C2 engine?</p>

A

<p>5

1H-65D-1
Page 1-B-2</p>

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67
Q

<p>What is the first section of the Arriel 2C2?</p>

A

<p>Accessory gearbox and transmission shaft

1H-65D-1
Page 1-B-2</p>

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68
Q

<p>What is the second section of the Arriel 2C2 engine?</p>

A

<p>Axial compressor

1H-65D-1
Page 1-B-2</p>

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69
Q

<p>What is the third section of the Arriel 2C2 engine?</p>

A

<p>Gas generator (N1)

1H-65D-1
Page 1-B-2</p>

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70
Q

<p>What is the forth section of the Arriel 2C2 engine?</p>

A

<p>Free power turbine

1H-65D-1
Page 1-B-2</p>

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71
Q

<p>What is the fifth section of the Arriel 2C2 engine ?</p>

A

<p>Reduction gearbox

1H-65D-1
Page 1-B-2</p>

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72
Q

<p>In the Arriel 2C2 when are the ignitors used?</p>

A

<p>Starting only

1H-65D-1
Page 1-B-2</p>

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73
Q

<p>In the Arriel 2C2 when are the fuel nozzles used?</p>

A

<p>Starting

1H-65D-1
Page 1-B-2</p>

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74
Q

<p>How long during starting are the ignitors and fuel nozzles used? </p>

A

<p>Until approximately 45% N1

1H-65D-1
Page 1-B-2</p>

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75
Q

<p>When does the Arriel 2C2 become self-sustaining?</p>

A

<p>Approximately 45% N1

1H-65D-1
Page 1-B-2</p>

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76
Q

<p>Once the Arriel 2C2 is self-sustaining how is fuel delivered to the combustion chamber?</p>

A

<p>Centrifugal fuel wheel rotating inside the combustion chamber

1H-65D-1
Page 1-B-2</p>

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77
Q

<p>What powers the compressor assembly of the Arriel 2C2? </p>

A

<p>A single stage gas turbine

1H-65D-1
Page 1-B-2 </p>

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78
Q

<p>What extracts energy for the power shaft via the reduction gearbox?</p>

A

<p>Single stage free power turbine

1H-65D-1
Page 1-B-2</p>

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79
Q

What makes up the gas generator section (N1) of the Arriel 2C2 engine?

A

Axial compressor, centrifugal compressor, and combustion chamber, and a gas generator

1H-65D-1
Page 1-B-2

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80
Q

<p>How fast does the gas generator turbine shaft turn at when it is running 100%?</p>

A

<p>52,000 RPM

1H-65D-1
Page 1-B-2</p>

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81
Q

<p>Where does N1C signal come from?</p>

A

<p>Electromagnetic sensor mounted on the FADEC alternator drive shaft

1H-65D-1
Page 1-B-2</p>

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82
Q

<p>What is N1A and N1B used for?</p>

A

<p>FADEC for engine control

1H-65D-1
Page 1-B-2</p>

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83
Q

<p>Where does N1A and N1B come from?</p>

A

<p>Derived from the dual-channel engine alternator

1H-65D-1
Page 1-B-2</p>

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84
Q

<p>What does the gas generator drive?</p>

A

<p>Starter generator, oil pump, fuel pump, and FADEC alternator

1H-65D-1
Page 1-B-2</p>

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85
Q

<p>The ELT transmits on what frequencies?</p>

A

<p>121.5 and 406 MHZ (243.0 may be heard as a resonant frequency)

1H-65D-1
Page 1-A-12</p>

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86
Q

<p>What is the max ramp weight for the MH-65D?</p>

A

<p>9,590 lbs

1H-65D-1
Page 1-A-2</p>

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87
Q

<p>What RPM is 100% N2?</p>

A

<p>39,000 RPM

1H-65D-1
Page 1-B-3</p>

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88
Q

<p>Where are N2A, N2B, and N2C signals come from?</p>

A

<p>Reduction gearbox casing and power turbine case

1H-65D-1
Page 1-B-3</p>

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89
Q

<p>Where does the N2A signal go?</p>

A

<p>Pilot NR gauge

1H-65D-1
Page 1-B-3</p>

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90
Q

<p>Where does N2B and N2C signals go?</p>

A

<p>FADEC and VEMD

1H-65D-1
Page 1-B-3</p>

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91
Q

<p>What accessories are driven by the power turbine?</p>

A

<p>Output shaft and engine compartment cooling fan

1H-65D-1
Page 1-B-3</p>

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92
Q

<p>What provides the engine with N2 overspeed protection?</p>

A

<p>Respective DECU in conjuction with the Engine Interface Unit (BIM)

1H-65D-1
Page 1-B-3</p>

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93
Q

<p>Where is the BIM located at?</p>

A

<p>In the baggage compartment

1H-65D-1
Page 1-B-3</p>

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94
Q

<p>At what N2 RPM does the engine get shut down? </p>

A

<p>429 RPM +/- 4RPM

1H-65D-1
Page 1-B-3</p>

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95
Q

<p>How is the engine shut down when there is a N2 overspeed?</p>

A

<p>Stop Electro-valve

1H-65D-1
Page 1-B-3</p>

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96
Q

<p>What gives the order to shuts down the engine in an N2 overspeed?</p>

A

<p>DECU through the BIM

1H-65D-1
Page 1-B-3</p>

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97
Q

<p>Can both engines be shut down for an N2 overspeed at the same time?</p>

A

<p>No

1H-65D-1
Page 1-B-3</p>

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98
Q

<p>How do you take the engine out of an overspeed protection setting?</p>

A

<p>Reset the BIM

1H-65D-1
Page 1-B-3</p>

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99
Q

<p>Besides doing overspeed protection with the DECU what else does the BIM do?</p>

A

<p>Start relay between the DECU and the respective engine

1H-65D-1
Page 1-B-3</p>

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100
Q

<p>What does the fuel-oil heat exchanger do?</p>

A

<p>Heats the engine fuel and aids in cooling the engine oil

1H-65D-1
Page 1-B-3</p>

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101
Q

<p>When does the FUEL FILT 1 or FUEL FILT 2 caution light comes on what PSI?</p>

A

<p>10 PSI difference across the filter

1H-65D-1
Page 1-B-4</p>

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102
Q

<p>When does the "ENG FUEL P" warning light come on?</p>

A

<p>Engine fuel pressure is less than 8.4 PSI

1H-65D-1
Page 1-B-4</p>

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103
Q

<p>The Flow meter and fuel manifold pressure transmitters provides signals for what?</p>

A

<p>The Engine Condition Monitoring System (ECMS) and fuel alert (BINGO) as well as cruise calculations

1H-65D-1
Page 1-B-4</p>

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104
Q

<p>What caution light comes on when there is a dual stepper motor failure?</p>

A

<p>FADEC FAIL light

1H-65D-1
Page 1-B-4</p>

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105
Q

<p>What is the light on the Emergency Fuel Shut-Of Levers (EFSL) used for?</p>

A

<p>Engine fire light

1H-65D-1
Page 1-B-4</p>

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106
Q

<p>What drives the engine oil pump?</p>

A

<p>Engine accessory gearbox

1H-65D-1
Page 1-B-5</p>

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107
Q

<p>At what PSI does the "ENG 1 Oil P" come on?</p>

A

<p>25PSI or below

1H-65D-1
Page 1-B-5</p>

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108
Q

<p>When does the oil pass through the mag plug?</p>

A

<p>After the three scavenge lines merge but before reaching the oil cooler

1H-65D-1
Page 1-B-5</p>

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109
Q

<p>When does the "OIL TEMP" warning light come on? </p>

A

<p>Engine oil exceeds 115 degree C

1H-65D-1
Page 1-B-5</p>

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110
Q

<p>How much can the oil tank hold?</p>

A

<p>2 gal

1H-65D-1
Page 1-B-5</p>

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111
Q

<p>Where does the Oil temp indication on the VEMD get its signal from?</p>

A

<p>Temperature probe located on the outlet side of the tank

1H-65D-1
Page 1-B-5</p>

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112
Q

<p>During a preflight what is the right level for the oil?</p>

A

<p>Bottom of the sight glass and the MIN line (without shaking the aircraft)

1H-65D-1
Page 1-B-5</p>

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113
Q

<p>How many engine oil coolers are on the MH-65D?</p>

A

<p>Two (one for each engine)

1H-65D-1
Page 1-B-6</p>

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114
Q

<p>What must be done before you can change from one oil trade mark or specification to another?</p>

A

<p>Flush the engine oil system

1H-65D-1
Page 1-B-6</p>

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115
Q

<p>What is the graduated scale on the VEMD for the engine oil pressure?</p>

A

<p>0 to 140 PSI

1H-65D-1
Page 1-B-7</p>

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116
Q

<p>What illuminates when the #1 engine drop below 25 PSI?</p>

A

<p>"ENG 1 OIL P" statue light and the red engine status light on the overhead

1H-65D-1
Page 1-B-7</p>

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117
Q

<p>What is the graduated scale on the VEMD for the engine oil temp?</p>

A

<p>-40 to 120 degree C

1H-65D-1
Page 1-B-7</p>

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118
Q

<p>How many thermocouples are used to measure Turbine Outlet Temperature?</p>

A

<p>8

1H-65D-1
Page 1-B-7</p>

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119
Q

<p>What provides an average TOT signal?</p>

A

<p>TOT conformation box

1H-65D-1
Page 1-B-7</p>

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120
Q

<p>Where does the TOT signal go?</p>

A

<p>FADEC and the VEMD

1H-65D-1
Page 1-B-7</p>

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121
Q

<p>What engine parameter does the DECU match on the engines?</p>

A

<p>N1

1H-65D-1
Page 1-B-7</p>

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122
Q

<p>What controls engine operation? </p>

A

<p>DECU

1H-65D-1
Page 1-B-7</p>

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123
Q

<p>How many channels are the DECUs?</p>

A

<p>2

1H-65D-1
Page 1-B-7</p>

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124
Q

<p>What happened during the major FADEC failure?</p>

A

<p>Fuel metering is frozen

1H-65D-1
Page 1-B-7</p>

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125
Q

<p>What will control the engine during a major FADEC failure?</p>

A

<p>EBCAU

1H-65D-1
Page 1-B-7</p>

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126
Q

<p>During normal operations what powers the DECUs?</p>

A

<p>Engine-driven alternators

1H-65D-1
Page 1-B-7</p>

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127
Q

<p>How are the DECUs powered by DC?</p>

A

<p>Internal transformer-rectifier

1H-65D-1
Page 1-B-7</p>

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128
Q

<p>How are the DECUs powered when the Emergency Cutoff switch is in the cutoff position?</p>

A

<p>Emergency Cutoff switch does not affect the engine drive alternators

1H-65D-1
Page 1-B-7</p>

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129
Q

<p>What does the DECU crosstalk function allow the system to do?</p>

A

<p>Allows seamless operation of both engines

1H-65D-1
Page 1-B-7</p>

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130
Q

<p>What do the FCS switches do?</p>

A

<p>Determines the basic operating laws of the FEDAC

1H-65D-1
Page 1-B-8</p>

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131
Q

<p>How do you self test of the FADEC?</p>

A

<p>When batteries are turned on

1H-65D-1
Page 1-B-8</p>

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132
Q

<p>What can you do to a steady GOV that you can not with a flashing GOV or FADEC FAIL light?</p>

A

<p>One-time recycling of the battery relays

1H-65D-1
Page 1-B-8</p>

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133
Q

<p>Can each engine on the aircraft be started by different power source?</p>

A

<p>No

1H-65D-1
Page 1-B-8</p>

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134
Q

<p>When does the start sequence of the engines become self-sustaining?</p>

A

<p>45% N1

1H-65D-1
Page 1-B-8</p>

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135
Q

<p>What is normal engine idle?</p>

A

<p>68% N1

1H-65D-1
Page 1-B-8</p>

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136
Q

<p>When will automatic engine shut down occur during start up?</p>

A

<p>TOT of 840 degrees C
TOT does not exceed 100 degrees C by 27%

1H-65D-1
Page 1-B-8</p>

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137
Q

<p>When will an inflight restart initiate?</p>

A

<p>N1 below 17%

1H-65D-1
Page 1-B-8</p>

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138
Q

<p>When does the DECU change from DC power to engine driven alternator?</p>

A

<p>65% N1

1H-65D-1
Page 1-B-8</p>

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139
Q

<p>What does the engine start-low idle function do?</p>

A

<p>Enables the rotor brake to remain engaged

1H-65D-1
Page 1-B-9</p>

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140
Q

<p>How many engines can be started with the engine start-low idle function?</p>

A

<p>1

1H-65D-1
Page 1-B-9</p>

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141
Q

<p>What does the engine idle at when using the engine start-low idle function?</p>

A

<p>52%

1H-65D-1
Page 1-B-9</p>

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142
Q

<p>How long can the START R.BK be used for?</p>

A

<p>60 Sec with engine oil <=16PSI

1H-65D-1
Page 1-B-9</p>

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143
Q

<p>How long is normal idle speed inhibited when the engine start-low idle function is turned off?</p>

A

<p>Until the rotor brake is released

1H-65D-1
Page 1-B-9</p>

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144
Q

<p>What tells the FADEC to operate in FLIGHT governing laws?</p>

A

<p>FCS advanced to FLIGHT position

1H-65D-1
Page 1-B-9</p>

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145
Q

<p>In the FLIGHT governing laws how long is torque and TOT limited for?</p>

A

<p>Until NR reaches 350 RPM

1H-65D-1
Page 1-B-9</p>

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146
Q

<p>What is adjusted to maintain a constant N2 and NR speed?</p>

A

<p>N1

1H-65D-1
Page 1-B-9</p>

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147
Q

<p>What makes the anticipation signal?</p>

A

<p>Collective lever position

1H-65D-1
Page 1-B-9</p>

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148
Q

<p>What does the anticipation signal do?</p>

A

<p>Reduces the reaction time of the engines

1H-65D-1
Page 1-B-9</p>

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149
Q

<p>In normal torque limitation flight envelope the FADEC will stop torque when?</p>

A

<p>110% (11.0)

1H-65D-1
Page 1-B-9</p>

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150
Q

<p>When will torque increase to 118% (11.8)?</p>

A

<p>NR decreases to <335 RPM

1H-65D-1
Page 1-B-9</p>

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151
Q

<p>When will torque go to 125% (12.5)?</p>

A

<p>NR<317 or drooping faster then 2 RPM/sec and NR<324RPM

1H-65D-1
Page 1-B-9</p>

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152
Q

<p>When will the N1 increase by +0.28% past N1, 2-min OEI rating?</p>

A

<p>NR<317 or NR<324RPM and decaying at 17.5 RPM/sec or greater

1H-65D-1
Page 1-B-9</p>

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153
Q

<p>What causes a Level 1 FADEC failure?</p>

A

<p>Loss of redundancy

1H-65D-1
Page 1-B-10</p>

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154
Q

<p>How do you know if you have a Level 1 FADEC Failure?</p>

A

<p>Flashing GOV

1H-65D-1
Page 1-B-10</p>

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155
Q

<p>When can you have a Level 1 FADEC failure?</p>

A

<p>When the FCS is in the IDLE or OFF position

1H-65D-1
Page 1-B-10</p>

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156
Q

<p>What is a Level 2 FADEC failure?</p>

A

<p>Loss of non redundant resource

1H-65D-1
Page 1-B-10</p>

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157
Q

<p>What is a Level 3 FADEC Failure?</p>

A

<p>Represent a total failure of the respective FADEC

1H-65D-1
Page 1-B-10</p>

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158
Q

<p>How do you know that you have a Level 3 FADEC failure?</p>

A

<p>FADEC FAIL light and a red engine status light

1H-65D-1
Page 1-B-10</p>

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159
Q

<p>What happens during a Level 3 FADEC failure?</p>

A

<p>Affected engine fuel flow will freeze at its present value

1H-65D-1
Page 1-B-10</p>

160
Q

<p>What is HIPSARM?</p>

A

<p>Hover increased Power Search and Rescue Mission

1H-65D-1
Page 1-B-11</p>

161
Q

<p>What is the HISPARM power setting?</p>

A

<p>In dual engine when above max continuous (8.8) and below maximum takeoff power (10.0)

1H-65D-1
Page 1-B-11</p>

162
Q

<p>What are the limiting factors of HIPSARM?</p>

A

<p>N1 or TOT

1H-65D-1
Page 1-B-11</p>

163
Q

<p>HIPSARM power may be accessed for up to how long?</p>

A

<p>30 Minutes

1H-65D-1
Page 1-B-11</p>

164
Q

<p>What is the symbol for HIPSARM?</p>

A

<p>White pie

1H-65D-1
Page 1-B-11</p>

165
Q

<p>When will the HIPSARM symbol begin to flash?</p>

A

<p>27 minutes and 30 sec

1H-65D-1
Page 1-B-11</p>

166
Q

<p>How long will the HIPSARM symbol flash for?</p>

A

<p>2 minutes and 30 seconds

1H-65D-1
Page 1-B-11</p>

167
Q

<p>When will the HIPSARM symbol turn solid white?</p>

A

<p>30 minutes

1H-65D-1
Page 1-B-11</p>

168
Q

<p>What is OEI?</p>

A

<p>One engine inoperative

1H-65D-1
Page 1-B-11</p>

169
Q

<p>When are you in OEI mode?</p>

A

<p>When an engine is being operated at less than 40% N1

1H-65D-1
Page 1-B-11</p>

170
Q

<p>When can OEI mode get activated when both engines are over 40% N1?</p>

A

<p>FADEC detects a 6% N1 split or frozen fuel meter

1H-65D-1
Page 1-B-11</p>

171
Q

<p>In training mode OEI what limit is automatically set?</p>

A

<p>OEI LO

1H-65D-1
Page 1-B-11</p>

172
Q

<p>In a real OEI mode what limit is automatically set?</p>

A

<p>OEI HI

1H-65D-1
Page 1-B-11</p>

173
Q

<p>How long can an engine operate in OEI HI?</p>

A

<p>3 periods no longer than 30 second durations

1H-65D-1
Page 1-B-11</p>

174
Q

<p>What is the total time an engine can accumulate in OEI HI?</p>

A

<p>90 seconds

1H-65D-1
Page 1-B-11</p>

175
Q

<p>What is the operating limit for OEI LO?</p>

A

<p>5 periods of use no longer then 2 minutes

1H-65D-1
Page 1-B-11</p>

176
Q

<p>What is operating limit for OEI CT?</p>

A

<p>No limit

1H-65D-1
Page 1-B-11</p>

177
Q

<p>Where is OEI rating logged?</p>

A

<p>VEMD

1H-65D-1
Page 1-B-11</p>

178
Q

<p>What is the symbol for OEI LO?</p>

A

<p>Yellow clock symbol

1H-65D-1
Page 1-B-11</p>

179
Q

<p>What is the symbol for OEI HI?</p>

A

<p>Red clock symbol

1H-65D-1
Page 1-B-11</p>

180
Q

<p>Where is the OEI usage found?</p>

A

<p>VEMD status page

1H-65D-1
Page 1-B-11</p>

181
Q

<p>What is the EBCAU short for?</p>

A

<p>Emergency Backup Control Auxiliary Unit

1H-65D-1
Page 1-B-11</p>

182
Q

<p>What does the EBCAU do?</p>

A

<p>Emergency control of the engine during a dual-channel FADEC failure

1H-65D-1
Page 1-B-11</p>

183
Q

<p>How does the EBCAU control the engine?</p>

A

<p>With 28VDC through the backup fuel actuator

1H-65D-1
Page 1-B-11</p>

184
Q

<p>How is the EBCAU energized?</p>

A

<p>FADEC backup switches

1H-65D-1
Page 1-B-11</p>

185
Q

<p>When is the engine status light illuminated?</p>

A

<p>During a dual-channel FADEC failure or loss of oil pressure

1H-65D-1
Page 1-B-11</p>

186
Q

<p>The EBCAU uses what parameter to control the engine?</p>

A

<p>Matches N1 of the good engine to the bad one

1H-65D-1
Page 1-B-11</p>

187
Q

<p>What should not be used for training?</p>

A

<p>EBCAU

1H-65D-1
Page 1-B-12</p>

188
Q

<p>What does the training switch do?</p>

A

<p>Simulates engine failure and allow training of single-engine flight profiles

1H-65D-1
Page 1-B-12</p>

189
Q

<p>What RPM does the failed engine go to when using the training switch?</p>

A

<p>N2=320RPM

1H-65D-1
Page 1-B-12</p>

190
Q

<p>What values are right and what values are wrong on the FLI page of the VEMD during training mode?</p>

A

<p>N1, TOT, TRQ numerical values are right but the FLI needle position is simulated at a reduced value to prevent engine damage

1H-65D-1
Page 1-B-12</p>

191
Q

<p>In training mode when numerical values are underscored in yellow or red are they at a real or simulated limit?</p>

A

<p>Real

1H-65D-1
Page 1-B-12</p>

192
Q

<p>In training mode what is OEI HI setting at compared to real OEI HI?</p>

A

<p>80%

1H-65D-1
Page 1-B-13</p>

193
Q

<p>What % of torque is available when in training mode OEI HI?</p>

A

<p>62%

1H-65D-1
Page 1-B-13</p>

194
Q

<p>When in training mode when will the idle engine back power up?</p>

A

<p>When NR droops to 320 RPM

1H-65D-1
Page 1-B-13</p>

195
Q

<p>If you are above 355 RPM what power setting will the FADEC go to if it goes from training mode to normal mode?</p>

A

<p>125%

1H-65D-1
Page 1-B-13</p>

196
Q

<p>What RPM does the NR HI give you?</p>

A

<p>365 RPM

1H-65D-1
Page 1-B-13</p>

197
Q

<p>What are the limits in NR HI?</p>

A

<p>135 KIAS and 40-degree angle of bank

1H-65D-1
Page 1-B-13</p>

198
Q

<p>At what altitude does NR speed up?</p>

A

<p>1650ft

1H-65D-1
Page 1-B-13</p>

199
Q

<p>Above 1650ft when does NR increase by 1 RPM?</p>

A

<p>820ft

1H-65D-1
Page 1-B-13</p>

200
Q

<p>What is the max NR speed when in NR Normal?</p>

A

<p>360 RPM

1H-65D-1
Page 1-B-13</p>

201
Q

<p>At what altitude does the NR speed max out?</p>

A

<p>5,740 ft

1H-65D-1
Page 1-B-13</p>

202
Q

<p>When the NR system fails what is the NR speed?</p>

A

<p>360 RPM

1H-65D-1
Page 1-B-13</p>

203
Q

<p>What pages do you have on the VEMD during normal operation?</p>

A

<p>Top= FLI
Bottom=Vehicle, Fuel, Engine Power Check (EPC), and System status page

1H-65D-1
Page 1-B-13</p>

204
Q

<p>What VEMD pages do you have if one screen fails? </p>

A

<p>FLI, Vehicle, and Fuel page

1H-65D-1
Page 1-B-14</p>

205
Q

<p>What info is found on the VEMD vehicle page?</p>

A

<p>Engine oil temp, engine oil pressure, MGB oil temp, MGB oil pressure and primary and secondary hydraulic pressure

1H-65D-1
Page 1-B-16</p>

206
Q

<p>How do you get numerical values to display on the vehicle page?</p>

A

<p>Pressing select, +, and Enter

1H-65D-1
Page 1-B-16</p>

207
Q

On the VEMD vehicle page what tells you that you are in the caution range?

A

Vertical yellow bar along the side of the scale, the numerical value will be displayed and underlined in yellow

1H-65D-1
Page 1-B-16

208
Q

What happens on the VEMD vehicle page if the value enters the warning range?

A

The vertical are turns red, Numerical value will be underlined in red and the vertical scale will increase in size

1H-65D-1
Page 1-B-16

209
Q

<p>What happens if the VEMD vehicle page is not selected but you enter the warning level of the value?</p>

A

<p>"VEH PARAM OVER LIMIT" annunciation will appear in the message zone

1H-65D-1
Page 1-B-16</p>

210
Q

<p>What happens on the vehicle page if the parameter fails?</p>

A

<p>Scale and label will both turn amber and the range markings and pointer will disappear

1H-65D-1
Page 1-B-16</p>

211
Q

<p>What is displayed on the VEMD Caution and Fuel Page?</p>

A

<p>Boost pump fuel pressure, fuel flow, quantity, endurance, and annunciations

1H-65D-1
Page 1-B-16</p>

212
Q

<p>What happens on the VEMD Caution and Fuel Page if the fuel drops below 3%</p>

A

<p>Bar and quantity will change to amber and a LOW alert will appear

1H-65D-1
Page 1-B-16</p>

213
Q

<p>What annunciations can be displayed on the VEMD Caution and Fuel page?</p>

A

<p>Eng 1 and 2 Chip, MGB and Tail Chip, Servo Limit, Pedal Limit, and LDG LOCK

1H-65D-1
Page 1-B-16</p>

214
Q

<p>When is the EPC initiated?</p>

A

<p>By selecting the EPC page on the VEMD

1H-65D-1
Page 1-B-17</p>

215
Q

<p>What does the VEMD system status page display? </p>

A

<p>FADEC system data

1H-65D-1
Page 1-B-17</p>

216
Q

<p>How do you tell on the FLI which parameter is over limit? </p>

A

<p>It will be underlined in red or yellow

1H-65D-1
Page 1-B-19</p>

217
Q

<p>What parameters are displayed on the FLI?</p>

A

<p>Torque, N1, and TOT

1H-65D-1
Page 1-B-19</p>

218
Q

<p>What parameter is displayed on the FLI needle?</p>

A

<p>The highest single parameter drives the FLI single needle

1H-65D-1
Page 1-B-19</p>

219
Q

<p>What is displayed on the Upper information zone of the FLI page?</p>

A

<p>Bleed valve symbols, OEI mode display, and Eng Idle annuncation

1H-65D-1
Page 1-B-19</p>

220
Q

<p>When does the bleed value symbol appear?</p>

A

<p>When that side bleed value is open

1H-65D-1
Page 1-B-19</p>

221
Q

<p>When will the Yellow ENG IDLE annunciation be displayed on the FLI page?</p>

A

<p>When the FADEC switch is placed in the IDLE position

1H-65D-1
Page 1-B-19</p>

222
Q

<p>What does Check Trq annunciation on the FLI message Zone mean?</p>

A

<p>Discrepancy between engine torques

1H-65D-1
Page 1-B-20</p>

223
Q

<p>Normally how is total torque calculated on the FLI?</p>

A

<p>TRQ1+TRQ2=Total Torque

1H-65D-1
Page 1-B-20</p>

224
Q

<p>What must the torque split on the engines be for a CHECK TRQ annunciation?</p>

A

<p>>7.5%

1H-65D-1
Page 1-B-20</p>

225
Q

<p>What can cause engine torque splits?</p>

A

<p>Disparity between engine strengths, out-of-wing line hovers, or sideward flight

1H-65D-1
Page 1-B-20</p>

226
Q

<p>With an engine torque split what is the new torque calculation?</p>

A

<p>Higher Engine Trq x 2 = total torque

1H-65D-1
Page 1-B-20</p>

227
Q

<p>How does the CDU calculate total engine torque?</p>

A

<p>TRQ1+TRQ2 no matter what the split is

1H-65D-1
Page 1-B-20</p>

228
Q

<p>What does a yellow triangle with a letter T inside it on the FLI mean?</p>

A

<p>Training Mode

1H-65D-1
Page 1-B-21</p>

229
Q

<p>What does the white circle inside a white square with a diagonal bar through it on the FLI mean?</p>

A

<p>P3 bleed air is open to heat the cabin

1H-65D-1
Page 1-B-21</p>

230
Q

<p>The lower Information zones on the FLI is for what kind of message? </p>

A

<p>Engine start annunciation and degradation of failure of the FLI

1H-65D-1
Page 1-B-21</p>

231
Q

<p>When does the FLI DEGR annunciation display on the FLI Lower Information Zones?</p>

A

<p>Anytime a N1, TOT, or TRQ parameter is not valid

1H-65D-1
Page 1-B-21</p>

232
Q

<p>When will FLI FAIL display on the FLI Lower Information Zone appear?</p>

A

<p>Anytime N1, TOT, and TRQ parameters are not valid on the same engine

1H-65D-1
Page 1-B-21</p>

233
Q

How do you tell which parameter is not valued on the FLI?

A

It loses its numerical value and will change to amber

1H-65D-1
Page 1-B-21

234
Q

<p>When will the start mode display on the FLI?</p>

A

<p>When the N1 of one engine is increasing and lowering then 60% or decreasing and lower than 40%

1H-65D-1
Page 1-B-22</p>

235
Q

<p>When will the flashing START annunciation appear on the FLI?</p>

A

<p>When ever the FADEC senses the starter is engaged

1H-65D-1
Page 1-B-22</p>

236
Q

When is it normal to see the FUEL PARAM OVERLIMIT?

A

During start until second engine boost pumps are on

1H-65D-1
Page 1-B-22

237
Q

<p>During start when will the TOT be underlined with a flashing red line?</p>

A

<p>TOT>750 degree C

1H-65D-1
Page 1-B-22</p>

238
Q

<p>During start when will the TOT be underline in a solid red line?</p>

A

<p>TOT=840 degree C

1H-65D-1
Page 1-B-22</p>

239
Q

<p>When will the FLI appear in AEO Mode?</p>

A

<p>Anytime both engines N1s are above 40% and neither FADEC is in an OEI, Training, or idle state

1H-65D-1
Page 1-B-23</p>

240
Q

<p>What is 10.7 on the FLI in AEO mode?</p>

A

<p>Maximum transient power

1H-65D-1
Page 1-B-23</p>

241
Q

<p>What is 10.0 on the FLI in AEO mode?</p>

A

<p>Maximum takeoff power

1H-65D-1
Page 1-B-23</p>

242
Q

<p>What is 8.8 on the FLI in AEO mode?</p>

A

<p>Maximum continuous power

1H-65D-1
Page 1-B-23</p>

243
Q

<p>What is the range of the yellow arc on the FLI in AEO mode?</p>

A

<p>8.8 to 10.0

1H-65D-1
Page 1-B-23</p>

244
Q

<p>At what setting is the red bar on the FLI in AEO mode at?</p>

A

<p>10.0

1H-65D-1
Page 1-B-23</p>

245
Q

<p>At what setting is the red diode on the FLI in AEO mode at?</p>

A

<p>10.7

1H-65D-1
Page 1-B-23</p>

246
Q

<p>In AEO mode when will the limiting parameter be underline in yellow?</p>

A

<p>When the needle enters the Yellow arc

1H-65D-1
Page 1-B-23</p>

247
Q

<p>In AEO mode when will the limiting parameter be underlined in red?</p>

A

<p>When the FLI exceeds the red bar

1H-65D-1
Page 1-B-23</p>

248
Q

<p>When will the FLI be in OEI Mode?</p>

A

<p>When ever N1 of either engine is lower than 40% or either engine is in idle

1H-65D-1
Page 1-B-23</p>

249
Q

<p>In FLI OEI mode what does the dashed yellow bar mean?</p>

A

<p>Continuous OEI power

1H-65D-1
Page 1-B-23</p>

250
Q

<p>In FLI OEI mode what the Dashed red bar mean?</p>

A

<p>2 min OEI power

1H-65D-1
Page 1-B-23</p>

251
Q

<p>In FLI OEI mode what does the Solid red bar mean?</p>

A

<p>30 sec OEI power

1H-65D-1
Page 1-B-23</p>

252
Q

<p>In FLI OEI mode when will the yellow pie symbol appear?</p>

A

<p>When the FLI needle enters the 2-min OEI range

1H-65D-1
Page 1-B-23</p>

253
Q

<p>In FLI OEI mode in the 2-min OEI range how long will the yellow pie symbol remain steady for? </p>

A

<p>1 min and 55 sec

1H-65D-1
Page 1-B-23</p>

254
Q

<p>How long will the yellow pie flash for in the FLI OEI mode in the 2-min OEI range?</p>

A

<p>5 sec

1H-65D-1
Page 1-B-23</p>

255
Q

<p>When will the yellow pie become a solid yellow circle when in FLI OEI mode and in the 2 min range?</p>

A

<p>2 minutes

1H-65D-1
Page 1-B-23</p>

256
Q

<p>What does the red pie symbol in the FLI in OEI mode mean?</p>

A

<p>30 sec OEI power range

1H-65D-1
Page 1-B-23</p>

257
Q

<p>How long will the red pie symbol be a steady red pie for on the FLI in OEI mode?</p>

A

<p>25 secs

1H-65D-1
Page 1-B-23</p>

258
Q

<p>How long will the red pie symbol flash for on the FLI in OEI mode?</p>

A

<p>5 sec

1H-65D-1
Page 1-B-23</p>

259
Q

<p>When will the red pie symbol turn solid on the FLI in OEI mode?</p>

A

<p>30 sec

1H-65D-1
Page 1-B-23</p>

260
Q

<p>On the onset of a single-engine condition what power setting is automatically set?</p>

A

<p>OEI-HI

1H-65D-1
Page 1-B-23</p>

261
Q

<p>When will the FLI enter into OEI training mode?</p>

A

<p>Anytime both engine's N1's are above 40% and FADEC is in training mode

1H-65D-1
Page 1-B-24</p>

262
Q

<p>When will the FLI enter into OEI GOV mode?</p>

A

<p>Whenever N1 on both engines is higher than 40% and there is a difference of at least 6% N1 between the two engines

1H-65D-1
Page 1-B-25</p>

263
Q

<p>How many reports are stored in the VEMD?</p>

A

<p>Last 7

1H-65D-1
Page 1-B-26</p>

264
Q

<p>How many over limit records are saved in the VEMD?</p>

A

<p>2

1H-65D-1
Page 1-B-26</p>

265
Q

<p>How many EPC are saved in the VEMD?</p>

A

<p>Last 8

1H-65D-1
Page 1-B-26</p>

266
Q

<p>How do you enter into the VEMD maintenance menu?</p>

A

<p>Turn on VEMD while holding "SCROLL" and "RESET"

1H-65D-1
Page 1-B-26</p>

267
Q

<p>What type of fire detectors are there in the engine compartment?</p>

A

<p>Bimetallic

1H-65D-1
Page 1-B-27</p>

268
Q

<p>How many fire detectors are there in each engine compartment?</p>

A

<p>3

1H-65D-1
Page 1-B-27</p>

269
Q

<p>Where are the three fire detectors located in the engine compartment and what temp do they go off?</p>

A

<p>2=accessory/reduction gearbox 200 degrees C
1=Gas generator 400 degree C

1H-65D-1
Page 1-B-27</p>

270
Q

<p>What indentations do you get for a fire in the engine compartment?</p>

A

<p>FIRE light on the instrument panel and fire light on the EFSL

1H-65D-1
Page 1-B-27</p>

271
Q

<p>What will cause a FAIL light to illuminate in the engine fire system?</p>

A

<p>Open circuit in the detector wiring harness or if power is lost to the fire detection circuit

1H-65D-1
Page 1-B-27</p>

272
Q

<p>What is in the engine fire extinguishing bottles?</p>

A

<p>HALON

1H-65D-1
Page 1-B-27</p>

273
Q

<p>Below what PSI does the L EXT and R EXT come on?</p>

A

<p><230 PSI

1H-65D-1
Page 1-B-27</p>

274
Q

<p>Pressing PRI Engine 1 fire extinguishing button will fire off which bottle?</p>

A

<p>Left

1H-65D-1
Page 1-B-27</p>

275
Q

<p>Pressing SEC Engine 2 fire extinguishing button will fire off which bottle? </p>

A

<p>Left

1H-65D-1
Page 1-B-27</p>

276
Q

<p>What do the ant-cone stops do?</p>

A

<p>Facilitates starting in high winds

1H-65D-1
Page 1-B-28</p>

277
Q

<p>What will cause uneven and excessive wear on the rotor brake?</p>

A

<p>The head turning with the rotor brake handle in any position other than fully on or fully off

1H-65D-1
Page 1-B-28</p>

278
Q

<p>Where is the rotor brake mounted?</p>

A

<p>On the MGB oil cooler fan shaft

1H-65D-1
Page 1-B-28</p>

279
Q

<p>What is the reduction ratio of the engine rotation to the Man Rotor head?</p>

A

<p>17 to 1

1H-65D-1
Page 1-B-33</p>

280
Q

<p>What is the ratio for the reduction between the engine input and the tail rotor speed?</p>

A

<p>1.5:1

1H-65D-1
Page 1-B-33</p>

281
Q

<p>What does the main MGB oil supply system oil go that the auxiliary system does not?</p>

A

<p>Oil cooler

1H-65D-1
Page 1-B-33</p>

282
Q

<p>What blocks the MGB oil supply auxiliary system from working when the main system is working?</p>

A

<p>Shuttle valve

1H-65D-1
Page 1-B-33</p>

283
Q

<p>What keeps the shuttle valve closed while the MGB Main oil supply system is working?</p>

A

<p>Higher pressure of the primary system over the auxiliary system

1H-65D-1
Page 1-B-33</p>

284
Q

<p>The inlet for which MGB oil supply system inlet is lower?</p>

A

<p>Auxiliary system

1H-65D-1
Page 1-B-33</p>

285
Q

When is NR HI used?

A

Hover flight, single-engine operations, and other demanding low speed maneuvers

1H-65D-1
Page 1-B-13

286
Q

What is the minimum crew for the MH-65D?

A

one pilot in the right seat and one aircrew member in the cabin

1H-65D-1
Page 5-2

287
Q

What is the operational envelope for the temperature range of the MH-65D?

A

-25 degree C (-13 degree F) and 55 degree C (131 degree F)

1H-65D-1
Page 5-2

288
Q

Who can grant a waver for the temperature operational envelope for the MH-65D?

A

CG-711

1H-65D-1
Page 5-2

289
Q

What is the total number of starter engagements for the MH-65D?

A

5

1H-65D-1
Page 5-2

290
Q

What is the cooling cycle for the starter engagements on the MH-65D?

A

minimum of 60 seconds between starting attempts and then 30 minutes after the fifth attempt

1H-65D-1
Page 5-2

291
Q

What is the time limit for cranking the starter in the MH-65D?

A

20 seconds

1H-65D-1
Page 5-2

292
Q

What is the cooling cycle for cranking the starters on the MH-65D?

A

minimum of 5-minutes cooling cycle between cranks and 30 minutes after the third crank

1H-65D-1
Page 5-2

293
Q

What is the rotor engagement/disengagments wind limits in the MH-65D?

A

55 knots within 20 degrees of the aircraft heading or 35 knots from all other directions

1H-65D-1
Page 5-3

294
Q

What should the oil temperature before advancing FADEC Control Switch post the IDLE position in the MH-65D?

A

0 degrees C

1H-65D-1
Page 5-7

295
Q

What is the maximum pressure the oil can reach before it should be recorded in maintenance records in the MH-65D?

A

128 psi

1H-65D-1
Page 5-7

296
Q

What is the maximum PSI for operating the flight control servo in the MH-65D?

A

1,060 psi

1H-65D-1
Page 5-8

297
Q

What is the minimum fuel PSI required for engine start in the MH-65D?

A

5.8 psi

1H-65D-1
Page 5-8

298
Q

What is the minimum fuel PSI for the starting phase in the MH-65D?

A

3.6 psi

1H-65D-1
Page 5-8

299
Q

What is the minimum fuel PSI for the operating phase in the MH-65D?

A

3.6 psi

1H-65D-1
Page 5-8

300
Q

What is the minimum battery volts required for starting the engines in the MH-65D?

A

17 VDC

1H-65D-1
Page 5-9

301
Q

Can the engines be started from different power sources?

A

No

1H-65D-1
Page 5-9

302
Q

What is the maximum voltage allowed in the DC electrical system for the MH-65D?

A

30 volts indicated on the voltmeter

1H-65D-1
Page 5-9

303
Q

What is 100% on the MH-65D loadmeter?

A

160 amps

1H-65D-1
Page 5-9

304
Q

What is the maximum continuous current the generators can produce on the MH-65D?

A

160 amps

1H-65D-1
Page 5-9

305
Q

When can the loadmeter be over 100% on the MH-65D?

A

during engine start or as the battery charges after an engine start

1H-65D-1
Page 5-9

306
Q

How long can the loadmeter be over 100% after an engine start in the MH-65D?

A

first minute

1H-65D-1
Page 5-9

307
Q

What should the load share be between generators on the MH-65D?

A

10%

1H-65D-1
Page 5-9

308
Q

What is the maximum voltage that a MH-65D AC electrical system can make?

A

120 volts

1H-65D-1
Page 5-9

309
Q

What is the 100% on the loadmeter amps per alternator phase equal to?

A

29 amps

1H-65D-1
Page 5-9

310
Q

What is the maximum ramp weight for the MH-65D?

A

9,590 lbs

1H-65D-1
Page 5-9

311
Q

What can you do to the MH-65D when it is at its maximum ramp weight?

A

Helicopter can be static, towed, or being ground taxied under its own power.

1H-65D-1
Page 5-9

312
Q

What is the cabin usable volume on an MH-65D?

A

176 cubic ft

1H-65D-1
Page 5-9

313
Q

How many pounds per square foot can the deck of the MH-65D be loaded?

A

125 pounds per square foot

1H-65D-1
Page 5-9

314
Q

What are the tiedown rings rated for on the MH-65D?

A

1,800 pounds acting upward or through a 30-degree arc from vertical

1H-65D-1
Page 5-9

315
Q

What is the usable baggage compartment volume on the MH-65D?

A

88 cubic ft

1H-65D-1
Page 5-9

316
Q

What is the maximum allowable loading in on the center composite panel in the baggage compartment on the MH-65D?

A

125 pound per square foot

1H-65D-1
Page 5-9

317
Q

What is the maximum allowable loading in the baggage compartment on the MH-65D?

A

440 pounds

1H-65D-1
Page 5-9

318
Q

What is the maximum allowable loading on the outboard metal panels in the baggage compartment on the MH-65D?

A

61.5 pounds

1H-65D-1
Page 5-9

319
Q

What determents the maximum acceleration under various flight conditions for the MH-65D?

A

The illumination of the LIMIT light

1H-65D-1
Page 5-9

320
Q

What is the maximum operating Density Altitude for takeoffs and landings for the MH-65D?

A

10,000

1H-65D-1
Page 5-9

321
Q

What is the maximum operating DA for forward flight for the MH-65D?

A

18,000

1H-65D-1
Page 5-9

322
Q

When shall the NR switch be placed in the HI position on the MH-65D?

A

During flight greater than or equal to 10 ft Above Ground Level/Above Water Level and all lateral flight

1H-65D-1
Page 5-11

323
Q

When should the NR switch be placed in the HI position on the MH-65D?

A

If a flight profile requires maximum performance

1H-65D-1
Page 5-11

324
Q

In the MH-65D what is considered hover flight?

A

Any zero or near zero ground speed operation in winds of 35 knots and below

1H-65D-1
Page 5-16

325
Q

In the MH-65D what is considered transition flight?

A

Flight from zero to 80 KIAS

1H-65D-1
Page 5-16

326
Q

In the MH-65D what is considered cruise flight?

A

Flight above 80 KIAS

1H-65D-1
Page 5-16

327
Q

What is the maximum permissible forward airspeed in the MH-65D?

A

175 KIAS at sea level

1H-65D-1
Page 5-17

328
Q

What is the maximum gross weight allowed when going 175 KIAS on the MH-65D?

A

6,614 LBS

1H-65D-1
Page 5-17

329
Q

What is the maximum G loading for VNE on the MH-65D?

A

1G (straight and level flight)

1H-65D-1
Page 5-17

330
Q

When hovering above 4,000 PA or at temperatures colder than -25 degrees C or warmer then 40 degrees C what is required on the MH-65D?

A

Increased monitoring of the MGB temperature

1H-65D-1
Page 5-18

331
Q

What is the maximum touchdown sink rate when the MH-65D is at a maximum gross weight of 8,900 lbs?

A

600 fpm

1H-65D-1
Page 5-19

332
Q

What will tell you in the MH-65D that the landing has exceeded 600 fpm rate of descent?

A

Activation of the ELT and/or aircraft emergency light system

1H-65D-1
Page 5-19

333
Q

What is the slope limitation for landing and stopping the rotor for the MH-65D?

A

10 degrees

1H-65D-1
Page 5-19

334
Q

What is the maximum rotor speed for using the rotor brake on the MH-65D?

A

170 RPM

1H-65D-1
Page 5-19

335
Q

How long do you need to let the rotor brake cool between applications on the MH-65D?

A

5 minutes

1H-65D-1
Page 5-19

336
Q

After three consecutive applications of the rotor brake on the MH-65D how long should you wait?

A

10 minutes

1H-65D-1
Page 5-19

337
Q

What operation is prohibited on the MH-65D when the rotor brake is on?

A

Operating both engines

1H-65D-1
Page 5-19

338
Q

What is the maximum duration that the rotor brake maybe on with one engine operating and with the START R.BK switch activated on the MH-65D?

A

15 minutes

1H-65D-1
Page 5-19

339
Q

What is the N1 of the operating engine with the START R.BK switch activated?

A

52%

1H-65D-1
Page 5-19

340
Q

What is the maximum braking time for a good rotor brake on the MH-65D?

A

13 seconds

1H-65D-1
Page 5-19

341
Q

What is the limiting altitude for inflation of the floats on the MH-65D?

A

9,800 ft PA

1H-65D-1
Page 5-19

342
Q

What is the limiting altitude for landing in the water with the floats in the MH-65D?

A

4,900 ft PA

1H-65D-1
Page 5-19

343
Q

When it is recommended to have the flotation system armed in the MH-65D?

A

200ft radar altitude

1H-65D-1
Page 5-19

344
Q

What is the maximum permissible load for the hoist on the MH-65D?

A

600 lbs

1H-65D-1
Page 5-19

345
Q

What is the rest period for 300 to 600 lbs for the hoist on the MH-65D?

A

30 sec

1H-65D-1
Page 5-19

346
Q

What is the rest period for the hoist when no load on the hoist on the MH-65D?

A

no rest required

1H-65D-1
Page 5-19

347
Q

What is the rest period for 300 lbs or less for the hoist on the MH-65D?

A

10 sec

1H-65D-1
Page 5-19

348
Q

What is the maximum permissible cargo hook load for the MH-65D?

A

2,000 lbs

1H-65D-1
Page 5-19

349
Q

What is the minimum crew required for external loads?

A

One pilot in the right seat
one aircrew member qualified for external cargo operations

1H-65D-1
Page 5-19

350
Q

What is prohibited when using the cargo hook?

A

Use of the hoist

1H-65D-1
Page 5-19

351
Q

What is the airspeed requirement for fuel jettison in the MH-65D?

A

40-120 kias

1H-65D-1
Page 5-19

352
Q

What must be done when jettisoning fuel below 60 Kias on the MH-65D??

A

Landing gear extended

1H-65D-1
Page 5-19

353
Q

Why do you extend the landing gear when fuel jettisoning below 60KIAS?

A

help keeps fuel clear of the fuselage

1H-65D-1
Page 5-19

354
Q

What should not be operated when jettisoning fuel on the MH-65D?

A

fuel transfer pump

1H-65D-1
Page 5-19

355
Q

At what weight can you land on a ship with the MH-65D?

A

8,900 lbs or less

1H-65D-1
Page 5-20

356
Q

What is the max speed for sliding door movement on the MH-65D?

A

80 KIAS

1H-65D-1
Page 5-20

357
Q

What is the max speed for the sliding door removed on the MH-65D?

A

120 KIAS

1H-65D-1
Page 5-20

358
Q

What is the max speed for the door locked opened on the MH-65D?

A

100 KIAS

1H-65D-1
Page 5-20

359
Q

What is the max speed for the hoist hatched locked open on the MH-65D?

A

80 KIAS forward
35 KT sideward

1H-65D-1
Page 5-20

360
Q

What is the max speed for movement of the hoist hatch on the MH-65D?

A

60 KIAS forward
30 KT sideward

1H-65D-1
Page 5-20

361
Q

What is the max speed with skis installed on the MH-66D?

A

120 KIAS

1H-65D-1
Page 5-20

362
Q

What is the max speed for landing on the snow with skis installed on the MH-65D?

A

35 KGS

1H-65D-1
Page 5-20

363
Q

What is the max sideward flight speed on the MH-65D?

A

35 kt

1H-65D-1
Page 5-20

364
Q

What is the max speed for landing the MH-65D?

A

60 KGS

1H-65D-1
Page 5-20

365
Q

What is the braking speed for the MH-65D below 8,900 lbs

A

35KGS

1H-65D-1
Page 5-20

366
Q

What is the max braking speed for the MH-65D above 8,900lbs?

A

30 KGS

1H-65D-1
Page 5-20

367
Q

What is the max speed for landing light extension on the MH-65D?

A

135 KIAS

1H-65D-1
Page 5-20

368
Q

What is the max speed with the cargo hook loaded on the MH-65D?

A

90 KIAS

1H-65D-1
Page 5-21

369
Q

What is the max speed for arming floats on the MH-65D?

A

90 KIAS

1H-65D-1
Page 5-21

370
Q

What is the max speed for inflated floats on the MH-65D?

A

90 KIAS

1H-65D-1
Page 5-21

371
Q

What is the max speed with NR in HI on the MH-65D?

A

135 KIAS

1H-65D-1
Page 5-21

372
Q

What is the max angle of bank for takeoff and landings on the MH-65D?

A

10 degrees

1H-65D-1
Page 5-21

373
Q

What is the max angle of bank with an external load on the MH-65D?

A

30 degrees

1H-65D-1
Page 5-21

374
Q

What is the max angle of bank with the NR switch in HI on the MH-65D?

A

40 degrees

1H-65D-1
Page 5-21

375
Q

What is the max angle of bank when at or above 110 KIAS?

A

45 degree

1H-65D-1
Page 5-21

376
Q

What is the max angle of bank when below 110 KIAS?

A

60 degrees

1H-65D-1
Page 5-21

377
Q

When will the ALT flag appear on the on the MH-65D?

A

When there is a loss of a valid radar altitude signal.

1H-65D-1
Page 1-D-12

378
Q

When it is normal to see the ALT flag appear on the MH-65D?

A

Climbing through 8000

1H-65D-1
Page 1-D-12

379
Q

What are the two times that you will get a compass warning flag on the BDI in the MH-65D?

A

Power lost to BDI or copilot compass signal becomes invalid

1H-65D-1
Page 1-D-12

380
Q

What direction can the double bar pointer display on the MH-65D’s BDI?

A
  • VOR
  • ADF

1H-65D-1
Page 1-D-14

381
Q

What can the single bar pointer point at on the MH-65D’s BDI?

A

VOR or TACAN

1H-65D-1
Page 1-D-14

382
Q

When will MAN be illumninated on the MH-65D BDI?

A

When TACAN is in manual mode

1H-65D-1
Page 1-D-14

383
Q

What distance does the BDI display in TACAN mode in the MH-65D?

A

Slant range distance

1H-65D-1
Page 1-D-14

384
Q

What are the two distances that can be displayed on the BDI in the MH-65D?

A

TCN and VOR

1H-65D-1
Page 1-D-15

385
Q

Below what speed is the airspeed indicator is unreliable?

A

25 KIAS

1H-65D-1
Page 1-D-15

386
Q

What provides the OAT reading on the CDU and the VEMD?

A

ADU

1H-65D-1
Page 1-D-15

387
Q

What does the encoded altimeter provide an altitude for?

A

TCAS

1H-65D-1
Page 1-D-17

388
Q

The encoded altimeter altitude is based off of what barometric setting?

A

29.92

1H-65D-1
Page 1-D-17

389
Q

What does the RadAlt provide a signal too?

A

Indicators, flight director computer, MFD, and CDU

1H-65D-1
Page 1-D-18

390
Q

How high can the RadAlt show you altitude on the Radalt indicators?

A

2,500 ft AGL

1H-65D-1
Page 1-D-18

391
Q

How high the ADI show a RadAlt altitude?

A

200 ft AGL

1H-65D-1
Page 1-D-18

392
Q

How high will the MFD hover page show the RadAlt altitude?

A

350 ft

1H-65D-1
Page 1-D-18

393
Q

How high will the CDU display the RadAlt altitude?

A

8,000 ft

1H-65D-1
Page 1-D-18

394
Q

How much can the difference be between he RadAlt analog indicator and the MFD?

A

5ft

1H-65D-1
Page 1-D-18

395
Q

If the MFD and the RadAlt analog indicator do not agree which must be the higher one?

A

MFD

1H-65D-1
Page 1-D-18

396
Q

How long does it take the RadAlt system to work up?

A

Approximately 10 minutes

1H-65D-1
Page 1-D-19

Archive (12 decks)

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