Systems Flashcards

1
Q

What wil Happen if the helicopter is shut down with one of its tail rotor cables disconnected?

A

The other will disconnect as well, leaving the blades in a fixed pitch

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2
Q

What is the cant of the Tail rotor and how much lift does it provide?

A

20deg
2.5%

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3
Q

Functions of the HMU

A

PMCANVDTO
Pumps fuel at a high pressure
Meters fuel to the ODV
Collective pitch compensation
Accel/deccel limiting (comp stalls/flameout)
Ng limiting
Variable Geometry
DEC/EDECU lockout over ride
Torque motor to trim NG
Opens Vapor Vent

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4
Q

What is significant about the outer loop?

A

The outer loop is controlled by the #2 FCC and controls trim. Has 100% Authority of the flight controls at the rate of 10% per second

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5
Q

How is DC power Obtained?

A

Batteries
DC Converters (2)

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6
Q

What Axes Have boost?

A

Collective, Pitch, Yaw

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7
Q

Hot Start Prevention

A

Will Abort start @900C as long as NG<60, NP<50

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8
Q

What are the minimum Parking Requirements

A

Gust Lock/Rotor Brake
Parking Brake
Tailwheel Locked
Wheels Chalked

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9
Q

Which axes have trim?

A

Collective
Pitch
Roll
Yaw

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10
Q

Functions of the ODV

A

HOPS
Hot start prevention
Overspeed prevention
Purges fuel
Sequences Fuel (PFHLO)

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11
Q

3 Windings of the Alternator

A

NID
NG signal to the cockpit
Ignition power to the exciters
Dec power

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12
Q

How much PSI does the pitch trim servo require?

A

1000PSI

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13
Q

How long can you fly with a GEN BRG caution?

A

up to 10 HRS

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14
Q

What does a T/R Quad Caution indicate?

A

One/both of the T/R cables have failed

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15
Q

Functions not available in lockout

A

TGT Limiting
Isochronus NP governing
Np reference (INCR/DECR)
Torque matching/load sharing

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16
Q

What Computes Heading, Altitude, Turn Rate

A

EGI

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17
Q

What does HYD pump 2 supply?

A

Pilot assist module, Primary Servo 2

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18
Q

How much pressure does the HYD system supply?

A

3000PSI

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19
Q

When do Engine Anti-Ice advisories appear?

A

Engine Anti-Ice on
Low power settings
Electrical failure

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20
Q

What Busses are powered with only the battery switches on?

A

Battery Bus
Battery Utility Bus
DC Essential Bus

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21
Q

When does the APU ACCUM LOW advisory appear?

A

<2600PSI

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22
Q

When can heading be coupled on the FDDCP?

A

> 50KIAS

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23
Q

When does the impending bypass pop on the pilot assist module?

A

1375PSI

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24
Q

What must be on for FPS to work

A

SAS, Boost, Trim

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25
Q

What does SAS provide? What axes?

A

SAS Provides dynamic stability with short term rate dampening
Pitch, Roll, Yaw

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26
Q

What does the backup pump supply?

A

Everything
APU Accumulator
#2 T/R Servo

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27
Q

What happens if there is a leak in the APU accumulator?

A

if it is >1.5GPM a velocity fuse will close the line

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28
Q

What should you do if the APU fails?

A

Check BITE codes

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29
Q

What type of rotor systems are on the UH-60?

A

Main- Fully Articulated (Lead, Lag, Flap, Feather)
Tail- Rigid

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30
Q

How can vertical speed be coupled?

A

> 50KIAS, 0-2000FPM

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31
Q

What does HYD pump 1 supply?

A

Primary servo 1
T/R servo 1

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32
Q

Why cant both stages of the primary servo’s be isolated at the same time?

A

Electrical interlock

33
Q

What type of bearings are used in the main rotor system?

A

Elastomeric Bearings

34
Q

When must inlet anti-Ice come on?

A

<4deg C- MUST
4-13 - MAY
>13 - WILL NOT

35
Q

Radio Locations

A

1 ARC 201 - Under Co-pilot Seat

#2 ARC 231-Nose
#3 ARC 231-Aft Avionics bay
#4 ARC 201- Aft Avionics bay

36
Q

When will a RSVR LOW caution appear?

A

60% of fluid remaining

37
Q

How are the HYD pumps driven?

A

1&2 - Accessory Modules
Backup- AC Motor

38
Q

What does Go-Around mode provide?

A

750 fpm clim @ 70KIAS

39
Q

What Switch is located on the #1 Accessory Module?

A

Oil Pressure- will illuminate @ 14PSI +/- 2

40
Q

Where can you not extenguish a fire if you have no A/C power?

A

2 Engine bay

41
Q

What Will cause you to switch from a 10min TGT limit to 2.5 min with an EDECU?

A

3% difference in NP VS reference
<96%NP
>5% per second NP drop
Below 50% Q
Engine out

42
Q

Equiptment avialible w/ battery power only

A

basically everything on #2 side

43
Q

When can airspeed be coupled on the FDDCP?

A

50-150 KIAS

44
Q

What sensor is located on the #2 Accesory module?

45
Q

How many fire detectors are on the aircraft?

46
Q

When will inlet anti-ice advisories appear?

A

93degC in inlet

47
Q

What is significant about the inner loop?

A

The inner loop is controlled by both FCC’s, controls the SAS and only has 10% authority of the controls

48
Q

Functions of the MMU

A

Collective to pitch
Counteracts downwash on the stabilator
Collective to roll
Counteracts translating tendency
Collective to yaw
Counteracts anti-torque
Yaw to Pitch
Counteracts the lift of the tail rotor
Collective to airspeed to yaw
Decreases as airspeed increases (0-40 Max, 40-100 decreases, >100 no mixing)

49
Q

What 5 lights turn on the backup pump?

A

HYD Pump 1 LOW
HYD Pump 1 Fail
T/R Servo 1 Fail
HYD pump 2 Fail
APU Accumulator low

50
Q

Where does the APU get its Fuel from

A

1 Fuel cell

51
Q

What system processes airspeed and Altitude?

52
Q

Functions of the DEC

A

INFLTHHOT
Isochronus NP governing(keeps NP@ Reference)
NP reference(INCR/DECR)
Fault codes
Load sharing/Q matching
TGT limiting
Hot start prevention
History counter
Overspeed prevention
Transient droop compensation

53
Q

How long is emergency power applied?

A

15 mins day
12 mins night

54
Q

How many filters are on each pump? When do the Bypasses pop?

A

2- Pressure and return
70+/- 10 PSI over normal

55
Q

How many bleed ports are on the engine?

A

3- Anti-ice start bleed valve & Pneumatic system

56
Q

What does FPS provide? In which axes?

A

FPS provides basic autopilot when coupled with trim
<50KIAS Heading hold
>50KIAS Heading hold & Turn
Coordination
Pitch
Roll
Yaw

57
Q

How much is MTA reduced with engine anti-ice on?

A

20% off the top

58
Q

What is the “Muscle” for trim

A

Electromechanical actuators
Collective
Roll
Yaw
Hydroelectromechanical actuator
Pitch

59
Q

What happens if both T/R cables fail?

A

The tail rotor becomes fixed pitch @ 10.5deg

60
Q

What are the 5 transmission modules?

A

Main Transmission
2 input modules
2 accessory modules

61
Q

What is attached to the accesory modules?

A

HYD Pump
Main Generator

62
Q

How are the main generators cooled?

A

Transmission oil

63
Q

What fire extenguisher must be used if there is no AC power?

64
Q

When must a fuel sample be done?

A

First flight of the day
4 hrs after refuel
Suspected contamination

65
Q

How long does it take the backup pump to turn on?

A

3-5 sec with APU generator
.5 sec with main generator

66
Q

What are the 5 subsystems of AFCS

A

SAS
Trim
FPS
Stabilator
Coupled flight director

67
Q

What limitations are there if the APU is the only source of AC power?

A

The backup pump and windshield de-ice can not be on at the same time

68
Q

How much is MTA decreased if the heater is on?

A

5% , 7.5% with aux heater

69
Q

What type of current is the primary source of power?

70
Q

What are the 4 sections of the engine?

A

Hot, Cold, Power turbine(NP), Accessory

71
Q

What controls the trim?

72
Q

What does ILS decel provide?

A

Deceleration on course/glideslope to 70KIAS @200’

73
Q

When can RALT be coupled?

A

0-1500’AGL

74
Q

When does TGT limiting not work?

A

Lockout
Compressor stalls
Engine starts

75
Q

Purpose of the Stabilator?

A

Provide static and dynamic stability in the pitch axis.
SCALP
Streamlines rotor downwash
Collective coupling
Angle of incidence
Lateral sideslip
Pitch rate feedback

76
Q

Methods of refuel

A

Pressure
359gal, 300gpm @55PSI
Closed Circuit
357gal, 110gpm@15PSI
Gravity
360gal

77
Q

Radio antenna locations

A

1 Whip on tail pylon

#2 bottom of tail
#3 top next to satcom
#4 tail pylon

78
Q

What are the 3 functions of trim?

A

Force Gradient
Muscle for trim
Electronic coupling