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Rucker Test 2 > all decks > Flashcards

all decks Flashcards

1
Q

Max hoist load?

A

600 lbs

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2
Q

Hoist Cable Length?

A

290’ usable cable, 300’ total. First and last 20’ colored orange.

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3
Q

Phases of a Hoist?

A

1: Enroute Phase 2: Operational Phase 3: Recovery Phase 4: Departure Phase

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4
Q

Blackhawk Engine?

A

TWO General Electric (GE) 700/ 701 Turbo Shaft Engine

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5
Q

Main Rotor Length?

A

53’ 8”

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6
Q

Overall Length?

A

64’ 10”

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7
Q

Blade Height? (With Droop Stops)

A

7’ 7”

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8
Q

Tail Rotor Height?

A

6’ 6” (If tail strut properly serviced)

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9
Q

Stabilizer Height?

A

Eye level (Don’t know if this is testable, throwing it on anyways)

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10
Q

5 Sections of UH-60?

A

1: Nose Section 2: Mid-Fuselage (Cabin) 3: Aft Fuselage 4: Tail Cone 5: Tail Rotor Pylon

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11
Q

Fuel Tanks?

A

2 Fuel Tanks Each: 180 gallons (~1225lbs) Total: 360 gallons (~2450lbs) (JP8 ~6.8lbs/gallon)

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12
Q

Max Weight Deckload?

A

300 pounds/ foot^2 or 2.08 pounds/ inch^2

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13
Q

How many Tie downs are there?

A

17 Floor (5,000lbs) 8 Cargo Door (3,500lbs) -Ceiling (4,000lbs) (No # given)

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14
Q

Left / Right Wheel High Slope Limit for any UH-60?

A

15 degrees

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15
Q

Cargo Storage Compartment Max Weight?

A

125 lbs

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16
Q

Auxiliary Power Unit (APU) Accumulator Minimum Start Pressure?

A

2,800 PSI

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17
Q

Slope Limitations?

A

-H-60 With FLIR: 6 degrees Nose down 15 degrees Nose high 15 Left/ Right Wheel Low Without FLIR: 6 degrees Nose up /down 15 degrees Left/ Right Wheel Low

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18
Q

Max Air Speed?

A

193 KIAS

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19
Q

Slope Limitations with Weather?

A

-Subtract 2 degrees for every 5 FULL Knots of wind -Nose down slope with winds >15 Knots is prohibited

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20
Q

Cabin Door Speed in Flight

A

-Can open/ close ONLY for mission tasks <80 Knots -Can fly with doors open up-to 100 KIAS (with soundproofing)

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21
Q

How many generators does the H-60 have?

A

3 Generators: -2x Main Generators (Primary) -1x APU (Secondary)

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22
Q

APU Functions?

A

Pneumatic: -Cabin Heating -Main Engine Starting (APU Accumulator) Electrical: -Ground Operations -Inflight Emergency Power

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23
Q

Where does the APU get its fuel supply?

A

From the #1 Fuel Tank

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24
Q

APU Fire?

A

1: Announce a problem 2: *Identify & Confirm Fire 3: Pull APU T-Handle 4: Switch on the Fire Suppression System APU T-Handle: Diverts extinguisher channels from main engines to APU and cuts APU fuel

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25
Q

What are the four modules of the T-701C/D engine?

A

Accessory Section Hot Section Cold Section Power Turbine

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26
Q

Which components have a bypass indicator on them?

A

The oil filter and fuel filter.

27
Q

What is the procedure for an emergency engine shutdown?

A

Power Control Levers (PCL) to off, fuel selector levers to off, fuel boost pumps off.

28
Q

The H-60 Main Transmission system consists of how many modules?

A

5: 1: Main Module (Transmission) 2: #1 Input Module 3: #1 Accessory Module 4: #2 Input Module 5: #2 Accessory Module

29
Q

Which chip detector is connected to a 30-second time delay to allow small chips and fuzz to burn off?

A

Main transmission.

30
Q

When should the Oil dipstick sides be checked? (Hot & Cold)

A

Hot Side: Within 30 min of shutdown Cold Side : 2 hours past shutdown (Just FYI 7 gallon oil capacity)

31
Q

What is the purpose of the lead stop?

A

To limit the lead spindle travel during rotor break operations.

32
Q

Is single engine operation with the gust lock engaged authorized on the H-60M that has a rotor brake installed?

A

No

33
Q

How long can the intermediate gear box run at cruise flight with loss of all oil?

A

The intermediate gear box may run at cruise flight for UP TO 30 minutes with loss of all oil.

34
Q

What are the primary components of the H-60 hydraulic system?

A

-Hydraulic Pump -Transfer Module -Primary Servos -Tail Rotor Servo

35
Q

The #1 Hydraulic System supplies hydraulic pressure to what components?

A

No. 1 System: #1 Hydraulic Pump -> #1 Transfer Module -> 1st Stage Primary Servos and 1st Stage Tail Rotor Servo.

36
Q

The #2 Hydraulic System supplies hydraulic pressure to what components?

A

No. 2 System: #2 Hydraulic Pump -> #2 Transfer Module -> 2nd Stage Primary Servos and Pilot Assist Module Servos

37
Q

The back-up hydraulic system provides hydraulic pressure to what components?

A

It supplies pressure through the utility module to the second stage tail rotor servo, and it recharges the APU accumulator following APU starts. It also supplies pressure to the #1 and #2 transfer modules to operate all servos normally supplied by the #1 and #2 hydraulic systems when those systems are not operational.

38
Q

The cyclic control system provides what controls for the helicopter.

A

forward, rearward, and lateral

39
Q

The tail rotor (directional) control system determines the helicopter’s what?

A

Yaw (Left / Right) by controlling the pitch of the tail rotor blades.

40
Q

What are the AFCS Subsystems?

A

SAS, FPS, TRIM, Stabilator control system, and Coupled FD (H-60M)

41
Q

True or False: The purpose of the HYD LEAK TEST switch is to electrically check all leak detection/isolation components?

A

TRUE

42
Q

In what position does the Yoke assembly lock in?

A

Trail Position

43
Q

Rating for Landing gear Shock Stages:

A

@11.25G’s: 1st Stage: 0-10 Feet/ Second 2nd Stage: 10-39 Feet/ Second

44
Q

What is considered adequate settling time for JP fuel prior to obtaining a fuel sample?

A

Four Hours

45
Q

How can the H-60 aircraft be refueled?

A

Gravity, Pressure and CCR.

46
Q

What type of current does the battery have?

A

DC

47
Q

What type of current does the Blackhawk use for primary power?

A

AC

48
Q

What power does the Generator output?

A

115/200 Voltage Alternating Current (VAC)

49
Q

What does the Swash Plate do?

A

Transfers input from the pilots to the main rotor flight controls

50
Q

What does the Main Rotor Dampeners do?

A

Reduces Lead and Lag Stresses on the rotors. (Gold band means good)

51
Q

What does the Bifilar System do?

A

Reduces Vibrations

52
Q

How many Pressure Reducer Indicator Button (LRB’s) are on the UH-60?

A

7 Total: -2 per Hydraulic Pump (3 pumps = 6) -1 Pilot Assist Module

53
Q

What do Droop Stops do?

A

Prevent the “Drooping” of the Rotor Blades as they slow and stop

54
Q

What does the Gust Lock do?

A

Locks the rotors in place so they cant spin when aircraft is parked. (Slides upwards from Aft cabin into the Rotor Brake Disc)

55
Q

What do the pitch control rods do?

A

Transmit all the movement of the flight controls from the swashplate to the main rotor blades.

56
Q

How many sections does the Tail Rotor Assembly Have

A

4 Tail Rotor Drive Shaft Sections… -Section I: Between the Main Transmission and Oil Cooler. -Section II: From Rotor Brake to Section III. (Sec. II has 3 rods). -Section III: Between Section II and the Intermediate Gearbox. -Section IV: Between Intermediate Gearbox and the Tail Rotor.

57
Q

True/ False: The APU fuel supply has emergency breakaway valves?

A

FALSE: Fuel Tanks 1 and 2 have emergency breakaway valves. The APU fuel line has no breakaway valve

58
Q

Pressure Refueling numbers?

A

179.5 Total Gallons (1/2 gallon air pocket) 55 PSI 300 Gallons/minute

59
Q

Things to look for in a Fuel Sample?

A

Color. Clarity Cloud or haze. Sediment. Water. Fibrous material.

60
Q

Restraint criteria for cargo?

A

12 G’s forward, 8 G’s lateral 3 G’ up/down/back

61
Q

True/ False: The Load Demand Spindle (LDS) takes input from the Collective?

A

TRUE: -The Load Demand Spindle (LDS) interfaces with the HMU with Collective inputs. (Collective and LDS both have “L”) -The Pilot Available Spindle (PAS) provides inputs into the HMU from changing the position of the Pilot Control Levers (PCL)

62
Q

Cargo Hook Weight Maximums?

A

UH-60 L/M: 9,000 lbs UH-60 A: 8,000lbs

63
Q

How are the generators cooled?

A

Primary Generators: Oil Cooled APU: Air Cooled

Rucker Test 2 (9 decks)

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