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Common Core > P2 Flight Evaluation > Flashcards

P2 Flight Evaluation Flashcards

1
Q

CAUTION INDICATIONS - ENG CHIP [SYSTEM 1 / SYSTEM 2]

A

*ON GROUND
1. Affected Engine - Identify
2. Single Engine Emergency Shutdown - Perform

*IN FLIGHT
1. OEI Flight Condition - Establish
2. Affected Engine - Identify
3. Single Engine Emergency Shutdown - Perform
4. Twist Grip (Affected Engine) - Rotate slowly to IDLE, check indications

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2
Q

CAUTION INDICATIONS - ENG OIL P [SYSTEM 1 / SYSTEM 2]

A
  1. Engine Oil Pressure - Check
  2. OEI Flight Condition - Establish
  3. Affected Engine - Identify
  4. Single Engine Emergency Shutdown - Perform
  5. LAND AS SOON AS PRACTICABLE
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3
Q

CAUTION INDICATIONS - XMSN OIL T

A
  1. XMSN Oil Temperature and Oil Pressure Indication - Check

*If indications are within limits:
2. LAND AS SOON AS PRACTICABLE

*If indications are above limit:
2. Power - Reduce, as much as possible
3. LAND AS SOON AS POSSIBLE

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4
Q

Single Engine Failure - Hover IGE (CLCAS)

A
  1. Collective Lever - Adjust to OEI limits or below
  2. Landing Attitude - Establish
  3. Collective Lever - Raise as necessary to stop descent and cushion landing
  4. Affected Engine - Identify
  5. Single Engine Emergency Shutdown - Perform
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5
Q

Single Engine Failure - Hover OGE [Forced Landing] (CALCAS)

A
  1. Collective Lever - Adjust to maintain rotor RPM
  2. Airspeed - Increase if possible
  3. Landing Attitude - Establish
  4. Collective Lever - Raise as necessary to stop descent and cushion landing
  5. Affected Engine - Identify
  6. Single Engine Emergency Shutdown - Perform
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6
Q

Single Engine Failure - Hover OGE [Fly-away] (CACRACASL)

A
  1. Collective Lever - Adjust to maintain rotor RPM
  2. Airspeed - Increase if possible
  3. Collective Lever - Adjust to OEI limits or below
  4. Rotor Speed - Trim to maximum
  5. Airspeed - Gain, 65KIAS (Vy)
  6. Collective Lever - Reduce to OEI MCP or below
  7. Affected Engine - Identify
  8. Single Engine Emergency Shutdown - Perform
  9. LAND AS SOON AS PRACTICABLE
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7
Q

Single Engine Failure - Flight (ORASL)

A
  1. OEI Flight Condition - Establish
  2. Rotor Speed - Trim to maximum
  3. Affected Engine - Identify
  4. Single Engine Emergency Shutdown - Perform
  5. LAND AS SOON AS PRACTICABLE
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8
Q

Single Engine Emergency Shutdown

A
  1. Twist Grip (Affected Engine) - Rotate slowly to IDLE, check indications, then to OFF
  2. Rotor Speed - Trim to maximum
  3. BLD HTG EMER/NORM sw - EMER
  4. BLD HTG Rheostat - ON
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9
Q

Engine Overspeed - Governor Failure (CVN-ATL)

A
  1. Collective Lever - Raise as necessary to maintain N2 and NRO within limits
  2. VAR NR System NORM/MAN Switch - Check MAN
  3. N2 TRIM Sw - Try to trim NRO to 101% with matched torque

*If step 3 is not possible:
4. Affected Engine - Identify
5. Twist Grip (Affected Engine) - Rotate towards IDLE until N2 and NRO stabilize in normal range and FLI needles match
6. LAND AS SOON AS PRACTICABLE

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10
Q

Engine Underspeed - Governor Failure (OBVAN-TL-S)

A
  1. OEI Flight Condition - Establish
  2. Bleed Air Consumers - Off
  3. VAR NR System NORM/MAN pb - Check MAN
  4. Affected Engine - Identify
  5. N2 TRIM Sw - Compensate N2/NRO drop and try to match torque

If torque match is not possible:
6. Twist Grip (Affected Engine) - Release stop plate and rotate towards FLIGHT until N2 and NRO stabilize in normal range and FLI needles match
7. LAND AS SOON AS POSSIBLE

If no residual torque (affected engine) is available:
8. Single Engine Emergency Shutdown - Perform

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11
Q

Engine Oil Temperature High (OATOSL)

A
  1. OEI Flight Condition - Establish
  2. Affected Engine - Identify
  3. Twist Grip (Affected Engine) - Adjust to 20-30% torque (TWIST GRIP caution indication comes on))
  4. Oil Temperature Indicator (Affected Engine) - Monitor

*If engine oil temperature still remains above limit:
5. Single Engine Emergency Shutdown - Perform
6. LAND AS SOON AS PRACTICABLE

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12
Q

Double Engine Failure - Hover IGE (RLC)

A
  1. Right Pedal - Apply as necessary to stop yaw
  2. Landing Attitude - Establish
  3. Collective Lever - Raise as necessary to cushion landing
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13
Q

Double Engine Failure - Flight

A
  1. Autorotation - Perform
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14
Q

Double Engine Emergency Shutdown

A

*ON GROUND
1. Both Twist Grips - OFF
2. Both FUEL PRIME PUMP sw - OFF
3. BAT MSTR sw - OFF

*IN FLIGHT
1. Both Twist Grips - OFF
2. Both EMER OFF sw - Press

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15
Q

Autorotation (CAD-B)

A
  1. Collective Lever - Reduce to maintain NRO within limits
  2. Airspeed - 75KIAS Recommended
  3. Double Engine Emergency Shutdown - Perform
  4. BAT MSTR Sw - OFF
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16
Q

Cabin Fire [On Ground] (DPF)

A
  1. Double Engine Emergency Shutdown - Perform
  2. Passengers - Alert / Evacuate
  3. Fire - Extinguish if possible
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17
Q

Cabin Fire [In Flight] (APHFFLD)

A
  1. Airspeed - 65 KIAS recommended
  2. Passengers - Alert
  3. Heating / Air Conditioner (if installed) - OFF
  4. Fire - Extinguish if possible
  5. Fumes, Smoke - Eliminate, open sliding dors, windows and vents (fresh air)
  6. LAND AS SOON AS POSSIBLE
  7. Double Engine Emergency Shutdown - Perform
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18
Q

Warning Panel Indications (CARB FLEX)

A

Cargo Smoke
AP
Rotor RPM
Bat Temp
Fire 1/2
Low Fuel
Eng Fail 1/2
XMSN Oil Pressure

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19
Q

WARNING LIGHT INDICATIONS - BAT TEMP

A

*ON GROUND
1. BAT MSTR sw - OFF

*IN FLIGHT
1. BAT MSTR sw - OFF
2. LAND AS SOON AS POSSIBLE

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20
Q

WARNING LIGHT INDICATIONS - ROTOR RPM

A
  1. Collective Lever - Adjust as necessary to maintain NRO within normal range
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21
Q

WARNING LIGHT INDICATIONS - FIRE [ENG 1 or ENG 2] On Ground

A
  1. FIRE sw (Affected Engine) - Raise guard, press
  2. Both FUEL PRIME PUMPS - Check off
  3. BOT 1 / BOT 2 pb - Press; Bottle 1 Activated; EXT indicator light comes on (EMER OFF SW pnl)
  4. Clock Stop Watch - Start (After BOT 1 Legend and EXT indicator light go off (EMER OFF SW pnl))
  5. Double Engine Emergency Shutdown - Perform
  6. BOT 1 / BOT 2 pb - Press; Bottle 2 Activated; EXT indicator light comes on (EMER OFF SW pnl)
  7. BAT MSTR sw - OFF
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22
Q

WARNING LIGHT INDICATIONS - FIRE [ENG 1 or ENG 2] In Flight (OAFBCASLBL)

A
  1. OEI Flight Condition - Establish
  2. Airspeed - Reduce if IAS is exceeding 100kts
  3. FIRE sw (Affected Engine) - Raise Guard, press
  4. BOT 1 / BOT 2 pb - Press; Bottle 1 Activated; EXT indicator light comes on (EMER OFF SW Panel)
  5. Clock Stop Watch - Start (After BOT 1 Legend and EXT indicator light go off (EMER OFF SW Panel))
  6. Affected Engine - Identify
  7. Single Engine Emergency Shutdown - Perform
  8. LAND AS SOON AS POSSIBLE
  9. BOT 1 / BOT 2 pb - Press; Bottle 2 Activated; EXT indicator light comes on (EMER OFF SW Panel)
  10. LAND IMMEDIATELY
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23
Q

WARNING LIGHT INDICATIONS - LOW FUEL

A

*If both FUEL LOW warning lights remain on:
1. LAND WITHIN 10 MINUTES

*If one FUEL LOW warning lights remain on:
1. Expect Single Engine Failure

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24
Q

WARNING LIGHT INDICATIONS - ENG 1 / ENG 2 FAIL

A
  1. OEI Flight Condition - Establish
  2. Affected Engine - Identify
  3. Single Engine Emergency Shutdown - Perform
  4. LAND AS SOON AS PRACTICABLE
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25
Q

WARNING LIGHT INDICATIONS - ENG OIL PRESS

A
  1. Engine Oil Pressure - Check
  2. OEI Flight Condition - Establish
  3. Affected Engine - Identify
  4. Single Engine Emergency Shutdown - Perform
  5. LAND AS SOON AS PRACTICABLE
26
Q

WARNING LIGHT INDICATIONS - XMSN OIL PRESS

A
  1. Power - Reduce
  2. LAND AS SOON AS PRACTICABLE

*If both indications are below 1.0 bar:
3. LAND IMMEDIATELY

27
Q

Engine Sections

A
  • Axial Compressor Section
  • High Pressure Gas Generator Section
  • Power Turbine Section
  • Reduction Gearbox
  • Main Transmission Shaft and Accessory Gearbox
28
Q

Dynamic Rollover

Definition

A

Susceptibility to a lateral rolling tendency

29
Q

Dynamic Rollover

Human Factors

A
  • Inattention
  • Inexperience
  • Failure to take timely corrective action
  • Inappropiate control input
  • Loss of visual reference
30
Q

Dynamic Rollover

Physical Factors

A
  • Main and Tail Rotor Thrust
  • Center of Gravity
  • Crosswind
  • Ground Surface Area
  • Large Slope Angle
31
Q

Dissymmetry of Lift

A

Unequal lift across the rotor disk resulting from the difference in the velocity of air over the advancing blade half and the retreating blade half.

32
Q

Settling With Power

Definition

A

Condition of powered flight in which the helicopter settles in its own downwash.

33
Q

Settling With Power

Conditions Conducive

A
  • Steep approach at high rate descent
  • Downwind approach
  • Formation flight approach
  • Hover above max hover ceiling
  • Masking / Unmasking
34
Q

Translating Tendency

Definition

A

Tendency of a single main rotor helicopter to drift laterally in the direction of tail rotor thrust

35
Q

Translating Tendency

Countermeasures

A
  • Pilot Induced Cyclic
  • Mast / Transmission Tilt
  • Cyclic or Collective Rigging
36
Q

Transverse Flow Effect

Definition

A

Differences in lift between the fore and aft portions of the rotor disk.

37
Q

Loss of Tail Rotor Effectiveness

A

Aero-dynamic condition that causes a helicopter to yaw rapidly and uncontrollably

38
Q

Names of LTE/LTA Causes

A
  • AOA Reduction (60-90)
  • Weathercock Stability (120-240)
  • Tail Rotor Vortex Ring State (210-330)
  • Main Rotor Disk Vortex Intereference (285-315)
39
Q

Grounding time for:

Anesthesia (General)

Anesthesia (Local)

Alcohol

Immunization

Blood (200 CC) and Plasma Donations

Altitude Chamber

SCUBA Diving

Simulator Sickness

Centrifuge Runs

A

Anesthesia (general) - 48 hr

Anesthesia (Local) - 12 hr

Alcohol - 12 hr or no symptoms

Immunization - 12 hr

Blood (200CC) and Plasma Donations - 72/24 hr

Altitude Chamber - 24 hr

SCUBA Diving - 24 hr

Simulator Sickness - 12 hr

Centrifuge Runs - 6 hr

40
Q

Define Stress

A

The nonspecific response of the body to any demand placed upon it

41
Q

Four Types of Stressors

A
  • Psychosocial (Job, Illness, Family)
  • Cognitive (Musts/Shoulds)
  • Physiological (Self-Imposed)
  • Environmental (Altitude, Speed, Hot/Cold)
42
Q

Define Fatigue

A

The state of feeling tired, weary, or sleepy that results from periods of anxiety, exposure to harsh environment, or loss of sleep

43
Q

Define Spatial Disorientation

A

The erroneous inability to determine one’s position, attitude and motion relative the earth or significant objects.

44
Q

Prevention of SD

A
  • Never fly VMC and IMC at the same time
  • Never fly without visual reference
  • Avoid fatigue, smoking, hypoxia, anxiety
  • Trust the instruments, proper scans
45
Q

Treatment of SD

A
  • Delay intuitive actions
  • Refer to instruments
  • Transfer controls to other pilot
46
Q

The sensory inputs the provide orientation and equilibrium are

A

Visual, Vestibular, and Proprioreceptive

47
Q

Relative motion

A

Falsely perceived self-motion in relation to the motion of another object

48
Q

Sensory Illusion

A

A false perception of reality caused by the conflict of orientation information from one or more mechanisms of the equilibrium

49
Q

Otolith Organ

A

Linear Acceleration

50
Q

Semicircular Canal

A

Angular Acceleration

51
Q

Hypoxia

A

When the body lacks Oxygen

52
Q

Hypoxic Hypoxia

A

Occurs when there is not enough Oxygen in the air or when decreasing atmospheric pressure prevents diffusion of Oxygen from the lungs to the bloodstream

53
Q

Hypemic Hypoxia

A

Reduction in blood’s Oxygen carrying capacity (i.e. Carbon Monoxide, Nitrites, Sulfa Drugs)

54
Q

Stagnant Hypoxia

A

Blood’s Oxygen carrying capacity is adequate but circulation is inadequate (i.e. Blood flow disruption or extreme gravitational forces)

55
Q

Histotoxic Hypoxia

A

Interference with the use of Oxygen by poisoning body tissues (i.e. Alcohol, Narcotics or poisons such as Cyanide)

56
Q

Types of Drag

A
  • Parasite
  • Profile
  • Induced
  • Total
57
Q

Parasitic Drag

A

Non-lifting portions of helicopter

58
Q

Profile Drag

A

Friction of rotor blades through air

59
Q

Induced Drag

A

Production of lift. Higher the AOA the more there is

60
Q

Total Drag

A

Sum of all drag

Common Core (10 decks)

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