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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
WARNING LIGHT INDICATIONS - ENG OIL PRESS
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
WARNING LIGHT INDICATIONS - XMSN OIL PRESS
1. Power - Reduce 2. LAND AS SOON AS PRACTICABLE *If both indications are below 1.0 bar: 3. LAND IMMEDIATELY
27
Engine Sections
- Axial Compressor Section - High Pressure Gas Generator Section - Power Turbine Section - Reduction Gearbox - Main Transmission Shaft and Accessory Gearbox
28
Dynamic Rollover | Definition
Susceptibility to a lateral rolling tendency
29
Dynamic Rollover | Human Factors
- Inattention - Inexperience - Failure to take timely corrective action - Inappropiate control input - Loss of visual reference
30
Dynamic Rollover | Physical Factors
- Main and Tail Rotor Thrust - Center of Gravity - Crosswind - Ground Surface Area - Large Slope Angle
31
Dissymmetry of Lift
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
Settling With Power | Definition
Condition of powered flight in which the helicopter settles in its own downwash.
33
Settling With Power | Conditions Conducive
- Steep approach at high rate descent - Downwind approach - Formation flight approach - Hover above max hover ceiling - Masking / Unmasking
34
Translating Tendency | Definition
Tendency of a single main rotor helicopter to drift laterally in the direction of tail rotor thrust
35
Translating Tendency | Countermeasures
- Pilot Induced Cyclic - Mast / Transmission Tilt - Cyclic or Collective Rigging
36
Transverse Flow Effect | Definition
Differences in lift between the fore and aft portions of the rotor disk.
37
Loss of Tail Rotor Effectiveness
Aero-dynamic condition that causes a helicopter to yaw rapidly and uncontrollably
38
Names of LTE/LTA Causes
- AOA Reduction (60-90) - Weathercock Stability (120-240) - Tail Rotor Vortex Ring State (210-330) - Main Rotor Disk Vortex Intereference (285-315)
39
Grounding time for: Anesthesia (General) Anesthesia (Local) Alcohol Immunization Blood (200 CC) and Plasma Donations Altitude Chamber SCUBA Diving Simulator Sickness Centrifuge Runs
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
Define Stress
The nonspecific response of the body to any demand placed upon it
41
Four Types of Stressors
- Psychosocial (Job, Illness, Family) - Cognitive (Musts/Shoulds) - Physiological (Self-Imposed) - Environmental (Altitude, Speed, Hot/Cold)
42
Define Fatigue
The state of feeling tired, weary, or sleepy that results from periods of anxiety, exposure to harsh environment, or loss of sleep
43
Define Spatial Disorientation
The erroneous inability to determine one’s position, attitude and motion relative the earth or significant objects.
44
Prevention of SD
- 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
Treatment of SD
- Delay intuitive actions - Refer to instruments - Transfer controls to other pilot
46
The sensory inputs the provide orientation and equilibrium are
Visual, Vestibular, and Proprioreceptive
47
Relative motion
Falsely perceived self-motion in relation to the motion of another object
48
Sensory Illusion
A false perception of reality caused by the conflict of orientation information
49
Otolith Organ
Linear Acceleration
50
Semicircular Canal
Angular Acceleration
51
Hypoxia
When the body lacks Oxygen
52
Hypoxic Hypoxia
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
Hypemic Hypoxia
Reduction in blood's Oxygen carrying capacity (i.e. Carbon Monoxide, Nitrites, Sulfa Drugs)
54
Stagnant Hypoxia
Blood's Oxygen carrying capacity is adequate but circulation is inadequate (i.e. Blood flow disruption or extreme gravitational forces)
55
Histotoxic Hypoxia
Interference with the use of Oxygen by poisoning body tissues (i.e. Alcohol, Narcotics or poisons such as Cyanide)
56
Types of Drag
- Parasite - Profile - Induced - Total
57
Parasitic Drag
Non-lifting portions of helicopter
58
Profile Drag
Friction of rotor blades through air
59
Induced Drag
Production of lift. Higher the AOA the more there is
60
Total Drag
Sum of all drag

Common Core (33 decks)

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