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TH-57 Bell 206 > EP's (CAMI's only) - NATOPS confirmed > Flashcards

EP's (CAMI's only) - NATOPS confirmed Flashcards

1
Q

Abort Start

A
  1. Twist grip - Close
  2. Starter - OFF after TOT stabilizes at 400*C or below
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2
Q

Compressor Stall

A
  1. Collective - Lower
  2. ENG Anti-ice switch - ON
  3. Cabin Heat Valve - ON
  4. Check power available

If power is insufficient to maintain level flight:
5. Autorotate
6. Twist grip - Flight Idle

If power is sufficient to maintain level flight:
7. Land as soon as possible

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3
Q

Engine Overspeed (Nf) Rotor RPM (Nr)

A
  1. Twist grip - Reduce (to maintain Nf/Nr in operating range)
  2. Collective/twist grip - Coordinate
  3. Land as soon as possible
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4
Q

Underspeeding Nf/Nr

A
  1. Collective - Lower as required to maintain a minimum of 90% Nr
  2. Twist grip - Full open
  3. GOV RPM - Full increase

If underspeed persists:
4. Check power available

If power is not sufficient:
5. Autorotate

If sufficient power is available:
6. Land as soon as possible

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5
Q

Fuel Control Failure

A
  1. Collective - Adjust as required to maintain Nr in operating range
  2. Twist grip - Adjust as required to maintain Nf in operating range
  3. Land as soon as possible
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6
Q

Engine Chip

A
  1. Check for secondary indications

If secondary indications exist:
2. Land as soon as possible
If no secondary indications exist, proceed as follows:

First chip light:
3. Press CLEAR CHIP
If ENG CHIP remains:
4. Land as soon as possible
If ENG CHIP extinguishes:
5. Note time and continue flight

Second chip light:
If within 30 minutes of the first:
6. Land as soon as possible
If more than 30 minutes have elapsed since the first light:
7. Proceed as with the first light

Any subsequent ENG CHIP caution light within 50 hours of the first:
8. Land as soon as possible

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7
Q

Engine Restart in Flight

A
  1. Ng - Note

If Ng is below 12 percent:
2. Twist grip - Close
3. Starter - ON
4. At 12 percent Ng, Twist grip - Full open

If Ng is 12 percent or above:
5. Starter - ON

If light-off occurs:
6. At 58 percent Ng, starter - OFF
7. Land as soon as possible

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8
Q

Emergency Shutdown

A
  1. Twist grip - Close
  2. Fuel valve - OFF
  3. BAT switch - OFF
  4. [C] STBY ATT IND switch - OFF
  5. [C] Rotor brake - Engage immediately
  6. Helicopter - Egress, as required. Use fire bottle or get clear of the aircraft as applicable
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9
Q

Main Drive Shaft Failure

A
  1. Autorotate
  2. Twist grip - Adjust, if necessary, to maintain Nf in operating range

When on deck:
Emergency shutdown - Complete

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10
Q

Sprag Clutch Slippage

A
  1. Autorotate
  2. Twist grip - FLT IDLE

If time and altitude permit:
3. Twist grip - Smoothly rotate to full open

If Nf/Nr are married:
4. Collective - Increase

If sprag clutch continues to slip:
5. Autorotate
6. Twist grip - Closed

If sprag clutch reengages:
7. Land as soon as possible

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11
Q

Transmission Malfunction

A

If failure is imminent:
1. Land immediately
2. Shoulder harness - Lock

If failure is not imminent:
3. Land as soon as possible

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12
Q

Transmission Chip

A

First TRANS CHIP caution light:
1. Check for secondary indications
If secondary indications exist:
2. Transmission Malfunction Procedure - Perform
If no secondary indications exist:
3. Press CLEAR CHIP

If TRANS CHIP caution light remains illuminated:
4. Transmission Malfunction Procedure - Perform
If TRANS CHIP light extinguishes:
5. Note the time and continue flight

Second TRANS CHIP caution light.
If within 30 minutes of the first:
6. Transmission Malfunction Procedure - Perform
If more than 30 minutes have elapsed since the first TRANS CHIP caution light:
7. Proceed as with the first TRANS CHIP caution light

Any subsequent TRANS CHIP caution light within 50 hours of the first:
8. Transmission Malfunction Procedure - Perform

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13
Q

Fuel Boost Pump Failure

A
  1. Descent - Initiate if above 6,000’ feet PA and flight permits
  2. Fuel pressure and quantity - Note
  3. Land as soon as possible

If only one boost pump has failed (fuel pressure 4 to 30 psi):
4. Land as soon as practicable

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14
Q

Suspected Fuel Leakage

A
  1. Land as soon as possible

If time and altitude permit:
2. Transmit position and intentions
3. Unnecessary electrical equipment - Secure

When on deck:
4. Emergency Shutdown - Complete

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15
Q

Airframe Fuel Filter Caution

A
  1. Land as soon as possible
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16
Q

Hydraulic Power Cylinder Malfunction

A
  1. HYDRAULIC BOOST switch - OFF
  2. Helicopter - Regain control
  3. Airspeed - Adjust (to obtain most comfortable control movement level)
  4. Land as soon as possible
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17
Q

Electrical Fire - Known Origin

A
  1. Affected equipment - Secure
  2. Affected circuit breakers - Pull

If fire persists:
3. Electrical Fire - Unknown Origin procedure - Execute

If fire extinguishes:
4. Land as soon as practicable

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18
Q

Electrical Fire - Unknown Origin

A
  1. BAT switch - OFF
  2. [C] STBY GEN switch - OFF
  3. [C] If in VMC, STBY ATT IND switch - OFF
  4. MAIN GEN switch - OFF

If fire persists:
5. Land immediately

If fire extinguishes:
6. Land as soon as possible

When on deck:
7. Emergency Shutdown - Complete

If electrical power is required to restore minimum equipment for continued flight, proceed as follows: SEE PCL for further steps

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19
Q

Engine Fire in Flight

A
  1. Confirm existence of fire

If fire exists:
2. Land immediately

If fire not confirmed:
3. Land as soon as possible

When on deck:
4. Emergency Shutdown - Complete

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20
Q

Fuselage Fire

A
  1. Land immediately

When on deck:
2. Emergency Shutdown - Complete

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21
Q

Smoke/Fume Elimination

A
  1. ECS and DEFOG blower - OFF
  2. Vents/windows - Open

If smoke/fumes persist:
3. Slip or skid aircraft to eliminate smoke and fumes

If source of the smoke and/or fumes cannot be identified:
4. Land as soon as possible

22
Q

Post Shutdown Fire (Internal)

A
  1. Starter - Engage
  2. Fuel valve - OFF
  3. Igniter circuit breaker - Pull
  4. Starter - Secure after fire is extinguished
23
Q

Mast Bumping

A

If mast bumping is suspected:
1. Establish positive G load and/or balanced flight (as required)
2. Land immediately

24
Q

Uncommanded Right Roll During Flight Below 1G

A
  1. Cyclic - Immediately apply aft to establish positive g load on rotor, then center laterally

When main rotor returns to a positive thrust condition:
2. Controls - As required to regain balanced flight

If mast bumping has occurred:
3. Land immediately

25
Q

Fixed Pitch in a Hover

A

Fixed Pitch Pedal in a Hover - Right Yaw:
If rate of rotation is not excessive and landing surface is smooth and firm:
1. Collective - Decrease to effect a power-on landing

If rate of rotation is excessive or landing surface is unsuitable for a power-on landing:
2. Twist grip - Reduce as nose approaches windline
3. Cyclic - Eliminate drift
4. Collective - Increase to cushion landing

Fixed Pitch Pedal in a Hover - Left Yaw:
If rate of rotation is not excessive and landing surface is smooth and firm:

  1. Collective - Decrease to affect a power-on landing

If rate of rotation is excessive or landing surface is unsuitable for a power-on landing:
2. Smoothly increase collective to stop the left yaw
3. When the left yaw has stopped, smoothly decrease collective to set up for a landing
4. Eliminate lateral drift with cyclic as the aircraft settles
5. Continue to smoothly lower collective once on deck to control yaw and transfer aircraft weight to the skids

26
Q

Loss of Tail Rotor Effectiveness

A
  1. Pedals - Full left
  2. Collective - Lower (as altitude permits)
  3. Airspeed - Increase

If spin cannot be stopped:
4. Autorotate

27
Q

High-Frequency Vibration

A
  1. ECS - OFF

If vibrations continue:
2. Land as soon as possible

If vibrations cease:
3. Land as soon as practicable

28
Q

Complete Loss of Tail Rotor Thrust

A

In a hover:
1. Twist grip - Flight idle
2. Cyclic - Eliminate drift
3. Collective - Increase to cushion landing

Transition to forward flight or hover/air taxi:
1. Twist grip - Flight idle
2. Cyclic - Eliminate sideward drift
3. Collective - Increase to cushion landing

At altitude:
4. Collective - Lower to control yaw

If yaw is not controllable:
5. Autorotate
6. Twist grip - Flight idle

If yaw is controllable:
7. Continue powered flight and set up to a suitable landing area at or above minimum rate of descent autorotational airspeed
8. Autorotate
9. Twist grip - Rotate to flight idle prior to touchdown

29
Q

Tail Rotor Chip Caution

A
  1. Land as soon as possible
30
Q

Engine Failure in Flight

A
  1. Autorotate
  2. Shoulder harness - Lock

If time and altitude permit:
3. Mayday - Transmit
4. Transponder - Emergency
5. Engine Restart in Flight procedure - as required

31
Q

Engine Failure at High Airspeed and Low Altitude

A
  1. Cyclic - Immediately apply aft
  2. Autorotate
32
Q

Emergency Descent

A
  1. Collective - Lower (to minimum pitch)
  2. Airspeed - 130 KIAS (122 KIAS Maximum with FCS on)
33
Q

Immediate Landing/Ditching

A
  1. Crew and Passengers - Alert
  2. Shoulder harness - Lock
  3. Mayday - Transmit
  4. Transponder - Emergency
  5. Doors - Open/Jettison - As required
  6. Landing light/search light - As required

When on deck:
7. Emergency Shutdown - Complete

If water landing:
8. Underwater Egress - Execute

34
Q

Underwater Egress

A
  1. SEBD - Don, as required
  2. Communication cords - Disconnect
  3. Doors - Open/Jettison
  4. Place hand on known reference point

Once all violent motion has stopped:
5. Shoulder harness/lapbelt - Release
6. Exit helicopter

After Egress:
7. Swim clear and inflate LPU

35
Q

Main Generator Malfunction

A
  1. MAIN GEN FIELD and MAIN GEN RESET circuit breakers - Check in
  2. MAIN GEN switch - Reset, then ON

If problem is not corrected:
3. MAIN GEN switch - OFF
4. Unnecessary electrical equipment - OFF
5. [C] NORMAL/RECOVER switch - As desired
6. [C] Voltmeter Select Switch - MAIN BAT
7. Land as soon as practicable

If problem is corrected:
8. Continue flight

36
Q

Standby Generator Failure [C]

A
  1. STBY GEN RELAY circuit breaker - In. Check voltmeter for indication
  2. STBY GEN switch - OFF, then ON

If power not restored:
3. STBY GEN switch - OFF
4. Land as soon as practicable

If power restored:
5. Continue flight

37
Q

Battery Hot Caution

A
  1. BAT Switch - Off
  2. Land as soon as possible
38
Q

Battery Temp Caution

A
  1. BAT Switch - Off
  2. Flight may be continued
39
Q

Spare Caution

A
  1. Check for other indications
  2. Land as soon as possible
40
Q

Overtorque

A

Indications:
1. Torque Gauge Flashes twice per second
2. TRQ Caution Light flashes twice per second
3. Torque limit exceeded

CAMI:

If overtorque exceeding 120%:
1. Land as soon as possible

If overtorque of 120% or less:
2. Land as soon as practicable

41
Q

Overtemp

A

Indications:
1. TOT gauge flashes twice per second
2. TOT caution light flashes twice per second
3. TOT limit exceeded

CAMI:
1. Land as soon as possible

42
Q

Ng, Nf, or Nr limits exceeded

A
  1. Land as soon as possible
43
Q

Pitot-Static Instruments

A
  1. PITOT HEAT switch(es) - HEAT

If pitot heat does not remedy the situation, accomplish the following:
2. [C] Alternate static source knob - Pull

If icing conditions are present:
3. Icing procedures - Execute

If icing conditions are not present:
4. Land as soon as practicable

44
Q

Torquemeter Wet Line Rupture

A
  1. Monitor engine oil instruments
  2. Land as soon as possible
45
Q

Engine or Transmission Oil Pressures

A

If engine oil pressure is exhibiting abnormal indications:
1. Land as soon as possible

If transmission oil pressure is exhibiting abnormal indications:
2. Transmission Malfunction Procedure - Perform

46
Q

Engine or Transmission Oil Temperature Malfunction

A

If engine oil temperature gauge exceeds red line limitations:
1. Land as soon as possible

If transmission oil temperature gauge exceeds red line limitations:
2. Transmission Malfunction Procedure - Perform

If either oil temperature gauge fluctuates or fails to zero:
3. Land as soon as practicable

47
Q

Icing

A
  1. ENG ANTI-ICING - ON
  2. PITOT HEAT switches - HEAT
  3. [C] Alternate static source knob - As required
  4. Descend or climb to a warmer temperature or vacate clouds/moisture

If unable to get clear of icing conditions:
5. Land as soon as possible

48
Q

Power Required Exceeds Power Available

A
  1. Collective - Lower as required to maintain a minimum of 90% Nr
  2. Twist grip - Full open
  3. Angle of bank - Level wings
  4. Airspeed - 50 KIAS (minimum power required airspeed)
  5. Jettison - As required

If impact is imminent:
6. Level skids to conform to terrain
7. Cushion the landing

49
Q

Vortex Ring State

A
  1. Controls - As required to clear vortex ring state

If impact is imminent:
2. Level skids to conform to terrain

50
Q

Rotor Blade Stall

A
  1. Severity of maneuver - Decrease
  2. Collective - Lower
  3. Airspeed - Decrease
  4. Altitude - Descend, if flight permits
  5. Rotor rpm - Increase
51
Q

Dynamic Rollover

A
  1. Collective - Lower to stop the roll
  2. Cyclic - Neutral

TH-57 Bell 206 (1 decks)

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