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Emergency Procedures > Robinson R44 > Flashcards

Robinson R44 Flashcards

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1
Q

Three Conditions Requiring Autorotation

A

Power Failure

Drivetrain Failure

Oil Pressure Failure

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2
Q

Tachometer Failure

A

If rotor or engine tachometer malfunctions in flight, use remaining tachometer to monitor RPM. If it is not clear which tachometer is malfunctioning or if both tachometers malfunction, allow governor to control RPM and land as soon as practical.

NOTE:

Each tachometer, the governor, and the low RPM horn are on separate power circuits. A special circuit allows the battery to supply power to the tachometers with the battery and alternator switches both off. (Low RPM horn and Governor are inoperative)

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3
Q

Low Rotor Horn

A

The horn activates simultaneously with the Low Rotor Caution Light and indicates rotor speed below 97% RPM. To restore RPM, lower collective, roll throttle on and, in forward flight apply aft cyclic. Horn and light are disabled when collective is full down.

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4
Q

Carbon Monoxide Light

A

Indicates elevated levels of carbon monoxide (CO) in cabin. Shut off heater and open nose and door vents. If hovering, land or transition to forward flight. If symptoms of CO poisoning (headache, drowsiness, dizziness) accompany light, land immediately.

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5
Q

Loss of Tail Rotor Thrust (Hover)

A

Failure is usually indicated by nose right yaw which cannot be stopped by applying left pedal

Immediately roll throttle off into overtravel spring and allow aircraft to settle

Raise collective just before touchdown to cushion landing

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6
Q

Land as Soon as Practical

A

Landing site is at pilot’s discretion based on nature of problem and available landing areas. Flight beyond nearest airport is not recommended.

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7
Q

Brake Light

A

Indicates rotor brake is engaged. Release immediately in flight or before starting engine.

Starter will not operate with rotor brake engaged

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8
Q

Air Restart Procedure

A

CAUTION

Do not attempt restart if engine malfunction is suspected or before safe autorotation is established (or below 2000’ AGL)

  1. Mixture – Full Rich
  2. Throttle – Closed, then cracked slightly
  3. Actuate starter with left hand
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9
Q

Governor Failure

A

If engine RPM governor malfunctions, grip throttle firmly to override the governor, then switch governor off. Complete flight using manual throttle control.

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10
Q

STARTER ON Light

A

Indicates starter motor is engaged. If light does not go out when ignition switch is released from start position, immediately pull mixture off and turn battery switch off.

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11
Q

Vortex Ring State Recovery
(Vichuard)

A

Raise collective to takeoff power
Left Pedal (as required)
Right Cyclic

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12
Q

Engine Fire (In Flight)

A
  1. Enter autorotation
  2. Cabin Heat – OFF (if time permits)
  3. Cabin Vent – ON (if time permits)
  4. If engine is running, perform normal landing, then pull fuel mixture OFF and shut fuel valve OFF;
    If engine stops running, shut fuel valve OFF and complete autorotation landing
  5. Battery switch – OFF
  6. If time permits, apply rotor brake to stop rotors
  7. Exit helicopter
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13
Q

Power Failure (Above 500 Feet AGL)

A
  1. Lower collective immediately to maintain rotor RPM
  2. Establish a steady glide at approximately 70 KIAS
  3. Adjust collective to keep RPM between 97 and 108% or apply full down collective if light weight prevents attaining above 97%
  4. Select landing spot and, if altitude permits, maneuver so landing will be into wind
  5. A restart may be attempted at pilot’s discretion if sufficient time is available (>2,000 AGL)
  6. If unable to restart, turn unnecessary switches and fuel valve off
  7. At about 40 feet AGL, begin cyclic flare to reduce rate of descent and forward speed
  8. At about 8 feet AGL, apply forward cyclic to level ship and raise collective just before touchdown to cushion landing
  9. Touch down in level attitude with nose straight ahead
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14
Q

M/R TEMP Light

A

Indicates excessive temperature of main rotor gearbox

NOTE

If light is accompanied by any indication of a problem such as noise, vibration, or temperature rise, land immediately.

If there is no other indication of a problem, land as soon as practical.

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15
Q

High RPM Warble

A

Indicates rotor speed is approaching 108% RPM limit. Raise collective as required to control RPM.

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16
Q

Maximum Glide Distance Configuration

A
  1. Airspeed approximately 90 KIAS
  2. Rotor RPM approximately 90%

Best glide ratio is about 4.7:1 or one nautical mile per 1,300 feet AGL

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17
Q

CLUTCH Light

A

Indicates clutch actuator is on, either engaging or disengaging clutch. When switch is in the ENGAGE position, light stays on until belts are properly tensioned. Never take off before the light goes out.

NOTE

Clutch light may come on momentarily during run-up or during flight to re-tension belts as they warm up and stretch slightly. This is normal. If however, the light flickers or comes on in flight and does not go out within 10 seconds, pull CLUTCH circuit breaker and land as soon as practical. Reduce power and land immediately if there are other indications of drive system failure (be prepared to enter autorotation).

18
Q

OIL Light

A

Indicates loss of engine power or oil pressure.

Check engine tachometer for power loss. Check oil pressure gauge and, if pressure loss is confirmed, land immediately.

Continued operation without oil pressure will cause serious engine damage and engine failure may occur.

19
Q

LOW FUEL Light

A

Indicates approximately three (3) gallons of usable fuel remaining. The engine will run out of fuel after ten (10) minutes at cruise power (18 gph)

Caution

Do not use low fuel caution light as a working indication of fuel quantity.

20
Q

Electrical Fire (In-Flight)

A
  1. Battery and Alternator switches - OFF
  2. Open cabin vents
  3. Land immediately
  4. Pull mixture OFF and shut fuel valve OFF
  5. If time permits, apply rotor brake to stop rotors
  6. Exit the helicopter

Note:
Low RPM warning system and governor are inoperative with battery and alternator switches both OFF

21
Q

Full Throttle Light

A

Indicates engine near full throttle. The governor will be ineffective because it cannot increase throttle to maintain RPM. Lower collective as required to extinguish light

CAUTION
Above 4,000 feet, throttle-collective correlation and governor are less effective. Therefore, power changes should be slow and smooth.

CAUTION
At high power settings above 6,000 feet, the throttle is frequently wide open and RPM must be controlled with collective.

22
Q

Fuel Filter Light (RAVEN II)

A

Indicates fuel strainer contamination. If no other indications of a problem, land as soon as practical. If light is accompanied by aux fuel pump warning light or erratic engine operation, land immediately.

23
Q

Power Failure (Between 8 feet and 500 feet AGL)

A
  1. Lower collective immediately to maintain rotor RPM
  2. Adjust collective to keep RPM between 97% and 108% or apply full down collective if light weight permits attaining above 97%
  3. Maintain airspeed until ground is approached, then begin cyclic flair to reduce rate of descent and forward speed
  4. At about 8 feet AGL apply forward cyclic to level ship and raise collective just before touchdown to cushion landing
  5. Touchdown in level attitude with nose straight ahead
24
Q

Engine Fire Light

A

Indicates possible fire in the engine compartment

Execute Engine Fire Procedure

Illuminates at 275 degrees +/- 10 degrees

25
Q

ALT Light

A

Indicates low voltage or possible alternator failure

Turn off nonessential equipment and switch ALT off then back on after one second. If light stays on or ammeter still indicates discharge, land as soon as practical.

Continued flight without a functioning alternator can result in loss of power to tachometers, producing a hazardous flight condition.

26
Q

Power Failure (Below 8 feet AGL)

A
  1. Apply right pedal as required to prevent yawing
  2. Allow helicopter to settle
  3. Raise collective just before touchdown to cushion landing
27
Q

Hydraulic System Failure

A

Hydraulic system failure indicated by heavy or stiff cyclic and collective controls

Loss of hydraulic fluid may cause intermittent and/or vibrating feedback in the controls

Control will be normal except for increase in stick forces

  1. HYD Switch - verify ON
  2. If hydraulics not restored, HYD switch - OFF
  3. Adjust airspeed and flight conditions as desired for comfortable control
  4. Land as soon as practical
28
Q

Emergency Water Landing (Power Off)

A
  1. Follow same procedures as for power failure over land until contacting the water. If time permits, unlatch doors prior to water contact.
  2. Apply lateral cyclic when aircraft contacts water to stop the rotors
  3. Release seatbelts and quickly clear aircraft when rotors stop
29
Q

AUX FUEL PUMP (Raven II)

A

Indicates low auxiliary fuel pump pressure. If no other indications of a problem, land as soon as practical. If light is accompanied by erratic engine operation, land immediately.

30
Q

Air Restart Procedure (Raven II)

A

CAUTION

Do not attempt restart if engine malfunction is suspected or before safe autorotation is established. Air restarts not recommended below 2000’ AGL

  1. Mixture – Off
  2. Throttle – Closed
  3. Starter Engaged
  4. Mixture - Move slowly rich while cranking
31
Q

LOW RPM Light

A

Indicates rotor speed below 97% RPM

To restore RPM, immediately lower collective and roll throttle on and, in forward flight, apply aft cyclic.

Light is disabled when collective is full down

32
Q

Vortex Ring State Recovery (Traditional)

A
  1. Lower collective
  2. Right Pedal
  3. Fwd Cyclic

SN-22

33
Q

GOV OFF Light

A

Indicates engine RPM governor is switched off.

34
Q

Minimum Rate of Descent Configuration

A
  1. Airspeed approximately 55 KIAS
  2. Rotor RPM approximately 90%
  3. Minimum rate of descent is about 1,350 feet per minute

Glide ratio is about 4:1 or one nautical mile per 1,500 feet AGL

35
Q

Emergency Water Landing

Power ON

A
  1. Descend to hover above water
  2. Unlatch doors
  3. Passengers exit aircraft
  4. Fly to safe distance from passengers to avoid possible injury by rotors
  5. Switch battery and alternator OFF
  6. Roll throttle off into overtravel spring
  7. Keep aircraft level and apply full collective as aircraft contacts water
  8. Apply lateral cyclic to stop rotors
  9. Release seat belt and quickly clear aircraft when rotors stop
36
Q

Loss of Tail Rotor Thrust

Forward Flight

A

Failure is usually indicated by nose right yaw which cannot be corrected by applying left pedal

  1. Immediately enter autorotation
  2. Maintain at least 70 KIAS if practical
  3. Select landing site, roll throttle off into overtravel spring, and perform autorotation landing

NOTE

When a suitable landing site is not available, the vertical stabilizer may permit limited controlled flight at low power settings and airspeeds above 70 KIAS; however, prior to reducing airspeed, enter full autorotation

37
Q

Low RPM Recovery

A
  1. Roll on Throttle
  2. Lower Collective
  3. Aft Cyclic (in forward flight)
38
Q

T/R CHIP Light

A

Indicates metallic particles in tail rotor gearbox

NOTE

If light is accompanied by any indication of a problem such as noise, vibration, or temperature rise, land immediately.

If there is no other indication of a problem, land as soon as practical.

39
Q

M/R CHIP Light

A

Indicates metallic particles in main rotor gearbox

NOTE

If light is accompanied by any indication of a problem such as noise, vibration, or temperature rise, land immediately. If there is no other indication of a problem, land as soon as practical.

40
Q

Engine Fire (During Start on Ground)

A
  1. Cranking – Continue and attempt to start which would suck flames and excess fuel into engine
  2. If engine starts, run at 60-70% RPM for a short time
  3. Fuel mixture – OFF
  4. Fuel Valve – OFF
  5. Battery Switch – OFF
  6. If time permits, apply rotor brake to stop rotors
  7. Exit helicopter
41
Q

HYD Light

A

Indicates hydraulic system is switched off

42
Q

Land Immediately

A

Land on the nearest clear area where a safe normal landing can be performed. Be prepared to enter autorotation during approach, if required

Emergency Procedures (3 decks)

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