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MD500 D Model > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

1
Q

Audible & visual warnings are provided for what?

A

Engine out
Low rotor

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2
Q

List the 10 caution & warning lights in order

A
  1. Engine out
  2. Transmission oil pressure
  3. Transmission oil temp
  4. Generator out
  5. Engine chips
  6. Main rotor transmission
  7. Tail rotor transmission
  8. Fuel low
  9. Fuel filter
  10. Press to test
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3
Q

Emergency Procedures
Complete Power Loss
Indicators

A

Red “Engine Out” warning light & audible warning
Left yaw
Drop in engine speed
Drop in rotor speed
Change in noise level

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4
Q

Emergency Procedures
Complete Power Loss
Conditions

A

Occurs when N¹ falls below 55%
Or
Nr falls below 468 RRPM

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5
Q

Emergency Procedures
Complete Power Loss
Procedures

A
  • Adjust collective to maintain rotor speed 410–523 rpm.
  • Apply pedal pressure as necessary to control yaw.
  • Adjust cyclic control as necessary to control airspeed. Airspeed below 131kts
  • After confirming complete loss of power, time & altitude permitting, place twistgrip in cutoff & close fuel shutoff valve.
  • Select landing area & maneuver as required.
  • If operating at reduced RRPM to extend glide or reduce RoD, restore RRPM by lowering collective prior to flare.
  • Flare as required for the terrain to reduce forward speed.
  • Touch down level attitude, increasing collective to cushion landing.
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6
Q

Emergency Procedures
Partial Power Loss
Indications

A

Under partial power conditions, the engine may operate smoothly with reduced power,
or
It may operate erratically with
intermittent surges of power.

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7
Q

Emergency Procedures
Partial Power Loss
Procedures

A
  • Turning the start pump ON may smooth out an erratic operating engine
    and/or restore power.
    Do NOT disregard the need to land.
  • If possible, fly at reduced power to the nearest safe landing area and land
    as soon as possible. Be prepared for a complete power loss at any time.
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8
Q

Emergency Procedures
Air Restart - Engine
Information

A

Because the exact cause of engine failure cannot be determined in flight, the decision to attempt a restart will depend on aircraft altitude, time available, rate of descent, and potential landing areas.
Do not attempt restart if a malfunction is suspected.

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9
Q

Emergency Procedures
Air Restart - Engine
Low Altitude / Time Critical Procedures

A
  • Close twist grip to cutoff position.
  • Press start/ignition button immediately.

Pressing the starter button actuates the igniter. If N1 is 18 percent or above, open twist grip immediately to ground idle. N1 speeds of 25 to 40 percent are preferred for coolest and fastest restarts.

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10
Q

Emergency Procedures
Air Restart - Engine
When altitude & Time Permit Procedures

A
  • Perform normal engine start if N1 has decayed below 18 percent. Refer to Section IV, Engine Starting.
  • Recommended airspeed is 60 knots IAS.
  • Advance twistgrip from ground idle to full open once N1 reaches 60 - 65%.
  • Collective pitch: increase as required once N2/NR are 103%
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11
Q

Emergency Procedures
Low Rotor Speed
Indications

A

Rotor below 468rpm

Red “Engine Out” warning light & audible warning.
Drop in rotor speed
Change in noise level

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12
Q

Emergency Procedures
Low Rotor Speed
Conditions

A

Engine Failure.
Transient rotor droop during large, rapid increases in power.
Governor failure producing an underspeed.

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13
Q

Emergency Procedures
Low Rotor Speed
Procedures

A
  • Respond immediately to the low rotor RPM warning by adjusting collective to maintain rotor RPM within limits.
  • Check other Caution/Warning indicators and engine instruments to confirm engine trouble and respond in accordance with appropriate procedures in this section.
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14
Q

Emergency Procedures
Water Landing - Power off
Procedures

A
  • Adjust collective pitch as necessary to establish autorotation.
  • If time permits, open doors and push door handle full down to prevent relatching.
  • Make autorotative approach, flaring as required to minimize forward speed at touchdown.
  • Level aircraft and apply full collective pitch as contact is made with the water.
  • When aircraft begins to roll, lower collective to full down to minimize blades skipping off the water.
  • Release safety harness and clear the aircraft as soon as the rotor blades have stopped turning.
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15
Q

Emergency Procedures
Water Landing - Power on
Procedures

A
  • Descend to hovering altitude over water.
  • Open doors and push door handle full down to prevent relatching.
  • Passengers and copilot exit aircraft.
  • Fly a safe distance away from all personnel in the water to avoid injury.
  • Close twistgrip to the cutoff position and perform a hovering autorotation.
  • Allow aircraft to settle in a level attitude while applying full collective pitch.
  • When aircraft begins to roll, reduce collective to full down to minimize blades skipping off the water.
  • Release safety harness and exit the aircraft as soon as the blades have stopped turning.
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16
Q

Emergency Procedures
Inflight Fire - Cabin Smoke Elimination
Procedures

A
  • Cabin heat (if source of smoke is the cabin heat duct) — OFF
  • Fresh air vent — OPEN
  • Pilot/Cabin door vents — OPEN AND FACING AFT

If necessary, open pilots’ door below 130kts

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17
Q

Emergency Procedures
Engine Fire on the Ground
Fire during startup Procedures

A
  • Twistgrip — CUTOFF
  • Starter — MOTOR UNTIL TOT IS BELOW 150°C
  • Fuel shut-off valve — PULL TO CLOSE
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18
Q

Emergency Procedures
Engine Fire on the Ground
Engine Compartment Fire Procedures

A
  • Twistgrip — CUTOFF
  • Fuel shutoff valve — PULL TO CLOSE
  • BATTERY/EXT PWR switch OFF
  • Passengers/crew — EVACUATE

If time and situation permit:
- Rotor brake (if installed) — APPLY
- Secure area — HAVE PASSENGERS MOVE A SAFE DISTANCE FROM THE AIRCRAFT
- Fire extinguisher — USE AS APPROPRIATE

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19
Q

Emergency Procedures
Engine Fire During Flight
Low Altitude Procedures

A
  • Land immediately — POWER ON APPROACH AND LANDING WITHOUT DELAY
  • Twistgrip — CUTOFF AS SOON AS HELICOPTER IS ON GROUND
  • Fuel shutoff valve — PULL TO CLOSE
  • BATTERY/EXT PWR — switch OFF
  • Passengers/crew — EVACUATE
20
Q

Emergency Procedures
Engine Fire During Flight
High Altitude Procedures

A

Circumstances may influence whether pilot is to execute power on or power off descent. If power OFF descent is chosen;

  • Collective — DOWN TO ESTABLISH AUTOROTATION TO SELECTED AREA
  • Twistgrip — CUTOFF
  • Fuel shutoff valve — PULL TO CLOSE
    Radio — ‘‘MAYDAY’’ CALL
  • Execute autorotational landing — MAINTAIN CONTROL
  • BATTERY/EXT PWR — switch OFF
    Passengers/crew — EVACUATE
21
Q

Emergency Procedures
Cabin Fire On Ground
Procedures

A
  • Twistgrip — CUTOFF
  • BATTERY/EXT PWR – switch OFF
  • Passengers/crew — EVACUATE

If time & situation permit:
- Rotor brake (if installed) — APPLY
- Secure area —- HAVE PASSENGERS MOVE A SAFE DISTANCE FROM THE AIRCRAFT
- Fire extinguisher — USE AS APPROPRIATE

22
Q

Emergency Procedures
Cabin Fire In Flight
Procedures

A
  • Land immediately — POWER ON APPROACH AND LANDING WITHOUT DELAY
  • Air vents — VENTILATE CABIN AS NECESSARY
  • Twistgrip — CUTOFF AS SOON AS HELICOPTER IS ON GROUND
  • BATTERY/EXT PWR — switch OFF
  • Passengers/crew — EVACUATE

If unable to land immediately & fire source can be identified:
- Malfunctioning system — OFF
- Fire extinguisher — USE AS NECESSARY
- Cabin — VENTILATE
- Land — AS SOON AS POSSIBLE

If fire source is unknown:
- Cabin heat — OFF
- Generator — OFF
- All electrical circuits (not required for safety of flight) — OFF
- Cabin — VENTILATE
- Land — AS SOON AS POSSIBLE

23
Q

Emergency Procedures
Fuel Control or Power Turbine Governor Failure
Indications

A

Failure is indicated by an instrument needle fluctuation.
A rise or drop of:
- N1
- N2/NR
- TOT
- Torque

24
Q

Emergency Procedures
Fuel Control or Power Turbine Governor Failure
Overspeed Indications

A

Engine torque, TOT, N1 and N2/NR, suddenly increasing.
Possible right yaw

25
Q

Emergency Procedures
Fuel Control or Power Turbine Governor Failure
Overspeed Procedures

A
  • Increase collective to load the main rotor, simultaneously rolling the twistgrip toward the ground idle position until control of N2 speed is obtained.
  • Manually control N2 speed (102-103%) with the pilots twistgrip.
  • If operating RPM cannot be controlled, close twistgrip to CUTOFF and make an autorotational landing.
26
Q

Emergency Procedures
Fuel Control or Power Turbine Governor Failure
Underspeed Indications

A
  • N2/NR decaying.
  • Possible left yaw.
  • Possible low rotor warning indication.
27
Q

Emergency Procedures
Fuel Control or Power Turbine Governor Failure
Underspeed Procedures

A
  • Lower collective to maintain rotor RPM in the green (410-523) and attempt level flight at 60 knots IAS.
  • If power is insufficient for level flight or a power-on decent, make an autorotational landing.
28
Q

Emergency Procedures
Fuel Control or Power Turbine Governor Failure
Turbine Governor Surge Indications

A

N2 fluctuating: governor not maintaining pre-set speed (102-103%N2)

29
Q

Emergency Procedures
Fuel Control or Power Turbine Governor Failure
Turbine Governor Surge Procedures

A
  • Turning the start pump ON may allow the engine to operate smoothly. If operation of the engine returns to normal, it may be possible to fly to a favorable landing area, however do not disregard the need to land.
  • Beep N2 to maximum.
  • Control N2 manually with twistgrip (102% to 103% N2).

NOTE: This action takes the governor out of the system allowing the pilot manual control of the N2 and should eliminate the surge.

30
Q

Emergency Procedures
Engine Chip Detector
Indications, Conditions & Procedures

A

I - Yellow “ENGINE CHIPS” light ON
C - Metal contamination of oil
P - Land ASAP

31
Q

Emergency Procedures
Low Engine Oil Pressure In-Flight
Indications & Procedures

A

I - Oil pressure decreasing below normal operating range.
P - Land ASAP

32
Q

Emergency Procedures
Engine Torque
Indications & Procedures

A

I - Loss of engine torque indication
P - Land ASAP

33
Q

Emergency Procedures
Main Rotor Transmission Oil Pressure
Indications, Conditions & Procedures

A

I - Red “XMSN OIL PRESS” light ON
C - Transmission oil pressure low
P - Land ASAP

34
Q

Emergency Procedures
Main Rotor Transmission Oil Temperature
Indications, Conditions & Procedures

A

I - Red “XMSN OIL TEMP” light ON
C - Transmission oil temp exceeds max limit
P - Land ASAP

35
Q

Emergency Procedures
Main Rotor Transmission Chip Detector
Indications, Conditions & Procedures

A

I - Yellow “M/R XMSN CHIPS” light ON
C - Metal contamination of oil
P - Land ASAP

36
Q

Emergency Procedures
Tail Rotor Transmission Chip Detector
Indications, Conditions & Procedures

A

I - Yellow “T/R XMSN CHIPS” light ON
C - Metal contamination of oil
P - Land ASAP

37
Q

What is One way lock failure?

A

The one way lock assembly is a self contained hydraulic unit that prevents aft feedback forces in the longitudinal cyclic control system.

38
Q

Emergency Procedures
One Way Lock Failure
Indications & Procedures

A

I - Aft feedback in the cyclic at high airspeed and/or during pull ups from high airspeed or higher than normal forces required to move the cyclic longitudinally.

P - Reduce airspeed to 100 KIAS or less.
- Limit cyclic movement to those movements required to safely fly the helicopter. Abnormal or extreme control inputs are not necessary.

39
Q

Emergency Procedures
Inoperative Trim
Conditions & Procedures

A

C - The trim motor fails to respond to application of the cyclic trim switch in
one or more directions

P - Establish a safe flight condition that produces the least cyclic control force. Normally straight and level at the last trimmed airspeed.
- Actuate the trim switch thru all positions in an attempt to restore trim capability and determine the extent of trim failure. If restored, trim to a near neutral position and land as soon as practical avoiding further trimming.
- If trim failure is determined to be in all directions, and control of the helicopter can be maintained safely, check/reset TRIM circuit breaker.
- Land as soon as practical if unable to reestablish full cyclic trim control with the pilot’s cyclic.

40
Q

Emergency Procedures
Runaway Trim
Indications & Procedures

A

I - An uncommanded longitudinal or lateral cyclic trim actuation. The cyclic may move to a full travel position or some intermediate position resulting in cyclic forces up to the maximum. Uncommanded movement can occur after cyclic trim switch actuation or as a result of an electrical short.

P - Establish a safe flight condition that produces the least cyclic control force.
- Utilize left hand and legs, as necessary, to apply pressure against the cyclic stick to relieve the right hand loads and conserve strength for landing. Use collective friction to prevent unwanted collective movement and associated power change.
- Actuate the trim switch thru all positions, several times if necessary, as this will generally re-establish trimming capability. When restored, trim to a near neutral position and land as soon as practical avoiding further trimming.
- If trim runaway is to the full forward position, accomplish landing into
the wind and do not hover downwind in winds in excess of 15 knots

41
Q

Ways to reduce forward & aft cyclic forces during a runaway trim.

A

Forward runaway - Maintain higher airspeeds
Aft runaway - Maintain slower airspeeds

42
Q

Emergency Procedures
Fuel Filter
Indications, Conditions & Procedures

A

I - Yellow “FUEL FILTER” light ON
C - A predetermined pressure differential across the filter has been reached & an impending bypass condition exists.
P - Turn on start pump.
- Continue flight
- Service the fuel filter prior to the next flight
If any unusual engine indications or conditions occur, land as soon as possible.

43
Q

Emergency Procedures
Fuel Low
Indications & Procedures

A

I - Yellow “FUEL LEVEL LOW” light on at 35 Ilbs of fuel
P - Avoid large steady side slip angles and uncoordinated maneuvers.
- Land ASAP

44
Q

Emergency Procedures
Battery Overtemperature
Red Indication
Conditions & Procedures

A

I - Red 160F light ON
C - Battery overtemp at 160F or above
P - Battery switch — OFF.
- Land as soon as possible

No further flights allowed until battery inspected.

45
Q

Emergency Procedures
Battery Overtemperature
Yellow Indication
Conditions & Procedures

A

I - Yellow 140F light ON
C - Battery overtemp at 140F
P - Battery switch — OFF.
- Battery must remain offline during remainder of flight

No further flights allowed until battery inspected.

46
Q

Emergency Procedures
Generator Malfunction
Indications, Conditions & Procedures

A

I - Yellow “GEN OUT” light ON
C - Generator is not powering electrical bus
P - Check generator (GEN) circuit breaker IN.
- Turn the generator switch OFF, then ON to reset.
- If GEN OUT indicator remains ON or comes back ON, pull generator circuit breaker OUT and insure generator switch is in the ON position for the remainder of the flight.
- If GEN OUT indicator remains ON, reduce electrical load to a minimum.
- Land as soon as practical.

NOTE: The generator switch must be in the ON position to enable the Engine Out/Low
Rotor audio warning to function as required.

47
Q

Emergency Procedures
Engine Air Particle Separator Filter Clogged
Indications, Conditions & Procedures

A

I - Yellow “FILTER CLOGGED” light ON
C - A predetermined pressure differential has been reached across the engine
air inlet.
P - FILTER BYPASS control handle — OPEN
- SCAV AIR — OFF
Service particle separator prior to next flight

MD500 D Model (5 decks)

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