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56 Cards in this Set
- Front
- Back
- 3rd side (hint)
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BAT TEMP |
overtemp > 70 °
warning gong |
<b>On ground:
1. BAT MSTRN sw - Off</b> 2. Engines - Shutdown <b>In flight snigle pilot: 1.BAT MSTR sw - Off 2. Land ASAP</b> 3. Engine shutdown - Perform 4.Visual Inspection of battery - Perform if inspection ervelas no damage 5. Start-up procedure - Perform 6. BAT MSTR sw - Off continue VMC, BAD DISCON appears 7. Land ASAPracticable |
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BAT TEMP
|
- overtemp > 70°
- warning gong |
<b><color red>On ground:
1. BAT MSTRN sw - Off</color></b> 2. Engines - Shutdown <b><color red>In flight single pilot: 1.BAT MSTR sw - Off 2. Land ASAP</color></b> 3. Engine shutdown - Perform 4.Visual Inspection of battery - Perform <i>if inspection ervelas no damage</i> 5. Start-up procedure - Perform 6. BAT MSTR sw - Off <i>continue VMC, BAD DISCON appears</i> 7. Land ASAPracticable <b><color red>in flight dual pilot: 1.BAT MSTR sw - Off 2. Land ASAP</color></b> 3. pilot remaining on seat - "hands on" 4. Engines - leave running in idle 5. visual inspection of battery - Perform <i>continue VMC if no damage, BAT DISCON appears</i> 6. Land ASAPracticable |
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ENG 1 FAIL
ENG 2 FAIL |
respective N1 below 50%
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<b><color red>1. OEI flight condition - Establish
2. Affected engine - Identify 3. Single engine emergency shutdown - Perform</color></b> |
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FIRE
|
- overtemp in engine compartment
- warning bell |
<b><color red>On ground:
1. FIRE sw 8affect. engine) - Raise guard, press 2. Both FUEL PRIME PUMPS - Check Off 3. BOT 1 / BOT 2 2pb - Press; bottle 1 activated; EXT indicator comes on 4.clock stop watch - Start 5. Double engine emergency shutdown - Perform</color></b> 6. Passengers - Evacuate <i>if situation permits and FIRE warning still on after 1 minute</i> <b><color red>7. BOT 1 / BOT 2 pb - Press; bottle 2 activated; EXT indicator comes on In flight: 1. OEI flight condition - Establish 2. Airspeed - Reduce if exceeding 100 KIAS 3. FIRE sw (aff. engine) - Raise guard, press 4. BOT 1 / BOT 2 pb - Press; bottle 1 activated; EXT indicator comes on 5. Clock stop watch - Start 6. Affected Engine - Identify 7. Single Engine Emergency Shutdown - Perform</color></b> 8. Passengers - Evacuate <b><color red>9. Land ASAP</color></b> <i>if FIRE warning ist still on after 1 minute</i> <b><color red>10. BOT 1 / BOT 2 pb - Press; bottle 2 activated; EXT indicator comes on</color></b> <i>if FIRE remains on</i> <b><color red>11. Land Immediately</color></b> |
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LOW FUEL 1
LOW FUEL 2 |
- respective supply fuel tank quantity is below 24kg
- warning gong |
1. Fuel quantity - Check
<i>if positive fuel indication</i> 2. both fuel pump XFER sw - Check On 3. Both fuel pump XFER cb - Check in <i>if both FUEL LÖOW remain on</i> <b><color red>4. Land within 10 minutes</color></b> <i>if one LOW FUEL remains on</i> <b><color red>4. Expect single engine failure</color></b> |
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ROTOR RPM
|
NRO low:
- 95% or less - steady light, pitching tone NRO high: - 106% or more - flashing light, steady tone |
1. Rotor RPM indicator - Check
<b><color red>2. Collective lever - Adjust as necessary to maintain in limits</color></b> |
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XMSN OIL PRESS
|
- pressure below minimum 1 bar
- warning gong |
<i>if one oil pressure below 1 bar:</i>
<b><color red>1. Power - Reduce</color></b> 2. Land ASAPracticable <i>if both pressures below 1 bar</i> <b><color red>3. Land immediately</color></b> |
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BAT DISCH
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DC power supplied by battery
|
1. DC Volts, GEN AMPS, BAT AMPS - Check
2. Elactrical consumption - Reduce as much as possible 3. Land ASAPracticable |
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BAT DISCON
|
Battery is offline (normal during EI`PU start or when BATN MSTR in Off position)
|
1. BAT MSTR sw - Check in On position
<i> if BAT DISCON remains On</i> 2. Land ASAPracticable |
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BLEED AIR
|
Bleed Air shut off and mixing valve remains open after shutting off bleed air heating
|
1. BLD HTG rheostat - Turn on and lower again to off
<i>if BLEED AIR caution dissapears</i> 2. Continue flight <i>if BLEED AIR caution comes on again</i> 2. Engine performance may be degraded, Use caution |
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BUSTIE OPN
<b><color red> </color></b> |
electrical systems are separated (load sharing impossible)
|
1. Respective BUSTIE sw - reset
<i>if BUSTIE OPN caution comes on again</i> 2. Land ASAPracticable |
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CAD FAN
|
failure of CAD fan during CPDS test
|
do not start engines
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CAU DEGR
|
degraded cautions due to loss of CAD lane or both VEMD lanes
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CPDS OVHT
|
normal operating temperature of instrument pane exceeded
<b><color red>- max remianing operating time is approx. 30 min</color></b> |
1. INST COOL cb - Check in
2. PUSH FOR AIR knob - Push 3. VENTILATION COCKPIT rheostat - HI 4. VENTILATION CABIN sw - ON <i>if caution remians on</i> 5. Land ASAPracticable |
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DOORS
|
any doors open
|
1. Doors - Check latched
<i>if still on</i> 2. Land ASAPracticable |
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ENG CHIP
|
chips detcted in engine oil
|
<b><color red>On ground:
1. Affected Engine - Identify 2. Single engine emergency shutdown - Perform In flight: 1. OEI flight condition - Establish 2. Affected engine - Identify<b><color red> <i>1. Alternatice</i> <b><color red>3. Singke engine emergency shutdown - Perform</color></b> <i>2. Alternative</i> <b><color red>3. Twist Grip 8aff. engine) - rotate slowly to IDLE, check indications</color></b> 4. Land ASAPracticable |
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ENG O FILT
|
engine oil filter contaminated
|
1. Engine oil pressure and temp - Monitor
2. Land ASAPracticable |
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ENG OIL P
|
aff. eng oil pressure below minimum
|
1. Engine oil pressure - Check
<b><color red>2. OEI flight condition - Establish 3. Affected engine - Identify 4. single engine emergency shutdown - Perform</color></b> 5. Land ASAPracticable |
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ENG PA DIS
|
parameter discrepancy between ENG 1 and 2
<b><color red>- do not try to match needles - avoid using max power </color></b> |
1. Engine digital values - compare to verify
2. Land ASAPracticable |
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ENG SPLIT
|
N1 indications differ more than 10%
|
1. Collective lever - Adjust to OEI limits or below
2. Bleed air consumer - off 3. Engines condition - Analyse 4. Continue in accordance with ENGINE UNDERSPEED-GOVERNOR FAILURE, ENGINE OVERSPEED_GOVERNOR FAILURE or VAR NR cautions, whichever is applicable |
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EPU DOOR
|
EPU door open
|
<b>On ground:</b>
<i>after EPU starts</i> EPU access door - Close <b>In flight:</b> Land ASAPracticable |
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EXT POWER
<b><color red> </color></b> |
external power supplied
|
<i>after EPU starts</i>
1. EPU cable - disconnect 2. EPU access door - close, check indication going off |
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FIRE E TEST
|
fire extinguishing system has been tested
|
n/a
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FIRE EXT
|
respective bottle is not available
|
Land ASAPracticable
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FLI DEGR
|
Loss of one engine parameter
- numerical value of failed parameter disappears - parameter designation is yellow |
<b><color red>- if it was the first limit the next value becomes first limit
- do not try to match needles - avoid using max power</color></b> Land ASAPracticable |
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FLI FAIL
|
Loss of 2 out of 3 signals f same engine
- numerical value of failed disappears - parameter desigantion will be yellow - ΔN1 displayed - needle of respective engine disappears |
<b><color red>
- do not try to match needles - avoid using max power</color></b> Land ASAPracticable |
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F PUMP FWD
F PUMP AFT |
failure of FWD or AFT fuel pump or dry run
- FWD pump failure - unusable 11.1kg - AFT pump failure - unusable 45.04kg |
1. Fuel level in main tank - Check
2. FUEL PUMP XFER (F or A) sw - Check On 3. XFER PUMP cb - Check In <i>if F PUMP FWD/AFT remains on</i> 4. Affected FUEL PUMP XFER sw - Off <i>if there is no fuel in the main tank</i> 2. affected FUEL PUMP XFER sw - Off |
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F PUMP JET
|
aft main tank not capable of delivering fuel to fwd main tank
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F PUMP AFT sw - Check On
get 0° pitch to reduce unusable main tank fuel to minimum |
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F QTY DEGR
|
failure of one main tank sensor
|
set pitch between -3° and +8° prior reading available fuel qty
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F QTY FAIL
|
failure of fuel quantity indication system
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Land ASAPracticable
<b>LOW FUEL warning light is only remaining accurate indication</b> |
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FUEL FILT
|
filters contaminated
|
<i>one caution</i>
Land ASAPracticable <b>be prepared for single engine failure</b> <i>both cautions</i> <b><color red>Land ASAP </color> be prepared for double engine failure</b> |
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FUEL PRESS
<b><color red> </color></b> |
engine fuel pump inlet pressure is low
|
1. FUEL PRIME PUMP sw - On, prime pump caution comes on
<i>if FUEL PRESS goes off:</i> 2. Land ASAPracticable <i>if FUEL PRESS remains on:</i> 2. FUEL PRIME PUMP sw - Off 3. Land ASAPacticable <b>be prepared for single engine failure</b> |
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FUEL VALVE
|
in other position then commanded
|
Land ASAPracticable
<b>be prepared for single engine failure</b> |
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F VALVE CL
|
Fuel valve in closed position
-respective ACTIVE light will come on |
n/a
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GEN DISCON 1 <b>or</b> 2
|
- respective generator failed or disconnected
- both non-essential busses are disconnected |
<i>if BUS TIE caution is also on:</i>
1. Electrical fire/shotz circuit procedure - Perform <i>if Voltmeter is >30.5V:</i> 1. Generator overvoltage procedure - Perform <i>if BUS TIE caution off and voltage normal:</i> 1. Affected GEN sw - RESET then NORM <i>if GEN DISCON remains on:</i> 2. Affected GEN sw - Off 3. DC Volts, GEn Amps, BAT Amps - Monitor 4. Electrical consumers - Reduce as much as possible 5. Land ASAPracticable |
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GEN DISCON 1<b>and 2</b>
|
- both generator failed or disconnected
- only ESS BUS 1+2 available |
1. GEN 1 sw - RESET, then NORM
2. DC Volts and GEN Amps - Check 3. GEN 1 sw - Off 4. GEN 2 sw - RESET, then NORM 5. DC Volts and GEN Amps - Check 6. GEN 2 sw - Off <i>if voltmeter is >30.5V:</i> 7. Generator overvoltage procedure - Perform <i>if voltmeter normal</i> 8. Both GEN sw - RESET, then NORM <i>if one or both GEN DISCON remain on:</i> 9. Respective GEN sw - Off 10. Electrical consumers - reduce as much as possible 11. EMER SHED BUS sw - On if necessary 12. DC Volts and BAT Amps - Monitor 13. Land ASAPracticable <b>amount of unusable fuel increases if EMER SHED BUS not switched on</b> |
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GEN OVHT
|
temp of generator high
|
1. affected GEN sw - Off
<b>if GEN OVHT remains on an dit smells like fre shut down the respective engine</b> <i>if GEN OVHT remains on mor than 1 minute <b><color red>2.OEI flight condition - Establish 3. Affected engine - Identify 4. single engine emergency shutdown - Perform </color></b> 5. Land ASAPracticable |
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HTG OVTEMP
|
overtemp in the bleed air duct system
|
1. BLD HTG rheostat - Off
<i>if caution goes off:</i> 2. BLD HTG rheostat - turn on slowly <i>if caution on again:</i> 3. BLD HTG rheostat - Off |
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HOR BAT
|
stby horizon is supplied by the emergency battery pack
|
n/a
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HYD PRESS
|
<b>
- Do not operate test button in flight - avoid hovering in high GM, calm wind - in case of loss of SYS 2 yaw command servo boost will be lost</b> |
Land ASAPracticable
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INPUT FAIL
|
CPDS test has detected one or more failed caution indications
<b>- flashing caution failed and will not be available any more</b> |
do not start engines
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INVERTER
|
all AC power consumers lose power
|
Inverter sw - Off
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MM EXCEED
|
Mast Moment >77%
MM EXCEED caution remains until Pwr Off |
Land ASAPracticable
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OVSP FAIL
|
Loss of at least one N2 or N1 sensor signal in affected engine overspeed protection system
<b>Affected engine no loger protected against overspeed</b> |
Land ASAPracticable
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PITOT HTR
|
Piot tube and/or static port heater failed or not switched on
|
1. Respective cb and sw - Check
2. Indications - Compare with normal oper. system |
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PRUIME PUMP
|
prime pumps in operation
|
n/a
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P0 DIS
|
- discrepancy betweeen both P0 sensors
- VNE unvalid |
Land ASAPracticable
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SHED EMER
|
switched to EMER On
|
1. Electrical consumers - reduce as much as possible
2. Land ASAPracticable |
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STARTER
|
if On after reaching IDLe speed a switch or realy is blocked
|
<b>On ground:</b>
1. Respective ENG START sw - Check off<i>if ENG START sw is off:</i> 2. affected engine - Identify 3. Single emergency engine shutdown - Perform <b>In flight:</b> 1. Land ASAPracticable |
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TWIST GRIP
|
affected TWIST GRIP not in FLIGHT position
|
1. Affected TWIST GRIP - check FLIGHT position
<i>if caution remains on:</i> 2. Land ASAPracticable |
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T0 DIS
|
- FLI DEGR caution appears
- discrepancy between both T0 sensors detected - N1 calculations affected - OAT is invalid |
<b>On ground:</b>
<i>if caution remains on more than 2 minutes after start up:</i> Normal engine shutdown - Perform <b>In flight:</b> Land ASAPracticable |
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VEMD FAN
|
failure of VEMD Fan during CPDS test
|
do not start engines
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VAR NR
|
- selftest of VR NR monitor box failed
- NRO not within expected limits - TRQ spilt >15% - Pwr supply for VAR NR sys interrupted - failure of FCDM or ADC - failure of N2 trim motor system - failure of VEMD Lane 1 |
1. VAR NR system NORM/MAN sw - Push to select MAN mode
<i>if under CAT B:</i> 2. Rotorspeed - Trim manually to 101%. Below 55 KIAS and above 6500ft DA trim to 104% <i>if under CAT A:</i> 2. Rotorspeed . trim manually to 101%. Below 55 KIAS trim to 104% <i>all conditions:</i> 3. Torque - Synchronize 4. Continue Flight <i>if Rotorspeed trimming <b>not</b> successfull: 3. Airspeed - Reduce IAS to VNE - 25 kts or below 4. Torque - Synchronize 5. Continue Flight <i>- with low NRO careful collective inputs - with lower NRO teh HOGE performance is reduced by 120 kg up to 10.000 ft DA - with low NRO avoid right crosswind landings</i> |
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XMSN CHIP
|
chips in the main transmission
|
1. XMSN oil pressure - check in normal range
2. Land ASAPracticable |
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XMSN OIL T
|
transmission oil temperature above maximum
|
<b>1. XMSN oil temperature an oil pressure indication - Check</b>
<i>if in limits</i> 2. Land ASAPracticable <i>if above limits</i> <b>2. Power - Redusce, as much as possible</b> <i>if oil temp remains above limit</i> <b>3. Land ASAP</b> |
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ENG CHP CT
ENG OF CT F FLT CT XMSN CHP CT XMSN OT CT |
failure of the respective CPDS caution during external test
|
do not start engines
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