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26 Cards in this Set
- Front
- Back
ENG chip light |
LASP |
|
Fuel low light |
Approx 50-75lbs remaining LAS Practicable |
|
Transmission Chip light |
LASP |
|
Tail rotor Chip light |
LASP |
|
Fuel Filter light |
LAS Practicable |
|
GEN Fail light |
Verify failure on load meter CK GEN Fuel CB - In CK GEN Reset CB - In GEN switch Reset - GEN *power not restored GEM - OFF LAS Practicable |
|
Engine out light |
ENG out (audio) Verify N1 <55% +-3 Verify N2 decreasing Accomplish engine out EP *if possible attempt restart |
|
Battery Hot light |
Deactivated LASP |
|
Engine fire in flight |
Autorotate Throttle - closed Fuel valve - OFF *time permitting: fuel boost CBs OUT Accomplish autorotate on BATT - OFF Do not restart engine |
|
Rotor Low RPM (light) |
Rotor RPM <90% Reduce Collective 90-107% Ensure throttle full open * if unable to maintain Nr, autorotate |
|
Transmission oil temp (light) |
XMSN oil temp =>100° (red line) Reduce power Verify with Guage LASP |
|
Transmission oil PSI |
XMSN oil PSI <30 PSI Reduce power Verify with Guage LASP |
|
Engine fire during start |
Throttle - closed Starter - continue to motor Fuel valve switch - OFF BATT - OFF Rotor break - Engage Exit helicopter |
|
Rt or Lft fuel pump (light) |
Descend below 6000 PA LAS Practicable |
|
SPARE LIGHT |
LASP |
|
Engine failure at a hover |
Autorotate Eng shutdown |
|
Ennis failure in flight |
Autorotate *attempt start if altitude permits Throttle - closed Fuel valve - OFF engine shutdown after landing |
|
Minimum rate of decent |
52 KIAS |
|
Minimum glade distance airspeed |
69 KIAS |
|
Nominal autorotate air speed |
61 KIAS |
|
Engine overspeed |
Throttle - retard to stabilize N1 or N2/Nr TOT - monitor Nr - maintain 90-107% with throttle |
|
Engine compressor stall |
Collective - reduce TOT and N1 - check normal indications Engine anti-ice - ON Heater - ON *continued flight possible Collective - increase slowly TOT and N1 - monitor LAS Practicable *continued flight not possible Autorotate Throttle - closed Fuel valve - OFF shutdown after landing |
|
Drive shaft failure |
Left yaw Rapid decrease Nr Rapid increase N2 Rotor Low audio Rotor Low RPM light Noise increase *autorotate |
|
Hydraulic failure |
Airspeed - reduce 60-80 KIAS HYDR SYS CB - Out *if hydraulics not restored HYDR SYS CB - In LAS Practicable Run on landing at approx 9 KIAS |
|
Flight control malfunction |
Attitude - maintain Hydraulics - OFF Airspeed - 60-80 KIAS LASP (HYD OFF landing) |
|
Excessive electrical load |
*DC load meter reads high * smoke or fumes GEN - OFF BATT - OFF LEFT fuel boost CB - In LAS Practicable |