BUSTIE OPN
- GEN AMPS. - Verify normal value
Normal value: - LAND ASA PRACTICABLE
if one GEN AMPS value shows XXX
- Failed system. - GEN sw OFF
- LAND ASA PRACTICABLE
if both GEN AMPS show XXX
2. Double GEN DISCON procedure
30min on battery
BAT DISCON
- BAT MSTR sw. - Reset, then ON
If caution remain ON - LAND ASA PRACTICABLE
CAD DEGR
- Failure of CAD lane
Or - Failure of both VEMD lanes
CAD FAN
Do not start
CPDS OVHT
- Pull for heating/defog knob. - Push
- Pull for AIR knob. - Pull
- VENT SYST rheostat - Turn to MAX
if caution remain ON
4. land within 30 min
DEGRADE
system I and/or II
Caution:
- Avoid using Max pwr and perform pwr variation slowly
- Maintain TQ>20% on each engine
- In case of eng main sw failure for shutdown, use twist grip
- Engine parameter. - Monitor ( compare with normal engine)
- LAND ASA PRACTICABLE
After landing
- Normal eng shutdown
- CAD (SYS 1/2). - Check for FADEC FAIL
ENG CHIP
” ON GROUND”
“1. Eng ident”
“2. Single eng emer shutdown”
“ON FLIGHT”
“1. OEI flight condition”
2. ENG CHIP sw. - BURN 1”
3. Chip pulse event record
If ENG CHIP remain ON
“4. Eng ident”
Alternative 1: “Single eng emer shutdown”
Alternative 2: “ ENG main sw. - IDLE”. If needed for landing
6. LASA PRACTICABLE
If ENG CHIP extinguish a second activation will be authorised
ENG CHP CT
ENG CHIP CAUTION IS NOT AVAILABLE
ENG FAIL
1 “ OEI flight conditions”
2 “ affected eng Ident”
3 “ Single eng emer shutdown perform”
4 LASA PRACTICABLE
ENG O FILT
1- eng Oil t&p Monitor
2- LASA PRACTICABLE
ENG OF CT
Eng O Filt caution is not available
Do not start
FIRE EXT
Fire extinguishing system is active
FADEC FAIL
1-“Collective lever Adjust to maintain NRo within normal range”
2-“Affected eng Ident by small chge”
3-“Respective TWIST GRIP Adjust slowly to set
80% (+-2%) N1 on the affected eng
Simultaneously adjust collective to maintain
eng within limits.
(When the OAT is below –10_C, adjust N1 to 77% ($ 2%) instead of 80%.)
AND AVOID QUICK TWIST GRIP ROTATIONS. HOLD MIN. 10% TORQUE ON THE NORMAL ENGINE TO MAINTAIN AUTOMATIC CONTROL OF VARIABLE NRO IN ACCORDANCE WITH SECTION 7, FLM EC 135 T2 (CPDS).
FLI DEGR
1- do not try to match the needles when different parameters are designated as first limit
Avoid using max Pwr. Use the needle of the other engine for limit indication
2-LASA PRACTICABLE
FLI FAIL
- Do not try to trim engines
2. LASA PRACTICABLE
F PUMP AFT and FWD
- Fuel qty. check
- FUEL PUMP XFER-A and XFER-F sw+ cb. Check on
Remaining flight 30min Vy / 20min at max range
F PUMP AFT
1- Fuel level main tank Chck
Qty ok
2- FUEL PUMP XFER-A sw ON
3- XFER-A pump cb Chck in
If remain on
4- FUEL PUMP XFER-A sw OFF
QTY LOW
2- FUEL PUMP XFER-A sw OFF
in hover condition the unusable fuel can be up to 71 kg
Qty unusable can be reduce to 7.5 kg when flying with 80 kias or more
F PUMP FWD
1- Fuel level main tank Chck
Qty ok
2- FUEL PUMP XFER-F sw ON
3- XFER-F pump cb Chck in
If remain on
4- FUEL PUMP XFER-F sw OFF
QTY LOW
2- FUEL PUMP XFER-F sw OFF
in forward flight condition the unusable fuel can be up to 59 kg
Qty unusable can be reduce to 3.6 kg when flying with 80 kIAS or less
F QTY DEGR
The degraded fuel qty indication represent the minimum fuel level within pitch attitude range -3 +6
Set pitch between 0 +/-1 before reding fuel qty, the calculate remaining flight endurance
F QTY FAIL
The fuel qty has failed
DO NOT calculate flight endurance according the fuel qty indication
Fuel qty information only by LOW FUEL warning
LASA PRACTICABLE
FUEL
1- fuel qty chck
If fuel in the main
2- FUEL PULP XFER-A-F Chck on
If 0 in the main
2- FUEL PULP XFER-A-F Chck oFF
3- LASA PRACTICABLE
FUEL FILT
“One caution”
LASA PRACTICABLE
“Both caution”
“LASAP”
FUEL PRESS
1- FUEL PRIME PUMP sw ON
2- LASA PRACTICABLE
be prepared for eng failure
FUEL VALVE
LASA PRACTICABLE
