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49 Cards in this Set
- Front
- Back
- 3rd side (hint)
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Warning Light Indications 🔲 ENG 1 or ENG 2 FAIL FAIL |
1. Establish OEM flight condition 🚁 2. Identify/Shutdown Affected Engine 3. LASA Practicable 🛬 |
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Warning Light Indications 🔲 FIRE or FIRE (Engine 1) (Engine 2) ➡️ ON GROUND |
1. Affected Engine FIRE sw - PRESS 🔳. (*affected engine will shut down - ACTIVE light🚦& BOT 1 light🚦& F VALVE CL 💡CAD) 2. Both Fuel Prime Pumps - check OFF 🎚. 3. BOT 1 / BOT 2 bp - PRESS 🔳. 🔛 BOT 1 activated - EXT 💡 comes on 🔛 (will discharge when N1 < 50%. When discharge is complete.. BOT 1🚦 & EXT🚦 lights go off - BOT 2 pb🚦comes on) 4. Clock - START ⏱ 5. Both Engines - SHUT DOWN ➡️ If 🔲 FIRE is still on after 1 minute — 6. BOT 1 / BOT 2 pb - PRESS 🔛 BOT 2 activated - EXT 💡 comes on 🔛 7. BATT MSTR sw - OFF 🎚 |
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Warning Light Indications 🔲 FIRE or FIRE (Engine 1) (Engine 2) ➡️ IN FLIGHT
(Conditions / Indications ⤴️ “hint”) |
1. Establish OEI Flight Condition 2. Airspeed < 100 KTS 3. AFFECTED Engine FIRE sw - PRESS 🔳. (*affected engine will shut down - ACTIVE light🚦& BOT 1 light🚦& F VALVE CL💡CAD) 4. Both Fuel Prime Pumps - check OFF 🎚. 5. BOT 1 / BOT 2 bp - PRESS 🔳. 🔛 BOT 1 activated - EXT 💡 comes on 🔛 (will discharge when N1 < 50% - when discharge is complete.. BOT 1🚦 & EXT🚦 lights go off & BOT 2 pb🚦comes ON) 6. Clock - START ⏱ 7. AFFECTED Engine - I.D. and SHUT DOWN 8. Land ASAP ➡️ If 🔲 FIRE is still on after 1 minute — 9. BOT 1 / BOT 2 pb - PRESS 🔛 BOT 2 activated - EXT 💡 comes on 🔛 ➡️ If 🔲 FIRE remains ON — 10. Land IMMEDIATELY |
Conditions / Indications ⤵️
❓ Overtemp in engine compartment
👀/👂 warning bell activated |
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Warning Light Indications 🔲 ROTOR RPM (Conditions / Indications ⤴️ “hint”) |
NRO LOW / NRO HIGH 1. Check rotor RPM 👀 2. Collective ➡️ Adjust to keep NRO in limits |
Conditions / Indications ⤵️ NRO LOW ⤵️ ❓NRO < 95% 👀 steady light 👂low pitch beeping NRO HIGH ⤵️ NRO > 106% 👀 Flashing light 👂gong NRO > 110% +👂steady high pitch tone |
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AVION OVHT (CAD)
(Conditions / Indications ⤴️ “hints”) |
⏳ The max remaining operating time is approx 30 min! 1. INST COOL cb ➡️ check IN 🔘 2. LASA Practicable 🛬 3. Maintain airspeed for air cooling 🌬 |
Conditions / Indications ⤵️ ❓ Normal operating temp of COM/NAV, FCDS, or AFCS exceeded |
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BAT DISCH (CAD)
(Conditions / Indications ⤴️ “hints”) |
1. DC VOLTS, GEN AMPS, and BAT AMPS ➡️ Check 👀 If generators are functioning normal ⤵️ 2. BAT MSTR sw ➡️ OFF 🎚 3. LASA Practicable 🛬 If generators not functioning ⤵️ 2. Reduce electrical consumption to save battery power 🪫 3. LASA Practicable 🛬 |
Conditions / Indications ⤵️ ❓DC power is supplied by battery ❓Short circuit on battery bus or line |
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BAT DISCON (CAD)
(Conditions / Indications ⤴️ “hints”) |
1. BAT MSTR sw ➡️ check ON 🎚 2. LASA Practicable 🛬 |
Conditions / Indications ⤵️ ❓Batt is off-line (Normal during EPU start or when BAT MSTR sw is OFF |
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BLEED AIR (CAD) (Conditions / Indications ⤴️ “hints”) |
1. BLD HTG rheostat ➡️ turn ON then OFF 2. Engine performance may be degraded |
Conditions / Indications ⤵️ ❓ Bleed air valves remain open after shutting off bleed air heating |
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➡️ In Flight BUSTIE OPN BUSTIE OPN (system 1) (system 2)
Condition in ⤴️ “hints” |
If GEN AMPS > 200 A ⤵️ 1. GEN sw (AFFECTED gen) ➡️ OFF 2. LASA Practicable If GEN AMPS normal (0-200 A) ⤵️ 1. LASA Practicable |
Condition ⤵️ ❓Electrical systems are separated (load sharing impossible) ❓If both BUSTIE OPN are on, the battery will not be charged |
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CAD FAN (CAD) |
🛑 don’t start engines |
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“CPDS OVHT”
(Conditions in ⤴️ “hints”) |
⏳ Max remaining time is approx 30 min 1. INST COOL cb ➡️ check IN 🔘 2. PUSH FOR AIR knob ➡️ PUSH 💨 3. VENT COCKPIT rheostat ➡️ HI 🎛 4. VENT CABIN sw ➡️ ON 🎚 5. LASA Practicable 🛬 |
Condition ⤵️ ❓Temp of instrument panel exceeded |
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ENG CHIP or ENG CHIP (system 1) (system 2)
⬆️ In Flight / ⬇️ On Ground |
1. ESTABLISH OEI Flight Condition 2. AFFECTED Engine ➡️ roll to IDLE Maintain the option to use affected engine for landing. If affected engine parameters fluctuate or are exceeded - perform single engine emergency shutdown 3. LASA Practicable
On Ground ⬇️ 1. Shut down the AFFECTED Engine |
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ENG O FILT or ENG O FILT (system 1) (system 2) |
📝 During engine start the ENG O FILT light may come on for up to 2 min 1. Engine oil press & temp ➡️ MONITOR 👀 2. LASA Practicable 🛬 |
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ENG OIL P or ENG OIL P (system 1) (system 2) |
1. Establish OEI Flight Condition 🚁 2. Shut down AFFECTED engine 🚫 3. LASA Practicable 🛬 |
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ENG PA DIS or ENG PA DIS (system 1) (system 2) Condition in ⤴️ “hints” |
🚧 Don’t try to match needles 🚧 Avoid using max power 1. Check Engine DIGITAL values 2. LASA Practicable |
❓Discrepancy between ENG 1 and ENG 2 is shown in yellow on FLI page |
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ENG PA DIS or ENG PA DIS (system 1) (system 2)
Condition / Indication in ⤴️ “hints” |
🚧 Don’t try to match needles 🚧 Avoid using max power 1. Check Engine DIGITAL values 2. LASA Practicable |
❓Discrepancy between ENG 1 and ENG 2 👀 Discrepancy shows in yellow on FLI page |
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ENG SPLIT and ENG SPLIT (system 1) (system 2)
Condition in ⤴️ “hint” |
1. Adjust power < OEI limits 2. Bleed Air consumers ➡️ OFF 3. Perform EP for Engine Overspeed/Underspeed Gov Failures or VAR NR |
Condition ⤵️ ❓N1 indicators show difference of 10% or more |
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FIRE EXT and/or FIRE EXT (system 1) (system 2)
Condition in ⤴️ “hint” |
LASA Practicable 🛬 |
Condition ⤵️ ❓Indicates that the respective fire extinguishing bottle is not available |
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FLI FAIL or FLI FAIL (system 1) (system 2)
Condition / Indication in ⤴️ “hint” |
🚧 don’t try to trim engines 🚧 avoid using max power 1. Use the FLI needle of the normal engine for limit indication, while comparing remaining digital parameter values 2. LASA Practicable 🛬 |
Condition / Indication ⤵️ ❓ loss of 2 out of 3 signals (TQ, N1, TOT) of the same engine 👀 numerical values of the failed parameters disappears 👀 the needle of the respective engine disappears |
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F PUMP FWD or F PUMP AFT
Condition in ⤴️ “hint” |
*If there is FUEL in the MAIN tank ⤵️ —1. FUEL PUMP XFER sw ➡️ check ON 🎚 —2. XFER PUMP cb ➡️ check IN 🔘 —3. Affected F PUMP XFER sw ➡️ OFF🎚 *If there is NO FUEL in the MAIN tank ⤵️ —1. Affected F PUMP XFER sw ➡️ OFF🎚 📝 In a fuel xfer pump failure - the main tank unusable fuel increases: ~ FWD pump failure ➡️ max 11 kg ~ AFT pump failure ➡️ max 45 kg |
Condition ⤵️ ❓Failure of fwd or aft transfer pump - or dry run |
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“ F PUMP JET ”
Condition in ⤴️ “hint” |
1. F PUMP AFT sw ➡️ check ON 👀 🧊 Main tank unusable fuel increases to: — In hover ➡️ 19.8 kg — At 0 pitch° attitude ➡️ 3.3 kg 📝 The F PUMP JET 💡light may come on shortly during hover flight with main tank fuel at approx 30 kg |
Condition ⤵️ ❓Aft (“main”) tank JET PUMP is not delivering fuel to fwd main tank |
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“ F QTY DEGR “
Condition in ⤴️ “hint” |
1. Set pitch attitude 🚁 between -3° and +8° before reading the approx available fuel quantity⛽️, then calculate remaining fuel ⏳ |
Condition ⤵️ ❓Failure of 1 main tank sensor ❓💡 represents the min fuel level within -3° and +8° pitch attitudes |
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“ F QTY FAIL “
Condition in ⤴️ “hint” |
👀/👂 Accurate fuel quantity is only provided by the LOW FUEL 💡 along with the gong 👂 1. LASA Practicable |
Condition ⤵️ ❓The fuel quantity system has failed. Do not calculate fuel amount using the normal fuel quantity indication |
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FUEL FILT and/or FUEL FILT (system 1) (system 2) |
If 1 caution light 💡 ⤵️ 1. be prepared for single engine failure 2. LASA Practicable 🛬 If BOTH caution lights 💡💡 ⤵️ 1. be prepared for double engine failure 2. LAND ASAP |
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FUEL PRESS or FUEL PRESS (system 1) (system 2) |
1. FUEL PRIME PUMP sw for AFFECTED Engine ➡️ ON🎚 (🔛 PRIME PUMP 💡 comes on 🔛) A. If 💡 goes OFF ~ 2. LASA Practicable 🛬 B. If 💡 remains ON ~ 2. FUEL PRIME PUMP sw ➡️ OFF🎚 3. LASA Practicable 🛬 |
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FUEL VALVE or FUEL VALVE (system 1) (system 2) |
LASA Practicable 🛬 |
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GEN DISCON or GEN DISCON (system 1) (system 2)
Condition in ⤴️ “hint” |
1. Volts/ Amps ➡️ CHECK 👀 If V < 28.2 or V > 28.8 / A < 0 or A > 200 ⤵️ 2. Both BUSTIE sw ➡️ OFF 🎚 If V > 30.5 then ⤵️ 3. Both GEN sw’s ➡️ OFF 4. Perform Generator Failure Isolation EP
(Finish this card……)
……. |
Condition ⤵️ ❓Generator has failed or is disconnected ❓Both non-essential buses are disconnected |
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GEN DISCON and GEN DISCON (system 1) (system 2)
Condition in ⤴️ “hint” |
(Finish this card……) |
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HYD PRESS or HYD PRESS (system 1) (system 2)
Condition / Indication in ⤴️ “hint” |
🚧 Don’t operate HYD TEST sw in flight 1. LASA Practicable |
Condition / Indication ⤵️ ❓/ 👀 With “system 2” failure - electrical yaw actuator is lost. YAW SAS💡 and/or ACTUATOR💡 may also illuminate |
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VAR NR
Conditions / Indications in ⤴️ “hint” |
1. VAR NR - NORM/MAN sw ➡️ MAN 🔳 2. NRO ➡️ trim to 104% < 55 kts or 101% > 55 kts (4-way beep sw on collective) ~ If NRO trimming was not successful ⤵️ 3. Reduce airspeed ➡️ < Vne -25 kts 4. TQ ➡️ sync 5. Continue Flight 🚁
📝 with lower rotor speed, HOGE is reduced by 120 kg up to 10k DA 📝 with lower rotor speed, avoid landings with right crosswinds |
Conditions / Indications ⤵️ 👀 “VAR NR” 💡 is normal on the ground 👀 “VAR NR” 💡 may come on during rapid power or airspeed changes ❓ rotor speed is not within expected limits ❓ TQ split > 15% (yellow MAN 🔳 appears) ❓ Failure of any number of systems |
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XMSN CHIP |
1. XSMN oil pressure ➡️ CHECK 👀 2. Power ➡️ reduce as much as possible 3. LASA Practicable 🛬 |
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XMSN OIL T |
1. XMSN oil T and P ➡️ CHECK 👀 ~ If indications are within limits ⤵️ 2. LASA Practicable 🛬 ~ If indications are above limits ⤵️ 2. Reduce Power ~ If temp 🌡 remains high ⤵️ 3. LAND ASAP 🛬 |
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Any “CT” 💡on CAD before start |
Do not start engines |
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Single Engine Failure ➡️ in HOVER
Indications in ⤴️ “hint” |
1. Cushion Landing 🚁
2. I.D. & Shutdown AFFECTED Engine (after landing)
📝 VAR NR system will revert to “MAN” mode automatically |
Indications ⤵️ 👀 Slight jerk yaw LEFT 👀/👂 All engine failure 💡‘s and 🔈’s |
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Single Engine Failure ➡️ HOGE
Indication in ⤴️ “hint” |
1. Rotor rpm ➡️ Adjust Collective 2. Airspeed ➡️ Increase if Possible 👉🏽 FORCED LANDING 👈🏽 (3.) Cushion Landing with Collective (4.) I.D. & Shutdown the AFFECTED Engine (after landing) 👉🏽 TRANSITION TO OEI FLIGHT 👈🏽 3. Adjust Collective to < OEI Limits 4. Rotor Speed ➡️ Trim to Max 🕥 5. Airspeed > 65 kts (Vy) 6. Maintain OEI Limits ➡️ MCP or less 7. I.D. & Shutdown AFFECTED Engine 8. LASA Practicable 🛬 📝 VAR NR system will revert to “MAN” mode automatically |
Indication ⤵️ 👀 Slight jerk yaw LEFT 👀/👂 All other associated 💡’s and 🔈’s |
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SINGLE ENGINE FAILURE ➡️ on TAKEOFF 👉🏽 Transition to OEI Flight 👈🏽 |
1. Collective ➡️ Maintain Rotor RPM 2. Adjust Collective ➡️ OEI Limits or less 3. Rotor Speed ➡️ Trim to Max 🕥 4. Airspeed > 65 kts (Vy) 5. Reduce Collective ➡️ OEI MCP or less 6. I.D. & Shutdown AFFECTED Engine 7. LASA Practicable |
Indications ⤵️ 👀 slight jerk yaw to the LEFT |
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Single Engine Landing ➡️ PROCEDURE |
1. Rotor Speed ➡️ Max 2. Bleed Air Heating ➡️ OFF 3. Airspeed ➡️ 65 kts (Vy) 4. Shallow Approach 5. Touchdown ➡️ Min Airspeed 📝 Touch down with as minimal airspeed as able without exceeding OEI power limits |
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Single Engine Emergency Shutdown ➡️ PROCEDURE
BLD HTG EMER/NORM ⤴️ “hint” |
1. Determine if current power situation will allow for OEI flight 2. Ensure ➡️ AFFECTED engine/controls 3. Adjust collective for OEI limits 4. Twist Grip ➡️ slowly to IDLE, check indications, then to OFF 5. Rotor Speed ➡️ Trim to Max |
Bleed air heating will be shut down automatically with OEI, however depending on power margin of the remaining engine, it may be re-engaged by ⤵️ 1. BLD HTG EMER/NORM sw ➡️ EMER 🎚 2. BLD HTG rheostat ➡️ ON ⚫️ |
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Driveshaft Failure / Engine Overspeed |
1. Establish OEI flight condition 2. I.D. and Shutdown AFFECTED Engine 3. LASA Practicable 🛬 |
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Engine Overspeed ➡️ Governor Failure
Conditions / Indications in ⤴️ “hint” |
1. Raise Collective ➡️ Determine whether it’s an Overspeed or Underspeed on the Triple Tach 2. Check VAR NR sw ➡️ MAN mode 🔳 3. N2 Trim sw ➡️ Match TQ / Increase NRO 4. Twist Throttle of AFFECTED Engine ➡️ roll down until FLI needles (1 & 2) match 5. LASA Practicable 🛬 6. Treat all power changes similar to a “FADEC FAILURE” adjusting throttle with power changes to match FLI needles |
Conditions / Indications ⤵️ 👀 NRO & N2 Increase 👀 AFFECTED ENGINE ➡️ TQ, N1, TOT Increase 👀 NORMAL ENGINE ➡️ TQ, TOT may decrease 💡’s ➡️ ROTOR RPM, VAR NR, ENG SPLIT |
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Engine Underspeed ➡️ Governor Failure
Conditions / Indications in ⤴️ “hint” |
Mxkd |
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Engine Underspeed ➡️ Governor Failure
Conditions / Indications in ⤴️ “hint” |
Mxkd |
Conditions / Indications ⤵️ 👀 NRO & N2 Decrease 👀 AFFECTED ENGINE ➡️ TQ, N1, TOT Decrease 👀 NORMAL ENGINE ➡️ NRO and N2 may decrease 💡’s ➡️ ROTOR RPM, VAR NR, ENG SPLIT |
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Engine Underspeed ➡️ Governor Failure
Conditions / Indications in ⤴️ “hint” |
1. Raise Collective ➡️ Determine whether it’s an Overspeed or Underspeed on the Triple Tach 🎛 2. Establish OEI Flight condition 3. Bleed Air 🥵 consumers ➡️ OFF 4. Check VAR NR sw ➡️ MAN mode 🔳 3. N2 TRIM sw ➡️ Match TQ / Increase NRO 4. Twist Throttle of AFFECTED Engine ➡️ roll down until FLI needles (1 & 2) match 5. LASA Practicable 🛬 6. Treat all power changes similar to a “FADEC FAILURE” adjusting throttle with power changes to match FLI needles 7. If no residual TQ on affected engine is available ➡️ shutdown AFFECTED Engine |
Conditions / Indications ⤵️ 👀 NRO & N2 Decrease 👀 AFFECTED ENGINE ➡️ TQ, N1, TOT Decrease 👀 NORMAL ENGINE ➡️ NRO and N2 may decrease 💡’s ➡️ ROTOR RPM, VAR NR, ENG SPLIT |
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Compressor Stall 💥
Conditions / Indications in ⤴️ “hint” |
1. Collective ➡️ Lower 2. Gauges 🎛 ➡️ Monitor 👀 3. Collective ➡️ Raise Slowly 4. If compressor stall💥 returns ➡️ I.D. (TOT) and Shutdown AFFECTED Engine 5. LASA Practicable 🛬 |
Conditions / Indications ⤵️ 👂🏼 popping sounds 👀 TQ & N1 may decrease 👀 TOT may increase 👀 yaw jerks |
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Droop Compensation Failure
Conditions / Indications in ⤴️ “hint” |
1. Maintain NRO 🕥 within limits with Collective.. avoid large power changes 2. LASA Practicable 🛬 |
Conditions / Indications ⤵️ 👀 NRO & N2 decrease when collective is raised 👀 NRO & N2 increase when collective is lowered |
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Engine Oil Temp High 🌡 |
1. Establish OEI Flight condition 2. I.D. AFFECTED Engine Twist Grip ➡️ Adjust to 20%-30% TQ 3. Affected Engine Oil T ➡️ Monitor 👀 ~ If Oil Temp remains above limit 👇🏽 4. AFFECTED Engine ➡️ Shutdown 5. LASA Practicable 🛬 |
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Autorotation Airspeeds 🚁 👉🏽 Recommended Auto kts 👉🏽 Min Rate of Decent kts 👉🏽 Max Range kts 👉🏽 Vne kts |
👉🏽 Recommended Auto ➡️ 75 kts 👉🏽 Min Rate of Decent ➡️ 60 kts 👉🏽 Max Range ➡️ 90 kts 👉🏽 Auto Vne ➡️ 90 kts |
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Cabin Fire 🔥💨
Indications in ⤴️ “hint” |
1. Airspeed ➡️ 65 kts recommended 2. Heating 🥵 / AC 🥶 ➡️ OFF 3. Extinguish Fire 🧯 4. Open doors, windows & vents 5. Land ASAP 🛬 6. Double Engine Shutdown |
Indications ⤵️ 👀 Smoke 💨 Burning Smell 🔥 |
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Electrical Fire (short circuit) |
1. Open windows & vents 2. If smoke source is identified, remove power to that source via sw or cb 3. Both BUS TIE sw’s ➡️ OFF 4. Both GEN 1 & GEN 2 sw’s ➡️ OFF 5. Electrical Consumers ➡️ Reduce 6. Follow “flow chart EP” for landing 🛬 |
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