UH-60 EMERGENCY PROCEDURES TRAINING & EVALUATION PROGRAM UNITED STATES ARMY
The purpose of this program is to train you in recognizing and correctly responding to a given emergency situation. Each situation is timed and you must give the correct answer within 30 seconds. The next slide will reveal the correct response.
WHAT IS THE DEFINITION OF: LAND AS SOON AS POSSIBLE
Landing at the nearest suitable landing area (e. g Landing at the nearest suitable landing area (e.g., open field) without delay. (The primary consideration is to ensure the survival of occupants)
WHAT IS THE DEFINITION OF: LAND AS SOON AS PRACTICABLE
Landing at a suitable landing area Landing at a suitable landing area. (The primary consideration is the urgency of the emergency)
WHAT IS THE DEFINITION OF: AUTOROTATE
Adjusting the flight controls as necessary to establish an autorotational descent and landing.
WHAT IS THE DEFINITION OF: EMERG ENG SHUTDOWN What is the caution?
1. ENG POWER CONT lever(s) - OFF 2. ENG FUEL selector - OFF 3 1. ENG POWER CONT lever(s) - OFF 2. ENG FUEL selector - OFF 3. FUEL BOOST PUMP CONTROL switch(es) - OFF CAUTION If TGT rises above 538 degrees C after shutdown, place AIR SOURCE HEAT/START switch as required, turn ENGINE IGNITION switch OFF, and press starter to motor engine for 30 seconds or until TGT decreases below 538 degrees C.
WHAT IS THE CAUTION FOR ECU LOCKOUT?
CAUTION When engine is controlled with ENG POWER CONT lever in LOCKOUT, engine response is much faster and TGT limiting system is inoperative. Care must be taken not to exceed TGT limits and keeping % RPM R and % RPM 1 and 2 in operating range.
WHAT IS THE DEFINITION OF: EMER APU START
1. FUEL PUMP switch - APU BOOST. 2. APU CONTR switch - ON.
HOW DO YOU USE THE COCKPIT DOOR AS AN EMERGENCY EXIT? WHAT IS THE WARNING FOR EMERGENCY EXITS?
To release door, the jettison handle is pulled to the rear; the door may then be jettisoned by kicking the lower forward corner. WARNING For helicopters without a roll-trim actuator, the cyclic shall be held at all times with the rotor turning. In cases where emergency exit is required prior to rotor coasting to a stop, make sure that the cyclic stick is centered until the last crewmember can depart the cockpit. Since the main rotor shaft has a 3 degree forward tilt, an exit to the right rear or left rear will provide the greatest rotor clearance safety.
Emergency equipment consists of what items?
1. ONE CRASH AXE 2. TWO FIRE EXTINGUISHERS 3. THREE FIRST AID KITS
WHAT IS THE GENERAL WARNING FOR ENGINE MALFUNCTION?
WARNING Prior to movement of either power-control lever, it is imperative that the malfunctioning engine and the corresponding power-control lever be identified. If the decision is made to shut down an engine, take at least five full seconds while retarding the ENG POWER CONT lever from FLY to IDLE, monitoring engine torque, Ng, TGT, Np and ENG OUT warning light on.
WHAT ARE THE WARNINGS FOR THIS SITUATION? #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM % RPM % TRQ #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP TEST RTR OVERSPEED 00 90 CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE 1 2 R 1 2 #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER 130 120 110 105 100 95 90 70 30 0 130 120 110 105 100 95 90 70 30 0 140 120 100 80 60 40 20 0 140 120 100 80 60 40 20 0 #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS WHAT ARE THE WARNINGS FOR THIS SITUATION? TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT 1 2 CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH 1 2 R CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 400 690 45 96 TOTAL FUEL TGT Ng 1-CHAN-2
SINGLE - ENGINE FAILURE 1. Collective - Adjust to maintain RPM R 2. External cargo/stores - Jettison (if required) If continued flight is not possible: 3. Land as soon as possible. If continued flight is possible: 4. Establish single-engine airspeed. 5. Land as soon as practicable. WARNING When the power available during single engine operation is marginal or less, consideration should be given to jettisoning the external stores. The engine anti-ice and cabin heater switches should be turned off as necessary to ensure maximum power is available on the remaining engine. WARNING Do not respond to engine-out audio and warning light until checking TGT and % RPM R.
MASTER CAUTION PRESS TO RESET WHAT IS THE WARNING FOR THIS SITUATION? #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM % RPM % TRQ #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP TEST RTR OVERSPEED 00 00 CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE 1 2 R 1 2 #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER 130 120 110 105 100 95 90 70 30 0 130 120 110 105 100 95 90 70 30 0 140 120 100 80 60 40 20 0 140 120 100 80 60 40 20 0 #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO WHAT IS THE WARNING FOR THIS SITUATION? MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT 1 2 CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH 1 2 R CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 450 310 15 35 TOTAL FUEL TGT Ng 1-CHAN-2
DUAL - ENGINE FAILURE AUTOROTATE WARNING Do not respond to engine-out audio and warning light until checking TGT and % RPM R. AUTOROTATE
MASTER CAUTION PRESS TO RESET WHAT IS THE CAUTION FOR THIS SITUATION? #1 ENG OUT #2 ENG OUT FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM % RPM % TRQ TEST RTR OVERSPEED 30 106 1 2 R 1 2 130 120 110 105 100 95 90 70 30 0 130 120 110 105 100 95 90 70 30 0 140 120 100 80 60 40 20 0 140 120 100 80 60 40 20 0 WHAT IS THE CAUTION FOR THIS SITUATION? 1 2 1 2 R FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED C X 10 PSI X 10 C X 100 % X 10 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 3 2 1 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 560 845 87 100 TOTAL FUEL TGT Ng 1-CHAN-2
DECREASING % RPMR CAUTION 1. Collective - Adjust to control RPMR. 2. ENG POWER CONT lever - LOCKOUT low power/TGT engine. Maintain TRQ approximately 10% below other engine. 3. Land as soon as practicable. CAUTION When engine is controlled with engine power-control lever lockout, engine response is much faster and the TGT limiting system is inoperative. Care must be taken not to exceed TGT limits and keeping % RPMR and % RPM 1 and 2 in operating range.
MASTER CAUTION PRESS TO RESET #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM % RPM % TRQ #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP TEST RTR OVERSPEED 45 80 CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE 1 2 R 1 2 #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER 130 120 110 105 100 95 90 70 30 0 130 120 110 105 100 95 90 70 30 0 140 120 100 80 60 40 20 0 140 120 100 80 60 40 20 0 #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT 1 2 CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH 1 2 R CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 605 702 90 96 TOTAL FUEL TGT Ng 1-CHAN-2
INCREASING % RPMR 1. ENG POWER CONT lever - Retard high power/TGT engine, maintain TRQ approximately 10% below other engine. 2. Land as soon as practicable. If effected engine does not respond to ENG POWER CONT lever movement in the range between FLY and IDLE the HMU may be malfunctioning internally. If this occurs: 3. Establish single engine airspeed. 4. Perform EMERG ENG SHUTDOWN. (affected engine) 5. Refer to single engine failure emergency procedure
MASTER CAUTION PRESS TO RESET #1 ENG OUT #2 ENG OUT FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM % RPM % TRQ TEST RTR OVERSPEED 92 80 1 2 R 1 2 130 120 110 105 100 95 90 70 30 0 130 120 110 105 100 95 90 70 30 0 140 120 100 80 60 40 20 0 140 120 100 80 60 40 20 0 1 2 1 2 R FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED C X 10 PSI X 10 C X 100 % X 10 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 3 2 1 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 820 700 101 94 TOTAL FUEL TGT Ng 1-CHAN-2
% TRQ SPLIT BETWEEN ENGINES 1 AND 2 1. If TGT of one engine exceeds limiter, retard ENG POWER CONT lever on that engine to reduce TGT. Retard the ENG POWER CONT lever to maintain torque of the manually controlled engine at approximately 10% below other engine. 2. If TGT limit on either engine is not exceeded, slowly retard ENG POWER CONT lever on high %TRQ engine and observe % TRQ of lower power engine. 3. If % TRQ or low power engine increases, ENG POWER CONT lever on high power engine - Retard and maintain 10% below other engine. (High side failure) 4. If % TRQ of low power engine does not increase, or % RPM R decreases, ENG POWER CONT lever - Return to FLY (Low side failure). 5. If additional power is required, low power ENG POWER CONT lever, momentarily move to LOCKOUT and adjust to set % TRQ approximately 10% below other engine. 6. Land as soon as practicable.
MASTER CAUTION PRESS TO RESET #1 ENG OUT #2 ENG OUT FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM % RPM % TRQ TEST RTR OVERSPEED 70 68 1 2 R 1 2 INDICATIONS: 1. Bang or Popping sound 2. Rapid increase in TGT 3. Fluctuations in Ng, Np, and TRQ 130 120 110 105 100 95 90 70 30 0 130 120 110 105 100 95 90 70 30 0 140 120 100 80 60 40 20 0 140 120 100 80 60 40 20 0 1 2 1 2 R FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED C X 10 PSI X 10 C X 100 % X 10 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 3 2 1 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 820 700 101 94 TOTAL FUEL TGT Ng 1-CHAN-2
COMPRESSOR STALL 1. Collective - Reduce. IF CONDITION PERSISTS: 2. ENG POWER CONT lever (affected engine) - Retard. (TGT should decrease) 3. ENG POWER CONT lever (affected engine) - FLY IF STALL CONDITION RECURS: 4. EMERG ENG SHUTDOWN (affected engine) 5. Refer to single-engine failure emergency procedure.
MASTER CAUTION PRESS TO RESET #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 605 640 93 94 TOTAL FUEL TGT Ng 1-CHAN-2
1. ENG POWER CONT lever - Retard to reduce torque on affected engine. If oil pressure is below minimum limits or if oil temperature remains above maximum limits 2. EMER ENG SHUTDOWN (affected engine) 3. Refer to single-engine failure emergency procedure
MASTER CAUTION PRESS TO RESET #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 605 640 93 94 TOTAL FUEL TGT Ng 1-CHAN-2
1. ENG POWER CONT lever - Retard to reduce torque on affected engine. If oil pressure is below minimum limits or if oil temperature remains above maximum limits 2. EMER ENG SHUTDOWN (affected engine) 3. Refer to single-engine failure emergency procedure
MASTER CAUTION PRESS TO RESET YOU ARE IN FLIGHT AT THIS TIME #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH YOU ARE IN FLIGHT AT THIS TIME MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 605 640 93 94 TOTAL FUEL TGT Ng 1-CHAN-2
1. ENG POWER CONT lever - Retard to reduce torque on affected engine. If oil pressure is below minimum limits or if oil temperature remains above maximum limits 2. EMER ENG SHUTDOWN (affected engine) 3. Refer to single-engine failure emergency procedure
MASTER CAUTION PRESS TO RESET #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 605 640 93 94 TOTAL FUEL TGT Ng 1-CHAN-2
1. ENG POWER CONT lever - Retard to reduce torque on affected engine. If oil pressure is below minimum limits or if oil temperature remains above maximum limits 2. EMER ENG SHUTDOWN (affected engine) 3. Refer to single-engine failure emergency procedure
MASTER CAUTION PRESS TO RESET #1 FUEL LOW #1 GEN #2 GEN #2 FUEL LOW #1 ENG OUT #2 ENG OUT #1 FUEL PRESS #1 GEN BRG #2 GEN BRG #2 FUEL PRESS #1 ENGINE OIL PRESS #1 CONV #2 CONV #2 ENGINE OIL PRESS FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM #1 ENGINE OIL TEMP AC ESS BUS OFF DC ESS BUS OFF #2 ENGINE OIL TEMP CHIP #1 ENGINE BATT LOW CHARGE BATTERY FAULT CHIP #2 ENGINE #1 FUEL FLTR BYPASS GUST LOCK PITCH BIAS FAIL #2 FUEL FLTR BYPASS #1 ENGINE STARTER #1 OIL FLTR BYPASS #2 OIL FLTR BYPASS #2 ENGINE STARTER #1 PRI SERVO PRESS #1 HYD PUMP #2 HYD PUMP #2 PRI SERVO PRESS TAIL ROTOR QUADRANT IRCM INOP AUX FUEL #1 TAIL RTR SERVO MAIN XMSN OIL TEMP INT XMSN OIL TEMP TAIL XMSN OIL TEMP APU OIL TEMP HI BOOST SERVO OFF STABILATOR SAS OFF TRIM FAIL LFT PITOT HEAT FLT PATH STAB IFF RT PITOT HEAT CHIP IMPUT MDL - LH CHIP INT XMSN CHIP TAIL XMSN CHIP IMPUT MDL - RH CHIP ACCESS MDL - LH CHIP MAIN MDL SUMP APU FAIL CHIP ACCESS MDL - RH MR DE-ICE FAIL MR DE-ICE FAULT TR DE-ICE FAIL ICE DETECTED MAIN XMSN OIL PRESS #1 RSVR LOW #2 RSVR LOW BACK-UP RSVR LOW FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED % X 10 #1 ENG ANTI-ICE ON #1 ENG INLET ANTI-ICE ON #2 ENG INLET ANTI-ICE ON #2 ENG ANTI-ICE ON C X 10 PSI X 10 C X 100 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 APU ON APU GEN ON PRIME BOOST PUMP ON BACK-UP PUMP ON 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 APU ACCUM LOW SEARCH LT ON LDG LT ON #2 TAIL RTR SERVO ON CARGO HOOK OPEN BRT/ DIM TEST HOOK ARMED PARKING BRAKE ON EXT PWR CONNECTED 3 2 1 FAILURE ADVISORY R E S E T POWER ON RESET CPTR SAS 2 TRIM RGYR ACCL CLTV A/S GYRO 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 605 640 93 94 TOTAL FUEL TGT Ng 1-CHAN-2
1. ENG POWER CONT lever - Retard to reduce torque on affected engine. If oil pressure is below minimum limits or if oil temperature remains above maximum limits 2. EMER ENG SHUTDOWN (affected engine) 3. Refer to single-engine failure emergency procedure
MASTER CAUTION PRESS TO RESET #1 ENG OUT #2 ENG OUT FIRE MASTER CAUTION PRESS TO RESET LOW ROTOR RPM % RPM % TRQ TEST RTR OVERSPEED 00 95 1 2 R 1 2 130 120 110 105 100 95 90 70 30 0 130 120 110 105 100 95 90 70 30 0 140 120 100 80 60 40 20 0 140 120 100 80 60 40 20 0 1 2 1 2 R FUEL XMSN ENG OIL TGT Ng QTY LBS X 100 TEMP PRESS C X 10 TEMP PSI X 10 PRESS TEMP SPEED C X 10 PSI X 10 C X 100 % X 10 19 11 7 6 5 4 3 0 18 14 12 10 8 4 0 -4 13 11 9 8 7 6 5 4 11 10 9 8 7 4 0 16 12 10 8 6 4 0 -4 9 8 7 6 5 4 2 0 14 12 10 8 6 4 2 0 3 2 1 1 2 1 2 1 2 1 2 1 2 DIM 2200 PUSH TO TEST ON OFF DIGITS 502 720 85 94 TOTAL FUEL TGT Ng 1-CHAN-2
ENGINE HIGH-SPEED SHAFT FAILURE 1. Collective - Adjust 2. EMERG ENG SHUTDOWN (affected engine). Do not attempt to restart. 3. Refer to single-engine emergency procedure.