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100 Cards in this Set
- Front
- Back
#1 PUMP/RSVR LOW/BKP ON
|
*1. SERVO SWITCH - 1ST OFF
*2. LAND AS SOON AS PRACTICABLE IF [#1 PUMP/1+B/U RSVR LOW] *3. LAND AS SOON AS POSSIBLE IF [#2 PRI SERVO] AND [HYD] WARNING APPEAR *4. LAND IMMEDIATELY |
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#1 PUMP/1+B/U RSVR LOW
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*1. LAND AS SOON AS POSSIBLE
IF THE [#2 PRI SERVO] AND [HYD] WARNING APPEAR *2. LAND IMMEDIATELY |
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#2 PUMP/RSVR LOW/BKUP ON
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*1. SERVO SWITCH - 2ND OFF
*2. LAND AS SOON AS PRACTICABLE IF [#2 PUMP/2+B/U RSVR LOW] *3. LAND AS SOON AS POSSIBLE IF [#1 PRI SERVO] AND [HYD] WARNING APPEAR *4. LAND IMMEDIATELY |
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#2 PUMP/2+B/U RSVR LOW
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*1. LAND AS SOON AS POSSIBLE
IF THE [#1 PRI SERVO] CAUTION AND [HYD] WARNING APPEAR *2. LAND IMMEDIATELY |
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[HYD]
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*1. LAND IMMEDIATELY
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[#1 HYD PUMP]
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*1. EXECUTE #1 HYDRAULIC PUMP FAILURE EP
IF NO OTHER HYD MALFUNCTIONS ARE PRESENT: 1. LAND AS SOON AS PRACTICABLE IF A BACKUP HYDRAULIC PUMP FAILURE OCCURS: 2. LOSS OF TAIL ROTOR CONTROL EMERGENCY-PERFORM 3. LAND AS SOON AS POSSIBLE |
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LOSS OF TAIL ROTOR CONTROL
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*1. COLLECTIVE/AIRSPEED-
ADJUST AS REQ TO CTRL YAW 2. TAIL SERVO-BKUP 3. BACKUP HYD PUMP-ON 4. EXT CARGO/FUEL/STORES-JETT/DUMP, AS REQ 5. APU EMERGENCY START-PERFORM 6. LAND AS SOON AS PRACTICABLE |
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2 HYD PUMP
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*1. EXECUTE #2 HYD PUMP FAILURE E.P.
IF NO OTHER HYDRAULIC MALFUNCTIONS ARE PRESENT: 1. LAND AS SOON AS PRACTICABLE IF A BACKUP HYDRAULIC PUMP FAILURE OCCURS: 2. MINIMIZE FLIGHT CONTROL MOVEMENTS 3. LAND AS SOON AS POSSIBLE |
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[#1 + #2 HYD PUMP FAIL]
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*1. RESTRICT CONTROL MOVEMENT
*2. LAND AS SOON AS POSSIBLE |
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WHAT CONDITIONS CAUSE AUTOMATIC BACKUP PUMP OPERATIONS
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[#1 PUMP]
[#2 PUMP] [#1 RSVR LOW] [#1 TAIL ROTOR SERVO] |
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IMMEDIATE LANDING/DITCHING
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*1. CREW AND PASSENGERS-ALERT
*2. SHOULDER HARNESS-LOCKED *3. EXTERNAL CARGO/STORES/FUEL-JETTISON/DUMP AS REQUIRED *4. SEARCHLIGHT-AS REQUIRED *5. MAYDAY/IFF-TRANSMIT/EMERG {START APU} IN THE FLARE: *6. WINDOWS-JETTISON, AS REQUIRED{WARNING: RESET HANDLE} *7. PCLs-OFF *8. ROTOR BRAKE-ON *9. ARMOR WINGS/CO-PILOT COLLECTIVE-STOW{WARNING: STOW ARMOR WINGS OVER WATER} *10. EGRESS |
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APU EMERGENCY START
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*1. ECS-OFF
*2. AIR SOURCE/ECS START SWITCH-APU *3. FUEL PUMP SWITCH-APU BOOST *4. APU CONTROL SWITCH-ON *5. APU GENERATOR-CHECK ON |
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ABORT START PROCEDURE
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*1. PCL-OFF
*2. IGNITOR SWITCH-OFF *3. STARTER-ENGAGE *4. STARTER DISENGAGE (AFTER 30SEC. AND TGT BELOW 540°) |
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ENGINE AIR RESTART
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{IF FAILURE WAS CATASTROPHIC, RESTART COULD CAUSE A FIRE}
*1. APU EMERGENCY START-AS REQUIRED *2. #1AND#2 FUEL BOOST PUSHBUTTONS-ON *3. ENGINE IGNITION SWITCH-ON *4. FUEL SEL LEVERS-DIR OR XFD {90% Ng OR HIGHER FOR X-BLEED START} *5. PCL-OFF *6. STARTER-ENGAGE *7. PCL-IDLE(TGT<80° IF TIME PERMITS) *8. PCL-FLY AFTER STARTER DROPOUT |
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STABILATOR FIXED 40° TRAILING EDGE DOWN: MAX AIRSPEED
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45 KTS.
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STABILATOR FIXED 30° TRAILING EDGE DOWN: MAX AIRSPEED
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60 KTS
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STABILATOR FIXED 20° TRAILING EDGE DOWN: MAX AIRSPEED
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80 KTS
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STABILATOR FIXED 10° TRAILING EDGE DOWN: MAX AIRSPEED
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100 KTS
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STABILATOR FIXED 0° TRAILING EDGE DOWN: MAX AIRSPEED
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150 KTS
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LOSS OF TAIL ROTOR DRIVE
(ALTITUDE AND AIRSPEED INSUFFICIENT TO AUTO) |
*1. COLLECTIVE-LOWER
*2. EXTERNAL CARGO AND STORES-JETTISON, AS REQUIRED {CAUTION: ALTITUDE MAY HAVE TO BE ADJUSTED BASED ON RATE OF TURN AND YAW} *3. PCLS-OFF WHEN DIRECTED(20-30 FT AGL) |
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LOSS OF TAIL ROTOR DRIVE
(ALTITUDE AND AIRSPEED SUFFICIENT TO ESTABLISH AUTOROTATION) |
*1. AUTOROTATION-ESTABLISH
*2. DRIVE FAILURE-ATTEMPT TO VERIFY *3. IMMEDIATE DITCHING/LANDING EP-PERFORM *4. PCLS-OFF WHEN DIRECTED (PRIOR TO FLARE) |
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[MAIN XMSN CHIP]
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*1. EXECUTE MAIN XMSN MALFUNCTION EP
IF SECONDARIES PRESENT: *1. LAND AS SOON AS POSSIBLE {80FT/80KTS} *2. APU EMERGENCY START PROCEDURE-PERFORM *3. #1 AND #2 GENERATORS-OFF, AS REQUIRED IF FAILURE IS IMMENINT: *4. LAND IMMEDIATELY IF THERE ARE NO SECONDARIES: *5. LAND AS SOON AS PRACTICABLE |
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[MAIN XMSN OIL HOT]
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*1. EXECUTE MAIN XMSN MALFUNCTION EP
IF SECONDARIES PRESENT: *1. LAND AS SOON AS POSSIBLE {80FT/80KTS} *2. APU EMERGENCY START PROCEDURE-PERFORM *3. #1 AND #2 GENERATORS-OFF, AS REQUIRED IF FAILURE IS IMMENINT: *4. LAND IMMEDIATELY IF THERE ARE NO SECONDARIES: *5. LAND AS SOON AS PRACTICABLE |
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[MAIN XMSN PRESS HI]
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*1. EXECUTE MAIN XMSN MALFUNCTION EP
IF SECONDARIES PRESENT: *1. LAND AS SOON AS POSSIBLE {80FT/80KTS} *2. APU EMERGENCY START PROCEDURE-PERFORM *3. #1 AND #2 GENERATORS-OFF, AS REQUIRED IF FAILURE IS IMMENINT: *4. LAND IMMEDIATELY IF THERE ARE NO SECONDARIES: *5. LAND AS SOON AS PRACTICABLE |
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[MAIN XMSN PRESS LOW]
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*1. EXECUTE MAIN XMSN MALFUNCTION EP
IF SECONDARIES PRESENT: *1. LAND AS SOON AS POSSIBLE {80FT/80KTS} *2. APU EMERGENCY START PROCEDURE-PERFORM *3. #1 AND #2 GENERATORS-OFF, AS REQUIRED IF FAILURE IS IMMENINT: *4. LAND IMMEDIATELY IF THERE ARE NO SECONDARIES: *5. LAND AS SOON AS PRACTICABLE |
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[TAIL XMSN CHIP]
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*1. TAIL OR INT XMSN MALFUNCTION EP
*1. LAND AS SOON AS POSSIBLE {TRANSIT SO YOU CAN ENTER AN AUTO IF NECESSARY, GET OUT DITCHING CHKLIST} IF FAILURE IS IMMENINT: *2. LAND IMMEDIATELY |
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[TAIL XMSN OIL HOT]
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*1. TAIL OR INT XMSN MALFUNCTION EP
*1. LAND AS SOON AS POSSIBLE {TRANSIT SO YOU CAN ENTER AN AUTO IF NECESSARY, GET OUT DITCHING CHKLIST} IF FAILURE IS IMMENINT: *2. LAND IMMEDIATELY |
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[INT XMSN CHIP]
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*1. TAIL OR INT XMSN MALFUNCTION EP
*1. LAND AS SOON AS POSSIBLE {TRANSIT SO YOU CAN ENTER AN AUTO IF NECESSARY, GET OUT DITCHING CHKLIST} IF FAILURE IS IMMENINT: *2. LAND IMMEDIATELY |
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[INT XMSN OIL HOT]
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*1. TAIL OR INT XMSN MALFUNCTION EP
*1. LAND AS SOON AS POSSIBLE {TRANSIT SO YOU CAN ENTER AN AUTO IF NECESSARY, GET OUT DITCHING CHKLIST} IF FAILURE IS IMMENINT: *2. LAND IMMEDIATELY |
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DUAL-ENGINE FAILURE IN FLIGHT
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*1. AUTOROTATION-PERFORM
*2. IMMEDIATE LANDING/DITCHING EP-PERFORM *3. ENGINE AIR RESTART EP-PERFORM |
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[AFCS DEGRADED]
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*1. SAFE ALTITUDE AND AIRSPEED-ESTABLISH (WAVEOFF, ITO AS REQ)
2. AFCS CONTROL PANEL-CHECK STATUS 3. AKNL ADVSY PUSHBUTTON-PRESS 4. FAIL ADVIAORY MODE RESET PUSHBUTTON-PRESS IF MALFUNCTION IS NOT ELIMINATED: 5. CMPTR PWR.RESET PUSHBUTTON-CYCLE 6. MALFUNCTIONING SYSTEM-OFF |
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[STABILATOR]
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*1. EXECUTE STAB AUTO MODE FAILURE EP
*1. CYCLIC-REDUCE AIRSPEED *2. COLLECTIVE DO NOT REDUCE *3. MAN SLEW SWITCH-ADJUST TO 0° WHEN SAFE ALTITUDE AND AIRSPEED: 4. STABILATOR C/B'S-CHECK 5. STABILATOR AUTO CONTROL PUSHBUTTON-PUSH ONCE |
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AC OR DC ELECTRICAL FAILURE
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*1. SAFE ALTITUDE AND AIRSPEED-ESTABLISH
{WARNING-ENSURE AIRSPEED LIMITS OK} *2. STABILATOR-CHK POSIT SLEW AS REQ {NOTE-STAB POSIT INDICATOR INOP WITHOUT AC ESSL} *3. APU EMERGENCY START PROC-PERFORM IF AC ELECTRICAL FAILURE: 4. #1 AND #2 GEN SWITCHES-RESET, ON IF DC ELECTRICAL FAILURE: 5. CONVERTER C/Bs-RESET IF AC AND/OR DC POWER NOT RESTORED: 6. LAND AS SOON AS PRACTICABLE 7. NONESSL ELECTRICAL EQUIPMENT-OFF |
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TGT LIMITS
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0°-810°C CONTINUOUS
810°-851° 30 MIN 851°-903° 2.5 MIN 903°-949° 12 SEC 949° MAX |
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Np LIMITS
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BELOW 96% AVOID
96-101% CONTINUOUS 101-120% 12 SEC. 120% MAX |
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Nr LIMITS
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BELOW 96% AVOID
96-101% CONTINUOUS 101-120% CAUTION 120% MAX |
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DUAL ENGINE TORQUE
(BELOW 80KTS) |
0-120 CONTINUOUS
120-144 10 SEC. 144% MAX |
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DUAL ENGINE TORQUE
(ABOVE 80KTS) |
0-106 CONTINUOUS
106-127 10 SEC. 127 MAX |
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SINGLE ENGINE TORQUE
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0-135 CONTINUOUS
135-144 10 SEC. 144 MAX |
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UNDERWATER EGRESS
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*1. PLACE HAND ON KNOWN REF POINT
*2. HABD-AS REQUIRED *3. ICS CORDS-DISCONNECT *4. HARNESS-RELEASE *5. EXIT HELICOPTER *6. SWIM CLEAR OF HELICOPTER AND INFLATE LPU |
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ENGINE MALFUNCTION IN FLIGHT
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*1. CONTROL Nr{WARNING: 105KIAS MAX}
*2. CONTENGENCY POWER-ON *3. SINGLE ENGING CONDITIONS-ESTABLISH a. AIRSPEED/AATTITUDE-ADJUST, AS REQ b. ENGINE ANTI-ICE SW-OFF, AS REQ c. EXTERNAL CARGO/STORES/FUEL-JETTISON/DUMP, AS REQ {WARNING: W/ENG ANTI-ICE UP TO 18%/49%TQ LOSS} *4. IDENTIFY MALFUNCTION 5. LAND AS SOON AS PRACTICABLE |
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ENGINE MALFUNCTION DURING HOVER/TAKEOFF
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*1. CONTROL Nr
*2. CONTGCY PWR SWITCH-ON IF A SUITABLE LANDING SITE EXITST OR UNABLE TO TRANSITION TO FORWARD FLIGHT: *3. SET LEVEL ATTITUDE, ELIMINATE DRIFT, CUSHION LANDING *4. ENGINE MALFUNCTION IN FLIGHT EMERGENCY PROCEDURE-PERFORM |
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ENGINE HIGH-SPEED SHAFT FAILURE
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{CAUTION: ENGINE WILL SHUTDOWN AND RELIGHT. ENGINE MUST BE SHUT DOWN MANUALLY TO PREVENT DAMAGE}
*1. ENGINE MALFUNCTION IN FLIGHT EMERGENCY PROCEDURE-PERFORM *2. PCL(MALF ENGINE)-OFF *3. FUEL SELECTOR LEVER(MALF ENGINE)-OFF |
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ENGINE HIGH-SIDE FAILURE IN FLIGHT
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*1. ENGINE MALFUNCTION IN FLIGHT EMERGENCY PROCEDURE-PERFORM
2. PCL(MALF ENGINE)-RETARD TO SET a. TQ 10% BELOW GOOD ENGINE b. MATCHED Ng c. MATCHED TGT |
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ENGINE HIGH-SIDE FAILURE ON DECK
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*1. PCLs-IDLE
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ENGINE LOW-SIDE FAILURE
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{CAUTION: IN LOCKOUT ENGINE RESPONSE IS MUCH FASTER, DO NOT EXCEED LIMITS}
*1. ENGINE MALFUNCION IN FLIGHT EMERGENCY PROCEDURE-PERFORM 2. PCL(MALF ENGING)-MOMMENTARILY ADVANCE TO LOCKOUT, THEN RETARD TO SET: a. TQ 10% BELOW GOOD ENGINE or b. MATCHED Ng or c. MATCHED TGT |
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ENGINE TORQUE OR TGT SPIKING/FLUCTUATIONS
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IF AND ENGINE INST IS SPIKING/FLUCTUATING AND INDUCING SECONDARY INDICATIONS IN Ng, Np, AND/OR Nr:
*1. ENGINE MALFUNCION IN FLIGHT EMERGENCY PROCEDURE-PERFORM {WARNING: PCL MOVEMENT MAY KILL ENG, TURN ON APU FIRST, USE LOW POWER SETTING WHILE MOVING PCL} IF FUEL CONTAMINATION IS SUSPECTED: *2. LAND AS SOON AS POSSIBLE 3. PCL(MALF ENGING)-MOMMENTARILY ADVANCE TO LOCKOUT, THEN RETARD TO SET: a. TQ 10% BELOW GOOD ENGINE or b. MATCHED Ng or c. MATCHED TGT IF FLUCTUATION PERSISTS: 4. PCL(ENG IN LOCKOUT)-RETARD TO IDLE, RETURN TO FLY 5. REPEAT STEPS 3&4 FOR OTHER ENGINE, AS REQ IF SPIKING W/ NO SECONDARIES: 6. LAND AS SOON AS PRACTICABLE |
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COCKPIT/CABIN FIRE(KNOWN SOURCE)
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*1. AFFECTED POWER SWITCH-OFF
*2. AFFECTED C/Bs-PULL *3. FIRE EXTINGUISHER-AS REQUIRED {WARNING: EXT VAPORS DISPLACE O2} IF FIRE CONTINUES: *4. LAND AS SOON AS POSSIBLE {WARNING: IF SEVERE ENOUGH-DITCH} IF FIRE EXTINGUISHED: 5. SMOKE AND FUMES ELIMINATION EP-PERFORM 6. LAND AS SOON AS PRACTICABLE |
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COCKPIT/CABIN FIRE(UNKNOWN SOURCE)
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*1. DOORS/WINDOWS/VENTS-CLOSE
*2. ECS-OFF *3. UNNECESSARY ELECTRICAL EQPT AND CBs-OFF/PULL IF FIRE CONTINUES: *4. LAND AS SOON AS POSSIBLE {WARNING: IF SEVERE ENOUGH-DITCH} 5. #1 GEN SWITCHES-OFF, AS REQ 6. BATT SWITCH-OFF, AS REQ IF FIRE EXTINGUISHED: 7. SMOKE AND FUMES ELIMINATION EP-PERFORM 8. LAND AS SOON AS PRACTICABLE |
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POSTSHUTDOWN ENGINE FIRE(TGT ABOVE 540°C)
|
*1. STARTER-ENGAGE, MOTOR ENGINE
IF FIRE PERSISTS, CONTINUE WHILE FIRE GUARD DISCHARGES INTO INTAKE *2. STARTER-SECURE(TGT BELOW 540°C) |
|
SMOKE AND FUMES ELIMINATION
|
*1. DOORS/WINDOWS/VENTS-OPEN
*2. AIRCRAFT-YAW, AS REQUIRED |
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GROUND RESONANCE
|
*1. GET AIRCRAFT AIRBORNE IMMEDIATELY
IF UNABLE TO GET AIRBORNE: *2. COLLECTIVE-LOWER *3. PCLs-OFF *4. ROTOR BRAKE-APPLY |
|
UNUSUAL ATTITUDE RECOVERY
|
*1. LEVEL WINGS
*2. NOSE ON HORIZON *3. CENTER BALL *4. STOP RATE OF CLIMB/DESCENT *5. CONTROL AIRSPEED |
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FIRE
|
*1. CONFIRM FIRE
*2. CONTGCY PWR SWITCH-ON *3. SINGLE-ENGINE CONDITIONS-ESTABLISH *4. PCL(AFFECTED ENGINE)-OFF *5. ENGINE T-HANDLE-PULL *6. FIRE EXTGH SW-MAIN(RES IF REQ) IF AIRBORNE: FIRE CONTINUES: *7. LAND IMMEDIATLEY FIRE APPEARS EXTINGUISHED: *8. LAND AS SOON AS POSSIBLE *9. SINGLE-ENGINE LANDING EP-PERFORM ON GROUND: *10. FIRE EXTINGUISHER-DISCHARGE INTO ENGINE COMPARTMENT |
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FIRE (APU)
|
*1. APU T-HANDLE-PULL
*2. CONFIRM FIRE *3. FIRE EXTGH SWITCH-RESERVE (MAIN IF REQUIRED AND AVAILABLE) IF AIRBORNE: FIRE CONTINUES: *4. LAND AS SOON AS POSSIBLE FIRE APPEARS EXTINGUISHED *5. LAND AS SOON AS PRACTICABLE ON GROUND: *6. FIRE EXTINGUISHER-AS REQUIRED 7. FUEL PUMP-OFF 8. APU CONTR SWITCH-OFF |
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#1 OR #2 FUEL FLTR BYPASS
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*1. FUEL SELECTOR LEVER (AFFECTED ENGINE)-XFD(DIR IF CURRENTLY IN XFD)
2. #1 AND #2 FUEL BOOST PUSHBUTTONS-ON 3. LAND AS SOON AS PRACTICABLE |
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#1 AND #2 FUEL FLTR BYPASS IN DIR/DIR
|
*1. #1 AND #2 FUEL BOOST PUSHBUTTONS-ON
*2. LAND AS SOON AS POSSIBLE (BE PREPARED FOR DUAL ENGING FAILURE) |
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#1 AND #2 FUEL FLTR BYPASS IN XFD/DIR
|
*1. FUEL SELECTOR LEVERS-SELECT OPPOSITE POSITIONS
2. LAND AS SOON AS PRACTICABLE |
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[#1] OR [#2 FUEL PRESS]
|
*1. FUEL SELECTOR LEVER(AFFECTED ENGINE)-XFD(DIR IF CURRENTLY IN XFD)
IF FUEL PRESS CAUTION DISSAPEARS: 2. LAND AS SOON AS PRACTICABLE IF FUEL PRESS CAUTION REMAINS: 3. FUEL SELECTOR LEVER(AFFECTED ENGINE)-DIR 4. #1 AND #2 FUEL BOOST PUSHBUTTONS-ON 5. LAND AS SOON AS PRACTICABLE |
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[#1] AND [#2 FUEL PRESS] IN DIR/DIR
|
*1. #1 & #2 FUEL BOOST PUSHBUTTONS-ON
*2. LAND AS SOON AS POSSIBLE (BE PREPARED FOR DUAL ENGINE FAILURE) |
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[#1] AND [#2 FUEL PRESS] IN XFD/DIR
|
*1. FUEL SELECTOR LEVERS-SELECT OPPOSITE POSITIONS
2. LAND AS SOON AS PRACTICABLE |
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[ROTOR BRAKE]
|
IF SECONDARY INDICATIONS ARE PRESENT:
*1. LAND AS SOON AS POSSIBLE 2. ROTOR BRAKE HANDLE-CHECK IN DETENT, ZERO PRESSURE IF NO SECONDARIES: 3. LAND AS SOON AS PRACTICABLE |
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BOOST SERVO HARDOVER
|
IF BOOST SERVO HARDOVER SUSPECTED:
*1. SAS/BOOST PUSHBUTTON-OFF 2. MINIMIZE FLIGHT CONTROL MOVEMENTS 3. LAND AS SOON AS PRACTICABLE. MAKE A SHALLOW APPROACH TO A HOVER, MAX 15 KTS XWIND. TAXI NO MORE THAN NECESSARY |
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MAXIMUM AIRSPEED
(Vne) |
180 KIAS
|
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MAXIMUM AUTOROTATION AIRSPEED
|
100 KIAS
|
|
MAXIMUM
SIDEWARD/REARWARD FLIGHT |
45 KIAS
|
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MAXIMUM
SIDEWARD/REARWARD FLIGHT WITH AN EXTERNAL LOAD |
35 KNOTS
|
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MAXIMUM AIRSPEED TWO SAS INOPERATIVE IN IMC
|
125 KIAS
|
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MAXIMUM AIRSPEED SAS/BOOST OFF
|
140 KIAS
|
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MAXIMUM AIRSPEED PRI SERVO PRESS CAUTION
|
125 KIAS
|
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MAXIMUM AIRSPEEDCABIN DOORS OPENING/CLOSING
|
100 KIAS
|
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MAXIMUM AIRSPEED CABIN DOORS OPEN
|
120 KIAS
|
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MAXIMUM AIRSPEED GUNNERS WINDOWS OPEN/CLOSED
|
170 KIAS
|
|
MAXIMUM AIRSPEED LANDING LIGHT IN TRANSITION
|
130 KIAS
|
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MAXIMUM AIRSPEED SEARCHLIGHT IN TRANSITION
|
100 KIAS
|
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MAXIMUM AIRSPEED AIRCRAFT GROSS WEIGHT >22,000 LBS W/EXT LOAD
|
120 KIAS
|
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MAXIMUM AIRSPEED TO JETTISON CRRC
|
140 KIAS
|
|
MAXIMUM AIRSPEED M240D:
CARRAIGE/FIRING- STOWING- BRASS COLLECTION BAG EMPTYING- |
120 KIAS
70 KIAS 40 KIAS |
|
MAXIMUM AIRSPEED BAMBI BUCKET:
FULL- EMPTY- DUMP- |
90 KIAS
70 KIAS 50 KIAS |
|
MAXIMUM AIRSPEED SINGLE ENGINE
|
105 KIAS
|
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Ng LIMITS
|
0-98 CONTINUOUS
98-102 30 MINUTES 102-105 12 SECONDS 105 MAXIMUM |
|
ENGINE OIL TEMP LIMITS
|
-50-135°C CONTINUOUS
135-150°C 30 MINUTES 150°C MAXIMUM |
|
ENGINE OIL PRESSURE LIMITS
|
22 PSI MINIMUM
22-50 PSI IDLE 26-100 PSI NORMAL 100-120 PSI PRECAUTIONARY 120 PSI MAXIMUM |
|
STARTER LIMITS:
DELAY BETWEEN ABORTED START ATTEMPTS |
60 SEC
|
|
STARTER LIMITS:
ENGAGE/DISENGAGE CYCLE OAT LESS THAN ___°C |
OAT LESS THAN 16°C
ENGAGE-60 SEC DISENGAGED ENGAGE-60 SEC DISENGAGED ENGAGE-60 SEC DISENGAGED ENGAGE-30 MIN DISENGAGED |
|
STARTER LIMITS:
ENGAGE/DISENGAGE CYCLE OAT ____°C TO ____°C |
16°C TO 52°C
ENGAGE-60 SEC DISENGAGED ENGAGE-30 MIN DISENGAGED |
|
STARTER LIMITS:
MOTOR ENGINE (IGNITION OFF) |
ENGAGE 2 MIN-DISENGAGED 5 MIN
ENGAGE 2 MIN-DISENGAGED 30 MIN |
|
MINIMUM PLANNED FUEL ON LANDING
|
NO LESS THAN 225lbs PER MAIN TANK
@300lbs PER MAIN TANK LIMIT AOB TO 30° |
|
APU LIMITS:
TEMPS BETWEEN ___ TO ___ WITH ROTORS ENGAGED IS LIMITED TO ______. |
TEMPS BETWEEN 43°C TO 60°C WITH ROTORS ENGAGED IS LIMITED TO 30 MINUTES.
|
|
APU LIMITS:
WITH ROTORS NOT ENGAGED, THE APU MAY BE OPERATED CONTINUOUSLY UP TO AND AMBIENT TEMPERATURE OF ___. |
WITH ROTORS NOT ENGAGED, THE APU MAY BE OPERATED CONTINUOUSLY UP TO AND AMBIENT TEMPERATURE OF 51°C.
|
|
BACKUP HYD PUMP LIMITS:
WITH OAT BETWEEN __°C AND __°C BACKUP PUMPIS LIMITED TO __ MINUTES OPERATING WITH A __ MINUTE COOL DOWN. |
WITH OAT BETWEEN 33°C AND 38°C BACKUP PUMPIS LIMITED TO 24 MINUTES OPERATING WITH A 72 MINUTE COOL DOWN.
WITH OAT BETWEEN 39°C AND 60°C BACKUP PUMPIS LIMITED TO 16 MINUTES OPERATING WITH A 48 MINUTE COOL DOWN. |
|
TEMPERATURE LIMITATIONS:
OPERATIONS BELOW ___°C OR ABOVE ___°C ARE PROHIBITED. |
OPERATIONS BELOW -40°C OR ABOVE 60°C ARE PROHIBITED.
|
|
MAXIMUM OPERATING DENSITY ALTITUDE
|
13,000FT
|
|
ANGLE OF BANK LIMITS:
NORMAL OPERATIONS |
45°
|
|
ANGLE OF BANK LIMITS:
OPERATIONS ABOVE 10,000 FT DA |
30°
|
|
ANGLE OF BANK LIMITS:
EITHER PRI SERVO PRESS CAUTION |
30°
|
|
ANGLE OF BANK LIMITS:
SAS/BOOST OFF FLIGHT |
30°
|
|
ANGLE OF BANK LIMITS:
BAMBI BUCKET MODEL 3542 |
30°
|
|
MAIN TRANSMISSION PRESSURE LIMITS
|
<20 PSI MIN
20-30 PSI IDLE AND TRANSIENT 30-65 PSI(HOVER) CONTINUOUS 45-60 PSI(LVL FLT) CONTINUOUS 65-130 PSI PRECAUTIONARY 130 PSI MAXIMUM |
|
MAIN TRANSMISSION TEMPERATURE LIMITS
|
-50-105°C CONTINUOUS
105°-120°C PRECAUTIONARY 120°C MAXIMUM |