MH-60S Limits and EPs

Start Studying!

Terms

undefined, object

copy deck

#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
#1 PUMP/1+B/U RSVR LOW: *1. LAND AS SOON AS POSSIBLE
IF THE [#2 PRI SERVO] AND [HYD] WARNING APPEAR
*2. LAND IMMEDIATELY
#2 PUMP/RSVR LOW/BKUP ON: *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
#2 PUMP/2+B/U RSVR LOW: *1. LAND AS SOON AS POSSIBLE
IF THE [#1 PRI SERVO] CAUTION AND [HYD] WARNING APPEAR
*2. LAND IMMEDIATELY
[HYD]: *1. LAND IMMEDIATELY
[#1 HYD PUMP]: *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
LOSS OF TAIL ROTOR CONTROL: *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
2 HYD PUMP: *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
[#1 + #2 HYD PUMP FAIL]: *1. RESTRICT CONTROL MOVEMENT
*2. LAND AS SOON AS POSSIBLE
WHAT CONDITIONS CAUSE AUTOMATIC BACKUP PUMP OPERATIONS: [#1 PUMP]
[#2 PUMP]
[#1 RSVR LOW]
[#1 TAIL ROTOR SERVO]
IMMEDIATE LANDING/DITCHING: *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
APU EMERGENCY START: *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
ABORT START PROCEDURE: *1. PCL-OFF
*2. IGNITOR SWITCH-OFF
*3. STARTER-ENGAGE
*4. STARTER DISENGAGE (AFTER 30SEC. AND TGT BELOW 540°)
ENGINE AIR RESTART: {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
STABILATOR FIXED 40° TRAILING EDGE DOWN: MAX AIRSPEED: 45 KTS.
STABILATOR FIXED 30° TRAILING EDGE DOWN: MAX AIRSPEED: 60 KTS
STABILATOR FIXED 20° TRAILING EDGE DOWN: MAX AIRSPEED: 80 KTS
STABILATOR FIXED 10° TRAILING EDGE DOWN: MAX AIRSPEED: 100 KTS
STABILATOR FIXED 0° TRAILING EDGE DOWN: MAX AIRSPEED: 150 KTS
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)
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)
[MAIN XMSN CHIP]: *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
[MAIN XMSN OIL HOT]: *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
[MAIN XMSN PRESS HI]: *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
[MAIN XMSN PRESS LOW]: *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
[TAIL XMSN CHIP]: *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
[TAIL XMSN OIL HOT]: *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
[INT XMSN CHIP]: *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
[INT XMSN OIL HOT]: *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
DUAL-ENGINE FAILURE IN FLIGHT: *1. AUTOROTATION-PERFORM
*2. IMMEDIATE LANDING/DITCHING EP-PERFORM
*3. ENGINE AIR RESTART EP-PERFORM
[AFCS DEGRADED]: *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
[STABILATOR]: *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
AC OR DC ELECTRICAL FAILURE: *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
TGT LIMITS: 0°-810°C CONTINUOUS
810°-851° 30 MIN
851°-903° 2.5 MIN
903°-949° 12 SEC
949° MAX
Np LIMITS: BELOW 96% AVOID
96-101% CONTINUOUS
101-120% 12 SEC.
120% MAX
Nr LIMITS: BELOW 96% AVOID
96-101% CONTINUOUS
101-120% CAUTION
120% MAX
DUAL ENGINE TORQUE (BELOW 80KTS): 0-120 CONTINUOUS
120-144 10 SEC.
144% MAX
DUAL ENGINE TORQUE (ABOVE 80KTS): 0-106 CONTINUOUS
106-127 10 SEC.
127 MAX
SINGLE ENGINE TORQUE: 0-135 CONTINUOUS
135-144 10 SEC.
144 MAX
UNDERWATER EGRESS: *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
ENGINE MALFUNCTION IN FLIGHT: *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
ENGINE MALFUNCTION DURING HOVER/TAKEOFF: *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
ENGINE HIGH-SPEED SHAFT FAILURE: {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
ENGINE HIGH-SIDE FAILURE IN FLIGHT: *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
ENGINE HIGH-SIDE FAILURE ON DECK: *1. PCLs-IDLE
ENGINE LOW-SIDE FAILURE: {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
ENGINE TORQUE OR TGT SPIKING/FLUCTUATIONS: 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
COCKPIT/CABIN FIRE(KNOWN SOURCE): *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
COCKPIT/CABIN FIRE(UNKNOWN SOURCE): *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&#2 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
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
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
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
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
#1 OR #2 FUEL FLTR BYPASS: *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
#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)
#1 AND #2 FUEL FLTR BYPASS IN XFD/DIR: *1. FUEL SELECTOR LEVERS-SELECT OPPOSITE POSITIONS
2. LAND AS SOON AS PRACTICABLE
[#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
[#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)
[#1] AND [#2 FUEL PRESS] IN XFD/DIR: *1. FUEL SELECTOR LEVERS-SELECT OPPOSITE POSITIONS
2. LAND AS SOON AS PRACTICABLE
[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
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
MAXIMUM AIRSPEED (Vne): 180 KIAS
MAXIMUM AUTOROTATION AIRSPEED: 100 KIAS
MAXIMUM SIDEWARD/REARWARD FLIGHT: 45 KIAS
MAXIMUM SIDEWARD/REARWARD FLIGHT WITH AN EXTERNAL LOAD: 35 KNOTS
MAXIMUM AIRSPEED TWO SAS INOPERATIVE IN IMC: 125 KIAS
MAXIMUM AIRSPEED SAS/BOOST OFF: 140 KIAS
MAXIMUM AIRSPEED PRI SERVO PRESS CAUTION: 125 KIAS
MAXIMUM AIRSPEEDCABIN DOORS OPENING/CLOSING: 100 KIAS
MAXIMUM AIRSPEED CABIN DOORS OPEN: 120 KIAS
MAXIMUM AIRSPEED GUNNERS WINDOWS OPEN/CLOSED: 170 KIAS
MAXIMUM AIRSPEED LANDING LIGHT IN TRANSITION: 130 KIAS
MAXIMUM AIRSPEED SEARCHLIGHT IN TRANSITION: 100 KIAS
MAXIMUM AIRSPEED AIRCRAFT GROSS WEIGHT >22,000 LBS W/EXT LOAD: 120 KIAS
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
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
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

Start Studying!

Deck Info

Number of cards 99