Mh-60R Limits And Ep's Superhawk

Front 1

LOSS OF SONAR DOME

Back 1

*1. SONAR CABLE CUT PROCEDURES - AS REQUIRED

Front 2

FREESTREAM RECOVERY

Back 2

*1. PAC "STBY FOR FREESTREEM"
*2. SO "DOME STPD, DEPTH___.
*3. SO "ARRAY FOLDED
*4. PAC "COMMENCNG FREESTREAM"
*5. PNAC "OFF CABLE ANGLE"
*6. PNAC MONITOR ENG AND FLT INST, WARN OTHER ACFT TO STAY CLEAR
*7. SO "DOME CLEAR"
*8. PAC ADJUST A/S TO MAINTAIN CABLE OFF FUNNEL. WITH DOME BELOW TRAIL MAINTAIN <70 KIAS AND 15 DEG AOB

Front 3

ALL STORES JETTISON

Back 3

*1. ALL STORE JETT - PRESS

Front 4

HELLFIRE MISSILE UNLATCHED

Back 4

*1. INFORM THE CREW

Front 5

HELLFIRE MISSILE MISFIRE

Back 5

*1. ALERT CREW

Front 6

HELLFIRE MISSLE HANGFIRE

Back 6

IF ROCKET MOTOR IGNITES AND AIRCRAFT YAWS:
*1. ADJUST CONTROLS AS REQURIED TO MAINTAIN STRAIGHT-AND-LEVEL FLIGHT.
*2. ALERT CREW

Front 7

ABORTED HELLFIRE MISSILE LAUNCH

Back 7

*1. ALERT CREW

Front 8

FLIR UNCOMMANDED LASING

Back 8

*1. MASTER ARM - SAFE
*2. LASER SELECT - SAFE
IF LASING CONTINUES:
*3. FLIR - OFF

Front 9

CARGO HOOK EMERGENCY RELEASE

Back 9

*1. ALERT CREW
{WARNING USE OF EMER RELEASE MAY CAUSE INJURY TO CREW. ENSURE CREW ARE CLEAR OF HOOK AREA PRIOR TO ACTIVATING}
*2 CYCLIC EMERGENCY RELEASE/CABLE SHEAR - PRESS

Front 10

UNDERWATER EGRESS

Back 10

*1. HABD - AS REQUIRED
*2. ICS CORDS - DISCONNECT
*3. DOOR/WINDOW - OPEN/JETTISON.
*4. PLACE HAND ON KNOWN REFERENCE POINT.
*5. HARNESS - RELEASE
*6. EXIT HELICOPTER
AFTER EGRESS:
*7. SWIM CLEAR OF HELICOPTER AND INFLATE LPU

Front 11

IMMEDIATE LANDING/DITCHING (PILOT)

Back 11

*1. CREW AND PASSENGERS-ALERT
*2. SHOULDER HARNESS-LOCKED
*3. EXTERNAL CARGO/ STORES/ FUEL - JETTISON/ DUMP AS REQ.
*4. SEARCHLIGHT - AS REQUIRED
*5. MAYDAY/IFF - TRANSMIT/ EMERG
{TIME PERMITTING START APU}
IN THE FLARE:
*6. WINDOWS - JETTISON AS REQ
*7. PCLs - OFF
*8. ROTOR BRAKE - ON
*9. CO-PILOT COLLECTIVE - STOW
AFTER ALL VIOLENT MOTION STOPS:
*10. EGRESS

Front 12

SMOKE AND FUMES ELIMINATION

Back 12

*1. AIRSPEED - ADJUST, AS REQUIRED.
*2. DOORS/WINDOWS/VENTS - OPEN
*3. AIRCRAFT - YAW AS REQUIRED

Front 13

COCKPIT FIRE/CABIN FIRE

Back 13

IF SOURCE IS KNOWN:
*1. AFFECTED POWER SWITCHES AND CBS - SECURE
*2. PORTABLE FIRE EXT. - AS REQ.
IF FIRE CONTINUES OR SOURCE IS UNKNOWN:
*3. CABIN/DOORS/VENTS/ECS - CLOSE/OFF, AS REQUIRED.
*4. UNNECESSARY ELECTRICAL EQUIPMENT AND CBS - SECURE.
IF FIRE CONTINUES:
*5. LAND AS SOON AS POSSIBLE

Front 14

APU FIRE

Back 14

*1. APU T-HANDLE-PULL
*2. CONFIRM FIRE
*3. FIRE EXTGH SWITCH-RESERVE (MAIN IF REQUIRED AND AVAILABLE)
IF AIRBORNE AND FIRE CONTINUES:
*4. LAND IMMEDIATELY
IF FIRE APPEARS EXTINGUISHED *5. LAND AS SOON AS POSSIBLE
IF ON GROUND:
*6. FIRE EXTINGUISHER-AS REQUIRED

Front 15

INTERNAL ENGINE FIRE

RISE IN TGT ABOVE 540°C AFTER SHUTDOWN

Back 15

*1. STARTER-ENGAGE MOTOR ENGINE

Front 16

EXTERNAL ENGINE FIRE

FIRE #1/#2 ENG

Back 16

*1. CONFIRM FIRE
*2. ENGINE MALF. IN FLIGHT EP- PERFORM.
*3. PCL(AFFECTED ENGINE)-OFF
*4. ENGINE T-HANDLE (AFFECTED ENGINE) - PULL
*5. FIRE EXTGH SWITCH - MAIN(RESERVE IF REQUIRED)
IF AIRBORNE AND FIRE CONTINUES:
*6. LAND IMMEDIATLEY
IF FIRE APPEARS EXTINGUISHED:
*7. LAND AS SOON AS POSSIBLE

Front 17

#1 AND #2 FUEL FLTR BYPASS OR #1 AND #2 FUEL PRESS CAUTION LIGHTS

Back 17

*1. LAND AS SOON AS POSSIBLE
*2. APU EMERGENCY START PROCEDURE - PERFORM
[WARNING]BE PREPARED FOR DUAL ENGINE FAILURE RECOMMEND AIRSPEED PROFILE IS 80 KIAS TO MINIMIZE Nr DROOP SHOULD DUAL-ENGINE FAILURE OCCUR
CONSIDER PERFORMING IMMEDIATE LANDING/DITCHING EP

Front 18

#1 OR #2 FUEL FLTR BYPASS OR #1 OR #2 FUEL PRESS CAUTION LIGHTS

Back 18

*1. FUEL SELECTOR LEVER (AFFECTED ENGINE)-XFD(DIR IF CURRENTLY IN XFD

Front 19

AC OR DC ELECTRICAL FAILURE

Back 19

*1. SAFE ALTITUDE AND AIRSPEED-ESTABLISH
*2. STABILATOR-CHK POSIT SLEW AS REQ {WARNING-ENSURE AIRSPEED VS. STABILATOR LIMITS ARE NOT EXCEEDED.}
*3. APU EMERGENCY START PROC-PERFORM

Front 20

UNUSUAL ATTITUDE RECOVERY

Back 20

*1. LEVEL WINGS
*2. NOSE ON HORIZON
*3. CENTER BALL
*4. STOP RATE OF CLIMB/DESCENT
*5. CONTROL AIRSPEED

Front 21

STABILATOR AUTO MODE FAILURE

[STABILATOR]

Back 21

*1. PAC CALL - "STAB, STAB, STAB."
*2. CYCLIC - ARREST PITCH RATE.
*3. COLLECTIVE - DO NOT REDUCE
*4. MAN SLEW SWITCH - ADJUST TO 0°

Front 22

AFCS DEGRADED

Back 22

*1. SAFE ALTITUDE AND AIRSPEED-ESTABLISH (WAVEOFF ITO AS REQ)

Front 23

UTILITY PUMP CAUTION LIGHTS

UTILITY HYD PUMP
UTILITY HYD PUMP HOT
UTILITY HYD RSVR LOW

Back 23

*1. ALERT CREW. STOP DOME AS REQUIRED

Front 24

BOOST SERVO HARDOVER

Back 24

*1. SAS/BOOST PUSHBUTTON-OFF

Front 25

#2 PRIMARY SERVO OR #2 TRANSFER MODULE LEAK

#2 RSVR LOW AND #2 HYD PUMP CAUTION LIGHTS AND BACK UP PUMP ON ADVISORY LIGHT ON

Back 25

*1. SERVO SWITCH - 2ND OFF.
*2. LAND AS SOON AS PRACTICAL.
IF THE BACKUP RSVR LOW CAUTION ALSO APPEARS OR THE BACKUP PUMP FAILS:
*3. LAND AS SOON AS POSSIBLE.
IF THE #1 PRI SERVO CAUTION AND/OR [HYD] WARNING APPEARS:
*4. LAND IMMEDIATELY

Front 26

#1 PRIMARY SERVO OR #1 TRANSFER MODULE LEAK

#1 RSVR LOW AND #1 HYD PUMP CAUTION LIGHTS ON AND BACK UP PUMP ON ADVISORY LIGHT ON

Back 26

*1. SERVO SWITCH - 1ST OFF
*2. LAND AS SOON AS PRACTICAL
IF THE BACKUP RSVR LOW CAUTION ALSO APPEARS OR THE BACKUP PUMP FAILS:
*3. LAND AS SOON AS POSSIBLE
IF THE #2 PRI SERVO CAUTION AND/OR [HYD] WARNING APPEAR
*4. LAND IMMEDIATELY

Front 27

HYDRAULIC SYSTEM WARNING

HYD

Back 27

*1. LAND IMMEDIATELY

Front 28

LOSS OF TAIL ROTOR CONTROL

Back 28

*1. COLLECTIVE/AIRSPEED- ADJUST AS REQ TO CTRL YAW

Front 29

LOSS OF TAIL ROTOR DRIVE (ALTITUDE AND AIRSPEED SUFFICIENT TO ESTABLISH AUTOROTATION)

Back 29

*1. PAC CALL - "AUTO, AUTO, AUTO."
*2. AUTOROTATION-ESTABLISH. CENTER TAIL ROTOR PEDALS
*3. DRIVE FAILURE-ATTEMPT TO VERIFY
*4. IMMEDIATE LANDING/DITCHING EP-PERFORM
*5. PCLs - OFF WHEN DIRECTED (PRIOR TO THE FLARE)

Front 30

LOSS OF TAIL ROTOR DRIVE (ALTITUDE AND AIRSPEED NOT SUFFICIENT TO ESTABLISH AUTOROTATION)

Back 30

*1. PAC CALL - "HOVER, HOVER, HOVER."
*2. COLLECTIVE-LOWER
*3. PNAC - HANDS ON PCLs.
*4. PCLS-OFF WHEN DIRECTED(APPROXIMATELY 20-30 FT AGL)

Front 31

INPUT CHIP (#1/#2) CAUTION LIGHTS ON

Back 31

*1. MAIN TRANSMISSION MALFUNCTION EMERGENCY PROCEDURE - PERFORM

Front 32

TAIL/INTERMEDIATE TRANSMISSION MALFUNCTION

INT XMSN CHIP OR TAIL XMSN CHIP OR INT XMSN OIL HOT OR TAIL XMSN OIL

Back 32

IF FAILURE IS IMMINENT:
*1. LAND IMMEDIATELY
{TRANSIT SO YOU CAN ENTER AN AUTO IF NECESSARY, PERFORM IMMEDIATE LANDING/DITCHING CHKLIST}

Front 33

MAIN TRANSMISSION MALFUNCTION

MAIN XMSN OIL HOT OR MAIN XMSN PRESS HI OR MAIN XMSN PRESS LOW OR ACCESSORY CHIP (#1/#2)OR MAIN XMSN CHIP [CAUTIONS]
OR
MAIN XMSN OIL HOT OR MAIN XMSN PRESS HI [ADVISORIES]

Back 33

IF FAILURE IS IMMINENT:
*1. LAND IMMEDIATELY
IF SECONDARY INDICATIONS ARE PRESENT
*2. LAND AS SOON AS POSSIBLE TRANSIT AT 80FT/80KTS

Front 34

ROTOR SPEED CAUTION LIGHTS ON

ROTOR SPEED > 127 / 137 / 142

Back 34

*1. LAND AS SOON AS PRACTICAL

Front 35

LOW ROTOR RPM

Back 35

*1. CONTROL Nr.

Front 36

HUNG DROOP STOP(S)

Back 36

*1. REENGAGE ROTOR TO GREATER THAN 75% Nr.

Front 37

UNUSUAL VIBRATIONS ON DECK

Back 37

*1. COLLECTIVE - LOWER
*2. PCLs - OFF
*3. ROTOR BRAKE - APPLY AS REQUIRED.

Front 38

APU EMERGENCY START

Back 38

*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

Front 39

ENGINE AIR RESTART

Back 39

*1. APU EMERGENCY START-AS REQUIRED
*2. ENGINE IGNITION SWITCH-NORM
*3. FUEL SEL LEVER(S)-DIR OR XFD
*4. PCL(S)-OFF
*5. STARTER(S)-ENGAGE
*6. PCL-IDLE(TGT<80° IF TIME PERMITS)
*7. PCL-FLY AFTER STARTER DROPOUT

Front 40

DUAL-ENGINE FAILURE IN FLIGHT

Back 40

*1. AUTOROTATION-PERFORM
*2. IMMEDIATE LANDING / DITCHING EP-PERFORM
If Time/altitude permit:
*3. ENGINE AIR RESTART EP-PERFORM

Front 41

SINGLE-ENGINE FAILURE IN FLIGHT

ENG OUT (#1/#2) AND TORQUE SPLIT

Back 41

*1. ENGINE MALFUNCTION IN FLIGHT EMERGENCY PROCEDURE - PERFORM

Front 42

ENGINE MALFUNCTION DURING HOVER/TAKEOFF

Back 42

*1. CONTROL Nr
*2. CONTGCY PWR SWITCH-ON
IF A SUITABLE LANDING SITE EXISTS OR UNABLE TO TRANSITION TO FORWARD FLIGHT:
*3. SET LEVEL ATTITUDE ELIMINATE DRIFT CUSHION LANDING
*4. ENGINE MALFUNCTION IN FLIGHT EMERGENCY PROCEDURE-PERFORM

Front 43

ABORT START PROCEDURE

Back 43

*1. PCL-OFF
*2. IGNITOR SWITCH-OFF
*3. STARTER-ENGAGE
4. STARTER DISENGAGE (AFTER 30SEC. AND TGT BELOW 540°)

Front 44

ENGINE HIGH-SPEED SHAFT FAILURE

Back 44

{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

Front 45

COMPRESSOR STALL

Back 45

*1. ENGINE MALFUNCTION IN FLIGHT EMERGENCY PROCEDURE - PERFORM
*2. PCL (MALFUNCTIONING ENGINE) - IDLE

Front 46

ENGINE TORQUE OR TGT SPIKING/FLUCTUATIONS

Back 46

IF AN ENG INST IS SPIKING/ FLUCTUATING AND INDUCING SEC. IND. IN Ng Np AND/OR Nr:
*1. ENGINE MALFUNCION IN FLIGHT EP - PERFORM
IF FUEL CONTAMINATION IS SUSPECTED:
*2. LAND AS SOON AS POSSIBLE
{WARNING: PCL MOVEMENT MAY PRECIPITATE ENG FAIL. CONSIDER PERF. APU EMER. START PROC. PRIOR TO MOVING PCL. MAINTAIN LOW PWR SETTING TO MIN. Nr DECAY RATE SHOULD ENG. FAIL}

Front 47

ENGINE LOW-SIDE FAILURE

Back 47

{CAUTION: IN LOCKOUT ENGINE RESPONSE IS MUCH FASTER AND TGT LIMITING IS INOP DO NOT EXCEED LIMITS}
*1. ENGINE MALFUNCION IN FLIGHT EMERGENCY PROCEDURE-PERFORM

Front 48

ENGINE HIGH-SIDE FAILURE ON DECK

Back 48

*1. PCLs-IDLE

Front 49

ENGINE HIGH-SIDE FAILURE IN FLIGHT

Back 49

*1. ENGINE MALFUNCTION IN FLIGHT EMERGENCY PROCEDURE-PERFORM
*2. PCL(MALF ENGINE)-RETARD TO SET
a. TQ 10% BELOW GOOD ENGINE,or
b. MATCHED Ng, or
c. MATCHED TGT

Front 50

ENGINE MALFUNCTION IN FLIGHT

Back 50

*1. CONTROL Nr
{WARNING: 105KIAS MAX}
*2. CONTINGENCY POWER-ON
*3. SINGLE ENGING CONDITIONS-ESTABLISH
*4. ENGINE ANTI-ICE SW-OFF, AS REQ
*5. EXTERNAL CARGO/STORES/FUEL-JETTISON/DUMP, AS REQ {WARNING: W/ENG ANTI-ICE UP TO 18%/49%TQ LOSS}
*6. IDENTIFY MALFUNCTION

Front 51

WHAT CONDITIONS CAUSE AUTOMATIC BACKUP PUMP OPERATIONS

Back 51

[#1 HYD PUMP] [#2 HYD PUMP] [#1 RSVR LOW] [#1 TAIL ROTOR SERVO]

Front 52

STABILATOR FIXED 40° TRAILING EDGE DOWN: MAX AIRSPEED

Back 52

45 KTS

Front 53

STABILATOR FIXED 30° TRAILING EDGE DOWN: MAX AIRSPEED

Back 53

60 KTS

Front 54

STABILATOR FIXED 20° TRAILING EDGE DOWN: MAX AIRSPEED

Back 54

80 KTS

Front 55

STABILATOR FIXED 10° TRAILING EDGE DOWN: MAX AIRSPEED

Back 55

100 KTS

Front 56

STABILATOR FIXED 0° TRAILING EDGE DOWN: MAX AIRSPEED

Back 56

150 KTS

Front 57

TGT LIMITS

Back 57

0°-810°C CONTINUOUS
810°-851° 30 MIN
851°-903° 2.5 MIN
903°-949° 12 SEC
949° MAX

Front 58

Np LIMITS

Back 58

<96% AVOID
96-101% CONTINUOUS
101-120% 12 SEC
120% MAX

Front 59

Nr LIMITS

Back 59

<96% AVOID
96-101% CONTINUOUS
101-120% CAUTION
120% MAX
123% FOR FCF AND AUTOROTATION ONLY
OVERSPEED LATCHES 127%, 137%, 142%

Front 60

DUAL ENGINE TORQUE (BELOW 80KTS)

Back 60

0-120 CONTINUOUS
120-144 10 SEC
144% MAX

Front 61

DUAL ENGINE TORQUE (ABOVE 80KTS)

Back 61

0-106 CONTINUOUS
106-127 10 SEC
127 MAX

Front 62

SINGLE ENGINE TORQUE

Back 62

0-135 CONTINUOUS
135-144 10 SEC
144 MAX

Front 63

MAXIMUM AIRSPEED (Vne)

Back 63

180 KIAS

Front 64

MAXIMUM AUTOROTATION AIRSPEED

Back 64

100 KIAS

Front 65

MAXIMUM SIDEWARD/REARWARD FLIGHT

Back 65

35 KIAS

Front 66

MAXIMUM AIRSPEED TWO SAS INOPERATIVE IN IMC

Back 66

125 KIAS

Front 67

MAXIMUM AIRSPEED BOOST OFF

Back 67

140 KIAS

Front 68

MAXIMUM AIRSPEED PRI SERVO PRESS CAUTION

Back 68

125 KIAS

Front 69

MAXIMUM AIRSPEEDCABIN DOORS OPENING/CLOSING

Back 69

60 KIAS

Front 70

MAXIMUM AIRSPEED SEARCHLIGHT IN FIXED POSITION OTHER THAN STOWED

Back 70

160 KIAS

Front 71

MAXIMUM AIRSPEED SEARCHLIGHT IN TRANSITION

Back 71

100 KIAS

Front 72

MAXIMUM AIRSPEED/AOB DOME AT TRAIL (CABLE EXTENDED 10 FEET, DOME APPROX 6 FEET BELOW AIRCRAFT)

MAX A/S AND AOB DOME BELOW TRAIL

Back 72

100 KIAS, 45 DEG AOB AT TRAIL

70 KIAS, 15 DEG AOB BELOW TRAIL

Front 73

MAXIMUM AIRSPEED SINGLE ENGINE

Back 73

105 KIAS

Front 74

Ng LIMITS

Back 74

0-98% CONTINUOUS
98%-102% 30 MINUTES
102-105% 12 SECONDS
105% MAXIMUM

Front 75

ENGINE OIL TEMP LIMITS

Back 75

-50-135°C CONTINUOUS
135-150°C 30 MINUTES
150°C MAXIMUM

Front 76

ENGINE OIL PRESSURE LIMITS

Back 76

22 PSI MINIMUM
22-26 PSI PRECAUTIONARY
26-100 PSI CONTINUOUS
100-120 PSI PRECAUTIONARY
120 PSI MAXIMUM

Front 77

STARTER LIMITS: DELAY BETWEEN ABORTED START ATTEMPTS

Back 77

60 SEC

Front 78

STARTER LIMITS: ENGAGE/DISENGAGE CYCLE OAT LESS THAN 16°C

Back 78

FIRST CYCLE 60 SEC DISENGAGED
SECOND CYCLE 60 SEC DISENGAGED
THIRD CYCLE 60 SEC DISENGAGED
FOURTH CYCLE 30 MIN DISENGAGED

Front 79

STARTER LIMITS: ENGAGE/DISENGAGE CYCLE OAT 16°C TO 52°C

Back 79

FIRST CYCLE 60 SEC DISENGAGED
SECOND CYCLE 30 MIN DISENGAGED

Front 80

STARTER LIMITS: MOTOR ENGINE (IGNITION OFF)

Back 80

ENGAGE 2 MIN-DISENGAGED 5 MIN ENGAGE 2 MIN-DISENGAGED 30 MIN

ALL TIMES CUMULATIVE WITHIN A 5-MINUTE PERIOD

Front 81

MINIMUM PLANNED FUEL ON LANDING

Back 81

NO LESS THAN 600lbs

Front 82

APU LIMITS: TEMPS ABOVE 43 DEG C WITH ROTORS ENGAGED IS LIMITED TO ______.

Back 82

30 MINUTES

Front 83

APU LIMITS: WITH ENGINE AND ROTORS NOT OPERATING THE APU MAY BE OPERATED CONTINUOUSLY UP TO AN AMBIENT TEMPERATURE OF ___.

Back 83

51°C.

Front 84

BACKUP HYD PUMP LIMITS: WITH OAT BETWEEN 33°C AND 38°C BACKUP PUMP IS LIMITED TO __ MINUTES OPERATING WITH A __ MINUTE COOL DOWN.

Back 84

24 MINUTES 72 MINUTE COOL DOWN.

Front 85

TEMPERATURE LIMITATIONS: OPERATIONS BELOW ___°C OR ABOVE ___°C ARE PROHIBITED.

Back 85

OPERATIONS BELOW -40°C(-40°F) OR ABOVE 60°C(140°F) ARE PROHIBITED.

Front 86

ANGLE OF BANK LIMITS: NORMAL OPERATIONS

Back 86

45°

Front 87

ANGLE OF BANK LIMITS: OPERATIONS ABOVE 10000 FT DA

Back 87

30°

Front 88

ANGLE OF BANK LIMITS: EITHER PRI SERVO PRESS CAUTION

Back 88

30°

Front 89

ANGLE OF BANK LIMITS: BOOST OFF FLIGHT

Back 89

30°

Front 90

MAIN TRANSMISSION PRESSURE LIMITS

Back 90

20 PSI MIN
20-30 PSI IDLE AND TRANSIENT
30-65 PSI CONTINUOUS
45-60 PSI(LVL FLT) CONTINUOUS
65-130 PSI PRECAUTIONARY
130 PSI MAXIMUM

Front 91

MAIN TRANSMISSION TEMPERATURE LIMITS

Back 91

-50-105°C CONTINUOUS
105°-120°C PRECAUTIONARY
120°C MAXIMUM

Front 92

MAMIMUM WIND VELOCITY FOR ROTOR ENGAGEMENT

Back 92

45 KTS FROM ANY DIRECTION

Front 93

SONOBUOY LAUNCH LIMITS

Back 93

70 TO 150 FEET UP TO 100 KIAS WITH DOME AT TRAIL
ABOVE 100 KIAS, 150 FEET OR ABOVE WITH DOME SEATED

Front 94

MAXIMUM AIRSPEED WITH WINDSHIELD WIPERS OPERATING

Back 94

130 KIAS

Front 95

BACKUP HYD PUMP LIMITS:
WITH OAT BETWEEN 39°C AND 60°C BACKUP PUMP IS LIMITED TO __MINUTES OPERATING WITH A __MINUTE COOLDOWN

Back 95

16 MINUTES 48 MINUTE COOL DOWN.

Front 96

PROHIBITED MANEUVERS

Back 96

1. AEROBATIC FLIGHT
2. PRACTICE FULL-AUTOROTATION LANDINGS
3. INTENTIONAL APPROACHES INTO OR INDUCEMENT OF RETREATING BLADE STALL

Front 97

ROTOR BRAKE OPERATING LIMITS

Back 97

MAX ROTOR SPEED FOR APPLICATION IS 76%
ROUTINE ROTOR STOPS SHALL BE MADE BETWEEN 30-50% AND LIMITED TO 180 PSI TO EXTEND SERVICE LIFE

Front 98

BLADE, PYLON, AND STABILATOR FOLD AND SPREAD LIMITATIONS

WIND SPEED AND TIME LIMITS

Back 98

45 KNOTS FROM ANY DIRECTION FOR BLADE FOLD AND PYLON/STABILATOR FOLD

FOLLOWING 3 BLADE FOLD AND SPREAD CYCLES, ALLOW A 10-MINUTE COOLING PERIOD

Front 99

LANDING LIMITATION

RATES OF DESCENT

Back 99

LEVEL TERRAIN 720 fpm GROSS WEIGHT <19,500 LBS 480 fpm GROSS WEIGHT >19,500 LBS
SLOPED TERRAIN SHALL NOT EXCEED 360 fpm

Front 100

LANDING LIMITATION

AIRSPEEDS TAILWHEEL LOCKED/UNLOCKED

Back 100

75 KTS WITH TAILWHEEL LOCKED

20 KTS WITH TAILWHEEL UNLOCKED

Front 101

SLOPE LANDING LIMITATIONS

Back 101

A. 9° NOSE-UP SLOPE
B. 12° CLOSS-SLOPE
C. 6° NOSE-DOWN SLOPE

Front 102

AIRCRAFT WEIGHT LIMITATIONS

Back 102

MAX GROSS WEIGHT 23,500LBS
RECOVERY CVN 23,500LBS
RECOVERY OTHER 22,500LBS

Front 103

INTERNAL LOAD WEIGHT LIMITATIONS

Back 103

300LBS PER SQUARE FOOT

Front 104

EXTERNAL LOAD LIMITATIONS

Back 104

CARGO HOOK 6,000LBS

RESCUE HOIST 600LBS

Front 105

CENTER OF GRAVITY LIMITATIONS

Back 105

AT MAX GROSS WEIGHT LATERAL CG IS 8.0 INCHES RIGHT AND 7.5 INCHES LEFT

Front 106

MINIMUM EQUIPMENT FOR NIGHT FLIGHT OVER WATER

Back 106

1. LAWS
2. ALTITUDE HOLD (RADALT OR BARALT)

Front 107

FLIGHTS INTO FORECAST OR KNOWN ICING

Back 107

ACFT EQUIPPED WITH OPERABLE ANTI-ICE AND BLADE DEICE ARE PERMITTED FLIGHT INTO FORECAST OR KNOWN TRACE OR LIGHT ICING. ALL OTHERS NO FLIGHT 5°C OR BELOW IN VISIBLE MOISTURE.
FLIGHT INTO KNOWN MODERATE OR SEVERE ICING IS PROHIBITED