SH-60B HELICOPTER. FLIGHT MANUAL (2008)

A1-H60BB-NFM--000

INDEX

Page

No.

AGM-114 Hellfire missile

launch/training procedure

7-77

Ability to maintain level flight,

Air taxi

7-89

single engine chart

27-1

Air--capable ship helicopter operations

8-4

Sample problem for use of ability to

Air--capable ship launch and

maintain level flight,

recovery procedures

8-5

single engine chart

27-1

Approach procedures

8-6

Abort start

12-21

Shipboard launch/recovery limitations

8-6

AC bus tie system

2-54

Air--capable ship launch and

AC electrical system

2-49

recovery procedures

8-5

AC ESS bus off caution light

12-61

Air--mass

9-44

Accelerometer null procedures

7-64

Air-to-air receive mode

16-12

Accessory module

2-33

Air-to-air transmit/receive mode

16-16

Adaptability/flexibility

19-3

Airborne release

8-23

Adjustment:

Airborne tactical officer

5-2

GAU-16/A headspace adjustment

9-59

Aircraft control changes

19-8

GAU-16/A headspace adjustment

Aircraft performance

9-45

checklist

9-60

In flight power available check

9-46

GAU-16/A timing adjustment

9-60

Power required

9-46

GAU-16/A timing adjustment checklist

9-61

Aircraft startup

8-15

Seat adjustment

2-129

Aircraft tiedown instructions

3-17

Advanced helicopter emergency

Aircraft tiedown requirements

3-17

egress lighting system

2-142

Main rotor tiedown

3-19

Aerodynamic limitations

4-8

Aircraft tiedown requirements

3-17

Airspeed operating limits

4-8

Aircraft tiedown/securing

3-17

Autorotation

4-12

Aircraft tiedown instructions

3-17

Controllable searchlight airspeed limits

4-8

Aircraft towing

3-14

Minimum height for safe landing

Aircrew currency requirements

5-6

after single- or dual-engine failure

4-8

Special mission/lookout non-aircrewman

5-6

AFCS caution lights

12-52

Aircrew definitions

19-6

AFCS degraded caution light on

12-52

Aircrew grading criteria

20-14

AFCS fail advisory lights

12-52

Flight evaluation grading criteria

20-14

SAS caution light on

12-53

Oral examination grading criteria

20-14

AFCS control panels

2-85

Aircrewman checklists

7-41

AFCS degraded caution light on

12-52

Before landing checklist

7-47

AFCS emergencies

12-50

Post flight checklist

7-49

Coupler emergencies

12-50

Post landing checks

7-48

Stabilator malfunctions

12-54

Post takeoff checks

7-47

Unusual attitude recovery

12-56

Prestart checklist

7-41

AFCS fail advisory lights

12-52

Pretakeoff checklist

7-44

AFCS voltage sensor relay

2-89

RAST recovery checklist

7-48

AGM--114 Hellfire preflight checklist

7-8

Utility systems checks

7-43

Index-1

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Aircrewman ground training

5-6

Practice autorotative approach

7-94

Aircrewman qualifications

5-5

Self--contained approach procedures

8-8

Aircrew currency requirements

5-6

Standard mountain approach and landing . . .

9-50

Night vision device aircrewman

5-6

Steep approach

7-92

Night vision device

Visual approach

8-7

aircrewman instructor

5-6

Approach procedures

8-6

Qualified observer

5-6

Instrument approach

8-7

Aircrewman utility systems checks

7-43

Landing transition

8-8

Cargo hook preoperational check

7-44

Self--contained approach procedures

8-8

Rescue hoist preoperational check

7-43

Visual approach

8-7

Airspeed indicator

2-112

Approach to landing

7-91

Airspeed operating limits

4-8

Normal approach

7-92

Airspeed system correction

Steep approach

7-92

from level flight charts

28-1

APU

2-47

Sample problem for airspeed system

Accessories

2-47

correction from level flight charts

28-1

Control and monitoring

2-47

Alert launch checklist

7-52

Controls

2-47

Engagement

7-57

Oil system servicing

3-14

Starting APU and engines

7-57

Operating limitations

4-17

Alpine meadows

9-45

Start system

2-49

Alternate engine start procedures

7-83

Turn--up checklist

7-84

Crossbleed start

7-83

APU emergencies

12-29

Alternator

2-10

Caution lights

12-29

Altitude hold

2-96

Emergency start

12-29

Altitude limitation

4-12

Fail caution light on

12-29

AN/PEQ-3 uncommanded lasing

12-101

Fire

12-70

Anabatic

9-43

Generator caution light on

12-29

Angle of attack

11-5

Oil temp hi caution light on

12-30

Anti--ice:

Area:

Eng inlet anti--ice on (#1/#2)

Cockpit -- left side (area 2)

7-2

advisory light on

12-28

Cockpit -- right side (area 11)

7-7

Engine and inlet anti--ice system

2-123

Confined area landing

7-93

Engine anti--ice check

7-63

Flight controls and hydraulics bay (area 3) . . .

7-3

Engine inlet anti--ice valve

2-17

Fuselage -- left side (area 5)

7-5

Anticollision lights

2-65

Fuselage -- right side (area 10)

7-7

Applicability

20-1

Main rotor/transmission/

Approach:

APU/engines (area 4)

7-4

Auto approach to a hover

2-97

Nose section (area 1)

7-2

Automatic approach checklist

7-52

Tail cone -- left side (area 6)

7-6

Instrument approach

8-7

Tail cone -- right side (area 9)

7-7

Instrument approach procedure

13-1

Tail pylon -- left side (area 7)

7-6

Loss of tail rotor control approach

Tail pylon -- right side (area 8)

7-6

and landing technique

12-39

ASQ--81 towed body down limit

Normal approach

7-92

switch malfunction

12-87

ORIGINAL

Index-2

A1-H60BB-NFM--000

Page

No.

ASQ--81 towed body fails

Aviation ship launch and

to seat properly

12-87

recovery procedures

8-3

Assembly:

Avionics cooling

2-122

Attitude gyro control assembly (AGCA)

(pilot and ATO)

16-4

Main rotor hub

2-25

Backlash

9-44

Assertiveness

19-2

Backup hyd pump fails to operate

12-49

Attitude and airspeed hold

2-95

Backup hydraulic pump

Attitude gyro control assembly

16-4

hot weather limitations

4-17

Attitude indicator

2-113

Backup hydraulic system

2-73

Audio converter-processor

15-2

Backup pump limits

4-17

Auto approach to a hover

2-97

Backup rsvr low caution light on

12-44

Automatic approach checklist

7-52

Bank angles limitation

4-12

Barometric altimeter

2-113

Automatic depart

2-98

Barometric altimeter/encoder

2-113

Automatic flight control system

2-84

Battery fault caution light

12-61

AFCS control panels

2-85

Battery low charge caution light

12-62

DAFCS

2-87

BDHI displayed data as a function

Stabilator system

2-89

of selected mode

16-9

Automatic preflight checks

2-105

Bearing-distance-heading indicators

16-5

Automatic sonobuoy launching

7-68

Before leaving the helicopter

14-4

Autopilot

2-95

Bingo profile, maximum range

Autopilot

2-95

with dual engine

25-1

Autorotation

4-12, 12-22

Blade damper accumulator

3-12

Autorotational descent

7--90, 11-12

Blade de--ice control panel

2-123

Autorotational entry

11-11

Blade de--ice system check

7-61

Autorotational recovery

11-12

Blade de--ice system operation

2-123

Autorotative state

11-11

Blade de--ice test panel

2-128

Aux fuel xfer fault caution light

12-67

Blade de--ice test system operation

2-128

Blade fold system

2-101

Auxiliary fuel system

2-45

Blade folding

2-101

Auxiliary fuel tanks

2-46

Blade retention

2-26

Fuel management control panel

2-45

Blade stall

11-3

Fuel transfer system

2-46

Blade stall causes

11-3

Manual fuel transfer check

2-46

Methods of eliminating

Auxiliary fuel tanks

2-46

roughness caused by blade stall

11-3

Auxiliary power unit system

2-47

Blade stall causes

11-3

Aviation ship helicopter operations

8-3

Blade stall chart

22-1

Aviation ship launch and

Sample problem for use

recovery procedures

8-3

of blade stall chart

22-1

Launch and recovery signals

8-3

Blade, pylon/stabilator fold or spread

4-15

Night and IMC operations

8-4

Blade/pylon/stabilator folding and spreading

8-2

Shipboard launch/recovery limitations

8-3

Blowback

11-2

Shutdown

8-4

Boost servo hardover

12-50

Waveoff procedures

8-4

Boost servos

2-82

Index-3

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Breakup and rendezvous procedures

9-35

Change of scans

13-2

Briefing/debriefing

6-1

Characteristics:

Crew brief and preflight

19-8

Engine oil system characteristics

14-2

Debriefing

6-8

General flight characteristics

11-1

General briefing

6-1

Maneuvering flight characteristics

11-6

Gunner brief

6-7

Rollover characteristics

11-13

Landing site evaluation brief

9-41

SH-60B tail rotor characteristics

11-4

Mission--specific briefing

6-2

Chart(s):

Passenger brief

6-8

Ability to maintain level flight,

single engine chart

27-1

Qualified observer brief

6-7

Blade stall chart

22-1

Density altitude chart

22-1

Engine performance charts

22-5

Cabin dome lights

2-68

Engine performance, contingency

Cabin inspection

7-10

(2.5 minute) power chart

22-5

Cable grip rigging procedures

12-89

Engine performance, intermediate

(30 minute) power chart

22-5

Rescue hoist cable cut

12-90

Engine performance, maximum

Rescue hoist cable separation

12-90

continuous power chart

22-5

Rescue hoist fouled cable

12-89

Functional checkflight charts

Runaway hoist

12-89

and tables

10-60

Canyon recce

9-50

Hover charts

23-1

Canyons and ravines

9-45

Maximum power check chart

10-57

Cargo delivery

9-21

Maximum range, standard day chart

25-1

Cargo hook preflight

9-22

Nautical miles per pound of

Crewman cargo procedures

9-24

fuel conversion chart

25-1

Electrical release

9-21

Range chart

27-1

Emergency release

9-22

Sample problem for airspeed system

In--flight procedures

9-24

correction from level flight charts

28-1

Manual release

9-22

Sample problem for climb performance,

Sideflare pattern

9-24, 9-25

single engine, 30 minute power chart

27-1

Cargo hook:

Sample problem for cruise capability,

Electrical release

2-137

time, and range chart

28-1

Emergency release

12-81

Sample problem for nautical miles per

Emergency release test

2-137

pound of fuel conversion chart

25-1

Preflight

9-22

Sample problem for use of ability to

maintain level flight,

Preoperational check

7-44

single engine chart

27-1

System

2-137

Sample problem for use of

Weight limitation

4-15

blade stall chart

22-1

Cargo pickup

9-20

Sample problem for use of density

Caution/advisory light system

2-117

altitude chart

22-1

Cautions

12-19, 12-20, 12-21

Sample problem for use of engine

Center of gravity limitations

4-15

performance, contingency (2.5 minute)

Central display unit

2-21

power, intermediate (30 minute) power

Change of controls

13-2

and maximum continuous power charts . . .

22-5

ORIGINAL

Index-4

A1-H60BB-NFM--000

Page

No.

Sample problem for use of maximum

Straightening

8-26

range, standard day chart

25-1

Tactical/combat

7-33

Sample problem for use of

Takeoff

7-32, 10-33

temperature conversion chart

22-1

Taxi

7-32, 10-32

Service ceiling

28-1

Traversing

8-11

Single/dual--engine fuel flow

25-1

VERTREP operations

7-61

Temperature conversion chart

22-1

White lighting

7-40

Torque factor chart

10-58

Chip-detector caution lights self-test

2-34

Use of charts

28-2

Circle recce

9-49

Checklist(s):

Circuit breaker numbering convention

12-6

AGM--114 Hellfire preflight

7-8

Circuit breaker panels

2-56

Aircrewman

7-41

Cirque recce

9-50

Aircrewman before landing

7-47

Cirques

9-45

Aircrewman post flight

7-49

Climb checks

10-36

Aircrewman prestart

7-41

Climb performance, dual-engine,

Aircrewman pretakeoff

7-44

30 minute power, zero wind

24-1

Alert launch

7-52

Sample problem for use of climb

APU turn--up

7-84

performance chart, dual-engine,

Automatic approach

7-52

30 minute power, zero wind

24-1

Checklist methods

19-8

Climb performance, single engine,

Engine fuel system priming

7-59

30 minute power

27-1

Fuel dump

7-59

Sample problem for climb performance,

single engine, 30 minute power chart

27-1

Functional checkflight

10-4

Climb procedures

7-90

GAU-16/A headspace adjustment

9-60

Cruise climb

7-90

GAU-16/A timing adjustment

9-61

Hot refuel

7-36

Initial climb to altitude

7-90

Maximum performance climb

7-90

Landing

7-35, 10-52

LSO console preoperational

8-10

Clock

2-116

MAD operational

7-81

Closed--book examination

20-3

Mission/weapons system

7-29, 10--31

Cockpit -- left side (area 2)

7-2

Mk 46 torpedo preflight

7-8

Cockpit -- right side (area 11)

7-7

Mk 50 torpedo preflight

7-9

Cockpit and sensor operator seats

2-129

NVD lighting

7-40

Seat adjustment

2-129

Pocket

12-6

Seat belts

2-129

Post landing

7-35, 10-52

Shoulder harness lock lever

2-129

Post launch

8-16

Cockpit fire/cabin fire

12-71

Post straightening

8-30

Cockpit interruptions and distractions

19-5

Post takeoff

7-33

Reducing human factor errors

19-5

Prelaunch

8-14

Cold--weather operations

14-1

RAST recovery

7-48

Before leaving the helicopter

14-4

Recovery

8-17

Cold--weather preflight check

14-1

Remote lasing

7-79

Engine oil system characteristics

14-2

Rig for rescue

7-60

Engine starting

14-2

Start

7-12

General

14-1

Index-5

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Cold--weather preflight check

14-1

Lighting considerations

9-40

Exterior inspection

14-1

Safety considerations during

Interior inspection

14-2

evaluation flights

20-4

Combustion section

2-1

Slope landing/takeoff considerations

11-14

Communication(s)

8-37, 15-1, 19--2

Tail rotor considerations

in low-speed flight

11-4

Control panel

15-3

Contour crawl

9-47

Hoist operator and maintenance ibs

15-14

Control(s):

Identification system

15-36

AFCS control panels

2-85

Intercommunication system

15-27

Aircraft control changes

19-8

Interference blanker

15-44

APU control and monitoring

2-47

Introduction

15-1

APU controls

2-47

Lost communication procedures

Attitude gyro control assembly

with a VERTREP load

9-29

(pilot and ATO)

16-4

Radio control panels

15-14

Automatic flight control system

2-84

Radio terminal set, AN/ARQ-44

Blade de--ice control panel

2-123

or AN/ARQ-44A

15-44

Change of

13-2

Radios

15-14

Communications control panel

15-3

Security equipment, TSEC/KG-45

15-35

Communications system control group

15-2

Speech security system

15-30

Digital electronic control unit

2-10

System control group

15-2

ECS control panel

2-121

Compass system

16-4

Engine control quadrant

2-6

Attitude gyro control assembly

16-4

Engine control system

2-6

Bearing-distance-heading indicators

16-5

Engine power control failure

12-12

Remote compass transmitters

Engine warmup and control exercise

14-3

(pilot and ATO), ML-1(MOD)

16-5

Environmental control system

2-121

Components of the navigation subsystem

16-1

Flight control servo systems

2-79

Compass system

16-4

Flight control system

2-79

Direction finder group AN/ARA-50

16-16

Flight controls and hydraulics

Navigation switching interface unit

16-1

bay (area 3)

7-3

On-top position indicator receiver

16-16

Fuel management control panel

2-45

Radar navigation set, AN/APN-217

16-9

Hover trim control panel

2-130

TACAN navigation set, AN/ARN-118(V)

16-11

Hydromechanical control unit

2-8

Compressor section

2-1

Loss of tail rotor control

12-41

Compressor stall

12-16

Loss of tail rotor control approach

Concept

20-1

and landing technique

12-39

Applicability

20-1

Loss of tail rotor control malfunctions

12-38

Conduct of flight

9-35

Mechanical control system

2-79

Conduct of the evaluation

20-3

Radio control panels

15-14

Confined area landing

7-93

RAST control panel indicators

2-109

Consecutive landing practice

Remote control unit

15-35

(RA yo--yos or free deck bounces)

8-25

Rescue hoist control panel

2-130

Considerations:

Restricted flight controls

12-39

GPS accuracy considerations

16-23

TACAN control

16-12

Landing considerations for one

Tail rotor control cable failures

12-38

or two wheel landings

9-14

Tail rotor control system

2-79

ORIGINAL

Index-6

A1-H60BB-NFM--000

Page

No.

Control mixing

2-82

Leadership

19-3

Controllable searchlight airspeed limits

4-8

Mission analysis

19-3

CONV (#1/#2) caution lights

12-61

Situational awareness

19-1

Convective

9-43

Cross--slope landing

11-15

Coordinated flight

11-6

Crossbleed start

7-83

Coupler emergencies

12-50

Crossover recce

9-49

Crew brief and preflight

19-8

Crosswind landing

7-92

Crew general responsibilities

19-6

Crowns

9-44

Dual--concurrence items

19-7

Cruise

7-90,

14-3, 14-9

Crew hover

2-100

Cruise and descent

2-13

Crew served weapon procedures

9-55

Cruise capability, time, and range

28-1

Hand signals

9-59

Sample problem for cruise capability,

M60D/M240D barrel change procedures

9-58

time, and range chart

28-1

M60D/M240D field of fire check

9-56

Cruise climb

7-90

M60D/M240D lock and load procedures

9-57

Cruise descent

7-90

M60D/M240D machine gun

9-55

CV night approaches

8-4

M60D/M240D machine gun

firing procedures

9-57

M60D/M240D rigging procedures

9-56

M60D/M240D stowing procedures

9-58

DAFCS

2-87

Voice commands

9-58

Damper failure

12-30

Crew--served weapons

12-97

Data-link antennas, AS-3273/ARQ-44

15-36

GAU-16/A emergencies

12-99

Day VERTREP operations

9-25

M60D/M240D emergencies

12-97

VERTREP safety

9-27

Crewman cargo procedures

9-24

DC bus tie system

2-55

Crewman safety belt anchor points

2-143

DC electrical system

2-54

Criteria:

DC ESS bus off caution light

12-61

Aircrew grading

20-14

De--ice:

Flight evaluation grading

20-4, 20-14

Blade de--ice control panel

2-123

Oral examination and OFT/WST

Blade de--ice system check

7-61

procedures evaluation grading

20-4

Blade de--ice system operation

2-123

Oral examination grading

20-14

Blade de--ice test panel

2-128

Pilot grading

20-4

Blade de--ice test system operation

2-128

Critical rollover

11-13

Helicopters equipped with blade

14-6

Dynamic rollover

11-13

Helicopters not equipped with blade

14-6

CRM attitude

19-4

CRM program administration

19-1

MR de--ice fail caution light

12-65

CRM skills and behaviors

19-1

MR de--ice fault caution light

12-65

Adaptability/flexibility

19-3

Rotor blade de--ice system

2-123

Assertiveness

19-2

TR de--ice fail caution light

12-65

Communication

19-2

De--ice malfunctions

12-63

CRM attitude

19-4

De--ice system caution lights

12-63

Decision making

19-2

Pwr main RTR and/or

Factors affecting CRM

19-4

pwr tail RTR light on

12-63

Index-7

ORIGINAL

A1-H60BB-NFM--000

Page

No.

De--ice system caution lights

12-63

Desert procedures

14-9

Ice detect fail caution light

12-64

Designation of pilots

10-1

Ice detected caution light

12-63

Digital electronic control unit

2-10

Left or right pitot heat caution lights

12-64

Dimensions

1-1

MR de--ice fail caution light

12-65

Direct deployment

9-15

MR de--ice fault caution light

12-65

Direction finder group AN/ARA-50

16-16

TR de--ice fail caution light

12-65

Display:

De--ice/anti-ice systems

2-122

Central display unit

2-21

De--ice master switch

2-122

Pilot display units

2-23

Engine and inlet anti--ice system

2-123

Vertical instrument display system

2-20

Pitot heater system

2-128

Division

9-31

Rotor blade de--ice system

2-123

Down--flow

9-44

Windshield anti-ice system

2-128

Down--slope landings

11-15

Windshield wiper and washer system

2-128

Drinking water container

2-143

Debriefing

6-8

Dual--concurrence items

19-7

Decision making

19-2

Dual--engine failure in flight/hover

12-22

Deck:

Dynamic rollover

11-13

Consecutive landing practice

(RA yo--yos or free deck bounces)

8-25

Deck conditions

8-4

Engine high--side failure on deck

12-14

ECS control panel

2-121

Flight/hangar deck procedures

8-1

ECS shutdown caution light on

12-20

Free deck landing

8-24

Electrical:

Helicopter on deck

3-8

AC electrical system

2-49

Unusual vibrations on deck

12-32

Cargo hook electrical release

2-137

Deck conditions

8-4

DC electrical system

2-54

DECU operation

2-11

Electrical release

9-21

Definitions

9-1, 20-1

Engine electrical system

2-10

Density altitude chart

22-1

Electrical system

2-49

Sample problem for use of density

AC bus tie system

2-54

altitude chart

22-1

AC electrical system

2-49

Descending

14-8

Circuit breaker panels

2-56

Descending flight and autorotation

11-10

DC bus tie system

2-55

Autorotational entry

11-11

DC electrical system

2-54

Autorotational recovery

11-12

Utility and test receptacles

2-65

Autorotative state

11-11

Electrical system caution lights

12-60

Vortex ring state/power settling

11-10

AC ESS bus off caution light

12-61

Descent

7-90

DC ESS bus off caution light

12-61

Autorotational descent

11-12

GEN BRG (#1/#2) caution lights

12-60

Autorotative descent

7-90

Electrical system malfunctions

12-56

Cruise descent

7-90

Battery fault caution light

12-61

Descent

7-90

Battery low charge caution light

12-62

Night/IMC descent over water

7-91

CONV (#1/#2) caution lights

12-61

Description

28-2

Electrical system caution lights

12-60

ORIGINAL

Index-8

A1-H60BB-NFM--000

Page

No.

Emergencies:

Airflow

2-5

AFCS

12-50

Alternate engine start procedures

7-83

APU

12-29

And engine inlet anti-ice limitations

4-17

Coupler

12-50

Anti--ice check

7-63

Fire

12-69

Anti--ice/start bleed valve malfunction

12-27

Bingo profile, maximum range

GAU-16/A

12-99

with dual engine

25-1

Hellfire missile

12-91

Bleed air

22-11

M60D/M240D

12-97

Chip detector

2-15

Main rotor system

12-30

Chip/engine oil pressure

Mission equipment/weapon system

12-81

low caution lights on

12-20

Simulated

19-8

Cleaning procedures

7-64

Stores

12-96

Combustion section

2-1

Torpedo

12-95

Compressor section

2-1

Emergency:

Control quadrant

2-6

Advanced helicopter emergency

External engine fire

12-69

egress lighting system

2-142

Fuel filter

2-6

APU emergency start

12-29

Fuel system

2-6

Cargo hook emergency release

12-81

Fuel system priming checklist

7-59

Cargo hook emergency release test

2-137

Gas--generator turbine

2-1

Crash position

12-77

High--side failure in flight

12-12

Equipment

2-140

High--side failure on deck

12-14

Helicopter emergency egress

Idle limits with gust lock engaged

4-6

lighting system

2-142

Inlet air flow

2-1

HIFR emergency procedures

8-38

Inlet anti--ice valve

2-17

Individual helicopter emergency

Inlet particle separator

2-1

egress lighting system

2-142

Inlet section

2-1

Locator transmitter systems

2-140

Internal engine fire

12-70

Panel

2-137

Limits

4-6

Release

9-22

Low--side failure in flight

12-14

RAST cable emergency release

12-83

Main frame and accessory section

2-5

Malfunction during hover/takeoff

12-21

Survival and emergency equipment

2-140

Malfunction in flight

12-12

Emergency locator transmitter systems

2-140

Maximum gross weight to

Emergency panel

2-137

hover in ground effect, single engine

27-1

Emergency release

9-22

Oil circulation through

Emitter hazard and standoff distances

4-15

the engine scroll vanes

2-19

Emitter hazards

8-31

Oil servicing

3-11

Eng inlet anti--ice on (#1/#2)

Oil system characteristics

14-2

advisory light on

12-28

Performance charts

22-5

Engagement

7-57

Performance, contingency (2.5 minute)

Engine

2-1

power chart

22-5

Ability to maintain level flight,

Performance, intermediate (30 minute)

single engine chart

27-1

power chart

22-5

Advisories

12-27

Performance, maximum

Air restart

12-24

continuous power chart

22-5

Index-9

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Engine (cont):

Hydromechanical control unit

2-8

Power turbine

2-5

Inputs to the HMU

2-8

Sample problem for maximum gross weight

Load demand system

2-6

to hover in ground effect, single engine . . .

27-2

Overspeed and drain valve

2-10

Sample problem for use of ability to

Engine electrical system

2-10

maintain level flight,

Alternator

2-10

single engine chart

27-1

DECU operation

2-11

Sample problem for use of engine

Digital electronic control unit

2-10

performance, contingency (2.5 minute)

Ignition system

2-12

power, intermediate (30 minute) power

Engine high speed shaft failure

12-16

and maximum continuous power charts . . .

22-5

Load demand system malfunction

12-17

Shutdown

14-9

Engine instruments

2-20

Shutdown in flight

12-24

Vertical instrument display system

2-20

Start and rotor engagement

8-2

Engine malfunctions

12-11

Start limits

4-6

Engine caution lights

12-19

Start, APU

2-16

Engine high speed shaft failure

12-16

Start, crossbleed

2-16

Engine malfunction in flight

12-12

Starter #1 or #2 advisory light on

12-28

Engine power control failure

12-12

Starter limits

4-6

Engine oil system

2-13

Starting

14-2, 14-9

Engine chip detector

2-15

Temperature limitations

4-6

Oil cooler

2-15

Torque or TGT spiking/fluctuations

12-15

Oil filter

2-15

Warmup and control exercise

14-3

Oil supply and scavenge system

2-15

Engine advisories

12-27

Oil tank

2-13

Eng inlet anti--ice on (#1/#2)

Engine oil temperature high

12-19

advisory light on

12-28

Abort start

12-21

Engine anti--ice/start bleed

Autorotation

12-22

valve malfunction

12-27

Dual--engine failure in flight/hover

12-22

Engine starter #1 or #2

Engine advisories

12-27

advisory light on

12-28

Engine air restart

12-24

Engine and inlet anti--ice system

2-16, 2-123

Engine malfunction

Engine anti--ice/start bleed valve

2-16

during hover/takeoff

12-21

Engine inlet anti--ice valve

2-17

Engine shutdown in flight

12-24

Engine oil circulation through

Single--engine failure

12-23

the engine scroll vanes

2-19

Single-engine landing

12-25

Engine caution lights

12-19

Engine operation summary

2-13

ECS shutdown caution light on

12-20

Cruise and descent

2-13

Engine chip/engine oil pressure

Starting and ground idle

2-13

low caution lights on

12-20

Summary

2-13

Engine control system

2-6

Takeoff and climb

2-13

Engine control quadrant

2-6

Engine parameter sensing

2-19

Engine fuel filter

2-6

N_g sensing

2-19

Engine fuel system

2-6

N_p and torque sensing

2-19

Engine-driven fuel boost pump

2-6

N_p sensing

2-19

HMU operation

2-9

TGT sensing

2-19

ORIGINAL

Index-10

A1-H60BB-NFM--000

Page

No.

Engine performance

22-5

Environmental restrictions

4-17

Torque factor sample problem

22-11

APU operating limitations

4-17

Backup hydraulic pump hot

Engine performance procedures

22-5

weather limitations

4-17

Engine bleed air

22-11

Engine and engine inlet

Maximum power check

22-5

anti-ice limitations

4-17

Torque factor method

22-5

Temperature limitations

4-17

Engine power checks

10-57

Equipment:

Maximum power check chart

10-57

Emergency

2-140

Sample problem 1

10-59

Litter installation

2-143

Sample problem 2

10-59

Minimum

4-16

Torque factor chart

10-58

Minimum equipment for passengers

4-16

Torque factor procedure

10-58

Miscellaneous

2-143

Torque factor procedure in flight

10-58

Personal flying equipment requirements

5-7

Torque factor terms

10-57

SAR

9-1

Torque factor TGT reference

10-58

Survival

2-140

Survival and emergency

2-140

Engine power control failure

12-12

Evaluation:

Engine high--side failure in flight

12-12

Conduct of the

20-3

Engine high--side failure on deck

12-14

Flight

20-3, 20-5

Engine low--side failure in flight

12-14

Flight evaluation grade determination

20-21

Engine start system

2-15

Flight evaluation grading criteria . . .

20-4, 20-14

Engine start, APU

2-16

Ground

20-2

Engine start, crossbleed

2-16

Landing site evaluation brief

9-41

Engine starting

14-2, 14-9

NATOPS evaluation forms

20-22

Cruise

14-3

OFT/WST

20-5

Engine warmup and control exercise

14-3

OFT/WST procedures

20-3

Landing

14-4

Oral

20-3

Takeoff

14-3

Oral examination and OFT/WST

Taxiing

14-3

procedures evaluation (if conducted)

20-3

Engine-driven fuel boost pump

2-6

Oral examination and OFT/WST

procedures evaluation grading criteria

20-4

Engine/APU boost/fuel prime system

2-39

Safety considerations during

Engine/APU fire-extinguishing system

2-118

evaluation flights

20-4

Fire-extinguishing system,

Examination:

impact switch operation

2-121

Closed--book

20-3

Engine/inlet anti--icing

14-5

Open--book

20-2, 20-3

Engines:

Oral

20-5

Starting APU and engines

7-57

Oral examination and OFT/WST

Starting engines and

procedures evaluation (if conducted)

20-3

rotor engagement

7-21, 10-13

Oral examination and OFT/WST

The engines

1-4

procedures evaluation grading criteria

20-4

Entrance and egress

2-121

Oral examination grading criteria

20-14

Environmental control system

2-121

Exceeding operational limits

4-1

Avionics cooling

2-122

Excess tail rotor thrust

12-40

ECS control panel

2-121

Explanation of terms

12-6

Index-11

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Exterior arrangement

1-4

FCF record cards

10-2

Exterior inspection

14-1

Figure eight recce

9-48

Exterior lighting

2-65

Final grade determination

20-22

Anticollision lights

2-65

Fire:

Landing/hover lights

2-66

APU fire

12-70

Position lights

2-65

Cockpit fire/cabin fire

12-71

Fire emergencies

12-69

Recovery assist secure and

traverse lights

2-66

Fire extinguisher system servicing

3-14

Rotor head light

2-66

Internal engine fire

12-70

Searchlight

2-65

M60D/M240D field of fire check

9-56

External engine fire

12-69

Fire emergencies

12-69

External power requirements

3-14

APU fire

12-70

Cockpit fire/cabin fire

12-71

External tank jettison

2-47

Emergency crash position

12-77

External engine fire

12-69

Factors affecting CRM

19-4

Immediate landing/ditching

12-73

Factors affecting range and endurance

21-1

Immediate landing/ditching

Factors increasing the likelihood of

(aircrewmen)

12-79

loss of tail rotor effectiveness

11-4

Immediate landing/ditching (pilot)

12-78

Failure(s):

Internal engine fire

12-70

Damper

12-30

Lost aircraft procedures

12-79

Dual--engine failure in flight/hover

12-22

Planned ditching

12-77

Engine high speed shaft

12-16

Smoke and fumes elimination

12-72

Engine high--side failure in flight

12-12

Sonobuoy lithium battery venting

12-72

Engine high--side failure on deck

12-14

Underwater egress

12-80

Engine low--side failure in flight

12-14

Fire-detection system

2-117

Engine power control

12-12

Fire extinguisher system servicing

3-14

M60D/M240D failure to

Fire-extinguishing system,

fire/jammed gun

12-98

impact switch operation

2-121

MAD reel failure with towed

Five-step sequence

19-4

body deployed

12-86

Flashing AFCS degraded caution light

12-52

Minimum height for safe landing

Flashing AFCS degraded caution light

after single- or dual-engine

4-8

with alt fail advisory light on

12-53

Practice single--engine failure in

Flight:

an HOGE (cut and run/cut gun)

7-95

Automatic flight control system

2-84

RAST main probe messenger

12-81

Checks

10-37

Rescue hoist

12-88

Stabilator auto mode

12-54

Conduct of

9-35

Stabilator indicating system

12-56

Control servo systems

2-79

Tail rotor control cable

12-38

Control system

2-79

Tail rotor servo

12-38

Controls and hydraulics bay (area 3)

7-3

Fault:

Coordinated

11-6

Aux fuel xfer fault caution light

12-67

Descending flight and autorotation

11-10

Battery fault caution light

12-61

Engine high--side failure in

12-12

MR de--ice fault caution light

12-65

Engine low--side failure in

12-14

FCF profile

10-2

Engine malfunction in

12-12

ORIGINAL

Index-12

A1-H60BB-NFM--000

Page

No.

Engine shutdown in

12-24

Flight in instrument

Evaluation

20-3, 20-5

meteorological conditions

4-16

Minimum aircraft equipment for

Evaluation grade determination

20-21

night or IMC flight over land

4-16

Evaluation grading criteria

20-4, 20-14

Minimum aircraft equipment for

Forward

11-2

night or IMC flight over water

4-17

General flight characteristics

11-1

Flight instruments

2-112

In flight power available check

9-46

Miscellaneous flight instruments

2-116

Instrument

5-7

Pitot static system

2-112

Instrument and console lights

2-66

Radar altimeter, AN/APN-194

2-113

Instrument flight conditions in formation . . .

9-36

Flight scheduling

7-1

Instrument flight procedures

13-1

Flight with external loads

9-20, 11-18

Level flight performance charts

28-2

Flight/form/division lead

9-35

Maneuvering

11-6

Flight/hangar deck procedures

8-1

Blade/pylon/stabilator

Maneuvering flight characteristics

11-6

folding and spreading

8-2

Miscellaneous flight instruments

2-116

Engine start and rotor engagement

8-2

Post flight checks

7-40, 10-57

General safety precautions

8-2

Restricted flight controls

12-39

Movement of helicopter

8-1

Scheduling

7-1

Flightcrew ground training

5-6

Sideward and rearward

7-89

Flightcrew qualifications

5-1

Slow-speed

11-2

Qualifications

5-1

Tail rotor considerations in low-speed

11-4

Waiver of requirements

5-1

Tail rotor spar loads in maneuvering

11-7

Flights from air--capable ships

5-7

Tail winds in transition to forward

11-2

FLIR uncommanded lasing

12-95

Torque factor procedure in

10-58

Flying:

Transition to forward

11-2

Mountain terrain

9-41

Unusual vibrations in

12-31

Terrain

9-39

With external loads

9-20, 11-18

Formation composition

9-31

Division

9-31

WOW advisory light on in

12-91

Section

9-31

Flight control servo systems

2-79

Formation flying

9-30

Control mixing

2-82

Conduct of flight

9-35

Pilot assist servos

2-82

Formation composition

9-31

Tail rotor servo

2-79

General

9-30

Flight control system

2-79

Instrument flight conditions in formation . . .

9-36

Automatic flight control system

2-84

Lead change

9-35

Flight control servo systems

2-79

Night formation

9-35

Mechanical control system

2-79

Rendezvous

9-31

Stability augmentation system

2-92

Responsibility

9-35

Flight evaluation

20-3, 20-5

Forward flight

11-2

Conduct of the evaluation

20-3

Four principles of application

19-5

Flight evaluation grading criteria

20-4

Four-per-revolution (17.2 hz)

11-19

Safety considerations during

Free cruise

9-31

evaluation flights

20-4

Free deck landing

8-24

Index-13

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Fuel:

Fuel system caution lights

12-66

Auxiliary fuel tanks

2-46

Aux fuel xfer fault caution light

12-67

Engine fuel filter

2-6

Fuel low caution lights

12-67

Engine fuel system

2-6

Pump/valve fail caution light

12-67

Engine fuel system priming checklist

7-59

Fuel system malfunctions

12-66

Dump checklist

7-59

Fuel system caution lights

12-66

Dump system

2-39

No HIFR/stuck main tank shutoff valve

12-68

Fueling with fuel susceptible to icing

3-7

Refueling hose jettison

12-68

Low caution lights

12-67

Uncommanded fuel dumping

12-69

Low level warning system

2-39

Fuel system servicing

3-1

Main fuel supply operation

2-36

Fueling with fuel susceptible to icing

3-7

Main tanks fuel quantity system

2-39

Gravity fueling

3-10

Management control panel

2-45

Pressure refueling

3-8

Manual fuel transfer check

2-46

Nautical miles per pound of

RAST operations for aircraft configured

fuel conversion chart

25-1

with external auxiliary fuel tank

3-10

Prime system operation

2-39

Use of different fuels

3-10

RAST operations for aircraft configured

Fuel transfer system

2-46

with external auxiliary fuel tank

3-10

Fueling:

Sample problem for nautical miles

Fueling with fuel susceptible to icing

3-7

per pound of fuel conversion chart

25-1

Gravity fueling

3-10

Selector levers

2-36

Functional checkflight

10-1

Single/dual-engine fuel flow

25-1

Designation of pilots

10-1

System

2-36

FCF profile

10-2

System caution lights

12-66

FCF record cards

10-2

System malfunctions

12-66

General information

10-1

System servicing

3-1

Ground checks

10-1

Transfer system

2-46

Limited FCF

10-3

Uncommanded fuel dumping

12-69

Fuel dump checklist

7-59

Special instructions

10-2

Fuel dump system

2-39

Functional checkflight charts and tables

10-60

System operation

2-40

Functional checkflight checklist

10-4

System operation (with FMCP)

2-40

Climb checks

10-36

Fuel low caution lights

12-67

Flight checks

10-37

Fuel low level warning system

2-39

Hover checks

10-34

Fuel management control panel

2-45

Landing checklist

10-52

Fuel prime system operation

2-39

Mission/weapons systems checklist

10-31

Fuel selector levers

2-36

Post flight checks

10-57

Fuel system

2-36

Post landing checklist

10-52

Auxiliary fuel system

2-45

Post takeoff checks

10-36

External tank jettison

2-47

Preflight check

10-4

Fuel dump system

2-39

Shutdown

10-53

Main fuel supply operation

2-36

Main tanks fuel quantity system

2-39

Start checks

10-4

Single-point pressure refueling system

2-40

Starting engines and rotor engagement

10-13

ORIGINAL

Index-14

A1-H60BB-NFM--000

Page

No.

Systems check

10-7

Global positioning system

16-17

Takeoff checklist

10-33

Navigation modes

16-17

Taxi checklist

10-32

GPS accuracy considerations

16-23

Fuselage -- left side (area 5)

7-5

Runoff error avoidance

16-23

Fuselage -- right side (area 10)

7-7

GPS data table

16-22

Fuselage stations and jack points

3-19

GPS options

16-20

Grading instructions

20-3

Closed--book examination

20-3

Open--book examination

20-3

G-loading in turns

11-8

Oral examination and OFT/WST

procedures evaluation (if conducted)

20-3

Gas--generator turbine

2-1

Gravity fueling

3-10

GAU--16/A clear weapon

procedures

9--63, 12-101

Gravity refueling

2-42

Ground:

GAU--16/A cook--off

12-99

Aircrewman ground training

5-6

GAU-16/A emergencies

12-99

Evaluation

20-2

AN/PEQ-3 uncommanded lasing

12-101

Flightcrew ground training

5-6

GAU-16/A firing procedures

9-62

One-per-revolution

11-19

GAU-16/A headspace adjustment

9-59

Resonance

11-19, 12-30

Definition

9-59

Training requirements

5-6

GAU-16/A headspace adjustment checklist . . .

9-60

Ground checks

10-1

GAU--16/A jammed gun

12-99

Ground effect

11-1

GAU-16/A lock and load procedures

9-62

Ground evaluation

20-2

GAU-16/A machine gun

9-59

Closed--book examination

20-3

GAU-16/A rigging procedures

9-61

Grading instructions

20-3

GAU--16/A runaway gun

12-100

OFT/WST procedures evaluation

20-3

GAU-16/A timing adjustment

9-60

Open--book examination

20-2

GAU-16/A timing adjustment checklist

9-61

Oral evaluation

20-3

GEN BRG(#1/#2) caution lights

12-60

Ground one-per-revolution

11-19

General

4-1, 7-1, 8-1, 8-32, 9-30, 9-39, 14-1

Ground resonance

11-19, 12-30

General arrangement

1-4

Ground training requirements

5-6

Exterior arrangement

1-4

Aircrewman ground training

5-6

Interior arrangement

1-5

Flightcrew ground training

5-6

General briefing

6-1

Guidelines

9-51

General flight characteristics

11-1

Gunner brief

6-7

Forward flight

11-2

Gust lock

12-33

Hover/slow speed flight

(at or below translational lift)

11-1

Slow-speed flight

11-2

H--60 pilot qualified in model

5-1

General information

10-1

Hand pump reservoir servicing

3-12

General safety precautions

8-2

Hand signals

9-59

General shipboard operations

8-1

Heading hold

2-96

Flight/hangar deck procedures

8-1

Health indicator test check

7-50

Visual landing aids

8-3

Helicopter emergency egress

Generator, APU generator caution light on . . .

12-29

lighting system

2-142

Index-15

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Helicopter in--flight refueling

8-32

Preflight inspection

14-9

Communications

8-37

Takeoff

14-9

General

8-32

Taxi

14-9

Night HIFR procedures

8-38

Hover augmentation/gust alleviation

2-96

Normal operations

8-34

Hover charts

23-1

Helicopter on deck

3-8

Indicated torque required to hover

Helicopter vibration

11-18

10 feet in ground effect

23-1

Ground resonance

11-19

Indicated torque required to hover out

Main rotor specific vibrations

11-18

of ground effect

23-1

Tail rotor specific vibrations

11-20

Maximum gross weight to hover out

Helicopters equipped with blade de--ice

14-6

of ground effect

23-2

Helicopters not equipped with blade de--ice

14-6

Maximum gross weight to hover,

Hellfire missile aborted launch

12-91

headwind or ground effect influence

23-1

Hellfire missile emergencies

12-91

Hover checks

10-34

Hellfire missile hangfire

12-92

Hover coupler

2-98

Hellfire missile misfire

12-94

Hover endurance, out of ground effect

26-1

Hellfire missile unlatched

12-95

Sample problem for hover endurance,

HF radio

15-26

out of ground effect

26-1

Control panel

15-28, 15-29

Hover trim control panel

2-130

HF radio operation

15-26

Hover/air taxi

11-4

HF test

15-27

Hover/slow speed flight (at or below

HIFR emergency procedures

8-38

translational lift)

11-1

HIFR procedure

8-35

Blowback

11-2

HIFR refueling system

2-42

Ground effect

11-1

HIFR systems

8-32

Transition to forward flight

11-2

NATO--compatible high capacity

Hovering

4-12

HIFR rig

8-32

Hovering turns

7-88

Wiggins/North Island HIFR rig

8-32

Hung droop stop(s)

12-33

High AOB (high-G) maneuvering effects

Hung sonobuoy/SLC

12-96

on lateral cg margin

11-9

Hung torpedo

12-95

High AOB turns

11-7

Hydraulic leak test

2-76

HMU operation

2-9

Hydraulic leak-detection/isolation

Hoist auxiliary cooling

2-136

(LDI) system

2-75

Hoist cable shear

2-136

Logic modules

2-75

Hoist operation

2-133

Reservoir fill system

2-76

Hoist operator and maintenance IBS

15-14

Hydraulic pump modules

2-73

Hot refuel checklist

7-36

Backup hydraulic system

2-73

Hot weather and desert operations

14-8

NO. 1 hydraulic system

2-73

Cruise

14-9

NO. 2 hydraulic system

2-73

Desert procedures

14-9

Engine shutdown

14-9

Hydraulic system malfunctions

12-42

Engine starting

14-9

Backup HYD pump fails to operate

12-49

Landing

14-9

Boost servo hardover

12-50

Postflight inspection

14-9

Hydraulic system caution lights

12-43

ORIGINAL

Index-16

A1-H60BB-NFM--000

Page

No.

NO. 1 hydraulic system malfunction

12-44

Indicated torque required to hover

NO. 2 hydraulic system malfunction

12-46

out of ground effect

23-1

Sample problem for use of indicated

Hydraulic system servicing

3-12

torque required to hover out of

Hand pump reservoir servicing

3-12

ground effect

23-1

Hydraulic systems

2-68

Indicator(s):

Hydraulic pump modules

2-73

Airspeed

2-112

Primary servo shutoff

2-75

Attitude

2-113

Transfer modules

2-74

Bearing--distance--heading

16-5

Hydromechanical control unit

2-8

Health indicator test check

7-50

On-top position indicator receiver

16-16

Outside air-temperature indicator

2-116

Pressure indicator

2-26

Ice detect fail caution light

12-64

RAST control panel indicators

2-109

Ice detected caution light

12-63

Vertical speed indicators

2-113

Ice precautions

14-5

Individual helicopter emergency egress

Engine/inlet anti--icing

14-5

lighting system

2-142

Initial climb to altitude

7-90

Helicopters equipped with blade de--ice

14-6

Initial shipboard landing qualification

5-3

Helicopters not equipped with

Initial VERTREP qualification

5-4

blade de--ice

14-6

Ice rate detector

14-6

Inlet air flow

2-1

Inlet particle separator

2-1

Pitot--static tube heater

14-7

Inlet section

2-1

Ice rate detector

14-6

Input module

2-30

Identification system

15-36

Input module chip caution lights on

12-36

Transponder computer,

Inputs to the HMU

2-8

KIT-1 TSEC series

15-40

Inspection:

IFF flashing caution

12-90

Cabin

7-10

IFF interrogator

15-42

Exterior

14-1

IFF transponder

15-36

Interior

14-2

Ignition system

2-12

Postflight

14-9

Illusions

9-42

Preflight

14-9

Immediate landing/ditching

12-73

Instrument approach

8-7

Immediate landing/ditching (aircrewmen)

12-79

Instrument approach procedure

13-1

Immediate landing/ditching (pilot)

12-78

Change of controls

13-2

Implementation

20-1

Change of scans

13-2

NATOPS evaluator

20-1

Instrument climbs and descents

13-1

NATOPS instructor

20-1

Instrument crew coordination

13-1

In flight power available check

9-46

Instrument climbs and descents

13-1

In-flight confidence test

16-16

Instrument flight

5-7

In--flight procedures

9-24

Instrument flight conditions in formation

9-36

In turbulent air

14-8

Inadvertent IMC procedures

9-36

Inadvertent IMC procedures

9-36

Instrument flight procedures

13-1

Indicated torque required to hover

Instrument range markings

4-1

10 feet in ground effect

23-1

Instrument takeoff

13-1

Index-17

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Instruments:

No--hover

7-93

Engine instruments

2-20

Post landing checklist

7-35, 10-52

Flight instruments

2-112

Running

7-92

Miscellaneous flight instruments

2-116

Tail landing gear

2-106

Insufficient tail rotor thrust

12-39

Unprepared site landing

7-93

Intercommunication system

15-27

Up--slope landings

11-15

Interference blanker

15-44

Vertical landing from a hover

7-92

Interior arrangement

1-5

Visual landing aids

8-3

Interior inspection

14-2

Landing checklist

7-35, 10-52

Interior lighting

2-66

Landing considerations for one or two

wheel landings

9-14

Cabin dome lights

2-68

Landing gear

2-105

Flight instrument and console lights

2-66

Main landing gear

2-105

Secondary lights

2-67

Tail landing gear

2-106

Thunderstorm utility lights

2-67

Landing limitations

4-15

Utility lights

2-67

Landing safety officer

5-4

Intermediate and tail gearbox chip/

LSO currency/requalification

5-4

temperature systems

2-34

LSO initial qualifications

5-4

Intermediate gearbox

2-33

LSO instruction

5-4

Internal engine fire

12-70

Special mission/lookout non-aircrewman

Interrogator computer, KIR-1/TSEC

15-43

initial qualification

5-5

Introduction

8-1, 9-1,

12-5, 15-1,

Landing site evaluation brief

9-41

16-1, 19-1, 21-1

Aircraft performance

9-45

Guidelines

9-51

Illusions

9-42

Jettison:

Mountain flying procedures and

techniques

9-46

External tank jettison

2-47

RAST messenger jettison

12-82

Mountain takeoff and departure

9-51

Refueling hose jettison (HIFR)

12-68

Mountain winds, turbulence and

topography

9-42

Selective jettison of M299 launcher

12-96

Standard mountain approach and

landing

9-50

Landing to effect a rescue

9-13

Landing transition

8-8

Katabatic

9-43

Landing/hover lights

2-66

Launch:

Alert launch checklist

7-52

Land--sea breezes

9-43

Hellfire missile aborted launch

12-91

Landing

14-4, 14-9

Post launch checklist

8-16

Approach to

7-91

Launch and recovery signals

8-3

Confined area

7-93

Launch procedures

8-15

Cross--slope

11-15

Launch/JETT fail caution light on

12-97

Crosswind

7-92

Lead change

9-35

Down--slope

11-15

Leadership

19-3

Free deck

8-24

Ledges

9-44

ORIGINAL

Index-18

A1-H60BB-NFM--000

Page

No.

Left or right pitot heat caution lights

12-64

Input module chip caution lights on

12-36

Left or right rack fan caution light on

12-90

Landing/hover lights

2-66

Level flight performance charts

28-2

Launch/JETT fail caution light on

12-97

Description

28-2

Left or right pitot heat caution lights

12-64

Use of charts

28-2

Left or right rack fan caution light on

12-90

Light(s):

Main rotor system caution/

advisory lights

12-33

AC ESS bus off caution

12-61

Main rotor warning

12-33

AFCS caution lights

12-52

Master caution

12-6

AFCS degraded caution light on

12-52

Miscellaneous caution/advisory lights

12-90

AFCS fail advisory lights

12-52

MR de--ice fail caution

12-65

Anticollision lights

2-65

MR de--ice fault caution

12-65

APU caution lights

12-29

Position lights

2-65

APU fail caution light on

12-29

Pump/valve fail caution

12-67

APU generator caution light on

12-29

PWR main RTR and/or PWR

APU oil TEMP HI caution light on

12-30

tail RTR light on

12-63

AUX fuel XFER fault caution light

12-67

Recovery assist secure and traverse lights . . .

2-66

Backup RSVR low caution light on

12-44

Rotor brake advisory light on

12-34

Battery fault caution

12-61

Rotor head

2-66

Battery low charge caution

12-62

SAS caution light on

12-53

Cabin dome lights

2-68

Secondary lights

2-67

Caution/advisory light system

2-117

Spread incomplete

12-34

Chip-detector caution lights self-test

2-34

Tail rotor quadrant caution light on

12-42

CONV (#1/#2) caution lights

12-61

Tail RTR servo leak without

De--ice system caution lights

12-63

#1 RSVR low caution

12-46

DC ESS bus off caution

12-61

Thunderstorm utility

2-67

ECS shutdown caution light on

12-20

TR de--ice fail caution

12-65

Electrical system caution lights

12-60

Utility

2-67

ENG inlet anti--ice on (#1/#2)

WOW advisory light on in flight

12-91

advisory light on

12-28

Lighting

2-65, 9-28

Engine caution lights

12-19

Advanced helicopter emergency

Engine chip/engine oil pressure low

egress lighting system

2-142

caution lights on

12-20

Exterior

2-65

Engine starter #1 or #2 advisory

Helicopter emergency egress

light on

12-28

lighting system

2-142

Flashing AFCS degraded caution

12-52

Individual helicopter emergency

Flashing AFCS degraded caution light

egress lighting system

2-142

with ALT fail advisory light on

12-53

Interior

2-66

Flight instrument and console lights

2-66

NVD lighting checklist

7-40

Fuel low caution lights

12-67

White lighting checklist

7-40

Fuel system caution lights

12-66

Lighting considerations

9-40

GEN BRG (#1/#2) caution lights

12-60

Limitation(s):

Hydraulic system caution lights

12-43

Aerodynamic

4-8

Ice detect fail caution

12-64

Altitude

4-12

Ice detected caution

12-63

APU operating

4-17

Index-19

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Limitation(s) (cont):

Lookout procedures

13-2

Backup hydraulic pump hot weather

4-17

Loss of tail rotor authority

11-4

Bank angles

4-12

Loss of tail rotor control

12-41

Cargo hook weight

4-15

Loss of tail rotor control approach and

landing technique

12-39

Center of gravity

4-15

Loss of tail rotor control malfunctions

12-38

Engine and engine inlet anti-ice

4-17

Engine temperature

4-6

Excess tail rotor thrust

12-40

Insufficient tail rotor thrust

12-39

Landing

4-15

Loss of tail rotor control

12-41

Main transmission module

4-6

Loss of tail rotor control approach

Maneuvering

4-12

and landing technique

12-39

Rescue hoist weight

4-16

Restricted flight controls

12-39

Shipboard launch/recovery

8-3, 8-6

Tail rotor control cable failures

12-38

Shipboard wind

4-15

Tail rotor servo failures

12-38

System

4-6

Loss of tail rotor drive

12-36

Temperature

4-17

Loss of tail rotor drive altitude and

Transmission oil pressure

4-7

airspeed not sufficient to establish

Weight

4-15

autorotation

12-38

Limitations for maneuvering with rescue

Loss of tail rotor drive altitude and

hoist loads

4-12

airspeed sufficient to establish

Limitations for maneuvering with

autorotation

12-37

sling loads

4-12

Loss of tail rotor drive altitude and airspeed

Limited FCF

10-3

not sufficient to establish autorotation

12-38

Limits:

Loss of tail rotor drive altitude and airspeed

Airspeed operating

4-8

sufficient to establish autorotation

12-37

Controllable searchlight airspeed

4-8

Loss of tail rotor effectiveness

11-4

Engine

4-6

Loss of translational lift

11-4

Engine idle limits with gust lock engaged . . .

4-6

Lost aircraft procedures (open ocean)

12-79

Engine start

4-6

Lost communication procedures

Engine starter

4-6

with a VERTREP load

9-29

Exceeding operational

4-1

Lost wingman VMC

9-36

MAD reeling machine operating

4-14

Low rotor RPM

12-33

Miscellaneous

4-14

LSO console preoperational checklist

8-10

LSO currency/requalification

5-4

Rotor brake operating

4-15

LSO initial qualifications

5-4

Rotor start and stop

4-7

LSO instruction

5-4

Transmission and rotor

4-6

Weight

4-15

Line operations

7-1

Litter installation equipment

2-143

M60D/M240D aircraft preparation/

Litter platform setup procedures

7-60

inspection

9-55

Load demand system

2-6

M60D/M240D barrel change procedures

9-58

Load demand system malfunction

12-17

M60D/M240D clear weapon procedures

12-99

Local mountain winds

9-43

M60D/M240D cook--off

12-97

Local winds

9-43

M60D/M240D emergencies

12-97

Logic modules

2-75

M60D/M240D failure to fire/jammed gun

12-98

ORIGINAL

Index-20

A1-H60BB-NFM--000

Page

No.

M60D/M240D field of fire check

9-56

Main rotor system emergencies

12-30

M60D/M240D lock and load procedures

9-57

Hung droop stop(s)

12-33

Main rotor system caution/

M60D/M240D machine gun

9-55

advisory lights

12-33

M60D/M240D machine gun firing

Main rotor warning light

12-33

procedures

9-57

Unusual vibrations

12-30

M60D/M240D rigging procedures

9-56

Main rotor tiedown

3-19

M60D/M240D runaway gun

12-98

Main rotor vertical 4/rev vibration cueing

11-7

M60D/M240D stowing procedures

9-58

Main rotor warning light

12-33

MAD altitude compensation procedure

7-82

Low rotor RPM

12-33

MAD deployment

7-81

Main rotor/transmission/APU/

MAD operational checklists

7-81

engines (area 4)

7-4

MAD reel failure with towed body

Main tanks fuel quantity system

2-39

deployed

12-86

Fuel low level warning system

2-39

MAD reeling machine operating limits

4-14

Main transmission

2-30

Accessory module

2-33

MAD retrieval

7-82

Input module

2-30

Main frame and accessory section

2-5

Main transmission lubrication system

2-33

Main fuel supply operation

2-36

Main transmission malfunction

12-35

Engine/APU boost/fuel prime system

2-39

Main transmission module limitations

4-6

Fuel selector levers

2-36

Main transmission oil system servicing

3-11

Main gearbox vibrations

2-34

Malfunctions:

Main landing gear

2-105

Engine

12-13, 12-14, 12-16,

Wheel brake system

2-106

12-17, 12-18, 12-21,

Main RAST probe

2-112

12-23, 12-24, 12-25

Engine malfunction in flight

12-12

Main rotor blade

2-24

Single--engine failure

12-23

Main rotor disk vortex

Maneuvering flight

11-6

(280° to 330° relative)

11-6

Coordinated flight

11-6

Main rotor flapping margin

11-7

G-loading in turns

11-8

Main rotor gust lock

2-30

High AOB (high-G) maneuvering

Main rotor head

2-24

effects on lateral cg margin

11-9

Main rotor RPM-indicating system

2-27

High AOB turns

11-7

Main rotor specific vibrations

11-18

Main rotor flapping margin

11-7

Four-per-revolution (17.2 Hz)

11-19

Main rotor vertical 4/Rev vibration cueing

11-7

Ground one-per-revolution

11-19

Maneuvering flight characteristics

11-6

One-per-revolution (4.3 Hz)

11-18

Power required exceeds power available . . .

11-10

One-per-revolution (6.5 Hz)

11-19

Rolling pullouts

11-8

Tail rotor spar loads in maneuvering

Main rotor system

2-23

flight

11-7

Main rotor blade

2-24

Maneuvering flight characteristics

11-6

Main rotor head

2-24

Maneuvering limitations

4-12

Main rotor system caution/advisory lights . . .

12-33

Altitude limitation

4-12

Gust lock

12-33

Bank angles limitation

4-12

Rotor brake advisory light on

12-34

Hovering

4-12

Rotor overspeed

12-34

Limitations for maneuvering with

Spread incomplete light

12-34

rescue hoist loads

4-12

Index-21

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Maneuvering limitations (cont):

Minimum equipment

4-16

Limitations for maneuvering

Flight in instrument meteorological

with sling loads

4-12

conditions

4-16

Prohibited maneuvers

4-12

Minimum aircraft equipment for flights

Maneuvering stability

2-97

into forecast or known icing conditions . . .

4-16

Manual fuel transfer check

2-46

Minimum equipment for passengers

4-16

Manual release

9-22

Minimum flightcrew requirements

5-6

Manual sonobuoy launching

7-68

Flights from air--capable ships

5-7

Instrument flight

5-7

Master caution light

12-6

SUW/ASW operational missions

5-7

Master warning system

2-116

Minimum height for safe landing after

Maximum gross weight takeoff

7-89

single- or dual-engine failure

4-8

Maximum gross weight to hover in

Minimum pilot currency requirements

5-2

ground effect, single engine

27-1

Pilot currency requirements

5-2

Sample problem for maximum gross

weight to hover in ground effect,

Miscellaneous caution/advisory lights

12-90

single engine

27-2

FLIR uncommanded lasing

12-95

Maximum gross weight to hover

Hellfire missile aborted launch

12-91

out of ground effect

23-2

Hellfire missile emergencies

12-91

Sample problem for use of maximum

IFF flashing caution

12-90

gross weight to hover,

Left or right rack fan caution light on

12-90

out of ground effect

23-2

Stores emergencies

12-96

Maximum gross weight to hover,

Torpedo emergencies

12-95

headwind or ground effect influence

23-1

WOW advisory light on in flight

12-91

Sample problem for use of maximum

Miscellaneous equipment

2-143

gross weight to hover, headwind or

Crewman safety belt anchor points

2-143

ground effect influence

23-1

Drinking water container

2-143

Maximum performance climb

7-90

Litter installation equipment

2-143

Maximum performance takeoffs

7-89

Rearview mirrors

2-143

Maximum power check

22-5

Miscellaneous flight instruments

2-116

Maximum power check chart

10-57

Clock

2-116

Maximum range, standard day chart

25-1

Outside air-temperature (OAT) indicator . . .

2-116

Sample problem for use of maximum

Standby magnetic compass

2-116

range, standard day chart

25-1

Miscellaneous limits

4-14

Mechanical

9-43

Blade, pylon/stabilator fold or spread

4-15

Mechanical control system

2-79

Emitter hazard and standoff distances

4-15

Tail rotor control system

2-79

Landing limitations

4-15

Methods of eliminating roughness

caused by blade stall

11-3

MAD reeling machine operating limits

4-14

Minimizing errors

19-1

Rotor brake operating limits

4-15

Minimum aircraft equipment for flights

Shipboard wind limitations

4-15

into forecast or known icing conditions

4-16

Mission analysis

19-3

Minimum aircraft equipment for night or

Mission equipment/weapon system

IMC flight over land

4-16

emergencies

12-81

Minimum aircraft equipment for night or

ASQ--81 towed body down limit switch

IMC flight over water

4-17

malfunction

12-87

ORIGINAL

Index-22

A1-H60BB-NFM--000

Page

No.

ASQ--81 towed body fails to seat

Primary servo or #1 transfer

properly

12-87

module leak

12-45

Cable grip rigging procedures

12-89

Primary servo or #2 transfer

Cargo hook emergency release

12-81

module leak

12-47

MAD reel failure with towed body

Transfer

2-74

deployed

12-86

Utility

2-75

RAST backup messenger cable

Mountain flying procedures and techniques . . .

9-46

employment

12-82

Canyon recce

9-50

RAST cable emergency release

12-83

Circle recce

9-49

RAST main probe fails to extend

12-84

Cirque recce

9-50

RAST main probe fails to retract

12-85

Contour crawl

9-47

RAST main probe messenger failure

12-81

Crossover recce

9-49

RAST messenger jettison

12-82

Figure eight recce

9-48

Rescue hoist failure

12-88

Wind finding

9-47

Mission overview

1-5

Mountain recce

9-48

Primary missions

1-8

Mountain takeoff and departure

9-51

Secondary missions

1-8

Mountain terrain flying

9-41

Mission planning

6-1

Mountain winds, turbulence

Mission--specific briefing

6-2

and topography

9-42

Mission/weapons system checklist

7-29

Topography

9-44

Mission/weapons systems checklist

10-31

Turbulence

9-43

Mistrap

8-23

Winds

9-42

Mk 46 MOD 5A (SW) slep torpedo

Movement of helicopter

8-1

launching (with AN/ASQ-165A)

7-73

MR de--ice fail caution light

12-65

Mk 46 MOD 5A (SW) slep torpedo

launching (with AN/ASQ-198)

7-75

MR de--ice fault caution light

12-65

Mk 46 torpedo preflight checklist

7-8

Multi--series qualified aircrew

20-2

Mk 50 torpedo preflight checklist

7-9

Multiplexer-demultiplexer,

TD-1254/ARQ-44

15-35

Mode:

Air-to-air receive

16-12

Air-to-air transmit/receive

16-16

Stabilator auto mode failure

12-54

Module(s):

NATO--compatible high capacity HIFR rig

8-32

Accessory module

2-33

NATOPS evaluation forms

20-22

Hydraulic logic, functions for a leak in

NATOPS evaluator

20-1

NO. 1 hydraulic system

2-77

NATOPS instructor

20-1

Hydraulic logic, functions for a leak in

NATOPS instructor/assistant

NO. 2 hydraulic system

2-78

NATOPS instructor

5-2

Hydraulic pump

2-73

Nautical miles per pound of fuel

Input

2-30

conversion chart

25-1

Input module chip caution lights on

12-36

Sample problem for nautical miles

Logic

2-75

per pound of fuel conversion chart

25-1

Main transmission module limitations

4-6

Navigation:

NO. 1 transfer

2-74

Components of the navigation subsystem . . .

16-1

NO. 2 transfer

2-75

Navigation modes

16-17

Index-23

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Navigation (cont):

NO. 1 transfer module

2-74

Navigation operations

16-1

NO. 2 hydraulic system

2-73

Navigation switching interface unit

16-1

NO. 2 hydraulic system malfunction

12-46

Radar navigation set, AN/APN-217

16-9

Pilot assist servo leak

12-47

Navigation modes

16-17

Pilot assist servo malfunction

12-48

Navigation operations

16-1

Primary servo or #2 transfer

Navigation switching interface unit

16-1

module leak

12-47

Ng sensing

2-19

NO. 2 transfer module

2-75

Night and IMC operations

8-4

NOE quickstop

7-94

CV night approaches

8-4

Normal approach

7-92

Deck conditions

8-4

Normal maneuvers

7-88

Night launches

8-4

Approach to landing

7-91

Night currency requirements

5-2

Climb procedures

7-90

Night formation

9-35

Cruise

7-90

Lost wingman VMC

9-36

Descent

7-90

Night HIFR procedures

8-38

Landings

7-92

Night launches

8-4

Night/IMC descent over water

7-91

Night VERTREP operations

9-27

NOE quickstop

7-94

Lighting

9-28

Practice autorotative approach

7-94

Night VERTREP safety

9-27

Practice single--engine failure in an

Procedures

9-28

HOGE (cut and run/cut gun)

7-95

Night VERTREP safety

9-27

Takeoff

7-88

Night vision device aircrewman

5-6

Taxi

7-88

Night vision device aircrewman instructor

5-6

Normal operations

8-34

Night vision device pilot

5-2

HIFR procedure

8-35

Night vision device pilot instructor

5-2

Normal takeoff

7-89

Night vision device procedures

9-39

Nose section (area 1)

7-2

General

9-39

N_p and torque sensing

2-19

Lighting considerations

9-40

N_p sensing

2-19

NVD operations over water

9-40

NVD lighting checklist

7-40

NVD physiology

9-40

NVD operations over water

9-40

NVD shipboard operations

9-41

NVD physiology

9-40

Night/IMC descent over water

7-91

NVD shipboard operations

9-41

Night/IMC search and rescue procedure

9-6

No APU shutdown procedures

7-86

No HIFR/stuck main tank shutoff valve

12-68

Obstacle clearance takeoff

7-89

No rotor brake start procedure

7-21, 10-14

No--hover landing

7-93

Officer:

Airborne tactical officer

5-2

NO. 1 hydraulic system

2-73

Landing safety officer

5-4

NO. 1 hydraulic system malfunction

12-44

OFT/WST evaluation

20-5

Primary servo or #1 transfer

module leak

12-45

OFT/WST procedures evaluation

20-3

Tail rotor servo leak

12-45

Oil cooler

2-15

Tail RTR servo leak without #1 RSVR

Oil filter

2-15

low caution light

12-46

Oil supply and scavenge system

2-15

ORIGINAL

Index-24

A1-H60BB-NFM--000

Page

No.

Oil system servicing

3-11

Operational risk management

19-4

Engine oil servicing

3-11

Five-step sequence

19-4

Four principles of application

19-5

Main transmission oil system servicing

3-11

Three levels of application

19-4

Tail and intermediate gearbox servicing

3-11

Optimum altitude for maximum range

28-2

Oil tank

2-13

Sample problem for optimum altitude

Oil temperature and pressure

for maximum range

28-2

monitoring system

2-15

Optimum altitude for maximum range chart . . .

28-7

On-top position indicator receiver

16-16

Oral evaluation

20-3

One times tail rotor speed (20 Hz)

11-20

Oral examination

20-5

One-per-revolution (4.3 Hz)

11-18

Oral examination and OFT/WST procedures

One-per-revolution (6.5 Hz)

11-19

evaluation (if conducted)

20-3

Open--book examination

20-2, 20-3

Oral examination and OFT/WST procedures

Operation(s):

evaluation grading criteria

20-4

Air--capable ship helicopter

8-4

OFT/WST evaluation

20-5

Aviation ship helicopter

8-3

Oral examination grading criteria

20-14

Blade de--ice system

2-123

Outside air-temperature (OAT) indicator

2-116

Overland SAR

9-13

Blade de--ice test system

2-128

Direct deployment

9-15

Cold--weather

14-1

Landing to effect a rescue

9-13

Day VERTREP

9-25

Rappelling

9-15

DECU

2-11

Rescue via hoist

9-15

Engine operation summary

2-13

Rescue via one or two wheels

9-14

Fire-extinguishing system, impact

Rescue/recovery methods

9-13

switch

2-121

Overspeed and drain valve

2-10

Fuel prime system

2-39

General shipboard

8-1

HF radio

15-26

Panel(s):

Hoist

2-133

AFCS control

2-85

Hot weather and desert

14-8

Blade de--ice control

2-123

Line

7-1

Blade de--ice test

2-128

Main fuel supply

2-36

Circuit breaker

2-56

Navigation

16-1

Communications control

15-3

Night and IMC

8-4

ECS control

2-121

Emergency

2-137

Night VERTREP

9-27

Fuel management control

2-45

Normal

8-34

Hover trim control panel

2-130

NVD operations over water

9-40

Pressure refueling panel

2-42

RAST operations for aircraft configured

Radio control

15-14

with external auxiliary fuel tank

3-10

Rescue hoist control

2-130

Special warfare support

9-39

Parade

9-31

System

2-40

Parking

3-16

System operation (with FMCP)

2-40

Passenger brief

6-8

TACAN

16-12

Personal flying equipment requirements

5-7

Vertical replenishment (VERTREP)

9-18

Pilot assist servo leak

12-47

VERTREP operations checklist

7-61

Pilot assist servo malfunction

12-48

Index-25

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Pilot assist servos

2-82

Post recovery

8-25

Pilot currency requirements

5-2

Post straightening checklist

8-30

Pilot display units

2-23

Post takeoff checklist

7-33

Pilot grading criteria

20-4

Post takeoff checks

10-36

Flight evaluation

20-5

Postflight inspection

14-9

Oral examination and OFT/WAT

Power required

9-46

procedures evaluation grading criteria

20-4

Power required exceeds power available

11-10

Pilot qualifications

5-1

Power turbine

2-5

Airborne tactical officer

5-2

Powerplant systems and related systems

2-1

Minimum pilot currency requirements

5-2

Engine

2-1

NATOPS instructor/assistant NATOPS

Engine and inlet anti-ice system

2-16

instructor

5-2

Engine control system

2-6

Night vision device pilot

5-2

Engine electrical system

2-10

Night vision device pilot instructor

5-2

Engine instruments

2-20

SH--60B functional checkflight pilot

5-2

Engine operation summary

2-13

SH--60B helicopter aircraft commander

5-1

Engine parameter sensing

2-19

SH--60B helicopter second pilot

5-1

Engine start system

2-15

Oil temperature and pressure

Pilot shipboard qualifications

5-2

monitoring system

2-15

Landing safety officer

5-4

Practice autorotative approach

7-94

Pilot VERTREP qualifications

5-4

Practice single--engine failure in an HOGE

Shipboard landing qualifications

5-3

(cut and run/cut gun)

7-95

Pilot VERTREP qualifications

5-4

Preflight

7-1

Initial VERTREP qualification

5-4

AGM--114 Hellfire preflight checklist

7-8

Shipboard VERTREP currency and

Automatic preflight checks

2-105

requalification requirements

5-4

Cabin inspection

7-10

Pinnacles

9-45

Cargo hook

9-22

Pitch bias actuator

2-101

Cockpit -- left side (area 2)

7-2

Pitot heater system

2-128

Cockpit -- right side (area 11)

7-7

Pitot static system

2-112

Cold--weather preflight check

14-1

Airspeed indicator

2-112

Crew brief and

19-8

Attitude indicator

2-113

Flight controls and hydraulics bay (area 3) . . .

7-3

Barometric altimeter

2-113

Fuselage -- left side (area 5)

7-5

Barometric altimeter/encoder

2-113

Fuselage -- right side (area 10)

7-7

Vertical speed indicators

2-113

General

7-1

Pitot--static tube heater

14-7

Main rotor/transmission/

Planned ditching

12-77

APU/engines (area 4)

7-4

Planning for and transport of cargo

21-1

Mk 46 torpedo preflight checklist

7-8

Pocket checklists

12-6

Mk 50 torpedo preflight checklist

7-9

Position lights

2-65

Nose section (area 1)

7-2

Post engagement checks

7-27, 10-20

Tail cone -- left side (area 6)

7-6

Post flight checks

7-40, 10-57

Tail cone -- right side (area 9)

7-7

Post landing checklist

7-35, 10-52

Tail pylon -- left side (area 7)

7-6

Hot refuel checklist

7-36

Tail pylon -- right side (area 8)

7-6

Post launch checklist

8-16

Preflight check

10-4

ORIGINAL

Index-26

A1-H60BB-NFM--000

Page

No.

Preflight inspection

14-9

HIFR

8-35

Prelaunch checklist

8-14

In--flight

9-24

Pressure:

Inadvertent IMC

9-36

Engine chip/engine oil pressure low

Instrument approach

13-1

caution lights on

12-20

Instrument flight

13-1

Indicator

2-26

Launch

8-15

Oil temperature and pressure

Litter platform setup

7-60

monitoring system

2-15

Lookout

13-2

Refueling

3-8

Lost aircraft procedures (open ocean)

12-79

Refueling panel

2-42

Lost communication procedures with

Single-point pressure refueling system

2-40

a VERTREP load

9-29

Transmission oil pressure limitations

4-7

M60D/M240D barrel change

9-58

Pressure indicator

2-26

M60D/M240D clear weapon

12-99

Pressure refueling

3-8

M60D/M240D lock and load

9-57

Helicopter on deck

3-8

M60D/M240D machine gun firing

9-57

Pressure refueling panel

2-42

M60D/M240D rigging

9-56

Prestart checks

7-12, 10-4

M60D/M240D stowing

9-58

Prevailing

9-42

MAD altitude compensation

7-82

Primary missions

1-8

Mountain flying procedures and

Primary servo or #1 transfer module leak

12-45

techniques

9-46

Primary servo or #2 transfer module leak

12-47

Night HIFR

8-38

Primary servo shutoff

2-75

Night/IMC search and rescue

9-6

Primary servos

2-79

Night vision device

9-39

Procedure(s)

9-28

No APU shutdown

7-86

Accelerometer null

7-64

No rotor brake start

7-21, 10-14

AGM-114 Hellfire missile launch/training . .

7-77

OFT/WST procedures evaluation

20-3

Air--capable ship launch and recovery

8-5

Oral examination and OFT/WST

Alternate engine start

7-83

procedures evaluation (if conducted)

20-3

Approach

8-6

Oral examination and OFT/WST

Aviation ship launch and recovery

8-3

procedures evaluation grading criteria

20-4

Breakup and rendezvous

9-35

Recovery assist

8-18

Cable grip rigging

12-89

Rotor brake start

7-24, 10--17

Climb

7-90

RSD unlatched

8-11

Crew served weapon

9-55

Self--contained approach

8-8

Crewman cargo

9-24

Special

7-50

Desert

14-9

Torque factor

10-58

Engine cleaning

7-64

Torque factor procedure in flight

10-58

Engine performance

22-5

Waveoff

8-4

Flight/hangar deck

8-1

Processor

15-35

GAU--16/A clear weapon

9--63, 12-101

Prohibited maneuvers

4-12

GAU-16/A firing

9-62

Pump/valve fail caution light

12-67

GAU-16/A lock and load

9-62

Pwr main RTR and/or PWR tail

GAU-16/A rigging

9-61

RTR light on

12-63

HIFR emergency

8-38

Pylon fold system

2-101

Index-27

ORIGINAL

A1-H60BB-NFM--000

Page

No.

RSD unlatched procedure

8-11

Traversing checklist

8-11

Qualification

5-1

RAST main probe fails to extend

12-84

Initial shipboard landing

5-3

RAST main probe fails to retract

12-85

Initial VERTREP

5-4

RAST main probe messenger failure

12-81

Special mission/lookout

RAST messenger jettison

12-82

non-aircrewman initial

5-5

RAST operations for aircraft configured

Qualified observer

5-6

with external auxiliary fuel tank

3-10

Qualified observer brief

6-7

RAST recovery checklist

7-48

RAST system

2-106

Main RAST probe

2-112

RAST control panel indicators

2-109

Radar altimeter, AN/APN-194

2-113

Rearview mirrors

2-143

Radar navigation set, AN/APN-217

16-9

Receiver/transmitter

16-11

Radio(s)

15-14

Receiver/transmitter RT-1275/ARQ-44

15-35

15-26

Recommended requirements for

HF radio operation

15-26

transitioning naval aviators

5-7

UHF radios, AN/ARC-159

15-14

Records and reports

20-22

UHF/VHF radios, AN/ARC-182

15-18

Recovery:

Radio control panels

15-14

Air--capable ship launch and recovery

Radio terminal set, AN/ARQ-44 (data link)

15-35

procedures

8-5

Radio terminal set, AN/ARQ-44 or

Autorotational

11-12

AN/ARQ-44A

15-44

Aviation ship launch and recovery

Rain precautions

14-8

procedures

8-3

Range chart

27-1

Launch and recovery signals

8-3

Range charts

25-1

RAST recovery checklist

7-48

Bingo profile, maximum range with

Unusual attitude

12-56, 13-2

dual engine

25-1

Recovery assist procedures

8-18

Maximum range, standard day chart

25-1

Airborne release

8-23

Nautical miles per pound of fuel

Consecutive landing practice

conversion chart

25-1

(RA yo--yos or free deck bounces)

8-25

Single/dual-engine fuel flow

25-1

Free deck landing

8-24

Rappelling

9-15

Mistrap

8-23

RAST backup messenger cable

Post recovery

8-25

employment

12-82

Post straightening checklist

8-30

RAST cable emergency release

12-83

RSD fails to latch

8-23

RAST control panel indicators

2-109

Straightening checklist

8-26

RAST equipped air--capable ships

8-9

Recovery assist secure and traverse lights

2-66

Aircraft startup

8-15

Recovery checklist

8-17

Launch procedures

8-15

Recovery from LTE

11-5

LSO console preoperational checklist

8-10

Reducing human factor errors

19-5

Post launch checklist

8-16

Refueling:

Prelaunch checklist

8-14

Gravity

2-42

Recovery assist (RA) procedures

8-18

Helicopter in--flight

8-32

Recovery checklist

8-17

HIFR refueling system

2-42

ORIGINAL

Index-28

A1-H60BB-NFM--000

Page

No.

Pressure

3-8

Rescue via one or two wheels

9-14

Pressure refueling panel

2-42

Rescue/recovery methods

9-13

Single-point pressure refueling system

2-40

Reservoir:

Refueling hose jettison (HIFR)

12-68

Hand pump reservoir servicing

3-12

Reservoir fill system

2-76

Remote compass transmitters

(pilot and ATO), ML-1(MOD)

16-5

Responsibility

9-35

Remote control unit

15-35

Flight/form/division lead

9-35

Wing

9-35

Remote lasing checklist

7-79

Restricted flight controls

12-39

Rendezvous

9-31

Return to force checks

7-35

Breakup and rendezvous procedures

9-35

Ridges

9-44

Requirements:

Rig for rescue checklist

7-60

Aircraft tiedown

3-17

RMU-42/A — mobile aircrew restraint

Aircrew currency

5-6

system

2-129

External power

3-14

Rolling pullouts

11-8

Ground training

5-6

Rollover characteristics

11-13

Minimum flightcrew

5-6

Critical rollover

11-13

Minimum pilot currency

5-2

Slope landing/takeoff considerations

11-14

Night currency

5-2

Static rollover

11-13

Personal flying equipment

5-7

Rotor(s):

Pilot currency

5-2

Engine start and rotor engagement

8-2

Recommended requirements for

Excess tail rotor thrust

12-40

transitioning naval aviators

5-7

Factors increasing the likelihood of

Shipboard landing currency and

loss of tail rotor effectiveness

11-4

requalification

5-3

HUB assembly, main

2-25

Shipboard VERTREP currency and

Insufficient tail rotor thrust

12-39

requalification

5-4

Loss of tail rotor authority

11-4

Waiver of

5-1

Loss of tail rotor control

12-41

Rescue hoist

2-130

Loss of tail rotor control approach and

Hoist auxiliary cooling

2-136

landing technique

12-39

Hoist cable shear

2-136

Loss of tail rotor control malfunctions

12-38

Hoist operation

2-133

Loss of tail rotor drive

12-36

Loss of tail rotor drive altitude and

Hover trim control panel

2-130

airspeed not sufficient to establish

Rescue hoist cable cut

12-90

autorotation

12-38

Rescue hoist cable separation

12-90

Loss of tail rotor drive altitude and

Rescue hoist control panel

2-130

airspeed sufficient to establish

Rescue hoist failure

12-88

autorotation

12-37

Rescue hoist fouled cable

12-89

Loss of tail rotor effectiveness

11-4

Rescue hoist preoperational check

7-43

Low rotor RPM

12-33

Rescue hoist weight limitations

4-16

Main rotor blade

2-24

Rescue precautions

9-1

Main rotor disk vortex

Night/IMC search and rescue procedure

9-6

(280° to 330° relative)

11-6

Swimmer deployment and survivor

Main rotor flapping margin

11-7

assistance

9-3

Main rotor gust lock

2-30

Rescue via hoist

9-15

Main rotor head

2-24

Index-29

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Rotor(s) (cont):

Rotor brake system

2-28

Main rotor RPM-indicating system

2-27

Main rotor gust lock

2-30

Main rotor specific vibrations

11-18

Rotor brake master cylinder

2-28

Main rotor system

2-23

Rotor head light

2-66

Main rotor system caution/

Rotor overspeed

4-8, 12-34

advisory lights

12-33

Rotor start and stop limits

4-7

Main rotor system emergencies

12-30

Rotor systems

2-23

Main rotor tiedown

3-19

Main rotor system

2-23

Main rotor vertical 4/rev vibration cueing . . .

11-7

Rotor brake system

2-28

Main rotor warning light

12-33

Tail rotor system

2-27

No rotor brake start procedure

7-21, 10-14

One times tail rotor speed (20 Hz)

11-20

RSD fails to latch

8-23

SH-60B tail rotor characteristics

11-4

RSD unlatched procedure

8-11

Starting

14-8

Runaway hoist

12-89

Starting engines and rotor

Running landing

7-92

engagement

7-21, 10-13

Running takeoff

7-89

Stopping

14-8

Runoff error avoidance

16-23

Tail rotor blades

2-28

Tail rotor considerations in

low-speed flight

11-4

Tail rotor control cable failures

12-38

Saddles

9-45

Tail rotor control system

2-79

Safety considerations during

Tail rotor drive shaft vibrations

evaluation flights

20-4

(high frequency)

11-20

Safety precautions

9-1, 13-2

Tail rotor head

2-28

Saltwater power deterioration

11-17

Tail rotor quadrant caution light on

12-42

Sample problem

21-1

Tail rotor servo

2-79

Sample problem 1

10-59

Tail rotor servo failures

12-38

Tail rotor servo leak

12-45

Sample problem 2

10-59

Tail rotor spar loads in maneuvering

Sample problem for airspeed system

flight

11-7

correction from level flight charts

28-1

Tail rotor specific vibrations

11-20

Sample problem for climb performance,

single engine, 30 minute power chart

27-1

Tail rotor system

2-27

Sample problem for cruise capability, time,

Tail rotor system malfunctions

12-36

and range chart

28-1

Tractor tail

11-4

Sample problem for hover endurance,

Transmission and rotor limits

4-6

out of ground effect

26-1

Rotor blade de--ice system

2-123

Sample problem for maximum gross weight

Blade de--ice control panel

2-123

to hover in ground effect, single engine

27-2

Blade de--ice system operation

2-123

Sample problem for nautical miles per

Blade de--ice test panel

2-128

pound of fuel conversion chart

25-1

Blade de--ice test system operation

2-128

Sample problem for optimum altitude

Rotor brake advisory light on

12-34

for maximum range

28-2

Rotor brake master cylinder

2-28

Sample problem for service ceiling,

Rotor brake operating limits

4-15

dual-engine, intermediate (30 minute)

Rotor brake start procedure

7--24, 10-17

power or torque placard limit

28-1

ORIGINAL

Index-30

A1-H60BB-NFM--000

Page

No.

Sample problem for service ceiling, single

Cockpit and sensor operator seats

2-129

engine, intermediate (30 minute) power

27-2

RMU-42/A — mobile aircrew restraint

Sample problem for use of ability to

system

2-129

maintain level flight, single engine chart

27-1

Seat adjustment

2-129

Sample problem for use of blade stall chart

22-1

Seat belts

2-129

Engine performance charts

22-5

Secondary lights

2-67

Secondary missions

1-8

Engine performance, intermediate

Section

9-31

(30 minute) power chart

22-5

Combustion

2-1

Engine performance, maximum

Compressor

2-1

continuous power chart

22-5

Inlet

2-1

Sample problem for use of engine

Main frame and accessory

2-5

performance, contingency (2.5 minute)

Nose section (area 1)

7-2

power, intermediate (30 minute) power

Selective jettison of M299 launcher

12-96

and maximum continuous power charts

22-5

Self--contained approach procedures

8-8

Torque factor terms

22-5

Sensor operator instructor and

Sample problem for use of climb

passenger seats

2-129

performance chart, dual-engine,

Service ceiling, dual-engine, intermediate

30 minute power, zero wind

24-1

(30 minute) power or torque placard limit

28-1

Sample problem for use of

Sample problem for service ceiling,

density altitude chart

22-1

dual-engine, intermediate (30 minute)

Sample problem for use of engine

power or torque placard limit

28-1

performance, contingency (2.5 minute)

Service ceiling, single engine, intermediate

power, intermediate (30 minute) power

(30 minute) power

27-2

and maximum continuous power charts

22-5

Sample problem for service ceiling,

Sample problem for use of indicated torque

single engine, intermediate

required to hover out of ground effect

23-1

(30 minute) power

27-2

Sample problem for use of maximum gross

Servicing:

weight to hover, headwind or ground

APU oil system

3-14

effect influence

23-1

Engine oil

3-11

Sample problem for use of maximum gross

Fire extinguisher system

3-14

weight to hover, out of ground effect

23-2

Fuel system

3-1

Sample problem for use of maximum

Hand pump reservoir

3-12

range, standard day chart

25-1

Hydraulic system

3-12

Sample problem for use of temperature

Main transmission oil system

3-11

conversion chart

22-1

Oil system

3-11

SAR equipment

9-1

Sonobuoy launcher pneumatic system

3-12

Tail and intermediate gearbox

3-11

SAS caution light on

12-53

Windshield washer system

3-14

Search and rescue

9-1

Servicing data

3-1

Overland SAR

9-13

SH--60B functional checkflight pilot

5-2

Rescue precautions

9-1

SH--60B helicopter aircraft commander

5-1

Safety precautions

9-1

SH--60B helicopter second pilot

5-1

Searchlight

2-65

SH-60B tail rotor characteristics

11-4

Seat(s)

2-129

Tail rotor considerations in

ASQ--81 towed body fails to seat

low-speed flight

11-4

properly

12-87

Tractor tail rotor

11-4

Index-31

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Sheer zone

9-44

Sonobuoy launching

7-68

Shipboard landing currency and

Automatic sonobuoy launching

7-68

requalification requirements

5-3

Manual sonobuoy launching

7-68

Shipboard landing qualification/currency

8-1

Sonobuoy lithium battery venting

12-72

Shipboard landing qualifications

5-3

Special instructions

10-2

Initial shipboard landing qualification

5-3

Special mission/lookout non-aircrewman

5-6

Shipboard landing currency and

Special mission/lookout non-aircrewman

requalification requirements

5-3

initial qualification

5-5

Shipboard launch/recovery limitations

8-3, 8-6

Special procedures

7-50

Shipboard VERTREP currency and

requalification requirements

5-4

Accelerometer null procedures

7-64

Shipboard wind limitations

4-15

Alert launch checklist

7-52

Shoulder harness lock lever

2-129

Alternate engine start procedures

7-83

Shoulders

9-44

APU turn--up checklist

7-84

Shutdown

7-36, 8-4, 10-53

Automatic approach checklist

7-52

Sideflare pattern

9-24, 9-25

Blade de--ice system check

7-61

Sideward and rearward flight

7-89

Engine anti--ice check

7-63

Simulated emergencies

19-8

Engine cleaning procedures

7-64

Simulated instrument flights

13-2

Engine fuel system priming checklist

7-59

Lookout procedures

13-2

Fuel dump checklist

7-59

Safety precautions

13-2

Health indicator test (HIT) check

7-50

Single--engine failure

12-23

Litter platform setup procedures

7-60

Single-engine landing

12-25

Single-point pressure refueling system

2-40

MAD operational checklists

7-81

Gravity refueling

2-42

No APU shutdown procedures

7-86

HIFR refueling system

2-42

Rig for rescue checklist

7-60

Pressure refueling panel

2-42

Sonobuoy launching

7-68

Suction defuel

2-42

Torpedo launching

7-69

Single/dual-engine fuel flow

25-1

VERTREP operations checklist

7-61

Situational awareness

19-1

Special warfare support operations

9-39

Slope landing/takeoff considerations

11-14

Speech security equipment, TSEC/KY-58

15-30

Cross--slope landing

11-15

Speech security system

15-30

Down--slope landings

11-15

Radio terminal set, AN/ARQ-44

Take off

11-16

(data link)

15-35

Up--slope landings

11-15

Speech security equipment,

Slow-speed flight

11-2

TSEC/KY-58

15-30

Stabilator effect in a hover/slow

Tactical speech security equipment,

speed flight below 30 knots

11-2

TSEC/KYV-5

15-32

Tail winds in transition to forward flight

11-2

Spread incomplete light

12-34

Translational lift

11-2

Stabilator auto mode failure

12-54

Smoke and fumes elimination

12-72

Snow precautions

14-4

Stabilator effect in a hover/slow speed

flight below 30 knots

11-2

Sonobuoy launcher pneumatic

system servicing

3-12

Stabilator indicating system failure

12-56

ORIGINAL

Index-32

A1-H60BB-NFM--000

Page

No.

Stabilator malfunctions

12-54

Starting rotors

14-8

Stabilator auto mode failure

12-54

Static rollover

11-13

Stabilator indicating system failure

12-56

Steep approach

7-92

Stabilator system

2-89

Stopping rotors

14-8

Stability augmentation system

2-92

Stores emergencies

12-96

Altitude hold

2-96

Hung sonobuoy/SLC

12-96

Attitude and airspeed hold

2-95

Launch/JETT fail caution light on

12-97

Auto approach to a hover

2-97

Selective jettison of M299 launcher

12-96

Automatic depart

2-98

Straightening checklist

8-26

Automatic preflight checks

2-105

Suction defuel

2-42

Autopilot

2-95

Summary

2-13

Blade fold system

2-101

Survival and emergency equipment

2-140

Heading hold

2-96

Emergency equipment

2-140

Hover augmentation/gust alleviation

2-96

Survival equipment

2-140

Hover coupler

2-98

Survival equipment

2-140

Maneuvering stability

2-97

SUW/ASW operational missions

5-7

Pitch bias actuator

2-101

Swimmer deployment and survivor

Pylon fold system

2-101

assistance

9-3

Trim system

2-95

System(s):

Turn coordination

2-97

AC bus tie

2-54

Stall:

AC electrical

2-49

Blade

11-3

Advanced helicopter emergency egress

Blade stall causes

11-3

lighting

2-142

Blade stall chart

22-1

APU start

2-49

Compressor

12-16

Automatic flight control

2-84

Methods of eliminating roughness caused

Auxiliary fuel

2-45

by blade

11-3

Auxiliary power unit

2-47

Sample problem for use of blade

Backup hydraulic

2-73

stall chart

22-1

Blade fold

2-101

Standard mountain approach and landing

9-50

Cargo hook

2-137

Standby magnetic compass

2-116

Caution/advisory light

2-117

Start checklist

7-12

Compass

16-4

Mission/weapons system checklist

7-29

DC bus tie

2-55

Prestart checks

7-12

DC electrical

2-54

Starting engines and rotor engagement

7-21

De--ice/anti-ice

2-122

Systems checks

7-17

Electrical

2-49

Start checks

10-4

Emergency locator transmitter

2-140

Prestart checks

10-4

Engine and inlet anti--ice

2-123

Starting and ground idle

2-13

Engine electrical

2-10

Starting APU and engines

7-57

Engine start

2-15

Starting engines and rotor

Engine/APU boost/fuel prime

2-39

engagement

7-21, 10-13

Engine/APU fire-extinguishing

2-118

No rotor brake start procedure

7-21, 10-14

Environmental control

2-121

Post engagement checks

7-27, 10-20

Fire-detection

2-117

Rotor brake start procedure

7--24, 10-17

Flight control

2-79

Index-33

ORIGINAL

A1-H60BB-NFM--000

Page

No.

System(s) (cont):

Transmission

2-30

Flight control servo

2-79

Transmission chip detector

2-34

Fuel

2-36

Trim

2-95

Fuel dump

2-39

Vertical instrument display

2-20

Fuel low level warning

2-39

Wheel brake

2-106

Fuel transfer

2-46

Windshield anti-ice

2-128

Global positioning

16-17

Windshield washer

2-129

Helicopter emergency egress lighting

2-142

Windshield wiper

2-128

HIFR

8-32

Windshield wiper and washer

2-128

HIFR refueling

2-42

System limitations

4-6

Hydraulic

2-68

Engine idle limits with gust lock engaged . . .

4-6

Hydraulic leak-detection/isolation

2-75

Engine limits

4-6

Engine start limits

4-6

Identification

15-36

Engine starter limits

4-6

Ignition

2-12

Individual helicopter emergency

Engine temperature limitations

4-6

egress lighting

2-142

System operation

2-40

Intercommunication

15-27

System operation (with FMCP)

2-40

Intermediate and tail gearbox chip/

Systems check

7--17, 10-7

temperature

2-34

Main rotor

2-23

Main rotor RPM-indicating

2-27

TACAN control

16-12

Main tanks fuel quantity

2-39

TACAN navigation set, AN/ARN-118(V)

16-11

Main transmission lubrication

2-33

Air-to-air receive mode

16-12

Master warning

2-116

Air-to-air transmit/receive mode

16-16

Mechanical control

2-79

In-flight confidence test

16-16

NO. 1 hydraulic

2-73

Receiver/transmitter

16-11

NO. 2 hydraulic

2-73

TACAN control

16-12

Oil supply and scavenge

2-15

TACAN operation

16-12

Pitot heater

2-128

Tactical speech security equipment,

Pitot static

2-112

TSEC/KYV-5

15-32

Powerplant systems and related

2-1

Tactical/combat checklist

7-33

Pylon fold

2-101

Tail and intermediate gearbox servicing

3-11

RAST

2-106

Tail bumper

2-106

Reservoir fill

2-76

Tail cone -- left side (area 6)

7-6

RMU-42/A — mobile aircrew restraint

2-129

Tail cone -- right side (area 9)

7-7

Rotor

2-23

Tail gearbox

2-33

Rotor blade de--ice

2-123

Tail landing gear

2-106

Rotor brake

2-28

Tail pylon -- left side (area 7)

7-6

Single-point pressure refueling

2-40

Tail pylon -- right side (area 8)

7-6

Speech security

15-30

Tail rotor blades

2-28

Stabilator

2-89

Tail rotor considerations in low-speed flight . . .

11-4

Stability augmentation

2-92

Factors increasing the likelihood of

Tail rotor

2-27

loss of tail rotor effectiveness

11-4

Tail rotor control

2-79

Hover/air taxi

11-4

ORIGINAL

Index-34

A1-H60BB-NFM--000

Page

No.

Loss of tail rotor authority

11-4

Running

7-89

Loss of tail rotor effectiveness

11-4

Sideward and rearward flight

7-89

Loss of translational lift

11-4

Takeoff and climb

2-13

Recovery from LTE

11-5

Takeoff checklist

7-32, 10-33

Tail rotor control cable failures

12-38

Takeoff to hover

7-88

Tail rotor control system

2-79

Tank(s):

Tail rotor drive shaft vibrations

Auxiliary fuel tanks

2-46

(high frequency)

11-20

External tank jettison

2-47

Tail rotor head

2-28

Main tanks fuel quantity system

2-39

Tail rotor quadrant

2-27

RAST operations for aircraft configured

Tail rotor quadrant caution light on

12-42

with external auxiliary fuel tank

3-10

Tail rotor servo

2-79

Taxi

7-88, 14-9

Tail rotor servo failures

12-38

Tail rotor servo leak

12-45

Taxi checklist

7-32, 10-32

Tail rotor spar loads in maneuvering flight

11-7

Taxiing

14-3

Tail rotor specific vibrations

11-20

Temperature conversion chart

22-1

One times tail rotor speed (20 Hz)

11-20

Sample problem for use of temperature

Tail rotor drive shaft vibrations

conversion chart

22-1

(high frequency)

11-20

Temperature limitations

4-17

Tail shake (five cycles per second)

11-20

Terrain flying

9-39

Tail rotor system

2-27

General

9-39

Tail rotor system malfunctions

12-36

Test:

Loss of tail rotor control malfunctions

12-38

Cargo hook emergency release

2-137

Loss of tail rotor drive

12-36

Health indicator test (HIT) check

7-50

Tail rotor quadrant caution light on

12-42

15-27

Tail RTR servo leak without #1 RSVR low

caution light

12-46

Hydraulic leak

2-76

Tail shake (five cycles per second)

11-20

In-flight confidence

16-16

Tail wheel lock

2-106

UHF/VHF

15-26

Tail winds in transition to forward flight

11-2

TGT sensing

2-19

Tail/intermediate transmission malfunction . . .

12-36

The engines

1-4

Take off

11-16

The helicopter

1-1

Takeoff

7-88, 14-3, 14-9

Three levels of application

19-4

Air taxi

7-89

Thunderstorm utility lights

2-67

Aircrewman post takeoff checks

7-47

Thunderstorms

14-7

Hovering turns

7-88

Thunderstorms and turbulence

14-7

Instrument

13-1

Tiedown:

Maximum gross weight

7-89

Aircraft tiedown instructions

3-17

Maximum performance

7-89

Aircraft tiedown requirements

3-17

Mountain takeoff and departure

9-51

Main rotor tiedown

3-19

Normal

7--89

Obstacle clearance

7-89

Topography

9-44

Post takeoff checklist

7-33

Torpedo emergencies

12-95

Post takeoff checks

10-36

Hung torpedo

12-95

Index-35

ORIGINAL

A1-H60BB-NFM--000

Page

No.

Torpedo launching

7-69

Main transmission

2-30

AGM-114 Hellfire missile launch/

Main transmission lubrication system

2-33

training procedure

7-77

Tail gearbox

2-33

Mk 46 MOD 5A (SW) SLEP torpedo

Transmission chip detector system

2-34

launching (with AN/ASQ-165A)

7-73

Transmission gauges

2-33

Remote lasing checklist

7-79

Transmission system malfunctions

12-35

Torpedo launching (with AN/ASQ-165A)

Input module chip caution lights on

12-36

except for Mk 46 MOD 5A (SW)

Main transmission malfunction

12-35

SLEP torpedo

7-69

Tail/intermediate transmission

Torpedo launching (with AN/ASQ-198)

malfunction

12-36

except for Mk 46 MOD 5A (SW)

Transponder computer, KIT-1 TSEC series . . .

15-40

SLEP torpedo

7-71

Traversing checklist

8-11

Torque factor chart

10-58

Trim system

2-95

Torque factor method

22-5

Turbulence

9--43, 14-7

Torque factor procedure

10-58

Descending

14-8

Torque factor procedure in flight

10-58

In turbulent air

14-8

Torque factor sample problem

22-11

Starting rotors

14-8

Torque factor terms

10-57, 22-5

Stopping rotors

14-8

Torque factor TGT reference

10-58

When encountering turbulent air

14-8

TR de--ice fail caution light

12-65

Turn coordination

2-97

Tractor tail rotor

11-4

Training:

Aircrewman ground training

5-6

Flightcrew ground training

5-6

UHF backup

15-17

Ground training requirements

5-6

UHF radios, AN/ARC-159

15-14

Transfer modules

2-74

UHF/VHF backup

15-23

NO. 1

2-74

UHF/VHF radios, AN/ARC-182

15-18

NO. 2

2-75

UHF/VHF test

15-26

Utility module

2-75

Uncommanded fuel dumping

12-69

Transition to forward flight

11-2

Underwater egress

12-80

Translational lift

11-2

Unit:

Transmission and rotor limits

4-6

Auxiliary power

2-48

Main transmission module limitations

4-6

Auxiliary power unit system

2-47

Rotor overspeed

4-8

Central display

2-21

Rotor start and stop limits

4-7

Hydromechanical control

2-8

Transmission oil pressure limitations

4-7

Navigation switching interface

16-1

Transmission chip detector system

2-34

Remote control

15-35

Transmission gauges

2-33

Unprepared site landing

7-93

Transmission oil pressure limitations

4-7

Transmission system

2-30

Unusual attitude recovery

12-56, 13-2

Chip-detector caution lights self-test

2-34

Unusual attitudes

13-2

Intermediate and tail gearbox chip/

Unusual vibrations

12-30

temperature systems

2-34

Damper failure

12-30

Intermediate gearbox

2-33

Ground resonance

12-30

Main gearbox vibrations

2-34

Unusual vibrations in flight

12-31

ORIGINAL

Index-36

A1-H60BB-NFM--000

Page

No.

Unusual vibrations on deck

12-32

Up--slope landings

11-15

Waiver of requirements

5-1

Use of charts

28-2

H--60 pilot qualified in model

5-1

Use of different fuels

3-10

Warning, caution(s), and advisories

2-116, 12--6

Utility and test receptacles

2-65

Caution/advisory light system

2-117

Master warning system

2-116

Utility lights

2-67

Waveoff procedures

8-4

Utility module

2-75

Weather vaning (120° to 240° relative)

11-6

Weight limitations

4-15

Cargo hook weight limitation

4-15

Center of gravity limitations

4-15

Valve:

Rescue hoist weight limitations

4-16

Engine anti--ice/start bleed

2-16

Weight limits

4-15

Wheel brake system

2-106

Engine inlet anti--ice

2-17

When encountering turbulent air

14-8

Overspeed and drain

2-10

White lighting checklist

7-40

Vertical instrument display system

2-20

Wiggins/North Island HIFR rig

8-32

Vertical landing from a hover

7-92

Wind:

Vertical replenishment (VERTREP)

Climb performance, dual-engine,

operations

9-18

30 minute power, zero wind

24-1

Cargo delivery

9-21

Sample problem for use of climb

performance chart, dual-engine,

Cargo pickup

9-20

30 minute power, zero wind

24-1

Day VERTREP operations

9-25

Shipboard wind limitations

4-15

Flight with external loads

9-20

Wind finding

9-47

Lost communication procedures

Wind finding

9-47

with a VERTREP load

9-29

Winds

9-42

Night VERTREP operations

9-27

Windshield anti-ice system

2-128

Vertical speed indicators

2-113

Windshield washer system

2-129

Windshield washer system servicing

3-14

VERTREP operations checklist

7-61

Windshield wiper and washer system

2-128

VERTREP safety

9-27

Windshield washer system

2-129

Vibration analysis

10-68

Windshield wiper system

2-128

Visual approach

8-7

Wing

9-35

Visual landing aids

8-3

WOW advisory light on in flight

12-91

Voice commands

9-58

Vortex ring state (210° to 330° relative)

11-6

Vortex ring state/power settling

11-10

Z-AHQ adapter

15-32

Index-37/(38 blank)

ORIGINAL

SH-60B HELICOPTER. FLIGHT MANUAL (2008) - page 13