UH-3H and UH-3H EXECUTIVE TRANSPORT. FLIGHT MANUAL (2000) - page 9

 

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UH-3H and UH-3H EXECUTIVE TRANSPORT. FLIGHT MANUAL (2000) - page 9

 

 

NAVAIR 01-230HLH-1
23-7
ORIGINAL
NAVAIR 01-230HLH-1
This Page Left Blank Intentionally
23-8
ORIGINAL
NAVAIR 01-230HLH-1
CHAPTER 24
Endurance
24.1
ENDURANCE CHARTS
3. From point D, continue to trace the gross weight
line up to the 4,000-foot pressure altitude line in the
The maximum endurance charts (Figure 24-1 and 24-
next block (point F), then trace left to the torque scale
2) provide fuel flow, indicated and calibrated airspeed, and
(point G), and read 44-percent torque.
approximate torque when gross weight is applied to
pressure altitude to produce maximum endurance.
24.1.2 Hover Endurance
- Two-Engine Chart.
The hover endurance - two-engine chart (Figure 24-2)
24.1.1 Maximum Endurance - Two-Engine Chart.
provides the fuel flow when gross weight is applied to
The maximum endurance - two-engine chart (Figure 24-1)
pressure altitude and OAT to provide hovering endurance.
provides the fuel flow, indicated and calibrated airspeed,
and approximate torque when gross weight is applied to
24.1.2.1 Sample Problem for Use of Hovering
pressure altitude to produce maximum endurance for the
Endurance - Two-Engine Chart (Figure 24-2).
helicopter.
24.1.1.1 Sample Problem for Use of Maximum
Endurance - Two Engine Chart (Figure 24-1).
1. Enter left side of chart at
18,000 pounds gross
weight
(point A), trace right to sea-level pressure
altitude line
(point B), then trace down to the OAT
baseline (point C).
1. Enter bottom of chart at 18,000 pounds gross weight
(point A), trace up to 4,000 foot pressure altitude line
2. From point C, follow the guideline to the
20 °C
(point B), then trace left to the fuel consumption scale
OAT line (point D), then trace down to the fuel-flow
(point C) and read 870 pounds of fuel per hour.
scale (point E) and read 1,475 pounds of fuel per hour.
2. From point B, continue to trace the gross weight
line up to the 4,000-foot pressure altitude line in the
next block (point D), then trace left to the airspeed
scale (point E) and read 66 KCAS and 62 KIAS.
24-1
ORIGINAL
NAVAIR 01-230HLH-1
24-2
ORIGINAL
NAVAIR 01-230HLH-1
24-3
ORIGINAL
NAVAIR 01-230HLH-1
This Page Left Blank Intentionally
24-4
ORIGINAL
NAVAIR 01-230HLH-1
CHAPTER 25
Emergency Operation
25.1
HEIGHT VELOCITY DIAGRAMS
25.2 CLIMB CHARTS
The height velocity diagrams (Figure 25-1 and 25-2)
The climb charts - one engine (Figure 25-3 and 25-4)
provide the limiting altitude and corresponding airspeed
are based on military power and provide one-engine climb
combinations for a safe landing after one or both engines
data for the helicopter on cold and warm days. The chart
have failed.
uses like factors in the same manner as the climb charts in
Chapter
22; therefore, explanatory test and sample
25.1.1 Height Velocity Diagram
- Two-Engine
problem data are not included.
Failure Chart. The height velocity diagram - two engine
failure chart (Figure 25-1) is based on a gross weight of
25.3 ABILITY TO MAINTAIN LEVEL FLIGHT
-
17,000 and 19,000 pounds, 100-percent Nr, and a standard
ONE-ENGINE CHART
day temperature at sea level.
The ability to maintain level flight - one-engine chart
25.1.1.1 Sample Problem for Use of Height
(Figure 25-5) provides the speed range wherein one-engine
Velocity Diagram
- Two-Engine Failure Chart
level flight may be maintained at various density altitudes
(Figure 25-1).
and gross weights at a torque value the engine is actually
producing.
25.3.1
Sample Problem for Use of Ability To
Maintain Level Flight - One-Engine Chart (Figure
25-5).
1. Enter left of chart at 300-foot altitude (point A) and
bottom of chart at 40 KIAS (point B).
2. Trace right from point A and up from point B until
the lines intersect at point C and note that sink rate
limit of the landing gear may be exceeded.
1. Convert 4,000-foot pressure altitude and 18 °C to
5,800-foot density altitude, then enter left side of chart
25.1.2 Height Velocity Diagram
- One-Engine
at 5,800-foot density altitude (point A) and trace right
Failure Chart. The height velocity diagram - one-engine
to 18,000 pounds gross weight (point B).
failure chart
(Figure 25-2) is based on gross weights of
15,000, 17,000, and 19,000 pounds; 100-percent Nr; and
2. From point B, trace down to the airspeed baseline
standard day temperature at sea level. Except for the
(point C).
additional gross weight parameters, the chart uses like
factors in the same manner as Figure 25-1.
3. From point C, follow the influence line down to
intersect the 90-percent torque line (point D).
25-1
ORIGINAL
NAVAIR 01-230HLH-1
The 90-percent torque available value is provided by
25.6 ENDURANCE CHART
Figure 20-6. Enter bottom of chart at 18 °C, proceed
upward to intersect the
4,000-foot pressure altitude
The maximum endurance - one-engine chart (Figure
line, then trace to the left side and read
90-percent
25-8) provides maximum endurance for the helicopter
torque.
during one-engine operation. The chart uses like factors in
the same manner as the endurance charts in Chapter 24;
4. From point D, trace left and read Vmin of 56 KIAS
therefore, explanatory text and sample problem data are
(point E).
not provided.
5. From point C, follow the influence line up to
25.7 LANDING DISTANCE GROUND ROLL
-
intersect the 90-percent torque line and read Vmax at 75
POWER-OFF
KIAS.
The landing distance ground roll
- power-off chart
25.4 ABILITY TO MAINTAIN
70 KNOTS AT
(Figure
25-9) provides the landing distance ground roll
VARIOUS ROTOR SPEEDS - ONE ENGINE
when pressure altitude, temperature, gross weight, and
CHART
headwind components are introduced into the chart.
The ability to maintain
70 knots at various rotor
25.7.1 Sample Problem for Use of Landing
speeds (Nr) - one-engine chart (Figure 25-6) provides the
Distance Ground Roll
- Power-Off Chart (Figure
gross weights at which the helicopter can maintain level
25-9).
flight at various pressure altitudes, temperatures, and rotor
speeds.
25.4.1 Sample Problem for Use of Ability To
Maintain
70 Knots at Various Rotor Speeds
-
One-Engine Chart (Figure 25-6).
1. Enter bottom of chart at 28 °C (point A), then trace
up to sea level pressure altitude (point B).
2. From point B, trace right
18,000 pounds gross
weight (point C).
1. Enter left side of chart at
4,000-foot pressure
3. From point C, trace down to the headwind baseline
altitude
(point A), trace right 20 °C OAT (point B),
(point D).
then trace down to the rotor speed baseline (point C).
4. From point D, follow the influence line to the 10-
2. From point C, follow the influence line to
102-
knot headwind line (point E).
percent Nr (point D), then trace down to the gross
weight scale (point E) and read 17,750 pounds.
5. From point E, trace down and read 160 feet ground
roll (point F).
25.5 RANGE CHART
The maximum range - one-engine chart (Figure 25-7)
is based on military power to provide maximum range for
the helicopter during one-engine operation. The chart uses
like factors in the same manner as the range charts in
Chapter
23; therefore, explanatory text and sample
problem data are not included.
25-2
ORIGINAL
NAVAIR 01-230HLH-1
Figure 25-1. Height Velocity Diagram - Two-Engine Failure
25-3
ORIGINAL
NAVAIR 01-230HLH-1
Figure 25-2. Height Velocity Diagram - One-Engine Failure
25-4
ORIGINAL
NAVAIR 01-230HLH-1
25-5
ORIGINAL
NAVAIR 01-230HLH-1
25-6
ORIGINAL
NAVAIR 01-230HLH-1
25-7
ORIGINAL
NAVAIR 01-230HLH-1
25-8
ORIGINAL
NAVAIR 01-230HLH-1
25-9
ORIGINAL
NAVAIR 01-230HLH-1
25-10
ORIGINAL
NAVAIR 01-230HLH-1
25-11
ORIGINAL
NAVAIR 01-230HLH-1
Figure 25-9. Landing Distance Ground Roll - Power-Off
25-12
ORIGINAL
NAVAIR 01-230HLH-1
CHAPTER 26
Special Charts
Not applicable.
26-1
ORIGINAL
NAVAIR 01-230HLH-1
This Page Left Blank Intentionally
26-2
ORIGINAL
NAVAIR-01-230HLH-1
INDEX
Paragraph
Page No
A
Abandoning Helicopter
12.34.7
12-46
Ability to Hover Out of Ground Effect at Various Rotor Speeds Chart
21.1.3
21-1
ABILITY TO MAINTAIN 70 KNOTS AT VARIOUS ROTOR SPEEDS - ONE
25.4
25-2
ENGINE CHART
ABILITY TO MAINTAIN LEVEL FLIGHT - ONE-ENGINE CHART
25.3
25-1
Acceleration Limitations
4.1.14
4-6
Acceptable Ground Power Units
3.1.3
3-4
ADDITIONAL MISSIONS/STATIC DISPLAYS
9.6
9-16
Additional Speed Limits
4.1.10
4-6
Adjustment of Fuel System for Different Fuels
3.2.4
3-6
ADVANCED INSTRUMENT FLYING
9.3
9-6
Adverse Weather Conditions
11.3.5
11-7
Advisory Panel
2.16.1
2-68
AFTER FINAL LANDING
7.18
7-26
After Takeoff
14.1.7
14-3
After Water Entry
12.34.3
12-43
AIMS Transponder System Components
15.15.1
15-16
Air Taxiing
7.7.2
7-18
AIRBORNE IDENTIFICATION MOBILE TRANSPONDER SYSTEM
15.15
15-16
AIR-CAPABLE SHIP OPERATIONS
8.4
8-12
Aircraft Discrepancy Book
7.2.6
7-2
AIRCRAFT PREPARATION
17.7.1
17-18
AIRSPEED CALIBRATION CHART
20.2
20-1
Airspeed Limitations
4.1.9
4-5
Aldis Lamp
2.23.6
2-93
Alert Checklist
9.7.2
9-18
Alternating Current Power Supply System
2.6.1
2-34
Alternating Current System Failure
12.21.1
12-27
Altitude Encoder
2.15.9
2-66
Altitude Limitations
4.1.13
4-6
ANTI-ICING SYSTEM
2.19
2-83
Application Checklist
12 38.1
12-50
Approach
18.14.2
18-24
APPROACH TO A HOVER
18.10
18-5
Approach/Landing Procedures
8.4.3
8-14
Approaches
7.16.2
7-26
APU Fire on the Ground (UH-3H Executive Transport)
12.40.3
12-53
Arrival/Return
18.4.10
18-3
ASE/AUX OFF
8.4.4
8-15
ASE Malfunction
12.25.2
12-33
ASN-123C TACTICAL NAVIGATION SYSTEM
15.20
15-23
Assisting Survivor
18.12.4
18-13
Attaching Bucket
18.14.1
18-24
Attitude and Heading Reference System (A/A24G-39 AHRS
2.15.5
2-63
Attitude Indicators
2.15.7
2-65
Automatic Blade Fold
9.5.5
9-14
INDEX-1
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
AUTOMATIC BLADE FOLD SYSTEM
2.13
2-61
Automatic Stabilization Equipment
2.10.1
2-53
AUTOMATIC STABILIZATION EQUIPMENT COUPLER SYSTEM
2.10
2-53
AUTOMATIC STABILIZATION EQUIPMENT SYSTEM FAILURE
12.25
12-32
AUTOROTATIONS
7.15
7-23
Auxiliary Flight Control Servo System
2.8.2
2-48
AUXILIARY FLOTATION COLLAR
12.38
12-50
AUXILIARY POWER UNIT (APU) SYSTEM (UH-3H Executive Transport)
2.1.11
2-21
AXIAL DRIVE SHAFT FAILURE
12.11.11
12-11
B
Background
17.1.2
17-1
BAMBI BUCKET OPERATIONS
18.14
18-24
BATTERY/DC EXTERNAL POWER START NO. 1 ENGINE
7.3
7-7
BEARING DISTANCE HEADING INDICATORS
15.16
15-18
Bearing Distance Heading Indicators
15.16.1
15-18
Beeper Trim Malfunction
12.25.3
12-33
Before Entering the Helicopter
14.1.2
14-2
BEFORE LANDING CHECK
7.13
7-21
Before Leaving Helicopter
14.1.9
14-3
Before Takeoff
14.1.6
14-2
Bifilar Absorber
2.3.2
2-23
Blade Fold
10.4.2
10-49
Blade Fold Control Panel
2.13.2
2-62
Blade Pressure Caution Light
12.19.1
12-21
Blade Spread
9.5.3
9-13
Blade Stall
11.2.5
11-3
Blade Stall
12.10.3
12-7
BLADE STALL CHART
20.6
20-3
Blade Tracking
10.1.6
10-2
Brake Pedals
2.12.8
2-61
Brief
18.4.2
18-2
Briefing
9.1.5
9-5
Briefing Format
6.4.5
6-2
BRIEFING/DEBRIEFING RESPONSIBILITIES
6.4
6-2
C
Cabin Door
12.35.3
12-49
Cabin Emergency Exit Hatches
12041
12-54
Cabin Heater Fan Switch
2.18.2
2-74
Cabin Heater Switch
2.18.1
2-74
Cabin Windows
12.35.4
12-49
Canteen
2.24.1
2-93
Cargo Deck (UH-3H)
2.25.6
2-99
Cargo Delivery
18.13.2
18-22
Cargo Door
4.1.20
4-6
Cargo Hook Manual Release Arm
2.25.5
2-99
Cargo Hook Release Buttons
2.25.2
2-99
Cargo Hook Stowage Line
2.25.4
2-99
INDEX-2
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
Cargo Pickup
18.13.1
18-21
Cargo Release Foot Pedal
2.25.3
2-99
CARGO SLING
2.25
2-96
Cargo Sling Control Panel
2.25.1
2-99
Cargo Sling Limitations
4.1.24
4-6
CARGO SLING OPERATIONS
18.13
18-21
Carrier-Based
7.17.3
7-26
Caution Panel
2.16.2
2-68
Center of Gravity Limitations
4.1.15
4-6
Cg Not Within Prescribed Limits
12.32.10
12-40
CHANNEL MONITOR Panel
2.10.5
2-58
Channel Monitor Test Switch
2.10.6
2-58
Chip Detector Caution Lights
2.4.5
2-28
Climb - Normal Power (Warm Day)
22.1.2
22-1
Climb - Normal Power Chart (Cold Day)
22.1.1
22-1
CLIMB CHARTS
22.1
22-1
CLIMB CHARTS
25.2
25-1
Clocks
2.15.3
2-63
Closed-Book Examination
19.2.2
19-2
Command Responsibility
6.4.3
6-2
COMMUNICATION AND ASSOCIATED ELECTRONIC EQUIPMENT
15.2
15-1
Communications
9.4.4
9-10
Compass System Control Panel
2.15.6
2-65
COMPRESSOR STALL
12.11.8
12-9
Conditions Requiring Functional Checkflight
10.1.5
10-1
Conduct of Flight
9.1.3
9-5
Constant Airspeed Climbs
9.3.4
9-8
Coupled Indications
12.24.1
12-32
COUPLER MALFUNCTIONS
12.32
12-37
Coupler System
2.10.2
2-54
COURSE INDICATOR (ID-387/ARN)
15.12
15-14
CREW BRIEFING
17.7.2
17-19
Crew Coordination
11.4.2
11-10
CREW COORDINATION CONCEPTS
18.2
18-1
CREW REST REQUIREMENTS
5.5
5-4
Crewman Evaluation
19.3.5
19-5
Crewman Evaluation
5.3.2
5-4
Crewman Evaluation Worksheet
19.3.7
19-7
Crewman Minimum Ground Training Before Flight
5.1.2
5-1
Crewman Oral Examination
19.3.6
19-6
Crewman Qualification
5.2.2
5-2
CREWMEMBER SEATS
2.2
2-85
Crewmen Safety Belts
2.21.2
2-85
Crew-Portable Hoist and Microphone Switch
2.22.3
2-88
CRITICAL PROCEDURES
12.2
12-1
Crosswind Landings
7.14.4
7-23
CRUISE CHECKS/FUEL MANAGEMENT
7.12
7-20
CV OPERATIONS
8.1
8-1
INDEX-3
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
D
Damper Fluid Tank Servicing
3.2.8
3-9
DANGER AREAS
3.9
3-20
Day VFR
18.12.6
18-13
Debrief
18.4.15
18-4
Debriefing Format
6.4.6
6-3
Definitions (FCF)
10.1.8
10-5
Definitions
19.1.2
19-1
DENSITY ALTITUDE CHART
20.4
20-2
Departure
18.4.7
18-3
Departure From a Coupled Hover
18.10.3
18-10
Descent /Approach
18.4.11
18-4
DESCRIPTION OF AIRCREW POSITIONS
18.3
18-2
Designation of Functional Checkflight Aircrewman
10.1.3
10-1
Designation of Pilots
10.1.1
10-1
DIM Control
15.20.6
15-28
Dimensions
1.1.3
1-2
Direct Current Power Supply System
2.6.2
2-37
Direct Current System Failure
12.21.2
12-30
DITCHING PROCEDURES
12.34
12-43
DOPPLER
15.17
15-22
Doppler Control/Indicator Panel
15.17.1
15-22
Doppler System Operation
15.17.2
15-22
Down-Limit Release (Scissors) Switch
2.12.2
2-59
DUAL-ENGINE FAILURE
12.14
12-16
Dual-Engine Failure During Flight (Autorotative Landing)
12.14.2
12-18
Dual-Engine Failure While Hovering at Low Altitude
12.14.1
12-18
Dual-Engine Landing Approach and Transition to a Hover
7.14.1
7-22
Dual-Engine Vertical Landing
12.33.5
12-42
Dual-Engine Vertical Water Takeoff
12.34.4
12-43
During Flight
14.1.8
14-3
Duties of Personnel
7.19.2
7-27
E
Effects of High Altitude
11.3.3
11-6
ELECTRICAL MALFUNCTION
12.21
12-27
ELECTRICAL POWER SUPPLY SYSTEM
2.6
2-34
EMERGENCIES
18.9
18-5
Emergency Aircrew Procedures
16.2.3
16-8
EMERGENCY DESCENT
12.17
12-18
EMERGENCY ENTRANCES AND EXITS
12.35
12-47
EMERGENCY EQUIPMENT
2.23
2-90
Emergency Jettison Procedures
12.39.2
12-51
Emergency Procedures
17.6
17-18
EMERGENCY ROTOR ENGAGEMENT
12.3
12-1
EMERGENCY WATER OPERATIONS
12.33
12-40
Emergency Water Towing With Emergency Floats Inflated
12.34.8
12-46
En Route
18.4.8
18-3
INDEX-4
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
ENDURANCE CHART
25.6
25-2
ENDURANCE CHARTS
24.1
24-1
Engine Air Inlet Anti-Icing System
2.19.1
2-83
Engine Anti-Ice Switches
2.19.3
2-84
Engine Anti-Icing System
2.19.2
2-84
Engine Control System
2.1.4
2-12
Engine Controls
2.1.5
2-14
ENGINE FAILURE
12.11
12-7
Engine Fire In Flight
12.4.2
12-2
Engine Fire on the Ground
12.4.1
12-1
Engine Fuel System
2.1.3
2-1
ENGINE GASPATH PROCEDURES
9.5
9-12
Engine Gaspath Procedures
9.5.7
9-15
Engine Instruments
2.1.6
2-15
Engine Limitations (T58-GE-402)
4.1.2
4-1
ENGINE MALFUNCTIONS
12.7
12-4
Engine Oil Pressure Fluctuations
12.9.6
12-6
Engine Oil Servicing
3.2.5
3-9
ENGINE OIL SYSTEM
2.2
2-21
Engine Performance - 691 °C T5 Chart
20.7.2
20-3
Engine Performance - 727 °C T5 Chart
20.7.1
20-3
Engine Ratings
1.1.2
1-2
Engine Shutdown in Flight
12.11.6
12-9
Engine Trim Checker (H219)
2.24.2
2-94
Erroneous Doppler Indicators.
18.10.2
18-10
ET APU Servicing
3.2.14
3-10
ET Cabin Emergency Exit Hatches
12.41
12-54
ET Environmental Air System
2.18.6
2-76
ET Exterior
12.41.2
12-54
ET Interior
12.41.1
12-54
ET Passenger Accommodations
2.21.3
2-86
Exterior
10.2.1
10-6
Exterior Lights
2.7.2
2-47
Exterior Release Handle
12.40.5
12-53
External Electrical Power Connections
3.1.1
3-1
EXTERNAL POWER REQUIREMENTS
3.1
3-1
F
Factors Affecting Range and Endurance
6.1.1
6-1
Familiarization
7.16.1
7-25
FINAL GRADE DETERMINATION
19.4
19-9
INDEX-5
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
FIRE
12.4
12-1
FIRE DETECTOR SYSTEM
2.17
2-73
Fire Extinguishing System
2.23.1
2-90
Fire Warning Lights and Test Switch
2.17.1
2-73
First Start (KY-58)
15.6.1
15-10
First-Aid Kits
2.23.7
2-93
FLEXIBLE DRIVE SHAFT FAILURE
12.11.14
12-13
Flight Crew Qualification
17.5
17-18
Flight Crew Qualification (Weapons Recovery)
5.2
5-1
FLIGHT CHARACTERISTICS
11.2
11-1
FLIGHT CHARACTERISTICS
12.10
12-7
FLIGHT CHECKS
10.3
10-27
FLIGHT CONTROL HYDRAULIC SERVO SYSTEM
12.22
12-30
Flight Control Malfunction
12.22.1
12-30
FLIGHT CONTROL SERVO HYDRAULIC SYSTEMS
2.8
2-48
Flight Control Servo Switch
2.8.3
2-49
FLIGHT CONTROL SERVO UNIT MALFUNCTION
12.24
12-31
FLIGHT CONTROL SYSTEM
2.9
2-49
FLIGHT CONTROLS JAMMED OR RESTRICTED
12.23
12-31
Flight Crew Qualifications
5.7.1
5-5
Flight Deck
8.2.3
8-1
FLIGHT EVALUATION
19.3
19-2
Flight Evaluation Grade Determination
19.3.8
19-9
Flight Evaluation Grading Criteria
19.3.1
19-2
FLIGHT INSTRUMENTS
2.15
2-63
Flight Preparation
17.7
17-18
FLIGHT TIME SUMMARY
5.6
5-5
Flight With Ice Shield
14.1.1
14-1
FLIGHT/HANGAR DECK PROCEDURES
8.2
8-1
Flight/Hangar Deck Procedures
8.4.1
8-12
FLIGHTCREW QUALIFICATIONS
5.2
5-1
Flood/Hover Lights
4.1.19
4-6
Flotation Bag Limitations
4.1.18
4-6
Flotation Bags
12.33.4
12-41
Flotation Gear System
2.23.4
2-93
Fluid Servicing and Capacities
3.2.15
3-11
Formation
18.5.2
18-4
Formation Composition
9.1.1
9-1
Formation Leader
6.4.1
6-2
FORMATION/TACTICS
9.1
9-1
Forms and Records
19.5.1
19-9
Forward Flight Checks
10.3.2
10-38
Free Turbine Speed (Nf)
2.1.2
2-1
Free-Air Temperature Gauge
2.15.2
2-63
Freshwater Wash
9.5.1
9-13
Fuel Boost Pump Failure
12.5.1
12-3
FUEL CONTROL CONTAMINATION
12.11.15
12-14
Fuel Crossfeed
7.12.1
7-21
Fuel Crossfeed Malfunctions
12.5.2
12-4
INDEX-6
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
FUEL CROSS-REFERENCE
3.4
3-13
Fuel Dump System
2.5.4
2-33
Fuel Dumping Afloat
12.33.3
12-41
Fuel Dumping in Flight
7.12.3
7-21
Fuel Filter Bypass
12.5.3
12-4
FUEL SYSTEM
2.5
2-30
FUEL SYSTEM FAILURE
12.5
12-3
Fuel System Limitations
4.1.3
4-1
Fuel System Management
2.5.3
2-33
Fuel System Servicing
3.2.1
3-4
Functional Checkflight Pilot Qualification
10.1.2
10-1
FUNCTIONAL CHECKFLIGHT PROCEDURES
10.1
10-1
Functional Checkfllght Procedures
18.5.1
18-4
Fuselage or Electrical Fire
12.4.3
12-2
G
Gas Generator Compressor Speed (Ng)
2.1.1
2-1
Gaspath Engine Burnout
9.5.9
9-15
Gaspath Engine Rinse
9.5.8
9-15
Gearbox Allowable Oil Leakage
4.1.6
4-5
General Safety Precautions
7.19.1
7-27
Grading Instructions
19.2.5
19-2
Gravity Refueling Procedures
3.2.2
3-4
GROUND EVALUATION
19.2
19-2
Ground Operation of Helicopter Engines and Rotors
7.2.2
7-1
Ground Resonance
11.2.2
11-1
GROUND TRAINING REQUIREMENTS
5.1
5-1
GROUNDSPEED AND DRIFT ANGLE INDICATOR
15.18
15-23
Guillotine
18.12.12
18-16
H
Hand Signals
8.3.9
8-12
Hangar Deck
8.2.1
8-1
Hangar Flight Deck
8.2.2
8-1
Hardover in the Fore-and-Aft Primary Servo or Blocked Common Return in
12.24.3
12-32
One Auxiliary Servo
Heater Fire
12.4.4
12-3
Heater/Air Conditioner Fire (UH-3H Executive Transport)
12.40.2
12-53
Heating and Ventilating Diffusers
2.18.3
2-74
HEATING SYSTEM
2.18
2-73
Height Velocity Diagram - One-Engine Failure Chart
25.1.2
25-1
Height Velocity Diagram - Two-Engine Failure Chart
25.1.1
25-1
HEIGHT VELOCITY DIAGRAMS
25.1
25-1
Helicopter Acceptance
7.2.5
7-2
Helicopter Emergency Egress Lighting System
2.23.3
2-91
Helicopter External Load Jettison
12.39.1
12-51
HELICOPTER IN-FLIGHT REFUELING PROCEDURES (HIFR)
9.4
9-8
Helicopter In-Flight Refueling System
2.5.2
2-33
INDEX-7
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
HELICOPTER LIGHTING
7.17
7-26
HELICOPTER TIEDOWN AND SECURING
3.8
3-17
Helicopter Tiedown and Securing Diagram
3.8.3
3-18
HELICOPTER TOWING
3.6
3-16
HELICOPTER WEAPONS RECOVERY SYSTEM PREFLIGHT PROCEDURES
17.7.4
17-20
HIFR Procedures
9.4.5
9-10
HIFR Systems
9.4.2
9-9
HIGH SPEED SHAFT (POWER TURBINE SHAFT)
12.11.10
12-10
Holding
13.3.5
13-3
Horizontal Adjustment Control Lever
2.20.2
2-85
HOVER CHARTS
21.1
21-1
Hover Checks
10.3.1
10-27
Hover Endurance - Two-Engine Chart
24.1.2
24-1
Hover Indicators
2.10.3
2-55
HOVER TRIM Control Panel
2.10.4
2-57
Hovering
7.9.2
7-19
Hovering Limitations
4.1.12
4-6
HUNG DROOP STOPS
12.29
12-36
Hydraulic System Fluid Servicing
3.2.6
3-9
I
Ice Shield Installation
20.1.2
20-1
ICE, RAIN, AND SNOW
14.1
14-1
IFF Control Panel
15.15.3
15-17
IFF Caution Light
15.15.3.7
15-18
Ignition System
2.1.8
2-19
Illumination of Servo System Caution Light
12.22.3
12-31
Immediate Emergency Procedures
12.11.1
12-7
Impending Rotary Rudder System Failure
12.20.4
12-27
Implementation
19.1.1
19-1
In Flight
12.23.2
12-31
Inadvertent Fuel Dumping in Flight
12.5.4
12-4
INADVERTENT OPENING AND/OR LOSS OF ACCESS PANELS/DOORS
12.36
12-50
Indicated Torque Required to Hover In Ground Effect - 10-Foot Chart
21.1.1
21-1
Indicated Torque Required to Hover Out of Ground Effect Chart
21.1.2
21-1
Inform Pilot
18.12.9
18-16
Inputs
15.20.1
15-24
Instrument Approaches
13.3.7
13-3
Instrument Check
9.3.1
9-6
Instrument Climb
13.3.3
13-2
Instrument Cruising Flight
13.3.4
13-2
Instrument Descent
13.3.6
13-3
INSTRUMENT FLIGHT CONDITIONS IN FORMATION
9.2
9-6
INSTRUMENT FLIGHT PROCEDURES
13.3
13-1
Instrument Procedures
18.4.9
18-3
Instrument Takeoff
13.3.2
13-2
Interior
10.2.2
10-6
Interior Lights
2.7.1
2-45
Interior Release Handle
12.40.4
12-53
INDEX-8
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
Intermediate and Tail Gearbox Oil Systems
2.4.4
2-28
Intermediate Gearbox
2.4.2
2-28
Intermediate Gearbox Servicing
3.2.10
3-9
Internal Fuel System
2.5.1
2-30
Interphone Control Panels
15.3.1
15-4
Interphone Operation
15.3.2
15-5
INTERPHONE-RADIO CONTROL SYSTEM (ICS)
15.3
15-1
J
Jammed Rescue Hoist
18.12.11
18-16
Jettison
12.11.5
12-9
K
Key Components of Flightcrew Coordination
18.2.1
18-1
KY-58 SPEECH SECURITY SYSTEM
15.6
15-10
L
Land-Based (Day)
7.17.1
7-26
Land-Based (Night)
7.17.2
7-26
LANDING
7.14
7-22
Landing
18.4.12
18-4
Landing After Attaining a Hover
7.14.2
7-22
Landing Considerations
8.3.7
8-12
LANDING DISTANCE GROUND ROLL - POWER-OFF
25.7
25-2
Landing Gear Actuating Lever
2.12.1
2-59
Landing Gear Emergency System
2.12.5
2-60
LANDING GEAR FAILURE
12.28
12-35
Landing Gear Fails to Retract
12.28.2
12-36
Landing Gear Position Indicators
2.12.4
2-59
LANDING GEAR SYSTEM
2.12
2-58
Landing Gear Warning Light
2.12.3
2-59
LANDING IN TREES
12.16
12-18
Landing Site Evaluation
11.3.2
11-5
Landing With Wheels Retracted or Improperly Lowered
12.28.1
12-35
Launch and Recovery Procedures
8.4.2
8-13
LAUNCHING AND RECOVERY PROCEDURES
8.3
8-4
Level Flight Characteristics Under Various Speed Conditions
11.2.1
11-1
LF AUTOMATIC DIRECTION FINDER (AN/ARN-59)
15.13
15-15
LF Automatic Direction Finder Operation
15.13.2
15-15
LF/ADF Control Panel
15.13.1
15-15
Liferaft
2.23.5
2-93
LIGHTING EQUIPMENT
2.7
2-45
LIMITATIONS
4.1
4-1
LINE OPERATIONS
7.2
7-1
Line Safety
7.2.1
7-1
Load Oscillation Techniques
12.39.3
12-52
Long-Term Parking
3.7.2
3-17
Lookout Doctrine
18.12.1
18-12
INDEX-9
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
Loss of ASE
12.32.6
12-39
Loss of Attitude Indicator
12.32.7
12-39
Loss of Doppler Receiver
12.32.1
12-37
Loss of Doppler Transmitter
12.32.2
12-38
Loss of Flightcrew Coordination
18.2.2
18-2
Loss of Generator
12.32.9
12-40
LOSS OF Ng SIGNAL TO FUEL CONTROL
12.11.12
12-12
LOSS OF P3 SIGNAL TO FUEL CONTROL
12.11.13
12-12
Loss of Radar Altimeter
12.32.4
12-38
Lost Sight During IFR Flight Procedures
9.2.1
9-6
LUBE PUMP OR SHAFT FAILURE
12.11.9
12-10
M
M-60-D MACHINEGUN SYSTEM
16.2
16-2
MAGR
15.20.10
15-30
Main Gearbox
2.4.1
2-24
Main Gearbox Oil Servicing
3.2.7
3-9
MAIN GEARBOX SYSTEM FAILURE
12.18
12-18
Main Gearbox Torque Limitations
4.1.8
4-5
Main Rotor Blade Tiedown
3.8.2
3-17
MAIN ROTOR OVERSPEED
12.19
12-21
Malfunction of Stick Trim
12.32.5
12-39
Maneuvers
4.1.11
4-6
Manual Approach Procedures
18.12.5
18-13
Manual Blade Folding Procedures
7.20.2
7-30
Map Case and Chart Board
2.24.3
2-95
Marine Markers Deployment Limitations
4.1.26
4-7
Maximum Continuous Operating Time
4.1.7
4-5
Maximum Endurance - Two-Engine Chart
24.1.1
24-1
MAXIMUM GLIDE
12.15
12-18
MAXIMUM RANGE
12.12
12-14
Maximum Range (-10) - Two-Engine Chart
23.1.1
23-1
Maximum Range (-402) - Normal Power Two-Engine Chart
23.1.5
23-2
MINIMUM ACCEPTABLE INDICATED TORQUE AND ENGINE
20.7
20-3
PERFORMANCE CHARTS
Minimum Crew Requirements
4.1.1
4-1
Mirror/Optical Landing System Approach
8.3.4
8-12
Mirrors Rearview
2.24.6
2-96
MISCELLANEOUS
2.24
2-93
Mission Checklist
9.7.1
9-17
MISSION PLANNING
6.1
6-1
Mission/Flight Planning
18.4.1
18-2
MISSION/SPECIAL CONSIDERATIONS
18.5
18-4
MK 146 MOD 0 HELICOPTER LAUNCH SYSTEM PROCEDURES
17.8.1
17-21
MK 146 MOD 0 LAUNCH SYSTEM (USED WITH MK 30 TARGETS)
17.2.1
17-1
MK 2 MOD 0/1 HELICOPTER WEAPON RECOVERY SYSTEM
17.2.3
17-8
INDEX-10
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
Mk 2 Mod 0/1 Entanglement Procedures
12.39.4
12-52
MK 2 MOD 0/1 HELICOPTER WEAPON RECOVERY PROCEDURES
17.8.3
17-32
MK 4 MOD 0 HELICOPTER DEPLOYED LIGHTWEIGHT RECOVERY SYSTEM
17.2.2
17-6
MK 4 MOD 0 HELICOPTER-DEPLOYED LIGHTWEIGHT TORPEDO
17.8.2
17-25
RECOVERY SYSTEM PROCEDURES
MK25 Marine Locator Marker
16.1.1
16-1
MK58 Marine Locator Marker
16.1.2
16-1
Mooring Rings
2.24.4
2-95
MOUNTAIN AND ROUGH TERRAIN FLYING
11.3
11-5
N
NATOPS FLIGHT EVALUATION
5.3
5-4
NAVIGATION
6.2
6-1
Navigation Processing
15.20.2
15-24
Nf Tachometer Fluctuations
12.9.4
12-6
Nf Tachometer System Malfunction
12.9.3
12-5
Ng Tachometer Fluctuations
12.9.2
12-5
Ng Tachometer System Malfunctions
12.9.1
12-5
Night and IFR Operations
8.3.3
8-11
NIGHT FLYING
7.16
7-25
Night Formation
9.1.7
9-6
Night/IFR Search and Rescue Procedures
18.12.14
18-17
NIGHT/INSTRUMENT FLIGHT RULES ALTERNATE/AUTOMATIC
18.7
18-4
APPROACHES AND DEPARTURES
Night/Low Visibility HIFR Approach
9.4.6
9-12
No. 1 Engine Checks
10.2.4
10-10
No. 1 Engine Secure
7.20.3
7-31
No. 1 Engine. Burnout
9.5.2
9-13
No. 2 Engine Burnout
9.5.4
9-14
No. 2 Engine Checks
10.2.6
10-20
No.1 Engine Secure
9.5.6
9-14
No.1 Engine secure (FCF)
10.4.2
9-14
Non-operational Briefing
6.4.4
6-2
Normal Operation (Heater)
2.18.4
2-74
Normal Operation (Rescue Hoist)
2.22.4
2-89
Normal Operation
9.4.3
9-9
NORMAL STARTING PROCEDURES
7.4
7-8
Nr Tachometer System Malfunction
12.9.9
12-7
O
OIL CROSS-REFERENCE
3.5
3-14
Oil Pressure Failure
12.9.7
12-6
Oil Temperature System Malfunction
12.9.8
12-6
OILS, GREASES, HYDRAULIC FLUIDS LISTINGS
3.3
3-12
Open-Book Examination
19.2.1
19-2
Operating Limits
17.4
17-18
Operational Flight Trainer/Weapon Systems Trainer Procedures Evaluation 19.2.4
19-2
Optimum Cross-Country Chart
23.1.2
23-1
INDEX-11
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
Oral Examination
19.2.3
19-2
Overspeed Protection System
2.1.10
2-20
P
PARKING
3.7
3-17
Parking Brake Handle
2.12.9
2-61
Performance
1.1.1
1-1
PERSONAL FLYING EQUIPMENT
5.4
5-4
Personnel Door
12.35.2
12-50
Pickup
18.14.3
18-24
Pilot Compartment Jettisonable Window Assembly
12.35.1
12-47
Pilot Evaluation
19.3.2
19-2
Pilot Evaluation
5.3.1
5-4
Pilot Evaluation Worksheet
19.3.4
19-4
Pilot Ground Training
5.1.1
5-1
Pilot in Command
6.4.2
6-2
Pilot Oral Emergency Worksheet
19.3.3
19-3
Pilot Procedure for External Cargo Sling Operation
18.13.3
18-22
Pilot Qualifications
5.2.1
5-1
Pitot Heaters
2.18.5
2-74
Pitot-Static System
2.15.4
2-63
Portable Fire Extinguisher
2.23.2
2-91
POSTFLIGHT
7.21
7-31
Postflight
18.4.14
18-4
Postflight Inspection
10.4.3
10-49
Post-landing/Taxi/Shutdown
18.4.13
18-4
Postshutdown Engine Fire
12.4.6
12-3
POSTTAKEOFF
7.11
7-20
POWER PLANT SYSTEMS
2.1
2-1
Power Supply Failure
12.25.1
12-32
Practice Autorotation
7.15.1
7-23
Practice Single-Engine Approach
7.14.5
7-23
PREFLIGHT
17.7.3
17-20
Preflight
18.4.3
18-3
PREFLIGHT CHECKS
10.2
10-6
Preflight Inspection
7.2.7
7-2
Pressure Refueling Aboard Ship With the Rotors Engaged
8.2.4
8-2
PRESSURE REFUELING WITH ROTORS ENGAGED ASHORE
7.19
7-27
Pressure-Refueling Procedures
3.2.3
3-5
Prestart Checks
10.2.3
10-6
PRETAKEOFF
7.8
7-18
Pretakeoff Checks
10.2.8
10-24
Primary Flight Control Servo System
2.8.1
2-48
Procedures
18.12.3
18-12
Purpose
17.1.1
17-1
PYLON FOLDING
2.14
2-62
INDEX-12
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
Q
Qualifications for Functional Checkflight Aircrewman
10.1.4
10-1
R
Radar Altimeter
2.15.10
2-67
Radar Altitude Warning System
2.15.11
2-67
RADIO MAGNETIC INDICATOR
15.14
15-16
Radio Operating Controls
15.2.1
15-1
RAIN INGESTION
12.8
12-5
RANGE CHART
25.5
25-2
RANGE CHARTS
23.1
23-1
Recommended Dual Concurrence Items
12.2.1
12-1
RECORDS AND REPORTS
19.5
19-9
Recovery Signals
8.3.5
8-12
Relief Tube
2.24.5
2-96
Rendezvous
9.1.2
9-5
RESCUE HOIST
2.22
2-88
Rescue Hoist Assist Handles
2.22.8
2-90
Rescue Hoist Cable Shear Switches
2.22.5
2-89
Rescue Hoist Limitations
4.1.17
4-6
RESCUE HOIST MALFUNCTION
12.27
12-33
Rescue Hoist Manual Override Valve
2.22.7
2-90
Rescue Hoist Master Switch
2.22.1
2-88
Rescue Hoist Shear Circuit Test Panel
2.22.6
2-90
Rescue Hoist Switch Panel
2.22.2
2-88
Rescue Situation
18.12.13
18-16
Responsibility
9.1.4
9-5
Restraint System Control Lever
2.20.3
2-85
Rollover Characteristics
11.2.6
11-3
Rotary Rudder Control System Failure
12.20.3
12-23
Rotary Rudder Drive System Failure
12.20.1
12-22
Rotary Rudder Drive System Failure While Hovering
12.20.2
12-23
Rotary Rudder Flight Control System
2.9.2
2-52
Rotary Rudder System
2.3.3
2-23
ROTARY RUDDER SYSTEM FAILURES
12.20
12-21
Rotary Wing Blade Folding
2.13.1
2-61
Rotary Wing Flight Control System
2.9.1
2-49
Rotary Wing System
2.3.1
2-22
Rotor Brake
2.4.7
2-29
ROTOR BRAKE CAUTION LIGHT
12.30
12-36
ROTOR BRAKE FAILURE
12.31
12-36
Rotor Disengagement
7.20.1
7-29
ROTOR SYSTEMS
2.3
2-22
Run-On Landings
7.14.3
7-22
INDEX-13
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
S
Sample Problem for Use of Ability To Maintain 70 Knots at Various Rotor
25.4.1
25-2
Speeds - One-Engine Chart
Sample Problem for Use of Ability To Maintain Level Flight - One-Engine
25.3.1
25-1
Chart
Sample Problem for Use of Airspeed Calibration Chart
20.2.1
20-2
Sample Problem for Use of Blade Stall Chart
20.6.1
20-3
Sample Problem for Use of Density Altitude Chart
20.4.1
20-2
Sample Problem for Use of Landing Distance Ground Roll - Power-Off
25.7.1
25-2
Chart
Sample Problem for Use of Temperature Conversion Chart
20.3.1
20-2
Sample Problem for use of Maximum Range (-402) Two Engine Chart
23.1.4
23-1
Sample Problem for Use of Torque Versus Engine Horsepower Chart
20.5.1
20-2
Sample Problem for Use of Unit Range and Fuel Flow Conversion Chart
23.1.7
23-2
Sar Freestream Recovery
12.32.8
12-39
SAR FREESTREAM RECOVERY
18.10.4
18-11
SAR LOST ICS PROCEDURES
18.11
18-11
SEARCHES AND RESCUE
18.12
18-12
SEARCHES AND RESCUE
18.8
18-4
Servicing
17.3
17-18
SERVICING DATA
3.2
3-4
Servo Hydraulic Pressure Failure
12.22.2
12-31
Servo Hydraulic Pressure Indicators
2.8.4
2-49
Settling With Power
11.2.3
11-1
Settling With Power
12.10.2
12-7
Shipboard Wind Limits
4.1.22
4-6
Shipboard Wind Limits
8.3.1
8-10
Shore-Based Procedures
17.8
17-21
Short-Term Parking
3.7.1
3-17
Shutdown (FCF)
10.4.1
10-49
SHUTDOWN
7.20
7-28
Shutdown (Ship-Based)
8.3.8
8-12
SHUTDOWN CHECKS
10.4
10-49
Sidelobe Lock-On
12.32.3
12-38
Signals
9.1.6
9-5
SIMULATED INSTRUMENT PROCEDURES
13.2
13-1
SINGLE INSTRUMENT INDICATIONS
12.9
12-5
Single-Engine Failure in Flight
12.11.4
12-8
Single-Engine Failure on Takeoff
12.11.2
12-8
Single-Engine Failure or Loss of Power in an Overwater Hover
12.33.7
12-42
Single-Engine Failure or Loss of Power While Hovering
12.11.3
12-8
SINGLE-ENGINE LANDING (LAND OR SHIP)
12.13
12-16
Single-Engine Restart During Flight
12.11.7
12-9
Single-Engine Water Landing
12.33.6
12-42
Single-Engine Water Takeoff
12.34.5
12-43
Single-Engine Waveoff
12.13.1
12-16
Sleeve-Spindle Oil Tanks, Self-Lubricated Rotary Wing Head Servicing
3.2.9
3-9
Smoke and Fume Elimination (UH-3H Executive Transport)
12.40.1
12-53
Smoke Lights
16.1
16-1
INDEX-14
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
Smoke/Fume/Noxious Gas Elimination
12.4.5
12-3
SPECIAL CHECKLISTS (UH-3H EXECUTIVE TRANSPORT)
9.7
9-17
SPECIAL EQUIPMENT REQUIRED
17.7.5
17-21
SPECIFIC RESPONSIBILITIES
18.4
18-2
Standard Terms
18.12.7
18-14
Standby Compass
2.15.1
2-63
Start and Engagement
18.4.4
18-3
STARTER HANGUP
12.6
12-4
Starter Limitations
4.1.4
4-1
Starter System
2.1.7
2-18
STARTING NO. 2 ENGINE AND ROTOR ENGAGEMENT
7.6
7-15
Static Displays
9.6.1
9-16
Stores
4.1.21
4-6
Straight-and-Level
9.3.2
9-6
Swimmer Rescue Hand Signals
18.12.8
18-15
System Tests
15.20.3
15-24
SYSTEMS CHECKLIST
7.5
7-11
Systems Checks
10.2.5
10-14
T
T5 System Malfunction
12.9.5
12-6
TACAN Control Panel
15.11.1
15-13
Tacan Navigation Set (AN/ARN-118(V)) Operation
15.11.2
15-14
TACAN SET (AN/ARN-118(V))
15.11
15-12
TACCO Panel
15.20.5
15-27
TACNAV Display
15.20.7
15-29
TACNAV Operating Procedures
15.20.8
15-29
TACNAV Processor Unit
15.20.4
15-27
Tactical Navigation System
6.2.1
6-1
Tail Gearbox
2.4.3
2-28
Tail Gearbox Servicing
3.2.11
3-9
Tail Pylon Unlock Light
12.20.5
12-27
Tail Takeoff Freewheel Unit Caution Light
12.18.1
12-20
Tailwheel Lock Handle
2.12.6
2-60
Takeoff
18.4.6
18-3
TAKEOFF CHECKLIST
7.9
7-18
Takeoff Procedures
7.9.1
7-18
TARGET DRONE RECOVERY SYSTEM OPERATING PROCEDURES
17.8.4
17-36
TARGET TORPEDO DRONE RECOVERY
17.2.4
17-9
Taxi (FCF)
10.2.7
10-24
Taxi
18.4.5
18-3
Taxi Limitations
4.1.23
4-6
TAXIING
7.7
7-17
Taxiing
14.1.5
14-2
Taxiing (Shore Based)
7.2.3
7-1
Taxiing Procedure
7.7.1
7-17
TEMPERATURE CONVERSION CHART
20.3
20-2
INDEX-15
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
TERRAIN FLYING
11.4
11-9
Tiedown Procedures
3.8.1
3-17
Tipover Limitations
4.1.25
4-7
Tire Servicing
3.2.13
3-10
To Secure Crossfeed
7.12.2
7-21
Torque Sensing System
2.1.9
2-19
Torque Sensing System Failure
12.18.2
12-21
TORQUE VERSUS ENGINE HORSEPOWER CHART
20.5
20-2
Towing
7.2.4
7-2
Towing Procedures
3.6.2
3-16
Traffic Patterns
8.3.2
8-10
TRAINING
18.6
18-4
TRANSITION TO CLIMB
7.10
7-20
Transmission Limitations
4.1.5
4-1
Transmission Oil Systems
2.4.6
2-28
TRANSMISSION SYSTEM
2.4
2-24
Transponder Test Set
15.15.2
15-17
Trimble Pack
15.20.9
15-30
Troop Seats
2.21.1
2-85
TROOP-CARRYING EQUIPMENT
2.21
2-85
TRUE AIRSPEED TRANSDUCER
15.19
15-23
Turbulent-Air Flight Techniques
11.3.4
11-6
Turn Rate Switches
2.15.8
2-65
Turns
9.3.3
9-8
Turns Using Automatic Stabilization Equipment
7.12.4
7-21
U
UH-3H EXECUTIVE TRANSPORT EMERGENCY PROCEDURES
12.40
12-53
UHF Antenna Selector Switch
15.4.2
15-9
UHF/ADF GROUP
15.7
15-10
UHF/ADF GROUP OPERATION
15.8
15-11
UHF/COMM (AN/ARC-159)
15.4.1
15-8
UHF/COMM SET (AN/ARC-159)
15.4
15-8
UHF/VHF/COMM (AN/ARC-182)
15.5.1
15-9
UHF/VHF/COMM SET (AN/ARC-182 (UH-3H))
15.5
15-9
Uncoupled Indications
12.24.2
12-32
UNDERWATER EGRESS
12.37
12-50
Unit Range and Fuel Flow Conversion Chart
23.1.3
23-1
Unit Range and Fuel Flow Conversion Chart (-402)
23.1.6
23-2
Unusual Attitudes
9.3.5
9-8
USAF Ground Power Units
3.1.2
3-1
Use of Hot Mike
18.12.10
18-16
Utility Hydraulic Pressure Indicator
2.11.1
2-58
UTILITY HYDRAULIC SYSTEM
2.11
2-58
UTILITY HYDRAULIC SYSTEM FAILURE
12.26
12-33
INDEX-16
ORIGINAL
NAVAIR-01-230HLH-1
Paragraph
Page No
V
Variable-Load Energy Absorber Control Dial
2.20.4
2-85
Vertical Adjustment Control Lever
2.20.1
2-85
Vertical Gyros
2.10.7
2-58
VHF Radio Receiver
15.10
15-12
VHF/COMM Operation
15.9.2
15-12
VHF/COMM SET (AN/ARC-186(V))
15.9
15-11
VHF/COMM SET (AN/ARC-186(V))
15.9.1
15-11
VHF/NAV SET (AN/ARC-126)
15.11.3
15-14
VHF/NAV SET (AN/ARC-126) Control Panel
15.11.4
15-14
Vibration Troubleshooting
10.1.7
10-2
Vibratory Forces
12.24.4
12-32
VISUAL COMMUNICATION - IN FLIGHT
15.21
15-31
Vortex Ring State
11.2.4
11-2
Vortex Ring State
12.10.1
12-7
W
Warmup and Ground Check
14.1.4
14-2
WARNING, CAUTION, AND ADVISORY LIGHTS
2.16
2-68
Water Drops
18.14.4
18-24
Water Landing (Controlled)
12.34.2
12-43
Water Landing (Uncontrolled)
12.34.1
12-43
Water Shutdown Procedures
12.34.6
12-46
Water Taxiing
12.33.2
12-41
Waveoff Procedures
8.3.6
8-12
Weapon Description
16.2.1
16-2
Weapon Operating Procedures
16.2.2
16-5
WEAPON RECOVERY EMERGENCIES
12.39
12-51
Weapon Recovery Indoctrination
5.7
5-5
Weapon Recovery Limitations
4.1.27
4-7
WEIGHT AND BALANCE
6.3
6-1
Weight Limitations
4.1.16
4-6
Wheelbrake System
2.12.7
2-61
Wind Direction and Velocity
11.3.1
11-5
Windshield Anti-Ice System
2.19.4
2-84
Windshield Washer
2.24.8
2-96
Windshield Washer Reservoir Servicing
3.2.12
3-9
Windshield Wiper System
2.24.7
2-96
INDEX-17
ORIGINAL
NAVAIR-01-230HLH-1
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INDEX-18
ORIGINAL

 

 

 

 

 

 

 

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