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BMS F-16C/D 4.34 - User Manual

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T.O. BMS1F-16CM-1 BMS 4.34 Change 2.00
BMS 4.34 Dash 1
© Red Dog 2012-2019 Page: 1
T.O. BMS1F-16CM-1
FLIGHT MANUAL
Combatsimchecklist series
F-16C/D BMS 4.34
Block 50 and 52
23 March 2019
CHANGE 2.00

Table of Contents

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Summary

LIST OF EFFECTIVE CHANGES

Change 2: (4.34)

Details updates for BMS 4.34, including general changes.

Change 1: (4.33)

Details updates for BMS 4.33, including specific system additions.

Change 0: (4.32)

Details the initial release version for BMS 4.32.

COPYRIGHT STATEMENTS

SECTION I DESCRIPTION & OPERATION

1.1 THE AIRCRAFT

Overview of the F-16 aircraft, including weights, dimensions, and speed characteristics.

1.2 COCKPIT ARRANGEMENT

Detailed layout and identification of all panels and controls within the F-16 cockpit.

1.2.1. LEFT CONSOLE

Description of the panels and controls located on the pilot's left console.

1.2.2. LEFT AUXILIARY CONSOLE

Description of the panels and controls on the left auxiliary console.

1.2.3. CENTRE CONSOLE

Description of the panels and instruments located on the center console.

1.2.4. RIGHT AUXILIARY CONSOLE

Description of the panels and instruments located on the right auxiliary console.

1.2.5. RIGHT CONSOLE

Description of the panels and controls located on the pilot's right console.

1.2.6. MISCELLANEOUS

Covers a few controls accessible to the pilot but not from cockpit controls.

1.3 UP FRONT CONTROLS

Detailed explanation of the Up Front Controls (UFC), including ICP and DED.

1.4 MULTI FUNCTION DISPLAYS

Explanation of the Multi Function Displays (MFDs) and their pages.

1.5 THE HEAD UP DISPLAY (HUD)

Explanation of the Heads Up Display (HUD) features and symbology.

1.6 THE ENGINE

Description of the F-16's engine system, modes, and instruments.

1.7 FUEL SYSTEM

Detailed explanation of the F-16 fuel system, tanks, and indications.

1.8 ENVIRONMENTAL CONTROL SYSTEM (ECS)

Description of the Environmental Control System (ECS) and its functions.

1.9 ELECTRICAL SYSTEM

Overview of the F-16's complex electrical system and its components.

1.10 HYDRAULIC SYSTEM

Description of the hydraulic systems supplying power to flight controls.

1.11 EMERGENCY POWER UNIT (EPU)

Explanation of the Emergency Power Unit (EPU) functions and operation.

1.12 FLIGHT CONTROL SYSTEM (FLCS)

Detailed explanation of the Flight Control System (FLCS) and its modes.

1.13 LANDING GEAR & BRAKES

Description of the landing gear operation and braking system.

1.14 AUTOPILOT OPERATION

Explanation of the F-16's autopilot system modes and operation.

1.15 INSTRUMENT LANDING SYSTEM

Description of the Instrument Landing System (ILS) and its cockpit controls.

1.16 IDENTIFICATION FRIEND or FOE (IFF)

Explanation of the Identification Friend or Foe (IFF) system and modes.

SECTION II NORMAL PROCEDURES

2.1. RAMP START in 3 SWEEPS

A step-by-step guide to starting the F-16 aircraft from ramp.

2.2. REFUELLING

Procedures for hotpit and air-to-air refuelling operations.

2.3. LANDING

Procedures for visual and instrument landing approaches.

SECTION III ABNORMAL & EMERGENCY PROCEDURES

3.1. WARNING AND CAUTION LIGHT AND PILOT FAULT SYSTEM

Understanding aircraft warning lights, caution lights, and fault displays.

3.2. WARNING LIGHT ANALYSIS

Analysis of specific warning lights and their associated causes.

3.3. CAUTION LIGHT ANALYSIS

Analysis of specific caution lights and their associated causes.

3.4. FAULT ANALYSIS

Detailed analysis of aircraft faults, including MFL and PFL.

3.5. GROUND EMERGENCIES

Procedures for handling emergencies that occur while on the ground.

3.6. TAKEOFF EMERGENCIES

Procedures for handling emergencies during the takeoff phase.

3.7. IN FLIGHT EMERGENCIES

Procedures for handling emergencies that occur during flight.

3.8. LANDING EMERGENCIES

Procedures for handling emergencies during the landing phase.

SECTION IV FLIGHT CHARACTERISTICS

4.1 Limit Cycle Oscillation

Description of complex buffeting and stores flutter phenomena.

4.2 Descent Warning Advisory

System providing audio warnings for unintended descents.

4.3 Category Loading

How aircraft configuration affects G-limits and departure susceptibility.

4.4. Departure from controlled flight

Understanding and recovering from aircraft departures.

4.5 Operating Limits & Restrictions

Engine limits and aircraft operating restrictions.

5. BIBLIOGRAPHY

6. ACKNOWLEDGMENT

Summary

LIST OF EFFECTIVE CHANGES

Change 2: (4.34)

Details updates for BMS 4.34, including general changes.

Change 1: (4.33)

Details updates for BMS 4.33, including specific system additions.

Change 0: (4.32)

Details the initial release version for BMS 4.32.

COPYRIGHT STATEMENTS

SECTION I DESCRIPTION & OPERATION

1.1 THE AIRCRAFT

Overview of the F-16 aircraft, including weights, dimensions, and speed characteristics.

1.2 COCKPIT ARRANGEMENT

Detailed layout and identification of all panels and controls within the F-16 cockpit.

1.2.1. LEFT CONSOLE

Description of the panels and controls located on the pilot's left console.

1.2.2. LEFT AUXILIARY CONSOLE

Description of the panels and controls on the left auxiliary console.

1.2.3. CENTRE CONSOLE

Description of the panels and instruments located on the center console.

1.2.4. RIGHT AUXILIARY CONSOLE

Description of the panels and instruments located on the right auxiliary console.

1.2.5. RIGHT CONSOLE

Description of the panels and controls located on the pilot's right console.

1.2.6. MISCELLANEOUS

Covers a few controls accessible to the pilot but not from cockpit controls.

1.3 UP FRONT CONTROLS

Detailed explanation of the Up Front Controls (UFC), including ICP and DED.

1.4 MULTI FUNCTION DISPLAYS

Explanation of the Multi Function Displays (MFDs) and their pages.

1.5 THE HEAD UP DISPLAY (HUD)

Explanation of the Heads Up Display (HUD) features and symbology.

1.6 THE ENGINE

Description of the F-16's engine system, modes, and instruments.

1.7 FUEL SYSTEM

Detailed explanation of the F-16 fuel system, tanks, and indications.

1.8 ENVIRONMENTAL CONTROL SYSTEM (ECS)

Description of the Environmental Control System (ECS) and its functions.

1.9 ELECTRICAL SYSTEM

Overview of the F-16's complex electrical system and its components.

1.10 HYDRAULIC SYSTEM

Description of the hydraulic systems supplying power to flight controls.

1.11 EMERGENCY POWER UNIT (EPU)

Explanation of the Emergency Power Unit (EPU) functions and operation.

1.12 FLIGHT CONTROL SYSTEM (FLCS)

Detailed explanation of the Flight Control System (FLCS) and its modes.

1.13 LANDING GEAR & BRAKES

Description of the landing gear operation and braking system.

1.14 AUTOPILOT OPERATION

Explanation of the F-16's autopilot system modes and operation.

1.15 INSTRUMENT LANDING SYSTEM

Description of the Instrument Landing System (ILS) and its cockpit controls.

1.16 IDENTIFICATION FRIEND or FOE (IFF)

Explanation of the Identification Friend or Foe (IFF) system and modes.

SECTION II NORMAL PROCEDURES

2.1. RAMP START in 3 SWEEPS

A step-by-step guide to starting the F-16 aircraft from ramp.

2.2. REFUELLING

Procedures for hotpit and air-to-air refuelling operations.

2.3. LANDING

Procedures for visual and instrument landing approaches.

SECTION III ABNORMAL & EMERGENCY PROCEDURES

3.1. WARNING AND CAUTION LIGHT AND PILOT FAULT SYSTEM

Understanding aircraft warning lights, caution lights, and fault displays.

3.2. WARNING LIGHT ANALYSIS

Analysis of specific warning lights and their associated causes.

3.3. CAUTION LIGHT ANALYSIS

Analysis of specific caution lights and their associated causes.

3.4. FAULT ANALYSIS

Detailed analysis of aircraft faults, including MFL and PFL.

3.5. GROUND EMERGENCIES

Procedures for handling emergencies that occur while on the ground.

3.6. TAKEOFF EMERGENCIES

Procedures for handling emergencies during the takeoff phase.

3.7. IN FLIGHT EMERGENCIES

Procedures for handling emergencies that occur during flight.

3.8. LANDING EMERGENCIES

Procedures for handling emergencies during the landing phase.

SECTION IV FLIGHT CHARACTERISTICS

4.1 Limit Cycle Oscillation

Description of complex buffeting and stores flutter phenomena.

4.2 Descent Warning Advisory

System providing audio warnings for unintended descents.

4.3 Category Loading

How aircraft configuration affects G-limits and departure susceptibility.

4.4. Departure from controlled flight

Understanding and recovering from aircraft departures.

4.5 Operating Limits & Restrictions

Engine limits and aircraft operating restrictions.

5. BIBLIOGRAPHY

6. ACKNOWLEDGMENT

BMS F-16C/D 4.34 Specifications

General IconGeneral
TypeMultirole Fighter
Primary usersUnited States Air Force, Numerous other countries
ManufacturerLockheed Martin
Max Takeoff Weight42, 300 lb (19, 200 kg)
Engine1 × F110-GE-129 afterburning turbofan
Max Speed1, 500 mph (2, 414 km/h, Mach 2+)
Crew1 (C model), 2 (D model)
RoleMultirole fighter
Service Ceiling50, 000 ft (15, 240 m)
Armament1 × M61 Vulcan 20mm cannon, AIM-9 Sidewinder, AIM-120 AMRAAM, various bombs and missiles