F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 35

T.O. GR1F16CJ1

238Change 1

GR1F-16CJ-1-1101A37

Danger Areas

0

20

40

60

80

100

120

140

160

180

200

0

10

20

30

40

50

60

70

80

90

100

8

4

0

4

8

12

20

10

0

10

20

30

TEMPERATURE

VELOCITY

WITH ENGINE OPERATING, EAR

PROTECTION SHOULD BE WORN

DUE TO HIGH NOISE LEVELS

VELOCITY

TEMPERATURE

25 FT

PLANE OF

ROTATION JFS
PLANE OF ROTATION

ENGINE TURBINE

ENGINE INLET

DANGER AREA

MIL THRUST

MAX AB THRUST

25 FT

ENGINE

0

10

20

30

40

50

60

70

80

90

100

8

4

0

4

8

12

TEMPERATURE

VELOCITY

IDLE THRUST

1540 KTS

948 KTS

652 KTS

356 KTS

296 KTS

237 KTS TO 215 FT

178 KTS TO 220 FT

1955 KTS

59 KTS TO 850 FT

119 KTS TO 448 FT

178 KTS TO 118 FT

1300 KTS

711 KTS

474 KTS

59 KTS TO 373 FT

296 KTS

237 KTS

119 KTS TO 155 FT

30 KTS TO 108 FT

148 KTS

119 KTS

89 KTS

59 KTS

ENGINE F100-PW-229

15 FT

ENGINE INLET

DANGER AREA

300 FT

300 FT

ENGINE INLET

DANGER AREA

TIRES

WITH HOT BRAKES, AVOID INFLATED

MLG TIRE SIDE AREA WITHIN 300 FEET

FOR 45 MINUTES AFTER AIRCRAFT HAS

STOPPED. IF REQUIRED, APPROACH

FROM THE FRONT OR REAR FOR

FIREFIGHTING PURPOSES ONLY.

DISTANCE FROM EXHAUST NOZZLE

FEET

3200 F

2200 F

1200 F

800 F

600 F

500 F

100 F TO 1160 FT

200 F TO 470 FT

300 F TO 270 FT

400 F

1000 F

600 F

500 F

400 F

100 F TO 378 FT

200 F TO 110 FT

300 F

DISTANCE FROM EXHAUST NOZZLE

FEET

DISTANCE FROM EXHAUST NOZZLE

FEET

400 F

300 F

250 F

100 F TO 132 FT

200 F

150 F

JET W

AKE RADIUS

FEET

JET W

AKE RADIUS

FEET

JET W

AKE RADIUS

FEET

Figure

 29.(Sheet 1)

T.O. GR1F16CJ1

239

GR1F-16CJ-1-1102X37

Danger Areas

OPERATING

TRANSMITTERS

MINIMUM SAFE DISTANCE

FROM ANTENNAS IN FEET

VOLATILE FLUIDS

PERSONNEL

EED

UPPER AND LOWER UHF/IFF
UPPER AND LOWER TACAN

VHF

FIRE CONTROL RADAR

UPPER UHF/IFF

ANTENNA

UPPER TACAN

ANTENNA

VHF ANTENNA

CENC AIR-MOTOR

EXHAUST 1200 F

LOWER UHF/IFF ANTENNA

JFS EXHAUST 1175 F

EPU EXHAUST 1600 F

ECS EXHAUST 325 F

LOWER TACAN ANTENNA

RADAR

60

60

RADIATION AND TEMPERATURE

RADAR

60

60

ECM POD

Distance from radar disc to forward

tip of radome = 5 feet.

ECM radiation is in a fan

pattern fore and aft.

AN/ALQ-119
AN/ALQ-131
AN/ALQ-176
AN/ALQ-184
AN/ALQ-188

QRC-80-01

NOTES:

21

1
1
1

120

6

15

6

31

6
6

120

6

15

6
6
6
6

ENGINE F100-PW-229

RADAR ALTIMETER

1

FORWARD

RADAR

ALTIMETER

ANTENNA

INTERNAL ECM

30

1.5

4

ECM ANTENNA

ECM ANTENNA

  (EACH SIDE)

Figure

 29.(Sheet 2)

T.O. GR1F16CJ1

240

50

100

150

200

250

FEET

0

10

20

30

40

50

60

70

80

95 dBA

IDLE THRUST

MAX AB THRUST

MIL THRUST

NOISE EXPOSURE LIMITS

1F-16X-1-4030X

80

85

90

95

100

105

110

115

120

125

130

0

1

2

3

4

5

6

7

8

SPL   dBA

DURATION   HOURS EXPOSURE LIMIT PER DAY

NOTES:

Attenuation factors and exposure limits are for typical

earmuffs and earplugs.

SPL   Sound pressure level.

dBA   Adjusted (human ear response) decibels.

LIMIT 15

MINUTES

PER DAY

WITH EAR

PROTECTION

LIMIT 5

MINUTES

PER DAY

WITH EAR

PROTECTION

NOTE:

Noise levels are

symmetrical and

may be altered

by surrounding

obstacles.

Danger Areas

ENGINE F100-PW-229

90

HAZARDOUS NOISE LEVEL AREAS

1000

800

600

400

200

200

400

600

800

1000

0

30

60

90

120

150

180

FEET

101 dBA

106 dBA

112 dBA

117 dBA

117 dBA

112 dBA

107 dBA

102 dBA

1000

800
700
600
500
400
300
200

200
300
400
500
600
700
800

1000

0

30

60

90

120

150

180

FEET

97 dBA

102

dBA

107 dBA

112 dBA

117

dBA

122

dBA

102 dBA

Figure 

29.(Sheet 3)

T.O. GR1F16CJ1

241

GR1F-16CJ-1-0104X37

With large asymmetries, reduce taxi speed,

avoid sharp turns and, when possible, turn

toward heavy wing to prevent possible tipping.

2 FEET

*6 INCHES

4 FEET 6 INCHES

5 FEET

5 FEET

3 FEET

2 FEET

3 FEET 6 INCHES

16 FEET 10 INCHES

R MISSILE

L MISSILE

R TAIL

PROBE

NLG

R MLG

L MLG

NOTES:

Turn radius can be

reduced to 38 feet by

using inside brake.
Maximum NWS deflection.

All distances are

approximate.

Avoid arresting cable

support donuts when

taxiing with centerline

stores installed.

*

Turning Radius and Ground Clearance

39 35

25

18

6

PIVOT POINT

FEET

Figure 210.

T.O. GR1F16CJ1

242

1F-16X-1-0015X

G-Suit Hose Routing (Typical)

TORSO

HARNESS

G-SUIT HOSE

SURVIVAL KIT

STRAP

LAPBELT

CANOPY SILL

REFERENCE

LINE

LEFT CONSOLE

REFERENCE LINE

(SEAT AT MIDHEIGHT)

Figure 211.

T.O. GR1F16CJ1

31

SECTION III

EMERGENCY PROCEDURES

TABLE OF CONTENTS

Page

INTRODUCTION

33

. . . . . . . . . . . . . . . . . . . . . . . . . 

WARNING AND CAUTION LIGHT

AND PILOT FAULT

LIST ANALYSIS

34

. . . . . . . . . . . . . . . . . . . . . . . . 

FORMAT

34

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

GROUND EMERGENCIES

326

. . . . . . . . . . . . . . . . 

Fire/Overheat/Fuel Leak (Ground)

326

. . . . . . . . 

Hot Start (Ground)

326

. . . . . . . . . . . . . . . . . . . . . . 

Hung Start/No Start 

PW 229

326

. . . . . . . . . . . . . 

Hung Start/No Start 

129

GE

326

. . . . . . . . . . . . . 

Engine Autoacceleration (Ground)

326

. . . . . . . . 

Antiskid Malfunction (Ground)

326

. . . . . . . . . . . 

Brake Failure

327

. . . . . . . . . . . . . . . . . . . . . . . . . . . 

Hot Brakes

328

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Main Generator Failure (Ground)

329

. . . . . . . . 

Main and Standby Generator Failure

(Ground)

329

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Emergency Entrance and Crew Rescue

329

. . . . 

Emergency Ground Jettison

329

. . . . . . . . . . . . . . 

Ground Egress

329

. . . . . . . . . . . . . . . . . . . . . . . . . . 

Hot Refueling Emergency

332

. . . . . . . . . . . . . . . . 

Activated EPU/Hydrazine Leak

332

. . . . . . . . . . 

NWS Failure/Hardover

332

. . . . . . . . . . . . . . . . . . 

TAKEOFF EMERGENCIES

333

. . . . . . . . . . . . . . . . 

Delayed Rotation

333

. . . . . . . . . . . . . . . . . . . . . . . . 

Abort

333

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Engine Malfunction on Takeoff

334

. . . . . . . . . . . 

Engine Failure on Takeoff

334

. . . . . . . . . . . . . . . 

AB Malfunction on Takeoff

335

. . . . . . . . . . . . . . . 

Low Thrust on Takeoff or at Low

Altitude (NonAB) 

PW 229

335

. . . . . . . . . . . . . 

Low Thrust on Takeoff or at Low

Altitude (NonAB) 

129

GE

336

. . . . . . . . . . . . . 

Engine Fire on Takeoff

336

. . . . . . . . . . . . . . . . . . 

LG Fails To Retract

336

. . . . . . . . . . . . . . . . . . . . . 

LG Handle Will Not Raise

336

. . . . . . . . . . . . . . . 

Blown Tire on Takeoff

337

. . . . . . . . . . . . . . . . . . . 

INFLIGHT EMERGENCIES

338

. . . . . . . . . . . . . . 

CANOPY Warning Light On

338

. . . . . . . . . . . . . 

Canopy Loss/Penetration in Flight

338

. . . . . . . . 

Drag Chute Deployed in Flight

338

. . . . . . . . . . . 

Cockpit Pressure/Temperature

Malfunction

339

. . . . . . . . . . . . . . . . . . . . . . . . . . 

EQUIP HOT Caution Light

340

. . . . . . . . . . . . . . 

Ejection

340

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Ejection (Immediate)

341

. . . . . . . . . . . . . . . . . . 

Ejection (Time Permitting)

341

. . . . . . . . . . . . 

Failure of Canopy To Separate

341

. . . . . . . . . 

Ejection Seat Failure

343

. . . . . . . . . . . . . . . . . . 

Ditching

343

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Electrical System Failures

343

. . . . . . . . . . . . . . . 

FLCS PMG Failure

343

. . . . . . . . . . . . . . . . . . . 

Single Generator Failures

(in Flight)

343

. . . . . . . . . . . . . . . . . . . . . . . . . 

Main and Standby Generator 

Failure (in Flight)

344

. . . . . . . . . . . . . . . . . . 

Main, Standby, and EPU Generator

Failure

345

. . . . . . . . . . . . . . . . . . . . . . . . . . . . 

EPU Malfunctions

347

. . . . . . . . . . . . . . . . . . . . 

Uncommanded EPU Operation

347

. . . . . . 

Abnormal EPU Operation

348

. . . . . . . . . . . 

FLCS RLY Light

349

. . . . . . . . . . . . . . . . . . . . . . 

Partial Electrical Power Loss

349

. . . . . . . . . . 

Aircraft Battery Failure

350

. . . . . . . . . . . . . . . 

Emergency Power Distribution

351

. . . . . . . . . 

Engine Malfunctions 

PW 229

361

. . . . . . . . . . . . . 

Engine Fire 

PW 229

361

. . . . . . . . . . . . . . . . . . . 

OVERHEAT Caution Light 

PW 229

362

. . . . 

Engine Vibrations 

PW 229

363

. . . . . . . . . . . . . 

Oil System Malfunction 

PW 229

363

. . . . . . . . 

ENGINE FAULT Caution 

Light 

PW 229

364

. . . . . . . . . . . . . . . . . . . . . . 

SEC Caution Light 

PW 229

364

. . . . . . . . . . . . 

FTIT Indicator Failure 

PW 229

365

. . . . . . . . 

Zero RPM/Erroneous RPM 

Indication 

PW 229

365

. . . . . . . . . . . . . . . . . . 

Abnormal Engine Response 

PW 229

365

. . . . 

Nozzle Failure 

PW 229

367

. . . . . . . . . . . . . . . . 

AB Blowout/Failure To 

Light 

PW 229

368

. . . . . . . . . . . . . . . . . . . . . . 

T.O. GR1F16CJ1

32

Engine Stalls 

PW 229

368

. . . . . . . . . . . . . . . . . . . . 

ABAssociated Engine 

Stalls 

PW 229

369

. . . . . . . . . . . . . . . . . . . . . . 

NonAB Engine Stalls 

PW 229

369

. . . . . . . . . 

Engine Stall Recovery 

PW 229

369

. . . . . . . . . 

Inlet Buzz 

PW 229

370

. . . . . . . . . . . . . . . . . . . . . . 

Engine Failure or Flameout 

PW 229

370

. . . . . . 

Tower Shaft Failure 

PW 229

370

. . . . . . . . . . . 

Low Altitude Engine Failure or

Flameout 

PW 229

371

. . . . . . . . . . . . . . . . . . 

Airstarts 

PW 229

371

. . . . . . . . . . . . . . . . . . . . . . . . 

High Altitude Airstart

Considerations 

PW 229

378

. . . . . . . . . . . . . 

Low Altitude Airstart 

Considerations 

PW 229

379

. . . . . . . . . . . . . 

Airstart Procedures 

PW 229

379

. . . . . . . . . . . 

Engine Malfunctions 

129

GE

381

. . . . . . . . . . . . . 

Engine Fire 

129

GE

381

. . . . . . . . . . . . . . . . . . . 

OVERHEAT Caution Light 

129

GE

382

. . . . 

Oil System Malfunction 

129

GE

383

. . . . . . . . 

ENGINE FAULT Caution 

Light 

129

GE

384

. . . . . . . . . . . . . . . . . . . . . . 

SEC Caution Light 

129

GE

384

. . . . . . . . . . . . 

FTIT Indicator Failure 

129

GE

385

. . . . . . . . 

Zero RPM/Erroneous RPM 

Indication 

129

GE

385

. . . . . . . . . . . . . . . . . . 

Abnormal Engine Response 

129

GE

386

. . . . 

AB Blowout/Failure To 

Light 

129

GE

387

. . . . . . . . . . . . . . . . . . . . . . 

Engine Stalls 

129

GE

388

. . . . . . . . . . . . . . . . . . . . 

ABAssociated Engine Stalls 

129

GE

388

. . . 

NonAB Engine Stalls 

129

GE

388

. . . . . . . . . 

Engine Stall Recovery 

129

GE

389

. . . . . . . . . 

Inlet Buzz 

129

GE

389

. . . . . . . . . . . . . . . . . . . . . . 

Bird Strike 

129

GE

389

. . . . . . . . . . . . . . . . . . . . . . 

Engine Overspeed 

129

GE

389

. . . . . . . . . . . . . . . 

Engine Failure or Flameout 

129

GE

389

. . . . . . 

Tower Shaft Failure 

129

GE

390

. . . . . . . . . . . 

Low Altitude Engine Failure or

Flameout 

129

GE

390

. . . . . . . . . . . . . . . . . . 

Airstarts 

129

GE

390

. . . . . . . . . . . . . . . . . . . . . . . . 

High Altitude Airstart

Considerations 

129

GE

395

. . . . . . . . . . . . . 

Low Altitude Airstart

Considerations 

129

GE

396

. . . . . . . . . . . . . 

Airstart Procedures 

129

GE

396

. . . . . . . . . . . 

Flameout Landing

398

. . . . . . . . . . . . . . . . . . . . . . 

Overhead Approach

399

. . . . . . . . . . . . . . . . . . . 

StraightIn Approach

3100

. . . . . . . . . . . . . . . . 

IMC Penetration

3100

. . . . . . . . . . . . . . . . . . . . . 

Landing Phase

3105

. . . . . . . . . . . . . . . . . . . . . . 

After Touchdown

3105

. . . . . . . . . . . . . . . . . . . . 

Flameout Landing Procedures

3105

. . . . . . . . 

Jettison

3107

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Selective Jettison

3107

. . . . . . . . . . . . . . . . . . . . 

Emergency Jettison

3108

. . . . . . . . . . . . . . . . . . 

FLCS Failures

3108

. . . . . . . . . . . . . . . . . . . . . . . . . 

Air Data Malfunctions

3108

. . . . . . . . . . . . . . . 

AOA Malfunction

3109

. . . . . . . . . . . . . . . . . . . . 

CADC Malfunction

3110

. . . . . . . . . . . . . . . . . . 

Servo Malfunction

3110

. . . . . . . . . . . . . . . . . . . 

FLCS Electronic Malfunctions

3110

. . . . . . . . 

FLCS Single Electronic Failure

3111

. . . . . 

FLCS Dual Electronic Failure

3111

. . . . . . 

FLCS Temperature Malfunction

3112

. . . . . . 

Autopilot Malfunctions

3112

. . . . . . . . . . . . . . . 

DBU ON Warning Light

3113

. . . . . . . . . . . . . . 

TF FAIL Warning Light

3113

. . . . . . . . . . . . . . 

LEF Malfunction (Symmetric)

3114

. . . . . . . . 

LEF Malfunction (Asymmetric)

3115

. . . . . . . 

Trim Malfunction

3116

. . . . . . . . . . . . . . . . . . . . 

Stick Interference

3116

. . . . . . . . . . . . . . . . . . . . 

Fuel Malfunctions

3117

. . . . . . . . . . . . . . . . . . . . . . 

Fuel Management System PFL

3117

. . . . . . . 

Fuel Leak

3117

. . . . . . . . . . . . . . . . . . . . . . . . . . . 

Fuel Low

3118

. . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Hot Fuel/Oil or Gravity Feed

3118

. . . . . . . . . . 

Fuel Imbalance

3119

. . . . . . . . . . . . . . . . . . . . . . 

Trapped External Fuel

3121

. . . . . . . . . . . . . . . 

Trapped CFT Fuel 

PX III

3122

. . . . . . . . . . . . . 

Hydraulic Malfunctions

3123

. . . . . . . . . . . . . . . . . 

Single Hydraulic Failure

3123

. . . . . . . . . . . . . 

System A Failure

3123

. . . . . . . . . . . . . . . . . . 

System B Failure

3123

. . . . . . . . . . . . . . . . . . 

Dual Hydraulic Failure

3124

. . . . . . . . . . . . . . 

System B and Generator Failure

(PTO Shaft)

3125

. . . . . . . . . . . . . . . . . . . . . . . 

EGI Failure 

PX III

3126

. . . . . . . . . . . . . . . . . . . . . 

INS Failures 

PX II

3127

. . . . . . . . . . . . . . . . . . . . . 

Total INS Failure 

PX II

3128

. . . . . . . . . . . . . . . 

OutofControl Recovery

3128

. . . . . . . . . . . . . . . . 

Oxygen Malfunction 

PX II

3130

. . . . . . . . . . . . . . 

OBOGS Malfunction 

PX III

3131

. . . . . . . . . . . . . 

PBG Malfunction

3131

. . . . . . . . . . . . . . . . . . . . . . 

Smoke or Fumes

3131

. . . . . . . . . . . . . . . . . . . . . . . 

T.O. GR1F16CJ1

33

LANDING EMERGENCIES

3132

. . . . . . . . . . . . . . . 

Straightin Landing

3132

. . . . . . . . . . . . . . . . . . . . 

Simulated Flameout (SFO) Landing

3132

. . . . . 

Controllability Check

3133

. . . . . . . . . . . . . . . . . . . 

Cable Arrestment

3134

. . . . . . . . . . . . . . . . . . . . . . 

Net Arrestment

3135

. . . . . . . . . . . . . . . . . . . . . . . . 

Landing With A Blown Tire

3135

. . . . . . . . . . . . . 

Landing With A Blown Main Gear

Tire

3136

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

Landing With A Blown Nose Gear

Tire

3136

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 

LG Extension Malfunctions

3137

. . . . . . . . . . . . . 

LG Handle Will Not Lower

3137

. . . . . . . . . . . 

LG Fails To Extend

3138

. . . . . . . . . . . . . . . . . . 

Alternate LG Extension

3139

. . . . . . . . . . . . . . 

Landing With LG Unsafe/Up

3140

. . . . . . . . . 

Antiskid Malfunction (Landing)

3140

. . . . . . . . . 

Asymmetric Stores (Landing)

3141

. . . . . . . . . . . 

NLG WOW Switch Failure

3145

. . . . . . . . . . . . . . 

Drag Chute Failure

3145

. . . . . . . . . . . . . . . . . . . . 

INTRODUCTION

This section covers the operation of the aircraft

during emergency/abnormal conditions. It includes a

discussion of problem indications and corrective

actions as well as procedural steps when applicable.

Adherence to these guidelines insures maximum

safety for the pilot and/or aircraft. The situations

covered are representative of the most probable

malfunctions. However, multiple emergencies, ad

verse weather, or other factors may require

modification of the recommended procedures. Only

those steps required to correct or manage the problem

should be accomplished. When dealing with emergen

cy/abnormal conditions, it is essential to determine

the most correct course of action by using sound

judgment and a full understanding of the applicable

system(s). When practical, other concerned agencies

(i.e., flight lead, tower, etc.) should be advised of the

problem and intended course of action.

When a voice WARNING or CAUTION message is

heard, check cockpit indications; then refer to the

appropriate emergency procedure for corrective

action.

When structural damage or any other failure that

may adversely affect aircraft handling characteris

tics is known or suspected, a controllability check

should be performed.

Certain steps (e.g., MASTER CAUTION reset, ELEC

CAUTION reset) are intentionally omitted from the

numbered procedures. Pilots are expected to perform

these actions without prompting, when warranted.

Three basic rules, which apply to all emergencies, are

established:

1.

MAINTAIN AIRCRAFT CONTROL.

2.

ANALYZE THE SITUATION AND TAKE

PROPER ACTION.

3.

LAND AS THE SITUATION DICTATES.

The following information provides general landing

guidance:

Land As Soon As Possible

An emergency will be declared. A landing should be

accomplished at the nearest suitable airfield

considering the severity of the emergency, weather

conditions, airfield facilities, lighting, aircraft GW,

and command guidance.

Land As Soon As Practical

Emergency conditions are less urgent and, although

the flight is to be terminated, the degree of the

emergency is such that an immediate landing at the

nearest suitable airfield may not be necessary.

F

The canopy should remain closed

during all emergencies that could

result in a crash or fire such as crash

landings, aborted takeoffs, and arrest

ments. The protection the canopy

affords far outweighs the isolated risk

of entrapment due to a canopy

malfunction or overturn.

F

Ejection is preferable to sliding into an

arrestment cable with the NLG col

lapsed. The cable may slide up over the

nose with unpredictable and poten

tially dangerous consequences to any

one in the cockpit(s).