Content .. 28 29 30 31 ..

F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 30

T.O. GR1F16CJ1

1224

1. VIDEO SEL Switch

2. HUD Monitor

3. Handgrip

4. BRT Control

5. Function Knob

GR1F-16CJ-1-0095X37

Aft Seat HUD Monitor

6. CONT Control

Figure 195.

T.O. GR1F16CJ1

1225

COCKPIT (EJECTION SEAT(S))
EMERGENCY GASEOUS

DOOR 2318

EXTERNAL POWER CABLE

DOOR 3306

IFF MODE 4

PANEL 3408 (TOP)

EPU (MONOPROPELLANT)

DOOR 3206

AMMUNITION LOADING

DOOR 3216

HYDRAULIC SYSTEM A

GROUND TEST AND

SERVICE CONNECTIONS

DOOR 3202

HYDRAULIC SYSTEM A

ACCUMULATOR

DOOR 3204

DEFUELING

DOOR 2105, 2107
GROUND COOLING

RECEPTACLE

NLG WHEEL WELL

LG/HOOK EMERGENCY

PNEUMATIC BOTTLE

(NITROGEN)

PANEL 3402 (TOP)

LEF POWER DRIVE UNIT

DOOR 3115

HYDRAULIC SYSTEM B

GROUND TEST AND

SERVICE CONNECTIONS

DOOR 3101

HYDRAULIC SYSTEM B

ACCUMULATOR

LMLG WHEEL WELL

HALON RESERVOIR

DOOR 3103

GROUND REFUELING

RECEPTACLE

DOOR 3318

ADG

CSD

DOOR 4304

BRAKE/JFS

ACCUMULATORS (2)

DOOR 4113

FLCS ACCUMULATORS (2)

GR1F-16CJ-1-0096A37

Servicing Diagram (Typical)

RECEPTACLE

DOOR 3308

LIQUID OXYGEN

DOOR 2317

ENGINE AND EMS GO-

NO-GO INDICATORS

DOOR 3218/3320

ENGINE OIL SIGHT GAGE

DOOR 3316

ENGINE OIL SERVICE

JOAP SAMPLE

BOTTOM VIEW

OXYGEN BOTTLE(S)

RECEPTACLE

PANEL 3412 (TOP)

EPU OIL SERVICE

DOOR 3208

EPU (NITROGEN)

HYDRAZINE LEAK

DETECTOR

DOOR 4214

DRAG CHUTE ACCUMULATOR

PX II

PW229 GE129

Figure 196.(Sheet 1)

T.O. GR1F16CJ1

1226

Servicing Diagram (Typical)

SERVICEABLE ITEM

SPECIFICATIONS

SERVICEABLE ITEM

USAF

NATO

FUEL

ENGINE/JFS

MILT5624, JP4
MILT5624, JP5
MILT83133, JP8
JET A, B (COMMERCIAL)
JET A1 (COMMERCIAL)

F40
F43 OR F44
F34
NONE
F35

OIL

ENGINE *

229

MILL7808J OR LATER

0 148

OIL

ENGINE *

129

MILL7808

0148

ADG/CSD/EPU

MILL7808

0148

HYDRAULIC FLUID

HYDRAULIC SYSTEMS A AND B

MILH5606

MILH83282

H515

H537

OXYGEN

GASEOUS

MILO27210, TYPE I

NONE

OXYGEN

LIQUID

MILO27210, TYPE II

NONE

EXTERNAL ELECTRICAL

POWER

115 (

15) VAC, 400 (

30) HZ

A/M32A60A

NONE

NITROGEN

GASEOUS

BBN441A, TYPE I, GRADE B

NONE

FUEL TANK INERTING

AGENT (OPTIONAL)

LIQUID

HALON 1301

NONE

MONOPROPELLANT (EPU)

LIQUID

HYDRAZINE (70% N

, 30%

NONE

*IF NECESSARY, ENGINE LUBRICATING OILS MILL7808 (NATO CODE 0148) AND MILL23699 (NATO CODE 0156) MAY BE MIXED. AT

THE FIRST OPPORTUNITY THEREAFTER, THE OIL SHALL BE DRAINED AND FLUSHED, AND THE ENGINE SERVICED WITH THE PROPER

LUBRICATING OIL AS SPECIFIED IN THE APPLICABLE ENGINE TECHNICAL ORDERS.

Figure 196.(Sheet 2)

T.O. GR1F16CJ1

SECTION II

NORMAL PROCEDURES

TABLE OF CONTENTS

Page

Introduction

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

Flight Planning

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

Takeoff and Landing Data Card

. . . . . . . . .

Cockpit Designation Code

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

Weight and Balance

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

Preflight Check

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

Exterior Inspection

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

Cockpit Access

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

Before Entering Cockpit

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

Cockpit Interior Check

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

Left Console

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

Left Auxiliary Console

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

Instrument Panel

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

Right Auxiliary Console

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

Right Console

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

After Cockpit Check Is

Complete Verify

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

Before Starting Engine

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

Starting Engine

PW 229

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

Starting Engine

129

210

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

After Engine Start

211

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

Before Taxi

217

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

Taxi

218

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

Before Takeoff

218

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

Takeoff

220

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

Normal Takeoff

220

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

Takeoff With Asymmetric Stores

222

. . . . . . . . .

Climb

222

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

Climb/InFlight/Operational Checks

222

. . . . . . . .

Air Refueling Procedures

223

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

Descent/Before Landing

223

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

Landing

223

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

Normal Landing

223

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

Short Field Landing (Dry Runway)

226

. . . . . .

Crosswind Landing

226

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

TouchandGo Landing

227

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

After Landing

227

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

Prior to Engine Shutdown

228

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

Engine Shutdown

229

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

Scramble

230

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

Preflight

230

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

Aircraft On Quick Response Status

230

. . . . . .

Hot Refueling

231

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

Hot Refueling Precautions

231

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

Prior to Hot Pit Entry

231

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

Prior to Hot Refueling

231

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

During Hot Refueling

232

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

Hot Refueling Complete

232

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

Quick Turnaround

232

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

Prior to Engine Shutdown

232

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

Special Procedures

232

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

EPU Hydrazine Support at NonF16

Bases

232

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

Supplemental Procedures

232

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

ILS Procedures

232

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

Exterior Inspection

232

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

Danger Areas

232

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

Turning Radius and Ground Clearance

232

. . . .

GSuit Hose Routing

232

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

Strange Field Procedures

232

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

INTRODUCTION

This section provides the actions required for normal

operation of the aircraft. Amplification is included

only when special considerations or techniques

should be observed. A complete knowledge of Section

III, EMERGENCY PROCEDURES, and Section V,

OPERATING LIMITATIONS, is required prior to

flight.

FLIGHT PLANNING

Refer to T.O. GR1F16CJ11.

TAKEOFF AND LANDING DATA CARD

A takeoff and landing data card is provided in the

Flight Crew Checklist for recording computed data.

COCKPIT DESIGNATION CODE

An asterisk (*) preceding steps is used to highlight

procedures for

aircraft which apply to both

cockpits.

WEIGHT AND BALANCE

For maximum GW limitations, refer to Section V,

OPERATING LIMITATIONS. For weight and

balance information, refer to the individual aircraft

Form F (DD Form 3654) and the Weight and Balance

Handbook.

T.O. GR1F16CJ1

PREFLIGHT CHECK

Check AFTO Form 781 for aircraft release and stores

status.

EXTERIOR INSPECTION

Refer to figure 24 for normal preflight inspection.

COCKPIT ACCESS

Refer to figure 21.

1. Canopy-Open by positioning external cano

py switch to the up position.

If winds exceed 30 knots, open the

canopy only as far as needed to enter/exit

the cockpit. Decreasing the canopy angle

reduces the possibility that the canopy

can be blown past full open.

2. Ladder-Position on cockpit sill.

A failure of the canopy actuator

could allow the canopy to fall during

transit. Do not position the ladder

until the canopy motion has stopped.

NOTE

Cockpit access is gained by the use

of two entrance ladders or moving one

ladder as required.

BEFORE ENTERING COCKPIT

*1. Ejection seat-Check.

Ejection safety lever-Safe (up).

Safety pins (2)-Removed (ejection safety

lever and EMERGENCY MANUAL CHUTE

handle).

1F-16X-1-1045A

Cockpit Access

(Typical)

EXTERNAL CANOPY SWITCH

(LOWER SURFACE OF LEFT

STRAKE)

Figure 21.

Survival KIT DEPLOYMENT switch-As

desired.

A Parachute Landing Fall (PLF) with

the survival kit not deployed may result

in injury.

RADIO BEACON-As desired.

Emergency oxygen bottle-1800 psi mini

mum.

Quickdisconnect (left side)-Connected.

Recovery parachute-Free from damage and

grease.

Inertia reel straps retaining pin (yel

low)-Visible in circular inspection hole.

Parachute risers and SEAWARS -Free from

damage and grease.

T.O. GR1F16CJ1

Rapidly pulling on the shoulder

harness to check the locking mecha

nism may cause damage to the locking

mechanism.

Lanyards from canopy to seat-Check.

Emergency oxygen hose quickdiscon

nect-Connected.

Environmental sensor pitot tubes-Clear of

obstructions and if flipup pitot tubes are

installed, safety pins (2) removed.

Quickdisconnect (right side)-Connected.

Electronic recovery sequencer battery indi

cator-White indication.

CANOPY JETTISON Thandle-Secure,

safety pin removed.

Lapbelt retaining pins (yellow)-Protrud

ing, both sides.

Lapbelts-Secure. (Pull up and forward,

both sides.)

Survival kit straps-Secure. (Pull up and

aft, both sides.)

2. MAIN PWR switch-OFF.

For solo flight:

3. Ejection seat-Safe, straps secure, pins

removed.

4. CANOPY JETTISON Thandle-Secure,

safety pin removed.

5. SPD BRK switch-Center.

6. FUEL MASTER switch-MASTER (guard

down).

7. ENG CONT switch-NORM (guard down).

8. Audio panels-Set:

COMM 1 mode knob-SQL.

COMM 2 mode knob-SQL.

All other knobs-CCW.

9. ALT GEAR handle-In.

10. ALT FLAPS switch-NORM.

11. GND JETT ENABLE switch-OFF.

12. DRAG CHUTE Switch-NORM.

13. HOOK switch-UP.

14. ARMT CONSENT switch-ARMT CON

SENT (guard down).

15. EJECTION MODE SEL handle-SOLO.

16. Interior LIGHTING control panel-All

knobs off.

17. OXYGEN REGULATOR-OFF and 100%.

18. Utility light-OFF and secured.

COCKPIT INTERIOR CHECK

The checklist steps are not arranged in a mandatory

order.

*1. Loose or foreign objects-Check.

A thorough cockpit interior preflight check

shall be accomplished prior to each flight

with emphasis on loose or foreign objects

that might cause injury to personnel or

damage to the aircraft.

*2. Harness and personal equipment-Fasten.

Attach the parachute risers to the harness.

Attach and adjust survival kit straps.

Secure and adjust the lapbelt. After

fastening lapbelt, hold right side of lapbelt

buckle stationary and shake and push left

side. Also insure that latching mechanism

has reset back to its original position and is

flush with buckle to insure a positive lock.

Connect oxygen hose, gsuit hose, vest hose,

and communication leads. Check operation

of the shoulder harness locking mechanism.

T.O. GR1F16CJ1

A partially locked lapbelt may open

during maneuvering flight or ejection

sequence.

Unobserved gsuit hose or vest hose

disconnects can contribute to gray/

blackout or loss of consciousness.

Failure to adjust survival kit straps to

achieve a snug fit between the pilot

and seat pan lid may result in injury

during ejection.

Failure to adequately secure and

tighten lapbelt may result in inability

to reach and operate the MPO switch

during outofcontrol situations.

Do not adjust seat height with survival

kit straps or lapbelt disconnected as

damage to the ejection seat or stick

may occur.

NOTE

Refer to figure 211. The recommended

routing of the gsuit hose is directly

under the torso harness and aft of the

survival kit strap to reduce the

possibility of a gsuit hose disconnect.

Gsuit hose routing must provide

sufficient slack to allow for maximum

mobility since inflight reconnect is

extremely difficult.

Excess gsuit hose must be properly

routed to prevent MANUAL TRIM

panel interference during flight.

Incorrectly routed or unsecured

gsuit hose may result in throttle

interference or disconnected gsuit hose.

*3. Rudder pedals-Adjust.

Adjust rudder pedals so that legs are flat on

the seat cushion to prevent the right leg

from hitting stick or injury during ejection.

Left Console

1. PROBE HEAT switch-OFF.

STICK CONTROL switch-As briefed

when

occupied; FWD for solo flight.

3. FLCS PWR TEST switch-NORM.

4. DEFOG lever-Midrange.

5. DIGITAL BACKUP switch-OFF.

*6. ALT FLAPS switch-NORM.

7. MANUAL TF FLY UP switch - ENABLE.

8. LE FLAPS switch-AUTO.

9. BIT switch-OFF.

10. TRIM/AP DISC switch-NORM.

11. ROLL, YAW, and PITCH TRIM-Center.

*12. FUEL MASTER switch-MASTER (guard

down and

safetywired).

13. TANK INERTING switch-OFF.

14. ENG FEED knob-NORM.

15. AIR REFUEL switch-CLOSE.

16. IFF MASTER knob-STBY.

17.

PX II

CNI,

PX III

C & I knob-BACKUP.

*18. TACAN-As desired.

19. EXT LIGHTING control panel-As required.

PX III

If ground operation of the

anticollision strobe light is anticipated

to be longer than 2 hours, the

ANTICOLLISION knob should be set

in position 1 to avoid overheating the

power supply and strobe.

20. MASTER light switch-NORM.

21. EPU switch-NORM (guard down).

22. MAIN PWR switch-OFF.

23. AVTR power switch-OFF.

24. AVTR

PX II

DISPLAY,

PX III

VIDEO SELECT

knob-HUD.

25. ECM power-Off.

*26. COMM 1 power knob-CW.

*27. COMM 1 mode knob-SQL.

T.O. GR1F16CJ1

Change 125

*28. COMM 2 power knob-CW.

*29. COMM 2 mode knob-SQL.

*30. TACAN power knob-CW.

31.

AB RESET switch-NORM.

32.

ENG CONT switch-PRI (guard down).

33.

ENG CONT switch-NORM (guard down).

34. JFS switch-OFF.

35. UHF radio backup control panel:

a. Function knob-BOTH.

b. Frequency-As desired.

36. Throttle-Verify freedom of motion, then OFF.

*37. SPD BRK switch-Forward.

*38. DOG FIGHT switch-Center.

Left Auxiliary Console

*1. ALT GEAR handle-In.

2. CMDS switches (9)-OFF.

3. RF switch-NORM.

PX III

SYMBOLOGY power knob-Off.

5. STORES CONFIG switch-As required.

6. LANDING TAXI LIGHTS switch-OFF.

*7. LG handle-DN.

*8. GND JETT ENABLE switch-OFF.

9. BRAKES channel switch-CHAN 1.

10. ANTISKID switch-ANTISKID.

*11. EMER STORES JETTISON button-Cover

intact.

*12. HOOK switch-UP.

Instrument Panel

1. ROLL switch-ATT HOLD.

2. PITCH switch-A/P OFF.

3. MASTER ARM switch-OFF.

ARMT CONSENT switch-ARMT CON

SENT (guard down).

5. LASER ARM switch-OFF.

*6. DRAG CHUTE switch-NORM.

*7. HUD/ASHM-Set.

*8. Altimeter-Set.

9. FUEL QTY SEL knob-NORM.

10. EXT FUEL TRANS switch-NORM.

NOTE

If a wing transfer valve fails and WING

FIRST is selected, fuel flows onto the

ground from the overboard vent line

under the left wing (outboard of the

fuel pylon). Selecting NORM should

stop the fuel spillage.

PX III

If CFT's are installed and an

external tank transfer valve fails to

close when the tank is empty and

WING FIRST or NORM is selected,

fuel is trapped in the CFT and some

trapped fuel may vent overboard.

Selecting CFT FIRST/NO FILL should

prevent trapped/vented CFT fuel.

*11. INSTR MODE knob-As desired.

Right Auxiliary Console

*1. Clock-Set.

EJECTION MODE SEL handle-

b2p

NORM or AFT (as briefed),

LESS

b2p

AFT.

SOLO position should not be selected

with the rear seat occupied.

Ejection initiated with the EJEC

TION MODE SEL handle in NORM

may incapacitate the

pilot at

airspeeds greater than 180 knots. Use

of the NORM position is therefore not

recommended.

Content .. 28 29 30 31 ..

F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 30

F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 30