Content .. 1 2 ..

F16C/D. FLIGHT MANUAL (2002) - page 1

T.O. GR1F16CJ1

15 OCTOBER 2002

CHANGE 115 JUNE 2003

FLIGHT MANUAL

HAF SERIES AIRCRAFT

F16C/D

BLOCKS 50 AND 52+

LOCKHEED MARTIN CORPORATION

F3365790C2002

F4262001D0058

GR1F-16C-1-0001X

Commanders are responsible for bringing this publication to the attention of all Air Force personnel cleared for

operation of subject aircraft.

T.O. GR1F16CJ1

T2Change 1

DISCLOSURE STATEMENT

This information is furnished on the conditions that it will not be released to another nation without the

specific authorization of the Department of the Air Force of the United States; it will be used for military

purposes only; the recipient will report promptly to the United States any known or suspected compromise;

and the information will be provided substantially the same degree of security afforded it by the Department

of Defense of the United States. Also, regardless of any other markings on the document, it will not be

downgraded or declassified without the written approval of the originating US agency. Any request for this

document should be referred to OOALC/YPXG, 6089 Wardleigh Road, Hill AFB, UT 840565838.

SUPPLEMENTAL NOTICE

This manual is incomplete without T.O. GR1F16CJ11 and T.O. GR1F16CJ12.

SUPERSEDURE NOTICE

See Technical Order Index, T.O. GR0171, for current status of Flight Manuals, Safety Supplements, Opera

tional Supplements, and Flight Crew Checklists.

This manual supersedes T.O. 11C130 and Interim Safety Supplements T.O. GR1F16CJ1SS27 and T.O.

GR1F16CJ1SS29, and Interim Operational Supplement T.O. GR1F16CJ1S31.

LIST OF EFFECTIVE PAGES

NOTE:Changes to the current issue are indicated by a vertical line in the outer margins of the page.

T.O. GR1F16CJ1

INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

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HAF

Dates of issue for original and changed pages are:

Original

15 Oct 02

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15 Jun 03

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42 Blank

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

LIST OF EFFECTIVE PAGES (Cont)

Page

No.

Page

No.

*Change

No.

*Change

No.

Page

No.

*Change

No.

INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.

T.O. GR1F16CJ1

* Zero in this column indicates an original page.

DChange 1

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

610

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Glossary 1

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Glossary 2

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Glossary 3

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Glossary 4

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Glossary 5

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

Glossary 6 Blank

. . . . . . . . .

T.O. GR1F16CJ1

Change 1a/(b blank)

FLIGHT MANUALS, SAFETY SUPPLEMENT, AND

OPERATIONAL SUPPLEMENT STATUS

This supplement status page is based on information available as of 15 June 2003. It is not an official status page.

Flight Manual

Basic Date

Change No. and Date

T.O. GR1F16CJ1

15 Oct 2002

15 Jun 2003

Supplemental Flight Manuals

Basic Date

Change No. and Date

T.O. GR1F16CJ11

9 Jun 1997

15 Nov 2002

T.O. GR1F16CJ12

15 Feb 2000

15 Mar 2003

Flight Crew Checklist

Basic Date

Change No. and Date

T.O. GR1F16CJ1CL1

15 Oct 2002

15 Jun 2003

INCORPORATED SAFETY AND OPERATIONAL SUPPLEMENTS

T.O. Number

Date

Short Title

Flight Manual

Sections Affected

GR1F16CJ1SS27

27 Nov 02

FLCS Failure That Results

In Loss Of Pitch Control

III

GR1F16CJ1SS29

29 Jan 03

Max Range Speeds and FO Pattern

Altitudes

III

GR1F16CJ1S31

30 Apr 03

Fuel Transfer Switch, Avionics

Fault & ECM Lights, and EGI

Align

OUTSTANDING SAFETY AND OPERATIONAL SUPPLEMENTS

T.O. Number

Date

Short Title

Flight Manual

Sections Affected

None

T.O. GR1F16CJ1

Change 1i

TABLE OF CONTENTS

SECTION I

Description and Operation

SECTION II

Normal Procedures

SECTION III

Emergency Procedures

SECTION IV

Crew Duties

SECTION V

Operating Limitations

SECTION V

Operating Limitations (Stores)

T.O. GR1F16CJ12

SECTION VI

Flight Characteristics

SECTION VII

Adverse Weather Operation

SECTION VIII

Air Refueling Procedures

GLOSSARY

Standard and Nonstandard Abbreviations

Glossary 1

APPENDIX A

Performance Data-F100PW229

T.O. GR1F16CJ11

APPENDIX B

Performance Data-F110GE129

T.O. GR1F16CJ11

APPENDIX C

Performance Data-F100PW229/CFT

T.O. GR1F16CJ11

T.O. GR1F16CJ1

iiChange 1

BEFORE

YOU

TAKE OFF,

READ THIS!

1F-16X-1-0002X

SCOPE

This manual contains the necessary information for

safe and efficient operation of the aircraft. These

instructions provide a general knowledge of the

aircraft and its characteristics and specific normal

and emergency operating procedures. Pilot experi

ence is recognized; therefore, basic flight principles

are avoided. Instructions in this manual are prepared

to be understandable to the least experienced pilot

who can be expected to operate the aircraft. This

manual provides the best possible operating instruc

tions under most conditions. Multiple emergencies,

adverse weather, terrain, etc., may require modifica

tion of the procedures. This manual must be used

with one or more of the following manuals to obtain

information necessary for safe and efficient opera

tion:

T.O. GR1F16CJ11

Supplemental Flight

Manual, F16C/D Air

craft

T.O. GR1F16CJ12

Supplemental Flight

Manual, F16C/D Air

craft

T.O. GR1F16CJ52

Loading Data

T.O. GR1F16CJ6CF1

Acceptance and Func

tional Check Flight

Procedures Manual,

F16C/D Aircraft

T.O. GR1F16CJ3411

Avionics and Nonnu

clear Weapons Deliv

ery Flight Manual

T.O. GR1F16CJ3412

Nonnuclear Weapons

Ballistics

T.O. 11C1

Basic Flight Crew Air

Refueling Procedures

PERMISSIBLE OPERATIONS

The flight manual takes a positive approach and

normally states only what can be done. Unusual

operations or configurations are prohibited unless

specifically covered herein. Clearance must be

obtained before any questionable operation which is

not specifically permitted in this manual is

attempted.

T.O. GR1F16CJ1

Change 1iii

HOW TO BE ASSURED OF HAVING LATEST DATA

Refer to T.O. GR0171 for a listing of all current flight

manuals, safety supplements, operational supple

ments, and checklists. Also, check the flight manual

title page, the title block of each safety and

operational supplement, and all status pages

contained in the flight manual or attached to formal

safety and operational supplements. Clear all

discrepancies before flight.

ARRANGEMENT

The manual is divided into eight sections and three

supplemental appendices.

ILLUSTRATIONS

Cockpit arrangement, cockpit console, and cockpit

instrument panel illustrations display the delivered

configuration plus the approved equipment modifica

tions. For details of equipment modification, see the

individual equipment illustration.

SUPPLEMENT INFORMATION AND GUIDELINES

Supplements are safety or operational and are

indicated 1SS or 1S, respectively. Supplements are

issued as interim electronic messages or formal

printed copies. All interim supplements are assigned

odd numbers, such as 1SS195. When an interim

supplement is formalized, it is assigned the next

following even number, such as 1SS196. Formal

supplements not preceded by an interim supplement

are also assigned even numbers. If an interim

supplement is not to be formalized, a statement

cancelling the next assigned even supplement

number is included in the REMARKS section of the

interim supplement. If a formal supplement is not

preceded by an interim supplement, a statement

cancelling the previous odd supplement number is

included on the status page of the formal supplement.

Occasionally, a supplement has dual references in the

instructions; this is because the supplement applies

to the present and subsequent manual. Minor

text/illustration changes or deletions are given as

instructions in the supplement. When lengthy

additions are required, the formal supplement

provides onesided insert page(s) to the flight manual

and checklist. This supplement page(s) is attached to

the original page(s). The original page(s) remains in

the manual or checklist in case the supplement is

rescinded and the page(s) is needed. Added page(s)

(e.g., 348.1) are inserted in proper numerical

sequence and may be printed on both sides.

SAFETY SUPPLEMENTS

Information involving safety is promptly forwarded

in a safety supplement. Urgent information is

published in interim safety supplements and

transmitted by electronic message. Formal supple

ments are mailed. The supplement title block and

status page (published with formal supplements

only) should be checked to determine the effect of the

supplement on this manual and other outstanding

supplements.

OPERATIONAL SUPPLEMENTS

Information involving changes to operating proce

dures is forwarded by operational supplements. The

procedure for handling operational supplements is

the same as for safety supplements.

CHECKLIST

The checklist contains itemized procedures without

all of the amplification. Primary line items in the

flight manual and checklist are identical.

HOW TO GET PERSONAL COPIES

Each pilot is entitled to a personal copy of the flight

manual, safety supplements, operational supple

ments, and a checklist. The required quantities

should be ordered before needed to assure their

timely receipt. Check with the publication distribu

tion officer whose job is to fulfill T.O. requests.

Country manuals and difference data are assigned a

Country Standard T.O. (CSTO) number and indexed

in the Security Assistance Program T.O. Index, T.O.

GR0171. Updates, stock, store, and issue of CSTO's

are a contractor supported function. Insure a system

is established at each base to deliver the publications

to the pilots immediately upon receipt.

FLIGHT MANUAL BINDERS

Looseleaf binders and sectionalized tabs are avail

able for use with the manual. They are obtained

through local purchase procedures and are listed in

the USAF supply channels and may be ordered on the

supply case through AFLC. Check with supply

personnel for assistance in procuring these items.

CHANGE SYMBOL

The change symbol, as illustrated by the black line in

the margin of this paragraph, indicates changes

made to the current issue.

T.O. GR1F16CJ1

WARNINGS, CAUTIONS, AND NOTES

The following definitions apply to Warnings,

Cautions, and Notes found throughout the manual:

Operating procedures, techniques,

etc., which could result in personal

injury or loss of life if not carefully

followed.

Operating procedures, techniques,

etc., which could result in damage to

equipment if not carefully followed.

NOTE

An operating procedure, technique,

etc., which is considered essential to

emphasize.

USE OF WORDS SHALL, WILL, SHOULD, AND

MAY

The word shall or will is used to indicate a mandatory

requirement. The word should is used to indicate a

nonmandatory desired or preferred method of

accomplishment. The word may is used to indicate an

acceptable or suggested means of accomplishment.

USE OF WORDS AS DESIRED AND AS REQUIRED

As desired allows pilot preference in switch/control

positioning.

As required indicates those actions which vary based

on mission requirements.

AIRSPEED REFERENCES

All references to airspeed quoted in knots refer to

indicated airspeed.

PILOT'S RESPONSIBILITY-TO LET US KNOW

Every effort is made to keep the flight manual

current. Review conferences with operating person

nel and a constant review of safety investigation and

flight test reports assure inclusion of the latest data

in the manual. Comments, corrections, and questions

regarding this manual or any phase of the flight

manual program are welcomed. These should be

forwarded on AF Form 847 in accordance with AFI

11215 through command headquarters to OOALC/

YPVT, 6080 Gum Lane, Hill AFB, UT 840565825.

PUBLICATION DATE

The date appearing on the title page represents the

currency of material contained herein.

AIRCRAFT AND COCKPIT DESIGNATION CODES

System and/or component effectivity for a particular

aircraft version/cockpit is denoted by a letter code

enclosed in a box located in the text or on an

illustration. The symbols and designations are as

follows:

No code-F16C and F16D aircraft

F16C aircraft

F16D aircraft

F16D aircraft, forward cockpit

F16D aircraft, rear cockpit

PX II

Peace Xenia II aircraft

PX III

Peace Xenia III aircraft

ENGINE DESIGNATION CODES

System and/or component effectivity for a particular

engine version is denoted by an engine code enclosed

in a box located in the text or on an illustration. The

symbols and designations are as follows:

No code-Either engine

PW 229

F100PW229

129

F110GE129

BLOCK DESIGNATION CODES/SERIAL NUMBER/

TAIL NUMBER CROSSREFERENCE

Because of differences in configuration between

aircraft and to avoid repetitious use of aircraft serial

numbers, a block effectivity system is used. The block

effectivities reflect the aircraft block, the aircraft

serial number, and the tail number. Attrited aircraft

are removed from the listing. This system is used

throughout the manual, both in text and illustra

tions.

T.O. GR1F16CJ1

Change 1v

AIRCRAFT MODIFICATION/RETROFIT INFORMA

TION

This list includes the applicable T.O./ECP effectivi

ties. It is not an official status page. Refer to T.O. 014

for the complete listing of TCTO's. Throughout this

manual, black TV screen symbols containing white

numerals (

(2)

) are used to distinguish information

related to aircraft which are modified by a specific

T.O./ECP. Information pertaining to modified aircraft

is identified by an appropriate effectivity symbol.

Information which is not identified by an effectivity

symbol is considered common to all aircraft.

Information pertaining only to unmodified aircraft

has the appropriate effectivity symbol preceded by

LESS

. For example,

LESS

(4)

indicates that the

information is only applicable to aircraft not modified

by a specific T.O./ECP.

TV CODE/

EFFECTIVITY

T.O. NO.

SHORT TITLE

PRODUCTION

RETROFIT

b1q

1F162121

Summary:

Flight Control Com

puter Software Up

date (ECP 2269)

F16C 931055,

and on

F16D NA

F16C 931045 thru

931054

F16D All

Retrofit authorized

Modification incorporates FLCS improvements, including improved reset capability for FLCC pow

er up failures and elimination of lateral accelerometer failures during gun firing.

b2p

1F162170

Summary:

Modification of the

Ejection Mode Selec

tor Valve Console

(ECP 2362)

F16C NA

F16D 991534,

and on

F16C NA

F16D 931077 thru

931084

Retrofit authorized

Modification enlarges the hole in the console to allow the EJECTION MODE SEL handle to seat

properly in the NORM position.

b2t

XX1F162077

Summary:

Installation of

Improved Antiskid

Braking System

(OCP H086)

(ECP 2478)

F16C 991500,

and on

F16D 991534,

and on

F16C 931045 thru

931076

F16D 931077 thru

931084

Retrofit authorized

Modification incorporates an improved Brake Control/Antiskid Assembly to replace the current

Brake Control and Antiskid Control Boxes.

b6n

Summary:

Flight Control Com

puter Software Up

date for CFT

(ECP 2495)

F16C 991500,

and on

F16D 991534,

and on

Retrofit NA

Modification incorporates flight control system software updates to provide increased roll rate capa

bility in CAT III with CFT's and eliminate an existing prohibited maneuver.

T.O. GR1F16CJ1

viChange 1

TV CODE/

EFFECTIVITY

T.O. NO.

SHORT TITLE

PRODUCTION

RETROFIT

b7n

TBD

Summary:

AVIONICS FAULT

caution/ECM lights

CDEEU mod

(ECP 2526)

F16C 991507,

and on

F16D 991541,

and on

TBD

Retrofit TBD

Modification to circuitry in the CDEEU which will allow the AVIONICS FAULT caution and ECM

lights to illuminate in both cockpits of aircraft.

III

Block Designation Codes/Serial

Number/Tail Number CrossĆReference

T.O. GR1F16CJ1

Change 1vii

BLOCK 50

Serial Numbers/
Tail Numbers

PX II

931045/045

931046/046

931047/047

931048/048

931049/049

931050/050

931051/051

931052/052

931053/053

931054/054

931055/055

931056/056

931057/057

931058/058

931059/059

931060/060

931061/061

931062/062

931063/063

931064/064

931065/065

931066/066

931067/067

931068/068

931069/069

931070/070

931071/071

931072/072

931073/073

931074/074

931075/075

931076/076

PX II

931077/077

931078/078

931079/079

931080/080

931081/081

931082/082

931083/083

931084/084

BLOCK 52+

Serial Numbers/
Tail Numbers

PX III

991500/500

991501/501

991502/502

991503/503

991504/504

991505/505

991506/506

991507/507

991508/508

991509/509

991510/510

991511/511

991512/512

991513/513

991514/514

991515/515

991516/516

991517/517

991518/518

991519/519

991520/520

991521/521

991522/522

991523/523

991524/524

991525/525

991526/526

991527/527

991528/528

991529/529

991530/530

991531/531

991532/532

991533/533

018530/534

018531/535

018532/536

018533/537

018534/538

018535/539

PX III

991534/600

991535/601

991536/602

991537/603

991538/604

991539/605

991540/606

991541/607

991542/608

991543/609

991544/610

991545/611

991546/612

991547/613

991548/614

991549/615

018536/616

018537/617

018538/618

018539/619

T.O. GR1F16CJ1

viiiChange 1

GR1F-16CJ-1-0003A37

T.O. GR1F16CJ1

SECTION I

DESCRIPTION AND OPERATION

TABLE OF CONTENTS

The Aircraft

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

Aircraft General Data

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

Aircraft General Arrangement

. . . . . . . . . . .

Aircraft Gross Weight (A/C GW)

. . . . . . . . . .

Cockpit Arrangement

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

Engine

PW 229

131

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

Engine General Description

PW 229

131

. . . . . .

Engine Fuel System

PW 229

131

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

Engine Control System

PW 229

131

. . . . . . . . . . .

Main Fuel Control (MFC)

PW 229

131

. . . . . .

Afterburner (AB) Fuel

Control

PW 229

131

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

Digital Electronic Engine Control

(DEEC)

PW 229

133

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

Secondary Engine Control

(SEC)

PW 229

133

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

Main Fuel Pump

PW 229

133

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

Afterburner (AB) Fuel

Pump

PW 229

133

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

Compressor Inlet Variable Vane

(CIVV) Control

PW 229

133

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

Rear Compressor Variable Vanes

(RCVV's)

PW 229

133

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

Compressor Bleed Air

PW 229

134

. . . . . . . . .

Pressurization and Dump

Valve

PW 229

134

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

Exhaust Nozzle

PW 229

134

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

Convergent Exhaust Nozzle Control

(CENC)

PW 229

134

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

LightOff Detector (LOD)

PW 229

134

. . . . . .

Engine Diagnostic Unit (EDU)

PW 229

134

. . . .

Engine Oil System

PW 229

134

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

FUEL/OIL HOT Caution

Light

PW 229

134

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

Engine AntiIce System

PW 229

135

. . . . . . . . . .

Engine ANTI ICE Switch

PW 229

135

. . . . . .

INLET ICING Caution

Light

PW 229

135

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

Engine and Accessory Drive

Gearboxes

PW 229

135

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

Engine Alternator

PW 229

135

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

Engine Ignition System

PW 229

135

. . . . . . . . . .

Jet Fuel Starter (JFS)

PW 229

136

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

ENG & JET START Control

Panel

PW 229

136

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

JFS Switch

PW 229

136

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

JFS RUN Light

PW 229

136

. . . . . . . . .

JFS Operation

PW 229

137

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

Engine Controls and

Indicators

PW 229

137

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

ENG CONT Switch

PW 229

137

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

AB RESET Switch

PW 229

139

. . . . . .

ENGINE FAULT Caution

Light

PW 229

139

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

Pilot Fault List Display

(PFLD)

PW 229

139

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

SEC Caution Light

PW 229

139

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

EEC Caution Light

PW 229

139

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

BUC Caution Light

PW 229

139

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

MAX POWER Switch

PW 229

139

. . . .

RPM Indicator

PW 229

139

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

NOZ POS Indicator

PW 229

139

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

FTIT Indicator

PW 229

139

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

FUEL FLOW Indicator

PW 229

139

. . . . . . . .

OIL Pressure Indicator

PW 229

139

. . . . . . . .

HYD/OIL PRESS Warning

Light

PW 229

139

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

ENGINE Warning Light

PW 229

140

. . . . . . .

Throttle

PW 229

140

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

Engine Operating

Characteristics

PW 229

140

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

Engine General

PW 229

140

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

Ground Operations

PW 229

140

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

NonAB Operation in

Flight

PW 229

140

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

AB Operation in Flight

PW 229

142

. . . . . . . .

SEC Operation

PW 229

142

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

Engine

129

144

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

General Description

129

144

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

Engine Fuel/Control System

129

144

. . . . . .

Digital Electronic Control

(DEC)

129

144

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

Afterburner Fuel Control

(AFC)

129

144

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

Main Engine Control (MEC)

129

144

. . .

Primary (PRI) Engine

Operation

129

144

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

Content .. 1 2 ..

//////////////////////////

F16C/D. FLIGHT MANUAL (2002) - page 1

F16C/D. FLIGHT MANUAL (2002) - page 1