T.O. GR1FĆ16CJĆ1

FLIGHT MANUAL
HAF SERIES AIRCRAFT

FĆ16C/D

BLOCKS 50 AND 52+

LOCKHEED MARTIN CORPORATION
F33657Ć90ĆCĆ2...
T.O. GR1FĆ16CJĆ1

DISCLOSURE STATEMENT
This information is furnished on the conditions that it will not be released to ano...
T.O. GR1FĆ16CJĆ1
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LIST OF EFFECTIVE PAGES
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No.

*Change
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T.O. GR1FĆ16CJĆ1
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Page
No.

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T.O. GR1FĆ16CJĆ1
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T.O. GR1FĆ16CJĆ1
FLIGHT MANUALS, SAFETY SUPPLEMENT, AND
OPERATIONAL SUPPLEMENT STATUS
This supplement status page is based...
T.O. GR1FĆ16CJĆ1

TABLE OF CONTENTS
SECTION I

Description and Operation

1Ć1

SECTION II

Normal Procedures

2Ć1

SECTION...
T.O. GR1FĆ16CJĆ1

BEFORE
YOU
TAKE OFF,
READ THIS!

1F-16X-1-0002X

T.O. GR1FĆ16CJĆ6CFĆ1

SCOPE
This manual contains the ne...
T.O. GR1FĆ16CJĆ1
HOW TO BE ASSURED OF HAVING LATEST DATA

SAFETY SUPPLEMENTS

Refer to T.O. GR0Ć1Ć71 for a listing of all ...
T.O. GR1FĆ16CJĆ1
WARNINGS, CAUTIONS, AND NOTES
The following definitions apply to Warnings,
Cautions, and Notes found thro...
T.O. GR1FĆ16CJĆ1
AIRCRAFT MODIFICATION/RETROFIT INFORMAĆ
TION
This list includes the applicable T.O./ECP effectiviĆ
ties. ...
T.O. GR1FĆ16CJĆ1
TV CODE/
T.O. NO.
b7n

TBD

SHORT TITLE
AVIONICS FAULT
caution/ECM lights
CDEEU mod
(ECP 2526)

EFFECTIVI...
T.O. GR1FĆ16CJĆ1

Block Designation Codes/Serial
Number/Tail Number CrossĆReference
BLOCK 50
Serial Numbers/
Tail Numbers
...
T.O. GR1FĆ16CJĆ1

C

D

GR1F-16CJ-1-0003A37

viiiąąąăChange 1
T.O. GR1FĆ16CJĆ1

SECTION I
DESCRIPTION AND OPERATION
TABLE OF CONTENTS
The Aircraft . . . . . . . . . . . . . . . . . . ....
T.O. GR1FĆ16CJĆ1
Hybrid (HYB) Engine
Operation GE 129 . . . . . . . . . . . . . . . . . .
Secondary Engine Control (SEC)
O...
T.O. GR1FĆ16CJĆ1
Standby AC Power System . . . . . . . . . . . . . . . 1Ć83
Emergency AC Power System . . . . . . . . . . ...
T.O. GR1FĆ16CJĆ1
FLCS Warning, Caution, and Indicator
Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
F...
T.O. GR1FĆ16CJĆ1
Oxygen System PX II . . . . . . . . . . . . . . . . . . . . .
Liquid Oxygen System . . . . . . . . . . . ...
T.O. GR1FĆ16CJĆ1
AIFF Interrogator . . . . . . . . . . . . . . . . . . . . . .
Operation of the Interrogator on
Upfront Co...
T.O. GR1FĆ16CJĆ1
AIRCRAFT GENERAL DATA

AIRCRAFT GROSS WEIGHT (A/C GW)

Refer to figure 1Ć1. The aircraft approximate
dime...
T.O. GR1FĆ16CJĆ1

General Data
AIM-9 MISSILE
MISSILE LAUNCHER
15.16

13.32
OUTBOARD STORES LOCATIONS

FLAPERON
40

370-GAL...
T.O. GR1FĆ16CJĆ1

WINGS
Area
Span
Aspect Ratio
Taper Ratio
Sweep (LE)
Dihedral
Airfoil
Incidence
Twist
At BL 54.0
At BL 18...
8

11

11

8

25

15
16
15
13 14

For antenna locations, refer
to ANTENNA LOCATIONS,
this section.

17
27

23

C

8
5

9 1...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX II
DF

DF
INSTRUMENT
PANEL

LEFT
AUXILIARY
CONSOLE

RIGHT
AUXILIAR...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX II
LEFT CONSOLE

23
22
24

1
2

21

20

4

18 19
17

14

5

15 16
...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX II
LEFT AUXILIARY CONSOLE

RIGHT AUXILIARY CONSOLE

DF

18

19

1
...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX II
INSTRUMENT PANEL

DF

1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
13...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX II
RIGHT CONSOLE

17

19

1
2

DF
18

4

3

16

5

6

15
14

10
13...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX II

INSTRUMENT
PANEL

LEFT
AUXILIARY
CONSOLE

RIGHT
AUXILIARY
CONSOL...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX II
LEFT CONSOLE

7
9
8

1
2

6

10
5
11

1.
2.
3.
4.
5.
6.
7.
8.
9.
...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX II
LEFT AUXILIARY CONSOLE

1

15

2

4
7

14

5

12
10

6
1

9

11
8...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX II
INSTRUMENT PANEL

1. MASTER CAUTION Light (Amber)
2. ENG FIRE and...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX II
RIGHT CONSOLE

7
8

6
1

5

2
4

1.
2.
3.
4.
5.
6.
7.
8.

3

Inte...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX III
DF

DF

INSTRUMENT
PANEL

LEFT
AUXILIARY
CONSOLE

RIGHT
AUXILI...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX III
LEFT CONSOLE

24
23
25

1
2

22

21

3

4

19 20

7

5

18

16...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX III
LEFT AUXILIARY CONSOLE

RIGHT AUXILIARY CONSOLE

DF

18

19

1...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX III
INSTRUMENT PANEL

DF

1.
2.
3.
4.
5.
6.
7.
8.
9.
10.
11.
12.
1...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement C DF (Typical) PX III
RIGHT CONSOLE

17

DF
18

4

3

16

5

6

15
14

19

1
2

20
1...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX III

INSTRUMENT
PANEL

LEFT
AUXILIARY
CONSOLE

RIGHT
AUXILIARY
CONSO...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX III
LEFT CONSOLE

7
9
8

1
2

6

10
5
11

1.
2.
3.
4.
5.
6.
7.
8.
9....
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX III
LEFT AUXILIARY CONSOLE

1

15

2

4
7

14

5

12
10

6
1

9

11
...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX III
INSTRUMENT PANEL

1. MASTER CAUTION Light (Amber) (NVIS)
40 41
3...
T.O. GR1FĆ16CJĆ1

Cockpit Arrangement DR (Typical) PX III
RIGHT CONSOLE

7
9

6

8

1

5

2
4

1.
2.
3.
4.
5.
6.
7.
8.
9.
...
T.O. GR1FĆ16CJĆ1

ENGINE

Main Fuel Control (MFC)

PW 229

ENGINE GENERAL DESCRIPTION

PW 229

Refer to figure 1Ć4. The ai...
T.O. GR1FĆ16CJĆ1

Engine Fuel/Control System Schematic
ENGINE F100-PW-229
(Typical)
LEGEND:
ELECTRICAL
MECHANICAL
ENG BLEE...
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Haf Flight Manual f16

  1. 1. T.O. GR1FĆ16CJĆ1 FLIGHT MANUAL HAF SERIES AIRCRAFT FĆ16C/D BLOCKS 50 AND 52+ LOCKHEED MARTIN CORPORATION F33657Ć90ĆCĆ2002 F42620Ć01ĆDĆ0058 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. 15 OCTOBER 2002 CHANGE 1ąąă15 JUNE 2003
  2. 2. T.O. GR1FĆ16CJĆ1 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 OOĆALC/YPXG, 6089 Wardleigh Road, Hill AFB, UT 84056Ć5838. SUPPLEMENTAL NOTICE This manual is incomplete without T.O. GR1FĆ16CJĆ1Ć1 and T.O. GR1FĆ16CJĆ1Ć2. SUPERSEDURE NOTICE See Technical Order Index, T.O. GR0Ć1Ć71, for current status of Flight Manuals, Safety Supplements, OperaĆ tional Supplements, and Flight Crew Checklists. This manual supersedes T.O. 1Ć1CĆ1Ć30 and Interim Safety Supplements T.O. GR1FĆ16CJĆ1SSĆ27 and T.O. GR1FĆ16CJĆ1SSĆ29, and Interim Operational Supplement T.O. GR1FĆ16CJĆ1SĆ31. TĆ2ąChange 1ąąă
  3. 3. T.O. GR1FĆ16CJĆ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. LIST OF EFFECTIVE PAGES NOTE:ąChanges to the current issue are indicated by a vertical line in the outer margins of the page. Dates of issue for original and changed pages are: Original . . . 0 . . . . 15 Oct 02 Change . . . . 1 . . . . 15 Jun 03 TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 522, CONSISTING OF THE FOLLOWING: Page No. * Change No. Title . . . . . . . . . . . . . . . . . . . . TĆ2 . . . . . . . . . . . . . . . . . . . . . . A ....................... B ....................... C ....................... D ....................... a ....................... b Blank . . . . . . . . . . . . . . . . . i ........................ ii . . . . . . . . . . . . . . . . . . . . . . . iii . . . . . . . . . . . . . . . . . . . . . . . iv . . . . . . . . . . . . . . . . . . . . . . . v........................ vi . . . . . . . . . . . . . . . . . . . . . . . vii . . . . . . . . . . . . . . . . . . . . . . viii . . . . . . . . . . . . . . . . . . . . . . 1Ć1 . . . . . . . . . . . . . . . . . . . . . . 1Ć2 . . . . . . . . . . . . . . . . . . . . . . 1Ć3 . . . . . . . . . . . . . . . . . . . . . . 1Ć4 . . . . . . . . . . . . . . . . . . . . . . 1Ć5 . . . . . . . . . . . . . . . . . . . . . . 1Ć6 . . . . . . . . . . . . . . . . . . . . . . 1Ć7 . . . . . . . . . . . . . . . . . . . . . . 1Ć8 . . . . . . . . . . . . . . . . . . . . . . 1Ć9 . . . . . . . . . . . . . . . . . . . . . . 1Ć10 . . . . . . . . . . . . . . . . . . . . . 1Ć11 . . . . . . . . . . . . . . . . . . . . . 1Ć12 . . . . . . . . . . . . . . . . . . . . . 1Ć13 . . . . . . . . . . . . . . . . . . . . . 1Ć14 . . . . . . . . . . . . . . . . . . . . . 1Ć15 . . . . . . . . . . . . . . . . . . . . . 1Ć16 . . . . . . . . . . . . . . . . . . . . . 1Ć17 . . . . . . . . . . . . . . . . . . . . . 1Ć18 . . . . . . . . . . . . . . . . . . . . . 1Ć19 . . . . . . . . . . . . . . . . . . . . . 1Ć20 . . . . . . . . . . . . . . . . . . . . . 1Ć21 . . . . . . . . . . . . . . . . . . . . . 1Ć22 . . . . . . . . . . . . . . . . . . . . . 1Ć23 . . . . . . . . . . . . . . . . . . . . . 1Ć24 . . . . . . . . . . . . . . . . . . . . . 1Ć25 . . . . . . . . . . . . . . . . . . . . . 1Ć26 . . . . . . . . . . . . . . . . . . . . . 1Ć27 . . . . . . . . . . . . . . . . . . . . . 1 1 1 1 1 1 1 0 1 1 1 0 1 1 1 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 1 1 0 0 Page No. * Change No. 1Ć28 . . . . . . . . . . . . . . . . . . . . . 1Ć29 . . . . . . . . . . . . . . . . . . . . . 1Ć30 . . . . . . . . . . . . . . . . . . . . . 1Ć31 . . . . . . . . . . . . . . . . . . . . . 1Ć32 . . . . . . . . . . . . . . . . . . . . . 1Ć33 . . . . . . . . . . . . . . . . . . . . . 1Ć34 . . . . . . . . . . . . . . . . . . . . . 1Ć35 . . . . . . . . . . . . . . . . . . . . . 1Ć36 . . . . . . . . . . . . . . . . . . . . . 1Ć37 . . . . . . . . . . . . . . . . . . . . . 1Ć38 . . . . . . . . . . . . . . . . . . . . . 1Ć39 . . . . . . . . . . . . . . . . . . . . . 1Ć40 . . . . . . . . . . . . . . . . . . . . . 1Ć41 . . . . . . . . . . . . . . . . . . . . . 1Ć42 . . . . . . . . . . . . . . . . . . . . . 1Ć43 . . . . . . . . . . . . . . . . . . . . . 1Ć44 . . . . . . . . . . . . . . . . . . . . . 1Ć45 . . . . . . . . . . . . . . . . . . . . . 1Ć46 . . . . . . . . . . . . . . . . . . . . . 1Ć47 . . . . . . . . . . . . . . . . . . . . . 1Ć48 . . . . . . . . . . . . . . . . . . . . . 1Ć49 . . . . . . . . . . . . . . . . . . . . . 1Ć50 . . . . . . . . . . . . . . . . . . . . . 1Ć51 . . . . . . . . . . . . . . . . . . . . . 1Ć52 . . . . . . . . . . . . . . . . . . . . . 1Ć53 . . . . . . . . . . . . . . . . . . . . . 1Ć54 . . . . . . . . . . . . . . . . . . . . . 1Ć55 . . . . . . . . . . . . . . . . . . . . . 1Ć56 . . . . . . . . . . . . . . . . . . . . . 1Ć57 . . . . . . . . . . . . . . . . . . . . . 1Ć58 . . . . . . . . . . . . . . . . . . . . . 1Ć59 . . . . . . . . . . . . . . . . . . . . . 1Ć60 . . . . . . . . . . . . . . . . . . . . . 1Ć61 . . . . . . . . . . . . . . . . . . . . . 1Ć62 . . . . . . . . . . . . . . . . . . . . . 1Ć63 . . . . . . . . . . . . . . . . . . . . . 1Ć64 . . . . . . . . . . . . . . . . . . . . . 1Ć65 . . . . . . . . . . . . . . . . . . . . . 1Ć66 . . . . . . . . . . . . . . . . . . . . . 1Ć67 . . . . . . . . . . . . . . . . . . . . . 1Ć68 . . . . . . . . . . . . . . . . . . . . . 1Ć69 . . . . . . . . . . . . . . . . . . . . . 1Ć70 . . . . . . . . . . . . . . . . . . . . . 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 Page No. * Change No. 1Ć71 . . . . . . . . . . . . . . . . . . . . . 1Ć72 . . . . . . . . . . . . . . . . . . . . . 1Ć73 . . . . . . . . . . . . . . . . . . . . . 1Ć74 . . . . . . . . . . . . . . . . . . . . . 1Ć75 . . . . . . . . . . . . . . . . . . . . . 1Ć76 . . . . . . . . . . . . . . . . . . . . . 1Ć77 . . . . . . . . . . . . . . . . . . . . . 1Ć78 . . . . . . . . . . . . . . . . . . . . . 1Ć79 . . . . . . . . . . . . . . . . . . . . . 1Ć80 . . . . . . . . . . . . . . . . . . . . . 1Ć81 . . . . . . . . . . . . . . . . . . . . . 1Ć82 . . . . . . . . . . . . . . . . . . . . . 1Ć83 . . . . . . . . . . . . . . . . . . . . . 1Ć84 . . . . . . . . . . . . . . . . . . . . . 1Ć85 . . . . . . . . . . . . . . . . . . . . . 1Ć86 . . . . . . . . . . . . . . . . . . . . . 1Ć87 . . . . . . . . . . . . . . . . . . . . . 1Ć88 . . . . . . . . . . . . . . . . . . . . . 1Ć89 . . . . . . . . . . . . . . . . . . . . . 1Ć90 . . . . . . . . . . . . . . . . . . . . . 1Ć91 . . . . . . . . . . . . . . . . . . . . . 1Ć92 . . . . . . . . . . . . . . . . . . . . . 1Ć93 . . . . . . . . . . . . . . . . . . . . . 1Ć94 . . . . . . . . . . . . . . . . . . . . . 1Ć95 . . . . . . . . . . . . . . . . . . . . . 1Ć96 . . . . . . . . . . . . . . . . . . . . . 1Ć97 . . . . . . . . . . . . . . . . . . . . . 1Ć98 . . . . . . . . . . . . . . . . . . . . . 1Ć99 . . . . . . . . . . . . . . . . . . . . . 1Ć100 . . . . . . . . . . . . . . . . . . . . 1Ć101 . . . . . . . . . . . . . . . . . . . . 1Ć102 . . . . . . . . . . . . . . . . . . . . 1Ć103 . . . . . . . . . . . . . . . . . . . . 1Ć104 . . . . . . . . . . . . . . . . . . . . 1Ć105 . . . . . . . . . . . . . . . . . . . . 1Ć106 . . . . . . . . . . . . . . . . . . . . 1Ć107 . . . . . . . . . . . . . . . . . . . . 1Ć108 . . . . . . . . . . . . . . . . . . . . 1Ć109 . . . . . . . . . . . . . . . . . . . . 1Ć110 . . . . . . . . . . . . . . . . . . . . 1Ć111 . . . . . . . . . . . . . . . . . . . . 1Ć112 . . . . . . . . . . . . . . . . . . . . 1Ć113 . . . . . . . . . . . . . . . . . . . . 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 * Zero in this column indicates an original page. BĆ1 HAF Change 1ąąąăA
  4. 4. T.O. GR1FĆ16CJĆ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. LIST OF EFFECTIVE PAGES (Cont) Page No. *Change No. 1Ć114 . . . . . . . . . . . . . . . . . . . . 1Ć115 . . . . . . . . . . . . . . . . . . . . 1Ć116 . . . . . . . . . . . . . . . . . . . . 1Ć117 . . . . . . . . . . . . . . . . . . . . 1Ć118 . . . . . . . . . . . . . . . . . . . . 1Ć119 . . . . . . . . . . . . . . . . . . . . 1Ć120 . . . . . . . . . . . . . . . . . . . . 1Ć121 . . . . . . . . . . . . . . . . . . . . 1Ć122 . . . . . . . . . . . . . . . . . . . . 1Ć123 . . . . . . . . . . . . . . . . . . . . 1Ć124 . . . . . . . . . . . . . . . . . . . . 1Ć125 . . . . . . . . . . . . . . . . . . . . 1Ć126 . . . . . . . . . . . . . . . . . . . . 1Ć127 . . . . . . . . . . . . . . . . . . . . 1Ć128 . . . . . . . . . . . . . . . . . . . . 1Ć129 . . . . . . . . . . . . . . . . . . . . 1Ć130 . . . . . . . . . . . . . . . . . . . . 1Ć131 . . . . . . . . . . . . . . . . . . . . 1Ć132 . . . . . . . . . . . . . . . . . . . . 1Ć133 . . . . . . . . . . . . . . . . . . . . 1Ć134 . . . . . . . . . . . . . . . . . . . . 1Ć135 . . . . . . . . . . . . . . . . . . . . 1Ć136 . . . . . . . . . . . . . . . . . . . . 1Ć137 . . . . . . . . . . . . . . . . . . . . 1Ć138 . . . . . . . . . . . . . . . . . . . . 1Ć139 . . . . . . . . . . . . . . . . . . . . 1Ć140 . . . . . . . . . . . . . . . . . . . . 1Ć141 . . . . . . . . . . . . . . . . . . . . 1Ć142 . . . . . . . . . . . . . . . . . . . . 1Ć143 . . . . . . . . . . . . . . . . . . . . 1Ć144 . . . . . . . . . . . . . . . . . . . . 1Ć145 . . . . . . . . . . . . . . . . . . . . 1Ć146 . . . . . . . . . . . . . . . . . . . . 1Ć147 . . . . . . . . . . . . . . . . . . . . 1Ć148 . . . . . . . . . . . . . . . . . . . . 1Ć149 . . . . . . . . . . . . . . . . . . . . 1Ć150 . . . . . . . . . . . . . . . . . . . . 1Ć151 . . . . . . . . . . . . . . . . . . . . 1Ć152 . . . . . . . . . . . . . . . . . . . . 1Ć153 . . . . . . . . . . . . . . . . . . . . 1Ć154 . . . . . . . . . . . . . . . . . . . . 1Ć155 . . . . . . . . . . . . . . . . . . . . 1Ć156 . . . . . . . . . . . . . . . . . . . . 1Ć157 . . . . . . . . . . . . . . . . . . . . 1Ć158 . . . . . . . . . . . . . . . . . . . . 1Ć159 . . . . . . . . . . . . . . . . . . . . 1Ć160 . . . . . . . . . . . . . . . . . . . . 1Ć161 . . . . . . . . . . . . . . . . . . . . 1Ć162 . . . . . . . . . . . . . . . . . . . . 1Ć163 . . . . . . . . . . . . . . . . . . . . 1Ć164 . . . . . . . . . . . . . . . . . . . . 1Ć165 . . . . . . . . . . . . . . . . . . . . 1Ć166 . . . . . . . . . . . . . . . . . . . . 1Ć167 . . . . . . . . . . . . . . . . . . . . 1Ć168 . . . . . . . . . . . . . . . . . . . . 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 Page No. *Change No. 1Ć169 . . . . . . . . . . . . . . . . . . . . 1Ć170 . . . . . . . . . . . . . . . . . . . . 1Ć171 . . . . . . . . . . . . . . . . . . . . 1Ć172 . . . . . . . . . . . . . . . . . . . . 1Ć173 . . . . . . . . . . . . . . . . . . . . 1Ć174 . . . . . . . . . . . . . . . . . . . . 1Ć175 . . . . . . . . . . . . . . . . . . . . 1Ć176 . . . . . . . . . . . . . . . . . . . . 1Ć177 . . . . . . . . . . . . . . . . . . . . 1Ć178 . . . . . . . . . . . . . . . . . . . . 1Ć179 . . . . . . . . . . . . . . . . . . . . 1Ć180 . . . . . . . . . . . . . . . . . . . . 1Ć181 . . . . . . . . . . . . . . . . . . . . 1Ć182 . . . . . . . . . . . . . . . . . . . . 1Ć183 . . . . . . . . . . . . . . . . . . . . 1Ć184 . . . . . . . . . . . . . . . . . . . . 1Ć185 . . . . . . . . . . . . . . . . . . . . 1Ć186 . . . . . . . . . . . . . . . . . . . . 1Ć187 . . . . . . . . . . . . . . . . . . . . 1Ć188 . . . . . . . . . . . . . . . . . . . . 1Ć189 . . . . . . . . . . . . . . . . . . . . 1Ć190 . . . . . . . . . . . . . . . . . . . . 1Ć191 . . . . . . . . . . . . . . . . . . . . 1Ć192 . . . . . . . . . . . . . . . . . . . . 1Ć193 . . . . . . . . . . . . . . . . . . . . 1Ć194 . . . . . . . . . . . . . . . . . . . . 1Ć195 . . . . . . . . . . . . . . . . . . . . 1Ć196 . . . . . . . . . . . . . . . . . . . . 1Ć197 . . . . . . . . . . . . . . . . . . . . 1Ć198 . . . . . . . . . . . . . . . . . . . . 1Ć199 . . . . . . . . . . . . . . . . . . . . 1Ć200 . . . . . . . . . . . . . . . . . . . . 1Ć201 . . . . . . . . . . . . . . . . . . . . 1Ć202 . . . . . . . . . . . . . . . . . . . . 1Ć203 . . . . . . . . . . . . . . . . . . . . 1Ć204 . . . . . . . . . . . . . . . . . . . . 1Ć205 . . . . . . . . . . . . . . . . . . . . 1Ć206 . . . . . . . . . . . . . . . . . . . . 1Ć207 . . . . . . . . . . . . . . . . . . . . 1Ć208 . . . . . . . . . . . . . . . . . . . . 1Ć209 . . . . . . . . . . . . . . . . . . . . 1Ć210 . . . . . . . . . . . . . . . . . . . . 1Ć211 . . . . . . . . . . . . . . . . . . . . 1Ć212 . . . . . . . . . . . . . . . . . . . . 1Ć213 . . . . . . . . . . . . . . . . . . . . 1Ć214 . . . . . . . . . . . . . . . . . . . . 1Ć215 . . . . . . . . . . . . . . . . . . . . 1Ć216 . . . . . . . . . . . . . . . . . . . . 1Ć217 . . . . . . . . . . . . . . . . . . . . 1Ć218 . . . . . . . . . . . . . . . . . . . . 1Ć219 . . . . . . . . . . . . . . . . . . . . 1Ć220 . . . . . . . . . . . . . . . . . . . . 1Ć221 . . . . . . . . . . . . . . . . . . . . 1Ć222 . . . . . . . . . . . . . . . . . . . . 1Ć223 . . . . . . . . . . . . . . . . . . . . 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 1 1 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 * Zero in this column indicates an original page. BąąąăChange 1 Page No. *Change No. 1Ć224 . . . . . . . . . . . . . . . . . . . . 1Ć225 . . . . . . . . . . . . . . . . . . . . 1Ć226 . . . . . . . . . . . . . . . . . . . . 2Ć1 . . . . . . . . . . . . . . . . . . . . . . 2Ć2 . . . . . . . . . . . . . . . . . . . . . . 2Ć3 . . . . . . . . . . . . . . . . . . . . . . 2Ć4 . . . . . . . . . . . . . . . . . . . . . . 2Ć5 . . . . . . . . . . . . . . . . . . . . . . 2Ć6 . . . . . . . . . . . . . . . . . . . . . . 2Ć7 . . . . . . . . . . . . . . . . . . . . . . 2Ć8 . . . . . . . . . . . . . . . . . . . . . . 2Ć9 . . . . . . . . . . . . . . . . . . . . . . 2Ć10 . . . . . . . . . . . . . . . . . . . . . 2Ć11 . . . . . . . . . . . . . . . . . . . . . 2Ć12 . . . . . . . . . . . . . . . . . . . . . 2Ć13 . . . . . . . . . . . . . . . . . . . . . 2Ć14 . . . . . . . . . . . . . . . . . . . . . 2Ć15 . . . . . . . . . . . . . . . . . . . . . 2Ć16 . . . . . . . . . . . . . . . . . . . . . 2Ć17 . . . . . . . . . . . . . . . . . . . . . 2Ć18 . . . . . . . . . . . . . . . . . . . . . 2Ć19 . . . . . . . . . . . . . . . . . . . . . 2Ć20 . . . . . . . . . . . . . . . . . . . . . 2Ć21 . . . . . . . . . . . . . . . . . . . . . 2Ć22 . . . . . . . . . . . . . . . . . . . . . 2Ć23 . . . . . . . . . . . . . . . . . . . . . 2Ć24 . . . . . . . . . . . . . . . . . . . . . 2Ć25 . . . . . . . . . . . . . . . . . . . . . 2Ć26 . . . . . . . . . . . . . . . . . . . . . 2Ć27 . . . . . . . . . . . . . . . . . . . . . 2Ć28 . . . . . . . . . . . . . . . . . . . . . 2Ć29 . . . . . . . . . . . . . . . . . . . . . 2Ć30 . . . . . . . . . . . . . . . . . . . . . 2Ć31 . . . . . . . . . . . . . . . . . . . . . 2Ć32 . . . . . . . . . . . . . . . . . . . . . 2Ć33 . . . . . . . . . . . . . . . . . . . . . 2Ć34 . . . . . . . . . . . . . . . . . . . . . 2Ć35 . . . . . . . . . . . . . . . . . . . . . 2Ć36 . . . . . . . . . . . . . . . . . . . . . 2Ć37 . . . . . . . . . . . . . . . . . . . . . 2Ć38 . . . . . . . . . . . . . . . . . . . . . 2Ć39 . . . . . . . . . . . . . . . . . . . . . 2Ć40 . . . . . . . . . . . . . . . . . . . . . 2Ć41 . . . . . . . . . . . . . . . . . . . . . 2Ć42 . . . . . . . . . . . . . . . . . . . . . 3Ć1 . . . . . . . . . . . . . . . . . . . . . . 3Ć2 . . . . . . . . . . . . . . . . . . . . . . 3Ć3 . . . . . . . . . . . . . . . . . . . . . . 3Ć4 . . . . . . . . . . . . . . . . . . . . . . 3Ć5 . . . . . . . . . . . . . . . . . . . . . . 3Ć6 . . . . . . . . . . . . . . . . . . . . . . 3Ć7 . . . . . . . . . . . . . . . . . . . . . . 3Ć8 . . . . . . . . . . . . . . . . . . . . . . 3Ć9 . . . . . . . . . . . . . . . . . . . . . . 3Ć10 . . . . . . . . . . . . . . . . . . . . . 0 0 0 0 0 0 0 1 0 0 0 0 0 0 1 1 0 0 0 1 0 0 0 0 0 1 0 0 1 0 0 0 1 0 0 0 1 1 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 1 0
  5. 5. T.O. GR1FĆ16CJĆ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. LIST OF EFFECTIVE PAGES (Cont) Page No. *Change No. 3Ć11 . . . . . . . . . . . . . . . . . . . . . 3Ć12 . . . . . . . . . . . . . . . . . . . . . 3Ć13 . . . . . . . . . . . . . . . . . . . . . 3Ć14 . . . . . . . . . . . . . . . . . . . . . 3Ć15 . . . . . . . . . . . . . . . . . . . . . 3Ć16 . . . . . . . . . . . . . . . . . . . . . 3Ć17 . . . . . . . . . . . . . . . . . . . . . 3Ć18 . . . . . . . . . . . . . . . . . . . . . 3Ć19 . . . . . . . . . . . . . . . . . . . . . 3Ć20 . . . . . . . . . . . . . . . . . . . . . 3Ć21 . . . . . . . . . . . . . . . . . . . . . 3Ć22 . . . . . . . . . . . . . . . . . . . . . 3Ć23 . . . . . . . . . . . . . . . . . . . . . 3Ć24 . . . . . . . . . . . . . . . . . . . . . 3Ć25 . . . . . . . . . . . . . . . . . . . . . 3Ć26 . . . . . . . . . . . . . . . . . . . . . 3Ć27 . . . . . . . . . . . . . . . . . . . . . 3Ć28 . . . . . . . . . . . . . . . . . . . . . 3Ć29 . . . . . . . . . . . . . . . . . . . . . 3Ć30 . . . . . . . . . . . . . . . . . . . . . 3Ć31 . . . . . . . . . . . . . . . . . . . . . 3Ć32 . . . . . . . . . . . . . . . . . . . . . 3Ć33 . . . . . . . . . . . . . . . . . . . . . 3Ć34 . . . . . . . . . . . . . . . . . . . . . 3Ć35 . . . . . . . . . . . . . . . . . . . . . 3Ć36 . . . . . . . . . . . . . . . . . . . . . 3Ć37 . . . . . . . . . . . . . . . . . . . . . 3Ć38 . . . . . . . . . . . . . . . . . . . . . 3Ć39 . . . . . . . . . . . . . . . . . . . . . 3Ć40 . . . . . . . . . . . . . . . . . . . . . 3Ć40.1 Added . . . . . . . . . . . . . 3Ć40.2 Blank Added . . . . . . 3Ć41 . . . . . . . . . . . . . . . . . . . . . 3Ć42 . . . . . . . . . . . . . . . . . . . . . 3Ć43 . . . . . . . . . . . . . . . . . . . . . 3Ć44 . . . . . . . . . . . . . . . . . . . . . 3Ć45 . . . . . . . . . . . . . . . . . . . . . 3Ć46 . . . . . . . . . . . . . . . . . . . . . 3Ć47 . . . . . . . . . . . . . . . . . . . . . 3Ć48 . . . . . . . . . . . . . . . . . . . . . 3Ć49 . . . . . . . . . . . . . . . . . . . . . 3Ć50 . . . . . . . . . . . . . . . . . . . . . 3Ć51 . . . . . . . . . . . . . . . . . . . . . 3Ć52 . . . . . . . . . . . . . . . . . . . . . 3Ć53 . . . . . . . . . . . . . . . . . . . . . 3Ć54 . . . . . . . . . . . . . . . . . . . . . 3Ć55 . . . . . . . . . . . . . . . . . . . . . 3Ć56 . . . . . . . . . . . . . . . . . . . . . 3Ć57 . . . . . . . . . . . . . . . . . . . . . 3Ć58 . . . . . . . . . . . . . . . . . . . . . 3Ć59 . . . . . . . . . . . . . . . . . . . . . 3Ć60 . . . . . . . . . . . . . . . . . . . . . 3Ć61 . . . . . . . . . . . . . . . . . . . . . 3Ć62 . . . . . . . . . . . . . . . . . . . . . 3Ć63 . . . . . . . . . . . . . . . . . . . . . 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 1 1 0 1 1 1 1 0 0 1 0 0 0 0 1 1 0 0 0 0 0 0 0 0 0 1 0 0 0 Page No. *Change No. 3Ć64 . . . . . . . . . . . . . . . . . . . . . 3Ć65 . . . . . . . . . . . . . . . . . . . . . 3Ć66 . . . . . . . . . . . . . . . . . . . . . 3Ć67 . . . . . . . . . . . . . . . . . . . . . 3Ć68 . . . . . . . . . . . . . . . . . . . . . 3Ć69 . . . . . . . . . . . . . . . . . . . . . 3Ć70 . . . . . . . . . . . . . . . . . . . . . 3Ć71 . . . . . . . . . . . . . . . . . . . . . 3Ć72 . . . . . . . . . . . . . . . . . . . . . 3Ć73 . . . . . . . . . . . . . . . . . . . . . 3Ć74 . . . . . . . . . . . . . . . . . . . . . 3Ć75 . . . . . . . . . . . . . . . . . . . . . 3Ć76 . . . . . . . . . . . . . . . . . . . . . 3Ć77 . . . . . . . . . . . . . . . . . . . . . 3Ć78 . . . . . . . . . . . . . . . . . . . . . 3Ć79 . . . . . . . . . . . . . . . . . . . . . 3Ć80 . . . . . . . . . . . . . . . . . . . . . 3Ć81 . . . . . . . . . . . . . . . . . . . . . 3Ć82 . . . . . . . . . . . . . . . . . . . . . 3Ć83 . . . . . . . . . . . . . . . . . . . . . 3Ć84 . . . . . . . . . . . . . . . . . . . . . 3Ć84.1 Added . . . . . . . . . . . . . 3Ć84.2 Blank Added . . . . . . 3Ć85 . . . . . . . . . . . . . . . . . . . . . 3Ć86 . . . . . . . . . . . . . . . . . . . . . 3Ć87 . . . . . . . . . . . . . . . . . . . . . 3Ć88 . . . . . . . . . . . . . . . . . . . . . 3Ć89 . . . . . . . . . . . . . . . . . . . . . 3Ć90 . . . . . . . . . . . . . . . . . . . . . 3Ć91 . . . . . . . . . . . . . . . . . . . . . 3Ć92 . . . . . . . . . . . . . . . . . . . . . 3Ć93 . . . . . . . . . . . . . . . . . . . . . 3Ć94 . . . . . . . . . . . . . . . . . . . . . 3Ć95 . . . . . . . . . . . . . . . . . . . . . 3Ć96 . . . . . . . . . . . . . . . . . . . . . 3Ć97 . . . . . . . . . . . . . . . . . . . . . 3Ć98 . . . . . . . . . . . . . . . . . . . . . 3Ć99 . . . . . . . . . . . . . . . . . . . . . 3Ć100 . . . . . . . . . . . . . . . . . . . . 3Ć101 . . . . . . . . . . . . . . . . . . . . 3Ć102 . . . . . . . . . . . . . . . . . . . . 3Ć103 . . . . . . . . . . . . . . . . . . . . 3Ć104 . . . . . . . . . . . . . . . . . . . . 3Ć105 . . . . . . . . . . . . . . . . . . . . 3Ć106 . . . . . . . . . . . . . . . . . . . . 3Ć107 . . . . . . . . . . . . . . . . . . . . 3Ć108 . . . . . . . . . . . . . . . . . . . . 3Ć109 . . . . . . . . . . . . . . . . . . . . 3Ć110 . . . . . . . . . . . . . . . . . . . . 3Ć111 . . . . . . . . . . . . . . . . . . . . 3Ć112 . . . . . . . . . . . . . . . . . . . . 3Ć113 . . . . . . . . . . . . . . . . . . . . 3Ć114 . . . . . . . . . . . . . . . . . . . . 3Ć115 . . . . . . . . . . . . . . . . . . . . 3Ć116 . . . . . . . . . . . . . . . . . . . . 1 0 1 1 0 0 0 1 0 0 0 0 0 0 0 0 1 1 1 0 1 1 1 1 0 1 0 0 0 0 0 0 0 0 1 1 1 1 0 1 1 1 0 1 1 1 0 0 0 1 1 1 0 0 0 Page No. *Change No. 3Ć117 . . . . . . . . . . . . . . . . . . . . 3Ć118 . . . . . . . . . . . . . . . . . . . . 3Ć119 . . . . . . . . . . . . . . . . . . . . 3Ć120 . . . . . . . . . . . . . . . . . . . . 3Ć121 . . . . . . . . . . . . . . . . . . . . 3Ć122 . . . . . . . . . . . . . . . . . . . . 3Ć122.1 Added . . . . . . . . . . . 3Ć122.2 Blank Added . . . . . 3Ć123 . . . . . . . . . . . . . . . . . . . . 3Ć124 . . . . . . . . . . . . . . . . . . . . 3Ć125 . . . . . . . . . . . . . . . . . . . . 3Ć126 . . . . . . . . . . . . . . . . . . . . 3Ć127 . . . . . . . . . . . . . . . . . . . . 3Ć128 . . . . . . . . . . . . . . . . . . . . 3Ć129 . . . . . . . . . . . . . . . . . . . . 3Ć130 . . . . . . . . . . . . . . . . . . . . 3Ć131 . . . . . . . . . . . . . . . . . . . . 3Ć132 . . . . . . . . . . . . . . . . . . . . 3Ć133 . . . . . . . . . . . . . . . . . . . . 3Ć134 . . . . . . . . . . . . . . . . . . . . 3Ć135 . . . . . . . . . . . . . . . . . . . . 3Ć136 . . . . . . . . . . . . . . . . . . . . 3Ć137 . . . . . . . . . . . . . . . . . . . . 3Ć138 . . . . . . . . . . . . . . . . . . . . 3Ć139 . . . . . . . . . . . . . . . . . . . . 3Ć140 . . . . . . . . . . . . . . . . . . . . 3Ć141 . . . . . . . . . . . . . . . . . . . . 3Ć142 . . . . . . . . . . . . . . . . . . . . 3Ć143 . . . . . . . . . . . . . . . . . . . . 3Ć144 . . . . . . . . . . . . . . . . . . . . 3Ć145 . . . . . . . . . . . . . . . . . . . . 3Ć146 Blank . . . . . . . . . . . . . 4Ć1 . . . . . . . . . . . . . . . . . . . . . . 4Ć2 Blank . . . . . . . . . . . . . . . . 5Ć1 . . . . . . . . . . . . . . . . . . . . . . 5Ć2 . . . . . . . . . . . . . . . . . . . . . . 5Ć3 . . . . . . . . . . . . . . . . . . . . . . 5Ć4 . . . . . . . . . . . . . . . . . . . . . . 5Ć5 . . . . . . . . . . . . . . . . . . . . . . 5Ć6 . . . . . . . . . . . . . . . . . . . . . . 5Ć7 . . . . . . . . . . . . . . . . . . . . . . 5Ć8 . . . . . . . . . . . . . . . . . . . . . . 5Ć9 . . . . . . . . . . . . . . . . . . . . . . 5Ć10 . . . . . . . . . . . . . . . . . . . . . 5Ć11 . . . . . . . . . . . . . . . . . . . . . 5Ć12 . . . . . . . . . . . . . . . . . . . . . 5Ć13 . . . . . . . . . . . . . . . . . . . . . 5Ć14 . . . . . . . . . . . . . . . . . . . . . 5Ć15 . . . . . . . . . . . . . . . . . . . . . 5Ć16 Blank . . . . . . . . . . . . . . . 6Ć1 . . . . . . . . . . . . . . . . . . . . . . 6Ć2 . . . . . . . . . . . . . . . . . . . . . . 6Ć3 . . . . . . . . . . . . . . . . . . . . . . 6Ć4 . . . . . . . . . . . . . . . . . . . . . . 6Ć5 . . . . . . . . . . . . . . . . . . . . . . 0 0 1 0 0 1 1 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 1 0 1 0 0 0 0 0 0 * Zero in this column indicates an original page. Change 1ąąąăC
  6. 6. T.O. GR1FĆ16CJĆ1 INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. LIST OF EFFECTIVE PAGES (Cont) Page No. *Change No. 6Ć6 . . . . . . . . . . . . . . . . . . . . . . 6Ć7 . . . . . . . . . . . . . . . . . . . . . . 6Ć8 . . . . . . . . . . . . . . . . . . . . . . 6Ć9 . . . . . . . . . . . . . . . . . . . . . . 6Ć10 . . . . . . . . . . . . . . . . . . . . . 6Ć11 . . . . . . . . . . . . . . . . . . . . . 6Ć12 . . . . . . . . . . . . . . . . . . . . . 6Ć13 . . . . . . . . . . . . . . . . . . . . . 6Ć14 . . . . . . . . . . . . . . . . . . . . . 6Ć15 . . . . . . . . . . . . . . . . . . . . . 6Ć16 . . . . . . . . . . . . . . . . . . . . . 7Ć1 . . . . . . . . . . . . . . . . . . . . . . 7Ć2 . . . . . . . . . . . . . . . . . . . . . . 7Ć3 . . . . . . . . . . . . . . . . . . . . . . 7Ć4 . . . . . . . . . . . . . . . . . . . . . . 7Ć5 . . . . . . . . . . . . . . . . . . . . . . 7Ć6 . . . . . . . . . . . . . . . . . . . . . . 7Ć7 . . . . . . . . . . . . . . . . . . . . . . 7Ć8 . . . . . . . . . . . . . . . . . . . . . . 8Ć1 Added . . . . . . . . . . . . . . . 8Ć2 Added . . . . . . . . . . . . . . . 8Ć3 Added . . . . . . . . . . . . . . . 8Ć4 Added . . . . . . . . . . . . . . . 8Ć5 Added . . . . . . . . . . . . . . . 8Ć6 Added . . . . . . . . . . . . . . . 8Ć7 Added . . . . . . . . . . . . . . . 8Ć8 Added . . . . . . . . . . . . . . . 8Ć9 Added . . . . . . . . . . . . . . . 8Ć10 Added . . . . . . . . . . . . . . 8Ć11 Added . . . . . . . . . . . . . . 8Ć12 Added . . . . . . . . . . . . . . 8Ć13 Added . . . . . . . . . . . . . . 8Ć14 Added . . . . . . . . . . . . . . 8Ć15 Added . . . . . . . . . . . . . . 8Ć16 Added . . . . . . . . . . . . . . 8Ć17 Added . . . . . . . . . . . . . . 8Ć18 Added . . . . . . . . . . . . . . 8Ć19 Added . . . . . . . . . . . . . . 8Ć20 Added . . . . . . . . . . . . . . 8Ć21 Added . . . . . . . . . . . . . . 8Ć22 Added . . . . . . . . . . . . . . 8Ć23 Added . . . . . . . . . . . . . . 8Ć24 Added . . . . . . . . . . . . . . 8Ć25 Added . . . . . . . . . . . . . . 8Ć26 Added . . . . . . . . . . . . . . 8Ć27 Added . . . . . . . . . . . . . . 8Ć28 Added . . . . . . . . . . . . . . 8Ć29 Added . . . . . . . . . . . . . . 8Ć30 Added . . . . . . . . . . . . . . 8Ć31 Added . . . . . . . . . . . . . . 8Ć32 Added . . . . . . . . . . . . . . 8Ć33 Added . . . . . . . . . . . . . . 8Ć34 Added . . . . . . . . . . . . . . 8Ć35 Added . . . . . . . . . . . . . . 8Ć36 Added . . . . . . . . . . . . . . 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Page No. *Change No. 8Ć37 Added . . . . . . . . . . . . . . 8Ć38 Blank Added . . . . . . . . Glossary 1 . . . . . . . . . . . . . . . Glossary 2 . . . . . . . . . . . . . . . Glossary 3 . . . . . . . . . . . . . . . Glossary 4 . . . . . . . . . . . . . . . Glossary 5 . . . . . . . . . . . . . . . Glossary 6 Blank . . . . . . . . . 1 1 1 1 1 1 0 0 * Zero in this column indicates an original page. DąąąăChange 1 Page No. *Change No.
  7. 7. T.O. GR1FĆ16CJĆ1 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. GR1FĆ16CJĆ1 15 Oct 2002 1 Supplemental Flight Manuals Basic Date Change No. and Date T.O. GR1FĆ16CJĆ1Ć1 9 Jun 1997 7 15 Nov 2002 T.O. GR1FĆ16CJĆ1Ć2 15 Feb 2000 5 15 Mar 2003 Flight Crew Checklist Basic Date Change No. and Date T.O. GR1FĆ16CJĆ1CLĆ1 15 Oct 2002 1 15 Jun 2003 15 Jun 2003 INCORPORATED SAFETY AND OPERATIONAL SUPPLEMENTS Flight Manual Sections Affected T.O. Number Date Short Title GR1FĆ16CJĆ1SSĆ27 27 Nov 02 FLCS Failure That Results In Loss Of Pitch Control III GR1FĆ16CJĆ1SSĆ29 29 Jan 03 Max Range Speeds and FO Pattern Altitudes III GR1FĆ16CJĆ1SĆ31 30 Apr 03 Fuel Transfer Switch, Avionics Fault & ECM Lights, and EGI Align II OUTSTANDING SAFETY AND OPERATIONAL SUPPLEMENTS T.O. Number Date Short Title Flight Manual Sections Affected None Change 1ąąąăa/(b blank)
  8. 8. T.O. GR1FĆ16CJĆ1 TABLE OF CONTENTS SECTION I Description and Operation 1Ć1 SECTION II Normal Procedures 2Ć1 SECTION III Emergency Procedures 3Ć1 SECTION IV Crew Duties 4Ć1 SECTION V Operating Limitations 5Ć1 SECTION V Operating Limitations (Stores) SECTION VI Flight Characteristics 6Ć1 SECTION VII Adverse Weather Operation 7Ć1 SECTION VIII Air Refueling Procedures 8Ć1 GLOSSARY Standard and Nonstandard Abbreviations APPENDIX A Performance DataĂ-ĂF100ĆPWĆ229 T.O. GR1FĆ16CJĆ1Ć1 APPENDIX B Performance DataĂ-ĂF110ĆGEĆ129 T.O. GR1FĆ16CJĆ1Ć1 APPENDIX C Performance DataĂ-ĂF100ĆPWĆ229/CFT T.O. GR1FĆ16CJĆ1Ć1 T.O. GR1FĆ16CJĆ1Ć2 Glossary 1 Change 1ąąąăi
  9. 9. T.O. GR1FĆ16CJĆ1 BEFORE YOU TAKE OFF, READ THIS! 1F-16X-1-0002X T.O. GR1FĆ16CJĆ6CFĆ1 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 experiĆ 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 instrucĆ tions under most conditions. Multiple emergencies, adverse weather, terrain, etc., may require modificaĆ 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 operaĆ tion: T.O. GR1FĆ16CJĆ1Ć1 Supplemental Flight Manual, FĆ16C/D AirĆ craft T.O. GR1FĆ16CJĆ1Ć2 Supplemental Flight Manual, FĆ16C/D AirĆ craft T.O. GR1FĆ16CJĆ5Ć2 Loading Data iiąąąăChange 1 Acceptance and FuncĆ tional Check Flight Procedures Manual, FĆ16C/D Aircraft T.O. GR1FĆ16CJĆ34Ć1Ć1 Avionics and NonnuĆ clear Weapons DelivĆ ery Flight Manual T.O. GR1FĆ16CJĆ34Ć1Ć2 Nonnuclear Weapons Ballistics T.O. 1Ć1CĆ1 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.
  10. 10. T.O. GR1FĆ16CJĆ1 HOW TO BE ASSURED OF HAVING LATEST DATA SAFETY SUPPLEMENTS Refer to T.O. GR0Ć1Ć71 for a listing of all current flight manuals, safety supplements, operational suppleĆ 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. Information involving safety is promptly forwarded in a safety supplement. Urgent information is published in interim safety supplements and transmitted by electronic message. Formal suppleĆ 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. 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 modificaĆ tions. For details of equipment modification, see the individual equipment illustration. SUPPLEMENT INFORMATION AND GUIDELINES Supplements are safety or operational and are indicated Ć1SS or Ć1S, respectively. Supplements are issued as interim electronic messages or formal printed copies. All interim supplements are assigned odd numbers, such as Ć1SSĆ195. When an interim supplement is formalized, it is assigned the next following even number, such as Ć1SSĆ196. 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 oneĆsided 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., 3Ć48.1) are inserted in proper numerical sequence and may be printed on both sides. OPERATIONAL SUPPLEMENTS Information involving changes to operating proceĆ 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 suppleĆ ments, and a checklist. The required quantities should be ordered before needed to assure their timely receipt. Check with the publication distribuĆ 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. GR0Ć1Ć71. 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 availĆ 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. Change 1ąąąăiii
  11. 11. T.O. GR1FĆ16CJĆ1 WARNINGS, CAUTIONS, AND NOTES The following definitions apply to Warnings, Cautions, and Notes found throughout the manual: 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 11Ć215 through command headquarters to OOĆALC/ YPVT, 6080 Gum Lane, Hill AFB, UT 84056Ć5825. PUBLICATION DATE 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. 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 codeĂ-ĂFĆ16C and FĆ16D aircraft NOTE C FĆ16C aircraft An operating procedure, technique, etc., which is considered essential to emphasize. D FĆ16D aircraft DF FĆ16D aircraft, forward cockpit DR FĆ16D aircraft, rear cockpit PX II Peace Xenia II aircraft PX III Peace Xenia III aircraft 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. 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 codeĂ-ĂEither engine PW 229 F100ĆPWĆ229 GE 129 F110ĆGEĆ129 AIRSPEED REFERENCES All references to airspeed quoted in knots refer to indicated airspeed. PILOT'S RESPONSIBILITYĂ-ĂTO LET US KNOW Every effort is made to keep the flight manual current. Review conferences with operating personĆ 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 ivąąąă BLOCK DESIGNATION CODES/SERIAL NUMBER/ TAIL NUMBER CROSSĆREFERENCE 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 illustraĆ tions.
  12. 12. T.O. GR1FĆ16CJĆ1 AIRCRAFT MODIFICATION/RETROFIT INFORMAĆ TION This list includes the applicable T.O./ECP effectiviĆ ties. It is not an official status page. Refer to T.O. 0Ć1Ć4 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 TV CODE/ T.O. NO. b1q 1FĆ16Ć2121 SHORT TITLE Flight Control ComĆ puter Software UpĆ date (ECP 2269) 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. EFFECTIVITY PRODUCTION RETROFIT FĆ16C 93Ć1055, and on FĆ16C 93Ć1045 thru 93Ć1054 FĆ16D NA FĆ16D All Summary: D D b2p Retrofit authorized Modification incorporates FLCS improvements, including improved reset capability for FLCC powĆ er up failures and elimination of lateral accelerometer failures during gun firing. 1FĆ16Ć2170 Modification of the Ejection Mode SelecĆ tor Valve Console (ECP 2362) FĆ16C NA FĆ16C NA FĆ16D 99Ć1534, and on FĆ16D 93Ć1077 thru 93Ć1084 FĆ16C 99Ć1500, and on FĆ16C 93Ć1045 thru 93Ć1076 FĆ16D 99Ć1534, and on FĆ16D 93Ć1077 thru 93Ć1084 Summary: D Retrofit authorized D Modification enlarges the hole in the console to allow the EJECTION MODE SEL handle to seat properly in the NORM position. b2t XX1FĆ16Ć2077 Summary: D D b6n NA Installation of Improved Antiskid Braking System (OCP H086) (ECP 2478) Retrofit authorized Modification incorporates an improved Brake Control/AntiĆskid Assembly to replace the current Brake Control and Antiskid Control Boxes. Flight Control ComĆ puter Software UpĆ date for CFT (ECP 2495) FĆ16C 99Ć1500, and on NA FĆ16D 99Ć1534, Summary: and on D Retrofit NA D Modification incorporates flight control system software updates to provide increased roll rate capaĆ bility in CAT III with CFT's and eliminate an existing prohibited maneuver. Change 1ąąąăv
  13. 13. T.O. GR1FĆ16CJĆ1 TV CODE/ T.O. NO. b7n TBD SHORT TITLE AVIONICS FAULT caution/ECM lights CDEEU mod (ECP 2526) EFFECTIVITY PRODUCTION RETROFIT FĆ16C 99Ć1507, and on TBD FĆ16D 99Ć1541, Summary: and on D Retrofit TBD D Modification to circuitry in the CDEEU which will allow the AVIONICS FAULT caution and ECM lights to illuminate in both cockpits of PX III D aircraft. viąąąăChange 1
  14. 14. T.O. GR1FĆ16CJĆ1 Block Designation Codes/Serial Number/Tail Number CrossĆReference BLOCK 50 Serial Numbers/ Tail Numbers C PX II 93Ć1045/045 93Ć1046/046 93Ć1047/047 93Ć1048/048 93Ć1049/049 93Ć1050/050 93Ć1051/051 93Ć1052/052 93Ć1053/053 93Ć1054/054 93Ć1055/055 93Ć1056/056 93Ć1057/057 93Ć1058/058 93Ć1059/059 93Ć1060/060 93Ć1061/061 93Ć1062/062 93Ć1063/063 93Ć1064/064 93Ć1065/065 93Ć1066/066 93Ć1067/067 93Ć1068/068 93Ć1069/069 93Ć1070/070 93Ć1071/071 93Ć1072/072 93Ć1073/073 93Ć1074/074 93Ć1075/075 93Ć1076/076 D PX II 93Ć1077/077 93Ć1078/078 93Ć1079/079 93Ć1080/080 93Ć1081/081 93Ć1082/082 93Ć1083/083 93Ć1084/084 BLOCK 52+ Serial Numbers/ Tail Numbers C PX III 99Ć1500/500 99Ć1501/501 99Ć1502/502 99Ć1503/503 99Ć1504/504 99Ć1505/505 99Ć1506/506 99Ć1507/507 99Ć1508/508 99Ć1509/509 99Ć1510/510 99Ć1511/511 99Ć1512/512 99Ć1513/513 99Ć1514/514 99Ć1515/515 99Ć1516/516 99Ć1517/517 99Ć1518/518 99Ć1519/519 99Ć1520/520 99Ć1521/521 99Ć1522/522 99Ć1523/523 99Ć1524/524 99Ć1525/525 99Ć1526/526 99Ć1527/527 99Ć1528/528 99Ć1529/529 99Ć1530/530 99Ć1531/531 99Ć1532/532 99Ć1533/533 01Ć8530/534 01Ć8531/535 01Ć8532/536 01Ć8533/537 01Ć8534/538 01Ć8535/539 D PX III 99Ć1534/600 99Ć1535/601 99Ć1536/602 99Ć1537/603 99Ć1538/604 99Ć1539/605 99Ć1540/606 99Ć1541/607 99Ć1542/608 99Ć1543/609 99Ć1544/610 99Ć1545/611 99Ć1546/612 99Ć1547/613 99Ć1548/614 99Ć1549/615 01Ć8536/616 01Ć8537/617 01Ć8538/618 01Ć8539/619 Change 1ąąąăvii
  15. 15. T.O. GR1FĆ16CJĆ1 C D GR1F-16CJ-1-0003A37 viiiąąąăChange 1
  16. 16. T.O. GR1FĆ16CJĆ1 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 . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine General Description PW 229 . . . . . . Engine Fuel System PW 229 . . . . . . . . . . . . . Engine Control System PW 229 . . . . . . . . . . . Main Fuel Control (MFC) PW 229 . . . . . . Afterburner (AB) Fuel Control PW 229 . . . . . . . . . . . . . . . . . . . . Digital Electronic Engine Control (DEEC) PW 229 . . . . . . . . . . . . . . . . . . . . Secondary Engine Control (SEC) PW 229 . . . . . . . . . . . . . . . . . . . . . . Main Fuel Pump PW 229 . . . . . . . . . . . . . . Afterburner (AB) Fuel Pump PW 229 . . . . . . . . . . . . . . . . . . . . . . Compressor Inlet Variable Vane (CIVV) Control PW 229 . . . . . . . . . . . . . Rear Compressor Variable Vanes (RCVV's) PW 229 . . . . . . . . . . . . . . . . . . . Compressor Bleed Air PW 229 . . . . . . . . . Pressurization and Dump Valve PW 229 . . . . . . . . . . . . . . . . . . . . . . Exhaust Nozzle PW 229 . . . . . . . . . . . . . . . . . . Convergent Exhaust Nozzle Control (CENC) PW 229 . . . . . . . . . . . . . . . . . . . . LightĆOff Detector (LOD) PW 229 . . . . . . Engine Diagnostic Unit (EDU) PW 229 . . . . Engine Oil System PW 229 . . . . . . . . . . . . . . . FUEL/OIL HOT Caution Light PW 229 . . . . . . . . . . . . . . . . . . . . . . Engine AntiĆIce System PW 229 . . . . . . . . . . Engine ANTI ICE Switch PW 229 . . . . . . INLET ICING Caution Light PW 229 . . . . . . . . . . . . . . . . . . . . . . Engine and Accessory Drive Gearboxes PW 229 . . . . . . . . . . . . . . . . . . . . Engine Alternator PW 229 . . . . . . . . . . . . . . . Engine Ignition System PW 229 . . . . . . . . . . 1Ć6 1Ć7 1Ć7 1Ć7 1Ć7 1Ć31 1Ć31 1Ć31 1Ć31 1Ć31 1Ć31 1Ć33 1Ć33 1Ć33 1Ć33 1Ć33 1Ć33 1Ć34 1Ć34 1Ć34 1Ć34 1Ć34 1Ć34 1Ć34 1Ć34 1Ć35 1Ć35 1Ć35 1Ć35 1Ć35 1Ć35 Jet Fuel Starter (JFS) PW 229 . . . . . . . . . . . . ENG & JET START Control Panel PW 229 . . . . . . . . . . . . . . . . . . . . . . . . JFS Switch C DF PW 229 . . . . . . . . . . . . . JFS RUN Light C DF PW 229 . . . . . . . . . JFS Operation PW 229 . . . . . . . . . . . . . . . . Engine Controls and Indicators PW 229 . . . . . . . . . . . . . . . . . . . . ENG CONT Switch PW 229 . . . . . . . . . . . . AB RESET Switch C DF PW 229 . . . . . . ENGINE FAULT Caution Light PW 229 . . . . . . . . . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) PW 229 . . . . . . . . . . . . . . . . . . . . SEC Caution Light PW 229 . . . . . . . . . . . . EEC Caution Light PW 229 . . . . . . . . . . . . BUC Caution Light PW 229 . . . . . . . . . . . . MAX POWER Switch C DF PW 229 . . . . RPM Indicator PW 229 . . . . . . . . . . . . . . . . NOZ POS Indicator PW 229 . . . . . . . . . . . . FTIT Indicator PW 229 . . . . . . . . . . . . . . . . FUEL FLOW Indicator PW 229 . . . . . . . . OIL Pressure Indicator PW 229 . . . . . . . . HYD/OIL PRESS Warning Light PW 229 . . . . . . . . . . . . . . . . . . . . . . ENGINE Warning Light PW 229 . . . . . . . Throttle PW 229 . . . . . . . . . . . . . . . . . . . . . . Engine Operating Characteristics PW 229 . . . . . . . . . . . . . . . . Engine General PW 229 . . . . . . . . . . . . . . . Ground Operations PW 229 . . . . . . . . . . . . NonĆAB Operation in Flight PW 229 . . . . . . . . . . . . . . . . . . . . . . AB Operation in Flight PW 229 . . . . . . . . SEC Operation PW 229 . . . . . . . . . . . . . . . . Engine GE 129 . . . . . . . . . . . . . . . . . . . . . . . . . . . . General Description GE 129 . . . . . . . . . . . . . Engine Fuel/Control System GE 129 . . . . . . Digital Electronic Control (DEC) GE 129 . . . . . . . . . . . . . . . . . . . . . Afterburner Fuel Control (AFC) GE 129 . . . . . . . . . . . . . . . . . . . . . . Main Engine Control (MEC) GE 129 . . . Primary (PRI) Engine Operation GE 129 . . . . . . . . . . . . . . . . . . 1Ć36 1Ć36 1Ć36 1Ć36 1Ć37 1Ć37 1Ć37 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć39 1Ć40 1Ć40 1Ć40 1Ć40 1Ć40 1Ć40 1Ć42 1Ć42 1Ć44 1Ć44 1Ć44 1Ć44 1Ć44 1Ć44 1Ć44 ąąąă1Ć1
  17. 17. T.O. GR1FĆ16CJĆ1 Hybrid (HYB) Engine Operation GE 129 . . . . . . . . . . . . . . . . . . Secondary Engine Control (SEC) Operation GE 129 . . . . . . . . . . . . . . . . . . Engine Fuel Boost Pump GE 129 . . . . . . . Main Fuel Pump GE 129 . . . . . . . . . . . . . . Afterburner (AB) Fuel Pump GE 129 . . . . . . . . . . . . . . . . . . . . . . Inlet Guide Vanes (IGV's) GE 129 . . . . . . Variable Stator Vanes (VSV's) GE 129 . . . . . . . . . . . . . . . . . . . . . Compressor Bleed Air GE 129 . . . . . . . . . Exhaust Nozzle GE 129 . . . . . . . . . . . . . . . . . . AB Flame Detector GE 129 . . . . . . . . . . . . . . Engine Monitoring System (EMS) GE 129 . . . . . . . . . . . . . . . . . . . . . . . . Engine Oil System GE 129 . . . . . . . . . . . . . . . FUEL/OIL HOT Caution Light GE 129 . . . . . . . . . . . . . . . . . . . . . . Engine AntiĆIce System GE 129 . . . . . . . . . . Engine ANTI ICE Switch GE 129 . . . . . . INLET ICING Caution Light GE 129 . . . . . . . . . . . . . . . . . . . . . . Engine and Accessory Drive Gearboxes GE 129 . . . . . . . . . . . . . . . . . . . . Engine Alternator GE 129 . . . . . . . . . . . . . . . Engine Ignition System GE 129 . . . . . . . . . . Jet Fuel Starter (JFS) GE 129 . . . . . . . . . . . . ENG & JET START Control Panel GE 129 . . . . . . . . . . . . . . . . . . . . . . . . JFS Switch C DF GE 129 . . . . . . . . . . . . . JFS RUN Light C DF GE 129 . . . . . . . . . JFS Operation GE 129 . . . . . . . . . . . . . . . . Engine Controls and Indicators GE 129 . . . . . . . . . . . . . . . . . . . . ENG CONT Switch GE 129 . . . . . . . . . . . . SEC Caution Light GE 129 . . . . . . . . . . . . EEC Caution Light GE 129 . . . . . . . . . . . . BUC Caution Light GE 129 . . . . . . . . . . . . MAX POWER Switch C DF GE 129 . . . . AB RESET Switch C DF GE 129 . . . . . . ENGINE FAULT Caution Light GE 129 . . . . . . . . . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) GE 129 . . . . . . . . . . . . . . . . . . . . RPM Indicator GE 129 . . . . . . . . . . . . . . . NOZ POS Indicator GE 129 . . . . . . . . . . . . FTIT Indicator GE 129 . . . . . . . . . . . . . . . . FUEL FLOW Indicator GE 129 . . . . . . . . OIL Pressure Indicator GE 129 . . . . . . . . 1Ć2ąąąă 1Ć46 1Ć47 1Ć47 1Ć47 1Ć47 1Ć47 1Ć47 1Ć47 1Ć47 1Ć48 1Ć48 1Ć48 1Ć48 1Ć48 1Ć49 1Ć49 1Ć49 1Ć49 1Ć49 1Ć50 1Ć50 1Ć50 1Ć51 1Ć51 1Ć51 1Ć51 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 1Ć53 HYD/OIL PRESS Warning Light GE 129 . . . . . . . . . . . . . . . . . . . . . . ENGINE Warning Light GE 129 . . . . . . . Throttle GE 129 . . . . . . . . . . . . . . . . . . . . . . Engine Operating Characteristics GE 129 . . . . . . . . . . . . . . . Ground Operations GE 129 . . . . . . . . . . . . NonĆAB Operation in Flight GE 129 . . . . AB Operation GE 129 . . . . . . . . . . . . . . . . . Inlet Thump GE 129 . . . . . . . . . . . . . . . . . . SEC Operation GE 129 . . . . . . . . . . . . . . . . Fire and Overheat Detection System . . . . . . . . FIRE & OHEAT DETECT Test Button C DF . . . . . . . . . . . . . . . . . . . . . . . . Fuel System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Tank System . . . . . . . . . . . . . . . . . . . . . . . Fuel Transfer System . . . . . . . . . . . . . . . . . . . . Fuel Tank Vent and Pressurization System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Fuel Supply System . . . . . . . . . . . . . . Fuel Quantity Indicating System . . . . . . . . . Reservoir Fuel Level Sensing System . . . . . Fuel Low Caution Lights . . . . . . . . . . . . . . HUD FUEL Low/Bingo Indication . . . . . . . . HUD TRP FUEL Warning . . . . . . . . . . . . . . . FUEL/OIL HOT Caution Light . . . . . . . . . . Fuel Tank Explosion Suppression System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Refueling System . . . . . . . . . . . . . . . . . . . . . . . Ground Refueling . . . . . . . . . . . . . . . . . . . . . Air Refueling (AR) System . . . . . . . . . . . . . NWS A/R DISC MSL STEP Button . . . . . . . . . . . . . . . . . . . . . . . . . . Air Refueling (AR) Status Indicator . . . . . . . . . . . . . . . . . . . . . . . . Environmental Control System (ECS) . . . . . . . Electrical Failures . . . . . . . . . . . . . . . . . . . . . . AirĆConditioning . . . . . . . . . . . . . . . . . . . . . . . . Pressurization . . . . . . . . . . . . . . . . . . . . . . . . . . AIR SOURCE Knob C DF . . . . . . . . . . . . . TEMP Knob C DF . . . . . . . . . . . . . . . . . . . . DEFOG Lever C DF . . . . . . . . . . . . . . . . . . EQUIP HOT Caution Light . . . . . . . . . . . . Cockpit Pressure Altimeter C DF . . . . . . CABIN PRESS Caution Light . . . . . . . . . . AntiĆG System . . . . . . . . . . . . . . . . . . . . . . . . . . Electrical System . . . . . . . . . . . . . . . . . . . . . . . . . . Main AC Power System . . . . . . . . . . . . . . . . . . Overcurrent Sensing Contactors . . . . . . . 1Ć53 1Ć54 1Ć54 1Ć54 1Ć54 1Ć54 1Ć56 1Ć56 1Ć56 1Ć58 1Ć58 1Ć58 1Ć58 1Ć58 1Ć61 1Ć61 1Ć74 1Ć74 1Ć74 1Ć74 1Ć74 1Ć77 1Ć77 1Ć77 1Ć77 1Ć77 1Ć78 1Ć78 1Ć78 1Ć78 1Ć80 1Ć80 1Ć81 1Ć81 1Ć81 1Ć82 1Ć82 1Ć82 1Ć82 1Ć82 1Ć82 1Ć83
  18. 18. T.O. GR1FĆ16CJĆ1 Standby AC Power System . . . . . . . . . . . . . . . 1Ć83 Emergency AC Power System . . . . . . . . . . . . 1Ć83 DC Power System . . . . . . . . . . . . . . . . . . . . . . . 1Ć83 FLCS Power Supply . . . . . . . . . . . . . . . . . . . . . 1Ć83 External Power Provisions . . . . . . . . . . . . . . . 1Ć86 Electrical System Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć86 Electrical Power Distribution . . . . . . . . . . . . 1Ć86 Electrical System Normal Operation . . . . . . 1Ć86 Hydraulic System . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć98 HYD PRESS Indicators and Warning Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć98 HYD PRESS Indicators . . . . . . . . . . . . . . . 1Ć98 HYD/OIL PRESS Warning Light . . . . . . . 1Ć98 Emergency Power Unit (EPU) . . . . . . . . . . . . . . 1Ć98 EPU Controls and Indicators . . . . . . . . . . . . . 1Ć99 EPU Ground Safety Switch . . . . . . . . . . . . 1Ć99 EPU Switch . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć99 EPU Run Light . . . . . . . . . . . . . . . . . . . . . . . 1Ć99 HYDRAZN Light . . . . . . . . . . . . . . . . . . . . . 1Ć99 AIR Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć99 EPU/GEN Test Switch . . . . . . . . . . . . . . . . 1Ć99 EPU FUEL Quantity Indicator C DF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć99 Hydrazine Leak Detector . . . . . . . . . . . . . . 1Ć99 EPU Fired Indicator . . . . . . . . . . . . . . . . . 1Ć102 EPU Operation . . . . . . . . . . . . . . . . . . . . . . . . 1Ć102 Landing Gear (LG) System . . . . . . . . . . . . . . . . 1Ć104 Main Landing Gear (MLG) . . . . . . . . . . . . . . 1Ć104 Nose Landing Gear (NLG) . . . . . . . . . . . . . . 1Ć104 Landing Gear Controls and Indicators . . . 1Ć104 Landing Gear Handle . . . . . . . . . . . . . . . . 1Ć104 Landing Gear Handle Down Permission Button . . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć104 DN LOCK REL Button . . . . . . . . . . . . . . . 1Ć104 ALT GEAR Handle . . . . . . . . . . . . . . . . . . 1Ć106 LG Warning Horn . . . . . . . . . . . . . . . . . . . 1Ć106 HORN SILENCER Button . . . . . . . . . . . . 1Ć106 TO/LDG CONFIG Warning Light . . . . . 1Ć106 WHEELS Down Lights . . . . . . . . . . . . . . . 1Ć106 Landing Gear WeightĆonĆWheels (WOW) Switches . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć106 Landing Gear Operation . . . . . . . . . . . . . . . . 1Ć106 Nosewheel Steering (NWS) System . . . . . . . . . 1Ć110 NWS Controls and Indicators . . . . . . . . . . . 1Ć110 NWS A/R DISC MSL STEP Button . . . . 1Ć110 NWS Light . . . . . . . . . . . . . . . . . . . . . . . . . . 1Ć110 NWS FAIL Caution Light . . . . . . . . . . . . 1Ć110 Nosewheel Steering (NWS) System D . . . . 1Ć110 Wheel Brake System . . . . . . . . . . . . . . . . . . . . . . Toe Brake System . . . . . . . . . . . . . . . . . . . . . . Spin Down Braking System . . . . . . . . . . . . . Brakes Channel Switch C DF . . . . . . . . . . . Parking Brake C DF . . . . . . . . . . . . . . . . . . . Antiskid System . . . . . . . . . . . . . . . . . . . . . . . ANTIĆSKID Switch C DF . . . . . . . . . . . . ANTI SKID Caution Light . . . . . . . . . . . . Speedbrake System . . . . . . . . . . . . . . . . . . . . . . . SPD BRK Switch . . . . . . . . . . . . . . . . . . . . SPEED BRAKE Position Indicator . . . . Drag Chute System . . . . . . . . . . . . . . . . . . . . . . . DRAG CHUTE Switch . . . . . . . . . . . . . . . Arrestment System . . . . . . . . . . . . . . . . . . . . . . . HOOK Switch . . . . . . . . . . . . . . . . . . . . . . . HOOK Caution Light . . . . . . . . . . . . . . . . Wing Flap System . . . . . . . . . . . . . . . . . . . . . . . . Leading Edge Flaps (LEF's) . . . . . . . . . . . . . LE FLAPS Switch . . . . . . . . . . . . . . . . . . . FLCS LEF LOCK PFL . . . . . . . . . . . . . . . Trailing Edge Flaps (TEF's) (Flaperons) . . . . . . . . . . . . . . . . . . . . . . . . . . ALT FLAPS Switch . . . . . . . . . . . . . . . . . . Flight Control System (FLCS) . . . . . . . . . . . . . Digital Backup (DBU) . . . . . . . . . . . . . . . . FLCS Limiters . . . . . . . . . . . . . . . . . . . . . . . . . AOA/G Limiter . . . . . . . . . . . . . . . . . . . . . . Roll Rate Limiter . . . . . . . . . . . . . . . . . . . . Rudder Authority Limiter . . . . . . . . . . . . Yaw Rate Limiter . . . . . . . . . . . . . . . . . . . . FLCS Gains . . . . . . . . . . . . . . . . . . . . . . . . . . . Cruise Gains . . . . . . . . . . . . . . . . . . . . . . . . Takeoff and Landing Gains . . . . . . . . . . . Standby Gains . . . . . . . . . . . . . . . . . . . . . . FLCS Data Recorder C DF . . . . . . . . . . . . . AngleĆofĆSideslip (AOS) Feedback Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . Gun Compensation . . . . . . . . . . . . . . . . . . . . . Flight Control System (FLCS) Controls . . . . . . . . . . . . . . . . . . . . . . . . . . . . Stick . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rudder Pedals . . . . . . . . . . . . . . . . . . . . . . . MANUAL TRIM Panel . . . . . . . . . . . . . . . MANUAL PITCH Override (MPO) Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . STORES CONFIG Switch C DF . . . . . . Low Speed Warning Tone . . . . . . . . . . . . . FLT CONTROL Panel (FLCP) C DF . . 1Ć110 1Ć110 1Ć111 1Ć111 1Ć111 1Ć116 1Ć117 1Ć117 1Ć117 1Ć117 1Ć117 1Ć117 1Ć118 1Ć118 1Ć118 1Ć118 1Ć118 1Ć118 1Ć118 1Ć118 1Ć120 1Ć120 1Ć120 1Ć120 1Ć121 1Ć121 1Ć121 1Ć121 1Ć121 1Ć121 1Ć127 1Ć127 1Ć127 1Ć127 1Ć127 1Ć127 1Ć127 1Ć127 1Ć130 1Ć130 1Ć130 1Ć130 1Ć130 1Ć130 ąąąă1Ć3
  19. 19. T.O. GR1FĆ16CJĆ1 FLCS Warning, Caution, and Indicator Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . FLCS Warning Light . . . . . . . . . . . . . . . . . DBU ON Warning Light . . . . . . . . . . . . . . TO/LDG CONFIG Warning Light . . . . . FLCS FAULT Caution Light . . . . . . . . . . BuiltĆIn Test (BIT) . . . . . . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) . . . . . . . Trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Autopilot Operation . . . . . . . . . . . . . . . . . . . . ADV MODE Switch . . . . . . . . . . . . . . . . . . Stick Steering . . . . . . . . . . . . . . . . . . . . . . . . . AOA System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AOA Indicator . . . . . . . . . . . . . . . . . . . . . . . AOA Indexer . . . . . . . . . . . . . . . . . . . . . . . . HUD AOA Display . . . . . . . . . . . . . . . . . . . Air Data System . . . . . . . . . . . . . . . . . . . . . . . . . . Air Data Probes . . . . . . . . . . . . . . . . . . . . . AOA Transmitters . . . . . . . . . . . . . . . . . . . Total Temperature Probe . . . . . . . . . . . . . Static Pressure Ports . . . . . . . . . . . . . . . . . Probe Heat Monitor . . . . . . . . . . . . . . . . . . PROBE HEAT Switch . . . . . . . . . . . . . . . . Pneumatic Sensor Assembly (PSA) . . . . . . Central Air Data Computer (CADC) . . . . . CADC Caution Light . . . . . . . . . . . . . . . . . Warning, Caution, and Indicator Lights . . . . Voice Message System (VMS) . . . . . . . . . . . VOICE MESSAGE Switch C DF . . . . . MASTER CAUTION Light . . . . . . . . . . . . . . Pilot Fault List Display (PFLD) . . . . . . . . . Caution Light Panel . . . . . . . . . . . . . . . . . . . . MAL & IND LTS Test Button . . . . . . . . . Lighting System . . . . . . . . . . . . . . . . . . . . . . . . . . Exterior Lighting . . . . . . . . . . . . . . . . . . . . . . Anticollision Strobe Light . . . . . . . . . . . . Position/Formation Lights . . . . . . . . . . . . Air Refueling Lights . . . . . . . . . . . . . . . . . Vertical TailĆMounted Floodlight . . . . . . Landing and Taxi Lights . . . . . . . . . . . . . Interior Lighting . . . . . . . . . . . . . . . . . . . . . . . PRIMARY CONSOLES Knob . . . . . . . . . PRIMARY INST PNL Knob . . . . . . . . . . . DATA ENTRY DISPLAY Knob . . . . . . . . MAL & IND LTS Switch . . . . . . . . . . . . . . FLOOD INST PNL Knob . . . . . . . . . . . . . FLOOD CONSOLES Knob . . . . . . . . . . . 1Ć4ąąąă 1Ć130 1Ć130 1Ć132 1Ć132 1Ć132 1Ć135 1Ć135 1Ć135 1Ć135 1Ć136 1Ć136 1Ć136 1Ć137 1Ć137 1Ć138 1Ć138 1Ć138 1Ć138 1Ć138 1Ć138 1Ć138 1Ć138 1Ć140 1Ć140 1Ć140 1Ć140 1Ć140 1Ć145 1Ć146 1Ć146 1Ć146 1Ć147 1Ć147 1Ć148 1Ć148 1Ć148 1Ć148 1Ć148 1Ć154 1Ć154 1Ć154 1Ć155 1Ć155 1Ć155 1Ć155 1Ć155 1Ć155 NVIS Switch PX III . . . . . . . . . . . . . . . . . . HandsĆOn Blackout (HOBO) Switch PX III . . . . . . . . . . . . . . . . . . . . . . Utility Light . . . . . . . . . . . . . . . . . . . . . . . . Cockpit Spotlights . . . . . . . . . . . . . . . . . . . Escape System . . . . . . . . . . . . . . . . . . . . . . . . . . . Canopy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Canopy Controls and Indicators . . . . . . . . . MANUAL CANOPY CONTROL Handcrank . . . . . . . . . . . . . . . . . . . . . . . Canopy Handle C DF . . . . . . . . . . . . . . . . Canopy Jettison . . . . . . . . . . . . . . . . . . . . . . . . Ejection Seat . . . . . . . . . . . . . . . . . . . . . . . . . . Ejection Handle . . . . . . . . . . . . . . . . . . . . . SHOULDER HARNESS Knob . . . . . . . . EMERGENCY MANUAL CHUTE Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . Ejection Safety Lever . . . . . . . . . . . . . . . . SEAT NOT ARMED Caution Light . . . . SEAT ADJ Switch . . . . . . . . . . . . . . . . . . . Shoulder Harness Straps/Parachute Risers . . . . . . . . . . . . . . . . . . . . . . . . . . . . Inertia Reel Straps . . . . . . . . . . . . . . . . . . Lapbelt . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Survival Kit . . . . . . . . . . . . . . . . . . . . . . . . . RADIO BEACON Switch . . . . . . . . . . . . . Emergency Oxygen . . . . . . . . . . . . . . . . . . Ejection Seat Operation . . . . . . . . . . . . . . . . Ejection Mode Envelopes . . . . . . . . . . . . . . . Ejection Sequence Times . . . . . . . . . . . . . . . . Canopy Jettison/Seat Ejection . . . . . . . . . . . Ejection Seat Performance . . . . . . . . . . . . . . Oxygen System PX III . . . . . . . . . . . . . . . . . . . . . Onboard Oxygen Generating System (OBOGS) . . . . . . . . . . . . . . . . . . . . OBOGS Backup Oxygen Supply (BOS) . . . . . . . . . . . . . . . . . . . . . . . . OBOGS Monitor . . . . . . . . . . . . . . . . . . . . . . . Emergency Oxygen Supply (EOS) . . . . . . . OBOGS BuiltĆInĆTests (BIT's) . . . . . . . . . . . OBOGS PowerĆUp BIT . . . . . . . . . . . . . . . . . OBOGS Periodic BIT . . . . . . . . . . . . . . . . . . . OBOGS Manual BIT . . . . . . . . . . . . . . . . . . . OBOGS Pneumatic BIT . . . . . . . . . . . . . . . . . Pressure Breathing for G (PBG) . . . . . . . . . Oxygen System Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . . . . Oxygen System Schematic . . . . . . . . . . . . . . 1Ć155 1Ć157 1Ć157 1Ć157 1Ć157 1Ć157 1Ć157 1Ć157 1Ć157 1Ć161 1Ć161 1Ć161 1Ć161 1Ć161 1Ć161 1Ć161 1Ć161 1Ć161 1Ć161 1Ć161 1Ć164 1Ć164 1Ć164 1Ć164 1Ć164 1Ć164 1Ć164 1Ć164 1Ć173 1Ć173 1Ć173 1Ć173 1Ć173 1Ć173 1Ć173 1Ć173 1Ć173 1Ć174 1Ć174 1Ć174 1Ć174
  20. 20. T.O. GR1FĆ16CJĆ1 Oxygen System PX II . . . . . . . . . . . . . . . . . . . . . Liquid Oxygen System . . . . . . . . . . . . . . . . . . Pressure Breathing for G (PBG) . . . . . . Oxygen System Controls and Indicators . . . . . . . . . . . . . . . . . . . . . . . . Oxygen Duration . . . . . . . . . . . . . . . . . . . . Emergency Oxygen System . . . . . . . . . . . . . Oxygen System Schematic . . . . . . . . . . . . . . Communications, Navigation, and IFF (CNI) Equipment . . . . . . . . . . . . . . . . . . . . . . Upfront Controls . . . . . . . . . . . . . . . . . . . . . . . DED/CNI Readouts . . . . . . . . . . . . . . . . . . . . CNI Readout/DED Page Summary . . . . IFF Control Panel C DF PX III . . . . . . . . . . C & I (Communications and IFF) Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IFF MASTER Knob . . . . . . . . . . . . . . . . . . IFF MĆ4 CODE Switch . . . . . . . . . . . . . . . IFF MODE 4 REPLY Switch . . . . . . . . . . IFF MODE 4 MONITOR Switch . . . . . . IFF ENABLE Switch . . . . . . . . . . . . . . . . . IFF MODE 1/MODE 3 Selector Levers . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUX COMM Panel C DF PX II . . . . . . . . . . CNI (Communications, Navigation, and IFF) Knob . . . . . . . . . . . . . . . . . . . . IFF MASTER Knob . . . . . . . . . . . . . . . . . . MĆ4 CODE Switch . . . . . . . . . . . . . . . . . . . IFF MODE 4 REPLY Switch . . . . . . . . . . IFF MODE 4 MONITOR Switch . . . . . . TACAN Function Switch . . . . . . . . . . . . . TACAN CHANNEL Selector Levers . . . AUDIO 1 Control Panel . . . . . . . . . . . . . . . . . COMM 1 (UHF) Power Knob . . . . . . . . . COMM 1 (UHF) Mode Knob . . . . . . . . . . COMM 2 (VHF) Power Knob . . . . . . . . . . COMM 2 (VHF) Mode Knob . . . . . . . . . . SECURE VOICE Knob . . . . . . . . . . . . . . . MSL Tone Knob . . . . . . . . . . . . . . . . . . . . . TF Tone Knob . . . . . . . . . . . . . . . . . . . . . . . THREAT Tone Knob . . . . . . . . . . . . . . . . . AUDIO 2 Control Panel . . . . . . . . . . . . . . . . . ILS Power Knob . . . . . . . . . . . . . . . . . . . . . TACAN Power Knob . . . . . . . . . . . . . . . . . INTERCOM Knob . . . . . . . . . . . . . . . . . . . HOT MIC CIPHER Switch . . . . . . . . . . . ANT SEL Panel C DF . . . . . . . . . . . . . . . . . . IFF ANT SEL Switch C DF . . . . . . . . . . UHF ANT SEL Switch C DF . . . . . . . . . Communications System . . . . . . . . . . . . . . . . . . 1Ć177 1Ć177 1Ć177 1Ć177 1Ć177 1Ć177 1Ć177 1Ć182 1Ć182 1Ć182 1Ć185 1Ć185 1Ć186 1Ć186 1Ć186 1Ć186 1Ć186 1Ć187 1Ć187 1Ć187 1Ć187 1Ć187 1Ć187 1Ć188 1Ć188 1Ć188 1Ć188 1Ć188 1Ć188 1Ć188 1Ć189 1Ć189 1Ć189 1Ć189 1Ć189 1Ć189 1Ć190 1Ć190 1Ć190 1Ć190 1Ć190 1Ć190 1Ć190 1Ć191 1Ć191 Antenna Locations . . . . . . . . . . . . . . . . . . . . . Have Quick (HQ) System . . . . . . . . . . . . . . . Single Word of Day (WOD) . . . . . . . . . . . Single WOD Transfer . . . . . . . . . . . . . . . . Multiple Word of Day (MWOD) . . . . . . . Automatic MWOD Loading PX III . . . . . TimeĆofĆDay (TOD) Transmission . . . . . TimeĆofĆDay (TOD) Reception PX III . . . TimeĆofĆDay (TOD) Reception PX II . . . Net Number . . . . . . . . . . . . . . . . . . . . . . . . . Antijamming (AJ) Mode Operation . . . . Have Quick (HQ) UHF Radio . . . . . . . . . . . . Operation of the UHF Radio on Upfront Controls . . . . . . . . . . . . . . . . . . UHF Radio Backup Control Panel . . . . . Function Knob . . . . . . . . . . . . . . . . . . . . . . Mode Knob PX II . . . . . . . . . . . . . . . . . . . . Mode Knob PX III . . . . . . . . . . . . . . . . . . . . CHAN Knob . . . . . . . . . . . . . . . . . . . . . . . . . Manual Frequency Knobs . . . . . . . . . . . . AĆ3Ć2ĆT Knob PX II . . . . . . . . . . . . . . . . . . AĆ3Ć2 Knob PX III . . . . . . . . . . . . . . . . . . . . VOL Knob . . . . . . . . . . . . . . . . . . . . . . . . . . SQUELCH Switch . . . . . . . . . . . . . . . . . . . TONE Button PX II . . . . . . . . . . . . . . . . . . CHAN Display PX III . . . . . . . . . . . . . . . . Frequency/Status Display PX III . . . . . . STATUS Button PX III . . . . . . . . . . . . . . . TĆTONE Switch PX III . . . . . . . . . . . . . . . . TEST DISPLAY Button PX III . . . . . . . . ZERO Switch PX III . . . . . . . . . . . . . . . . . . FILL Connector PX III . . . . . . . . . . . . . . . VHF Radio . . . . . . . . . . . . . . . . . . . . . . . . . . . . Operation of the VHF Radio on Upfront Controls . . . . . . . . . . . . . . . . . . Zeroize Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . Navigation Systems . . . . . . . . . . . . . . . . . . . . . . Embedded Global Positioning and Inertial Navigation Set (EGI) PX III . . . . . . . . . . . Global Positioning System (GPS) PX II . . . Inertial Navigation Set (INS) PX II . . . . . . Tactical Air Navigation (TACAN) System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Operation of the TACAN on Upfront Controls . . . . . . . . . . . . . . . . . . . . . . . . . . Terrain Following Radar (TFR) System . . . . . AIFF System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AIFF Transponder PX II . . . . . . . . . . . . . . . . AIFF Transponder PX III . . . . . . . . . . . . . . . Operation of the Transponder on Upfront Controls PX II . . . . . . . . . . . . . Operation of the Transponder on Upfront Controls PX III . . . . . . . . . . . . 1Ć191 1Ć191 1Ć191 1Ć191 1Ć191 1Ć193 1Ć193 1Ć193 1Ć193 1Ć194 1Ć194 1Ć194 1Ć194 1Ć196 1Ć196 1Ć196 1Ć196 1Ć197 1Ć197 1Ć197 1Ć197 1Ć197 1Ć197 1Ć197 1Ć197 1Ć197 1Ć198 1Ć198 1Ć198 1Ć198 1Ć198 1Ć198 1Ć198 1Ć199 1Ć199 1Ć199 1Ć200 1Ć200 1Ć200 1Ć200 1Ć200 1Ć200 1Ć201 1Ć201 1Ć201 1Ć202 ąąąă1Ć5
  21. 21. T.O. GR1FĆ16CJĆ1 AIFF Interrogator . . . . . . . . . . . . . . . . . . . . . . Operation of the Interrogator on Upfront Controls PX II . . . . . . . . . . . . . Operation of the Interrogator on Upfront Controls PX III . . . . . . . . . . . . AIFF Controls and Indicators . . . . . . . . . . . IFF IDENT Button . . . . . . . . . . . . . . . . . . IFF (Mode 4) Caution Light . . . . . . . . . . . UHF VHF IFF Transmit Switch PX II . . . . . . . . . . . . . . . . . . . . . . Target Management Switch PX III . . . . . Instrument Landing System (ILS) . . . . . . . . . ILS Controls . . . . . . . . . . . . . . . . . . . . . . . . Operation of the ILS on Upfront Controls . . . . . . . . . . . . . . . . . . . . . . . . . . MRK BCN Light . . . . . . . . . . . . . . . . . . . . . INSTR MODE Select Panel . . . . . . . . . . . . . . . . INSTR HDG Knob C DF . . . . . . . . . . . . . INSTR MODE Knob . . . . . . . . . . . . . . . . . Navigation Aids and Display . . . . . . . . . . Instrument Modes . . . . . . . . . . . . . . . . . . . Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Airspeed/Mach Indicator . . . . . . . . . . . . . . . . Standby Attitude Indicator (SAI) . . . . . . . . Vertical Velocity Indicator (VVI) . . . . . . . . . Magnetic Compass . . . . . . . . . . . . . . . . . . . . . Attitude Director Indicator (ADI) . . . . . . . . Horizontal Situation Indicator (HSI) . . . . . Clock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Crash Survivable Flight Data Recorder (CSFDR) . . . . . . . . . . . . . . . . . . . . . FĆ16D Aircraft . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Controls DR . . . . . . . . . . . . . . . . . . . . Throttle DR . . . . . . . . . . . . . . . . . . . . . . . . . ENG CONT Switch DR . . . . . . . . . . . . . . . Fuel System . . . . . . . . . . . . . . . . . . . . . . . . . . . Fuel Control Panel DR . . . . . . . . . . . . . . . Speedbrake System . . . . . . . . . . . . . . . . . . . . SPD BRK Switch DR . . . . . . . . . . . . . . . . . Drag Chute System . . . . . . . . . . . . . . . . . . . . DRAG CHUTE Switch DR . . . . . . . . . . . . Landing Gear (LG) System . . . . . . . . . . . . . . DN LOCK REL Button DR . . . . . . . . . . . Flight Control System . . . . . . . . . . . . . . . . . . Stick Control Operation . . . . . . . . . . . . . . . . STICK CONTROL Switch DF . . . . . . . . . Stick Indicator DR . . . . . . . . . . . . . . . . . . . Stick OVRD Lights D . . . . . . . . . . . . . . . . 1Ć6ąąąă 1Ć203 1Ć204 1Ć204 1Ć204 1Ć204 1Ć204 1Ć204 1Ć205 1Ć205 1Ć205 1Ć206 1Ć206 1Ć206 1Ć206 1Ć206 1Ć206 1Ć206 1Ć215 1Ć215 1Ć216 1Ć216 1Ć216 1Ć216 1Ć216 1Ć216 1Ć217 1Ć217 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć219 1Ć220 1Ć220 1Ć220 Escape System D . . . . . . . . . . . . . . . . . . . . . . EJECTION MODE SEL Handle DR . . . Communications System . . . . . . . . . . . . . . . INSTR Mode Select Panel D . . . . . . . . . . . . Flight Instruments DR . . . . . . . . . . . . . . . . . Accelerometer DR . . . . . . . . . . . . . . . . . . . . Aft Station Interface Unit (ASIU) DR PX III . . . . . . . . . . . . . . . . . . . . STICK CONTROL Switch DR PX III . . . ASIU Switch DR PX III . . . . . . . . . . . . . . . Multifunction Display (MFD) DR . . . . . . . . Throttle and Stick Switches/Controls DR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ARMT CONSENT Switch DR . . . . . . . . . . . Aft Seat HUD Monitor (ASHM) DR . . . . . . Servicing Diagram . . . . . . . . . . . . . . . . . . . . . 1Ć220 1Ć220 1Ć221 1Ć221 1Ć221 1Ć221 1Ć221 1Ć221 1Ć222 1Ć222 1Ć222 1Ć222 1Ć222 1Ć222 THE AIRCRAFT The FĆ16C is a singleĆengine, singleĆseat, multirole tactical fighter with full airĆtoĆair and airĆtoĆsurface combat capabilities. The FĆ16D is a twoĆseat (tandem) version and performs the secondary role of a trainer. The fuselage is characterized by a large bubble canopy, forebody strakes, and an underfuseĆ lage engine air inlet. The wing and tail surfaces are thin and feature moderate aft sweep. The wing has automatic leading edge flaps which enhance performance over a wide speed range. Flaperons are mounted on the trailing edge of the wing and combine the functions of flaps and ailerons. The horizontal tails have a small negative dihedral and provide pitch and roll control through symmetrical/ differential deflection. The vertical tail, augmented by twin ventral fins, provides directional stability. All flight control surfaces are actuated hydraulically by two independent hydraulic systems and are directed by signals through a flyĆbyĆwire system. The fire control system includes a fire control radar with search and tracking capability; two multifuncĆ tion displays (MFD's) for presentation of navigation, radar, weapons, and other information; and a headĆup display (HUD). Upfront controls provide a central control point for fire control, communicaĆ tions, navigation, and IFF functions. A stores management system (SMS) presents a visual display on a selected MFD for inventory, control, and release of all stores. Basic armament includes a fuselageĆmounted multibarrel 20 mm gun and an airĆtoĆair missile on each wingtip. Additional stores of various types can be carried on pylons mounted under the wings and on the fuselage.
  22. 22. T.O. GR1FĆ16CJĆ1 AIRCRAFT GENERAL DATA AIRCRAFT GROSS WEIGHT (A/C GW) Refer to figure 1Ć1. The aircraft approximate dimensions are: The GW of the aircraft including pilot, oil, two tip AIMĆ120 missiles, and a full load of 20 mm ammunition is approximately 21,000 pounds and with full internal JPĆ8 fuel 28,200 pounds. D SpanĂ-Ăincluding missile fins = 32 feet 10 inches D LengthĂ-Ăincluding nose probe = 49 feet 5.2 inches D HeightĂ-Ătop of vertical tail = 16 feet 10 inches D HeightĂ-Ătop of canopy = 9 feet 4 inches D Tread = 7 feet 9 inches D Wheelbase = 13 feet 2 inches Refer to TURNING RADIUS AND GROUND CLEARANCE, Section II. C The GW of the aircraft including pilot, oil, two tip AIMĆ120 missiles, and a full load of 20 mm ammunition is approximately 21,600 pounds and with full internal JPĆ8 fuel 27,500 pounds. PX II D PX III D The GW of the aircraft including pilot, oil, two tip AIMĆ120 missiles, and a full load of 20 mm ammunition is approximately 21,900 pounds and with full internal JPĆ8 fuel 27,800 pounds. PX III CFT's add approximately 900 pounds when empty and hold approximately 3000 pounds of JPĆ8 fuel. These GW's are approximate and shall not be used for computing aircraft performance. For maximum GW limitations, refer to Section V, OPERATING LIMITAĆ TIONS. For detailed information, refer to T.O. GR1FĆ16CJĆ1Ć1, Part I. COCKPIT ARRANGEMENT AIRCRAFT GENERAL ARRANGEMENT Refer to figure 1Ć2 for general arrangement and overall view of the aircraft. Refer to figure 1Ć3. The cockpit is conventional except for the seat, which is reclined 30 degrees, and the stick, which is mounted on the right console. The cockpit contains no circuit breakers. ąąąă1Ć7
  23. 23. T.O. GR1FĆ16CJĆ1 General Data AIM-9 MISSILE MISSILE LAUNCHER 15.16 13.32 OUTBOARD STORES LOCATIONS FLAPERON 40 370-GALLON FUEL TANK 37.39 69.63 28.63 95.82 30.63 195.52 18 FT 4.2 IN. SPEEDBRAKE HINGE 29.72 70.87 8.45 135.84 190.43 12.05 44.42 SHADED AREA REPRESENTS PX III D AIRCRAFT 49 FT 5.2 IN. OVERALL LENGTH 46.80 82.05 15.35 29.08 108.62 15 95.0 101.0 19.5 16 FT 10.0 IN. OVERALL HEIGHT 22.20 STATIC GROUND LINE 49.81 NOTE: Dimensions are in inches unless specified otherwise. GR1F-16CJ-1-0004-1A37 Figure 1Ć1.ă(Sheet 1) 1Ć8ąąąă
  24. 24. T.O. GR1FĆ16CJĆ1 WINGS Area Span Aspect Ratio Taper Ratio Sweep (LE) Dihedral Airfoil Incidence Twist At BL 54.0 At BL 180.0 Flaperon Area LEF Area HORIZONTAL TAILS Area Aspect Ratio Taper Ratio Sweep (LE) Dihedral Airfoil At Root At Tip VERTICAL TAIL Area Aspect Ratio Taper Ratio Sweep (LE) Airfoil At Root At Tip Rudder Area 300 Sq Ft 30 Ft 3.0 0.2275 40 0 NACA 64A204 0 0 3 31.32 Sq Ft 36.71 Sq Ft VENTRAL FIN (EACH) Area Span Aspect Ratio Taper Ratio Sweep (LE) Dihedral (Cant) Airfoil At Root At Tip 8.03 Sq Ft 23.356 In. Theo (27.5 In. Actual) 0.472 (Theo) 0.760 (Theo) 30 15 Outboard 3.886% Modified Wedge Constant 0.03R SPEEDBRAKES Area (4 Element Clamshell) 63.70 Sq Ft 2.114 0.390 (Theo) 40 -10 6% Biconvex 3.5% Biconvex 54.75 Sq Ft 1.294 0.437 47.5 5.3% Biconvex 3.0% Biconvex 11.65 Sq Ft LANDING GEAR (LG) Main Gear (MLG) Tire Size Stroke Static Rolling Radius Nose Gear (NLG) Tire Size Stroke Static Rolling Radius 14.26 Sq Ft (3.565 Sq Ft Ea) 27.75 x 8.75-14.5 24 Ply 10.5 In. 11.9 In. 17.9 x 6.7R8 22 Ply 10.0 In. 7.5 In. ENGINE F100ĆPWĆ229 Thrust Engine Compressor Face Diameter Engine Length 29,000 Lb Class 34.8 In. 208 In. F110-GE-129 Thrust Engine Compressor Face Diameter Engine Length 29,500 Lb Class 35.8 In. 183.76 In. 32 FT 10 IN. * OVERALL SPAN W/MISSILES 31 FT OVERALL SPAN W/O MISSILES 10 46.5 93.0 * Add 3 inches for AIM-120 missiles GR1F-16CJ-1-0004-2A37 Figure 1Ć1.ă(Sheet 2) ąąąă1Ć9
  25. 25. 8 11 11 8 25 15 16 15 13 14 For antenna locations, refer to ANTENNA LOCATIONS, this section. 17 27 23 C 8 5 9 10 11 22 17 18 19 20 30 21 28 29 31 12 38 6 7 39 37 40 32 33 41 34 34 17 35 36 42 17 2 1 4 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 26 24 D T.O. GR1FĆ16CJĆ1 1Ć10ąąąă General Arrangement (Typical) Air Data (Pitot) Probe Nose Radome AOA Probe AOA Transmitter Forward Electronic Equipment Bay Cockpit Pressure Regulator Cockpit Pressure Safety Valve HUD/ASHM Instrument Panel Canopy (Movable) Ejection Seat Canopy (Fixed) AIM-9 Missile Missile Launcher AR and Formation Light Position/Formation Light 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 32. 3 63 62 61 60 59 54 55 56 58 57 Static Discharger LEF Drive Unit Hydraulic Reservoir AR Slipway FLCS Accumulators Anticollision Strobe Light Power Supply Vertical Tail Attachment Fittings Vertical Tail Vertical Tail-Mounted Floodlight Anticollision Strobe Light Rudder Position Light Drag Chute Fairing Rudder ISA Turbofan Engine Speedbrake Figure 1Ć2. 52 53 33. 34. 35. 36. 37. 38. 39. 40. 41. 42. 43. 44. 45. 46. 47. 48. 51 44 50 49 44 48 47 Speedbrake Actuator Chaff/Flare Dispenser Horizontal Tail ISA Horizontal Tail Formation Light Flaperon ISA Hook Flaperon Wing Structural Box Fixed Trailing Edge Panel Asymmetry Brake LEF Rotary Actuator LEF Torque Shaft LEF Wing Attachment Fittings MLG 46 45 44 44 43 49. 50. 51. 52. 53. 54. 55. 56. 57. 58. 59. 60. 61. 62. 63. 14 13 16 MLG Door LEF Angle Drive Gearbox Air-Conditioning Package M61A1 20MM Gun Ammunition Drum EPU Nitrogen Bottle Gun Port NLG Door Position Light NLG Engine Air Inlet Left Console Throttle Strake Lower Equipment Compartment GR1F-16CJ-1-0005X37
  26. 26. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX II DF DF INSTRUMENT PANEL LEFT AUXILIARY CONSOLE RIGHT AUXILIARY CONSOLE STICK THROTTLE DF LEFT CONSOLE RIGHT CONSOLE DF GR1F-16CJ-1-0006A37 Figure 1Ć3.ă(Sheet 1) ąąąă1Ć11
  27. 27. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX II LEFT CONSOLE 23 22 24 1 2 21 20 4 18 19 17 14 5 15 16 13 11 3 6 7 9 12 8 DF 10 1. UHF Backup Control Panel 2. AUDIO 1 Control Panel 3. AUDIO 2 Control Panel 4. ECM Control Panel 5. AVTR Control Panel 6. EXT LIGHTING Control Panel 7. MANUAL TRIM Panel 8. G-Suit Hose Connection 9. ANTI G TEST Button 10. DF STICK CONTROL Switch 11. Stowage 12. TEST Switch Panel 13. DEFOG Lever 14. FLT CONTROL Panel 15. Fuel Control Panel 16. AUX COMM Panel 17. CANOPY JETTISON T-Handle 18. EPU Control Panel 19. ELEC Control Panel 20. Throttle FRICTION Control 21. ENG & JET START Control Panel 22. MANUAL PITCH Override Switch 23. CHAFF/FLARE Dispense Button 24. Throttle DF GR1F-16CJ-1-0007A37 Figure 1Ć3.ă(Sheet 2) 1Ć12ąąąă
  28. 28. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX II LEFT AUXILIARY CONSOLE RIGHT AUXILIARY CONSOLE DF 18 19 1 2 3 5 17 1 6 16 15 12 14 13 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 4 7 10 4 3 8 11 2 6 5 7 8 9 EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) ANTI-SKID Switch DN LOCK REL Button LG Handle Down Permission Button LG Handle LG Handle Warning Light (Red) LANDING TAXI LIGHTS Switch CMDS Control Panel RF Transmit Panel RWR Aux Control Panel ALT GEAR Handle ALT GEAR Reset Button SPEED BRAKE Position Indicator STORES CONFIG Switch HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) BRAKES Channel Switch 9 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 10 Magnetic Compass FUEL Quantity Indicator Pilot Fault List Display System A HYD PRESS Indicator System B HYD PRESS Indicator Caution Light Panel LIQUID OXYGEN Quantity Indicator EPU FUEL Quantity Indicator Cockpit Pressure Altimeter Clock GR1F-16CJ-1-0008A37 Figure 1Ć3.ă(Sheet 3) ąąąă1Ć13
  29. 29. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX II INSTRUMENT PANEL DF 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. HUD Combiner Glass DF AOA Indexer AR Status/NWS Indicator 42 2 Integrated Control Panel (ICP) Standby Attitude Indicator FUEL FLOW Indicator 41 Data Entry Display 40 ENG FIRE and ENGINE Warning 39 Lights (Red) 38 36 HYD/OIL PRESS Warning Light (Red) 37 FLCS and DBU ON Warning 35 34 Lights (Red) 28 TO/LDG CONFIG Warning Light (Red) 33 32 CANOPY Warning Light (Red) 31 Right MFD 22 OIL Pressure Indicator 29 NOZ POS Indicator 30 RPM Indicator 23 30. Autopilot ROLL Switch FTIT Indicator 31. ADV MODE Switch Vertical Velocity Indicator 32. MASTER ARM Switch 21 MRK BCN Light 33. C ALT REL Button FUEL QTY SEL Panel 34. LASER ARM Switch Rudder PEDAL ADJ Knob 35. IFF IDENT Button AOA Indicator 36. DRAG CHUTE Switch INSTR MODE Select Panel 37. RWR Prime Control Panel Airspeed/Mach Indicator 38. Azimuth Display/Indicator Attitude Director Indicator 39. F-ACK Button Horizontal Situation Indicator 40. TF FAIL Warning Light (Red) Altimeter 41. MASTER CAUTION Light (Amber) Left MFD 42. ECM Light (Green), DF ECM (Green) and OVRD (Amber) Light Autopilot PITCH Switch Figure 1Ć3.ă(Sheet 4) 1Ć14ąąąă 3 7 6 8 9 1 4 24 12 14 15 16 5 13 27 25 18 19 26 20 36 34 10 11 17 DF 39 32 31 30 29 GR1F-16CJ-1-0009A37
  30. 30. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX II RIGHT CONSOLE 17 19 1 2 DF 18 4 3 16 5 6 15 14 10 13 12 7 9 8 11 DF 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. SNSR PWR Control Panel HUD Control Panel Interior LIGHTING Control Panel NUCLEAR CONSENT Switch (Guarded) PLAIN Cipher Switch AIR COND Control Panel ENGINE ANTI-ICE Switch Utility Light ANT SEL Panel AVIONICS POWER Panel OXYGEN REGULATOR Panel DTU Control Panel Stowage Oxygen/Communication Hookup VOICE MESSAGE Switch ZEROIZE Switch Stick DF NWS Control Button/Indicator (Green) SEAT ADJ Switch GR1F-16CJ-1-0010A37 Figure 1Ć3.ă(Sheet 5) ąąąă1Ć15
  31. 31. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX II INSTRUMENT PANEL LEFT AUXILIARY CONSOLE RIGHT AUXILIARY CONSOLE STICK THROTTLE LEFT CONSOLE RIGHT CONSOLE GR1F-16CJ-1-0011A37 Figure 1Ć3.ă(Sheet 6) 1Ć16ąąąă
  32. 32. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX II LEFT CONSOLE 7 9 8 1 2 6 10 5 11 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 4 3 AUDIO 1 Control Panel AUDIO 2 Control Panel G-Suit Hose Connection ANTI G TEST Button MAL & IND LTS Test Button FUEL MASTER Switch MANUAL PITCH Override Switch ENG CONT Switch Throttle CANOPY JETTISON T-Handle Stowage GR1F-16CJ-1-0012A37 Figure 1Ć3.ă(Sheet 7) ąąąă1Ć17
  33. 33. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX II LEFT AUXILIARY CONSOLE 1 15 2 4 7 14 5 12 10 6 1 9 11 8 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 3 RIGHT AUXILIARY CONSOLE 6 13 3 4 EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) DN LOCK REL Button LG Handle Down Permission Button LG Handle Warning Light (Red) LG Handle ALT GEAR Handle ALT GEAR Reset Button Blank Panel SPEED BRAKE Position Indicator ALT FLAPS Switch (Lever Lock) HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) DRAG CHUTE Switch Figure 1Ć3.ă(Sheet 8) 1Ć18ąąąă 2 5 1. 2. 3. 4. 5. 6. Clock FUEL Quantity Indicator System B HYD PRESS Indicator System A HYD PRESS Indicator EJECTION MODE SELECT Handle Caution Light Panel GR1F-16CJ-1-0013A37
  34. 34. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX II INSTRUMENT PANEL 1. MASTER CAUTION Light (Amber) 2. ENG FIRE and ENGINE Warning Lights (Red) 3. HYD/OIL PRESS Warning Light (Red) 4. FLCS and DBU ON Warning Lights (Red) 5. AR Status/NWS Indicator 6. TO/LDG CONFIG Warning Light (Red) 7. CANOPY Warning Light (Red) 8. Right MFD 9. VIDEO SEL Switch 10. Standby Attitude Indicator 11. FUEL FLOW Indicator 12. OIL Pressure Indicator 13. FAULT ACK Button 14. NOZ POS Indicator 15. RPM Indicator 16. FTIT Indicator 17. Pilot Fault List Display 18. Accelerometer 19. Altimeter 20. Vertical Velocity Indicator 21. Attitude Director Indicator 22. Horizontal Situation Indicator 23. MRK BCN Light 24. Rudder PEDAL ADJ Knob 25. INSTR MODE Select Panel 26. AOA Indicator 27. Airspeed/Mach Indicator 28. ARMT CONSENT Switch (Guarded) 39 32 33 38 37 40 41 35 IFF IDENT Button Data Entry Display Integrated Keyboard Panel (IKP) Stick Indicator OVRD Light (Amber) Blank Azimuth Display/Indicator Left MFD AOA Indexer TF FAIL Warning Light (Red) Handgrip ECM Light (Green) Aft Seat HUD Monitor 5 8 11 36 7 9 12 10 28 26 25 21 22 13 14 15 27 19 18 31 29. 30. 31. 32. 33. 34. 35. 36. 37. 38. 39. 40. 41. 46 1 34 30 29 2 3 17 20 16 23 24 GR1F-16CJ-1-0014A37 Figure 1Ć3.ă(Sheet 9) ąąąă1Ć19
  35. 35. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX II RIGHT CONSOLE 7 8 6 1 5 2 4 1. 2. 3. 4. 5. 6. 7. 8. 3 Interior LIGHTING Control Panel OXYGEN REGULATOR Panel Utility Light Oxygen/Communications Hookup Stowage NWS Control Button/Indicator (Green) Stick SEAT ADJ Switch GR1F-16CJ-1-0015A37 Figure 1Ć3.ă(Sheet 10) 1Ć20ąąąă
  36. 36. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX III DF DF INSTRUMENT PANEL LEFT AUXILIARY CONSOLE RIGHT AUXILIARY CONSOLE STICK THROTTLE DF RIGHT CONSOLE LEFT CONSOLE DF GR1F-16CJ-1-1006X37 Figure 1Ć3. (Sheet 11) Change 1ąąąă1Ć21
  37. 37. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX III LEFT CONSOLE 24 23 25 1 2 22 21 3 4 19 20 7 5 18 16 17 14 15 8 13 10 12 6 9 DF 11 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. UHF Backup Control Panel AUDIO 1 Control Panel AUDIO 2 Control Panel ECM Control Panel AVTR Control Panel EXT LIGHTING Control Panel JHMCS Connection MANUAL TRIM Panel G-Suit Hose Connection ANTI G TEST Button DF STICK CONTROL Switch Stowage TEST Switch Panel DEFOG Lever FLT CONTROL Panel Fuel Control Panel IFF Panel CANOPY JETTISON T-Handle EPU Control Panel ELEC Control Panel Throttle FRICTION Control ENG & JET START Control Panel MANUAL PITCH Override Switch CHAFF/FLARE Dispense Button Throttle GR1F-16CJ-1-1007X37 Figure 1Ć3. (Sheet 12) 1Ć22ąąąă
  38. 38. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX III LEFT AUXILIARY CONSOLE RIGHT AUXILIARY CONSOLE DF 18 19 1 2 3 5 17 1 6 16 15 12 14 13 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 4 7 10 4 3 8 11 2 5 6 7 9 EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) ANTI-SKID Switch DN LOCK REL Button LG Handle Down Permission Button LG Handle LG Handle Warning Light (Red) LANDING TAXI LIGHTS Switch CMDS Control Panel HMCS Panel RWR Aux Control Panel ALT GEAR Handle ALT GEAR Reset Button SPEED BRAKE Position Indicator STORES CONFIG Switch HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) BRAKES Channel Switch 8 1. 2. 3. 4. 5. 6. 7. 8. 9. 9 Magnetic Compass FUEL Quantity Indicator Pilot Fault List Display System A HYD PRESS Indicator System B HYD PRESS Indicator Caution Light Panel EPU FUEL Quantity Indicator Cockpit Pressure Altimeter Clock GR1F-16CJ-1-1008X37 Figure 1Ć3. (Sheet 13) ąąąă1Ć23
  39. 39. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX III INSTRUMENT PANEL DF 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. HUD Combiner Glass AOA Indexer AR Status/NWS Indicator Integrated Control Panel (ICP) Standby Attitude Indicator FUEL FLOW Indicator Data Entry Display ENG FIRE and ENGINE Warning 38 Lights (Red) 35 HYD/OIL PRESS Warning Light (Red) FLCS and DBU ON Warning 34 Lights (Red) TO/LDG CONFIG Warning Light (Red) CANOPY and OXY LOW Warning Lights (Red) 31 Right MFD OIL Pressure Indicator NOZ POS Indicator 30 RPM Indicator 30. Autopilot ROLL Switch FTIT Indicator 31. ADV MODE Switch Vertical Velocity Indicator 32. MASTER ARM Switch MRK BCN Light 33. LASER ARM Switch FUEL QTY SEL Panel 34. IFF IDENT Button Rudder PEDAL ADJ Knob 35. DRAG CHUTE Switch AOA Indicator 36. RWR Prime Control Panel INSTR MODE Select Panel 37. Azimuth Display/Indicator Airspeed/Mach Indicator 38. F-ACK Button Attitude Director Indicator 39. TF FAIL Warning Light (Red) Horizontal Situation Indicator 40. MASTER CAUTION Light (Amber) Altimeter 41. ECM Light (Green), DF ECM (Green) Left MFD and OVRD (Amber) Light Autopilot PITCH Switch Figure 1Ć3. (Sheet 14) 1Ć24ąąąăChange 1 41 36 33 32 4 37 28 7 6 8 9 1 40 39 29 3 2 24 5 27 22 25 23 26 20 13 18 19 10 11 12 14 15 16 17 21 GR1F-16CJ-1-1009X37
  40. 40. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement C DF (Typical) PX III RIGHT CONSOLE 17 DF 18 4 3 16 5 6 15 14 19 1 2 20 10 13 12 7 9 8 11 DF 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. SNSR PWR Control Panel HUD Control Panel Interior LIGHTING Control Panel NUCLEAR CONSENT Switch (Guarded) PLAIN Cipher Switch AIR COND Control Panel ENGINE ANTI-ICE Switch Utility Light ANT SEL Panel AVIONICS POWER Panel OBOGS MONITOR Panel UDTU Stowage Oxygen/Communication Hookup VOICE MESSAGE Switch ZEROIZE Switch Stick DF NWS Control Button/Indicator (Green) SEAT ADJ Switch OXYGEN Panel GR1F-16CJ-1-1010X37 Figure 1Ć3. (Sheet 15) Change 1ąąąă1Ć25
  41. 41. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX III INSTRUMENT PANEL LEFT AUXILIARY CONSOLE RIGHT AUXILIARY CONSOLE STICK THROTTLE LEFT CONSOLE RIGHT CONSOLE GR1F-16CJ-1-1011X37 Figure 1Ć3. (Sheet 16) 1Ć26ąąąă
  42. 42. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX III LEFT CONSOLE 7 9 8 1 2 6 10 5 11 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 4 3 AUDIO 1 Control Panel AUDIO 2 Control Panel G-Suit Hose Connection ANTI G TEST Button MAL & IND LTS Test Button FUEL MASTER Switch MANUAL PITCH Override Switch ENG CONT Switch Throttle CANOPY JETTISON T-Handle Stowage GR1F-16CJ-1-1012X37 Figure 1Ć3. (Sheet 17) ąąąă1Ć27
  43. 43. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX III LEFT AUXILIARY CONSOLE 1 15 2 4 7 14 5 12 10 6 1 9 11 8 1. 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. 14. 15. 3 RIGHT AUXILIARY CONSOLE 6 13 3 4 EMER STORES JETTISON Button (Covered) WHEELS Down Lights (Green) HOOK Switch (Lever Lock) DN LOCK REL Button LG Handle Down Permission Button LG Handle Warning Light (Red) LG Handle ALT GEAR Handle ALT GEAR Reset Button Blank Panel SPEED BRAKE Position Indicator ALT FLAPS Switch (Lever Lock) HORN SILENCER Button GND JETT ENABLE Switch (Lever Lock) DRAG CHUTE Switch Figure 1Ć3. (Sheet 18) 1Ć28ąąąă 2 5 1. 2. 3. 4. 5. 6. Clock FUEL Quantity Indicator System B HYD PRESS Indicator System A HYD PRESS Indicator EJECTION MODE SELECT Handle Caution Light Panel GR1F-16CJ-1-1013X37
  44. 44. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX III INSTRUMENT PANEL 1. MASTER CAUTION Light (Amber) (NVIS) 40 41 38 2. ENG FIRE and ENGINE Warning 2 3 46 Lights (Red) 37 39 3. HYD/OIL PRESS Warning Light (Red) 1 4. FLCS and DBU ON Warning Lights (Red) 5 5. AR Status/NWS Indicator 34 6. TO/LDG CONFIG Warning Light (Red) 33 7. CANOPY and OXY LOW Warning Lights (Red) 8 8. Right MFD (NVIS) 32 36 11 10 9. VIDEO SEL Switch 35 10. Standby Attitude Indicator 27 19 18 11. FUEL FLOW Indicator 31 12. OIL Pressure Indicator 21 17 13. FAULT ACK Button 28 20 14. NOZ POS Indicator 30 29 26 22 15. RPM Indicator 23 29. MASTER MODE Caution Lights (NVIS) 25 16. FTIT Indicator 30. Data Entry Display 17. Pilot Fault List Display 24 31. Integrated Keyboard Panel (IKP) (NVIS) 18. Accelerometer 32. IFF IDENT Button 19. Altimeter 33. Stick Indicator 20. Vertical Velocity Indicator 34. Blank 21. Attitude Director Indicator 35. Azimuth Display/Indicator (NVIS) 22. Horizontal Situation Indicator 36. Left MFD (NVIS) 23. MRK BCN Light 37. AOA Indexer (NVIS) 24. Rudder PEDAL ADJ Knob 38. TF FAIL Warning Light (Red) 25. INSTR MODE Select Panel 39. Handgrip 26. AOA Indicator 40. ECM and OVRD Lights (Amber) 27. Airspeed/Mach Indicator 41. Aft Seat HUD Monitor (NVIS) 28. ARMT CONSENT Switch (Guarded) 7 9 12 13 14 15 16 GR1F-16CJ-1-1014X37 Figure 1Ć3. (Sheet 19) ąąąă1Ć29
  45. 45. T.O. GR1FĆ16CJĆ1 Cockpit Arrangement DR (Typical) PX III RIGHT CONSOLE 7 9 6 8 1 5 2 4 1. 2. 3. 4. 5. 6. 7. 8. 9. 3 Interior LIGHTING Control Panel OXYGEN REGULATOR Panel Utility Light Oxygen/Communications Hookup Stowage NWS Control Button/Indicator (Green) Stick SEAT ADJ Switch STICK CONTROL/ASIU Panel GR1F-16CJ-1-1015X37 Figure 1Ć3. (Sheet 20) 1Ć30ąąąă
  46. 46. T.O. GR1FĆ16CJĆ1 ENGINE Main Fuel Control (MFC) PW 229 ENGINE GENERAL DESCRIPTION PW 229 Refer to figure 1Ć4. The aircraft is powered by a single F100ĆPWĆ229 afterburning turbofan engine. MaxiĆ mum thrust is approximately 29,000 pounds. ENGINE FUEL SYSTEM PW 229 Refer to figure 1Ć5. The engine fuel system delivers the required fuel to the engine for combustion and for use by the control system for scheduling the engine variable geometry. ENGINE CONTROL SYSTEM PW 229 The MFC operates in both the PRI and SEC modes. During PRI control, the MFC receives throttle inputs, fuel from the main fuel pump, and electrical commands from the DEEC. It controls main ignition, start bleed strap position, main engine fuel flow, and rear compressor variable vane (RCVV) position. The MFC also provides actuation pressure to the compressor inlet variable vane (CIVV) control, the convergent exhaust nozzle control (CENC), and both the AB fuel control and AB pump controller. In SEC, the MFC receives throttle inputs, fuel from the main fuel pump, and static pressure and total temperature signals from the fan inlet case. The MFC controls main engine fuel flow, start bleed strap position, RCVV's, and engine ignition. Afterburner (AB) Fuel Control PW 229 The engine control system is composed of three major components:ąthe main fuel control (MFC), the AB fuel control, and the digital electronic engine control (DEEC). The engine has two modes of operaĆ tion:ąprimary (PRI) and secondary (SEC). PW 229 During primary operation, the AB fuel control receives fuel from the AB fuel pump and electrical commands from the DEEC. It provides AB ignition, AB segment sequencing, and fuel flow to the AB segments. During SEC control, AB fuel flow is inhibited. F100-PW-229 Engine FAN MODULE FAN 3 STAGES CORE ENGINE MODULE FAN DRIVE TURBINE MODULE REAR COMPRESSOR 10 STAGES COMBUSTION CHAMBER RCVV FAN DUCT AB MODULE AB SPRAY RINGS AND FLAME HOLDER CONVERGENT NOZZLE DIVERGENT NOZZLE INLET PRESSURE PROBE CIVV ENGINE DIAGNOSTIC UNIT MAIN FUEL PUMP ENGINE-DRIVEN GEARBOX AB LIGHT-OFF DETECTOR HIGH PRESSURE TURBINE AB FUEL CONTROL MAIN FUEL CONTROL DIGITAL ELECTRONIC ENGINE CONTROL 1F-16X-1-4004X Figure 1Ć4. ąąąă1Ć31
  47. 47. T.O. GR1FĆ16CJĆ1 Engine Fuel/Control System Schematic ENGINE F100-PW-229 (Typical) LEGEND: ELECTRICAL MECHANICAL ENG BLEED AIR FUEL (COOLING) FUEL PRESSURIZATION AND DUMP VALVE ENGINE LUBE OIL TO AND FROM OIL SYSTEM MFP BOOST PRESS MFP PRESSURE ENGINE DIAGNOSTIC UNIT (EDU) RCVV CIVV START BLEED SERVO PRESSURE BOOST PUMP PRESS FUEL/OIL COOLER ACTUATION PRESSURE ANTIICING VALVE ENGINE SIGNALS MAIN FUEL CONTROL (MFC) DIGITAL ELECTRONIC ENGINE CONTROL (DEEC) CONTROL AND FEEDBACK ENGINE AB FUEL CONTROL (AFC) ENGINE CONTROL AND FEEDBACK ENGINE FAN DUCT AB PUMP CONTROLLER AB FUEL PUMP LIGHT-OFF DETECTOR ENGINE BLEED AIR (FOR ACTUATION) AIRFRAME ENGINE INLET CASE ENGINE BLEED AIR FOR TURBINE POWER CIVV ACTUATOR CENC OVBD ENGINE BLEED AIR RCVV ACTUATOR AIRFRAME SIGNALS ENGINE CONTROL AND FEEDBACK AIRFRAME SIGNALS AB FUEL FLOW RTN TO RSVRS MAIN FUEL PUMP THROTTLE FUEL FLOW TRANSMITTER FUEL LINE STRAINER MAIN FUEL SHUTOFF VALVE FUEL/OIL HEAT EXCHANGER AB RESET COCKPIT ANTI-ICE ENGINE DATA REQUEST ICE DETECTOR SIGNAL MACH ENGINE SIGNALS ENGINE FAULT FTIT NOZ POS OIL RPM FROM FFP ENGINE ELECTRONIC CONTROL COOLING FUEL SHUTOFF VALVE GR1F-16CJ-1-1017X37 Figure 1Ć5. 1Ć32ąąąă

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