F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 10

T.O. GR1F16CJ1

164

GR1F-16CJ-1-1026-1X37

E

D

C

B

A

4

3

2

1

T

T

FWD

RSVR

AFT

RSVR

FROM ECS

F-1

F-2

RIGHT

WING

LEFT

WING

**

*

6

7

**

HALON RSVR

*

Fuel System    (Typical)

C

TRANSFER

SWITCH

EXTERNAL TANK

(TYPICAL)

FUEL QTY

SEL PANEL

TANK

INERTING

SWITCH

FUEL

QUANTITY

INDICATOR

FLOAT

SWITCH

PX III

*

* *

*

* *

CFT DRY

PAN

Figure 120.(Sheet 3)

T.O. GR1F16CJ1

165

5

TRANSFER

TRIM

VALVE

AIR

REFUEL

SWITCH

LEGEND:

A-1

T

*

**

TRANSFER SHUTOFF VALVE

TRANSFER PUMP (ELECTRICAL)

BOOST PUMP (ELECTRICAL)

REFUEL SHUTOFF VALVE

SOLENOID VALVE

CROSSFEED VALVE

TRANSFER PUMP

(FUEL PRESSURE DRIVEN)

SUCTION FEED VALVE

DISCONNECT

FUEL EJECTOR PUMP

ELECTRIC MOTOR OPERATED

SHUTOFF VALVE
ORIFICE
CHECK VALVE

TO RIGHT WING EXT TANK

TO CENTERLINE TANK

HALON/AIR MIXING VALVE

EXT TANK VENT & PRESS VALVE

INT TANK VENT & PRESS VALVE

REMOTE SENSING PRESSURE

RELIEF VALVE

AR RECEPTACLE

A

B

C

D

E

OVERBOARD VENT
FUEL SUPPLY
BOOST PUMP PRESSURE
PUMP DRIVE PRESSURE

TANK INERTING PRESSURE

FUEL TRANSFER

TRANSFER/REFUEL

PRESSURIZATION

REFUEL/TRANSFER
ECS PRESSURIZATION SUPPLY

TRANSFER BLEED

TANK PRESSURIZATION

CAUTION LIGHTS

CAUTION LIGHT

TO JFS

TEMPERATURE SENSOR

GROUND COOLING RECEPTACLE

STANDPIPE OPENING AT TOP

OF TANK

STANDPIPE OPENING AT

BOTTOM OF TANK

FUEL TANK CONNECTING

STANDPIPE

ELECTRICAL

ENG FEED

KNOB

FUEL MASTER

SWITCH

FUEL/OIL

HOT

FWD

FUEL LOW

AFT

FUEL LOW

PUMP

DRIVE

PRESSURE

FROM

HYD

SYS A

FUEL FLOW

PROPORTIONER

FUEL FLOW

INDICATOR

FUEL FLOW

TRANSMITTER

TO ENGINE

GROUND REFUELING

RECEPTACLE

AR STATUS

INDICATOR

FUEL/OIL HEAT

EXCHANGER

DEC

TO RIGHT CFT

** *

8

CONFORMAL FUEL TANK

(TYPICAL)

REMOTE SENSING PRESSURE

F

RELIEF VALVE (CFT)

F

GR1F-16CJ-1-1026-2X37

TO VENT TANK

TO WING

Figure 120.(Sheet 4)

T.O. GR1F16CJ1

166

GR1F-16CJ-1-0027-1A37

Fuel System

D

(Typical)

E

D

C

B

A

4

3

2

1

T

T

FWD

RSVR

AFT

RSVR

EXTERNAL TANK
(TYPICAL)

FROM ECS

FLOAT
SWITCH

F-1

RIGHT

WING

LEFT

WING

*

**

**

*

6

7

DF

HALON RSVR

FWD & AFT FUEL

QUANTITY INDICATORS

TANK

INERTING

SWITCH

FUEL QTY

SEL PANEL

TRANSFER

SWITCH

F-2

PX II

Figure 121.(Sheet 1)

T.O. GR1F16CJ1

167

GR1F-16CJ-1-0027-2X37

5

PUMP

DRIVE

PRESSURE

FROM HYD

SYS A

FUEL FLOW

PROPORTIONER

TO JFS

ENG FEED

KNOB

TRANSFER

TRIM

VALVE

AIR

REFUEL

SWITCH

TO ENGINE

FUEL/OIL HEAT EXCHANGER

A-1

OVERBOARD VENT

FUEL SUPPLY
BOOST PUMP PRESSURE
PUMP DRIVE PRESSURE

TANK INERTING PRESSURE

FUEL TRANSFER

TRANSFER/REFUEL

PRESSURIZATION

REFUEL/TRANSFER
ECS PRESSURIZATION SUPPLY

TRANSFER BLEED

TANK PRESSURIZATION

FUEL FLOW TRANSMITTER

LEGEND:

T

*

**

TRANSFER SHUTOFF VALVE

TRANSFER PUMP (ELECTRICAL)

BOOST PUMP (ELECTRICAL)

REFUEL SHUTOFF VALVE

SOLENOID VALVE

CROSSFEED VALVE

TRANSFER PUMP

(FUEL PRESSURE DRIVEN)

SUCTION FEED VALVE

DISCONNECT

FUEL EJECTOR PUMP

ELECTRIC MOTOR OPERATED

SHUTOFF VALVE
ORIFICE
CHECK VALVE

TO RIGHT WING EXT TANK

TO CENTERLINE TANK

HALON/AIR MIXING VALVE
EXT TANK VENT & PRESS VALVE
INT TANK VENT & PRESS VALVE
REMOTE SENSING PRESSURE

RELIEF VALVE

AR RECEPTACLE

A

B

C

D

E

TEMPERATURE SENSOR

GROUND COOLING RECEPTACLE

STANDPIPE OPENING AT TOP

OF TANK

STANDPIPE OPENING AT

BOTTOM OF TANK

FUEL TANK CONNECTING

STANDPIPE

ELECTRICAL

FWD

FUEL LOW

AFT

FUEL LOW

FWD

FUEL LOW

AFT

FUEL LOW

CAUTION LIGHT

FWD & AFT

FUEL/OIL

HOT

GROUND REFUELING

RECEPTACLE

FWD AR

STATUS

INDICATOR

AFT AR

STATUS

INDICATOR

FWD CAUTION

LIGHTS

AFT CAUTION

LIGHTS

DEC

FWD FUEL

MASTER SWITCH

AFT FUEL

MASTER SWITCH

FWD & AFT FUEL

FLOW INDICATOR

Figure 121.(Sheet 2)

T.O. GR1F16CJ1

168

GR1F-16CJ-1-1027-1X37

Fuel System

D

(Typical)

E

D

C

B

A

4

3

2

1

T

T

FWD

RSVR

AFT

RSVR

EXTERNAL TANK
(TYPICAL)

FROM ECS

FLOAT
SWITCH

F-1

RIGHT

WING

LEFT

WING

*

**

**

*

6

7

DF

HALON RSVR

FWD & AFT FUEL

QUANTITY INDICATORS

TANK

INERTING

SWITCH

FUEL QTY

SEL PANEL

TRANSFER

SWITCH

F-2

*

* *

PX III

*

* *

CFT DRY

PAN

Figure 121.(Sheet 3)

T.O. GR1F16CJ1

169

GR1F-16CJ-1-1027-2X37

5

PUMP

DRIVE

PRESSURE

FROM HYD

SYS A

FUEL FLOW

PROPORTIONER

TO JFS

ENG FEED

KNOB

TRANSFER

TRIM

VALVE

AIR

REFUEL

SWITCH

TO ENGINE

FUEL/OIL HEAT EXCHANGER

A-1

OVERBOARD VENT

FUEL SUPPLY
BOOST PUMP PRESSURE
PUMP DRIVE PRESSURE

TANK INERTING PRESSURE

FUEL TRANSFER

TRANSFER/REFUEL

PRESSURIZATION

REFUEL/TRANSFER
ECS PRESSURIZATION SUPPLY

TRANSFER BLEED

TANK PRESSURIZATION

FUEL FLOW TRANSMITTER

LEGEND:

T

*

**

TRANSFER SHUTOFF VALVE

TRANSFER PUMP (ELECTRICAL)

BOOST PUMP (ELECTRICAL)

REFUEL SHUTOFF VALVE

SOLENOID VALVE

CROSSFEED VALVE

TRANSFER PUMP

(FUEL PRESSURE DRIVEN)

SUCTION FEED VALVE

DISCONNECT

FUEL EJECTOR PUMP

ELECTRIC MOTOR OPERATED

SHUTOFF VALVE
ORIFICE
CHECK VALVE

TO RIGHT WING EXT TANK

TO CENTERLINE TANK

HALON/AIR MIXING VALVE
EXT TANK VENT & PRESS VALVE
INT TANK VENT & PRESS VALVE
REMOTE SENSING PRESSURE

RELIEF VALVE

AR RECEPTACLE

A

B

C

D

E

TEMPERATURE SENSOR

GROUND COOLING RECEPTACLE

STANDPIPE OPENING AT TOP

OF TANK

STANDPIPE OPENING AT

BOTTOM OF TANK

FUEL TANK CONNECTING

STANDPIPE

ELECTRICAL

FWD

FUEL LOW

AFT

FUEL LOW

FWD

FUEL LOW

AFT

FUEL LOW

CAUTION LIGHT

FWD & AFT

FUEL/OIL

HOT

GROUND REFUELING

RECEPTACLE

FWD AR

STATUS

INDICATOR

AFT AR

STATUS

INDICATOR

FWD CAUTION

LIGHTS

AFT CAUTION

LIGHTS

DEC

FWD FUEL

MASTER SWITCH

AFT FUEL

MASTER SWITCH

FWD & AFT FUEL

FLOW INDICATOR

**

TO RIGHT CFT

*

8

CONFORMAL FUEL TANK

(TYPICAL)

REMOTE SENSING PRESSURE

F

RELIEF VALVE (CFT)

F

TO VENT TANK

TO WING

Figure 121.(Sheet 4)

T.O. GR1F16CJ1

170Change 1

GR1F-16CJ-1-0025A37

Fuel Quantity Indication and Tank

Arrangement (Typical)

FUEL QUANTITY INDICATIONS (JP-8) WITH

NORM SELECTED AND FULL INTERNAL

TANKS WITH TWO FULL 370-GALLON

EXTERNAL WING TANKS.

C

D

2

4

5

6

7

10

3

8

9

1

PX II

C

D

TANK LOCATION

FUELQTYSEL

KNOB SET

TINGS

POINTER

FUEL

QTY (LB) JP4

FUEL

QTY (LB) JP5/8

FUEL

QTY (LB) JP4

FUEL

QTY (LB) JP5/8

1. LEFT INTERNAL WING
2. RIGHT INTERNAL WING

INT WING

INT WING

AL

FR

525

$

100

525

$

100

550

$

100

550

$

100

525

$

100

525

$

100

550

$

100

550

$

100

3. F1 FUSELAGE
4. F2 FUSELAGE
5. FWD RESERVOIR

NORM

FR

3100

$

100

3250

$

100

1800

$

100

1890

$

100

6. AFT RESERVOIR
7. A1 FUSELAGE

NORM

AL

2675

$

100

2810

$

100

2675

$

100

2810

$

100

5. FWD RESERVOIR
6. AFT RESERVOIR

RSVR

RSVR

FR

AL

460

$

30

460

$

30

480

$

30

480

$

30

460

$

30

460

$

30

480

$

30

480

$

30

8. CENTERLINE
9. LEFTEXTERNALWING

370/600

10. RIGHTEXTERNALWING

370/600

EXT CTR

EXT WING

EXT WING

FR
AL

FR

1800

$

100

2300/3750

$

100

2300/3750

$

100

1890

$

100

2420/3925

$

100

2420/3925

$

100

1800

$

100

2300/3750

$

100

2300/3750

$

100

1890

$

100

2420/3925

$

100

2420/3925

$

100

TOTAL INTERNAL FUEL

6825

$

300

7160

$

300

5575

$

300

5800

$

300

TOTAL EXTERNAL FUEL (370/600)

6400/9300

$

300 6730/9740

$

300 6400/9300

$

300 6730/9740

$

300

NOTES:

1. Tolerances are due to indication errors with the variations in density resulting from temperatures, additives, etc.
2. The quantity of wing fuel varies depending upon aircraft attitude during refueling.
3. Usable fuel and indicated fuel quantities are approximately equal.
4. Indications are approximate and shall not be used for computing weight and balance data. Refer to T.O. GR1F16CJ11 for detailed

information.

Figure

 122. (Sheet 1)

T.O. GR1F16CJ1

171

GR1F-16CJ-1-1025X37

Fuel Quantity Indication and Tank

Arrangement (Typical)

FUEL QUANTITY INDICATIONS (JP-8) WITH

NORM SELECTED AND FULL INTERNAL

TANKS WITH TWO FULL 370-GALLON

EXTERNAL WING TANKS.

C

D

PX III

2

4

5

6

7

10

3

8

9

1

CFT

CFT

C

D

TANK LOCATION

FUELQTYSEL

KNOB SET

TINGS

POINTER

FUEL

QTY (LB) JP4

FUEL

QTY (LB) JP5/8

FUEL

QTY (LB) JP4

FUEL

QTY (LB) JP5/8

1. LEFT INTERNAL 

WING/WITH CFT

2. RIGHT INTERNAL

WING/WITH CFT

INT WING

& CFT

INT WING

& CFT

AL

FR

525/1965

$

100

525/1965

$

100

550/2080

$

100

550/2080

$

100

525/1965

$

100

525/1965

$

100

550/2080

$

100

550/2080

$

100

3. F1 FUSELAGE
4. F2 FUSELAGE
5. FWD RESERVOIR

NORM

FR

3100

$

100

3250

$

100

1800

$

100

1890

$

100

6. AFT RESERVOIR
7. A1 FUSELAGE

NORM

AL

2675

$

100

2810

$

100

2675

$

100

2810

$

100

5. FWD RESERVOIR
6. AFT RESERVOIR

RSVR

RSVR

FR

AL

460

$

30

460

$

30

480

$

30

480

$

30

460

$

30

460

$

30

480

$

30

480

$

30

8. CENTERLINE
9. LEFTEXTERNALWING

370/600

10. RIGHTEXTERNALWING

370/600

EXT CTR

EXT WING

EXT WING

FR
AL

FR

1800

$

100

2300/3750

$

100

2300/3750

$

100

1890

$

100

2420/3925

$

100

2420/3925

$

100

1800

$

100

2300/3750

$

100

2300/3750

$

100

1890

$

100

2420/3925

$

100

2420/3925

$

100

TOTAL INTERNAL FUEL (Without CFT's/With CFT's)

6825/9705

$

300

7160/10220

$

300

5525/8405

$

300

5800/8860

$

300

TOTAL EXTERNAL FUEL (370/600)

6400/9300

$

300

6730/9740

$

300

6400/9300

$

300

6730/9740

$

300

NOTES:

1. Tolerances are due to indication errors with the variations in density resulting from temperatures, additives, etc.

2. The quantity of wing fuel varies depending upon aircraft attitude during refueling.

3. Usable fuel and indicated fuel quantities are approximately equal.

4. Indications are approximate and shall not be used for computing weight and balance data. Refer to T.O. GR1F16CJ11 for detailed

information.

5. Actual reservoir quantities are 23 pounds less than indicated because of provisions for CFT's.

Figure

 122. (Sheet 2)