Content .. 53 54 55 56 ..

F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 55

T.O. GR1F16CJ1

Instrument Markings

GR1F-16CJ-1-0129X37

FTIT

RPM

HYDRAULIC PRESSURE

OIL PRESSURE

935 C ENGINE START

108% MAXIMUM

3250 PSI MAXIMUM

2850-3250 PSI NORMAL

65 PSI MAXIMUM

15 PSI MINIMUM

ENGINE F110-GE-129

980 C MAXIMUM

Figure 51. (Sheet 2)

T.O. GR1F16CJ1

Engine Limitations

ENGINE F100PW229

GROUND

CONDITION

FTIT

RPM

OIL PSI

REMARKS

START

800

During cold start, oil pressure may be 100 psi for up to 1 minute

IDLE

625

15 (min)

Maximum FTIT in SEC is 650

MIL/AB

1070

3095

At MIL and above, oil pressure must increase 15 psi minimum above

IDLE oil pressure. Use transient rpm limit for takeoff

TRANSIENT

1090

3095

Time above 1070

is limited to 10 seconds

FLUCTUA

TION

5 IDLE

Must remain within steadystate limits. Inphase fluctuations of more

than one instrument or fluctuations accompanied by thrust surges indi

cate engine control problems Nozzle fluctuations limited to

2% at

above

IDLE

cate engine control problems. Nozzle fluctuations limited to

2% at

and above MIL. Fluctuations not permitted below MIL

IN FLIGHT

CONDITION

FTIT

RPM

OIL PSI

REMARKS

AIRSTART

870

IDLE

15 (min)

MIL/AB

1070

3095

Oil pressure must increase as rpm increases. Use transient rpm limit

with LG handle DN and for 3 minutes after LG handle is placed UP

TRANSIENT

1090

3095

Time above 1070

is limited to 10 seconds

FLUCTUA

TION

5 IDLE

Same as ground operation. Zero oil pressure is allowable for periods up

to 1 minute during flight at less than +1g

above

IDLE

Figure 52.(Sheet 1)

T.O. GR1F16CJ1

Engine Limitations

ENGINE F110GE129

GROUND

CONDITION

FTIT

RPM

OIL PSI

REMARKS

START

935

During cold start, oil pressure may be 100 psi for up to 2 minutes

IDLE

650

15 (min)

MIL/AB

980

108

2565

At MIL and above, oil pressure must increase 10 PSI minimum above

IDLE oil pressure

TRANSIENT

980

109

2565

FLUCTUATION

Must remain within steadystate limits. Nozzle fluctuations limited to

IN FLIGHT

CONDITION

FTIT

RPM

OIL PSI

REMARKS

AIRSTART

935

IDLE

15 (min)

MIL/AB

980

108

2565

Oil pressure must increase as rpm increases

TRANSIENT

980

109

2565

FLUCTUATION

Must remain within steadystate limits. Zero oil pressure is allowable

for periods up to 1 minute during flight at less than +1g

Figure 52. (Sheet 2)

T.O. GR1F16CJ1

510

1F-16X-1-4018X

MINIMIZE THROTTLE

MOVEMENTS IN SEC

TITUDE 1000 FEET

0.0

0.4

0.8

1.2

1.6

2.0

MACH NUMBER

0.2

0.6

1.0

1.4

1.8

2.2

Engine

NOTES:

Transfers from SEC to PRI should be performed below 40,000 feet MSL and subsonic with the throttle at

MIL or below.

ENGINE F100-PW-229

UNRESTRICTED THROTTLE

MOVEMENT IN SEC

Maximum operating airspeed is 800 knots from sea level to 30,000 feet MSL. Above 30,000 feet MSL, the

aircraft is limited to 2.05 mach.

DO NOT RETARD

THROTTLE BELOW

MIL UNTIL SUB-

SONIC IN SEC

Operational Envelope

Figure 53.(Sheet 1)

T.O. GR1F16CJ1

511

TITUDE 1000 FEET

0.0

MACH NUMBER

1F-16X-1-4019X

0.4

0.8

1.2

1.6

2.0

0.2

0.6

1.0

1.4

1.8

2.2

UNRESTRICTED THROTTLE

MOVEMENT IN SEC

Engine Operational Envelope

ENGINE F110-GE-129

DO NOT RETARD

THROTTLE BELOW

MIL UNTIL SUB-

SONIC IN SEC

Figure 53. (Sheet 2)

T.O. GR1F16CJ1

512

Jet Fuel Starter Limits

CONDITION

LIMITS

Normal Ground Operation

* Continuous motoring of the engine shall not exceed 4 minutes. After 4 minutes of con

tinuous motoring, a normal engine start may be initiated after 5 minutes of cooling

Normal Ground Operation

A minimum wait of 1 minute is required after each JFS start attempt to allow fuel

drainage from the JFS

Hot Start of Engine

Motor until FTIT is below 200

Airstart/In Flight

Below 20,000 feet MSL and 400 knots. 3minute maximum run time when the engine

is operating satisfactorily above 60 percent rpm; otherwise, unlimited

*Motoring is defined as JFS rotating the engine at 22 percent rpm,25 percent rpm

minimum with the throttle in OFF.

NOTES:

OAT between 20

F (-6

C) and 100

F (38

C). A minimum brake/JFS accumulator pressure of 3000 psi is required

for START 1 and 2800 psi is required for START 2.

OAT between -25

F (-32

C) and 20

F (-6

C) or OAT above 100

F (38

C). START 2 and a minimum brake/JFS accu

mulator pressure of 2800 psi are required.

OAT below -25

F (-32

C). START 2 and a minimum brake/JFS accumulator pressure of 3200 psi are required.

If one brake JFS accumulator is depleted, verify a minimum pressure of 3000 psi in the remaining brake/JFS accu

mulator before attempting START 2.

129

229

Figure

54.

T.O. GR1F16CJ1

Change 1513

Cable/Net Arrestment Limits

Compatible Cable Systems With Established Aircraft Limits

BAK6

BAK9

BAK12 (Standard, Extended, and Dual)

BAK13 (Navy designation is E28)

BAK14

BAK15 (NI) (Net barrier with cable for hook)

MAAS

*44B2L

ROUTINE ARRESTMENT

A planned event. Operational conditions are such that each landing requires arrestment. Such

operational conditions include operating from highways or from runways that are too short for

normal landings. The standard factor of safety is used to determine the maximum engagement

speed.

LIMITS - 150 knots for GW less than/equal to 42,300 pounds, 130 knots for GW greater

than 42,300 pounds, (*156 knots).

LIMITS - 146 knots (*160 knots).

EMERGENCY ARRESTMENT

An unplanned event. A reduced factor of safety is accepted and the corresponding maximum en

gagement speed is slightly higher than for a routine arrestment. With a ground level ejection capa

bility, a reduced factor of safety for the arrestment is possible since the pilot can still eject if the

arrestment fails.

LIMITS - 160 knots for GW less than/equal to 42,300 pounds, 140 knots for GW greater

than 42,300 pounds, (*171 knots).

LIMITS - 160 knots (*174 knots).

III

Compatible Cable Systems Without Established Aircraft Limits

Use of arresting systems without established aircraft limits may result

in failure of the hook, hook backup structure, or nose landing gear.

BLISS 500S6

TAGS BLISS 500S6B Transportable

44B3H/SP/WR

MAGS 44B3H/SP/WR Mobile

RHAG MK1

RHAG MK2

PUAG

PAAG

PIV/BAK12 Portable

Figure 55.(Sheet 1)

T.O. GR1F16CJ1

514

Cable/Net Arrestment Limits

Compatible Strut Engagement/Cable Systems Without Established Aircraft Limits

Use of arresting systems without established aircraft limits may result

in failure of the hook, hook backup structure, or nose landing gear.

MA1A Modified

MA1A/E5

MA1A/BAK9

MA1A/BAK12

NOTE

Attempting to engage an unmodified (nonhook capable) MA1A will most

likely be unsuccessful.

Compatible Net Barrier Systems

BAK15

SAFEBAR (Safeland Barrier)

Stanchions

61QSII

61QSIIM

MK6

NOTE

The above stanchions can be rigged with the following nets: HP30, HP40,

MEN241, MEN301, 24, 30, or 40. In addition, they will be associated with

the following energy absorbers: Chain (E5), BAK9, BAK12, BAK13,

34B, 44B, 500S, BEFAB 6:3, BEFAB 21:2, and BEFAB 24:4.

Other Net Systems

ARZ30/40

BEFAB 21:2/MK VI1 stanchion

BEFAB 6:3/MK VI1 stanchion

MK12A

RAF TYPE A

RAF TYPE B

Figure 55.(Sheet 2)

Content .. 53 54 55 56 ..

F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 55

F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 55