F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 36

 

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F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 36

 

 

T.O. GR1F16CJ1

34

F

If it appears that the aircraft will

depart a prepared surface above

normal taxi speed during an aborted

takeoff or a landing and goaround is

not possible, eject since breakup of

cockpit structure may occur. Retract

ing the LG to prevent departure from a

prepared surface is not recommended

since the MLG will probably not

retract symmetrically.

F

If remaining with an aircraft that will

depart a prepared surface, shut down

the engine, if feasible. This action

reduces the potential for fire, reduces

engine damage, and permits EPU

turnoff if an MLG WOW signal is lost.

WARNING AND CAUTION LIGHT

AND PILOT FAULT LIST ANALYSIS

Refer to figures 31, 32, and 33 for analysis and

amplification of warning and caution light and Pilot

Fault List procedures. Fault trees show interrela

tionships with examples of problem events and

corrective action.

FORMAT

The format of Emergency Procedures differs slightly

between the Checklist and the Flight Manual.

Procedures in the Checklist have been grouped by

malfunction category (engine, electrical, etc.) to

provide maximum inflight utility. In the Flight

Manual, procedures are listed by the phase of flight

in which the emergency may occur. In the Checklist,

some procedures are split into two independent

sidebyside series of steps and are separated by a

straight line; in the Flight Manual, these sideby

side steps appear in a continuous column and can be

identified by repeat numbering of steps following

conditional statements beginning with the word if.

Amplification following procedural steps in the

Flight Manual is repeated in the Checklist under the

heading Inoperative Equipment, Other Indications,

or Other Considerations. A thorough review of the

layout and content of the Checklist and Flight

Manual is recommended prior to inflight use.

T.O. GR1F16CJ1

35

GR1F-16CJ-1-0106X37

Warning Light Analysis

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

PROBABLE

MALFUNCTION

IN FIRE DETECT

SYSTEM

THROTTLE TO

MINIMUM PRAC-

TICAL THRUST

ENGINE FIRE

PERSISTS

Are there

other signs of fire?

(Visual, FTIT, OVERHEAT

Caution Light, Engine

Response, etc.)

YES

LAND AS SOON AS POSSIBLE

EJECT

NOTES:

Refer to:

GROUND EMERGENCIES.

GROUND EGRESS.

ENGINE FIRE.

EJECTION.

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

BELOW 10,000 FEET

MSL, <190 KNOTS

AND AT LEAST 250

FPM DESCENT

BELOW 10,000 FEET

MSL, <190 KNOTS

AND AT LEAST 250

FPM DESCENT

Are all

WHEELS down

lights green?

ONE OR

MORE

GREEN

LIGHTS

NOT ON

3 GREEN

LIGHTS

INCREASE AIRSPEED, DECREASE

SINK RATE, OR PLACE LG

HANDLE   DN

ABORT AIRCRAFT

TEF'S NOT FULLY

DOWN

TEF'S NOT FULLY

DOWN

AIR

GND

AIR

YES

NO

SEE B

SEE A

ENG FIRE

ENG FIRE

CONFIG

TO/LDG

CONFIG

TO/LDG

Engine compartment fire

Refer to ENGINE FIRE

NO

A.

For in-flight LG problems, refer to

LANDING EMERGENCIES

If TEF's do not extend, execute land-

ing using normal AOA (approximately

20 knots faster than normal)

Aircraft configuration wrong for

takeoff or landing

Any of the following:

1. LG not down and locked

2. TEF's not fully down

B.

LG/TEF'S NOT

DOWN *

ANY/ALL LG NOT

DOWN AND

LOCKED **

** NOTES:

LG warning horn

sounds.

LG Handle   DN

(Malfunction)

LG Handle   UP

(No Malfunction)

* NOTE:

LG warning horn sounds.

LG handle warning

light illuminates.

Figure 31.(Sheet 1)

T.O. GR1F16CJ1

36

GR1F-16CJ-1-1107X37

Warning Light Analysis

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

Is EPU

run light

on?

Is ELEC

SYS caution

light on?

Low pressure in one or both hydraulic

systems, low engine oil pressure, or low

oil pressure switch failure

Check pressure indicators to determine sys-

tem and condition

Refer to:

OIL SYSTEM MALFUNCTION

HYDRAULIC MALFUNCTIONS

CHECK OIL AND

HYD PRESS

INDICATORS

OIL PRESSURE

NORMAL

OIL PRESSURE

SWITCH FAILURE

MONITOR

OIL PRESSURE

INDICATOR

REFER TO

SYSTEM A

FAILURE

REFER TO

SYSTEM B

FAILURE

REFER TO DUAL

HYDRAULIC

FAILURE

PTO SHAFT

FAILURE

DUAL HYDRAULIC

FAILURE

SYSTEM A

HYDRAULIC

FAILURE

SYSTEM A

HYD PRESS

INDICATOR ONLY

BELOW 1000 PSI

ENGINE OIL

SYSTEM MAL-

FUNCTION, MINI-

MIZE THROTTLE

MOVEMENT.

LAND AS SOON

AS POSSIBLE

OIL PRESSURE

BELOW 15 PSI

SYSTEM B

HYD PRESS

INDICATOR ONLY

BELOW 1000 PSI

SYSTEM B

HYDRAULIC

FAILURE

REFER TO SYSTEM B

AND MAIN GENERATOR

FAILURE (PTO SHAFT)

NO

NO

YES

YES

OIL

HYD

EJECT

BOTH HYD PRESS

INDICATORS BE-

LOW 1000 PSI

WITH EPU SWITCH

IN NORM OR ON

TOTAL HYDRAULIC FAILURE

(EPU MAY STILL RUN AND

POWER THE EPU GENERATOR,

BUT EPU RUN LIGHT DOES

NOT ILLUMINATE UNLESS

SYSTEM A IS RESTORED)

PRESS

HYD/OIL

PRESS

HYD/OIL

REFER TO OIL

SYSTEM

MALFUNCTION

PW229

Figure 31.(Sheet 2)

T.O. GR1F16CJ1

37

GR1F16CJ10107A37

Warning Light Analysis

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

Is EPU

run light

on?

Is ELEC

SYS caution

light on?

Low pressure in one or both hydraulic

systems, low engine oil pressure, or low

oil pressure switch failure

Check pressure indicators to determine sys-

tem and condition

Refer to:

OIL SYSTEM MALFUNCTION

HYDRAULIC MALFUNCTIONS

CHECK OIL AND

HYD PRESS

INDICATORS

OIL PRESSURE

NORMAL

LOW OIL

PRESSURE

SWITCH

FAILURE

REFER TO

SYSTEM B

FAILURE

REFER TO DUAL

HYDRAULIC

FAILURE

PTO SHAFT

FAILURE

DUAL HYDRAULIC

FAILURE

SYSTEM A

HYDRAULIC

FAILURE

SYSTEM A

HYD PRESS

INDICATOR ONLY

BELOW 1000 PSI

ENGINE OIL

SYSTEM MAL-

FUNCTION, MINI-

MIZE THROTTLE

MOVEMENT.

LAND AS SOON

AS POSSIBLE

OIL PRESSURE

BELOW 15 PSI

SYSTEM B

HYD PRESS

INDICATOR ONLY

BELOW 1000 PSI

SYSTEM B

HYDRAULIC

FAILURE

REFER TO SYSTEM B

AND GENERATOR

FAILURE (PTO SHAFT)

NO

NO

YES

YES

OIL

HYD

MONITOR OIL

PRESSURE

INDICATOR

REFER TO

SYSTEM A

FAILURE

MONITOR NOZ

POS INDICATOR

EJECT

BOTH HYD PRESS

INDICATORS BE-

LOW 1000 PSI

WITH EPU SWITCH

IN NORM OR ON

TOTAL HYDRAULIC FAILURE

(EPU MAY STILL RUN AND

POWER THE EPU GENERATOR,

BUT EPU RUN LIGHT DOES

NOT ILLUMINATE UNLESS

SYSTEM A IS RESTORED)

PRESS

HYD/OIL

PRESS

HYD/OIL

REFER TO OIL

SYSTEM

MALFUNCTION

GE129

Figure 31.(Sheet 3)

T.O. GR1F16CJ1

38

GR1F-16CJ-1-0108X37

Warning Light Analysis

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

UP

DOWN

SEE A

SEE A

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

A.

B.

CHECK

WHEELS

DOWN

LIGHTS

SEE B

SEE A

Is canopy

handle up

or down?

CANOPY

NOT

SECURE

POSITION HANDLE

DOWN

CANOPY HOOKS

NOT FULLY

ENGAGED

ANY/ALL LG OR

LG DOORS NOT

FULLY UP AND

LOCKED

IN FLIGHT

Canopy hooks or lock not secure

Push handle down farther into

locked (outboard) position or if

on the ground, inform maintenance
Refer to CANOPY LOSS/PENE-

TRATION IN FLIGHT

Refer to LG FAILS TO RETRACT

Refer to LG FAILS TO EXTEND

LG or LG door not in position

commanded by LG handle

LG handle warning

light illuminated

A.

NONILLUMINATED LIGHT INDICATES

ASSOCIATED LG IS NOT DOWN AND

LOCKED (MAY ALSO HAVE LG WARN-

ING HORN AND TO/LDG CONFIG

WARNING LIGHT)

CANOPY

CANOPY

Figure 31.(Sheet 4)

T.O. GR1F16CJ1

Change 139

Warning Light Analysis

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

TF FAIL

TF system failure

Climb to a safe altitude. Refer to TF FAIL WARN

ING LIGHT

FLCS

One or more malfunctions

Note PFL(s) displayed and refer to PILOT

FAULT LIST - FLCS

DBU ON

FLCC operating with backup software 

program

Refer to DBU ON WARNING LIGHT

CANOPY

Partial pressure oxygen low

Refer to OBOGS MALFUNCTION 

       

, this

section

PX

III

CANOPY

OXY LOW

PX

III

BIT has detected a fault

section

OXY LOW

Regulator pressure below 5 psi

Flashing WARN symbol

WARN

One or more red glareshield warning

lights illuminated

Check for specific illuminated warning light

WARN

Reset by toggling WARN RESET switch on ICP

Flashing TRP FUEL and FUEL warning

symbols

A trapped

 

external fuel condition is de

tected

Reset FUEL by toggling WARN RESET

switch on ICP

FUEL

TRP FUEL

Check fuel tank quantities and refer to

TRAPPED EXTERNAL FUEL

Figure 31.(Sheet 5)

T.O. GR1F16CJ1

310

GR1F-16CJ-1-1109X37

Warning Light Analysis

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

ENGINE

ENGINE

ENGINE

ALTERNATOR

FAILURE

CHECK RPM AND

FTIT INDICATIONS

Is

RPM

abnormally

low?

Is

RPM

erroneously

zero?

Is

FTIT

abnormally

high?

ENGINE

FLAMEOUT

YES

NO

YES

NO

YES

NO

SEE A

SEE B

Check rpm and FTIT indications

Engine flameout

Engine alternator failure

Engine warning system failure or

RPM/FTIT indicator failure

Engine overtemperature

Place throttle to OFF and initiate airstart.

Refer to AIRSTARTS

Refer to ZERO RPM

Land as soon as possible

A.

B.

C.

Land as soon as practical

D.

ENGINE OVERTEMPERATURE

SEE C

SEE D

ENGINE WARNING SYSTEM

FAILURE OR RPM/FTIT

INDICATOR FAILURE

PW229

Figure 31.(Sheet 6)

T.O. GR1F16CJ1

311

GR1F-16CJ-1-0109A37

Warning Light Analysis

WARNING LIGHT

CAUSE

CORRECTIVE ACTION/REMARKS

ENGINE

ALTERNATOR

FAILURE

CHECK RPM AND

FTIT INDICATIONS

ENGINE OVERTEMPERATURE

Is

RPM

abnormally

low?

Is

RPM

erroneously

zero?

Is

FTIT

abnormally

high?

ENGINE

FLAMEOUT

YES

NO

YES

NO

YES

NO

SEE A

SEE B

Check rpm and FTIT indications

Engine flameout

Engine alternator failure

Engine overtemperature

Place throttle to OFF and initiate airstart.

Refer to AIRSTARTS

Refer to ZERO RPM

Land as soon as possible

A.

B.

C.

SEE C

Land as soon as practical

D.

SEE D

ENGINE

ENGINE

Engine warning system failure or

RPM/FTIT indicator failure

ENGINE WARNING SYSTEM

FAILURE OR RPM/FTIT

INDICATOR FAILURE

GE129

Figure 31.(Sheet 7)

 

 

 

 

 

 

 

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