F16C/D (BLOCKS 50 AND 52+). FLIGHT MANUAL (15 OCTOBER 2002) - page 42

T.O. GR1F16CJ1

351

2.

Land as soon as practical.

3.

Refer to ACTIVATED EPU/HYDRAZINE

LEAK, this section.

If EPU runs abnormally:

4.

EPU switch-OFF, then NORM.

5.

Land as soon as possible.

6.

Refer to ACTIVATED EPU/HYDRAZINE

LEAK, this section.

Prior to shutdown:

7.

Loose items-Secure.

8.

Canopy-Open.

Emergency Power Distribution

Refer to figure 36.

T.O. GR1F16CJ1

352

Emergency Power Distribution

MAIN GENERATOR FAILED

BUS ASSIGNMENT

SYSTEM

INOPERATIVE EQUIPMENT

NONESS AC

NACELLE

NONESS DC

NO. 1

NO. 2

NO. 1

NO. 2

ENGINE

EMSC

129

GE

X

NAV/COMM

            VHF Radio

PX

II

*

FUEL

Pumps 1, 2, 4 & 5

X

*

            CFT Pumps

PX

III

X

FUEL/OIL HOT Caution Light

(oil hot signal)

129

GE

X

STORES MGT

AIM120

***

Stations 3, 5 & 7-EO, RadarGuided

Weapons, ECM Pods

**

Stations 4 & 6-EO, RadarGuided Weapons

X

AVIONICS

DTU

X

             FCC

PX

II

X

FCR

Radar

*

             GPS

PX

II

X

TWS

X

X

LIGHTS

Flood Console

X

Flood Instrument

X

Formation

X

Taxi

X

OTHER

                 ASIU

PX

III

D

*

ECM Control

*

Halon Heater

X

            HMCS

PX

III

X

Inlet Strut Heater

X

            INS Heater

PX

II

X

Nacelle Ejector Shutoff

X

Seat Adjustment

X

Total Temperature Probe Heater

X

NOTE:

Equipment on nonessential ac bus No. 1 or nonessential ac bus No. 2 may be functional with MAIN GEN

light on (bus contactor failure).

*Aft equipment bay nonessential dc bus.

**Overcurrent sensing contactors.

***Nacelle nonessential ac bus.

Figure 36.(Sheet 1)

T.O. GR1F16CJ1

353

Emergency Power Distribution

MAIN AND STANDBY GENERATORS FAILED

(All equipment from sheet 1 plus the following:)

SYSTEM

INOPERATIVE EQUIPMENT

BUS ASSIGNMENT

SYSTEM

INOPERATIVE EQUIPMENT

ESS AC

ESS DC

FUEL

Pump 3

X

X

Tank Inerting

X

STORES MGT

AIM9

*

Arm and Release Power-Stations 1 Thru 9

X

AVIONICS

Radar Altimeter

X

MFD's

X

PFLD

*

OTHER

Air Data Probe Heater (fuselage)

*

                   ASHM

PX

III

D

X

Battery Charger

X

            Data Link

PX

III

X

NOTE

:

Equipment on this sheet may operate if MAIN GEN light was caused by bus contactor failure at nonessen

tial bus No. 1.

*Nacelle essential ac bus.

Figure 36.(Sheet 2)

T.O. GR1F16CJ1

354

Emergency Power Distribution

MAIN, STANDBY, AND EPU GENERATORS FAILED

(All equipment from sheets 1 and 2 plus the following:)

BUS ASSIGNMENT

SYSTEM

INOPERATIVE EQUIPMENT

EMER AC

EMER DC

NO. 1

NO. 2

NO. 1

NO. 2

ENGINE

Engine ANTI ICE Switch

X

ENGINE FAULT Caution Light

X

Engine Ice Detector

X

Fire/Overheat Detect and Test

X

HYD PRESS Indicators

X

Low Energy Ignition Power

129

GE

X

NOZ POS Indicator

X

OIL Pressure Indicator

X

FLIGHT

ADI

X

INSTRUMENT

Altimeter (ELECT)

X

AOA Indexer

X

AOA Indicator

X

HSI

X

Turn Needle

X

INSTR MODE Select Switch

X

VVI

X

FUEL

Automatic Forward Fuel Transfer

X

FUEL FLOW Indicator

X

FUEL LOW Caution Lights

X

FUEL Quantity Indicator

X

FLIGHT

Autopilot

X

CONTROLS

DBU ON Warning Light (branches A & B)

X

DBU ON Warning Light (branches C & D)

X

FLCS FAULT Caution Light

(branches A & B)

C DF

X

FLCS FAULT Caution Light

(branches C & D)

DR

X

FLCS RESET Switch (branches A & B)

X

FLCS RESET Switch (branches C & D)

X

FLCS Power Source (branches A & B)

X

FLCS Power Source (branches C & D)

X

FLCS Warning Light (branches A & B)

X

FLCS Warning Light (branches C & D)

X

Figure 36.(Sheet 3)

T.O. GR1F16CJ1

355

Emergency Power Distribution

MAIN, STANDBY, AND EPU GENERATORS FAILED-CONT

(All equipment from sheets 1, 2, and 3 plus the following:)

BUS ASSIGNMENT

SYSTEM

INOPERATIVE EQUIPMENT

EMER AC

EMER DC

NO. 1

NO. 2

NO. 1

NO. 2

FLIGHT

CONTROLS

LEF's

X

CONTROLS

(cont)

Speedbrakes

X

(cont)

Stick Trim

X

NAV/COMM

            EGI

PX

III

X

IFF

X

            INS

PX

II

X

X

ILS

X

TACAN

X

X

            VHF Radio

PX

III

X

STORES MGT

ALT REL Button

C

X

CIU*

X

X

Chaff Dispenser

X

Gun

X

X

EMER JETT Button*

X

X

MASTER ARM Switch

X

MSL STEP Switch

X

NUCLEAR CONSENT Switch

X

STORES CONFIG Caution Light

X

WPN REL Button

C DF

X

WPN REL Button

DR

X

AVIONICS

CADC

X

CADC Caution Light

X

HUD

X

HUD/CTVS

X

ICP/IKP

X

MFD Video Control

X

            MMC*

PX

III

X

X

X

X

Upfront Controls

X

X

*Indicates redundancy.

Figure 36.(Sheet 4)

T.O. GR1F16CJ1

356

Emergency Power Distribution

MAIN, STANDBY, AND EPU GENERATORS FAILED-CONT

(All equipment from sheets 1, 2, 3, and 4 plus the following)

BUS ASSIGNMENT

SYSTEM

INOPERATIVE EQUIPMENT

EMER AC

EMER DC

NO. 1

NO. 2

NO. 1

NO. 2

LIGHTS

ANTICOLLISION Strobe

X

AR (flood)

X

AR (slipway)

X

Landing

X

LANDING/TAXI/External Switches

X

MAL & IND LTS TEST/BRT DIM

X

POSITION

X

PRIMARY CONSOLES

X

PRIMARY INST PNL

X

LG/NWS/

BRAKES

LG Hydraulic Isolation

X

BRAKES

LG Sequence (doors)

X

LG UPDN Command

X

NWS

X

WHEELS Down Lights

X

OTHER

Air Data Probe Heater (nose)

X

AOA Probe Heaters

X

AR System

X

AVTR/CTVS

X

CABIN PRESS Caution Light

X

CAMERA/GUN Trigger

X

Cockpit Pressure Dump Capability

X

Cockpit Temperature Control

X

Engine Bleed Air Valves (close capability)

X

EQUIP HOT Caution Light

X

INLET ICING Caution Light

X

            LIQUID OXYGEN Quantity

Indicator

C DF

PX

II

X

Figure 36.(Sheet 5)

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357

Emergency Power Distribution

MAIN, STANDBY, AND EPU GENERATORS FAILED-CONT

(All equipment from sheets 1, 2, 3, 4, and 5 plus the following)

BUS ASSIGNMENT

SYSTEM

INOPERATIVE EQUIPMENT

EMER AC

EMER DC

NO. 1

NO. 2

NO. 1

NO. 2

OTHER -

continued

             OXY LOW Caution Light

PX

II

X

             OXY LOW Warning Light

PX

III

X

             OBOGS Caution Light

PX

III

X

             OBOGS Concentrator

PX

III

X

             OBOGS Monitor

PX

III

X

Probe Heat Monitor

X

PROBE HEAT Switch

X

SEAT NOT ARMED Caution Light

X

Figure 36.(Sheet 6)

T.O. GR1F16CJ1

358

Emergency Power Distribution

OPERATING EQUIPMENT-MAIN, STANDBY, AND EPU GENERATORS FAILED

BUS ASSIGNMENT

SYSTEM

OPERATING EQUIPMENT

BATTERY

NO. 1

BATTERY

NO. 2

ENGINE

             EDU

PW

229

X

             Electrical Throttle Position

129

GE

X

PRI (no supersonic stall protection)*
PRI/SEC Transfer Circuit*

INSTRUMENTS Airspeed/Mach Indicator*

Altimeter (PNEU)*
FTIT Indicator

X

RPM Indicator

X

SAI

X

FUEL

External Fuel Transfer*
FUEL MASTER Switch

X

FFP*

FLIGHT 

CONTROLS

Functional (except LEF's, speedbrakes, autopilot, and

stick trim)*

NAV/COMM

Intercom

X

Magnetic Compass*
UHF Radio

X

LIGHTS

Spotlights

X

Utility Light

X

LG/NWS/

BRAKES

Alternate LG Extension*

BRAKES

Antiskid/Channel 1 Brakes

X

Antiskid/Channel 2 Brakes

X

LG Uplock/Downlock

X

MLG WOW (branches A & B)

X

MLG WOW (branches C & D)

X

NLG WOW (branches A & B)

X

NLG WOW (branches C & D)

X

Parking Brake

X

*Indicates items that do not require power through the battery buses.

Figure 36.(Sheet 7)