Eaws Fixed Wing Reconnaissance

Front 1

DESCRIBE THE PHYSICAL CHARACTERISTICS OF THE EP-3E AIRCRAFT

Back 1

4 ENGINE, LOW-WING, ELECTRONIC WARFARE AND RECONNAISSANCE A/C UTILIZING STATE OF THE ART SURVEILLANCE. 4 ALLISON T56-A-14 TURBOPROP ENGINES POWER IT. 19 CREW STATIONS, 24 DITCHING
99' 8" LONG, 105'11" WING SPAN, 34'3" HIGH

Front 2

WHAT IS THE EP-3E TOTAL FUEL CAPACITY?

Back 2

9,200 US GALLONS

Front 3

STATE THE PURPOSE OF THE AIRCREW POSITION:
MISSION COMMANDER
(EWAC/MC)

Back 3

RESPONSIBLE FOR ALL PHASES OF MISSION EXCEPT SAFETY

Front 4

STATE THE PURPOSE OF THE AIRCREW POSITION:
ELECTRONIC WARFARE A/C COMMANDER (EWAC)

Back 4

SAFETY/SURVIVAL EQUIPTMENT/PROCEDURES

Front 5

STATE THE PURPOSE OF THE AIRCREW POSITION:
CO-PILOT (2P)

Back 5

BACKUP FOR PILOT, COMM DUTY, CHECKLISTS

Front 6

STATE THE PURPOSE OF THE AIRCREW POSITION:
FLIGHT ENGINEER (FE)

Back 6

EXTERIOR/INTERRIOR CHECKS, MONITOR ENGINES/SYSTEMS/INDICATORS

Front 7

STATE THE PURPOSE OF THE AIRCREW POSITION:
NAVIGATOR/COMMUNICATOR (NAV/COM)

Back 7

DRAFTS/AUTHENTICATES/ENCRYPTS/TRANSMITS MESSAGES

Front 8

STATE THE PURPOSE OF THE AIRCREW POSITION:
SECURE COMMUNICATIONS OPERATOR (SECURE COMM)

Back 8

ENSURES COMM'S ARE RAPID/EFFECTIVE AND RIGHT

Front 9

STATE THE PURPOSE OF THE AIRCREW POSITION:
SENIOR EVALUATOR (SEVAL)

Back 9

MISSION BRIEF, FAMILIAR WITH OBJECTIVES OF MISSION

Front 10

STATE THE PURPOSE OF THE AIRCREW POSITION:
TACTICAL EVALUATOR (EVAL)

Back 10

DIRECTS ESM OPERATORS

Front 11

STATE THE PURPOSE OF THE AIRCREW POSITION:
SPECIAL EVALUATOR

Back 11

DIRECTS SPECIAL OPERATORS

Front 12

STATE THE PURPOSE OF THE AIRCREW POSITION:
RADAR/ESM OPERATOR (BIG LOOK)

Back 12

DETECTING/IDENTIFING SIGNIFICANT DATE

Front 13

STATE THE PURPOSE OF THE AIRCREW POSITION:
LABORATORY OPERATOR (LABOP)

Back 13

DETECTING/ IDENTIFING SIGNIFICANT DATA

Front 14

STATE THE PURPOSE OF THE AIRCREW POSITION:
ESM OPERATOR (EWOP)

Back 14

DETCTING/IDENTIFING DATA

Front 15

STATE THE PURPOSE OF THE AIRCREW POSITION:
SPECIAL OPERATOR SUPERVISOR

Back 15

MONITORS ACTIVITIES OF SPECIAL OPERATORS

Front 16

STATE THE PURPOSE OF THE AIRCREW POSITION:
SPECIAL OPERATOR

Back 16

DETECTING/IDENTIFING DATA

Front 17

STATE THE PURPOSE OF THE AIRCREW POSITION:
RECORD

Back 17

DIGITAL RECORDINGS

Front 18

STATE THE PURPOSE OF THE AIRCREW POSITION:
SCIENCE AND TECHNOLOGY OPERATOR (S&T)

Back 18

DETECTING/IDENTIFING DATA, PROTOTYPE EQUIPTMENT

Front 19

STATE THE PURPOSE OF THE AIRCREW POSITION:
INFLIGHT TECH (IFT)

Back 19

MAINTAINING OPERATION CAPABILITIES, REPAIR

Front 20

STATE THE PURPOSE OF THE AIRCREW POSITION:
OBSERVER

Back 20

REPORTS TACTICAL INFO TO SEVAL, PILOT, CO-PILOT

Front 21

STATE THE MAXIMUM NUMBER OF DITCHING STATIONS IN THE EP-3E

Back 21

24

Front 22

STATE THE PURPOSE OF ENGINE LOITER OPERATIONS

Back 22

PROVIDE SUBSTANTIAL REDUCTIN IN THE FUEL FLOW REQUIRED...

Front 23

DISCUSS THE DANGER ZONES OF THE EP-3

Back 23

PROP ARC, JET BLAST, COMPRESSOR/TURBINE AREAS, APU/AIR MULTIPLIER, RADAR RADIATIN AREA NOISE HAZARD, WING/FLAP

Front 24

DISCUSS THE RESPONSIBILITIES OF THE TRAINING DEPARTMENT

Back 24

SUPERVISE OR CONDUCT ALL SQUADRON TRAINING, COORDINAETE GMT AND PROFESSIONAL TRAINING, OPERATIONAL TRAINING TO ACHIEVE HIGH LEVEL OF MISSION READINESS

Front 25

MOPP

Back 25

MISSION ORIENTED PROTECTIVE POSTURE....
4 LEVELS THAT REQUIRE USE OF CBR GEAR

Front 26

MAST TRAINER

Back 26

MISSION AVIONICS SYSTEMS TRAINER....
COMPUTER SIMULATED TRAINER FOR OPERATORS

Front 27

PRE-DEPLOYMENT TRAINING

Back 27

SITE SPECIFIC SO AIRCREW KNOWS WHAT TO EXPECT

Front 28

MTIP

Back 28

MAINTENANCE TRAINING IMPROVEMENT PROGRAM....
TRAIN AND QUALIFY PERSONNEL

Front 29

AIRCREW COORDINATIN TRAINING (ACT)

Back 29

COMMUNICATIONS TRAINING FOR AIRCREW

Front 30

REQUIRED OPERATIONAL CAPABILITIES (ROC)

Back 30

MINIMUM MANNING LEVELS TO ACCOMPLISH THE MISSION

Front 31

EXPLAIN THE PURPOSE OF THE SQUADRON PLANNING BOARD FOR TRAINING (PBFT)

Back 31

CO'S RESPONSIBILITY TO DEVELOP UNITS TRAINING PROGRAM FOR WELL QUALIFIED PERSONNEL

Front 32

STATE THE HIGHEST AND LOWEST LEVELS OF READINESS

Back 32

HIGH-LOW
T1,T2,T3,T4
R1,R2,R3,R4

Front 33

STATE THE PURPOSE OF THE FOLLOWING FLIGHT CREW PROGRESS BOARD:
OFFICER PROFESSIONAL DEVELOPMENT BOARD (OPDB)

Back 33

TRACK DEVELOPMENT OF AIRCREW O'S

Front 34

STATE THE PURPOSE OF THE FOLLOWING FLIGHT CREW PROGRESS BOARD:
ENLISTED AIRCREW PROFESSIONAL DEVELOPMENT BOARD (EAPDB)

Back 34

REVIEW AIRCREW WHO FAIL TO QUALIFY WITHIN EXPECTED TIME LIMITS

Front 35

STATE THE PURPOSE OF THE FOLLOWING FLIGHT CREW PROGRESS BOARD:
MISSION BOARD (MB)

Back 35

DETERMINE PROGRESS AND NOTE DEFIENCIES

Front 36

STATE THE PURPOSE OF THE FOLLOWING FLIGHT CREW PROGRESS BOARD:
TRAINING REVIEW BOARD (TRB)

Back 36

USED TO IDENTIFY AIRCREW MEMBERS DEFICIENCIES, RECOMMEND REMEDIAL TRAINING

Front 37

WHAT ARE YOUR COMMANDS AREAS OF RESPONSIBILITY (AORS)

Back 37

3RD FLEET, 5TH FLEET, 7TH FLEET

Front 38

DISCUSS THE RESPONSIBILITIES OF THE OPERATIONS DEPARTMENT

Back 38

SCHEDULES, MANAGES AND EMPLOYS THE SQUADRONS A/C AND AIRCREW TO ACCOMPLISH MISSIONS

Front 39

DEFINE THE DUTIES, RESPONSIBILITIES AND AUTHORITY OF THE NATOPS DEPARTMENT

Back 39

IDENTIFY AND ELIMINATE HAZARDS, STANDARDIZE TRAINING AND MIN FLIGHT STANDARDS ARE MET THROUGH NATOPS, ENSURE PROGRAMS COMPLY WITH DIRECTIVES

Front 40

DESCRIBE THE BASIC PURPOSE OF THE FOLLOWING COMMON FLIGHTS RELATED TO AIRCRAFT FLIGHT PROFICIENCY:
INSTRUMENT TRAINING

Back 40

UPTILIZATION OF A/C INSTRUMENTS TO MAINTAIN PROFICENCY

Front 41

DESCRIBE THE BASIC PURPOSE OF THE FOLLOWING COMMON FLIGHTS RELATED TO AIRCRAFT FLIGHT PROFICIENCY:
DEDICATED FIELD WORK (DFW)

Back 41

MAINTAIN DAY LANDINGS, NIGHT LANDINGS, EMERGENCY LANDINGS AND TOUCH AND GO'S

Front 42

DESCRIBE THE BASIC PURPOSE OF THE FOLLOWING COMMON FLIGHTS RELATED TO AIRCRAFT FLIGHT PROFICIENCY:
NATOPS INSTRUMENT EVALUATION

Back 42

FAA AND NAVY ANNUAL CHECKS FOR PILOTS

Front 43

CONDITIONS OF FLIGHT

Back 43

1. EVASION/RIGGING
2.NORMAL FLIGHT
3. EQUIPTMENT CHECK
4. A/C INSPECTION//INTEGRITY CHECK
5. TAKE OFF/LANDING

Front 44

HSU

Back 44

HYDRAULIC SERVICE CENTER

Front 45

HSU

Back 45

HYDRAULIC SERVICE UNIT

Front 46

MLG

Back 46

MAIN LANDING GEAR

Front 47

AVGFE

Back 47

AVIATION GAS FREE ENGINEERING

Front 48

DISCUSS THE CORROSION PRONE AREAS OF THE EP-3E A/C.

Back 48

ALONG SEEMS OF ALLUMINUM ALLOY STRUCTURES, BOX BEAM SKIN CENTROID RISERS, CADMIUM PLATED STEEL FASTNERS, UNPAINTED SURFACES, CHIPPED PAINT, EXT...

Front 49

DISCUSS THE TYPE OF CONSTRUCTION USED IN THE EP-3E AIRCRAFT

Back 49

ALL METAL, WING CONSISTS OF A BOX BEAM COMPRISING TWO MAIN SPARS, FUSELAGE IS SEMIMONOCOQUE CONSTRUCTION CONSISTINCY OF SKINS, STRINGERS, LONGERONS, BULHEADS OR FRAMES

Front 50

DESCRIBE THE TYPE OF LANDING GEAR UTILIZED ON THE EP-3E AIRCRAFT

Back 50

2 WHEELS, FORWARD RETRACTING STRUTS, DESIGNED TO FREE FALL AND LOCK INTO PLACE IN THE EVENT OF LOSS OF HYDRAULICS.

Front 51

QEC

Back 51

QUICK ENGINE CHANGE

Front 52

RPM

Back 52

ROTATIONS PER MINUTE/REVOLUTIONS PER MINUTE

Front 53

APU

Back 53

AUXILLARY POWER UNIT

Front 54

EDC

Back 54

ENGINE DRIVEN COMPRESSOR

Front 55

TIT

Back 55

TURBINE INLET TEMPERATURE

Front 56

SHP

Back 56

SHAFT HORSEPOWER

Front 57

STATE THE TYPE AND MODEL OF THE EP3E

Back 57

ALLISON T-56-A-14 TURBOPROP

Front 58

DISCUSS THE PURPOSE OF THE CONSTANT SPEED PROP

Back 58

MAINTAINS SELECTED RPM BY TURNING PROPS TO A LOWER ANGLE

Front 59

DISCUSS THE EP-E3 AIRCRAFT FUELING METHODS

Back 59

CENTER POINT FUELING DESIGNED TO ACCEPT 600 GALLONS OF FUEL PER MINUTE FROM 2 TRUCKS AT 55 PSI
OVER WING GRAVITY FEED, THREW OVER WING GRAVITY FILLER WELLS IN EACH MAIN TANK

Front 60

ADF

Back 60

AUTOMATIC DIRECTION FINDING

Front 61

GPS

Back 61

GLOBAL POSITIONING SYSTEM

Front 62

ESM

Back 62

ELECTRONIC SUPPORT MEASURES

Front 63

SSIP

Back 63

SENSOR SYSTEM IMPROVEMENT PROGRAM

Front 64

VOR

Back 64

VHF OMNIDIRECTIONAL RANGING

Front 65

CRT

Back 65

CATHODE RAY TUBE

Front 66

DCMS

Back 66

DIGITAL COMMUNICATIONS MANAGEMENT SYSTEM

Front 67

RADALT

Back 67

RADAR ALTIMETER

Front 68

ESD

Back 68

ELECTROSTATIC SENSITIVE DIVICE

Front 69

DISCUSS THE TWO SYSTEMS THAT COMPRISE MISSION AVIONICS

Back 69

ESM AND SPECIAL

Front 70

DISCUSS THE FOUR RADIO COMMUNICATION SETS USED ON THE EP-3E AIRCRAFT

Back 70

ARC-94 HF'S, URR-74 (V)2 HF'S, ARC-182 VHF/UHF, ARC-187.

Front 71

AFCS

Back 71

AUTOMATIC FLIGHT CONTROL SYSTEM

Front 72

MELC

Back 72

MAIN ELECTRICAL LOAD CENTER

Front 73

AOA

Back 73

ANGLE OF ATTACK

Front 74

INS

Back 74

INERTIAL NAVIGATION

Front 75

DISCUSS THE ELECTRICAL POWER SUPPLY SYSTEM

Back 75

POWER IS SUPPLIED BY 3 ENGINE DRIVEN DRIVEN GENERATORS (90 KVA) AS WELL AS A 60KVA APU, ADDITIONALLY A 24 VOLT 31 AMP BATTERY FOR DC POWER, THE GENERATOS SUPPLY 120 VOLT, 3 PHASE POWER @ 400 HZ

Front 76

LPP

Back 76

LIVE PERSERVER PERSONAL

Front 77

LPA

Back 77

LIVE PRESERVER ASSEMBLY

Front 78

SV-2

Back 78

SURVIVAL VEST

Front 79

EDC

Back 79

ENGINE DRIVEN COMPRESSOR

Front 80

HRD

Back 80

HIGH RATE OF DISCHARGE

Front 81

CAD

Back 81

CARTRIDGE ACTUATED DEVICE

Front 82

DISCUSS THE PURPOSE OF AIRCRAFT CABIN PRESSURIZATOIN AND AIR CONDITIONING

Back 82

PROVIDES ENVIRONMENT CONTROL AND ELECTRONIC COOLING IN FLIGHT AND ON THE GROUND

Front 83

DISCUSS THE PURPOSE OF AIRCRAFT OXYGEN SYSTEMS

Back 83

SUPPLY 3 AIRCREWMEN 3.5 HOURS OF OXYGEN AT 25,000FT. 3 PORTABLE OXYGEN BOTTLES THAT WILL SUPPLY 100% OXYGEN FOR 22 MINUTES, 18 SOLID STATE OXYGEN PACKS THAT PROVIDE 20 MINUTES OF OXYGEN

Front 84

Aircraft structure:
what is its function, where is it located
~Fuselage~

Back 84

main structure or body of aircraft which everything is attached. provides room for crew, passengers, cargo and accessories

Front 85

Aircraft structure:
what is its function, where is it located
~Empennage

Back 85

Stabilizing surface of a/c. Consists of vertical and horizontal airfoils

Front 86

Aircraft structure:
what is its function, where is it located
~Wing~

Back 86

develop lift when they are moved through the air

Front 87

Flight controls:
what is its function, where is it located
~Flaps~

Back 87

high lift, fowler type, increase wing area, provide lift

Front 88

Flight controls:
what is its function, where is it located
~ailerons

Back 88

Provide roll

Front 89

Flight controls:
what is its function, where is it located
~rudder

Back 89

Vertical stab, provide yaw

Front 90

Flight controls:
what is its function, where is it located
~Elevators~

Back 90

horizontal stab, provide pitch

Front 91

Flight controls:
what is its function, where is it located
~Trim Tab~

Back 91

ailerons, elevators and rudder, used to newtralize the a/c movement, controls located in the center control pedestal in flight station

Front 92

Hydraulics:
what is its function, where is it located
~Pumps~

Back 92

funcion of the a/c. system #1 is powered by 2 motor driven hyd. pumps who's output is made available to every hydraulically operated part. 1b is powered by DC and used primarily for charging the brake accumilator. System #2 is powered by one motor driven pump and used to assist in the operation of the wing flaps, radome, aierons, rudder and elevator booster units. Located in the HSC.

Front 93

Hydraulics:
what is its function, where is it located
~Resevoirs~

Back 93

Each system has its own resevoir. #1 has a capacity of 5.6 gallos, #2 has a 1 gallon capacity

Front 94

Hydraulics:
what is its function, where is it located
~booster assemblies~

Back 94

three booster assemblies which assist with a/c control movement. the aileron boost package is located in the HSC. The rudder, located in the aft fuselage, elevator, aft fuselage

Front 95

Airframe Components:
~Forward Radome~

Back 95

houses color weather radar in nose of A/c

Front 96

Airframe Components:
~aft radome

Back 96

Houses high band radar antenna, located on the bottom of the a/c aft the wings

Front 97

Airframe Components:
~upper canoe

Back 97

Houses various antennas located on the top middle to aft of the wings

Front 98

Airframe Components:
~lower canoe

Back 98

Houses varoius anntennas, located on the bottom of a/c aft of the nose wheel well

Front 99

What are the precautions associated with pressurized hydraulic components?

Back 99

use extreme caution when troubleshooting hydraulic systems to avoid accidental injection of fluid under the skin. can result in serious injury and great pain.

Front 100

Engine:
Function..
Located..

Back 100

compressed air flows through a diffuser which directs it to six combustion liners. Fuel air mix is ignited, combustion produces hot gases that dischare through aft ends causing turbine to rotate

Front 101

Engine accessory section:
Function..
Located...

Back 101

mounted on bottom of compressor, driven by a compressor extention shaft via a bevel gearing assembly. consists of engine fuel pump, fuel control unit, speed sensitive control, speed sensitive valve, main oil pump and scavenge oil pumps.

Front 102

Reduction gear assembly:
Funcion.....
Located.....

Back 102

reduces teh high rpm, low torque output of the power section to a low rpm, high torque output to be used by the prop shaft.

Front 103

Aircraft propeller system:
Function...
TYPE/model

Back 103

4 bladed hamilton standard 54H60-77 prop provides an efficient and flexible means of converting engine shaft horsepower to thrust. 2 main sections; rotating /non-rotating. it is a constant speed, variable pitch, full feathering prop

Front 104

Four main subassemblies of the propeller

Back 104

Barrel- structural foundation of prop blades, dome and control assembly
Dome- Pitch control piston and a CAM and gear train that converts linear travel of the piston into a rotart motion
Blade assembly
Control Assembly- Consists of the various components necessary for control of prop blade angle

Front 105

Auxilary power unit

Back 105

gas turbine compressor driving a 60kva generator. air bled from the compressor is used for engine starting and ground air conditioning. makes a/c self sustained, requires only battery

Front 106

Five subsystems that comprise the fuel system

Back 106

Fuel tanks
fueling system
transfer system
crossfeed system
dump system

Front 107

what safety precuations must be observed during fueling operations?

Back 107

NO RF transmission, allow 3 minutes before using the dipstick, may cause static discharge, must hault fueling if wing tank 5 is over filled, wing tank fuel spills from vent, loud or unusual noise is accompanied by wing vibration

Front 108

Digital communications management system (DCMS)

Back 108

process audo/data throughout the plane, interface between digital and analog devices and operators

Front 109

ultra high frequency (UHF)

Back 109

225.00 to 399.975 MHz

Front 110

very high frequency (VHF)

Back 110

30 to 399.975 MHz

Front 111

High Frequency (HF)

Back 111

2 to 29.999 MHz (am, usb, lsb, data, cw)

Front 112

Satellite communication (SATCOM)

Back 112

UHF-1, KY58, Antenna switching assembly

Front 113

Secure Communications

Back 113

all radios except HF-1, HF2, UHF-3, utilizes Ky-58's

Front 114

Tactical AIr Navigation (tacan)

Back 114

operates with surface beacon for nav purposes, provides bearing and distance within 300nm or 105 miles

Front 115

Global positioning system (GPS)

Back 115

Position coordinates elevations, speed and time

Front 116

Automatic direction finder (ADF)

Back 116

Relative bearing of a revieved UHF signal, indicates bearing on pilot or copilot HSI's

Front 117

VHF Omnirange

Back 117

airway radio nav, communmications receptions and ILS approaches

Front 118

APN-234 Color weather radar

Back 118

weather information relative to cloud formation, rainfall rate, thunderstorms and icing.... 240 miles

Front 119

AMS-1 Stormscope

Back 119

helps pilots avoid turbulance and other hazards 150,000 sq miles.

Front 120

ALR-81 countermeausres reciever set

Back 120

detects RF signals, display signal activity and providing IF, video and audio signals

Front 121

ALR-76

Back 121

detects, processes, identifies electromagnetic signals in the micorwave freq ranges with particular emphasis on radar signals

Front 122

ulq-16 pulse analyzer

Back 122

automatic or manual analysis on signals to extract fundamental signal parameters for ESM

Front 123

OE-319 antenna group

Back 123

6 freq bands, apx-76 or alq 108, Transmit and recieve for 134

Front 124

oe-320 antenna group

Back 124

air born DF for alr-44 and alr-81

Front 125

ip-1159 pulse indicator

Back 125

5 trace synchro scope that can display processed and unprocessed video signals

Front 126

ush-33 recorder reproducer set

Back 126

28 track video recorder-reproducer that recieves, records and reproduces data in the 400Hz to 2MHz freq range

Front 127

ALD-9 direction finder set

Back 127

df set that calculates teh direction of arrival fro revieved HF, VHF and UHF signals

Front 128

ARR-81 countermeasures set

Back 128

4 channel 4 track audio tape recorder, records in its freq range

Front 129

video distribution

Back 129

provides amplification, selection and distribution of video signals

Front 130

rf distribution

Back 130

8 rf distribution groups in the a/c...... 5 ESM, 3 special.. provides amplification, selection and rf distibution in all TB's

Front 131

computer funtional group

Back 131

enables computer control over the equiptment connected to the 1553 bus or to other busses via the cv-4006/a bus converters

Front 132

Story Teller

Back 132

provides MC with teh ability to track multiple onboard sensor inputs, correlate this data with info revieved from outside sources, and communicate info to force commanders

Front 133

Story book

Back 133

integrated special signals acquisition data processing and data fusion subsytems that provides situational awareness based on special signals exploration

Front 134

Story Classic

Back 134

Provides the system interface for control signals and data between all major components of the SC system

Front 135

Aircraft battery... what is its function, where is it located?

Back 135

one 24v 31 amp battery, used to start APU, revieves a continuous charge from TR#3

Front 136

Main Generator.. what is its function and where is it located??

Back 136

generates 3 phase, 120 vac, 400 hz power in A/C.. engine 2-4 and APU.

Front 137

Transformer Rectifier.... what is its function and where is it located?

Back 137

rectify the a/c input to a 27vdc output for use in A/C. 2 in MLC and 1 in FLC

Front 138

Supervisory Panel... where is it located and what does it do?

Back 138

each generator has one, contains voltage regulators and provides overvoltage, undervoltage off frequency and feeder fault protection in MLC.

Front 139

AC Power

Back 139

controled by a transfer and runaround system, ensure power source is connected to Main AC buses A and B

Front 140

DC Power

Back 140

Consists of 3 27v 200 amp tranformer rectifiers, 6 DC buses , an inverter, a 24v batery and 2 power blocking diodes

Front 141

Rotating Beacon

Back 141

provide anti-collisoin warning to other A/C

Front 142

Wing tip lights

Back 142

red-port
green-stbd

Front 143

tail lights

Back 143

top and bottom of aft fuselage

Front 144

landing lights

Back 144

under wings, can be retracted when not in use, operate in any position

Front 145

taxi lights

Back 145

left and right of nosegear strut

Front 146

Advisory light

Back 146

Green is for normal operation mode of system or transitiong state

Front 147

caustion light

Back 147

yellow is of a cautionary nature, indicating action by pilots may be required

Front 148

Warning light

Back 148

red, potentially hazardous situation or impending dange and immediate action by pilots must be taken

Front 149

PB-20N

Back 149

Auto Pilot- maintain A/C on any selected heading

Front 150

ASW-31

Back 150

Auto pilot- controls/stabilizes A/C about its 3 axis

Front 151

Intertial Navigation systems (INS)

Back 151

Support navigation, weapons delivery, attitude and flight control requirements

Front 152

Periscope Sextant

Back 152

Navigation by stars

Front 153

State the precautions for working with energized circuits

Back 153

disconnect electrical power before working on electrical or electronic equiptment, and before removing and installing units or components. voltages are dangerous to life.

Front 154

LPP-1

Back 154

single compartment, yoke type flotation assembly. contains a whistle, dye marker, steady burning water activated light

Front 155

SV-2

Back 155

survival best which contains 11 required survival items, worn by aircrew

Front 156

Life rafts

Back 156

a/c contains 2 12 man rafts, located by each overwing exit

Front 157

anti-exposure suits

Back 157

warn if water is below 50 degrees F, or air is below 32 degrees F.

Front 158

Parachutes

Back 158

backpack type, 28' Flat canopy, ripcord on left side of harness, 24 on A/C

Front 159

Cabin air compressor (EDC)

Back 159

mounted on generators of engine 2 and 3, single stage centrifugal type compressors coupled directly to the reduction gearbox accesory drivetrain

Front 160

cabin exhaust fan

Back 160

cabin air exhausted overboard through the outflow valve

Front 161

outflow valve

Back 161

four positions to control cabin pressure

Front 162

refrigeration turbine

Back 162

2-2 stage air cycle cooling units installed in the nose wheel

Front 163

heat exchanger

Back 163

ram air duct blow air across to cool for airconditioner

Front 164

APU air multiplier package

Back 164

takes in ambient air, compresses it, combines it with APU bleed air then routes it to teh air cycle cooling system

Front 165

Fire Extinguishing systems

Back 165

2 independent, electronically controlled high rate of discharge fire systems, onoe for both sides. when fired its discharged into all 3 zones of the engine selected. each system includes 2 containers located forward of teh fore wall in the inboard engine nacelles

Front 166

oxygen system

Back 166

supply 3 aircrew for 3.5 hours at 25000ft, 3 portable o2 bottles that will supply 100% O2 for 22 minutes, 18 solid state O2 packs, provide 20 minutes of O2

Front 167

What warning is associated with the use of a portable fire extinguisher

Back 167

extinguishment of fire by HALON 1301, may produce decomposition by products, characterized by sharp acrid odor that may be harmful

Front 168

State and explain your commands mission statement

Back 168

Vq-1
In defense of our great nation, we conduct critical peactime and combat reconnaissance for fleet and theater commanders to project power and protect strike forces

Front 169

State the comands operational chain of command

Back 169

operational control of the squadron is accomplished by commander, patrol and reconnaissance force, 7th fleet and commander patrol and reconnaissance forch 5th fleet

Front 170

What are the EP-3e's primary warfare missions?

Back 170

AAW- anti air warfare
ASUW- anti surface warfare
C3- Command control and communications
EW- electronic warfare
FSO- fleet support operations

Front 171

AAW

Back 171

Anti air warfare- detection, tracking, distruction or neutralization of enemy air platforms and airborn weapons, weather launched from air, surface, sub-surface or land

Front 172

Discuss teh role of the EP-3e in AAW missions

Back 172

Detect, track and identify air targets using visual reconnaissance and esm that utilize radar and passive sensors

Front 173

Define the term ASU

Back 173

Detection, tracking, distruction or neutralization of surface combatants or merchant ships