Eaws

Front 1

Intake radius

Back 1

9 feet, 25 feet at military

Front 2

Apu exhaust velocity

Back 2

142 mph at a temp of 328 to350f

Front 3

Type of engine

Back 3

F404-ge-400. Low bypass, axial flow, dual spool, turbo fan engine of modular construction with afterburner.

Front 4

Ignition system is made up of

Back 4

Alternator, ECA, fuel control, ignition exciter, main igniter, AB igniter, AB flame sensor, two fan speed transmitters and a thermocouple harness.

Front 5

Engine lubrication

Back 5

Self contained recirculation, dry sump requiring no external connections or inputs.

Front 6

Secondary power system

Back 6

Consists of APU and AMAD

Front 7

Three modes of operation for APU

Back 7

GMM, MES and ECS

Front 8

How is AMAD connected to the APU

Back 8

Pneumatic through the ATS.

Front 9

How long is ignition system energized

Back 9

Until N2 rpm is 54% or greater or the throttle is retarded below idle.

Front 10

Barometric altimeter

Back 10

Uses pitot static pressure to indicate altitude above sea level

Front 11

Radar altimeter

Back 11

Uses radio echos to determine altitude above ground level.

Front 12

Azimuth

Back 12

The angular position or bearing in a horizontal plane usually measured clockwise from true north

Front 13

Bearing

Back 13

Angular position of an object with respect to a reference point or line

Front 14

Range

Back 14

The distance of an object from an observer

Front 15

Heading

Back 15

Actual orientation of the aircraft's longitudinal axis at any instance. True heading is direction measured by true north

Front 16

Magnetic heading

Back 16

Uses the direction of the earth's magnetic field at that location as the reference.

Front 17

Relative heading

Back 17

Uses the current direction that the object is facing the 0/360 azimuth alignment

Front 18

VHF

Back 18

Very high frequency

Front 19

UHF

Back 19

Ultra high frequency

Front 20

TACAN

Back 20

Tactical air navigation. Used to determine relative bearing and slant range distance to a TACAN ground station or equipped aircraft.

Front 21

INS

Back 21

Inertial navigation system. Self contained, fully automatic, dead reckoning navigation system. It detects motion and provides acceleration, velocity, present position, pitch, roll and true heading to related systems.

Front 22

GPS

Back 22

Global positioning system. Receives info from satellite. Pilot and aircraft systems are continuously updated present position, velocity and time information.

Front 23

ARI

Back 23

Attitude reference indicator. Uses gyro and provides a minimum three minutes of attitude info with loss of power. Provide backup pitch and roll attitude for use by other systems.

Front 24

ILS

Back 24

Instrument landing system. All weather approach guidance system. Provides steering info during approach by decoding azimuth and elevation microwave signals received from surface transmitters. Signals are displayed on the HUD and the ARI.

Front 25

ADC

Back 25

Air data computer.

Front 26

ADSU

Back 26

Airstream direction sensing unit

Front 27

TTP

Back 27

Total temperature probe

Front 28

Data link

Back 28

Two way UHF communications link

Front 29

Radar

Back 29

Radio detection and ranging. Provides air to air and air to ground modes for target detection.

Front 30

DDI

Back 30

Digital display indicators. There are two. LDDI Provides NVIS (night vision image system)

Front 31

Hero

Back 31

Hazards of electromagnetic radiation to ordinance.

Front 32

Yellow ordinance

Back 32

High explosive

Front 33

Brown ordinance

Back 33

Rocket motor

Front 34

Stations for LAU-7

Back 34

1 and 9

Front 35

Lau-116 stations

Back 35

4 and 6

Front 36

Suu-63 with bru-32

Back 36

2, 3, 7 and 8.

Front 37

Suu-62 with bru-32

Back 37

Station 5

Front 38

Gun

Back 38

M61a1 20mm gun

Front 39

CADS used to jettison weapons stores

Back 39

Mk. 19, Mk. 125 and Mk. 107

Front 40

Cluster bombs

Back 40

Anti tank bomb clusters. Free fall weapons used against armored vehicles.

Front 41

Types of air to air missiles

Back 41

Aim-7 (sparrow), aim-9 (sidewinder), aim-120 (AMRAAM) advanced medium range air to air missile.

Front 42

What are types of AGM missiles

Back 42

AGM-65 (maverick), -84, -84d (harpoon), -84e (slam) stand of land attack missile, -84h (slam-er), -88 (harm) high speed anti radiation missile.

Front 43

Rate of fire for m61a1 20mm gun

Back 43

4000 low rate, 6000 high rate.

Front 44

Oxygen is in liquid form at

Back 44

-297 farenheit

Front 45

Pilot PPE

Back 45

Flight suit, aviator boots, g suit, I.D. tags, survival radio, gloves, knife, survival kit, signal device, flashlight, life preserver, laser, eye protection

Front 46

What type ejection seat is used

Back 46

Sju-17a

Front 47

How is ejection seat operated

Back 47

Ballistic gas pressure. Each seat initiator contains two cartridges (left and right). Gasses from the right cartridge start the canopy jettison sequence. The left activates redundant and provides a back up source to fire the seat.

Front 48

Emergency oxygen system

Back 48

Contained in seat pan. A 100 cubic inch emergency oxygen cylinder.

Front 49

Canopy system

Back 49

Pyrotechnicaly operated emergency canopy removal.

Front 50

What does ECS provide (12 subsystems)

Back 50

Bleed air control, bleed air leak detection, air cycle conditioning, cabin cooling and defog, avionics cooling, cabin pressurization, g suit, OBOGS, windshield anti-ice and rain removal, radar liquid cooling, canopy seal and wave guide pressurization.

Front 51

How does fire extinguishing system work

Back 51

Uses single tank with 3 lines for they're APU and each engine. System is a one shot one bay system.

Front 52

SEAD mission

Back 52

Suppression of enemy air defenses

Front 53

WAS mission

Back 53

War at sea

Front 54

CAS

Back 54

Close air support

Front 55

MAS mission

Back 55

Maritime air superiority

Front 56

ACM mission

Back 56

Air combat maneuvering

Front 57

CAP mission

Back 57

Combat air patrol

Front 58

VMC mission

Back 58

Visual meteorological conditions. VFR is permitted.

Front 59

IMC

Back 59

Instrument meteorological conditions. IFR (instrument flight rules). Blind flying utilizing instruments.

Front 60

CATCC

Back 60

Carrier air traffic control center

Front 61

MOVLAS

Back 61

Manually operated visual landing aid system. Back up for FLOLS.

Front 62

AAW mission

Back 62

Anti air warfare

Front 63

AMW

Back 63

Amphibious warfare. Hornet us used primarily as CAS

Front 64

CCC

Back 64

Command control and communications.

Front 65

MIW

Back 65

Mine warfare

Front 66

MOB

Back 66

Mobility

Front 67

NCO

Back 67

Non combatant operations

Front 68

STW

Back 68

Strike warfare

Front 69

IAS

Back 69

Intercommunication audio system

Front 70

Electrical supply consists of

Back 70

2 generators, 2 transformer rectifiers, 1 battery with dedicated charger, and a power distribution bus.