c130h1

c12 compass

r

1c-130h-2-34gs-00-1 34-24-00

components

magnetic azimuth detector (mad)

digital controller

annunciator

MAG-DG switch

synchronization knob

digital readout

latitude N-S switch

latitude knob

earths rate and coriolis computer

power adequacy indicator

Directional gyro

gyro proper

drift bias circuit

slaving output stage

earths rate correction

gimbal error control

amplifier -power supply

amplifier Rack

slaving amplifier 1a1

slaving amplifier 1a2

servomechanism

remote magnetic compensator

regulated school power supply

index error differential

transmission error compensation

coriolis error compensation

one-cycle error compensation

magnetic compass calibrator connection

Modes

Heading (Mag) Mode

slaving amplifier

heading information

heading (DG) mode

heading information

turn rate cutoff

fast swing

Error compensation

meridian convergence error

coriolis error

earths rate error

one-cycle error

transmission error (two-cycle)

index error

Air force standard flight director system

r

1c-130h-2-34gs-00-134-23-00

components

attitude director indicator (adi)

airplane symbol

pitch trim knob

adi turn needle

bank steering bar

glideslope pointer

pitch steering bar

adi warning flags

horizontal situation indicator (hsi)

compass card

heading marker

bearing pointer

course deviation

miles indicator (dme)

flight director computer (fdc)

displacement gyro

rate switching gyro

rate gyro transmitter

rate gyro relay

flight director mode selector (fdms) panels

FDMS panel NAV SEL switches

Fly Fir normal/manual switches

vert ref ins/vg switches

adi normal/pilot repeat switch

adi mode select switch

copilots adi repeat indicator

selected nav system off indicator

adi ske on indicators

navigation instrument relay panel (NIRP) assembly

sensitivity relay

Modes

heading (hdg) mode

TACAN mode

VOR/ILS Mode

self-contained navigation system (SCNS) mode

I-dop mode

I-ins mode

AN/AYW-1(V) auto pilot system

components

automatic flight control processor

test operations panel (TOP)

flight control panel (FCP)

integrated pitch and roll control

AP1 and AP2 switches

LAT switch

pitch switch

built-in Test (BIT) switch

alt hld switch and annunciator

Servos

NVIS lighting

memory loader verifier (MLV) data port

air data sensor (ADS)

modes

lateral and vertical modes

attitude source