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c130h1

The document describes the standard flight director system for the C-130H aircraft, detailing various operational modes and components integral to its functionality. It outlines multiple navigation modes, including TACAN, heading, and I-DOP modes, among others.

c130h1

c130h1

AN/AYW-1(V) auto pilot system

modes
attitude source
lateral and vertical modes
air data sensor (ADS)
memory loader verifier (MLV) data port
NVIS lighting
Servos
flight control panel (FCP)

alt hld switch and annunciator

built-in Test (BIT) switch

pitch switch

LAT switch

AP1 and AP2 switches

integrated pitch and roll control

test operations panel (TOP)
automatic flight control processor

Air force standard flight director system

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

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I-ins mode
I-dop mode
self-contained navigation system (SCNS) mode
VOR/ILS Mode
TACAN mode
heading (hdg) mode
sensitivity relay
navigation instrument relay panel (NIRP) assembly
adi ske on indicators
selected nav system off indicator
copilots adi repeat indicator
adi mode select switch
flight director mode selector (fdms) panels

adi normal/pilot repeat switch

vert ref ins/vg switches

Fly Fir normal/manual switches

FDMS panel NAV SEL switches

rate gyro relay
rate gyro transmitter
rate switching gyro
displacement gyro
flight director computer (fdc)
horizontal situation indicator (hsi)

miles indicator (dme)

course deviation

bearing pointer

heading marker

compass card

attitude director indicator (adi)

adi warning flags

pitch steering bar

glideslope pointer

bank steering bar

adi turn needle

pitch trim knob

airplane symbol

c12 compass

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

34-24-00

Error compensation
index error
transmission error (two-cycle)
one-cycle error
earths rate error
coriolis error
meridian convergence error
Modes
heading (DG) mode

fast swing

turn rate cutoff

Heading (Mag) Mode

heading information

slaving amplifier

components
remote magnetic compensator

magnetic compass calibrator connection

one-cycle error compensation

coriolis error compensation

transmission error compensation

index error differential

regulated school power supply

amplifier -power supply

servomechanism

slaving amplifier 1a2

slaving amplifier 1a1

amplifier Rack

Directional gyro

gimbal error control

earths rate correction

slaving output stage

drift bias circuit

gyro proper

digital controller

power adequacy indicator

earths rate and coriolis computer

latitude knob

latitude N-S switch

digital readout

synchronization knob

MAG-DG switch

annunciator

magnetic azimuth detector (mad)