TB 43-0123
UH-60 AFCS
NSN: N/A
EIC: NIA
(Illustration Not Available)
UH-60 AFCS Automatic Flight Control System
1. Brief Description:. The UH-60 Automatic Flight
2. Applicable Tools and Test Equipment: See
Control System is an electro-hydromechanical system
that provides inputs to the fight controls to assist the pilot
Type No.
AVW
AVIM
in maneuvering and handling the aircraft. The three
AN/USM-23
X
major subsystems of the AFCS are the analog stability
AN/USM451 (2 ea
X
augmentation system (SAS 1), the digital AFCS (SAS 2)
MK-693/A
X
and the stabilator system. They provide oscillation
TK-101/G
X
damping (dynamic stability) and maintain desired
TS-3920/ASM
X
attitude, speed and heading (static stability). Major
7365
X
components of the UH-60 AFCS are:
Stopwatch
X
AM-7105/A
Synchro Signal (SAS)
NOTE
Amplifier
Refer to TM 11-1520-237-23-2 and -3 for special
AM-7106/A
Elec. Control (Stabilatory
and locally tools, adapters, etc.
Amplifier (2 ea)
C-10909/A
Flight Control Panel
3. Applicable Publications:
CN-1552/A
Rate Gyro
TM 11-1520-237-23-1 (Pertains to UH-60 Aircraft)
CN-1564/A
Rate Gyro
TM 11-1520-237-23-2 (Pertains to UH-60 Aircraft)
CP-1446/A
Computer
TM 11-1520-237-23-3 (Pertains to UH-60 Aircraft)
ID-2279/A
Stabilator Indicator Indictor
TM 11-1520-237-23P (Pertains to UH-60 Aircraft)
(2 ea)
MT-6227/A
Vibration Tray
TR-322/A
Air Data Transducer
TR-323/A
Air Speed Transducer
TR-326/A
Linear Servo
Accelerometer (2 ea)
70400-06712-042
Stabilator Position Sensor
70901-02002-106
Stick Position Sensor
II-H-4
