SONALERT PILOTE
AUTOMATIQUE
AUTOPILOT SONALERT
0
0
HORIZON
DIRECTEUR DE VOL
FLIGHT DIRECTOR
INDICATOR
SYSTEME DE CAP
COMPASS SYSTEM
( 34 - 21 - 00 )
HSI
CENTRALE DE CAP
SLAVED DIRECTIONAL GYRO
BOITIER COMPENSATEUR
SLAVING ACCESSORY
VANNE DE FLUX
FLUX VALVE
AIAH
Validity : KFC 150 without EFIS
TRIM ELECTRIQUE MANUEL
( INVERSEUR DOUBLE )
MANUAL ELECTRICAL PITCH TRIM
( DUAL INVERTER )
A81
BOITIER DE COMMANDE
PRESELECTION ALTITUDE (OPT.)
ALT / VERT. SPEED SELECTOR (OPT.)
BOITE DE COMMANDE AUDIO
AUDIO CONTROL BOX
( 23 -11 - 00 )
SONALERT ALARME ALTITUDE
ALT. ALERT SONALERT
BARRE BUS 2 BUS 2 BAR
A/P
BARRE BUS BJ6 BJ6 BUS BAR
A82
CALCULATEUR DE VOL
FLIGHT COMPUTER
B38
SERVOMOTEUR COMPENSATEUR
DE PROFONDEUR
PITCH TRIM SERVO ACTUATOR
A81
BOITIER DE COMMANDE
PRESELECTION ALTITUDE (OPT.)
ALT / VERT. SPEED SELECTOR (OPT.)
B36
SERVOMOTEUR DE ROULIS
ROLL SERVO ACTUATOR
B35
SERVOMOTEUR DE PROFONDEUR
PITCH SERVO ACTUATOR
AIAH
Validity : KFC 150 without EFIS Autopilot — Electrical schematic
Figure 1 (2/2)
22-12-00 (FM) Page 3
DEC 99
2. LOCATION (Figures 2, 3, 4 and 5)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
A82 flight computer 1 251 C / 22-12-00
B36 roll servo—actuator 1 230 218 or 218F 22-12-00
B35 pitch servo—actuator 1 220 219 and 242 22-12-00
B38 pitch trim servo—actuator 1 220 219 and 242 22-12-00
A81 altitude / vertical speed selector (option) 1 250 / 22-12-00
M80 mode annunciator (option) 1 250 / 22-12-00
AUTOPILOT MASTER switch 1 250 / 22-12-00
Control push—buttons (pilot control wheel) 1 230 / 22-12-00
Warning buzzer (Autopilot sonalert) 1 240 241 22-12-00
Alt. alert sonalert (option) 1 240 241 22-12-00
"BJ6" bus bar 1 230 232L 22-12-00
Circuit breakers :
— "A / P"
— "TRIM"
— "ALT SEL" (option) 1
1
1 230
230
230 232L
232L
232L WM
WM
WM
3. DESCRIPTION
A. A82 flight computer
A82 flight computer consists of an electronic box enclosing the processing circuits and the two modules storing the values determined upon system certification. These replaceable modules are installed on the top and bottom boards.
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