22 - AUTO FLIGHT
- 22-00 AUTO FLIGHT
- 22-10 AUTOPILOT/FLIGHT DIRECTOR (AP/FD)
- 22-11 AP/FD ENGAGEMENT
- 22-12 CRUISE MODES
- 22-13 COMMON MODES
- 22-30 AUTOTHRUST
- 22-31 AUTOTHRUST ENGAGEMENT
- 22-32 AUTOTHRUST MODES
- 22-60 FLIGHT AUGMENTATION COMPUTER (FAC)
- 22-61 ARTIFICIAL FEEL AND RUDDER TRAVEL LIMITING COMPUTATION
- 22-62 RUDDER TRIM COMPUTATION
- 22-63 YAW DAMPER COMPUTATION
- 22-64 CONFIGURATION AND OPERATIONAL SPEED COMPUTATION
- 22-65 ENGAGEMENT AND INTERNAL MONITORING
- 22-66 FLIGHT AUGMENTATION COMPUTER (FAC)
- 22-67 FAC: ELECTRICAL AND HYDRAULIC POWER SUPPLY
- 22-68 FAC: DISCRETE/ANALOG INTERFACES
- 22-69 FAC: ARINC BUS INTERFACES
- 22-70 FLIGHT MANAGEMENT SYSTEM (FMS)
- 22-71 FLIGHT PLAN/DATA BASE
- 22-72 NAVIGATION/LATERAL FUNCTIONS
- 22-73 PERFORMANCE/VERTICAL FUNCTIONS
- 22-74 OPERATIONAL USE
- 22-75 EIS DISPLAYS
- 22-76 DATA LINK AND PRINTER FUNCTIONS
- 22-81 FLIGHT CONTROL UNIT (FCU)
- 22-82 MULTIPURPOSE CONTROL AND DISPLAY UNIT (MCDU)
- 22-83 FLIGHT MANAGEMENT AND GUIDANCE COMPUTER (FMGC)
- 22-84 FMGS: ELECTRICAL POWER SUPPLY
- 22-85 FMGS: DISCRETE/ANALOG INTERFACES
- 22-86 FMGS: BUS INTERFACES
- 22-91 FAULT ISOLATION FUNCTION - PRINCIPLE
- 22-92 AFS FAULT ISOLATION
- 22-96 AFS TEST
- 22-97 LAND CAT III CAPABILITY TEST