IAS250
FMSSPDMAN
HDG090
HDG
15000
ALT
FT
FT
V/S-1000
DNUP
BRT
MAXIDLEREVMAX
REV
REV
MAXIDLEREVMAX
REV
REV
67° MAX REV ↔ MAX · independent levers · finger lift to reverse
ENGINE
CONT
IGNITION
IGNITION
START
L ENG
CRANKAUTOR ENG
CRANK
CRANKAUTOR ENG
CRANK
PILOT
EVENT
EVENT
L ENG
R ENG
Panel layout follows the supplied reference. Fire-handle and bottle-discharge consequences are explicitly simplified training logic.
Squib/cartridge fail simulation — [ASSUMED, no source]: a failed squib only shows FAIL once that bottle is actually fired.
RET1/41/23/4FULLMAX
012345
012345
FLAP LIMIT (VFE)
1 · 230 KT 2 · 210 KT
>3 · 210 KT< 4 · 190 KT
5 · 170 KT
1 · 230 KT 2 · 210 KT
>3 · 210 KT< 4 · 190 KT
5 · 170 KT
ALTN FLAPNORM > DPLY <
CENTRE PEDESTAL
TQA · ENGINE · SPOILER · SLAT/FLAP
TQA · ENGINE · SPOILER · SLAT/FLAP
AILERON
RUDDER
LIGHTING CONTROL / COCKPIT DOOR
DSPL
LWR
LWR
INTEG
ISI · MAIN · GSHLD
ISI · MAIN · GSHLD
FLOOD
OFF · BRT
OFF · BRT
COCKPIT DOORUNLOCK
PEDESTAL SERVICE / DISPLAY CONTROL
LEFT CONTROL TUNING PANEL
CURSOR CONTROL PANEL 1
MULTIFUNCTION KEYBOARD PANEL 1
REVERSION SWITCH PANEL
RIGHT CONTROL TUNING PANEL
CURSOR CONTROL PANEL 2
MULTIFUNCTION KEYBOARD PANEL 2
RADIO TUNING SYSTEM APPLICATION / CNS
AUDIO CONTROL PANEL 1
AUDIO CONTROL PANEL 2
AUDIO CONTROL PANEL 3
Source boundary: CTP/MKP RTSA access, CTP OFF/inhibit and cross-side control, VHF ON/OFF, squelch, 8.33/25 selection and the 30-second PTT timeout are source-confirmed by ATA 23/31. Channel-name validation, audio mixing and DLK/CPDLC/SATCOM/GWX application content remain configurable pending operator/application specifications.
ATA 22 AUTOFLIGHT MODE SIMULATION
IAS
ALTITUDE
RADIO ALT
THRUST LEVER
FD guidance / deviation trainer inputs (simulated instructor inputs — not computed guidance)
Mode colours: active/captured modes are green; armed modes are white. Phase buttons are scenario shortcuts. FCP, AP, AT, FD, XFR, EDM, approach, autoland and go-around logic follows the supplied ATA 22 training material; aircraft dynamics and mode capture timing are simplified and configurable.
A220 OVERHEAD PANEL
L ENG
BTL 1
BTL 2
APU
BTL
R ENG
BTL 1
BTL 2
LIGHTING
ENTRANCE
DOME
AURAL / HEAT
AURAL WARN
PROBE HEAT
WINDOW HEAT
L SIDE
L WSHLD
R WSHLD
R SIDE
PRIM FLT CTRL
PFCC 1
PFCC 2
PFCC 3
CVR
TEST
TEST
ERASE
INTEG / ANNUN LTS
CB INTEG
OVHD INTEG
COMPASS
ANNUN BRT
SERV INT
MECH
CALL
CALL
READING / WIPER
READING
WIPER
HYDRAULIC
HYD 3A
PTU
HYD 3B
HYD 2B
ELECTRICAL
BUS ISOLPULL TURN
BATT 1
AUTO
AUTO
BATT 2
AUTO
AUTO
TESTAPUTAWS
PULL TURN
FUEL
MAN XFR
L BOOST PUMP
R BOOST PUMP
COCKPITC H
FWDC H
AFTC H
FWD VENTOFF · VENT
LO HEAT · HI HEAT
LO HEAT · HI HEAT
AFT VENTOFF · VENT
LO HEAT · HI HEAT
LO HEAT · HI HEAT
XBLEED
MAN
CLSDAUTOMAN
OPEN
CLSDAUTOMAN
OPEN
ANTI-ICE
L COWL
AUTO
AUTO
WING
AUTO
AUTO
R COWL
AUTO
AUTO
ELT
TEST
ELT
FOR AVIATION EMER USE ONLY
UNAUTHORIZED OPERATION PROHIBITED
UNAUTHORIZED OPERATION PROHIBITED
CARGO
FWD
BTL
AFT
EQUIP COOLING
INLET
EXHAUST
PRESSURIZATION
EMER DEPRESS
MAX ΔP8.1 PSI T/D1.80 PSI LDG
AUTO PRESS
DITCHING
MAN RATEDNUP
PAX OXY
EVAC / EMER LTS
EVAC CMD
EMER LTSOFFARMONPULL
PUSH
PUSH
READING / WIPER
READING
WIPER
EXT LIGHTS
NAV
BEACON
STROBE
LOGO
WING INSP
TAXI
TAXI
LDG LIGHTS
L
NOSE
R
PAX SIGNS
SEAT BELTS
NO PED
ATA 24-70 CIRCUIT BREAKER APPLICATION · NORMAL MODE
Confirmed normal-mode application: monitor FUSE/TCB/FBWPC-CPD/SSPC-CB state, location and rating; acknowledge trips; command SSPC-CB IN or OUT; sort by STATUS/BUS/LOCATION/SYSTEM; and filter by the source lists. LOCK and failed-CB reset are maintenance-mode functions and are intentionally not provided here. The catalogue contains only identities visible in ATA 24 Figure 85. “DEMO TRIP” is clearly separated instructor injection. No unsupported free-text search, pulled-state label or invented breaker data has been added.
ATA 49-60 APU CONTROL
Confirmed: single APU switch OFF/RUN/START (pull-turn, spring-return from START); start sequence rpm thresholds (0/7/50/60/88-95/91-98/100/106%) and the 60-second cooldown [ATA49-60 p.49-92 to 49-95]. Configurable trainer timing: the seconds-long door-open/ramp/spooldown durations are not given by the source, which specifies rpm thresholds only. In integrated mode the parent trainer runs this sequence and owns generator/bleed availability; the standalone file uses a simplified local model. APU fire detection/extinguishing is deferred to a later ATA 26 stage.