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.
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 <
Control placement represented from the supplied pedestal figure; detent force and surface response are configurable.
CENTRE PEDESTAL BUILD 3.2
TQA, engine/fire, high-lift and ACP faces traced to supplied references · trainer-only consequences are marked
TQA, engine/fire, high-lift and ACP faces traced to supplied references · trainer-only consequences are marked
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
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
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.
ATA 21 / 36 AIR PANEL · BLEED AIR AND ECS
XBLEED
MAN
CLSDAUTOMAN
OPEN
CLSDAUTOMAN
OPEN
Confirmed: AIR panel control identities and arrangement, IASC dual DC ESS supplies, AUTO/MAN XBLEED behaviour, FCV/pack selection, RAM AIR DC ESS BUS 3 supply, AIR-page symbols and related ATA 21/36 messages. Configurable trainer inputs: nominal pressure/temperature/cabin values and the amber instructor fault buttons. They are fault injection controls, not aircraft panel controls.
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.