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Feature or Capability |
VP-50
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VP-X
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VP-200/Duo
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Electrical System |
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Electronic circuit breakers used throughout |
X
|
X
|
X
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Solid-state short circuit protection |
X
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X
|
X
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Over-current protection for each circuit (fully configurable) |
X
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X
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X
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User re-settable circuit protection |
X
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X
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X
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Open-circuit detection (detects burned out landing light, inop boost pump, etc.) |
X
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X
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X
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Status (on, off, fault) of each electrical device |
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X
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X
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Display of real-time current draw per circuit |
X
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X
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X
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Display of overall aircraft current draw |
X
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X
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X
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Low-voltage alarm |
X
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X
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X
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Dual low-voltage alarm trip points (with and without engine running) |
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X
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Over-voltage alert |
X
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X
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X
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Over-voltage protection and automatic alternator shut-off |
X
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X
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X
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Single alternator support |
X
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X
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X
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Dual alternator support |
X
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X
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X
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Supports internally-regulated alternators |
X
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X
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X
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Supports externally-regulated alternators (voltage regulator must be used) |
X
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X
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X
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Supports B&C SD-8 and SD-20 |
X
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X
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X
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Supports single battery electrical system configuration |
X
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X
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X
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Supports single battery with aux battery electrical system configuration |
X
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X
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X
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Supports dual battery, dual alternator, dual independent electrical system configuration |
|
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Duo
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Graphical display of electrical system and status of components |
|
X
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X
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Supports 14v and 28v systems. |
X
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X
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X
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Cabin and instrument panel light dimming (built-in) |
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X
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Taxi and landing light soft start (for halogen bulbs) |
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X
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Backups for critical avionics |
X
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X
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X
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Endurance bus circuitry (backup power) built in |
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X
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Switched power circuits (2A to 18A capacity) |
21
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32
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30/58
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Aux battery voltage display |
X
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X
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X
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Auto-pilot disconnect warning (senses when autopilot turns off) |
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X
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Individual circuit shut-off timer |
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X
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Automatic control of battery contactor |
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X
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Detection of battery contactor failure and automatic engagement of backup power and load shedding |
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X
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Built-in circuits for control of starter contactor |
|
X
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X
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14v regulated circuit (3A capacity) |
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X
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X
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Trim System |
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Solid-state trim control system |
X
|
X
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X
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Trim circuits (motor and position feedback) |
2
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2
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2
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Runaway trim protection |
X
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X
|
X
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Backup pitch trim control |
X
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X
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X
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Trim position indicators |
X
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X
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X
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Visual feedback while trim is running |
X
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X
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X
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14v regulated trim motor output (no need to buy DC-DC converter for 28v systems) |
X
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X
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X
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Automatic variable speed trim motor to reduce trim sensitivity at higher speeds |
|
X
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X
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Switch activated variable speed trim motor to reduce trim sensitivity at higher speeds |
X
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Verify correct position of trim for each phase of flight |
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X
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Power-on trim switch fault detection |
X
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X
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X
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Flap System |
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Solid-state flap control system |
|
X
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X
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Flap circuits (motor and position feedback) |
|
X
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X
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Electronic motor braking |
|
X
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X
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Disable co-pilot stick switches from display screen button |
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X
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Visual feedback while flaps are running |
|
X
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X
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Flap position display |
|
X
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X
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Flap over-speed warning (user configurable) |
|
X
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X
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Disable flap down switch above specified airspeed |
|
X
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X
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Momentary flap operation (moves when switch pressed) |
|
X
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X
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Position based flaps (moves to next configurable position) |
|
X
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X
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Motor run-on protection |
|
X
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X
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Verify correct position of flaps for each phase of flight |
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|
X
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Power-on flap switch fault detection |
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X
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X
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Wig-Wag |
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Landing light pulse (wig-wag) |
X
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X
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X
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Wig-wag automatic when above specified speed |
|
X
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X
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Manual wig-wag swtich |
X
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Light warm-up period (configurable) |
X
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X
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X
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Special Features |
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Mode determination (pre-flight, before start, start, after start, taxi, run-up, take off, cruise, maneuver, and landing modes) with automatic and manual sequencing |
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X
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Mode-based automatic device switching (on/off) |
|
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X
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Panel switches to turn devices on/off |
8
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10
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3
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Engine gauges are optimized for each phase of flight (configurable) |
|
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X
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Climate Control System integration |
|
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X
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Built-in mag switch, with audio and visual alarms for incorrect position during each phase of flight |
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X
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"Before Takoff Check" button to verify correct position of trim, flaps and mag switch |
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X
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Built-in emergency handling |
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X
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Built-in master switch |
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X
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Automatically turns off master switch if pilot forgets |
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X
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Verifies correct position of trim, flaps, and mag switch for each phase of flight. |
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X
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User-configurable load-shedding for both VMC and IMC conditions |
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X
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Landing gear circuit disable on ground |
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X
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Landing gear up, down, and in-transition indicators |
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X
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Landing gear up audio & visual warning on landing |
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X
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Indication of VLE on gear indicators |
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X
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Audio verification of gear down “three green” and gear up. |
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X
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Encrypted remote control with four user-configurable buttons |
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X
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Automatic canopy seal infaltion/deflation system for Lancair |
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X
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Auto Boost (turns on boost pump if fuel pressure drops) |
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X
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Checklists |
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User configurable checklists |
|
|
X
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Checklists displayed automatically for each phase of flight |
|
|
X
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Automatic emergency checklist display |
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X
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Starter |
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Disable starter when engine running |
|
X
|
X
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Key code required to enable starter (no mechanical key needed) |
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X
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Starter engaged annunciator |
|
X
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X
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Display |
|
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Engine gauges with visual and audio alerts for exceedences |
|
|
X
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Engine gauges for piston engines |
|
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X
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Engine gauges for turbine engines |
|
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X
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Engine gauges for Subaru engines |
|
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X
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Engine leaning (EGT) display with peak detection |
|
|
X
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Engine data logging |
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|
X
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Displays RPM drop and delta during mag check |
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X
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Fuel tank level display (left and right tanks) |
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X
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Fuel totalizer display |
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|
X
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Accepts engine data from popular engine monitors |
|
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X
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Annuncaitors for door, canopy, chips, etc. |
|
|
X
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Status indicators for GPS, air data, and engine data inputs |
|
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X
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Timer- flight time and engine time |
|
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X
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Future software upgrades provided at no charge |
X
|
X
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X
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USB data port for software updates, data downloading, and keyboard input |
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via EFIS
|
X
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RS-232 serial data port for software updates |
X
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Display |
16 Char
|
EFIS
|
Color LCD
|