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Avionics & Wiring

ATA Chapter 42 — N720AK Systems Reference

Overview

This section covers N720AK’s avionics stack as an integrated system — how everything is wired together, the panel layout, connector types, and the data flow between components. Individual avionics boxes are documented in their own system pages; this page covers the interconnections.

Avionics Stack

SystemComponentNotes
Audio PanelGarmin GMA 245Bluetooth, 4-place intercom, S/N 3YL000434
Nav/GPS/ComGarmin GTN 650Certified IFR, single Bob Archer nav antenna, S/N 1Z8021616
EFISDynon Skyview HDXPrimary flight display
AutopilotDynon 3-axisRoll, pitch, yaw damper servos
AP PanelDynonAutopilot control panel
Com PanelDynonCom frequency control
Knob PanelsDynon
CO DetectorCO Guardian 452-101-012Guardian Avionics
TransponderADS-B Out
ELTArtex ELT 345406 MHz
Bus ManagerflyEFII System32See Electrical Power
Power DistributionVPX SportSee Electrical Power
Instrument PanelAerosport 310Aerosport Products
Overhead ConsoleAerosport CarbonAerosport Products
Map Lights (x2)MAPLIGHT-R-24SteinAir

CO Guardian 452

Model: 452-101-012 (Certified Remote Mount CO Detector for Dynon Systems) S/N: 112081 Status: Not currently installed. The unit was replaced under RMA 11096 (Dec 2025). The Dynon EMS pin it previously occupied (pin 31, brown/blue wire) is now used by the Monkworkz MZ-30 generator proportional current output.

Wiring for future reinstallation:

  • The brown/blue wire for the CO Guardian’s EFIS connection is tied up near the Dynon EMS connector
  • Audio warning line runs from the CO detector location to the GMA 245 Music input (currently disconnected, difficult to reach behind panel)
  • Dynon sensor definition file: CO Guardian Sensor Config (RevC) — already filed in GDrive Configs/Dynon
  • Circuit breaker: 7277-2-2 (2A, 14/28 VDC Avionics)
  • RS-232 interface available (optional)

References:

Software Versions

SystemVersionAs OfUpdate Source
Dynon Skyview HDX17.42026-03-06Dynon HDX Software Updates
Garmin GTN 650Main SW 6.732026-03-06Garmin GTN Software
flyEFII System32Version 86, Build 0012026-03-06flyEFII
Dynon aviation databaseCycle 2602 (Feb 19 – Mar 18)2026-03-06Dynon US Aviation Data
Seattle Avionics ChartDataCurrent (all 50 states)2026-03-06Seattle Avionics

Panel Layout

Data Flow

Known Wiring Notes

Serial 4 (Dynon ↔ GTN 650): The blue and green wires are intentionally flipped on this serial connection. This swap was done during installation — the TX/RX lines needed to be crossed for proper communication between the Dynon SkyView and GTN 650 on serial port 4.

Disconnected audio warning line: The old CO audio warning line runs from the former CO detector location to the GMA 245 Music input. This line is currently disconnected. It is difficult to reach — runs behind the panel.

Disconnected serial 4 line: A serial 4 cable was cut — it leads from one of the GTN 650’s serial outputs to the Dynon’s serial 4 port. Both connections are a major pain to reach and worth documenting on an updated schematic.

Wiring

Inspection & Maintenance

Connector References

EMS Sensors

Dynon EMS engine sensor inventory for N720AK:

FunctionDynon P/NDescriptionQtyNotes
Fuel pressure105492-002150 PSI fluid pressure (= Kavlico v2 103757-000)1Configured as KAV V2 150PSI DIFF mode; purple gasket removed
Oil pressure105492-002150 PSI fluid pressure (= Kavlico v2 103757-000)1Purple gasket removed
MAP104781-000MAP sensor, 1/8“ hose, 0–60 inHg1Discontinued; replacement is 105493-000 (1/8-27 NPT). Automotive-style sender
Oil temperature100409-001Oil/coolant temp, 5/8-18 UNF1Lycoming/Continental/Superior compatible
CHT100404-000CHT, adjustable bayonet, 3/8-24 UNF6One per cylinder
EGT100405-000EGT, 1.00–2.25“ hose clamp6One per cylinder
Alternator amps100412-000Amps shunt, 0–60A1Primary alternator current sensing
Generator currentMonkworkz MZ-30 proportional output on EMS pin 3110–2.7V = 0–30A; Dynon sensor: MONKWORKZ CURRENT (AMPS, name=MZ30)
Generator statusMonkworkz MZ-30 status wire on EMS pin1CONTACT-type sensor; Dynon sensor: MONKWORKZ STATUS (name=MZ30_S). Wire not yet physically connected

MAP Blanking Threshold

The MAP sensor definition (100434-000, all calibration variants) uses a min_val parameter that blanks the reading below a threshold. This was lowered from 2.0 PSI (4.07 inHg) to 1.5 PSI (3.05 inHg) on 2026-03-17 to prevent MAP and fuel pressure (DIFF mode) from blanking at high altitude idle with constant-speed propeller. Change approved by Don Jones, Dynon Customer Support (Zendesk #186497, 2026-03-16).

EMS Wiring

The Dynon SkyView Installation Guide page 7-7 shows the EMS wiring diagram for engine sensor connections.

References