# N739MA: 2020 Magnus FUSION 212

- Status: Valid registration
- Airframe: [Magnus FUSION 212](https://openairdocs.org/model/magnus-fusion-212) (registry code 056365I, 2 seats)
- Engine: [Rotax 912ULS series](https://openairdocs.org/engine/rotax-912uls-series) (registry code 55572)
- Serial number: MF-212-20-0021
- Year built: 2020
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Light sport, airplane
- Airworthiness date: July 10, 2021
- Certificate issued: June 25, 2024
- Expires: June 30, 2031
- Mode S code: A9ED8E
- Registered owner: [Schunter Frederick](https://openairdocs.org/faa-owner/SCHUNTER%20FREDERICK)
- Location: [Spokane, WA](https://openairdocs.org/faa-place/WA/Spokane)
- Owner type: Individual
- Owner's area on the map: 47.7407° N, 117.2614° W: Placed by OpenAirDocs at the center of ZIP code 99217, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=739MA
- Page: https://openairdocs.org/aircraft/N739MA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rotax 912ULS model are included.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Magnus FUSION 212)

None in force.

### Matched by engine (Rotax 912ULS series)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N739MA.

## FAA accident and incident reports

None matched to N739MA.

## Reports on N739MA not matched to an aircraft (1)

They name N739MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20190718015809I](https://openairdocs.org/incident/20190718015809I), Jul 18, 2019: Boeing 737-8Q8 (N739MA), Nadi Fiji, Minor damage. On July 18, 2019 N739MA departed Nadi internalional airport, Fiji (nan) for brisbane, australia ^(bne)with 155 passengers and 2 infants on board. During climb…

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N739MA not matched to an aircraft (45)

They name N739MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MYWA2020021900197](https://openairdocs.org/sdr/MYWA2020021900197), Feb 19, 2020: BATTERY PACK. INOPERATIVE. LT FWD EMERGENCY LIGHT OVER WING EXTERIOR WAS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. REFERENCE MAI LOGPAGE 255921.
- [SDR MYWA2019071800001](https://openairdocs.org/sdr/MYWA2019071800001), Jul 18, 2019: ENGINE. MALFUNCTIONED. DURING CLIMB OUT, THE #1 ENGINE FAILED. THERE WAS AN EGT EXCEEDANCE IN CONJUNCTION WITH AN OIL PRESSURE AND OIL QUANTITY LOSS. THE CREW COMMANDED A SHUTDOWN OF 
- [SDR MYWA201609090001](https://openairdocs.org/sdr/MYWA201609090001), Sep 8, 2016: UNKNOWN. MALFUNCTIONED. WHEN GEAR HANDLE WAS SET TO OFF, AFTER TAKEOFF NOSE GEAR EXTENDED. AIRCRAFT FLEW WITH GEAR POSITION LEVER IN THE UP POSITION.
- [SDR MYWA201204090039](https://openairdocs.org/sdr/MYWA201204090039), Apr 9, 2012: SMOKE DETECTOR. INOPERATIVE. AFT FIRE DETECTOR "A" LOOP INOPERATIVE. REMOVED AND REPLACED AFT SMOKE DETECTOR IAW MM 26-16-01, NO DISCREPANCIES NOTED.
- [SDR MYWA201202030016](https://openairdocs.org/sdr/MYWA201202030016), Feb 3, 2012: WIRE. BROKEN. FOUND BROKEN WIRE ON BATTERY PACK CONNECTOR M1672 PIN 13. REPAIRED WIRE IAW AMM 20-38-12. OPS CHECKS NORMAL.
- [SDR MYWA120016](https://openairdocs.org/sdr/MYWA120016), Feb 3, 2012: LIGHT. INOPERATIVE. EMERGENCY BULL NOSE LIGHT WILL NOT ILLUMINATE AT SEAT ROW 25 DEF.
- [SDR MYWA110105](https://openairdocs.org/sdr/MYWA110105), Nov 1, 2011: CONTROL UNIT. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: ELEC LIGHT ON ELECTRICAL PANEL ILLUMINATED ON GROUND. ACCOMPLISHED STANDBY POWER/BATTERY CHARGER TEST IAW 737-800 OPS MANUAL PAGE 63 A
- [SDR MYWA110103](https://openairdocs.org/sdr/MYWA110103), Oct 4, 2011: SMOKE DETECTOR. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: AFT CARGO LOOP "A" DET INOP. REMOVED AND REPLACED AFT CARGO LOOP "A" SMOKE DETECTOR IAW AMM 26-16-01 AND SMOKE DETECTION TESTS OK IAW 
- [SDR MYWA110098](https://openairdocs.org/sdr/MYWA110098), Sep 15, 2011: THERMOSTAT. DEFECTIVE. ETOPS SIGNIFICANT SYSTEM: DUCT PRESSURE SPLIT 40 PSI SPLIT IN CLIMB (L 50/R10) PSI 26 PSI SPLIT IN CRUISE (L40/R14) PSI 20 PSI L AND R ON DESCENT. ACCOMPLISHED 
- [SDR MYWA110082](https://openairdocs.org/sdr/MYWA110082), Aug 2, 2011: STARTER GEN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: APU MAINT AND FAULT LIGHTS ON WHEN STARTING APU. REMOVED AND REPLACED APU STARTER GENERATER IAW B737-800 AMM 49-41-21 APU STARTING & O
- [SDR MYWA110080](https://openairdocs.org/sdr/MYWA110080), Jul 29, 2011: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: APU GENERATOR OFF BUS LIGHT ON WITH APU GEN ON LINE. PERFORMED OPS TEST & BITE CHECK ON APU GENERATOR CONTROL UNIT. DURING TEST, NO PR
- [SDR MYWA110076](https://openairdocs.org/sdr/MYWA110076), Jul 19, 2011: WARNING SYSTEM. FALSE ACTIVATION. ETOPS SIGNIFICANT SYSTEM: ELEC LIGHT ON. ACCOMPLISHED BITE TEST OF BATTERY/ ELECTRICAL PANEL. CLEARED FAULT IAW 737-800 FIM 24-31 TASK 801 OPS CHECK NORMAL.
- [SDR MYWA110068](https://openairdocs.org/sdr/MYWA110068), Jul 6, 2011: ENGINE. VIBRATION. ETOPS SIGNIFICANT SYSTEM: NR 2 ENG VIB MONITOR READS 2.0 IN DESCENT. ACCOMPLISHED NR 2 ENGINE AVM TRIM BALANCE AT LOCATION 6 INST P-14LOC 11 INST P14 LOC12 INST
- [SDR MYWA110057](https://openairdocs.org/sdr/MYWA110057), Jun 19, 2011: WARNING SYSTEM. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: APU LIGHT ON DURING RECALL. RE-BOOT THE A/C BITE AND OPS CHECK OK IAW AMM 49-11-00 & 49-61-00. NO FAULTS NOTED.
- [SDR MYWA110051](https://openairdocs.org/sdr/MYWA110051), Jun 14, 2011: BLEED AIR SYS. FLUCTUATES. ETOPS SIGNIFICANT SYSTEM: DUCT PRESSURE RIGHT SIDE 25 PSI DUCT PRESSURE LEFT SIDE 45 PSI CLIMB AND CRUISE. C/W FIM 36-10 TASK SUPPORT PG 315 NR 2 ENG FIG 306 OK
- [SDR MYWA110048](https://openairdocs.org/sdr/MYWA110048), Jun 11, 2011: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: DUCT PRESSURE ON RIGHT SIDE SHOWS 20 PSI BELOW LEFT DUCT ON CLIMB + CRUISE. CHECKED THE DUCT PRESSURE ON GROUND OPS CHECKS NORMAL PER 
- [SDR MYWA110042](https://openairdocs.org/sdr/MYWA110042), Apr 22, 2011: VALVE. INOPERATIVE. ETOPS SIGNIFICANT SYS: ON CLIMB OUT FROM ICT, LT DUCT PRESSURE 41 RT DUCT PRESSURE 26 EVEN IN CRUISE AND DECENT. REPLACED HIGH STAGE VALVE AND PRSOV.
- [SDR MYWA110038](https://openairdocs.org/sdr/MYWA110038), Mar 25, 2011: UNKNOWN. OUT OF LIMITS. ETOPS SIGNIFICANT SYSTEM: USING FMC CDU FOUND RT ENGINE FAULT. VBV POSITION SIGNAL IS OUT OF RANGE. TROUBLE SHOT AS PER FIM 75-32 TASK 802-803 PERFORMED RESISTA
- [SDR MYWA110035](https://openairdocs.org/sdr/MYWA110035), Mar 12, 2011: TRANSDUCER. OUT OF ADJUST. ETOPS SIGNIFICANT SYSTEM: ENGINE CONTROL LIGHT ILLUMINATED WITH NR 1 ENGINE RUNNING. FOUND NR 1 ENGINE OUTBOARD T/R SLEEVE LVDT OUT OF ADJUSTMENT. ADJUSTED PER 
- [SDR MYWA110033A](https://openairdocs.org/sdr/MYWA110033A), Mar 11, 2011: WARNING LIGHT. FALSE ACTIVATION. ETOPS SIGNIFICANT SYSTEM: ENGINE CONTROL LIGHT ON ENGINE NR 1, AFTER LANDING. PERFORMED BITE TEST, LIGHT EXTINGUISHED.
- [SDR MYWA110033](https://openairdocs.org/sdr/MYWA110033), Mar 9, 2011: SMOKE DETECTOR. NO TEST. ETOPS SIGNIFICANT SYSTEM: B-LOOP AFT CARGO SMOKE DETECTOR DOES NOT TEST.
- [SDR MYWA110023](https://openairdocs.org/sdr/MYWA110023), Feb 12, 2011: REGULATOR. FAULTY. ETOPS SIGNIFICANT SYSTEM: ON CLIMBOUT, PRESSURIZATION CHECK, RIGHT DUCT PRESSURE AT 30 PSI LEFT DUCT PRESSURE AT 45 PSI AT CRUISE, RIGHT DUCT PRESSURE 30 PSI LE
- [SDR MYWA100139](https://openairdocs.org/sdr/MYWA100139), Dec 31, 2010: DETECTOR. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM: AFT CARGO B LOOP DETECTOR INOP. REPLACED DETECTOR. SYSTEM CHECKS NORMAL.
- [SDR MYWA100131](https://openairdocs.org/sdr/MYWA100131), Dec 20, 2010: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYS: LT ENGINE BLEED TRIP OFF LIGHT ILLUMINATES AND WILL NOT RESET FOR MORE THAN 2 MINUTES. RESET LT ENGINE BLEED LIGHT. PERFORMED ENGINE BLEE
- [SDR MYWA100123](https://openairdocs.org/sdr/MYWA100123), Nov 24, 2010: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYS: DURING PREFLIGHT, A SYS ELEC/HYD LIGHT REMAINED ILLUMINATED WITH THE PUMP ON AND 3030 PSI SYS PRESSURE.
- [SDR MYWA100107](https://openairdocs.org/sdr/MYWA100107), Sep 19, 2010: AUTOPILOT SYS. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: AUTOPILOT "A" DOES NOT ENGAGE WHEN CMD IS PUSHED. LIGHT DOES NOT ILLUMINATE AND STATUS DOES NOT SHOW ON FMAP.
- [SDR MYWA100102](https://openairdocs.org/sdr/MYWA100102), Aug 29, 2010: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: "RA" SHOWS ON CAPT'S SIDE DISPLAY UNIT.
- [SDR MYWA100099](https://openairdocs.org/sdr/MYWA100099), Aug 28, 2010: WARNING SYSTEM. ACTIVATED. ETOPS SIGNIFICANT SYSTEM: AFTER PUSHBACK, MACH TRIM LIGHT ILLUMINATED ON RECALL.
- [SDR MYWA100100R1](https://openairdocs.org/sdr/MYWA100100R1), Aug 22, 2010: SMOKE DETECTOR. FAILED. ETOPS SIGNIFICANT SYSTEM: AFT CARGO B LOOP SMOKE DETECTOR FAILED TEST.
- [SDR MYWA100101](https://openairdocs.org/sdr/MYWA100101), Aug 19, 2010: FIRE LOOP. NO TEST. ETOPS SIGNIFICANT SYSTEM: FWD CARGO FIRE LOOP A WOULD NOT TEST.
- [SDR MYWA100091](https://openairdocs.org/sdr/MYWA100091), Jun 6, 2010: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM - PACK LIGHT ILLUMINATES DURING RECALL.
- [SDR MYWA100090](https://openairdocs.org/sdr/MYWA100090), Jun 5, 2010: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM - LT PACK LIGHT ON AT RECALL.
- [SDR MYWA100082](https://openairdocs.org/sdr/MYWA100082), May 30, 2010: CONTROLLER. FAILED. ETOPS SIGNIFICANT SYSTEM - LEFT PACK CONTROLLER FAILED IN ONE CHANNEL.
- [SDR MYWA100081](https://openairdocs.org/sdr/MYWA100081), May 30, 2010: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - AIR CONDITIONING COOLING INSUFFICIENT.
- [SDR MYWA100074](https://openairdocs.org/sdr/MYWA100074), May 6, 2010: MICROPHONE. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM - PA SYSTEM DOES NOT OPERATE FROM FLIGHT COMPARTMENT.
- [SDR MYWA00048](https://openairdocs.org/sdr/MYWA00048), Apr 29, 2010: STARTER. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE FAILED TO START.
- [SDR MYWA100059](https://openairdocs.org/sdr/MYWA100059), Apr 9, 2010: TRIM SYSTEM. OUT OF LIMITS. ETOPS SIGNIFICANT ITEM - DURING FUNCTIONAL CHECK FLIGHT, ACFT TRIM OPERATIONAL PARAMETERS WERE OUT OF CHART LIMITS.
- [SDR MYWA100010](https://openairdocs.org/sdr/MYWA100010), Jan 28, 2010: INDICATOR. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM - NR 2 FUEL QUANTITY INDICATOR INOP.
- [SDR MYWA100009](https://openairdocs.org/sdr/MYWA100009), Jan 20, 2010: ENGINE. OIL CONSUMPTION. ETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE HIGH OIL CONSUMPTION.
- [SDR MYWA100008](https://openairdocs.org/sdr/MYWA100008), Jan 16, 2010: TRIM MOTOR. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM - CONTROL WHEEL TRIM SWITCHES DO NOT OPERATE.
- [SDR MYWA09072](https://openairdocs.org/sdr/MYWA09072), Dec 17, 2009: CONNECTOR. DIRTY. ETOPS SIGNIFICANT SYSTEM - NR 2 FUEL GAUGE AT SINGLE POINT REFUELING PANEL READING 1500 KIL LESS THAN FLIGHT DECK GAUGE.
- [SDR MYWA09062](https://openairdocs.org/sdr/MYWA09062), Nov 24, 2009: WARNING SYSTEM. ACTIVATED. ETOPS SIGNIFICANT SYSTEM - ABORTED TAKEOFF IN ATL FOR ENGINE MASTER CAUTION INDICATION. AIRSPEED LESS THAN 65 KTS.
- [SDR MYWA090056](https://openairdocs.org/sdr/MYWA090056), Nov 24, 2009: WARNING SYSTEM. MALFUNCTIONED. ABORTED TAKEOFF IN ATLANTA FOR MASTER CAUTION ENG INDICATION AIRSPEED LESS THAN 65 KTS. PERFORMED ENGINE CONTROL LIGHT BITE CHECK PER FIM 73-06-801, NO FAULTS N
- [SDR MYW2004F00007](https://openairdocs.org/sdr/MYW2004F00007), Jun 7, 2004: DISPLAY. SHORTED. DURING CRUISE, (ISFD) INTEGRATED STANDBY FLIGHT DISPLAY, DISPLAYED OUT OF ORDER MSG ONLY. AIRCRAFT DIVERTED. TROUBLESHOT SYSTEM. REMOVED AND REPLACED ISFD IAW 3
- [SDR MYW2004F00004](https://openairdocs.org/sdr/MYW2004F00004), May 23, 2004: CONTROL UNIT. SHORTED. DURING PREFLIGHT CHECK, FOUND AFT CARGO FIRE DETECTOR CIRCUIT BREAKER POPPED AND WOULD OT RESET. TROUBLESHOT SYSTEM. FOUND AFT CARGO SMOKE DETECTOR ELECTRONIC U

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Earlier aircraft with N739MA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N739MA before.

- [Cancelled 1991-05-02](https://openairdocs.org/deregistered/N739MA-1991-05-02): Mitsubishi MU-2B-26A, S/N 354SA. Exported to Brazil. Owner: [Rockwell Ditzler Assoc Inc](https://openairdocs.org/faa-owner/ROCKWELL%20DITZLER%20ASSOC%20INC), [Pittsburgh, PA](https://openairdocs.org/faa-place/PA/Pittsburgh)

## Related

- Other Magnus FUSION 212 aircraft: https://openairdocs.org/model/magnus-fusion-212/aircraft.md
- The Rotax 912ULS series engine: https://openairdocs.org/engine/rotax-912uls-series.md

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