# N738MA: 2020 Magnus FUSION 212

- Status: Valid registration
- Airframe: [Magnus FUSION 212](https://openairdocs.org/model/magnus-fusion-212) (registry code 06001CO, 2 seats)
- Engine: [Rotax 912 IS series](https://openairdocs.org/engine/rotax-912-is-series) (registry code 55593)
- Data sheets: [TCDS E00051EN](https://openairdocs.org/tcds/E00051EN) (BRP-Rotax GmbH & Co KG) (OpenAirDocs)
- Serial number: MF-212-20-0016
- Year built: 2020
- Type: Fixed wing single engine
- Engine type: 4 cycle
- Airworthiness: Light sport, airplane
- Airworthiness date: May 3, 2021
- Certificate issued: August 2, 2021
- Expires: August 31, 2028
- Mode S code: A9E9D7
- Registered owner: [Zipper Aviation LLC](https://openairdocs.org/faa-owner/ZIPPER%20AVIATION%20LLC)
- Location: [Shelbyville, IN](https://openairdocs.org/faa-place/IN/Shelbyville)
- Owner type: LLC
- Owner's area on the map: 39.5265° N, 85.7734° W: Placed by OpenAirDocs at the center of ZIP code 46176, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=738MA
- Page: https://openairdocs.org/aircraft/N738MA

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 912 IS model are included.

## ADs that may apply (OpenAirDocs): 3 in force

### Matched by airframe (Magnus FUSION 212)

None in force.

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

- [AD 2026-16-11](https://openairdocs.org/ad/2026-16-11): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Aug 28, 2026
- [AD 2025-15-03](https://openairdocs.org/ad/2025-15-03): Reciprocating Engine Oil System · BRP-Rotax 912 iSc2 Sport, 912 iSc3 Sport, 915 iSc2 C24 and 1 more. Effective Aug 6, 2025
- [AD 2023-17-13](https://openairdocs.org/ad/2023-17-13): Reciprocating Engine Front Section · BRP-Rotax 912 F2, 912 F3, 912 F4 and 16 more. Effective Sep 20, 2023

### Historical (superseded or no longer in force)

- [AD 2025-07-02](https://openairdocs.org/ad/2025-07-02) (historical): Reciprocating Engine Oil System · BRP-Rotax 912 iSc2 Sport, 912 iSc3 Sport, 915 iSc2 C24 and 1 more. Effective Apr 21, 2025

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N738MA.

## FAA accident and incident reports

None matched to N738MA.

## Reports on N738MA not matched to an aircraft (2)

They name N738MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Accident 20131230024219A](https://openairdocs.org/incident/20131230024219A), Dec 30, 2013: Boeing 737-8Q8 (N738MA), Boston, MA, Substantial damage, 1 fatal. N738MA a B737-800 operated by miami air was preparing for departure from the signature FBO ramp at bos. Flight crew was onboard. Signature FBO employees were…
- [Incident 19790919023789I](https://openairdocs.org/incident/19790919023789I), Sep 19, 1979: Mtsbsi MU2B26A (N738MA), Binghamton, NY. Gear door red light due to doors improperly connected. Airplane just out of maintenance.

## 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 N738MA not matched to an aircraft (53, newest 50)

They name N738MA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR MYWA2020021300157](https://openairdocs.org/sdr/MYWA2020021300157), Apr 10, 2019: BATTERY PACK. DISCHARGED. WE HAD A FEW EMERGENCY LIGHT BATTERY PACK P/N: D717-01-100 THAT FAILED DURING FUNCTIONAL CHECK. 11472,11388,11388, 11387, 11386,11385,210667,450464,458637,45874
- [SDR MYWA2017081100188](https://openairdocs.org/sdr/MYWA2017081100188), Aug 11, 2017: SUPPORT BRACKET. CRACKED. DURING A SCHEDULED INSPECTION, FOUND A CRACK AT SUPPORT BRACKET BETWEEN BS 312 TO 328, LEFT SIDE, 16 INCHES IN LENGTH. REPLACED IAW SRM 53-10-51.
- [SDR MYWA201708110187](https://openairdocs.org/sdr/MYWA201708110187), Aug 11, 2017: PLATE. CRACKED. DURING A SCHEDULED INSPECTION, FOUND A CRACK AT NUT PLATE AREA OF THE RT PLATE AT AFT CARGO BAY BS 807 TO 879, 71 INCHES IN LENGTH. REPLACED IAW SRM 53-00-53.
- [SDR 2017F00102](https://openairdocs.org/sdr/2017F00102), Jun 30, 2017: LIGHT. INOPERATIVE. AFT LEFT HAND AISLE EMERGENCY EXIT LIGHT INOP.
- [SDR MYWA2017061900253](https://openairdocs.org/sdr/MYWA2017061900253), Jun 15, 2017: LAMP. INOPERATIVE. FOUND INTERIOR LT AFT EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP.
- [SDR MYWA20121106002](https://openairdocs.org/sdr/MYWA20121106002), Nov 5, 2012: LIGHT. INOPERATIVE. DURING AIRCRAFT DAILY INSPECTION (PRE-TRANSIT CHECK), MAINTENANCE NOTED LEFT SIDE FORWARD EMERGENCY WING/SLIDE LIGHT INOPERTATIVE. RELAMPED LEFT FORWARD WING/SL
- [SDR MYWA07232012738](https://openairdocs.org/sdr/MYWA07232012738), Jul 23, 2012: CONTROL UNIT. INOPERATIVE. DURING TROUBLESHOOTING FOUND SPCU INOPERATIVE. PERFORMED OPS TEST ON STANDBY POWER SYSTEM AND CLEARED FAULT. CHECK ALL VOLTAGE READINGS NORMAL AND TEST CHECK IA
- [SDR MYWA072020127381](https://openairdocs.org/sdr/MYWA072020127381), Jul 20, 2012: CONTROL VALVE. INOPERATIVE. AT 350 HAVE PNEU DUCT SPLIT LEFT SIDE 17 PSI RT 35 PSI. TROUBLESHOT IN COMPLIANCE W/FIM 36-10 TASK 807/806, AMM 36-11-00-700-801, FOUND PRE-COOLER VALVE INOPERA
- [SDR MYWA07202012738](https://openairdocs.org/sdr/MYWA07202012738), Jul 20, 2012: VALVE. INOPERATIVE. 20 PSI DUCT PRESSURE SPLIT AT FL350 IN CRUISE. LEFT INDICATING 17 PSI. RT INDICATING 37 PSI. TROUBLESHOT IAW FIM 36-10 TASK 807/906 AMM 36-11-00-700-801. FOUND 
- [SDR MYWA2012F00118](https://openairdocs.org/sdr/MYWA2012F00118), Jun 24, 2012: DOOR. UNKNOWN. AIR RETURN DUE TO L-1 DOOR NOT SEALING. ALL LIGHT INDICATIONS PRIOR TO T/O WERE NORMAL. CYCLED L-1 DOOR SEVERAL TIMES, OPS CHECKS NORMAL IAW AMM 52-11-00 ACFT O
- [SDR MYWA120051](https://openairdocs.org/sdr/MYWA120051), Apr 25, 2012: LENS. MISSING. L-2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LOWER EXIT SIGN ASSY PER B737-800 AMM 33-51-01, OPS CHECKED GOOD.
- [SDR MYWA120038S](https://openairdocs.org/sdr/MYWA120038S), Mar 27, 2012: WIRE. SHORTED. FOUND EMERGENCY AISLE LIGHT ON ROW 25 RT INOPERATIVE. DURING TROUBLESHOOTING, FOUND WIRE W0154-0040-20 GROUNDED AT L1419 CEILING LIGHT ASSY AND BLOWING FUSE F3 
- [SDR MYWA120038](https://openairdocs.org/sdr/MYWA120038), Mar 27, 2012: LIGHT. INOPERATIVE. DURING PT FOUND EMERGENCY AISLE LIGHT ON ROW 25 RT INOP.
- [SDR MYWA120034](https://openairdocs.org/sdr/MYWA120034), Mar 15, 2012: WARNING SYSTEM. INTERMITTENT. ETOPS SIGNIFICANT SYSTEM: CONT CAB ZONE TEMP LIGHT ILLUMINATED ON RECALL. PERFORMED BITE TEST AND DETERMINED FAULT INTERMITTENT IAW MM 21-62 TASK 804. NO FURTHE
- [SDR MYWA110139](https://openairdocs.org/sdr/MYWA110139), Dec 23, 2011: WARNING SYSTEM. FALSE ACTIVATION. ETOPS SIGNIFICANT SYSTEM: ON POWER UP FOR TAKE OFF ENG MASTER CAUTION ILLUMINATED. BOTH ALT EEC'S ILLUMINATED. LOW SPEED ABORT PERFORMED. PERFORMED BITE CHECK, 
- [SDR MYWA110121](https://openairdocs.org/sdr/MYWA110121), Nov 30, 2011: FILTER. DIRTY. ETOPS SIGNIFICANT SYSTEM: #2 ENG IDG DPI POPPED. R&R #2 IDG SCAVENGE FILTER. DRAINED OIL R&R #2 IDG CASE DRAIN FILTER. SERVICED IDG IAW 24-11-41 NO LEAKS NOTED.
- [SDR MYWA110115](https://openairdocs.org/sdr/MYWA110115), Nov 2, 2011: HMU. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: NR 2 ENG SLOW TO ACCELERATE. FAULT CODE 75-10392. REMOVED AND REPLACED NR 2 ENGINE HMU PER B737-800 AMM 73-21-10 OPS CHECK NORMAL. NO 
- [SDR MYWA110106](https://openairdocs.org/sdr/MYWA110106), Nov 1, 2011: SENSOR. DEFECTIVE. ETOPS SIGNIFICANT SYSTEM: ENG NR 2 NO BLEED WHEN SW SELECTED WITH ENGINE RUNNING. PER HEALTH CHECK REMOVED AND REPLACED 450 SENSOR IAW AMM 36-11-05. REMOVED AND
- [SDR MYWA110095](https://openairdocs.org/sdr/MYWA110095), Aug 30, 2011: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFCANT SYSTEM: DUCT PRESSURE INDICATION L&R POINTERS NOT THE SAME (SPLIT) THE ENGINE IS THE BLEED SOURCE L20/R41 / 92.2N1 / FL360. AS PER BOEING 737-8
- [SDR MYWA110090](https://openairdocs.org/sdr/MYWA110090), Aug 17, 2011: UNKNOWN. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: APU DOES NOT START, NO APU INDICATION LIGHTS ON. PERFORMED APU BITE. TEST OK NO FAULTS FOUND IAW FIM 49-15 TASK 805 AND OPERATIONAL SY
- [SDR MYWA110074](https://openairdocs.org/sdr/MYWA110074), Jul 13, 2011: WARNING SYSTEM. ACTIVATED. ETOPS SIGNIFICANT SYSTEM: LEFT PACK LIGHT ON GROUND, LIGHT STAYS OFF AFTER RESET. PERFORMED BITE TEST TO LT ZONE CONTROLLER BITE TEST PASSED AT THIS TIME. NO LT
- [SDR MYWA110066A](https://openairdocs.org/sdr/MYWA110066A), Jul 5, 2011: CONTROLLER. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: LEFT PACK LIGHT ILUMINATED ON RECALL. PERFORMED RESET OF PACK CONTROLLER IAW 737-800 21-62 -00, OPS CHECKS OK.
- [SDR MYWA110065](https://openairdocs.org/sdr/MYWA110065), Jul 5, 2011: CONTROLLER. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: LEFT PACK LIGHT ILLUMINATES IN FLIGHT DURING "RECALL" LIGHT WILL RESET WITH MASTER CAUTION. PERFORMED BITE TO LEFT ZONE TEMP CONTROLLE
- [SDR MYWA110064](https://openairdocs.org/sdr/MYWA110064), Jul 4, 2011: CONTROLLER. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: ZONE TEMP LIGHT ON, COMES ON AGAIN ON REST (CONT CABIN). REMOVED AND REPLACED NR 2 ZONE TEMP CONTROLLER IAW 737-800 AMM 21-61-00, OPS 
- [SDR MYWA110063](https://openairdocs.org/sdr/MYWA110063), Jul 2, 2011: CONTROLLER. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM: LEFT PACK LIGHT ON, ON RECALL. PERFORMED BITE TEST OF (L) PACK CONTROLLER RESET CONTROLLER NO FAULTS DETECTED NO PACK LIGHT ON RECALL,
- [SDR MYWA110047](https://openairdocs.org/sdr/MYWA110047), Jun 6, 2011: WARNING SYSTEM. FALSE ACTIVATION. ETOPS SIGNIFICANT SYSTEM: RIGHT AFTER NR 1 ENGINE START ENGINE OVERHEAT LIGHT CAME ON NR 1 ENGINE LOOP "A" INOP. C/W NR 1 ENGINE LOOP "A" INSP IAW AMM 26-21-00.
- [SDR MYWA110032](https://openairdocs.org/sdr/MYWA110032), Mar 9, 2011: CONNECTOR. UNSECURE. ETOPS SIGNIFICANT SYSTEM: CENTER RIGHT FUEL LOW PRESSURE LIGHT DOESN'T ILLUMINATE WHEN LOW OR NO PRESSURE. FOUND RT CTR FUEL LOW PRESSURE SWITCH CONNECTOR NOT F
- [SDR MYWA110021](https://openairdocs.org/sdr/MYWA110021), Feb 11, 2011: BATTERY. WEAK. ETOPS SIGNIFICANT SYSTEM: ON OPS CHECK OF APU, APU WAS SLOW TO START DUE TO WEAK BATTERIES.
- [SDR MYWA110022](https://openairdocs.org/sdr/MYWA110022), Feb 10, 2011: CONTROL VALVE. FAILED. ETOPS SIGNIFICANT SYSTEM: NR 2 ENGINE PRECOOLER CONTROL VALVE AND WING TAI SOLENOID FAIL TEST. REPLACED PRECOOLER CONTROL VALVE.
- [SDR MYWA100135](https://openairdocs.org/sdr/MYWA100135), Dec 23, 2010: SMOKE DETECTOR. NO TEST. ETOPS SIGNIFICANT SYSTEM: AFT CARGO FIRE DETECTOR "A" LOOP DID NOT TEST. REPLACED A-2 SMOKE DETECTOR SYSTEM CHECK NORMAL.
- [SDR MYWA100130](https://openairdocs.org/sdr/MYWA100130), Dec 18, 2010: VALVE. INOPERATIVE. ETOPS SIGNIFICANT SYS: DURING CLIMB, THROUGH FL240, LT DUCT PRESSURE INDICATED 22 PSI AND RT DUCT PRESSURE INDICATED 42 PSI. REPLACED NR1 ENGINE HIGH STAGE VALV
- [SDR MYWA100129](https://openairdocs.org/sdr/MYWA100129), Dec 17, 2010: UNKNOWN. UNKNOWN. ETOPS SIGNIFICANT SYSTEM: DURING CLIMB THROUGH FL370, LEFT DUCT PRESSURE INDICATED 22 PSI AND RIGHT DUCT PRESSURE INDICATED 45 PSI. AFTER LANDING ACCOMPLISHED H
- [SDR MYWA100128](https://openairdocs.org/sdr/MYWA100128), Dec 17, 2010: TERMINAL. LOOSE. ETOPS SIGNIFICANT SYSTEM: DURING TAXI R2 WINDOW OVERHEAT ILLUMINATED. FOUND WINDOW HEAT SENSOR TERMINAL LOOSE. RE-SECURED AND OPS CHECK NORMAL.
- [SDR MYWA100125](https://openairdocs.org/sdr/MYWA100125), Dec 3, 2010: INDICATOR. INOPERATIVE. ETOPS SIGNIFICANT SYS: PRESSURIZATION CONTROL PANEL LCD INDICATORS NOT WORKING CORRECTLY, SYS OK.
- [SDR MYWA100112](https://openairdocs.org/sdr/MYWA100112), Oct 3, 2010: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM: PUMP SYSTEM "A" ELECTRIC LIGHT ILLUMINATED WITH SWITCH IN THE ON POSITION.
- [SDR MYWA100111](https://openairdocs.org/sdr/MYWA100111), Oct 3, 2010: WARNING SYSTEM. ACTIVATED. ETOPS SIGNIFICANT SYSTEM: "A" HYD SYSTEM LOW PRESSURE LIGHT ILLUMINATED DURING CRUISE.
- [SDR MYWA100104](https://openairdocs.org/sdr/MYWA100104), Sep 7, 2010: WARNING LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM: AUTO FAIL LIGHT AND ALTN LIGHT ON, OFF WHEN ALTN SELECTED.
- [SDR MYWA100098](https://openairdocs.org/sdr/MYWA100098), Aug 8, 2010: ANTI-ICE SYSTEM. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM: FLIGHTDECK L1 WINDOW HEAT INOP.
- [SDR MYWA100088](https://openairdocs.org/sdr/MYWA100088), Jun 19, 2010: LIGHT. ILLUMINATED. ETOPS SIGNIFICANT SYSTEM - AFT CABIN ZONE TEMP LIGHT COMES DURING RECALL.
- [SDR MYWA100089](https://openairdocs.org/sdr/MYWA100089), Jun 2, 2010: STRAP. BROKEN. ETOPS SIGNIFICANT SYSTEM - CAPTS O2 MASK STRAP BROKEN.
- [SDR MYWA100080](https://openairdocs.org/sdr/MYWA100080), May 27, 2010: OVERHEAT LOOP. NO TEST. ETOPS SIGNIFICANT SYSTEM - NR 2 ENGINE B-LOOP OVERHEAT DETECTION WOULD NOT TEST.
- [SDR MYWA100071](https://openairdocs.org/sdr/MYWA100071), May 2, 2010: BLEED AIR SYS. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - NO BLEED AIR FROM APU.
- [SDR MYWA100058](https://openairdocs.org/sdr/MYWA100058), Apr 23, 2010: ACTUATOR. LEAKING. ETOPS SIGNIFICANT ITEM - NR 12 SPOILER ACTUATOR LEAKING REF DMI 229543/14.
- [SDR MYWA100057](https://openairdocs.org/sdr/MYWA100057), Apr 22, 2010: ACTUATOR. LEAKING. ETOPS SIGNIFICANT ITEM - NR 12 SPOILER ACTUATOR LEAKING.
- [SDR MYWA100055](https://openairdocs.org/sdr/MYWA100055), Apr 10, 2010: LIGHT. ILLUMINATED. ETOPS SIGNIFICANT ITEM - CONTROL CABIN LIGHT ILLUMINATES ON RECALL AND GOES OUT ON MASTER CAUTION RESET.
- [SDR MYWA100032](https://openairdocs.org/sdr/MYWA100032), Feb 8, 2010: APU. SHUTDOWN. ETOPS SIGNIFICANT SYSTEM - APU AUTO SHUTDOWN ON START.
- [SDR MYWA100007](https://openairdocs.org/sdr/MYWA100007), Jan 8, 2010: SENSOR. INOPERATIVE. ETOPS SIGNIFICANT SYSTEM - ON DESCENT LT "BLEED TRIP OFF" LIGHT ILLUMINATED. RESET = OFF LT DUCT PRESSURE "0" RESET TWICE.
- [SDR MYWA100004](https://openairdocs.org/sdr/MYWA100004), Jan 3, 2010: SHUTOFF VALVE. MALFUNCTIONED. ETOPS SIGNIFICANT SYSTEM - DESENDING FROM FLT LEVEL 410 LEFT BLEED TRIP OFF LIGHT ILLUMINATED, RESET OK. DESENDING FROM 310 BLEED TRIP OFF AGAIN.
- [SDR MYWA09075](https://openairdocs.org/sdr/MYWA09075), Dec 24, 2009: APU. FAILED. ETOPS SIGNIFICANT SYSTEM - APU FAILED TO START, OVERTEMP AUTO SHUTDOWN.
- [SDR MYWA09073](https://openairdocs.org/sdr/MYWA09073), Dec 17, 2009: START VALVE. OPEN. ETOPS SIGNIFICANT SYSTEM - NR 2 ENG START VALVE REMAINS OPEN DURING ENGINE START.

All 53: https://openairdocs.org/aircraft/N738MA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

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

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