- Registered owner
- Baur York
- Location
- Leavenworth, WA
- Owner type
- Individual
- Serial number
- 21089C
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Certificate issued
- July 8, 2020
- Expires
- July 31, 2027
- Mode S code
- A24DB7
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 5
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1996 | 1 |
|---|---|
| 1998 | 1 |
| 2000 | 1 |
| 2005 | 1 |
| 2008 | 1 |
| 2014 | 1 |
| 2022 | 1 |
Superseded and historical ADs · 2
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Maule MXT-7-180A
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemNTSB investigations
No NTSB investigations matched to N248AMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Maule MXT-7-180A aircraft
FAA incident reports
No FAA accident or incident reports matched to N248AMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Maule MXT-7-180A aircraft
Service difficulty reports
No reports matched to N248AGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Maule MXT-7-180A aircraft
Reports on N248A not matched to an aircraft · 12
They name N248A, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 99ZZZX3160Indicator · malfunctionedNOTED UPON INSTALLATION AND ENGINE LEAK/FUNCTIONAL TESTS, THAT OIL PRESSURE/TEMPERATURE INDICATOR WAS INDICATING 'LOW' PRESSURE (SYSTEM WAS BLED PRIOR TO TESTS). INSTALLED "CALIBRATED' DIRECT READING PRESSURE GAUGE FOR CONFIRMATION. ENGINE RUN-UP AND TEST COSDR 98ZZZX4271Actuator · corrodedNOTED DURING PHASE NR 1 'FLOAT' INSPECTION (SBL AAIP 50 HR), THE LT AND RT MAIN LANDING GEAR EXTEND/RETRACT ACTUATOR CYLINDER (OUTER HOUSING) INDICATED 'CELL CORROSION'. THIS CORROSION WAS NOTED AT THE MANUFACTURER'S ATTACH POINTS OF THE ELECTRICAL HARNESS (NSDR 98ZZZX4270Actuator · corrodedNOTED DURING PHASE NR 1 'FLOAT' INSPECTION (SBL AAIP 50 HR), THE LT AND RT MAIN LANDING GEAR EXTEND/RETRACT ACTUATOR CYLINDER (OUTER HOUSING) INDICATED 'CELL CORROSION'. THIS CORROSION WAS NOTED AT THE MANUFACTURER'S ATTACH POINTS OF THE ELECTRICAL HARNESS (N
STCs that may be installed · 126
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Maule MXT-7-180A
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA12472IBInstallation of the MT-Propeller Entwicklung GmbH MTV-15-B/203-58 propellerSTC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.