- Registered owner
- Boyer James A
- Location
- Lancaster, OH
- Owner type
- Individual
- Serial number
- 2675
- Year built
- 1935
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- May 30, 1955
- Certificate issued
- February 13, 2014
- Expires
- February 28, 2030
- Mode S code
- A0CD11
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 1
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
Airframe · Fairchild 24 C8C
AD 46-40-01Fuel Tank Selector Valve PlacardInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N15038Matched 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 Fairchild 24 C8C aircraft
FAA incident reports
No FAA accident or incident reports matched to N15038Matched 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 Fairchild 24 C8C aircraft
Service difficulty reports
No reports matched to N15038General 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 Fairchild 24 C8C aircraft
STCs that may be installed · 14
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Fairchild 24 C8C
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA02511SEInstallation of replacement fuel quantity indicator sending unit(s)STC SA01967WIUse of GAMI G100UL High Octane Unleaded AvgasSTC SA04776NYThe HIPEC Covering and Finishing System must be performed and maintainedSTC SA02428SEInstallation of an Air Stream Switch for an electric time recording device on non-pressurized aircraftSTC SA02283SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30PSTC SA02402SE PAGE 1Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30CSTC SA00068SEInstallation of fuel flow/pressure instruments. (W/TSIO-360-MB1)STC SA01988SEInstallation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.STC SA1008WEInstallation of Poly-Fiber covering material.STC SA5925NMInstallation of oil pressure/temperature instrument.STC SA5924NMInstallation of RPM instrument.STC SA2244CEOperation of airplane on unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index(RON+MON) /2 per ASTM Specification D-439. Intermixing with aviation gasoline also approved.STC SA4-1210Installation of Eonnex cover on aircraft surfaces.