- Registered owner
- Utah State University
- Location
- Logan, UT
- Owner type
- Government
- Serial number
- 40.FC024
- Year built
- 2006
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- July 10, 2006
- Certificate issued
- July 17, 2006
- Expires
- December 31, 2027
- Mode S code
- A50B06
Diamond Aircraft Ind DA40 FTCDS A47CEAirframe · Diamond Aircraft Ind DA40 FTCDS E-286Engine · Lycoming O-360-A4M
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 33
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1963 | 1 |
|---|---|
| 1967 | 1 |
| 1969 | 1 |
| 1977 | 1 |
| 1980 | 1 |
| 1981 | 1 |
| 1982 | 1 |
| 1989 | 2 |
| 1991 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 1 |
| 2004 | 1 |
| 2006 | 4 |
| 2007 | 3 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 2 |
| 2014 | 2 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2024 | 2 |
| 2026 | 2 |
Airframe · Diamond Aircraft Ind DA40 F
AD 2026-06-03Hoses and tubesAD 2024-19-08Nose/Tail Landing GearAD 2022-13-06Cargo CompartmentsInformation bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Diamond Aircraft Ind DA40 F
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-09-12Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 InstallationsSAIB CE-08-14Electrical PowerEngine · Lycoming O-360-A4M
SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersSAIB NE-08-32R1Propeller Governor Idler Gear Shaft Set ScrewSAIB NE-14-13Reciprocating Engine - Cylinder Mounting StudsSAIB NE-13-06Pushrod Shroud Spring Retainers, Engine Components Part No. AEL14995, for Lycoming Engines 320, 360, and 540 Series EnginesSAIB NE-06-32R1Reciprocating Engine - CrankshaftHistorical bulletins · 1
NTSB investigations
No NTSB investigations matched to N424FPMatched 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 Diamond Aircraft Ind DA40 F aircraft
FAA incident reports
No FAA accident or incident reports matched to N424FPMatched 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 Diamond Aircraft Ind DA40 F aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2024FA0000787Bolt · brokenRIGHT MAIN LANDING GEAR ATTACHMENT BOLT BROKE. ONE OF TWO THAT HOLD THE OUTBOARD GEAR LEG ATTACHED THE SECOND BOLT WAS BENT FROM BEING THE ONLY BOLT HOLDING THE GEAR LEG IN PLACE. THE PILOTS CAN NOT SEE THE BOLT IS BROKEN DURING PER-FLIGHTS AND COULD MAKE AS MSDR 2023FA0000529Pressure Switch · leakingDURING CURSE FLIGHT THE PILOT NOTICED THE OIL PRESSURE GAUGE START FLICKERING JUST A LITTLE AND DECIDED TO RETURN TO THE AIRPORT. THE FLIGHT BACK TO THE AIRPORT TOOK ABOUT 15 MINS. AS THE PILOTS EXITED THE AIRPLANE THEY NOTICED OIL ALL OVER IT. MAINTENANCE FOUSDR 2017FA0000285Pressure Switch · leakingDURING PRE-FLIGHT, THE PILOT DISCOVERED A LARGE OIL SPOT ON GROUND COMING FROM ENGINE COWLING. REMOVED THE ENGINE COWLING, DISCOVERED THE OIL PRESSURE SWITCH TO BE LEAKING.SDR 2010FA0000795Arm · looseDISTRIBUTOR ARM COMING LOOSE FORM THE GEAR. WHEN THE ARM COMES LOOSE, IT CAUSES WEAR ON THE ARM CTR AND AS THE CTR WEARS TO A LARGER DIAMETER HOLE, THE ARM FLIES OUT CLOSING THE GAP AND GRINDS INTO THE CONTACTS OF THE DISTRIBUTOR BLOCK. THE MAG RAN NORMAL ANSDR 2009FA0000496Window · debondedRT REAR FUSELAGE CABIN WINDOW DISBONDED FROM FUSELAGE ALONG THE FWD EDGE OF WINDOW. WINDOW CONTINURE TO FLEX OTWARD WITH CABIN AIR PRESSURE DURING FLIGHT. SUBSEQUENT REMOVEAL OF WINDOW CLEARLY SHOWS NO BOND BETWEEN THE STRUCTURAL ADHESIVE AND THE FWD EDGE OFSDR 2008FA0000136Pump · inoperativeAFTER A PREVIOUS FLIGHT, AND BEFORE THE NEXT STUDENTS FLIGHT, THE ELECTRIC FUEL PUMP WAS FOUND TO BE INOPERATIVE. INADEQUATE COOLING IS WHAT WE BELIEVE TO BE THE SOURCE OF THE MALFUNCTIONS. PROVIDE RAM AIR FOR PROPER COOLING OF FUEL PUMP AND MOTOR. (K)
STCs that may be installed · 99
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Diamond Aircraft Ind DA40 F
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA12428CHInstallation of the Lycoming Engines Electronic Ignition System (EIS)STC SA02279ATInstallation of a Boom Beam bulb, starter, and ballast