- Registered owner
- Utah State University
- Location
- Logan, UT
- Owner type
- Government
- Serial number
- 40.FC022
- Year built
- 2006
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal, utility
- Airworthiness date
- July 5, 2006
- Certificate issued
- July 17, 2006
- Expires
- December 31, 2027
- Mode S code
- A50398
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 N422FPMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2018FA0000397Attach Bolt · shearedLEFT HAND, FWD LANDING GEAR BRACE BOLT SHEARED LEVEL WITH THE NUT. ALSO CAUSED DELAMINATION OF A PORTION OF THE FUSELAGE DIRECTLY UNDERNEATH THE LANDING GEAR BRACE POINT. FOUND DURING 100 HOUR INSPECTION.SDR 2009FA0000499Window · debondedRT REAR FUSELAGE CABIN WINDOW DISBONDED FROM FUSELAGE ALONG THE FWD EDGE OF WINDOW. WINDOW CONTINUES TO FLEX OUTWARD WITH CABIN AIR PRESSURE DURING FLIGHT. SUBSEQUENT REMOVAL OF WINDOW CLEARLY SHOWS NO BOND BETWEEN THE STRUCTURAL ADHESIVE AND THE FWD EDGE OSDR 2009FA0000498Hinge · debondedUPON PRE-FLIGHT, PILOT FOUND FWD HINGE OF LT REAR DOOR ASSY TO BE CRACKED OR DEBONDED WHERE HINGE ENTERS THE DOOR ASSY. DOOR REMOVED FOR REPAIR BY MFG. (K)SDR 2007FA0000787Air Box · brokenCARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE WHILE IN FLIGHT. (K)SDR 2007FA0000057Attach Fitting · bentAFT CABIN DOOR ASSY SEPARATED FROM AC DURING FLIGHT. CONTROL OF THE AC WAS MAINTAINED AND LANDED SAFELY AT DEPARTURE AIRPORT. DOOR WAS EVENTUALLY RECOVERED AND UPON VISUAL INSPECTION OF THE DOOR, THE AFT DOOR LATCH PIN WAS NOT ENGAGED. THE FRONT DOOR LATCH
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