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

From the FAA registry file of October 24, 2026.

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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.

1963In forceSuperseded2026
ADs by the year they took effect: 41 ADs
19631
19671
19691
19771
19801
19811
19821
19892
19911
19921
19951
19962
19971
20041
20064
20073
20082
20092
20101
20111
20122
20142
20171
20201
20222
20242
20262
See all 41 ADs

Information bulletins that may apply · 8

Advisory, not mandatory.

Historical 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.Oct 1, 2018 · N422FP · Diamon DA40 · Main Landing Gear Attach SectionSDR 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 OMay 19, 2009 · N422FP · Diamon DA40 · Passenger Compartment WindowsSDR 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)May 19, 2009 · N422FP · Diamon DA40 · Fuselage, Door HingeSDR 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)May 21, 2007 · N422FP · Diamon DA40 · Engine Air Intake SystemSDR 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 Jan 5, 2007 · N422FP · Diamon DA40 · Passenger/Crew Doors

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.

See all 99 STCs