Registered owner
Utah State University
Location
Logan, UT
Owner type
Government
Serial number
40.FC017
Year built
2006
Type
Fixed wing single engine
Engine
Reciprocating
Airworthiness
Standard, normal, utility
Airworthiness date
July 6, 2006
Certificate issued
July 17, 2006
Expires
December 31, 2027
Mode S code
A4EEAC

From the FAA registry file of October 22, 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 N417FPMatched 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 N417FPMatched 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 · 5

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2023FA0000060Bolt · brokenRIGHT OUTBOARD FORWARD MAIN LANDING GEAR MOUNT BOLT BROKE. BOLT NOT BEING SEEN BROKEN DURING PREFLIGHT INSPECTIONS AND LOOKS TO HAVE BEEN BROKEN FOR A LOT OF HOURS BEFORE BEING FOUND DURING THE 100 HOUR INSPECTION. NEXT BIGGER SIZE BOLT SHOULD FIX THE PROBLEMFeb 1, 2023 · N417FP · Diamon DA40 · Standard Practices/StructuresSDR 2018FA0000396Attach Bolt · shearedFOUND RH FRWD LANDING GEAR ATTACH BOLT SHEARED AT BOLT THREADS DURING 100 HR INSPECTION. FORCE OF BOLT BREAKING CAUSED ATTACHMENT PLATE TO HIT BOTTOM OF FUSELAGE DELAMNINATING OUTER SKIN FROM FUSELAGE.Oct 1, 2018 · N417FP · Diamon DA40 · Main Landing Gear Attach SectionSDR 2017FA0000172Lever · crackedFOUND CRACK IN ELEVATOR MASS BALANCE LEVER 7INCH FROM THE AFT END. CRACK WAS FOUND DURING A NORMAL 100 HOUR INSPECTION.May 3, 2017 · N417FP · Diamon DA40 · Elevator StructureSDR 2008FA0000128Pump · 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)Feb 15, 2008 · N417FP · Diamon DA40 · Fuel Boost PumpSDR 2006FA0001050Wire Harness · damagedTOTAL ELECTRICAL SYSTEM FAILURE IN FLIGHT. INSPECTION REVEALED THAT THE MAIN POWER WIRE’S RING TERMINAL TO THE ALTERNATOR HAD FAILED CAUSING ARCING WHICH SHORTED THE ALTERNATOR OUT AND CAUSED THE MAIN AND ESSENTIAL BUSS CIRCUIT BREAKERS TO POP. POSSIBLE CAUSOct 25, 2006 · N417FP · Diamon DA40 · Engine System Wiring

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