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Aircraft record

N425FP2006 Diamond DA40 F

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply3 service difficulty reports

Registration
Valid
expires Dec 31, 2027
Based in
Logan, UT
owner city / state
Engine
O-360-A4M · 180 hp
Lycoming
Owners
1
since 2006
NTSB events
None
since 1982
ADs may apply
9
confirm with A&P
Service reports
3
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Utah State University
Owner type
Government
City, state
Logan, UT
Certificate issued
Jul 17, 2006
Expires
Dec 31, 2027
Airworthiness
Standard · Normal, Utility
Airworthiness date
Jun 20, 2006

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Diamond
Model
DA40 F
Year
2006
Serial number
40.FC025
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A50EBD

Engine

Make and model
Lycoming O-360-A4m
Type
Reciprocating
Power
180 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2006 – nowUtah State UniversityLogan, UT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (9)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2026-06-03Hoses and tubesApr 30, 2026Airframe (DA40 F)
2024-19-08Nose/Tail Landing GearNov 29, 2024Airframe (DA40 F)
2022-13-06Cargo CompartmentsAug 11, 2022Airframe (DA40 F)Only with: Includes Model DA 40 D airplanes that have been converted to Model DA 40 NG airplanes.
2014-13-08WingsAug 27, 2014Airframe (DA40 F)Certain serial numbers: DA 40 40.006–40.009; DA 40 40.011–40.1071; DA 40 40.1073–40.1077; DA 40 F 40.FC001–40.FC029
2010-25-01Diamond Aircraft Industries GmbH Models DA 40 and DA 40F AirplanesJan 11, 2011Airframe (DA40 F)
Show all 9 ADs
ADSubjectEffectiveApplies to
2009-07-14Diamond Aircraft Industries GmbH Model DA 40 and DA 40F AirplanesMay 11, 2009Airframe (DA40 F)Certain serial numbers: DA 40 40.377; DA 40 40.420; DA 40 40.422; DA 40 40.644–40.693; DA 40 40.695–40.842; DA 40 40.844; …
2006-10-21Engine Components Incorporated (ECi) Reciprocating Engine Connecting RodsJun 22, 2006Engine (O-360-A4M)Only with: ECi connecting rods P/N AEL11750 (forging P/N AEL11488) installed, rod serial numbers 54/6 and below, produced between January 2002 and January 2004.
2006-06-16Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, and…Apr 27, 2006Engine (O-360-A4M)Only with: Engines manufactured new or rebuilt, overhauled, or that had a crankshaft installed after March 1, 1999.
2005-19-11Lycoming Engines (Formerly Textron Lycoming) AEIO-360, IO-360, O-360, LIO-360, LO-360…Oct 21, 2005Engine (O-360-A4M)Only with: Engines rated at 300 HP or lower, manufactured new, rebuilt, or overhauled after March 1, 1999, or that had a crankshaft installed after March 1, 1999.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (3)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Landing gear · bolt · brokenNov 9, 2023

    RIGHT AFT MAIN LANDING GEAR BOLT BROKE. THIS IS ONE OF TWO OUTBOARD MOUNT BOLTS THIS BOLT WAS INSTALLED NEW 10/03/2018 AND HAD 2764.6 TTSN THE BOLT BROKE IN THE THREADED AREA. THE PILOTS CANNOT SEE THE BOLTS DURING THE PRE-FLIGHT INSPECTION AND CAN MAKE HUNDREDS OF LANDING WITH THE BOLT BROKEN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · window · debondedMay 19, 2009

    RT REAR FUSELAGE CABIN WINDOW DISBONDED FROM FUSELAGE ALONG THE FWD EDGE OF WIINDOW. 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 OF THE WINDOW. REINSTALLED WINDOW IAW MFG…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · air box · brokenMay 16, 2007

    CARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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