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Aircraft record

N423FP2006 Diamond DA40 F

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 19829 ADs may apply9 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
9
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
Jul 11, 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.FC023
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
A5074F

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 (9)

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.

  • Ignition · arm · looseJul 15, 2010

    DISTRIBUTOR 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 AND WAS FOUND DURING AN INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ignition · arm · looseJul 15, 2010

    DISTRIBUTOR 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 AND WAS FOUND DURING AN INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ice and rain protection · control arm · brokenFeb 6, 2008

    CARBURETOR HEAT CONTROL ARM BROKE OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE. RECOMMEND INSTALLIING THICKER MATERIAL ON CARB HEAT CONTROL ARM LEVER, DIFFERENT WELDING/HEAT TREATING PROCESS, OR DIFFERENT ATTACHMENT PROVISION ALTOGETHER. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reports
  • Power plant · control arm · brokenNov 26, 2007

    CARBURETOR HEAT CONTROL ARM BROKEN OFF OF CARB AIR BOX CAUSING UNCONTROLLED SELECTION OF CARB HEAT VS RAM (COLD) AIR INTAKE. RECOMMEND INSTALLED THICKER MATERIAL ON CARB HEAT CONTROL ARM LEVER. DIFFERENT WELDING PROCESS, OR DIFFERENT ATTACHMENT PROVISION ALTOGETHER. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · control arm · brokenOct 18, 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.
  • Power plant · control arm · brokenSep 13, 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.
  • Fuel · pump · inoperativeJul 27, 2007

    AFTER 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 PROPER COOLING OF THE FUEL PUMP AND MOTOR. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · gearshaft · seizedJan 5, 2007

    REMOVED VACUUM DRIVE ASSEMBLY AND FOUND DRIVE GEAR SHAFT SEIZED AND (3) TEETH BROKEN OFF OF DRIVE GEAR. FURTHER INSPECTION REVEALED NO LUBRICATION PORT FOR PRESSURIZED ENGINE OIL TO LUBRICATE THE DRIVE GEAR SHAFT. ALL (3) TEETH WER FOUND IN THE OIL PUMP INLET SCREEN. (K)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · cap · leakingOct 10, 2006

    UPON PREFLIGHT OF THE AIRCRAFT, AND AFTER SITTING OUTSIDE OF THE HANGAR DURING A RAINSTORM, 2 OR 3 SUMP GLASSES WERE FILLED WITH WATER FROM EACH WING FUEL TANK SUMP DRAIN. FURTHER INSPECTION OF 9 OTHER AC OF THE SAME MAKE AND MODEL FOUND 2 OTHER AC WITH SIMILAR AMOUNTS OF WATER IN THE SUMP DRAINS.…

    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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