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Aircraft record

N303FD2008 Agusta Spa AW139

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply7 service difficulty reports

Registration
Valid
expires Oct 31, 2028
Based in
Van Nuys, CA
owner city / state
Engine
PT6C-67C · 1679 hp
P&W Canada
Owners
1
since 2008
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
7
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Los Angeles City
Owner type
Government
City, state
Van Nuys, CA
Certificate issued
Oct 17, 2008
Expires
Oct 31, 2028
Airworthiness
Standard · Transport
Airworthiness date
Oct 6, 2008

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
Agusta Spa
Model
AW139
Year
2008
Serial number
41012
Aircraft type
Rotorcraft
Category
Land
Certification
Type Certificated
Seats
17
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Type certificate data sheet
R00002RD
Mode S code
A32AF8

Engine

Make and model
P&W Canada Pt6c-67c
Type
Turbo-shaft
Power
1679 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. 2008 – nowLos Angeles CityVan Nuys, CA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (1)

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
2013-03-14Pratt & Whitney Canada Corp Turboshaft EnginesMar 26, 2013Engine (PT6C-67C)Only with: Engines that have not had P&WC Service Bulletin No. PT6C-72-41056 incorporated.

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

Service Difficulty Reports (7)

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.

  • Fuselage · skin · delaminatedApr 5, 2018

    MAJOR DELAMINATION ON THE TAILBOOM SKIN.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · contactor · burnedApr 2, 2016

    AFTER EXECUTING SEVERAL PRACTICE HOIST EVOLUTIONS, SMELLED A FAINT ODOR OF BURNING ELECTRICAL AND SIMULTANEOUSLY EXPERIENCED A 2 GEN FAIL WITH A BUS TIE FAIL IN THE CAS WINDOW. THE ACFT EXPERIENCED A K10 BUSS TIE CONTACTOR FAILURE. THIS CONTACTOR CONNECTS THE NR 1 AND NR 2 MAIN LOAD BUSES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · indicator · malfunctionedAug 4, 2009

    IN FLIGHT CAS MESSAGE INTERMITTANTLY ILLUMINATED: NR 1 AHRS FAIL, NR 1 AP FAIL, AFCS DEGRADED, AVIONICS FAIL. REPLACEMENT OF AHRU CORRECTED THE SQUAWK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Fuselage · skin · deformedJul 2, 2009

    TAIL ASSY LT AND RT SIDES , SKIN DEFORMATION BETWEEN STA 8700.1 TO 9436.1 AND BETWEEN WL 2176.8 TO 2060.8. SKIN IS BUBBLING OTBD BETWEEN THE 2 HONEYCOMB AREAS OF THE PANEL ON BOTH SIDES OF BOOM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Autoflight · unknown · multiple failJul 2, 2009

    LOW TORQUE INDICATION (30-40 PERCENT) ON BOTH PILOT'S AND COPILOT'S PFD/MFD DURING MAX GROSS WEIGHT TAKEOFF. CAS INDICATIONS: 1 AP FAIL, AVIONIC FAULT, 1 AHRS FAIL, AFCS DEGRADED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Equipment and furnishings · hook · unserviceableJun 26, 2009

    PERFORMED SB 42315-489-01, THE HOOK HAS UNACCEPTABLE IRREGULARITIES AND DISCONTINUITIES. REMOVED HOOK FROM SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · probe · inoperativeJun 18, 2009

    FUEL QUANTITY READS ZERO. NO SIGNAL FROM PROBE. REPLACEMENT PROBE FIXED DISCREPANCY.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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