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Aircraft record

N152PH2012 Agustawestland Philadelphia AW139

Registration validUnclaimedSource: FAA, updated Oct 17, 2026

Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply9 service difficulty reports

Registration
Valid
expires Sep 30, 2029
Based in
Lafayette, LA
owner city / state
Engine
PT6C-67C · 1679 hp
P&W Canada
Owners
1
since 2019
NTSB events
None
since 1982
ADs may apply
1
confirm with A&P
Service reports
9
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Registered owner
Phi Aviation LLC
Owner type
LLC
City, state
Lafayette, LA
Certificate issued
Sep 4, 2019
Expires
Sep 30, 2029
Airworthiness
Standard · Transport
Airworthiness date
Nov 20, 2012

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
Agustawestland Philadelphia
Model
AW139
Year
2012
Serial number
41316
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
A0D2EA

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. 2019 – nowPhi Aviation LLCLafayette, LA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (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.

  • Main rotor drive · connector · contaminatedJun 28, 2024

    AFTER TAKE-OFF DURING CLIMB OUT MAIN GEAR BOX CHIP SUMP KEEP CAME ON AND OFF NONSTOP. RTB. FOUND OIL & WATER IN SUMP CHIP PLUG CONNECTOR. CLEANED CONNECTOR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · engine · inoperativeMay 2, 2023

    DURING TAKEOFF, BUT PRIOR TO DP, PIC NOTED LARGE TORQUE SPLIT AND#2 ENGINE OPERATING OUT OF LIMITS. ABORTED TAKEOFF.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · damper · departedAug 29, 2022

    ON A NORMAL APPROACH TO THE H AT THE NORTH RAMP, AT ABOUT 150 AGL, WE SUDDENLY FELT A STRONG VIBRATION. WE PROCEEDED TO LAND AND SHUT DOWN ON THE H (NO TAXI). POST FLIGHT REVEALED THAT ONE TAIL ROTOR DAMPER DEPARTED THE AIRCRAFT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 9 reports
  • Hydraulic power · module · leakingOct 7, 2019

    DURING BEFORE LANDING CHECK, MAIN GEAR FAILED TO LOCK DOWN. EMERGENCY PROCEDURE PERFORMED, GEAR LOCKED DOWN WITH BUTTON. NR 2 HYDRAULIC MODULE LEAKING INTERNALLY. MODULE TO BE REPLACED WITH SERVICEABLE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · control panel · odorJun 5, 2019

    ON SHORT FINAL, A WAFT OF SMOKE ENTERED THE COCKPIT ACCOMPANIED BY ELECTRICAL BURNING SMELL. LIGHT CONTROL PANEL HAS SMOKE SMELL. CONTROL PANEL WILL BE REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · structure · separatedMar 22, 2018

    LEFT SIDE BONDED PANEL SEPERATED ON SIDE SKIN AT BOOM STATION FROM 9970 TO 10.149 ON INSIDE SKIN TWO PLACES BOOM STATION 9817 TO 9868 AND 9970 TO 10.274. REPLACED TAIL STRUCTURE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · structure · separatedMar 22, 2018

    SEPERATION INSIDE BOOM IN VERTICAL PYLON AREA BOOM STATION 11,951 TO 12,052. REPLACED WITH NEW TAIL STRUCTURE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Tail rotor · erosion shield · brokenJun 9, 2017

    AFTER REVIEW OF HUMS DOWNLOAD, FOUND HIGH TAIL ROTOR AND TAIL ROTOR GEARBOX READINGS. INSPECTED TAIL ROTOR AND FOUND RED TAIL ROTOR BLADE BONDING STRIP BROKEN OFF. REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Main rotor · blade · damagedJan 19, 2016

    AFTER LANDING POST FLIGHT INSPECTION REVEALED DAMAGE TO UNDERSIDE NEAR TIP OF WHITE MAIN ROTOR BLADE. FOUND YELLOW TAIL ROTOR BLADE EROSION SHIELD EXTENSION BROKE OFF AT ATTACHMENT LOCATION.

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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