# N139JP: 2005 Agusta AB139, registration cancelled 2024-09-10 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 10, 2024 - Status when cancelled: Valid registration - Airframe: [Agusta AB139](https://openairdocs.org/model/agusta-ab139) (registry code 0260110) - Engine: [Pratt & Whitney Canada PT6C-67C](https://openairdocs.org/engine/pratt-whitney-canada-pt6c-67c) (registry code 52174) - Data sheets: [TCDS R00002RD](https://openairdocs.org/tcds/R00002RD), [TCDS E00068EN](https://openairdocs.org/tcds/E00068EN) (OpenAirDocs) - Serial number: 31039 - Year built: 2005 - Type of aircraft: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, transport - Airworthiness date: March 31, 2008 - Certificate issued: May 15, 2006 - Last registry action: October 20, 2023 - Mode S code: A09D76 - Owner when cancelled: [Chevron U S A Inc](https://openairdocs.org/faa-owner/CHEVRON%20U%20S%20A%20INC) - Location: [Picayune, MS](https://openairdocs.org/faa-place/MS/Picayune) - Owner type: Corporation - Owner's area on the map: 30.5347° N, 89.6180° W: Placed by OpenAirDocs at the center of ZIP code 39466, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N139JP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=139JP - Page: https://openairdocs.org/deregistered/N139JP-2024-09-10 From the FAA registry file of November 12, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Agusta AB139: https://openairdocs.org/model/agusta-ab139.md ## Service difficulty reports (21) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR AC2A2020081013902](https://openairdocs.org/sdr/AC2A2020081013902), Aug 8, 2020: CHECK VALVE. SEPARATED. HEATER WILL NOT BLOW HOT AIR, DURING TROUBLESHOOTING FOUND HIGHT PRESSURE CHECK VALVE FLAPPER HALVES BEING SEPARATED FROM CHECK VALVE BODY ON ONE SIDE. - [SDR AC2A2020081013901](https://openairdocs.org/sdr/AC2A2020081013901), Aug 8, 2020: CHECK VALVE. SEPARATED. HEATER WILL NOT BLOW HOT AIR; DURING TROUBLESHOOTING FOUND HEATER TEMPERATURE CONTROL VALVE (P/N 3G2140V00751) TO BE DAMAGED FROM HIGHT PRESSURE CHECK VALVE (P/ - [SDR AC2A2020033001](https://openairdocs.org/sdr/AC2A2020033001), Mar 27, 2020: FUEL CONTROL. MALFUNCTIONED. WHEN ADVANCING #1 ENGINE FROM IDLE TO FLIGHT POSITION, #1 ENGINE BEGAN TO "RUN AWAY" AND THE AIRCRAFT SPUN APPROXIMATELY 25-30 DEGREES ON THE PAD AND STARTED TO - [SDR AC2A2020032313902](https://openairdocs.org/sdr/AC2A2020032313902), Nov 29, 2019: PRESSURE SWITCH. LEAKING. HYDRAULIC FLUID LEAKING FROM VENT HOLE. - [SDR AC2A2020032313901](https://openairdocs.org/sdr/AC2A2020032313901), Nov 29, 2019: PRESSURE SWITCH. LEAKING. FLUID LEAKING FROM VENT HOLE ON PRESSURE SWITCH. - [SDR AC2R2018022001](https://openairdocs.org/sdr/AC2R2018022001), Feb 18, 2018: BOLT. BROKEN. HEAD OF BOLT BROKE OFF. - [SDR AC2R2018042002](https://openairdocs.org/sdr/AC2R2018042002), Feb 6, 2018: BEARING. CONTAMINATED. OIL COOLER FAN BEARING CONTAMINATED. - [SDR AC2R2017082402](https://openairdocs.org/sdr/AC2R2017082402), Aug 24, 2017: SWITCH. MALFUNCTIONED. HIGH RESISTANCE WHEN CLOSED. REMOVED AND INSTALLED SERVICEABLE SWITCH. - [SDR AC2R2017082401](https://openairdocs.org/sdr/AC2R2017082401), Aug 24, 2017: SWITCH. SHORTED. SWITCH WAS SHORTED TO CASE AND CAUSED LANDING GEAR NOT TO EXTEND PROPERLY. REMOVED AND INSTALLED SERVICEABLE SWITCH. - [SDR AC2R2016051701](https://openairdocs.org/sdr/AC2R2016051701), May 17, 2016: FIREWALL. CRACKED. THE NR 2 ENGINE FIREWALL HAS A 45MM CRACK AT BS 5700, WL 2670 AND BUTT LINE 780. WE ARE REQUESTING OPTIONS FOR AN REPAIR OF THE CRACKED AREA. THE NR 1 ENGINE FI - [SDR AC2R2016050401](https://openairdocs.org/sdr/AC2R2016050401), May 4, 2016: SKIN. CORRODED. RT UPPER SKIN CORRODED BS 3120 - 6700. - [SDR AC2R9JP03062011](https://openairdocs.org/sdr/AC2R9JP03062011), Mar 3, 2011: LINK. CRACKED. FOUND MAIN ROTOR TENSION LINK CRACKED DURING VISUAL INSPECTION. REPLACED TENSION LINK. - [SDR AC2R9JP02222011](https://openairdocs.org/sdr/AC2R9JP02222011), Feb 20, 2011: FITTING. CRACKED. DURING ROUTINE 50 HR INSP, FOUND THE SUPPORT FITTING WHERE THE INTERMEDIATE GEARBOX ATTACHES TO THE TAILBOOM WAS CRACKED. REMAINING ACFT IN OUR FLEET WERE INSPE - [SDR AC2R12062010001](https://openairdocs.org/sdr/AC2R12062010001), Dec 6, 2010: ANGLE. CRACKED. (AC2R) CRACKED FORE AND AFT ANGLE, PN 3P5333A19561, RT SIDE FUEL DRY BAY AREA. - [SDR AC2A2009081482852](https://openairdocs.org/sdr/AC2A2009081482852), Aug 14, 2009: PRESSURE SWITCH. MALFUNCTIONED. TURNING DOWNWIND AFTER TAKEOFF, NR 2 SERVO LIGHT ILLUMINATED. FOLLOWED ESTABLISHED EMERGENCY PROCEDURE. PRESSURE SWITCH MALFUNCTIONED. - [SDR AC2A2008093078342](https://openairdocs.org/sdr/AC2A2008093078342), Sep 30, 2008: ROD END. BROKEN. DURING TRANSITION FROM CLIMB TO CRUISE FLIGHT THE ACFT DEVELOPED A SEVERE VIBRATION. FOUND TAIL ROTOR DAMPER ROD END BROKEN. REPLACED TAIL ROTOR BLADE AND DAMPE - [SDR AC2A021408001](https://openairdocs.org/sdr/AC2A021408001), Feb 14, 2008: GEARBOX. MAKING METAL. IN CRUISE FLIGHT, AT 3500 MSL, THE MGB CHIP SUMP CAS MESSAGE CAME ON. FOLLOWED THE EMERGENCY PROCEDURE. THE CHIP BURNER WOULD NOT CLEAR THE CHIP. LANDED AT AIRP - [SDR AC2A114524](https://openairdocs.org/sdr/AC2A114524), Mar 14, 2007: CONNECTOR. DIRTY. WHILE IN FLIGHT, NR 2 SERVO CAS LIGHT ILLUMINATED. ON HYDRAULIC SYSTEM SYNOPTIC PAGE, THE NR 2 FWD, RT, LT AND T/R SERVOS ALL INDICATED JAMS. EMERGENCY CHECK LI - [SDR AC2A113056](https://openairdocs.org/sdr/AC2A113056), Nov 28, 2006: ATTACH FITTING. CRACKED. THREE (3) CRACKS FOUND IN FUSELAGE TO TAILBOOM ATTACH STRUCTURE ON FUSELAGE SIDE. (1 )CRACK IN THE RADIUS OF THE BULKHEAD AND (2) CRACKS RADIATING FROM HILOK FA - [SDR AC2A111381](https://openairdocs.org/sdr/AC2A111381), Oct 7, 2006: CLAMP. CRACKED. TAIL ROTOR DAMPER CLAMP CRACKED, REPLACED CLAMP. - [SDR AC2A110707](https://openairdocs.org/sdr/AC2A110707), Jul 1, 2006: SEAL. FAILED. SEAL BREAKING DOWN, COMING APART AND LEAVING A GAP, REPLACED SEAL. ## Other aircraft with N139JP - [Cancelled 2002-12-20](https://openairdocs.org/deregistered/N139JP-2002-12-20): Cessna 210N, S/N 21063810, built 1980. Triennial form not returned. Owner: [Browne J Danforth](https://openairdocs.org/faa-owner/BROWNE%20J%20DANFORTH), [Odessa, FL](https://openairdocs.org/faa-place/FL/Odessa) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.