# N761PH: 1981 Sikorsky S-76A, registration cancelled 2017-08-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 30, 2017 - Status when cancelled: Valid registration - Airframe: [Sikorsky S-76A](https://openairdocs.org/model/sikorsky-s-76a) (registry code 8143006) - Engine: [Turbomeca ARRIEL-1SER](https://openairdocs.org/engine/turbomeca-arriel-1ser) (registry code 60030) - Data sheets: [TCDS H1NE](https://openairdocs.org/tcds/H1NE) (OpenAirDocs) - Serial number: 760224 - Year built: 1981 - Type of aircraft: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, transport - Airworthiness date: December 22, 2000 - Certificate issued: May 10, 2002 - Last registry action: February 3, 2017 - Mode S code: AA468C - Owner when cancelled: [Phi Inc](https://openairdocs.org/faa-owner/PHI%20INC) - Location: [Lafayette, LA](https://openairdocs.org/faa-place/LA/Lafayette) - Owner type: Corporation - Owner's area on the map: 30.1552° N, 92.0282° W: Placed by OpenAirDocs at the center of ZIP code 70508, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N761PH - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=761PH - Page: https://openairdocs.org/deregistered/N761PH-2017-08-30 From the FAA registry file of October 29, 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 Sikorsky S-76A: https://openairdocs.org/model/sikorsky-s-76a.md ## Service difficulty reports (36) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR HEEA126609](https://openairdocs.org/sdr/HEEA126609), Nov 12, 2009: CONNECTOR. DIRTY. ON LANDING, LANDING GEAR WOULD NOT EXTEND. USED CHECKLIST AND NOTIFIED MX. LANDING GEAR CAME DOWN AND LOCKED AFTER RAISING AND LOWERING THE HANDLE A FEW TIMES. - [SDR HEEA107686](https://openairdocs.org/sdr/HEEA107686), Jan 2, 2006: SQUAT SWITCH. OUT OF ADJUST. AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. MAINTENANCE ADJUSTED THE RIGHT HAND WEIGHT ON WHEELS SWITCH. - [SDR HEEA107308](https://openairdocs.org/sdr/HEEA107308), Nov 15, 2005: DOWNLOCK. FALSE INDICATION. TEN MINUTES OUT, AN AIRCRAFT REPORTED THAT ONE MAIN LANDING GEAR WAS DOWN OR PARTIALLY DOWN. SLOWED TO 130 KTS AND FLEW BY TOWER AND THEY CONFIRMED THE LT MAIN - [SDR HEEA093483](https://openairdocs.org/sdr/HEEA093483), Jan 25, 2004: ENGINE. FAILED. WHILE IN CRUISE FLIGHT HEARD A BUMP, THE AIRCRAFT YAWED, NR 1 ENGINE OUT LIGHT CAME ON, MAST CAUTION LIGHT CAME ON, ENGINE CHIP LIGHT CAME ON, AND ALL GAUGES WE - [SDR HEEA088367](https://openairdocs.org/sdr/HEEA088367), Jul 12, 2003: BLADE. ERODED. PRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OR TAIL ROTOR BLADE. - [SDR HEEA088366](https://openairdocs.org/sdr/HEEA088366), Jul 12, 2003: BLADE. WORN. PRIMARY RUBBER ON THE LEADING EDGE HAS ERODED TO THE FIBERGLASS SKIN AND WIRE MESH OF TAIL ROTOR BLADE. - [SDR HEEA088440](https://openairdocs.org/sdr/HEEA088440), Jul 9, 2003: ACTUATOR. CORRODED. AFCS ACTUATOR WORN AND CORRODED. REPLACED CLUTCH WASHER A768336-1 DUE TO WORN; ROD END BEARING MS21151-8C DUE TO ROUGH; POTENTIOMETER (2 EA) A768343-3 DUE TO NU - [SDR HEEA088439](https://openairdocs.org/sdr/HEEA088439), Jul 9, 2003: ACTUATOR. ROUGH. WORN AND CORRODED. REPLACED CLUTCH WASHER A7683361 DUE TO WORN; ROD END BEARING MS21151-8C DUE TO ROUGH; POTENTIOMETER (2 EA) A768343-3 DUE TO WORN. REPAIRED. - [SDR HEEA087970](https://openairdocs.org/sdr/HEEA087970), Jun 21, 2003: TIP CAP. DEBONDED. THE "C" CHANNEL HAS SOME DEBONDING AND THE TOP OUTSIDE DOUBLER SEPERATED. - [SDR HEEA086571](https://openairdocs.org/sdr/HEEA086571), May 22, 2003: BRAKE. STICKING. ROLL MAG BRAKE STICKS IN LATERAL MODE. TO BE SENT TO VENDOR. - [SDR HEEA086564](https://openairdocs.org/sdr/HEEA086564), May 22, 2003: TIP CAP. SEPARATED. THE CRESENT SHAPE DOUBLER UPPER AND LOWER SIDE IS SEPARATED. - [SDR HEEA086520](https://openairdocs.org/sdr/HEEA086520), May 21, 2003: BLADE. SEPARATED. SEPERATED ON THE LOWER SIDE NEAR STATION 44. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. - [SDR HEEA086519](https://openairdocs.org/sdr/HEEA086519), May 21, 2003: SCISSORS. WORN. WORN BEARINGS. REPLACED WASHER MS200002C12 DUE TO WORN; BEARING (4 EA) SB5200-103 DUE TO WORN. REPAIRED. - [SDR HEEA084900](https://openairdocs.org/sdr/HEEA084900), Feb 28, 2003: COMPUTER. FAILED. WEATHER RADAR SYSTEM COMPUTER INTERMITTENTLY SHUTS DOWN AFTER TEN MINUTES. TO BE SENT TO VENDOR FOR REPAIR. - [SDR HEEA084893](https://openairdocs.org/sdr/HEEA084893), Feb 27, 2003: COMPUTER. INOPERATIVE. WEATHER RADAR COMPUTER WILL NOT PAINT. - [SDR HEEA084890](https://openairdocs.org/sdr/HEEA084890), Feb 27, 2003: INDICATOR. INTERMITTENT. WEATHER RADAR INTERMITTENTLY SHUTS DOWN AFTER TEN MINUTES. - [SDR HEEA084195](https://openairdocs.org/sdr/HEEA084195), Feb 13, 2003: RECEIVER. INOPERATIVE. VOR INOPERATIVE. IN SHOP REPAIR. - [SDR HEEA084178](https://openairdocs.org/sdr/HEEA084178), Feb 12, 2003: GENERATOR. MALFUNCTIONED. AC GENERATOR FALLS OFF LINE IN FLIGHT. - [SDR HEEA084171](https://openairdocs.org/sdr/HEEA084171), Feb 12, 2003: BLADE. CRACKED. MAIN ROTOR BLADE TITANIUM LEADING EDGE HAS A COMPLETE CHORDWISE CRACK WITH SEPARATION BEYOND LIMITS. - [SDR HEEA084170](https://openairdocs.org/sdr/HEEA084170), Feb 12, 2003: BLADE. DAMAGED. MAIN ROTOR BLADE NICKEL STRIP HAS A CRACK AT THE VERY TIP AND IS STARTING TO PEEL. - [SDR HEEA082815](https://openairdocs.org/sdr/HEEA082815), Jan 2, 2003: MODULE. MALFUNCTIONED. ROTOR BRAKE CYCLES CONTINUOUSLY. - [SDR HEEA082814](https://openairdocs.org/sdr/HEEA082814), Jan 2, 2003: POWERPACK. MALFUNCTIONED. ROTOR BRAKE POWERPACK KEEPS CYCLING. - [SDR HEEA082813](https://openairdocs.org/sdr/HEEA082813), Jan 2, 2003: POWERPACK. MALFUNCTIONED. ROTOR BRAKE WILL NOT STOP MOTORING. - [SDR HEEA082812](https://openairdocs.org/sdr/HEEA082812), Jan 2, 2003: MODULE. MALFUNCTIONED. ROTOR BRAKE KEEPS MOTORING. - [SDR HEEA082811](https://openairdocs.org/sdr/HEEA082811), Jan 2, 2003: MODULE. MALFUNCTIONED. ROTOR BRAKE CYCLING ON AND OFF WHEN IN THE ON POSITION. - [SDR HEEA082810](https://openairdocs.org/sdr/HEEA082810), Jan 2, 2003: POWERPACK. MALFUNCTIONED. ROTOR BRAKE WILL NOT STOP CYCLING. - [SDR HEEA082805](https://openairdocs.org/sdr/HEEA082805), Jan 2, 2003: POWERPACK. MALFUNCTIONED. ROTOR BRAKE POWER PACK CYCLES ON AND OFF EVERY 3 SECONDS WHEN HARD BRAKE PRESSURE ON. - [SDR HEEA082804](https://openairdocs.org/sdr/HEEA082804), Jan 2, 2003: POWERPACK. MALFUNCTIONED. POWER CYCLES ON APPROX. EVERY 5 SECONDS, POWER PACK WILL NOT HOLD PRESSURE. - [SDR HEEA082537](https://openairdocs.org/sdr/HEEA082537), Dec 13, 2002: THERMOCOUPLE. DAMAGED. THERMOCOUPLE LEAD HAS OPEN IN THERMOCOUPLE END. - [SDR HEEA082534](https://openairdocs.org/sdr/HEEA082534), Dec 13, 2002: GPS. MALFUNCTIONED. ANTENNA FAULT, RAIM UNRELIABLE. SENT TO ASM FREEFLIGHT FOR INSPECTION AND REPAIR. - [SDR HEEA082519](https://openairdocs.org/sdr/HEEA082519), Dec 13, 2002: POWERPACK. MALFUNCTIONED. WILL NOT MAINTAIN PRESSURE. KEEPS CYCLING ON. - [SDR HEEA082449](https://openairdocs.org/sdr/HEEA082449), Dec 12, 2002: BLADE. DAMAGED. TAIL ROTOR BLADE PADDLE "A" HAS HOLE THROUGH THE END CAP. SENT TO INTERNATIONAL AVIATION COMPOSITES FOR INSPECTION AND REPAIR. - [SDR HEEA079362](https://openairdocs.org/sdr/HEEA079362), May 30, 2002: DISPLAY. MALFUNCTIONED. WEATHER RADAR UNIT UNRELIABLE. - [SDR HEEA078718](https://openairdocs.org/sdr/HEEA078718), May 20, 2002: BEARING. WORN. SWASHPLATE BEARING HAS WORN TEFLON. REPLACED WITH SERVICEABLE BEARINGS. - [SDR HEEA072595](https://openairdocs.org/sdr/HEEA072595), Apr 17, 2001: TRANSCEIVER. WEAK. WEAK RECEIVE AND TRANSMIT. - [SDR HEEA071925](https://openairdocs.org/sdr/HEEA071925), Apr 5, 2001: CONTROL PANEL. MALFUNCTIONED. NEEDS EVALUATION. PERFORMED PRELIMINARY INSPECTION AND TESTED. FOUND SWITCHES S1, S4, S5, S8, LIGHT PANEL, VOLUME KNOB AND TRANSMIT KNOB BAD. ALSO LIGHT PANEL L --- 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.