# N705AL: Sikorsky S-76, registration cancelled 2013-08-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 23, 2013 - Status when cancelled: Sale reported, canceled - Airframe: [Sikorsky S-76](https://openairdocs.org/model/sikorsky-s-76) (registry code 8143010) - Engine: [Allison 250-C30S](https://openairdocs.org/engine/allison-250-c30s) (registry code 03098) - Data sheets: [TCDS H1NE](https://openairdocs.org/tcds/H1NE), [TCDS E1GL](https://openairdocs.org/tcds/E1GL) (OpenAirDocs) - Serial number: 760267 - Type of aircraft: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, transport - Airworthiness date: June 4, 1984 - Last registry action: July 21, 2008 - Mode S code: A9672C - Location: [Breaux Bridge, LA](https://openairdocs.org/faa-place/LA/Breaux%20Bridge) - Owner type: Individual - Owner's area on the map: 30.2908° N, 91.7864° W: Placed by OpenAirDocs at the center of ZIP code 70517, within about 7 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N705AL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=705AL - Page: https://openairdocs.org/deregistered/N705AL-2013-08-23 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-76: https://openairdocs.org/model/sikorsky-s-76.md ## Service difficulty reports (24) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ALG2005F00120](https://openairdocs.org/sdr/ALG2005F00120), Nov 7, 2005: ENGINE. FAILED. ON PRELANDING CHECK, ENGINE OIL PRESSURE DECREASED AND OIL TEMPERATURE INCREASED ABOVE THE RED LINE. ON LONG FINAL TO THE BASE, SHUTDOWN NR 1 ENGINE. AFTER LAND - [SDR ALGA105940](https://openairdocs.org/sdr/ALGA105940), Aug 25, 2005: HUB. CRACKED. CRACKED DAMPER LUG / REPLACED WITH NEW HUB BY FIELD MAINTENANCE. - [SDR ALG2005F00037](https://openairdocs.org/sdr/ALG2005F00037), Jul 1, 2005: BATTERY. INOPERATIVE. DURING FLIGHT, THE BATTERY HOT LIGHT CAME ON, THEN THE BTTERY OFF LIGHT CAME ON. THE PILOT FOLLOWED THE EMERGENCY CHECK LIST AND LANDED. THE MECHANIC REMOVED AN - [SDR ALG2004F00056](https://openairdocs.org/sdr/ALG2004F00056), Oct 9, 2004: AMPLIFIER. INOPERATIVE. IN CRUISE FLIGHT, BOTH ENGINES STARTED SURGING, EMERGENCY CHECK LIST COMPLIED WITH AND RUN ON LANDING. MAINTENANCE COMPLIED WITH VISUAL INSP OF BOTH ENGINES AND - [SDR 2004F00357](https://openairdocs.org/sdr/2004F00357), Aug 4, 2004: FITTING. BROKEN. ON DEPARTURE HEARD LOUD BANG AS LANDING GEAR WAS RETRACTED. THE NOSE GEAR WOULD NOT LOCK IN THE UP POSITION, RETURNED TO HMA AND MAINTENANCE FOUND THE DOOR STRU - [SDR ALGA088095](https://openairdocs.org/sdr/ALGA088095), Jul 14, 2003: GEAR. INOPERATIVE. T/M GEAR REMOVED FOR INSPECTION IAW SBT-076 REMOVED AND REPLACED T/M GEAR. - [SDR ALGA085818](https://openairdocs.org/sdr/ALGA085818), Mar 25, 2003: GEAR. DEFECTIVE. TO COMPLIED WITH MANDATORY SERVICE BULLETIN T-075. PARTS WITH EFFECTIVE S/N'S MAY EXPERIENCE A PROBLEM THAT COULD RESULT IN A N2 DECOUPLE EVENT. REMOVED AND REP - [SDR ALGA085813](https://openairdocs.org/sdr/ALGA085813), Mar 24, 2003: PINION GEAR. SPALLED. ON INSPECTION FOUND SPALLING ON GEAR TEETH. REMOVED AND REPLACED. - [SDR ALG2003F00016](https://openairdocs.org/sdr/ALG2003F00016), Nov 18, 2002: BULB. FAILED. DURING PREFLIGHT CHECK, BAGGAGE COMPARTMENT SMOKE DETECTOR WOULD NOT TEST, THE MECHANIC REPLACED THE BULB AND THE AIRCRAFT WAS RETURNED TO SERVICE. - [SDR ALG2003F00003](https://openairdocs.org/sdr/ALG2003F00003), Oct 12, 2002: CHIP DETECTOR. DIRTY. DURING FLIGHT, NR 1 ENGINE CHIP DETECTOR LIGHT ILLUMINATED, THE PILOT FOLLOWED CORRECTIVE ACTION IAW EMERGENCY CHECKLIST, UPON LANDING THE MECHANIC REMOVED AND - [SDR ALG2003F00053](https://openairdocs.org/sdr/ALG2003F00053), Oct 7, 2002: FUEL NOZZLE. INOPERATIVE. AFTER DROOP COMPENSATOR CHECK, THE PILOT SET THE NR 2 ENGINE TO 100 PERCENT AND ADJUSTED THE NR 1 ENGINE TO 100 PERCENT. THEN THE NR 1 ENGINE FAILED (FLAMED OUT - [SDR ALG2003F00052](https://openairdocs.org/sdr/ALG2003F00052), Oct 7, 2002: FUEL CONTROL. INOPERATIVE. DURING RUN-UP, AFTER DROOP COMPENSATOR CHECK, THE PILOT SET THE NR 2 ENGINE TO 100 PERCENT AND ADJUSTED THE NR 1 ENGINE TO 100 PERCENT. THEN THE NR 1 ENGINE FAI - [SDR ALG2003F00051](https://openairdocs.org/sdr/ALG2003F00051), Oct 7, 2002: GOVERNOR. INOPERATIVE. DURING RUN-UP, AFTER DROOP COMPENSATOR CHECK, THE PILOT SET THE NR 2 ENGINE TO 100 PERCENT AND ADJUSTED THE NR 1 ENGINE TO 100 PERCENT. THEN THE NR 1 ENGINE FAI - [SDR ALG2001F00024](https://openairdocs.org/sdr/ALG2001F00024), Jun 17, 2001: ROD END. CRACKED. DURING FIELD INSPECTION, FOUND ROD END CRACKED AT BARREL NUT SEAT. - [SDR 20010517CW003](https://openairdocs.org/sdr/20010517CW003), Apr 4, 2001: ENGINE. POWER LOSS. ENROUTE, (55 MILES OUTBOUND) NR 1 ENGINE DROPPED OFFLINE, N1 DROPPED TO 36.8 PERCENT, T 5 DROPPED TO 580 DEGREES C AND TORQUE TO 30 PERCENT, PC TUBE FOUND BROKE - [SDR 20010420CW013](https://openairdocs.org/sdr/20010420CW013), Mar 3, 2001: FIRE DETECTOR. INOPERATIVE. DURING PRESTART CHECK, FLAME DETECTOR WOULD NOT TEST. - [SDR 20010328CW010](https://openairdocs.org/sdr/20010328CW010), Mar 3, 2001: FIRE DETECTOR. WILL NOT TEST. FOUND DURING PRE-START CHECK, FLAME DETECTOR WOULD NOT TEST. - [SDR 20010328CW009](https://openairdocs.org/sdr/20010328CW009), Feb 24, 2001: TRANSPONDER. MELTED. IN CRUSE FLIGHT, SMOKE IN COCKPIT, ACRID SMELL IN COCKPIT. PHOTOCELL AND ADJACENT AREA OF CONTROL HEAD MELTED. - [SDR 99ZZZX2535](https://openairdocs.org/sdr/99ZZZX2535), May 21, 1999: LANDING GEAR. MALFUNCTIONED. DURING APPROACH, GEAR HANDLE WAS LOWER. NOSE GEAR DID NOT EXTEND. - [SDR 98ZZZX1257](https://openairdocs.org/sdr/98ZZZX1257), Dec 18, 1997: BLADE. CRACKED. DISCOVERED DURING 500-HOUR INSPECTION, FOUND M/R BLADE SKIN CRACKED AT FORWARD EDGE OF TRIM TAB. - [SDR 98ZZZX1258](https://openairdocs.org/sdr/98ZZZX1258), Dec 1, 1997: SEAL. LEAKING. IN FIELD 12-97, OIL LEAKING FROM STRUT AND PROBLEM SERVICING STRUT. STRUT WOULD NOT ACTUATE PROPERLY. FOUND LOW OIL LEVER IN CYLINDER PREVENTING PROPER ACTUATIN - [SDR 97ZZZX257](https://openairdocs.org/sdr/97ZZZX257), Oct 18, 1996: BLADE. DEBONDED. DURING 500 HOUR INSPECTION FOUND UPPER SURFACE SKIN DEBONDED APPROXIMATELY 5 INCHES BY 6.50 INCHES AT RIGHT STA 53. SKIN CRACKED AT FORWARD EDGE OF TRIM TAB. - [SDR 95ZZZX2814](https://openairdocs.org/sdr/95ZZZX2814), May 9, 1995: BUSHING. WORN. DURING SHOP TEAR DOWN AND INSPECTION FOR REPAIR DUE TO WEAK OPERATION, FOUND BUSHING ID WORN PAST LIMITS. SUSPECT CAUSE - CONTAMINATED OIL. - [SDR 95ZZZX2813](https://openairdocs.org/sdr/95ZZZX2813), May 9, 1995: BUSHING. WORN. DURING SHOP TEAR DOWN AND INSPECTION FOR REPAIR DUE TO WEAK OPERATION, FOUND BUSHING ID WORN PAST LIMITS. SUSPECT CAUSE - CONTAMINATED OIL. ## Other aircraft with N705AL - [Registered now](https://openairdocs.org/aircraft/N705AL): Boeing 737-9, S/N 67427, built 2023 --- 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.