# N519AL: Sikorsky S-76A, registration cancelled 2022-07-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 2, 2022 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Sikorsky S-76A](https://openairdocs.org/model/sikorsky-s-76a) (registry code 8143006) - Engine: [Allison 250-C30 series](https://openairdocs.org/engine/allison-250-c30-series) (registry code 03015) - Data sheets: [TCDS H1NE](https://openairdocs.org/tcds/H1NE), [TCDS E1GL](https://openairdocs.org/tcds/E1GL) (OpenAirDocs) - Serial number: 760058 - Type of aircraft: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, transport - Airworthiness date: June 17, 1998 - Certificate issued: March 5, 2019 - Last registry action: March 5, 2019 - Mode S code: A682E9 - Owner when cancelled: [Arrow Aviation Company LLC](https://openairdocs.org/faa-owner/ARROW%20AVIATION%20COMPANY%20LLC) - Location: [Broussard, LA](https://openairdocs.org/faa-place/LA/Broussard) - Owner type: LLC - Owner's area on the map: 30.1347° N, 91.9273° W: Placed by OpenAirDocs at the center of ZIP code 70518, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N519AL - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=519AL - Page: https://openairdocs.org/deregistered/N519AL-2022-07-02 From the FAA registry file of October 31, 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 (31) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ALGA201308017578](https://openairdocs.org/sdr/ALGA201308017578), Jul 31, 2013: SERVO. FLAKING. MAIN ROTOR SERVO HAD THE NR 2 CRANK BOLT INSTALLED LOOSELY. ON DISASSEMBLY OF THE SERVO, PLASMA COATING WAS DISCOVERED IN ALL INTERNAL LOCATIONS. - [SDR ALGA2012110729109](https://openairdocs.org/sdr/ALGA2012110729109), Nov 5, 2012: CHIN BUBBLE. CRACKED. RIGHT CHIN BUBBLE CRACKED, REMOVED AND REPLACED. - [SDR ALGA2012032200012](https://openairdocs.org/sdr/ALGA2012032200012), Mar 22, 2012: PISTON. ERODED. SERVO LOCKED UP FOUR TIMES ON FUNCTIONAL CHECK ON HYD BENCH. FOUND PLASMA COATING BROKE OFF SYS 1 AND 2 PISTONS. PLASMA WAS FOUND IN BOTH SYS BYPASS SPOOL, SLEE - [SDR ALGA201203220011](https://openairdocs.org/sdr/ALGA201203220011), Mar 22, 2012: PISTON. ERODED. SERVO LOCKED UP 4 TIMES ON FUNCTIONAL CHECK ON HYD BENCH. FOUND PLASMA COATING BROKE OFF SYS 1 AND 2 PISTONS. PLASMA WAS FOUND IN BOTH SYS BYPASS SPOOL, SLEEVES - [SDR ALGAR201201300058](https://openairdocs.org/sdr/ALGAR201201300058), Jan 30, 2012: COVER. DEBONDED. FOUND PADDLE "A" TIP WEIGHT COVER DEBONDED AND MOISTURE INGRESS IN WEIGHT POCKET. - [SDR ALGA1062011519AL4](https://openairdocs.org/sdr/ALGA1062011519AL4), Oct 6, 2011: FLOOR PANEL. CORRODED. FOUND CO-PILOTS FLOOR PANEL CORRODED. - [SDR ALGA1062011519AL3](https://openairdocs.org/sdr/ALGA1062011519AL3), Oct 6, 2011: FLOOR PANEL. CORRODED. FOUND FLOOR PANEL CORRODED. - [SDR ALGA1062011519AL2](https://openairdocs.org/sdr/ALGA1062011519AL2), Oct 6, 2011: FLOOR PANEL. CORRODED. FOUND FLOOR PANEL CORRODED. - [SDR ALGA20111006001](https://openairdocs.org/sdr/ALGA20111006001), Oct 6, 2011: FLOOR PANEL. CORRODED. FOUND PILOTS FLOOR PANEL CORRODED, PN 7620402006-048, SN 16100711. - [SDR ALGA10062011519AL](https://openairdocs.org/sdr/ALGA10062011519AL), Oct 6, 2011: FLOOR PANEL. CORRODED. FOUND FLOOR PANEL CORRODED. - [SDR ALG2006F00031](https://openairdocs.org/sdr/ALG2006F00031), Mar 21, 2006: EXPLOSIVE LINK. OUT OF ADJUST. ON TAKEOFF, LANDING GEAR WAS RETRACTED, 3 GREEN LIGHTS WENT OUT, AND RED UNLOCKED LIGHT ILLUMINATED. MAINTENANCE ADJUSTED LT MAIN GEAR EXPLOSIVE LINK, APPLIED H - [SDR ALG2006F00015](https://openairdocs.org/sdr/ALG2006F00015), Jan 24, 2006: INVERTER. FAILED. ON TAKEOFF, HP1 AND HP2 WENT OFF LINE. REPLACED NR 1 INVERTER WITH SERVICEABLE UNIT. AIRCRAFT OPS CHECK GOOD. (K) - [SDR ALG2005F00090](https://openairdocs.org/sdr/ALG2005F00090), Nov 29, 2005: SEAL. LEAKING. AFTER LANDING, OIL WAS OBSERVED ON MAIN GEAR AND TAILBOOM. REPLACED GEARBOX SEAL (STARTER/ GENERATOR) AND OIL RING ON STARTER/GENERATOR. ALL WORK C/W ICW C-30 M - [SDR ALG2005F00071](https://openairdocs.org/sdr/ALG2005F00071), Oct 5, 2005: FUEL FILTER. FAILED. AFTER TAKEOFF, FUEL PRESSURE DROPPED TO 4 PSI. RETURNED TO BASE AND NOTIFIED MAINTENANCE. MAINTENANCE REPLACED NR 1 FUEL FILTER. GROUND RUN AND OPS CHECK GOOD I - [SDR ALG2005F00032](https://openairdocs.org/sdr/ALG2005F00032), May 25, 2005: BATTERY. INOPERATIVE. DURING FLIGHT, BATTERY HOT AND BATTERY OFF LIGHT ILLUMINATED. EMERGENCY CHECKLIST CONSULTED, TURNED BATTERY SWITCH OFF AS A PRECAUTION. PROCEEDED FOR MAINTENANC - [SDR ALG2005F00028](https://openairdocs.org/sdr/ALG2005F00028), May 8, 2005: VALVE. LEAKING. WHILE HOVERING OUT FOR TAKEOFF, NOTICED HYDRAULIC FLUID ON THE HELIPAD. RETURNED TO PAD TO INVESTIGATE AND SHUTDOWN HELICOPTER AND THEN CONTACTED MAINTENANCE. M - [SDR ALG2005F00024](https://openairdocs.org/sdr/ALG2005F00024), Apr 16, 2005: WIRE. BROKEN. UPON PERFORMING THE T/O CHECK LIST, BOTH CREW MEMBERS NOTICED THAT THE LANDING GEARS WOULD NOT ACTUATE TO THE UP POSITION. CHECKED THE CIRCUIT BREAKERS AND RECY - [SDR ALGA094285](https://openairdocs.org/sdr/ALGA094285), Apr 28, 2004: GEAR. SPALLED. FOUND SPALLING AND GALLING ON PINION GEAR TEETH. SENT TO VENDOR FOR WARRANTY CREDIT. - [SDR ALG2004F00004](https://openairdocs.org/sdr/ALG2004F00004), Feb 16, 2004: AMPLIFIER. INOPERATIVE. FIRE WARNING LIGHT ON NR 2 ENGINE ILLUMINATED. NO FIRE WAS SEEN. MAINTENANCE REMOVED AND REPLACED FIRE DETECTOR CONTROL AMP. - [SDR ALG2004F00000](https://openairdocs.org/sdr/ALG2004F00000), Jan 8, 2004: ENGINE. MAKING METAL. IN FLIGHT, NR 2 ENGINE CHIP LIGHT CAME ON. MAINTENANCE FOUND METAL ON FWD PLUG ON NR 2 ENGINE. SMALL RING OF TINY FLAKES ON OUTSIDE PERIMETER OF CHIP PLUG. AIRC - [SDR ALGA087751](https://openairdocs.org/sdr/ALGA087751), Jun 24, 2003: SEAL. LEAKING. MULTIPLE INPUT SEALS LEAKING WHEN RUN-UP ON TEST STAND. REPLACED SEALS WITH NEW. - [SDR ALG2003F00015](https://openairdocs.org/sdr/ALG2003F00015), Dec 5, 2002: HYDRAULIC SYSTEM. LOW. IN CRUISE FLIGHT PILOT NOTICED A KICK IN THE FLIGHT CONTROLS AND A SLIGHT FLUCTUATION IN NR 2 HYDRAULIC GAUGE THIS WAS FOLLOWED BY CHATTERING IN THE CYCLIC CONT - [SDR ALG2003F00045](https://openairdocs.org/sdr/ALG2003F00045), Sep 30, 2002: CONTROL PANEL. INOPERATIVE. DURING LANDING, THE LANDING GEAR WARNING HORN WENT ON AND STAYED ON WITH THE GEAR DOWN AND LOCKED (3 GREEN LIGHT). UPON LANDING THE LANDING GEAR WAS PINNED IAW - [SDR ALG2001F00032](https://openairdocs.org/sdr/ALG2001F00032), Oct 16, 2001: RELAY. FAULTY. DURING PRESTART CHECK OF THE ENGINE FIRE EXTINGUISHING SYSTEM. BOTTLE FIRED DURING TEST, RELAY COIL WAS FOUND FAULTY. - [SDR ALG2001F00027](https://openairdocs.org/sdr/ALG2001F00027), Oct 16, 2001: RELAY. FAULTY. DURING PRESTART CHECK OF THE ENGINE FIRE EXTINGUISHING SYSTEM, BOTTLE FIRED DURING TEST, RELAY COIL FOUND FAULTY. - [SDR 20001113SH012](https://openairdocs.org/sdr/20001113SH012), Aug 31, 2000: SUPPORT BRACKET. BROKEN. DURING COMPLIANCE OF ASB 76-67-44, FOUND CYCLIC SUPPORT NOT TO BE THE CORRECT CONFIGURATION. (X) - [SDR 20000912SH008](https://openairdocs.org/sdr/20000912SH008), Aug 15, 2000: WARNING LIGHT. ILLUMINATED. BEFORE LANDING, UNSAFE GEAR INDICATION, (LEFT MAIN, NO GREEN, RED STAYED ON). RECYCLED GEAR AND ALL GREEN LIGHTS ILLUMINATED. VISUALLY CHECKED GEAR AND SWITCHES - [SDR 99ZZZX3686](https://openairdocs.org/sdr/99ZZZX3686), Aug 23, 1999: TORQUE SHAFT. FAILED. AFTER LEVELING OFF AT 3,500 FEET, A LARGE TORQUE SPLIT WITH NR 2 ENGINE DROPPING TO 61 PERCENT N1 - T5 450 DEGREES TORQUE 30 PERCENT, COLLECTIVE WAS REDUCED TO - [SDR 99ZZZX3685](https://openairdocs.org/sdr/99ZZZX3685), Aug 23, 1999: BEEP MOTOR. FAILED. AFTER LEVELING OFF AT 3,500 FEET, A LARGE TORQUE SPLIT WITH NR 2 ENGINE DROPPING TO 61 PERCENT N1 - T5 450 DEGREES TORQUE 30 PERCENT, COLLECTIVE WAS REDUCED TO - [SDR 99ZZZX3684](https://openairdocs.org/sdr/99ZZZX3684), Aug 23, 1999: GOVERNOR. FAILED. AFTER LEVELING OFF AT 3,500 FEET, A LARGE TORQUE SPLIT WITH NR 2 ENGINE DROPPING TO 61 PERCENT N1 - T5 450 DEGREES TORQUE 30 PERCENT, COLLECTIVE WAS REDUCED TO - [SDR 98ZZZX4757](https://openairdocs.org/sdr/98ZZZX4757), Oct 14, 1998: ADI. MALFUNCTIONED. DURING CLIMB-OUT, SMOKE WAS NOTICED IN THE COCKPIT. FOUND COPILOT'S ADI DEFECTIVE. REMOVED AND INSTALLED SERVICEABLE UNIT. --- 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.