- Registered owner
- Sikorsky Aircraft Corp
- Location
- Stratford, CT
- Owner type
- Corporation
- Serial number
- 760031
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Mode S code
- AA5F4B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 58
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1980 | 1 |
|---|---|
| 1981 | 4 |
| 1982 | 4 |
| 1984 | 3 |
| 1985 | 3 |
| 1986 | 3 |
| 1987 | 3 |
| 1989 | 2 |
| 1991 | 2 |
| 1995 | 1 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
| 2010 | 3 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 1 |
| 2015 | 2 |
| 2016 | 1 |
| 2018 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 62 ADs
Information bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N768ALMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Sikorsky S-76A aircraft
FAA incident reports · 6
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 19980130011159IPwr On Vertical Ldng/Rtrcrft · Gulf Mexico, LANarrative: on 30 jan 1998, at 0900 CT, a Sikorsky SK-76-A N768AL, operated by offshore logistics, inc., certificate no. ALGA151C, struck a safety fence with the left main landing gear while landing on an offshore oil platform. The landing gear collapsed…Incident 19910111005839IFcd/Prec Ldg From Cruise · Patterson, LANR1 engine chip detector light on. Engine failed. Vectored for landing. Turbine wheel had burst.Incident 19901212063829IFcd/Prec Ldg From Cruise · Patterson, LANR1 engine power surge. Secured and landed. Governor failed due to bearing failure.Incident 19900531034669IPower On Descent (Rotorcraft) · Gulf Of Mexico, LAExperienced limitation to left cyclic control travel on approach. Left cyclic control stop was improperly adjusted.Incident 19810428029609INormal Cruise · Cameron, LAThe two and one half bearing failed debris caused oil pump to shear shaft.Incident 19800325040129INormal Cruise · Sabine, TXUpper forward part of right passenger door came off in flight, the day after an emergency release test.
Service difficulty reports · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ALG2003F00068Wire · failedDURING PRESTART CHECKLIST. WHEN THE (AUX ESS POWER) CHECK WAS DONE, THE PILOT FLOAT BOTTLE DISCHARGED, AFTER APPROXIMATELY 2-3 SECONDS. WHILE SWITCH WAS ENGAGED FLOAT (ARM) SWITCH WAS OFF FLOAT (TEST) SWITCH WAS IN (NORMAL). REPAIRED CHAFFED AND BROKEN WIRSDR ALG2001F00004Compressor Wheel · corrodedRECEIVED TURBINE FROM FIELD TO REPAIR FOR HIGH FREQUENCY AND VIBES. REMOVED OUTER COMBUSTION CASE FROM TURBINE TO INSPECT FOR HIGH FREQUENCY AND FOUND 1ST STAGE WHEEL BLADES TO HAVE BEEN ATTACKED BY SULPHADATION. MFG SHOULD USE THE NEW GENERATION OF COATING SDR 98ZZZX308Flame Detector · failedNR 1 ENGINE T-HANDLE FIRE LIGHT ILLUMINATED INTERMITTENTLY. REMOVED AND REPLACED NR 1 ENGINE FORWARD FLAME DETECTOR.SDR 97ZZZX4413Wheel Blades · erodedTURBINE ASSEMBLY RECEIVED DUE TO 2,000 HOUR OVERHAUL. FOUND FIRST STAGE WHEEL HAD BURNED AND ERODED BLADES CAUSED BY SULFIDATION.SDR 97ZZZX4431Wheel Blades · brokenTURBINE ASSEMBLY WAS RECEIVED WITH ENGINE ASSEMBLY DUE TO MAKING METAL. UPON INSPECTION OF G.P. SECTION, FOUND SULFIDATION ON 1ST STAGE WHEEL. 1ST STAGE WHEEL: PN 23053299, SN X-138702, TT 1,348.1 HOURS, TC 1,697. SCRAPPED DUE TO MISSING BROKEN AND CRACKEDSDR 97ZZZX945Skin · crackedDURING PHASE INSPECTION, FOUND CRACK IN PYLON SKIN ACROSS RIVET HOLE. THIS CRACK EMANATED FROM CORROSION OF THE SKIN. FURTHER INSPECTION REVEALED CORROSION ON VARIOUS MEMBERS IN THE PYLON.SDR 97ZZZX260Blade · debondedDURING DAILY INSPECTION, FOUND UPPER SURFACE SKIN DEBONDED APPROXIMATELY 20 INCHES BY 8.50 INCHES NEAR BLADE TIP.SDR 96ZZZX2217Blade · crackedDURING 500-HOUR INSPECTION, FOUND BLADE SPAR CRACKED AT ROOT END BUSHING HOLE. SUBMITTER STATED CAUSE UNKNOWN.SDR 96ZZZX2218Bearing · galledUPON DISASSEMBLY OF GEARBOX, CLEANED AND INSPECTED PARTS AS REQUIRED. FOUND EXCESSIVE GALLING ON PTO AFT, BEARING INNER RACE. EXCESSIVE GALLING, BEARING INNER RACE, POSSIBLY DUE TO BEARING CAGE OUT-OF-ROUND CAUSING TIGHT FIT BETWEEN INNER AND OUTER RACE AND SDR 96ZZZX1822Detector · malfunctionDURING LEVEL FLIGHT, NR 1 ENGINE FIRE T-HANDLE ILLUMINATED. PERFORMED TIGHT TURN, LOOKING FOR INDICATION OF SMOKE. NOTED NO SMOKE, ALL ENGINE INDICATIONS WERE NORMAL. DURING TROUBLESHOOTING, FOUND ENGINE NR 1 FLAME DETECTOR BAD. REPLACED FLAME DETECTOR. OSDR 96ZZZX737Wire · chafedDURING FLIGHT, A ELECTRICAL SPARK WAS SEEN IN THE VICINITY OF THE OVERHEAD CIRCUIT BREAKER PANEL. REMOVED OVERHEAD ON PILOT'S SIDE AND FOUND A WIRE CHAFED AGAINST THE AFT RIGHT CORNER OF THE DL SWITCH BOX. CHAFE WAS REPAIRED.SDR 95ZZZX6780Blade Assy · debondTAIL ROTOR BLADE DISBOND DETECTED DURING DAILY INSPECTION. FOUND APPROXIMATELY 1 INCH BY 1 INCH SKIN DELAMINATION AT TIP WEIGHT AREA. POSSIBLY CAUSED BY RUST FORMING ON TIP WEIGHT HARDWARE.
STCs that may be installed · 352
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 352 STCs