N5401GSikorsky S-76
This N-number isn't registered right now. Below is its last known registration, canceled Oct 31, 2017.
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply11 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Rotorcraft Assets LLC
- Owner type
- Corporation
- City, state
- Broussard, LA
- Certificate issued
- Jul 26, 2011
- Canceled
- Oct 31, 2017
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jul 15, 1992
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Sikorsky
- Model
- S-76
- Serial number
- 760137
- Aircraft type
- Rotorcraft
- Category
- Land
- Certification
- Type Certificated
- Seats
- 14
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Type certificate data sheet
- H1NE
- Mode S code
- A6DA6E
Engine
- Type
- Turbo-shaft
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2011 – 2017Rotorcraft Assets LLCBroussard, LA
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (1)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-11-52 | Sikorsky Aircraft Corporation Model S-76 Series Helicopters | Aug 31, 2000 | Airframe (S-76) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (11)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Electrical power · brushes · detachedApr 11, 2003
PART IS DISBONDED. THE ATTACHING LEAD AND SPRING WEAR PLATE AND RIVET CAME APART. REPLACED ALL FOUR BRUSHES AND RAN IN BRUSHES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · corrodedMar 2, 2003
COROSION FOUND ON ANGLE DURING INSPECTION. PART WAS REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine oil · thermostat · inoperativeDec 27, 2001
THERMOSTAT, HIGH ENGINE OIL TEMPERATURE IN FLIGHT. REMOVED AND REPLACED THERMOSTAT. CURED PROBLEM.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Engine oil · thermostat · inaccurateDec 27, 2001
HIGH ENGINE OIL TEMPERATURE IN FLIGHT. REPLACED THERMOSTAT. CURED PROBLEM.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · bearing · deterioratedApr 5, 2001
PART IS DETERIORATED. BEARING CAGE FAILED ALLOWING ALL BALLS TO GROUP TOGETHER. NO BALLS WERE LOST OR DETERIORATED OVERHAULED STARTER - GENERATOR AND REPLACED BEARINGS.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Rotor flight controls · fitting · crackedOct 17, 2000
PART IS CRACKED. REPLACED CRACKED COLLECTIVE SOCKET.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · blade · corrodedJul 7, 2000
DURING ZONE 1 INSPECTION, CORROSION WAS FOUND THROUGHOUT THE LOWER SURFACE OF THE YELLOW MAIN ROTOR BLADE. THE ALUMINUM WIRE MESH WAS FOUND WITH NUMEROUS SMALL PITS OF CORROSION THROUGHOUT THE LOWER SURFACE OF THE BLADE. REMOVED CORROSION AND SPOT PAINTED PER COMPOSITE REPAIR MANUAL. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor · blade · corrodedJul 7, 2000
DURING ZONE 1 INSPECTION, CORROSION WAS FOUND THROUGHOUT LOWER SURFACE OF MAIN ROTOR BLADE. THE ALUMINUM WIRE MESH WAS FOUND WITH NUMEROUS CORROSION PITS THROUGHOUT THE LOWER SURFACE OF THE BLADE. REMOVED CORROSION AND SPOT PAINTED PER COMPOSITE REPAIR MANUAL. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Autoflight · potentiometer · failedSep 20, 1999
FEEDBACK POTENTIOMETER PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. SUBMITTER STATED CAUSED ACTUATOR TO KICK IN-FLIGHT. COMPONENT P/N 7690001802106.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · hinge · corrodedMay 8, 1997
CORROSION WHERE BUSHINGS GO THROUGH HINGE. REPLACED DOOR HINGE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 11 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026