N5403CSikorsky S-76
This N-number isn't registered right now. Below is its last known registration, canceled Aug 6, 2004.
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply11 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Chevron USA INC
- Owner type
- Corporation
- City, state
- Picayune, MS
- Certificate issued
- Aug 28, 1985
- Canceled
- Aug 6, 2004
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
- 760141
- 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
- A6DAB0
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- 1985 – 2004Chevron USA INCPicayune, MS
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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.
- Engine · gearshaft · wornJul 12, 2001
EXCESSIVE SPLINE WEAR ON AFT END. REPLACED WITH NEW.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Navigation · altimeter · out of toleranceApr 2, 2001
VIBRATOR INOP,AUTOPILOT CORRECTION POTENTIOMETER OUT OF TOLERANCE AND OFF FLAG STICKS. REPLACED INST.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Main rotor drive · chip detector · leakingJan 22, 2001
PART LEAKS AT CONNECTOR. REPLACED CHIP DETECTOR
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Rotor flight controls · fitting · crackedAug 22, 2000
FOUND SMALL CRACK IN UNDERSIDE OF FITTING. VERIFIED CRACK WITH NDT. REPLACED FITTING. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · crackedMay 20, 2000
T-ANGLE FOUND CRACKED SIX INCHES FORWARD ON PILOTS AFT DOOR POST. REPAIRED PER SRM. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Rotor flight controls · bearing · bindingApr 26, 2000
INTERMITTENT BINDING IN FLIGHT CONTROL WHEN ROLL INPUT IS APPLIED. REPLACED WORN BEARING. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine · scroll · crackedFeb 24, 2000
SCROLL CRACKED AT NORMAL LOCATION. REPLACED SCROLL. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number. - Electrical power · potentiometer · failedSep 21, 1999
FEEDBACK POTENTIOMETER PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. SUBMITTER STATED CAUSED ACTUATOR TO KICK IN-FLIGHT. COMP P/N 7690001802106.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Autoflight · potentiometer · failedAug 24, 1999
FEEDBACK POTENTIOMETER PREMATURE FAILURE, SUBMITTER STATED SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. CAUSES ACTUATOR TO KICK IN-FLIGHT. COMPONENT P/N 769000180210L.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Equipment and furnishings · rescue light · defectiveJun 13, 1998
UPON COMPLETION OF LIFE VEST INSPECTION (12 EACH), EVERY RESCUE LIGHT WITH A MNAUFACTURE DATE OF JUNE, 1997, HAD FAILED DUE TO CASE SWELLING (9 EACH) AFTER ONLY 3 MONTHS IN SERVICE. OTHER LIGHTS WITH DIFFERENT MANUFACTURE DATES DID NOT FAIL DURING THE SAME 3 MONTH PERIOD.
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 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026