- Registered owner
- Chevron USA Inc
- Location
- Picayune, MS
- Owner type
- Corporation
- Serial number
- 920204
- Year built
- 2013
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- May 31, 2013
- Certificate issued
- July 2, 2013
- Expires
- July 31, 2029
- Mode S code
- A2FE03
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 42
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2005 | 1 |
|---|---|
| 2006 | 3 |
| 2007 | 1 |
| 2009 | 4 |
| 2010 | 3 |
| 2011 | 4 |
| 2012 | 4 |
| 2013 | 3 |
| 2014 | 3 |
| 2015 | 2 |
| 2016 | 3 |
| 2017 | 7 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 1 |
| 2021 | 5 |
| 2022 | 4 |
| 2023 | 2 |
| 2024 | 2 |
See all 54 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N292MHMatched 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-92A aircraft
FAA incident reports
No FAA accident or incident reports matched to N292MHMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Sikorsky S-92A aircraft
Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR AC2A202502289202Support Frame · elongatedDURING OUR INSPECTION, WE DISCOVERED WORKING HYLOC FASTENERS AT THE FS 345.6 FRAME AND THE BL -16.5 TRANSMISSION MOUNT INTERCOSTAL FITTING. WHEN WE GRABBED THE COLLAR WITH PLIERS, WE NOTICED THAT THE FASTENER SHOWING THE MOST SIGNS OF WEAR HAS SLIGHT MOVEMENT.SDR AC2A202502289201Frame · corrodedUPON INSPECTION OF THE L/H SPONSON UPPER CENTRAL ATTACHMENT POINT (FS 361) WE HAD EVIDENCE OF LOOSE HARDWARE. UPON REMOVAL OF HARDWARE, WE FOUND THE BOLTS CORRODED AND CORROSION WITHIN THE BUSHING OF THE HOLE. THERE IS NO EVIDENCE OF FRETTING OR MUD WHERE THE SDR AC2A202202039201Connector · damagedPILOT REPORT IN FMR - #1 ENGINE FIRE LIGHT ILLUMINATED WITH NO SECONDARY INDICATIONS. PILOT REPORT IN OPERATOR AOCR - DURING CRUISE FLIGHT ENGINE 1 FIRE LIGHT INTERMITTENTLY ILLUMINATED THEN EXTINGUISHED. MAINTENANCE REPORT IN FMR - UPON RETURN TO BASE #1 ENSDR AC2A202201099201Generator · explodedAPU GENERATOR FAIL CAS MESSAGE DISPLAYED DURING RETURN FLIGHT. SUBSEQUENT EVALUATION AFTER LANDING AND SHUTDOWN REVEALED THE APU GENERATOR HAD DISINTEGRATED INTERNALLY AND REQUIRED REPLACEMENTSDR AC2A202110029201Servo · unserviceableTAIL ROTOR SERVO CONTROL LINKAGE INTERCONNECT LINK BEARINGS WORN TO LIMITSSDR AC2A2020040392001Cover · brokenAFT FLOAT COVER P/N 92250-12801-109 LEFT FORWARD ATTACHMENT HOLE IS BROKEN AT UPPER EDGE. ATTEMPTS TO OBTAIN REPAIR CRITERIA FROM OEM HAS NOT BEEN SUCCESSFUL AND HAVE BEEN EXHAUSTED. REPLACEMENT PARTS ARE NOT READILY AVAILABLE.SDR AC2R201907149201Blade · separatedABRASION STRIP SEPARATION.SDR AC2R2019060549206Servo · wornBEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.SDR AC2R2018011201Wire · chafedAPU FIRE WARNING MESSAGE ILLUMINATED. THIS WAS A FALSE WARNING. A CHAFED WIRE WAS DISCOVERED.SDR AC2A201710110001Warning Light · illuminatedBATTERY HOT AND BATTERY CHARGE FAIL EICAS ILLUMINATED IN FLIGHT, AIRCRAFT RETURNED TO BASE.SDR AC2A2MH07032017Seal · failedNR 3 HYDRAULIC RESERVOIR LOW CAUTION LIGHT ILLUMINATED IN FLIGHT, FOLLOWED BY A NR 3 HYDRAULIC PUMP FAIL LIGHT. AIRCRAFT MADE A PRECAUTIONARY LANDING. FOUND A FLUID LEAK AT PILOT OPERATED CHECK VALVE ON HYDRAULIC SUPPLY MODULE. REMOVED THE CHECK VALVE AND FOUSDR AC2R2019060549205Servo · wornBEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.SDR AC2R2019060549204Servo · wornBEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.SDR AC2R2016060701Fire Detector · contaminatedDURING CRUISE FLIGHT, THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED APPROXIMATELY 7 TIMES. FOUND DIRT, WATER IN NR 2 FLAME DETECTOR CONNECTOR. CLEANED AND SAFETIED CONNECTOR. PERFORMED FIRE DETECTION TEST. NO DEFECTS NOTED. FOUND SERVICEABLE.
STCs that may be installed · 120
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 120 STCs