- Serial number
- 920249
- Year built
- 2014
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, transport
- Airworthiness date
- July 9, 2014
- Certificate issued
- November 16, 2017
- Expires
- November 30, 2027
- Mode S code
- A48B10
- Registered owner
- Chevron USA Inc
- Location
- Picayune, MS
- Owner type
- Corporation
From the FAA registry file of October 20, 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. Not a compliance determination.
| 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. Matched the same way as ADs.
NTSB investigations
No NTSB investigations matched to N392JSMatched by N-number and event date. 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 N392JSMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Sikorsky S-92A aircraft
Service difficulty reports · 10
SDR AC2A202303169201Switch · closedINERTIA SWITCH FAILED TO THE CLOSED POSITION ACTIVATING AFT PRIMARY SQUIB.SDR AC2A202208069204Flange · crackedFOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.SDR AC2A202208069203Flange · crackedFOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.SDR AC2A202208069202Flange · crackedFOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.SDR AC2A202208069201Flange · crackedFOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.SDR AC2A2021052501Attach Bolt · shearedDURING AIRCRAFT SHUTDOWN THE UPPER ANTI-FLAP STOP RETAINING BOLTS SHEARED AND THE ANTI-FLAP STOP AND A PORTION OF THE SHIM PACK DEPARTED THE MAIN ROTOR HUB ASSEMBLY.SDR AC2A202105250137Bolt · shearedTHE UPPER ANTI-FLAP STOP RETAINING BOLT HEADS SHEARED ALLOWING THE ANTI-FLAP STOP AND HALF OF THE SHIM PACK TO DEPART THE MAIN ROTOR HUB.SDR AC2A201807109201Gearbox · crackedDURING THE 375 HOUR REPLACEMENT OF THE MGB LUBE PUMP VESPEL SPLINE ADAPTER ON THE NR 2 SIDE, THE UPPER STUD WAS BROKEN. AFTER FURTHER INVESTIGATION OF THE R/H MGB LUBE PUMP UPPER STUD AREA WE DISCOVERED CRACKING OF THE CASE AROUND THE BASE OF THE STUDSSDR AC2R2019060549208Servo · wornBEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.SDR AC2R2019060549207Servo · wornBEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.