N392JS
Registered owner: CHEVRON USA INC, MS (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CHEVRON USA PRODUCTION COMPANY (AC2A) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
10 reports on file, 2017-05-02 – 2023-03-16.
Part: SWITCH — CLOSED (CABIN) · airframe 6,690 hrs · 6,790 cycles
INERTIA SWITCH FAILED TO THE CLOSED POSITION ACTIVATING AFT PRIMARY SQUIB.
Part: FLANGE — CRACKED · airframe 6,216 hrs · 6,233 cycles
FOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.
Part: FLANGE — CRACKED · airframe 6,210 hrs · 6,226 cycles
FOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.
Part: FLANGE — CRACKED · airframe 6,190 hrs · 6,201 cycles
FOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.
Part: FLANGE — CRACKED · airframe 5,970 hrs · 5,925 cycles
FOUND WELDMENT ASSEMBLY CRACKED AT FLANGE.
Part: ATTACH BOLT — SHEARED (M/R HUB) · airframe 5,413 hrs · 5,298 cycles
DURING 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.
Part: BOLT — SHEARED (M/R HUB) · airframe 5,413 hrs · 5,298 cycles
THE 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.
Part: GEARBOX — CRACKED (MAIN ROTOR) · airframe 3,359 hrs · 1,375 cycles
DURING 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 STUDS
Part: SERVO — WORN (MAIN ROTOR) · airframe 2,989 hrs
BEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.
Part: SERVO — WORN (MAIN ROTOR) · airframe 2,311 hrs
BEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.