N921GL
Registered owner: CHEVRON U S A 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.
5 reports on file, 2013-12-01 – 2024-03-19.
Part: BUSHING — CRACKED (MOUNT) · airframe 8,318 hrs · 3,790 cycles
THREE OF THE BUSHINGS ON THE RH MOUNTING FOOT WAS FOUND TO BE FRACTURED.
Part: SERVO — WORN (MAIN ROTOR) · airframe 5,220 hrs
BEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.
Part: ROD END — DAMAGED (TAIL ROTOR PCS) · airframe 3,497 hrs
FOUND TAIL ROTOR PITCH CHANGE SHAFT (PCS)- INPUT CONTROL TUBE ROD END BEARING OUTER RING WAS NO LONGER SECURE IN THE ROD END. ONCE THE ROD END WAS REMOVED FROM THE PCS, THE BEARING DID NOT HAVE ANY RESISTANCE TO KEEP IT INSTALLED INTO RODEND. THE ROD END WAS REPLACED WITH NEW.
Part: SERVO — WORN (MAIN ROTOR) · airframe 1,823 hrs
BEARINGS, LINKAGE AND SLINED PIVOT SHAFT WORN.
Part: DAMPER — DETERIORATED (ZONE 400) · airframe 209 hrs
BLUE MAIN ROTOR DAMPER OTBD BARREL NUT FOUND DAMAGED ON DAILY INSPECTION. REMOVED FAULTY BLUE DAMPER ASSEMBLY, PN 92106-15801-103 AND INSTALLED NEW DAMPER ASSEMBLY OF SAME PN. INSPECTED ALL OTHER DAMPERS IN SERVICE AND REPORTED INCIDENT TO TECHNICAL REPRESENTATIVE AND INSPECTION DEPARTMENT.