N401GC
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
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.
2 reports on file, 2018-08-07 – 2021-07-02.
Part: COMBUST CHAMBER — LEAKING (ENGINE) · airframe 2,936 hrs · 4,460 cycles
A SPECIAL INSPECTION WAS INITIATED ON ALL OF THE OUTER COMBUSTION CASES IN THE FLEET IAW ROLLS-ROYCE OVERHAUL MANUAL M250-C47B 72-40-00. AIR LEAKAGE WAS FOUND BETWEEN THE TUBE ATTACH FLANGE AND THE OUTER COMBUSTION CASE BODY. THE OUTER COMBUSTION CASE WAS REMOVED FROM SERVICE AND A SERVICEABLE OUTER COMBUSTION CASE WAS INSTALLED.
Part: BULKHEAD — CRACKED (TAILBOOM) · airframe 2,339 hrs · 3,535 cycles
FOUND FORWARD TAILBOOM BULKHEAD CRACKED DURING PHASE A, 300 HOUR INSPECTION. THE CRACK WAS LOCATED BETWEEN THE UPPER TWO RIVETS AT THE 12 O'CLOCK POSITION, TERMINATING AT EACH RIVET HOLE. THE BULKHEAD WAS REMOVED AND REPLACED