N1821
Registered owner: GM LEASING CO LLC, LA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Air Evac EMS, Inc. (EVCA) | 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.
6 reports on file, 2010-04-05 – 2023-10-26.
Part: BLADE — CRACKED (MAIN ROTOR) · airframe 5,804 hrs · 13,251 cycles
VAN HORN M/R BLADE INBOARD TRIM TABS CRACKED.
Part: BLADE — CRACKED (MAIN ROTOR) · airframe 5,804 hrs · 13,251 cycles
VAN HORN M/R BLADE INBOARD TRIM TABS CRACKED.
Part: TUBE — CRACKED (PG AIR) · airframe 4,266 hrs · 13,179 cycles
BY VISUAL INSPECTION, FOUND PG AIR LINE FROM ACCUMULATOR TO FUEL CONTROL CRACKED APPROXIMATELY HALF THE CIRCUMFERENCE AND 1/2 INCH FROM FITTING.
Part: BLADE — DEBONDED (TAIL ROTOR) · airframe 3,970 hrs · 12,326 cycles
DURING INSPECTION FOUND EVIDENCE OF DEBONDING ON T/R BLADE P/N 206-016-201-135 S/N CS20648. REMOVED T/R HUB AND BLADE ASSEMBLY P/N 206-011-810-157G S/N HB2825 AND INSTALLED SERVICEABLE T/R HUB AND BLADE ASSEMBLY P/N 206-011-810-157G S/N HB2767 IAW BOTH BHT-206L4-MM-7.
Part: FRAME — CRACKED (FUSELAGE) · airframe 2,810 hrs · 8,819 cycles
WHILE PERFORMING INSPECTIONS OF THE ACFT IT WAS FOUND THAT THE FS 145 BULKHEAD HAD A CRACKED CLIP, PN 206-033-107-055 WITH 5 CRACKS, ALL MEASURING BETWEEN 3/32" & 5/16" IN LENGTH. UPON REMOVAL OF THE CLIP, FRAME, PN 206-033-107-121 WAS FOUND TO HAVE MULTIPLE CRACKS WITH ONE MEASURING IN EXCESS OF 1 INCH.
Part: BEARING — FLAKING (TRANSMISSION) · airframe 516 hrs · 1,761 cycles
INTERMITTENT TRANSMISSION CHIP LIGHT IN FLIGHT, DISASSEMBLED TRANSMISSION AND FOUND SEVERAL PLANETARY ROLLER BEARINGS FLAKING AND PITTING.