N2193X

BELL 206B · Rotorcraft · 1 engine · 5 seats · Valid Registration

Registered owner: INDUSTRIAL HELICOPTERS LLC, LA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
INDUSTRIAL HELICOPTERSOperatoron 2026-07-21Operator named in NTSB report

Accident & incident history

Accident · 2026-07-21 Operator named in NTSB report
BELL 206B Serious injury Part 137INDUSTRIAL HELICOPTERS

Operated by INDUSTRIAL HELICOPTERS LLC (per NTSB report)

Not yet finalized — may be revised.
Source: NTSB case WPR26LA277

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, 2000-07-11 – 2004-10-13.

OTHER · 2004-10-13 Unresolved
ATA 5320

Part: ANGLE — CRACKED (BOX BEAM)

LT LOWER CAP ANGLE PN 206-031-200-037 CRACKED 5.250 IN. MEASURED FROM THE FORWARD TIP OF THE CAP ANGLE ON THE HORIZONTAL SECTION AND OF THE CAP ANGLE ON THE HORIZONTAL SECTION AND 5.625 IN. FROM THE FORWARD TIP OF THE CAP ANGLE ON THE VERTICAL SECTION GOING THROUGH RIVET HOLE. ENCLOSED ARE 2 EA. PICTURES OF THE CRACK FOR YOUR REVIEW. THE CRACK WAS FOUND DURING NORMAL MAINTENANCE. DO NOT KNOW THE CAUSE, NOR HAVE PREVENTIVE RECOMMENDATION. THE CAP ANGLE IS BEING REPLACED WITH LIKE PART.

Source: SDR IIFR004F
OTHER · 2000-07-11 Unresolved
ATA 6710

Part: BEARING — BINDING (ENGINE BAY)

LINEAR ACTUATAORS, PN 206-062-721-001 AND 721-109 FAILED PREMATURELY DUE TO OVERSTAKING OF BEARING ROD END P/N 251401501299 CAUSING BEARING TO BE TIGHT AND BINDING WHERE ADJUSTMENTS ARE MADE. ACTUATOR MOTOR IS NOT STRONG ENOUGH TO OVERCOME BEARING STIFFNESS. SUBMITTER SUGGESTED USING BRG WITH LESS BREAK FREE FORCE,THAT IS NOT STAKED SO TIGHT TO ALL FREE MOVEMENT OF BRG AND LINEAR ACTUATOR.

Source: SDR 20000804SH005