N17592

BELL 206L-3 · Rotorcraft · 1 engine · 7 seats · Valid Registration

Registered owner: PREMIER ROTORS LLC, LA (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
PREMIER ROTORS LLCOperatoron 2024-04-23Operator named in NTSB report

Accident & incident history

Accident · 2024-04-23 Operator named in NTSB report
BELL 206L-3 No injuries Part 91 — PREMIER ROTORS LLC

Operated by PREMIER ROTORS LLC (per NTSB report)

Source: NTSB case WPR24LA134

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.

13 reports on file, 1997-04-14 – 2003-04-17.

OTHER · 2003-04-17 Matched by certificate designator
ATA 3213

Part: CROSSTUBE — CORRODED (MLG) · airframe 10,280 hrs

PART IS CORRODED. CORROSION PITS BEYOND LIMITS. WILL COMPLETE NEW PART INFORMATION FOR THIS MMIR WHEN 592 RETURNS FROM RE-FURB. OLD CROSSTUBE WILL BE RETURNED AT THAT TIME ALSO. PART WAS REPLACED.

Source: SDR AC2A086268
Earlier reports · 1997–2001 · 12 reports

2001

OTHER · 2001-08-11 Matched by certificate designator
ATA 5320

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 8,963 hrs

STIFFENER IS CRACKED. REPAIRED WITH DER APPROVAL.

Source: SDR AC2A075834
OTHER · 2001-08-11 Matched by certificate designator
ATA 5320

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 8,963 hrs

STIFFENER IS CRACKED. REPAIRED WITH DER APPROVAL.

Source: SDR AC2A075835
OTHER · 2001-04-26 Matched by certificate designator
ATA 7810

Part: EXHAUST STACK — CRACKED (ENGINE) · airframe 7,959 hrs

CRACKED. REPLACED EXHAUST ASSY.

Source: SDR AC2A072832
FLUID LOSS; WARNING INDICATION · 2001-02-20 Matched by certificate designator
ATA 2910

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 8,515 hrs

AT CRUISE TO LEEVILLE (LA) HELIPORT, THE PILOT HEARD A LOUD GRINDING NOISE FOLLOWED BY COMPLETE HYDRAULIC FAILURE. THE PILOT PERFORMED THE EMERGENCY PROCEDURE THEN CONFIRMED IT WITH THE BOOK WITH NO CORRECTION TO THE EMERGENCY. PILOT PERFORMED A SHALLOW APPROACH WITH A SLIGHT RUN ON LANDING, AND SHUT DOWN THE AIRCRAFT. REPLACED HYDRAULIC LINE P/N 70-053H000A100A.

Source: SDR AC2A072815

2000

OTHER · 2000-12-08 Matched by certificate designator
ATA 7810

Part: EXHAUST STACK — CRACKED (ENGINE) · airframe 8,276 hrs

CRACKED.

Source: SDR AC2A072799
OTHER · 2000-08-26 Matched by certificate designator
ATA 7810

Part: EXHAUST PIPE — CRACKED (ENGINE)

REMOVED AND REPLACED CRACKED EXHAUST DUCT. (X)

Source: SDR AC2A0000090

1999

OTHER · 1999-12-11 Matched by certificate designator
ATA 7810

Part: EXHAUST PIPE — CRACKED (ENGINE)

EXHAUST ASSEMBLY CRACKED. REPLACED. (X)

Source: SDR AC2A0000011
OTHER · 1999-06-08 Unresolved
ATA 7810

Part: STACK — CRACKED (EXHAUST)

EXHAUST STACK CRACKED.

Source: SDR 99ZZZX3365
OTHER · 1999-02-03 Unresolved
ATA 7810

Part: STACK — CRACKED (EXHAUST)

EXHAUST STACK CRACKED AT WELDED AREA ALONG SEAT SEAM.

Source: SDR 99ZZZX3039

1998

OTHER · 1998-10-29 Unresolved
ATA 7810

Part: STACK — CRACKED (EXHAUST)

CRACK NEXT TO WELD ON AFT SIDE.

Source: SDR 99ZZZX3035

1997

OTHER · 1997-04-22 Unresolved
ATA 5302

Part: FITTING — CRACKED (TAIL BOOM LT)

TAIL BOOM LT ATTACH FITTING FOUND CRACKED ON PHASE B (320 HR) INSPECTION. REPLACED FITTING.

Source: SDR 97ZZZX2311
OTHER · 1997-04-14 Unresolved
ATA 2140

Part: SILENCER ASSY — CORRODED (HEATER)

HEATER SILENCER HAS CORROSION AT INLET AREA AND OUTER SHIELD WHERE BLEED AIR TUBE SUPPORT PLATE IS ATTACHED.

Source: SDR 97ZZZX2310