- Registered owner
- Veturis David
- Location
- Lake Forest, CA
- Owner type
- Individual
- Serial number
- 45779
- Year built
- 1983
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Airworthiness
- Standard, normal
- Airworthiness date
- August 30, 1983
- Certificate issued
- September 10, 2012
- Expires
- September 30, 2028
- Mode S code
- A36AA6
Bell Helicopter Textron 206L-1TCDS H2SWAirframe · Bell Helicopter Textron 206L-1TCDS E1GLEngine · Allison 250-C28 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Allison 250-C28 model are included below.
On this page
Airworthiness directives that may apply · 85
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1978 | 1 |
|---|---|
| 1979 | 2 |
| 1980 | 4 |
| 1981 | 3 |
| 1982 | 3 |
| 1983 | 2 |
| 1985 | 2 |
| 1986 | 7 |
| 1987 | 1 |
| 1988 | 2 |
| 1989 | 3 |
| 1991 | 4 |
| 1992 | 2 |
| 1994 | 3 |
| 1995 | 3 |
| 1996 | 3 |
| 1999 | 3 |
| 2001 | 1 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 3 |
| 2006 | 1 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 3 |
| 2013 | 3 |
| 2014 | 2 |
| 2015 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2019 | 2 |
| 2021 | 4 |
| 2022 | 4 |
| 2023 | 2 |
| 2024 | 1 |
Airframe · Bell Helicopter Textron 206L-1
AD 2024-20-07Emergency Equipment; Emergency Flotation SectionAD 2023-11-07Ground Proximity SystemAD 2023-06-05Tail Rotor Drive ShaftInformation bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Bell Helicopter Textron 206L-1
SAIB SW-19-05Tail Rotor Drive System, Spline DamageSAIB SW-18-02Loss of Hardware Tail Rotor Drive Shaft CouplingsSAIB SW-12-45Garmin Model 400W/500W Series GPS-WAAS Navigation SystemSAIB SW-10-42R1Emergency Float KitsSAIB SW-08-42Emergency Float with Liferaft Kits (kits)SAIB SW-05-24SAIB SW-04-92Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N3190PMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Bell Helicopter Textron 206L-1 aircraft
FAA incident reports
No FAA accident or incident reports matched to N3190PMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Bell Helicopter Textron 206L-1 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ALG2005F00081Lens · missingIN CRUISE FLIGHT, FELT BUMP IN T/R PEDALS, UPON LANDING, NOTIFIED MAINTENANCE. INSPECTION OF AIRCRAFT BY MAINTENANCE FOUND THE UPPER WHITE STROBE LENS MISSING AND DAMAGE TO ONE TAIL ROTOR BLADE. INSTALLED NEW WHITE LENS AND REPLACED THE T/R ASSY WITH A SERVISDR 97ZZZX939Blade · corrodedDISCOVERED DURING DAILY INSPECTION, FOUND TIP BLOCK AND WEIGHT PACKAGE CORRODED AND CAUSED SPAR TO BECOME DEFORMED AT TIP.SDR 97ZZZX243Lever Assy · wornDAILY INSPECTION FOUND BEARINGS AND SPACERS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH NAS6605D64 BOLTS. NORMAL USE CAUSES PARTS TO WEAR OUT TOO SOON. WORN PARTS TT 475.0 HOURS.SDR 97ZZZX244Blade · corrodedDURING DAILY INSPECTION, FOUND M/R BLADE SPAR LEADING EDGE CORRODED BEYOND LIMITS.SDR 95ZZZX4094Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, 206-010-338-001, SPACERS, 4 EACH, 206-010-337-001, BEARINGS, 2 EACH, 206-010-338-003, BUSHINGS, 2 EACH, NAS6605D64, BOLTS, 1 EACH, 206-010-470-101, BEARING.SDR 95ZZZX4093Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH, 206-010-338-001, SPACERS, 4 EACH, 206-010-337-001, BEARINGS, 2 EACH, 206-010-338-003, BUSHINGS, 2 EACH, NAS6605D64, BOLTS, 1 EACH, 206-010-470-101, BEARING.SDR 95ZZZX2782Housing · wornDURING DISASSEMBLY AND INSPECTION FOR OVERHAUL, FOUND CYLINDER ID WORN PAST LIMITS. PROBABLY CAUSED BY OIL CONTAMINATION AND/OR PART HAS HAD A LONG SERVICE LIFE.
STCs that may be installed · 465
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.