Registered owner
Veturis David
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

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.

1978In forceSuperseded2026
ADs by the year they took effect: 93 ADs
19781
19792
19804
19813
19823
19832
19852
19867
19871
19882
19893
19914
19922
19943
19953
19963
19993
20011
20023
20032
20043
20053
20061
20072
20082
20092
20101
20111
20123
20133
20142
20151
20171
20181
20192
20214
20224
20232
20241
See all 95 ADs

Information bulletins that may apply · 7

Advisory, not mandatory.

Historical 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 SERVIOct 19, 2005 · N3190P · Bell 206L1 · Exterior LightingSDR 97ZZZX939Blade · corrodedDISCOVERED DURING DAILY INSPECTION, FOUND TIP BLOCK AND WEIGHT PACKAGE CORRODED AND CAUSED SPAR TO BECOME DEFORMED AT TIP.Nov 22, 1996 · N3190P · Bell 206L1 · Main Rotor BladesSDR 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.Nov 7, 1996 · N3190P · Bell 206L1 · Main Rotor Mast/SwashplateSDR 97ZZZX244Blade · corrodedDURING DAILY INSPECTION, FOUND M/R BLADE SPAR LEADING EDGE CORRODED BEYOND LIMITS.Oct 30, 1996 · N3190P · Bell 206L1 · Main Rotor BladesSDR 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.Jun 27, 1995 · N3190P · Bell 206L1 · Main Rotor Mast/SwashplateSDR 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.Jun 27, 1995 · N3190P · Bell 206L1 · Main Rotor Mast/SwashplateSDR 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.May 9, 1995 · N3190P · Bell 206L1 · Rotorcraft Servo System

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.

See all 465 STCs