- Registered owner
- Bo LLC
- Location
- Wilmington, DE
- Owner type
- LLC
- Serial number
- 6021
- Type
- Rotorcraft
- Engine
- Turbo-shaft
- Certificate issued
- April 2, 2026
- Expires
- April 30, 2033
- Mode S code
- A7CFC2
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 0
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
No ADs matched this aircraft’s modelsADs on appliances, propellers and installed equipment aren’t matched by model; check those separately.
Information bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N602MBMatched 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 Messerschmitt-Bolkow-Blohm BO 105 P aircraft
FAA incident reports
No FAA accident or incident reports matched to N602MBMatched 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 Messerschmitt-Bolkow-Blohm BO 105 P aircraft
Service difficulty reports
No reports matched to N602MBGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Messerschmitt-Bolkow-Blohm BO 105 P aircraft
Reports on N602MB not matched to an aircraft · 7
They name N602MB, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2016FA0000583Alternator · failedPRIMARY ALTERNATOR FAILED IN FLIGHT.SDR 2016FA0000539Belt · shearedSQUEALING SOUND AT ENGINE START VOLTMETER SHOWING DISCHARGE. ALTERNATOR BELT WAS SHEARED.SDR 2012FA0000522Attach Fitting · crackedDURING AN ANNNUAL INSPECTION, FOUND A .7500" CRACK IN THE LT MAIN LANDING GEAR OUTBOARD ATTACH FITTING AS VIEWED THROUGH A FLOOR ACCESS PANEL. THE CRACK IS IN THE RADIUS OF THE FITTING AFT AND BELOW THE MLG SPRING. FOUND NO HISTORY OF A HARD LANDING.
STCs that may be installed
No STCs matched this aircraft’s modelsSTCs change type-certificated designs, and this aircraft isn’t type certificated.