OpenAirDocs.org

N611SJ

Open the Markdown

2009 Eurocopter Deutschland MBB-BK 117 C-2 · Turbomeca ARRIEL-1E2

Open in FAA registry

© OpenStreetMap
Registered owners
Aspirus Wausau Hospital Inc DBAAspirus Medevac
Location
Wausau, WI
Owner type
Corporation
Serial number
9303
Year built
2009
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
October 15, 2009
Certificate issued
November 7, 2022
Expires
November 30, 2029
Mode S code
A7F40E
Eurocopter Deutschland MBB-BK 117 C-2Airframe model · 8 seats · 2 engines · 109 registeredTCDS H13EUAirframe · Eurocopter Deutschland MBB-BK 117 C-2TCDS E19EUEngine · Turbomeca ARRIEL-1E2

From the FAA registry file of October 24, 2026.

On this page

Airworthiness directives that may apply · 72

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

2003In forceSuperseded2026
See all 88 ADs

Information bulletins that may apply · 3

Advisory, not mandatory.

NTSB investigations

No NTSB investigations matched to N611SJMatched 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 Eurocopter Deutschland MBB-BK 117 C-2 aircraft

FAA incident reports

No FAA accident or incident reports matched to N611SJMatched 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 Eurocopter Deutschland MBB-BK 117 C-2 aircraft

Service difficulty reports · 4

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2A6R2022020962903Frame · noneDURING INSPECTION, FOUND THE RH FRAME 4 INNER SKIN (PN: B533K5605-203) IS DAMAGED IN THE FORM OF DISCREPANT HOLES FROM THE INSTALLATION OF AN INTERIOR PANEL BRACKET. THERE ARE 2EA DISCREPANT HOLES NEAR THE FWD EDGE OF THE INNER SKIN. Feb 9, 2022 · N611SJ · Bolkms BK117C2 · Fuselage Structure (General)SDR 2A6R2022020962902Frame · corrodedDURING INSPECTION, FOUND DAMAGE IN THE FORM OF CORROSION TO THE STA1672.5 FRAME WEB (PN: B531K1323-209), FRAME 1 DESCRIPTION OF WORK: REPAIRED THE DAMAGE IN ACCORDANCE WITH AIRBUS REPAIR DESIGN APPROVAL RDAS-BK117-53-2022-0134A ISSUE A DATED 20 JAN 2022. APPFeb 9, 2022 · N611SJ · Bolkms BK117C2 · Fuselage Structure (General)SDR 2A6R2022020962901Upper Sheet · corrodedDURING INSPECTION, THE COCKPIT FLOOR UPPER SHEET (PN: B531M8020201) AND LOWER SHEET (PN: B531M8021201) ARE DAMAGED IN THE FORM OF CORROSION AT THE LOCATIONS OF THE FWD GROUNDING POINTS. THE CORROSION AREAS FOR THE UPPER SHEET WERE MEASURED TO BE APPROXIMATELY Feb 9, 2022 · N611SJ · Bolkms BK117C2 · Fuselage Structure (General)SDR QMLA2020100520052Cap · missingIN CRUISE FLIGHT, PILOT AND CREW NOTED A BANG, FOLLOWED BY APPROX 45 SEC TO ONE MINUTE OF VIBRATION. VIBRATION WENT AWAY, AIRCRAFT WAS SAFELY LANDED AT KONA (WINONA MUNICIPAL AIRPORT). UPON POST FLIGHT WALK AROUND, DAMAGE TO YELLOW MR BLADE WAS OBSERVED AND Oct 5, 2020 · N611SJ · Bolkms BK117C2 · Main Rotor Head

STCs that may be installed · 111

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 111 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N611SJ before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.

2009Bell 222U · S/N 47564Cancelled Nov 6, 2009 · Triennial form not returned · Built 1987 · Air Methods Corporation, Englewood, CO