N281CB

Cancelled 2023

Deregistered aircraft · 1981 Bell 206B · Allison 250-C20 series

Cancelled
March 4, 2023
Status when cancelled
Registration expired, pending cancellation
Serial number
3303
Year built
1981
Type
Rotorcraft
Engine
Turbo-prop
Airworthiness
Standard, normal
Airworthiness date
April 3, 1995
Certificate issued
November 18, 2010
Last registry action
October 28, 2019
Mode S code
A2D1E6
Owner when cancelled
Extreme Properties Inc
Location
Bismarck, ND
Owner type
Corporation

From the FAA registry file of October 31, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

NTSB investigations · 1

Matched to this aircraft by N281CB and the event date: up to this one’s cancellation.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N281CB and the event date: up to this one’s cancellation.

Service difficulty reports · 6

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

SDR JJWA0049155Skid · crackedSKID GEAR LANDING TUBE FOUND DISSIMILAR METAL CORROSION CRACK STARTING WITH SKID SHOE INSERT NUT AFT CROSSTUBE FITTING, NON-REPAIRABLE AREA. TUBE ONLY 3 YEARS OLD, CRACK MAY HAVE BEEN MISSED ON PAST INSPECTORS.Sep 25, 2002 · N281CB · Bell 206B · Wheel/Ski/FloatSDR JJWA0049154Skid · corrodedHIGH SKID GEAR TUBE DISSIMILAR METAL CORROSION CRACK FOUND STARTING WITH SKID SHOE INSERT NUT UNDER AFT CROSSTUBE TITTING, ONLY 3 YEARS OLD, CRACK MAY HAVE BEEN MISSED FOR A WHILE ON INSPECTIONS.Sep 25, 2002 · N281CB · Bell 206B · Wheel/Ski/FloatSDR JJWA080369Stiffener · crackedFOUND STIFFNER CRACKED DURING INSPECTION - CRACK ORIGINATED IN LOWEST HI-LOCK FASTNER POSITION 2.875Jul 15, 2002 · N281CB · Bell 206A · Fuselage Miscellaneous StructureSDR JJW2002F00000Stiffener · crackedFOUND STIFFNER CRACKED DURING INSPECTION - CRACK ORIGINATED IN LOWEST HI-LOCK FASTENER POSITION 2.875 INCH BELOW TOP OF PART. ALSO SPLICED NEW WEB (PN 206031106349S) DUE TO CRACK IN WEB FROM SAME LOCATION. REPLACED STIFFNER. ALL WORK IAW SRM.Jul 12, 2002 · N281CB · Bell 206B · Fuselage Miscellaneous StructureSDR JJWA078248Rib · crackedREMOVED BOTH HORIZONTAL STABILIZERS THAT HAD BEEN LAST INSTALLED OVER 5 YEARS AGO. FOUND EXCESSIVE CORROSION IN SPAR CLAMP AREA ON RIB CLOSEST TO TAILBOOM. REQUIRES TOTAL RIBE REPLACEMENT OF $1966 RIB. INSPECTED OTHER RIB ALSO HAD CORROSION & PIECE MISSING SO Mar 21, 2002 · N281CB · Bell 206B · Rotorcraft Tail BoomSDR JJWA077061Actuator · corrodedACTUATOR FAILED AFTER FEBRUARY 2001 OVERHAUL. NO ALODINE OR OTHER CORROSION PROTECTION ON INSIDE OF CASE.INTERNAL CORROSION CAUSED FAILURE.Nov 5, 2001 · N281CB · Bell 206B · Main Rotor Control