N222LN

Cancelled 2015

Deregistered aircraft · 1985 Bell 222U · Lycoming LTS-101 series

Cancelled
November 2, 2015
Exported to
South Africa
Status when cancelled
Sale reported
Serial number
47544
Year built
1985
Type
Rotorcraft
Engine
Turbo-shaft
Airworthiness
Standard, transport
Airworthiness date
February 25, 2004
Last registry action
July 7, 2015
Mode S code
A1E976
Owner when cancelled
Sale Reported
Location
Spring, TX
Owner type
Individual

From the FAA registry file of November 4, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 5

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

SDR QMLA2012103012172Transmission · contaminatedDURING CRUISE FLIGHT, LOWER TRANSMISSION CHIP LIGHT ILLUMINATED . PRESSURE AND TEMPERTURE WERE NORMAL RANGE. CHIP WOULD NOT BURN OFF.Oct 30, 2012 · N222LN · Bell 222U · Main Rotor GearboxSDR QMLA2012090612146Skin · crackedDURING AIRWORTHINESS CHECK, A CRACK IN A PRE-EXISTING SKIN REPAIR LOCATED ON THE TOP DECK OF THE HELICOPTER BETWEEN THE SYS 1 AND 2 HYD FILTER MANIFOLDS AT APPROX BS 233. ON REMOVAL OF CRACKED PATCH, A TWO PART CRACK APPROX 5 INCHES RUNNING FORE & AFT WAS UNCOSep 6, 2012 · N222LN · Bell 222U · Fuselage Main, Plate/SkinSDR QMLA2012031512029Shaft · shearedDURING CRUISE FLIGHT, NR 2 ENGINE OIL TEMPERATURE JUMPED FROM 80 DEGREES C TO OVER 120 DEGREES C. THE FLIGHT WAS ABORTED AND RETURNED TO BASE USING MINIMUM POWER FROM THE ENGINE UNTIL LANDING, APPROXIMATLY 10 MINUTES LATER. OIL PRESSURE REMAINED IN THE GREMar 15, 2012 · N222LN · Bell 222U · Turbine Engine Accessory DriveSDR QMLA2011072511082Door Frame · crackedINTERMITTENT FLICKERING OF DOOR LIGHT ON CAUTION/ADVISORY PANEL MADE ME INITIATE A VISUAL INSPECTION OF CABIN DOOR FRAMES DUE TO PAST EXPERIENCE WITH CRACKS IN THESE AREAS CAUSING THIS LIGHT TO FLICKER. FOUND RIGHT CABIN DOOR FRAME, EXTRUSION, AND SKIN CRACKEDJul 25, 2011 · N222LN · Bell 222U · Fuselage Main, StructureSDR QMLA2011050211055Bulkhead · crackedDURING SCHEDULED MX, FOUND A CRACK ALONG STA 270 BULKHEAD, BUTTLINE 8.5 LT, WATERLINE 81.6. CRACK ORIGINATED FROM LOCK FASTENER JOINING LT AFT NODAL BEAM SUPPORT, PN 222-031-592-103 AND STA 270 BULKHEAD. NO PREVIOUS REPAIRS IN THIS AREA. ACFT OUT OF SERVICE.May 2, 2011 · N222LN · Bell 222U · Fuselage Main, Bulkhead

Other aircraft with N222LN · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N222LN is registered now to the first aircraft listed.