N266AV

Cancelled 2010

Deregistered aircraft · 1999 Airbus Industrie A320-214 · CFM International CFM56 series

Cancelled
April 30, 2010
Exported to
Bermuda
Status when cancelled
Triennial form not returned
Serial number
1152
Year built
1999
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
December 12, 2003
Certificate issued
October 22, 2003
Last registry action
October 20, 2009
Mode S code
A2955B
Owner when cancelled
Lift Italy LLC
Location
Stamford, CT
Owner type
Corporation

From the FAA registry file of October 29, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 6

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

SDR U30A2009031100001Power Supply · odorDURING CRUISE, THE CABIN CREW NOTICED A STRONG ELECTRICAL BURNED ODOR, (NO VISIBLE SMOKE). THE VIDEO TAPE REPRODUCER (VTR) SYSTEM WAS SUSPECT, SO THE SYS WAS POWERED DOWN AND CIRCUIT BREAKERS PULLED. THE ODOR DISSIPATED. LANDING WAS NORMAL AND UNEVENTFUL. MX CMar 9, 2009 · N266AV · Airbus A320214 · Entertainment SystemSDR U30A200800003Actuator · malfunctionedFLT 690 ORD-SRQ. ON APPROACH, THE FLAPS JAMMED AT ZERO, AND THE SLATS EXTENDED NORMALLY. CREW PERFORMED A GO-AROUND, AND DECIDED TO DIVERT TO PIE AND NOTIFIED ATC & DECLARED AN EMERGENCY AS A PRECAUTION. THE APPROACH WAS COMMENCED, AND THE AIRCRAFT LANDED WJan 29, 2008 · N266AV · Airbus A320214 · Trailing Edge Flap ActuatorSDR U30A200800001Control Unit · stickingFLT 561, PUJ-ORD, ON APPROACH THE FLAPS WOULD NOT EXTEND FROM ZERO POSITION. SLATS EXTENDED NORMALLY (ECAM FLAP FAULT WHEN FLAPS 2 SELECTED). ECAM WERE ACTIONS FOLLOWED, AND FCOM & QRH WERE CONSULTED, AND IT WAS NECESSARY TO PREPARE & BRIEF FOR A ZERO FLAP AJan 26, 2008 · N266AV · Airbus A320214 · Trailing Edge Flap Control SystemSDR U30A200600007Sensor · faultyFLT 131 BWI-PHL, CREW REPORTED HIGH BRAKE TEMPERATURE ON LEFT INBOARD MAIN AFTER TAKEOFF. DURING APPROACH INTO PHL, THE CREW REQUESTED EMERGENCY EQUIPMENT TO BE STANDING BY. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE BRAKE TEMP MONITJun 1, 2006 · N266AV · Airbus A320214 · Landing Gear Brake SystemSDR U30A200400006Selector Valve · faultyON FLT 280 EWR-PIE AFTER TAKEOFF, THE CREW HAD ECAM INDICATIONS THAT THE LANDING GEAR DOORS WERE NOT CLOSED AND THE LANDING GEAR WAS NOT UPLOCKED. THE CREW ATTEMPTED A GEAR RE-CYCLE WITH NO SUCCESS. AFTER PLACING THE GEAR HANDLE DOWN & CONFIRMING 3 GREEN (DOMay 25, 2004 · N266AV · Airbus A320214 · Landing Gear Retraction/Extension SystemSDR U30A200400004Spoiler · malfunctionedDURING APPROACH, THE CREW SELECTED FULL FLAPS AND THE AIRPLANE STARTED TO VIBRATE. THE CREW ELECTED TO PERFORM A GO-AROUND AND PERFORM THE LANDING USING FLAPS IN CONFIGURATION 3. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. NOTApr 18, 2004 · N266AV · Airbus A320214 · Drag Control System

Other aircraft with N266AV · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N266AV is registered now to the first aircraft listed.