N260AV

Cancelled 2012

Deregistered aircraft · 2001 Airbus Industrie A320-214 · CFM International CFM56-5B4/P series

Cancelled
April 11, 2012
Exported to
Colombia
Status when cancelled
Valid registration
Serial number
1564
Year built
2001
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
November 25, 2008
Certificate issued
November 20, 2008
Last registry action
July 9, 2010
Mode S code
A27F11
Owner when cancelled
Afs Investments 70 LLC
Location
Stamford, CT
Owner type
Corporation

From the FAA registry file of October 28, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 14

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

SDR U30A2011030800003Battery Pack · dischargedMX FOUND THE RT OVERWING EXIT EMERGENCY LIGHTING WAS INOP (BATTERY FAIL), DURING THE DAILY CHECK. MX R & R THE BATTERY, PN 3214-31, SN 33520, RT OVERWING EMERGENCY EXIT (EPSU FIN 12WL) IAW AMM 33-51-38PB401, OPS CKD OK. ACFT RETURNED TO SERVICE. (CLOSED)Mar 7, 2011 · N260AV · Airbus A320214 · Emergency LightingSDR U30A2011011200001Skin · dentedDURING HEAVY MX, A MAJOR REPAIR WAS ACCOMPLISHED TO REPAIR 4 DENTS LOCATED AFT OF THE L1 DOOR, BELOW 2ND PAX WINDOW FR 23-24, STGR 23-24. ALL WORK WAS ACCOMPLIAHED IAW (TD) 70542213/013 ISSUE A, DATED 17-DEC-10 & APPROVED BY REPAIR APPROVAL DESIGN SHEET (RAS) Dec 22, 2010 · N260AV · Airbus A320214 · Fuselage Main, Plate/SkinSDR U30A200500009Skin · dentedGROUND HANDLING EQUIPMENT CAME IN CONTACT WITH LT FWD SIDE OF AIRCRAFT. DAMAGE INSPECTION PER SRM & WITHIN ALLOWABLES FOR 3000 FC. PERMANENT MAJOR REPAIR ACCOMPLISHED TO LT SIDE OF FUSELAGE, DENT NEAR STRINGER 24 & FRAME 9. REPAIRED UNDER USA 3000 AIRLINES Sep 14, 2005 · N260AV · Airbus A320214 · Fuselage Main, Plate/SkinSDR U30A200500003Structure · damagedDURING POST FLIGHT, DAILY INSPECTION, GROUND EQUIPMENT INDUCED DAMAGE WAS FOUND TO LOWER AFT CORNER OF L2 (LT AFT PAX/CREW ) DOOR. MAINTENANCE INSPECTED THE DOOR IAW SRM. MAINTENANCE ALSO PERFORMED A HFEC (HIGH FREQUENCY EDDY CURRENT) INSPECTION IN COMPLIANCEMay 5, 2005 · N260AV · Airbus A320214 · Passenger/Crew DoorsSDR U30A200400010Odor · detectedON INITIAL DESCENT, THE LEAD FLIGHT ATTENDANT ADVISED THE CAPTAIN OF A STRONG SMELL OF BURNING RUBBER AROUND ROW 7. THE FO WENT TO THE CABIN AND CONFIRMED THE SMELL. THERE WAS NO SMOKE AND NO HEAT RADIATING FROM THE FLOOR OR OVERHEAD BINS. THE LEAD FA WAS IAug 14, 2004 · N260AV · Airbus A320214 · Air Distribution SystemSDR U30A200300020Smoke Detector · malfunctionedDURING CRUISE ON FLT 123 MDPC-KPHL THE MASTER WARNING FOR "LAV SMOKE" TRIGGERED BY HAIRSPRAY. NO ACTUAL SMOKE PRESENT. ON FLT 100, MMUN-KPHL, (LATER SAME DAY,TAT 4642.8, 1748 CYC.) DURING CRUISE "LAV SMOKE" WARNING WAS TRIGGERED BY AIR FRESHENER USED BY CABIN Jul 10, 2003 · N260AV · Airbus A320214 · Smoke DetectionSDR U30A200300006Flashlight · inoperativeAfter Flt 257 in EWR, during weekly service, the # 1 Forward Flight Attendant Emergency flashlight was inop. Replaced flashlight.Feb 19, 2003 · N260AV · Airbus A320214 · Emergency EquipmentSDR U30A200200032Light · inoperativeDURING SCHEDULED INSPECTION AT YWG, EMERGENCY EXIT (11WL), THE EMERGENCY PATHWAY SYSTEM UNIT (EPSU) FAILED TO OPERATE. REPLACED EPSU AND TESTED SYSTEM IAW AMM 33-51-38-401. NO FURTHER DEFECTS NOTED.Dec 3, 2002 · N260AV · Airbus A320214 · Emergency LightingSDR U30A200200026Battery Pack · dischargedDURING DAILY INSPECTION AT ORD, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED BATTERY PACK I/A W AMM 33-51-38-401 AND OPERATIONALLY CHECKED THE SYSTEM WITH NO FURTHER DEFECTS.Nov 11, 2002 · N260AV · Airbus A320214 · Emergency LightingSDR U30A200200025Computer · malfunctionedDURING CRUISE OF FLT 135 MYNN (NASSAU) TO KBWI (BALTIMORE) NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) FAULTED ON ECAM. PERFORMED RESET OF SYSTEM AT BWI IN ACCORDANCE WITH TSM TASK 24-00-00-810-818. NO DEFECTS NOTED, MESSAGE CLEARED AND AIRCRAFT WAS RETURNOct 28, 2002 · N260AV · Airbus A320214 · Autopilot ComputerSDR U30A200200016Fwc · faultyFlight 165 PUJ-PHL; Flap position indicator occasionally showing slats in movement with flaps up - Master Wrn Lt shows "Master" on Capt side & "Warn" on F/O side concurrently with slat indication - no change in VMAX indication on PFD and no aural warning. WithJul 14, 2002 · N260AV · Airbus A320214 · Central WarningSDR U30A200200009Warning System · malfunctionedAFTER LANDING AT PUJ, FLT 258, ECAM NESSAGE FOR FWC NR 2 FAULTED ( IN CONJUNCTION WITH FLT/CNTL FLAPS LOCKED - WTB ON, FLAP SYSTEM NR 2 FAULTED, SEE U30A200200008). POWERED DOWN AIRCRAFT, BITE TEST PERFORMED - MESSAGE CLEARED.Jul 8, 2002 · N260AV · Airbus A320214 · Central WarningSDR U30A200200008Warning System · false indicationAFTER LANDING AT PUJ, FLT 258, ECAM MESSAGE FLT/CNTL FLAPS LOCKED WING TIP BRAKE (WTB) ON, FLAP SYSTEM NR 2 FAULT. (ALSO HAD FLIGHT WARNING COMPUTER FAULT, FWC. SEE U30A200200009). COMPLIED WITH BITE TEST 27-54-00-710-002, NO FAULT FOUND, SYSTEM RESET. FLAPS OJul 8, 2002 · N260AV · Airbus A320214 · Central WarningSDR U30A200200007Computer · malfunctionedNR 1 AUTOPILOT FAULTED DURING PRE-FLIGHT IN PUJ (FLT 0125 PUJ-BWI). DEFERRED NR 1 AUTOPILOT PER MEL 22-10-01-1 ON 07/05/2002. UPON RETURN TO MAINTENANCE BASE(07/06/2002) IN PHL, REMOVED & REPLACED NR 1 FLIGHT MANAGEMENT GUIDANCE COMPUTER (NR 1 FMGC) IN ACCORDJul 5, 2002 · N260AV · Airbus A320214 · Flight Management Computing Hardware System

Other aircraft with N260AV · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N260AV is registered now to the first aircraft listed.