N262AV

Cancelled 2012

Deregistered aircraft · 2002 Airbus A320-214 · CFM International CFM56 series

Cancelled
May 4, 2012
Exported to
Colombia
Status when cancelled
Valid registration
Serial number
1725
Year built
2002
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 11, 2002
Certificate issued
May 20, 2003
Last registry action
March 28, 2012
Mode S code
A2867F
Owner type
Corporation

From the FAA registry file of October 27, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N262AV and the event date: up to this one’s cancellation.

Service difficulty reports · 13

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

SDR U30A2011022800002Epsu · faultyAT GATE, PRIOR TO DEPARTURE, FLT 362 ORD-CVG, THE LT OVERWING EXIT EMERGENCY LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE LT OVERWING (EPSU) EMERGENCY POWER SUPPLY UNIT (11WL), IAW AMM 33-51-38PB401 & OP'S CK'D OK. AIRCRAFT WAS RETURNED TO SERVICE.Feb 27, 2011 · N262AV · Airbus A320214 · Emergency LightingSDR U30A2009122200010Transformer · shortedIN CLIMB ECAM ELEC DC BUS 2 FAULT 20-DEC-09 EMER RTF CUN. CONCLUSIONS: TRANSFORMER RECTIFIER(TR) PN Y005-3, SN 5255, FIN 1PU2. SUSPECTED THAT INITIAL SHORT CIRCUIT OCCURRED IN TR, POSSIBLY DUE TO FOREIGN METALLIC FILINGS LEADING TO CB 2PU2 POPPED OUT. THE NODec 20, 2009 · N262AV · Airbus A320214 · DC Power Distribution SystemSDR U30A2009120800007Connector · corrodedIN CRUISE, ECAM FOR: ENG 2 REVERSER FAULT. FCOM REQUIRES TO LAND ASAP. ACFT DIVERTED. BOTH ENGINES CONTINUED TO PRODUCE NORMAL THRUST AND THERE WAS NO INDICATION THAT A REVERSER DEPLOYED OR WAS PRESSURIZED. UPON LANDING ROLLOUT, CREW RECEIVED:LDG GEAR DISAGREEDec 6, 2009 · N262AV · Airbus A320214 · Engine Exhaust System WiringSDR A6WA200940319Slide · failedSLIDE WAS REMOVED (R2 DOOR), ON 14-APR-09. THIS S/R WAS A SCHEDULED REMOVAL FOR TIME, AND WE COMPLIED WITH A "SAMPLE" ACTUAL DEPLOYMENT OF THE S/R IAW OUR MX PROGRAM REQUIREMENT. THE R2 PAX DOOR (ASSIST BOTTLE PRESSURE WAS CHECKED AND OK) OPENED CORRECTLY, ANDApr 14, 2009 · N262AV · Airbus A320214 · Escape SlideSDR U30A2009041500004Slide · failedSLIDE WAS REMOVED (R2 DOOR), ON 14-APR-09. THIS S/R WAS A SCHEDULED REMOVAL FOR TIME, AND WE COMPLIED WITH A "SAMPLE" ACTUAL DEPLOYMENT OF THE S/R IAW OUR MX PROGRAM REQUIREMENT. THE R2 PAX DOOR (ASSIST BOTTLE PRESSURE WAS CHECKED AND OK) OPENED CORRECTLY, ANDApr 14, 2009 · N262AV · Airbus A320214 · Escape SlideSDR U30A200700003Slide · partial inflateAIRCRAFT IN MAINTENANCE. MPD TASK 25624104, "OPERATIONAL TEST OF THE ESCAPE-SLIDE DEPLOYMENT, FWD/AFT PASSENGER/CREW DOOR" WAS BEING PERFORMED ON THE L2 PAX/CREW DOOR SLIDE/RAFT. THE SLIDE/RAFT FAILED TO DEPLOY PROPERLY. THE PACK OPENED UP & THE BOTTLE DROPPEDJul 13, 2007 · N262AV · Airbus A320214 · Escape SlideSDR U30A200600006Skin · dentedTHE REPAIR WAS C/W TO A SKIN DENT BETWEEN FRAME 24A-25 AND STRINGER 42-43 RT. REPAIRED UNDER USA 3000 EO 05-53-014, DATED APRIL 20,2005, WHICH INCORPORATES THE PERMANENT REPAIR DEFINITION PER AIRBUS SRM 53-00-11 PARAGRAPH 4K, FIGURE 221. REMOVED DAMAGED SKINApr 30, 2006 · N262AV · Airbus A320214 · Fuselage Main, Plate/SkinSDR U30A200400009Glowstrip · crackedAFTER FLT 609, RSW-ORD, DURING MAINTENANCE, THE EMERGENCY FLOOR PATHWAY LIGHTING PHOTO LUMINESCENT STRIP BETWEEN SEAT ROWS 2 DEF AND 5 DEF WAS IDENTIFIED AS DAMAGED. MAINTENANCE REPLACED THE PHOTO LUMINESCENT STRIP BETWEEN ROWS 2 DEF AND 5 DEF IAW AMM 33-51-21Jul 26, 2004 · N262AV · Airbus A320214 · Emergency EquipmentSDR U30A200300008Computer · faultyDURING CRUISE ON FLT 0441 CUN-CLE, NR 2 FMGC WILL NOT RESET AND AUTOPILOT NR 2 WOULD NOT ENGAGE AS A RESULT. DEFERRED PER MEL 22-10-01. ON MARCH 11, 2003, REPLACED NR 2 FLIGHT MANAGEMENT GUIDANCE COMPUTER (FMGC) IAW AMM 22-83-34-400-001. TESTED AFS OK. PERMar 10, 2003 · N262AV · Airbus A320214 · Autopilot SystemSDR U30A200200034Gust Lock · failedIN EWR AFTER FLT 257, LEFT FORWARD PAX/CREW ENTRANCE DOOR (L1) GUST LOCK FAILED TO ENGAGE. UPON FURTHER INSPECTION, FOUND DEBRIS IN DOOR GAS ROD BUSHING (WHICH CAUSED ROD TO BIND ON BUSHING). CLEARED DEBRIS AND FREED UP DOOR GAS ROD AND GUST LOCK MECHANISM ODec 9, 2002 · N262AV · Airbus A320214 · Passenger/Crew DoorsSDR U30A200200029Cylinder · dischargedDURING "DAILY" INSPECTION AFTER FLT 155 IN PHL, THE L1 CREW / PASSENGER DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. SERVICED THE EMERGENCY OPERATION CYLINDER WITH NITROGEN IAW AMM 52-10-00-614-050. FOR PRECAUTIONARY MEASURES; REPLACED SEALS AND PACKINGNov 22, 2002 · N262AV · Airbus A320214 · Passenger/Crew DoorsSDR U30A200200027Light · crackedAFTER FLT 9262, DURING DAILY INSPECTION, A SECTION OF PHOTOILLUMINESCENT STRIP ON FLOOR AT SEAT 1R IS CRACKED (ALTHOUGH STILL OPERATIONAL). REPLACED PHOTOILLUMINSCENT STRIP SECTION AT SEAT 1R PER AMM 33-51-21-000-001. OPS CK'D OK.Nov 12, 2002 · N262AV · Airbus A320214 · Emergency LightingSDR U30A200200021Computer · faultyDURING PREFLIGHT FOR FLT 1371 AT ORD, ECAM MESSAGE INDICATED AP2, CAT 3 DUAL. AFS BITE CALLS FOR FMGC NR 2 REPLACEMENT. DEFERRED NR 2 FMGC PER MEL 22-83-01-2. AIRCRAFT OPERATED ORD-CUN-PHL. UPON ARRIVAL AT PHL THE NR 2 FMGC (FLIGHT MANAGEMENT GUIDANCE COMPAug 17, 2002 · N262AV · Airbus A320214 · Autopilot Computer

Other aircraft with N262AV · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N262AV is registered now to the first aircraft listed.