N213FR

Cancelled 2023

Deregistered aircraft · 2011 Airbus A320-214 · CFM International CFM56-5B4 series

Cancelled
October 26, 2023
Exported to
Indonesia
Status when cancelled
Valid registration
Serial number
4704
Year built
2011
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 20, 2011
Certificate issued
May 19, 2011
Last registry action
January 22, 2023
Mode S code
A1C534
Owner when cancelled
Bank Of Utah Trustee
Owner type
Corporation

From the FAA registry file of November 3, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

FAA incident reports · 2

FAA accident and incident reports matched to this aircraft by N213FR 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 F3LA2023072500102Doubler · corrodedDISCREPANCY: REFERENCE AIRBORNE /PEMCO N/R 13872.0698 AIRCRAFT WAS NOT GOUNDED AND IS IN CHECK FOR SCHEDULED MX. FD/CR PII ROW 137 RH AFT FUSELAGE CORROSION IN PREVIOUS DOUBLER REPAIR, AT OVERBOARD VENT VACUUM TOILET SYSTEM. CHECK FOR SERVICEABLILITY AND REPAIJun 4, 2023 · N213FR · Airbus A320214 · Fuselage Main, Plate/SkinSDR F3LA2023072800103Floor Support · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO NR 13872.0457 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHEDULED MX. MAIN CABIN FWD WER AREA RIGHT FLOOR STRUCTURE O/B BEAM Y-1292 BETWEEN FR 16 TO FR 20 HAS CORROSION. CORRECTIVE ACTION: EVALUATED AND REPLACED MAIN CMay 31, 2023 · N213FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2023070600089Door Sill · corrodedDISCREPANCY REFERENCE AIRBORNE/PEMCO N/R 13872.0443 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. R2 DOOR CUT OUT SILL AT FR66 CORRODED AFT OF GIRT BAR FITTING. CORRECTIVE ACTION: EVALUATED AND REPLACED R2 DOOR SILL IAW A320 SRM 51-90-00, 53-41May 31, 2023 · N213FR · Airbus A320214 · Fuselage Miscellaneous StructureSDR F3LA2023070600088Floorbeam · corrodedREFERENCE AIRBORNE/PEMCO N/R 13872.0461 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. MAIN CABIN AFT WET AREA RIGHT FLOOR STRUCTURE O/B BEAM Y-1292 AT FWD FR66 HAS CORROSION. EVALUATED AND REPLACED RIGHT FLOOR BEAM O/B-Y1292 AT AFT FR66 IAW A32May 31, 2023 · N213FR · Airbus A320214 · Fuselage Main, Floor BeamSDR F3LA2023062700085Beam · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. MAIN CABIN AFT WET AREA RIGHT FLOOR STRUCTURE BEAM Y-765 BETWEEN FR66 TO FR70 HAS CORROSION. REMOVED AND REPLACED MAIN CABIN AFT WET AREA RIGHT FLOOR STRUCTURE BEAM Y-765 BETWEEN FR66 TO FR70 IAW A3May 31, 2023 · N213FR · Airbus A320214 · Fuselage Main, StructureSDR F3LA2023062100083Beam · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13872.0460 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. MAIN CABIN FWD WET AREA LEFT FLOORS STRUCTURE I/B BEAM Y-503.0 BETWEEN FR14 TO FR16 HAS CORROSION CORRECTIVE ACTION: MAIN CABIN FWD WET AREA LEFT May 31, 2023 · N213FR · Airbus A320214 · Fuselage Main, StructureSDR F3LA2023063000087Shear Plate · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 13872.0389 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING PRIMARY INSPECTION WAS FOUND SERVAL CORROSION ON AFT WET AREA- R/H LATERAL SHEAR PLARE BETWEEN FR68 TO FR70 CORRECTIVE ACTION: REMOVED AND RMay 29, 2023 · N213FR · Airbus A320214 · Fuselage Main, StructureSDR F3LA2023110100009Diaphragm · blownDISCREPANCY: REFERENCE LOG PAGE LP176836 ITEM 3, DURING HEAVY INSPECTION FOUND R2 DOOR DOOR DAMPENER DIAPHRAM BLOWN. CORRECTIVE ACTION: REPLACED DIAPHRAGM AND SHEAR PIN. TORQUE WRENCH S/N F9TAB4787C DUE 11/2023, REFERENCE AMM 52-10-00-610-001-A.//END//Jan 10, 2023 · N213FR · Airbus A320214 · Service DoorsSDR F3LA2020120700050Girt Bar · out of adjustDOOR 1L ARMING/DISARMING SYSTEM SWITCHED FROM ARMED INDICATION TO DISARMED ON TAXI IN SHOWED ARMED. CORRECTIVE ACTION: ADJUSTED GIRT BAR ONTO DOOR FITTINGS. OPERATIONS CHECK GOOD OK FOR SERVICE, AMM 25-62-44-420-065-E.Dec 6, 2020 · N213FR · Airbus A320214 · Emergency EquipmentSDR F3LA2019121390149Unknown · odorSMELL OF BURNT OIL DURING DECENT FROM 10000 INTO DESTINATION. COCKPIT ONLY. THRUST AT IDLE, HP BLEED ENGAGED. PER TSM 05-50-00-810-831, CLASSIFIED AS TYPE 1. PERFORMED TSM TASK 49-00-810-874. NO ODORS PRESENT IN THE CABIN.Dec 7, 2019 · N213FR · Airbus A320214 · Air Distribution SystemSDR F3LA2019010700004Sensor · defectiveDISCREPANCY: REFERENCE LP1132436-2 ECAM FOR ENG 2 COMPRESSOR VANE DURING FLIGHT. A FEW SPURIOUS COMPRESSOR STALL INDICATORS ON ECAM. ALL WARNINGS GONE AFTER ABOUT 10 MINUTES WITH NO FURTHER ISSUES. AIRCRAFT WAS GROUNDED DUE TO DISCREPANCY. CORRECTIVE ACTION: RJan 3, 2019 · N213FR · Airbus A320214 · Compressor Bleed ControlSDR F3LA2018022600290Skin · corrodedEXTERNAL FUSELAGE SKIN CORRODED BELOW LAVATORY VENT. REPAIRED THE SKIN IAW 80426356 AND EA A2-53R-34063.Feb 22, 2018 · N213FR · Airbus A320214 · Fuselage Main, Plate/SkinSDR F3LA2012121400821Connector · disconnectedEMERGENCY LIGHTS LOCATED AT PASSENGER SEATS AT ROW 25 AND 26 ARE INOPERATIVE. RECONNECTED SEAL TO WALL DISCONNECT CONNECTOR. PERFORMED OPERATIONAL CHECKS. OPERATIONAL CHECKS GOOD IAW AMM 33-51-00-71O-001-A.Dec 12, 2012 · N213FR · Airbus A320214 · Light System Wiring