Serial number
8811
Year built
2019
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
March 28, 2019
Certificate issued
December 2, 2020
Expires
December 31, 2027
Mode S code
A3D7DC
Registered owner
Bank Of Utah Trustee
Owner type
Corporation

From the FAA registry file of October 20, 2026.

On this page

Airworthiness directives that may apply · 99

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment. Not a compliance determination.

2017In forceSuperseded2026
ADs by the year they took effect: 151 ADs
20173
201811
201915
202020
202112
202217
202315
202414
202524
202620
See all 151 ADs

Information bulletins that may apply · 1

Advisory, not mandatory. Matched the same way as ADs.

NTSB investigations

No NTSB investigations matched to N347FRMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Airbus A320-251N aircraft

FAA incident reports

No FAA accident or incident reports matched to N347FRMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A320-251N aircraft

Service difficulty reports · 8

SDR F3LA202508260287Power Supply · no testAIRCRAFT WAS UNDERGOING HEAVY SERVICE CHECK DURING RON MAINTENANCE, ITEM #3 BATT/EPSU (11WL) EMER L FAULT. R&R EPSU BATTERY 11WL REF AMM 33-51-38-400-001-A/AMM 33-51-38-400-001 TEST OK.Aug 26, 2025 · N347FR · Airbus A320251N · Emergency LightingSDR F3LA202503070197Clamp · looseDISCREPANCY: ENG 1 FIRE ECAM AFTER LANDING. ENGINE 1 BOTTLE DISCHARGED. UPON INSPECTION OF THE #1 ENG, FOUND PYLON BLEED DUCT CLAMPS LOOSE. TORQUED PYLON DUCT CLAMPS IAW AMM 36-11-49-400-330-A. NO EVIDENCE OF A FIRE.Mar 5, 2025 · N347FR · Airbus A320251N · Pneumatic Distribution SystemSDR F3LA2024092300143Battery · failedREFERENCE LTPR NR 5001334236-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS FOUND EPSU BATTERY 13 WL INOP. REPLACEMENT REQUIRED IAW AMM 33-51-38-000-002-A REV.99. REPLACED EPSU BATTERY 13WL IAW AMM 33-51-38-400-002 RSep 20, 2024 · N347FR · Airbus A320251N · Emergency LightingSDR F3LA2024092300142Battery · failedREFERENCE LTPR NR 5001334222-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS FOUND EPSU BATTERIES 10 WL INPO REPLACEMENT REQUIRED IAW AMM 33-51-38-000-002-A REV. 99. REPLACED EPSU BATTERY AND POWER SUPPLY 10WL IAW AMMSep 20, 2024 · N347FR · Airbus A320251N · Emergency LightingSDR F3LA2024092300141Battery · failedREFERENCE LTPR NR 5001334233-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INCOMING CHECKS FOUND EPSU BATTERIES 11 WL INPO REPLACEMENT REQUIRED IAW AMM 33-51-38-000-002-A REV/99. REPLACED EPSU BATTERY AND POWER SUPPLY 11WL IAW AMM Sep 20, 2024 · N347FR · Airbus A320251N · Emergency LightingSDR F3LA2024091800132Door Seal · corrodedREFERENCE NR#5001334171-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. RH AFT DOOR SILL BEAM NUT PLATE HOLE AT FR68 IS CORRODED. REPAIR REQUIRED AFTER EVALUATION AS PER A320 NEO SRM 53-41-14-283-002 REV.41. REPAIRED BY INSTALLATION OF REPASep 17, 2024 · N347FR · Airbus A320251N · Fuselage Main, StructureSDR F3LA2022040800024Tube · damagedDISCREPANCY: LP188829-2, HYD G RSVR LO LVL. CORRECTIVE ACTION: SERVICED HYD G RSVR IAW AMM 12-12-29-611-001-A, ADDITIONAL CORRECTIVE ACTION FROM LP188830-2: #1 ENG HYD LEAK FOUND. CORRECTIVE ACTION: R/R PRESS ASSY IAW AMM 20-23-11-911-001-A./END/Apr 7, 2022 · N347FR · Airbus A320251N · Hydraulic System, MainSDR F3LA202006050028Connector · looseEPSU AT FIN 11WL FAULTS DURING TEST ON HEAVY CHECK. REMOVED LT OVERWING SLIDE, FOUND LOOSE CONNECTOR, TIGHTENED CONNECTOR. REINSTALLED SLIDE ON ITEM 2 OF THIS LOG PAGE AND PERFORMED OPS TEST PER AMM 33-51-15-400-001-A, NO FAULTS FOUND.Jun 5, 2020 · N347FR · Airbus A320251N · Light System Wiring