Registered owner
Bank Of Utah Trustee
Owner type
Corporation
Serial number
7538
Year built
2017
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
April 5, 2017
Certificate issued
October 17, 2024
Expires
October 31, 2031
Mode S code
A33D97

From the FAA registry file of October 24, 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.

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.

NTSB investigations

No NTSB investigations matched to N308FRMatched by N-number and event date, checked against the reported serial number, make and model. 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 N308FRMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Airbus A320-251N aircraft

Service difficulty reports · 8

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

SDR F3LA2022131200163Seat Track · corrodedFWD WET AREA, SEAT TRACK WAS CORRODED ON UPPER FLANGE FRAMES 16-18. REMOVED & REPLACED IAW SRM 51-74-00, 51-42-11, 51-44-11, ESPM 20-33-44-01.Nov 30, 2022 · N308FR · Airbus A320251N · Fuselage, Seat/Cargo Attach FittingsSDR F3LA2022131200162Shear Web · crackedAFT WET AREA, RIGHT SHEAR WEB CRACKED, LIGHT CORROSION ON LOWER SURFACE AND CORROSION AROUND FASTENER HOLE. REMOVED & REPLACED AFT R/H SHEA WEB IAW A320 SRM 51-72-11-911-001A.Nov 30, 2022 · N308FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2022121200161Shear Web · crackedAFT WET AREA, LEFT SHEAR WEB CRACKED. REMOVED AND REPLACED LEFT SHEAR WEB AT AFT WET AREA IAW SRM 51-72-11-911-001. REMOVED AND REINSTALLED VOR ANTENNA CABLE SYSTEM #2 AT AFT WET AREA IAW ESPM 20-33-22-02.Nov 30, 2022 · N308FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2022120700158Door Sill · corrodedR2 DOOR SILL AFT FASTENER HOLE CORRODED. REPAIRED R2 DOOR SILL IAW A-320 NEO SRM 43-41-14-283-002 AND SRM 53-41-14-300-001 NO FURTHER ACTION REQUIRED. (REPAIR CATEGORY A)Nov 30, 2022 · N308FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2022120700157Threshold · corrodedL2 THRESHOLD HAS CORROSION AROUND FASTENER HOLE AND CORROSION ON ONE FASTENER HEAD. REPAIRED L2 DOOR SILL IAW A-320 NEO SRM 43-41-14-283-002 AND SRM 53-41-14-300-001 NO FURTHER ACTION REQUIRED. (REPAIR CATEGORY A)Nov 30, 2022 · N308FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2022063000067Pipe · leakingDISCREPANCY: REFERENCE LP236654 LOSS OF GREEN HYDRAULIC PRESSURE AFTER TAKE OFF. PERFORMED LANDING GEAR GRAVITY DROP ENGINE #1. REFERENCE LP236656 HYDRAULIC PUMP CAVEATTED DUE TO HYDRAULIC LEAK - CORRECTIVE ACTION: REFERENCE LP 236656 REMOVED AND REPLACED HYDRJun 24, 2022 · N308FR · Airbus A320251N · Hydraulic Pump (Electric/Engine), MainSDR F3LA202206300066Pipe · leakingDISCREPANCY: REFERENCE LP236656; LOSS OF GREEN HYDRAULIC PRESSURE AFTER TAKE OFF. PERFORMED LANDING GEAR GRAVITY DROP ENGINE #1 HYDRAULIC PUMP CAVEATTED DUE TO HYDRAULIC LEAK - REMOVED AND REPLACED HYDRAULIC PUMP IAW AMM 29-11-51-400-808-AC. LP236657 HYDRAULIJun 24, 2022 · N308FR · Airbus A320251N · Hydraulic System, MainSDR F3LA2018101600451Fuel Line · leakingDISCREPANCY: REFERENCE LOG PAGE LP1133184 ITEM 1, FOUND EVIDENCE OF FUEL LEAK FROM DRAIN MAST NR 2 ENGINE. CORRECTIVE ACTION: REMOVED FUEL TUBE BETWEEN FUEL PUMP AND MAIN HEAT EXCHANGER REFERENCE 72-00-00-17A-530A-C. INSTALLED REFERENCE 72-00-00-17A-710AC. TWFOct 15, 2018 · N308FR · Airbus A320251N · Aircraft Fuel Distribution System

STCs that may be installed · 149

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 149 STCs