- Registered owner
- Wilmington Trust Co Trustee
- Location
- Wilmington, DE
- Owner type
- Corporation
- Serial number
- 7925
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 5, 2017
- Certificate issued
- December 4, 2017
- Expires
- December 31, 2027
- Mode S code
- A37A02
Airbus A320-251NTCDS A28NMAirframe · Airbus A320-251NTCDS E00089ENEngine · CFM International LEAP-1A26
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.
| 2017 | 3 |
|---|---|
| 2018 | 11 |
| 2019 | 15 |
| 2020 | 20 |
| 2021 | 12 |
| 2022 | 17 |
| 2023 | 15 |
| 2024 | 14 |
| 2025 | 24 |
| 2026 | 20 |
See all 151 ADs
Information bulletins that may apply · 1
Advisory, not mandatory.
Airframe · Airbus A320-251N
SAIB NE-19-03Escape Slide Maintenance Tasks and Intervals - JASC 2565NTSB investigations
No NTSB investigations matched to N323FRMatched 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 N323FRMatched 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 · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR F3LA202502110185Floorbeam · corrodedREFERENCE AIRBORNE/PEMCO N/R 16011.0162 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. UPON REMOVING FLOOR PANEL 261LG, FOUND CORROSION ON FLOOR BEAM Y765. REMOVED AND REPLACED FLOORBEAM Y765 IAW A320 SRM 51-72-11, SRM 53-41-14, AMM 53-00-000-80SDR F3LA202501070175Selector Valve · stuckACFT WAS GROUNDED DUE TO BRAKES NORMAL BRAKE FAULT ECAM REPEATEDLY SURGING FELT IN BRAKE PEDALS DURING NORMAL ALT BK TRANSFER REF LP441987. REMOVED AND REPLACED ALTERNATE BRAKING SELECTOR VALVE PN C24993000 WORK DONE IAW 37-43-00-710-001 LEAK CHECK GOOD A/C SDR F3LA2023061900081Door Sill · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 14018.0238 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. L2 DOOR, DOOR SILL FASTENERS CORRODED
CORRECTIVE ACTION: EVALUATED 2EA NUT PLATE HOLES AT L2 DOOR AFT DOOR SILL AFTER FURTHER EVALUATION FOUND OUTSDR F3LA2023061900080Shear Plate · corrodedDISCREPANCY: REFERENCE AIRBORNE/PEMCO N/R 14018.0237 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULE MX. R/H AFT GALLEY SHEAR PLATE HAS SURFACE CORROSION
CORRECTIVE ACTION: REMOVED & REPLACED MAIN CABIN FLOOR STRUCTURE R/H FR69-70 SHEAR PLATE IAW A320 SDR F3LA2023061600079Shear Plate · crackedDISCREPANCY: REFERENCE AIRBONRE/PEMCO N/R 14018.0236 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX/ L/H AFT GALLEY SHEAR PLATE CRACKED
CORRECTIVE ACTION: REMOVED & REPLACED MAIN CABIN FLOOR STRUCTURE L/H FR69-70 SHEAR PLATE IAW A320 SRM 51-72-11SDR F3LA2023031000030Ruddervator · uncontrollableDISCREPANCY: RUDDER TRIM SYSTEM MADE 4 UNCOMMANDED TRIM INPUTS BETWEEN 1.3 AND 1.9 UNITS RIGHT. RUDDER TRIM RETURNED TO NEUTRAL WITHIN 1 MINUTE OF EACH EVENT.
CORRECTIVE ACTION: AS PER TSM 22-62-00-810-809-A STEP 4A CONTINUITY CHECK PERFORMED. REMOVED AND REPSDR F3LA2022081000085Elbow · leakingDISCREPANCY REFERENCE LP250150 ITEM 1 WHILE IN FLIGHT RECEIVED HYD G LOW PRESSURE ECAM FOLLOWED BY HYD G RSVR LOW LEVEL. PERFORMED APPLICABLE ECAM AND QRH PROCEDURES. GREEN SYSTEM SHOWED FULL LOSS OF FLUID.
CORRECTIVE ACTION: REMOVED AND REPLACED PRESSURE PIPSDR F3LA2022061500061Pipe · crackedDISCREPANCY: REFERENCE LOG PAGE LP224100 ITEM 1, FOUND YELLOW SYSTEM LEAK ON ENG 2 PYLON SUCTION
CORRECTIVE ACTION: REFERENCE LP224100 ITEM 1, REMOVED AND REPLACED CRACKED PIPE IN PYLON AMM 29-13-49-400-812-A AND AMM 20-21-12-911-050-A. REFERENCE LP224100 ITESDR F3LA2022061500060Reservoir · low quantityDISCREPANCY: REFERENCE LOG PAGE LP224098 ITEM 1, "HYD Y RSVR LO LVL".
CORRECTIVE ACTION: SERVICED Y HYD REF. AMM 12-12-29-611-001-A.SDR F3LA2022030800004Computer · inaccurateDISCREPANCY: REFERENCE LP168010 ITEM 1: L/G LGCIU 1 FAULT. RECYCLED L/G MANUAL EXTENSION PER QRH FAULT REMAINS. REFERENCE LP168010 ITEM 2: L/G DOORS NOT CLOSED. RESOLUTION: RETURNED L/G SYSTEM BACK TO THE NORMAL MADE AFTER FREE FALL EXTENSION IAW 32-00-00-860SDR F3LA202110190077Slide Raft · inoperativeLP183473 ITEM 2 DISCREPENCY --- EMER POWER SUPPLY UNIT 10WL INOP. CORRECTIVE ACTION LP189477 ITEM 1 -- R+R R1 DOOR SLIDE IAW AMM 25-62-44-00-802-A +25-62-44-400-802-A TW JC-2756 DUE DATE 6/14/2022SDR F3LA2020022530012Switch · failedPASSENGER O2 SYSTEM ACTUATED DURING FLIGHT FOR UNKNOWN REASON. 02/27/2020 SUPPLEMENT - CORRECTIVE ACTION: REFERENCE PEMCO NR 2788N3 AND LP1254353 ITEM 1, CABIN ALTITUDE PRESSURIZATION SWITCH FOUND FAULTY. REMOVED AND REPLACED CABIN ALTITUDE PRESSURIZATION SWITSDR F3LA201910150127Hose · frayedFIRST OFFICER`S OXYGEN MASK HOSE FRAYING. REMOVED AND REPLACED FO 02 MASK, OPS CHECK GOOD. AMM 35-12-41-400-002.SDR F3LA201910070121Control Unit · inoperativeSTRONG SMELL OF SOMETHING BURNING JUST BEFORE PUSHING FROM GATE . BRAKE SYSTEM 2 FAULT AT SAME TIME. INSPECTED AND FOUND NR 2 BSCU INOPERATIVE, REMOVED & REPLACED THE NR 2 BSCU, OPS CHECKED GOOD IAW AMM 32-42-34-401, ACFT OK FOR SERVICE.SDR F3LA2018103000474Fuel Line · leakingNR 1 ENGINE LEAKING FUEL. REMOVED AND REPLACED THREE GASKETS AT FUEL PUMP IAW 73-11-05 PB401 CONF 03. UPON FUEL LEAK CHECK FOUND FUEL LINE LEAKING. REMOVED AND REPLACED NR 1 ENGINE FUEL LINE FROM HEAT EXCHANGER TO FUEL PUMP IAW AMM 73-11-05 PB401.
LEAK CHECK
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.
Airframe · Airbus A320-251N
STC ST12434ACReplacement of the wing fuel tank access panel gasketSTC ST02714CHModify the aircraft interior to match standard passenger configurationsSTC ST00885LAInstallation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.