Location
Columbia, MD
Owner type
Corporation
Serial number
8516
Year built
2018
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 18, 2018
Certificate issued
October 18, 2018
Expires
October 31, 2028
Mode S code
A3C192

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 N341FRMatched 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 N341FRMatched 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 · 10

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

SDR F3LA202508200285Servo Valve · failedAIRCRAFT WAS UNDERGOING SERVICE CHECK DURING RON MAINTENANCE AND WORKING MDDR# 1235083, NO FLIGHT DELAY. LP599245 ITEM 1 F/CTL AIL SERVO FAULT PLACED ON MEL 27-14-01B CN 1235081 PLACARD INSTALLED AND R/H WING INBOARD SERVO VALVE 33CE2 DEACTIVED. REMOVED ANDAug 19, 2025 · N341FR · Airbus A320251N · Aileron Control SystemSDR F3LA202507140268Servo Valve · faultedLP461953 #2 ON CLIMB OUT IN A RIGHT TURN PLANE SHOOK VIOLENTLY SPEED 320 ALT 260 FOLLOWED BY FLT CTL AIL SERVO FAULT. FOLLOWED TSM 27-10-00-810-820-A, REMOVED AND REPLACED RH AILERON INBD SERVO CONTROL (33CE2) PER A320 AMM 27-14-51-000-001-A, 27-14-51-400-00Jul 11, 2025 · N341FR · Airbus A320251N · Aileron Control SystemSDR F3LA202412250173Computer · faultedACFT WAS TAKEN OUT OF SERVICE FOR THIS EVENT. REFERENCE LOG PAGE LP464308 ITEM 3, F/CTL AIL SERVO FAULT. REMOVED AND REPLACED ELAC 1 2CE1 REF. AMM 27-93-34-000-001-A AND AMM 27-93-400-001-A. OPS TEST GOOD. A/C OK FOR SERVICE.LAND CAT IIIB RETAINED.Dec 24, 2024 · N341FR · Airbus A320251N · Elevator Control SystemSDR F3LA202412250172Fuse · failedACFT WAS TAKEN OUT OF SERVICE FOR THIS EVENT. REFERENCE LOG PAGE LP464308 ITEM 2, ELEC DC ESS BUS SHED. REPLACED FUSE 20PC1 REF. AMM 24-35-00-960-801-A. OPS TEST GOOD. A/C OK FOR SERVICE. T/W S/N F9TAB12568C D/D 03/2025.Dec 24, 2024 · N341FR · Airbus A320251N · DC Generating SystemSDR F3LA202412250171Computer · faultyACFT WAS TAKEN OUT OF SERVICE FOR THIS EVENT. REFERENCE LOG PAGE LP464309 ITEM 1, F/CTL ELAC 1 FAULT. REMOVED AND REPLACED ELAC 1 2CE1 REF. AMM 27-93-34-000-001-A AND AMM 27-93-400-001-A. OPS TEST GOOD. A/C OK FOR SERVICE. LAND CAT IIIB RETAINED. REF. LP464Dec 24, 2024 · N341FR · Airbus A320251N · Elevator Control SystemSDR F3LA2024081300114Valve · bypassingLOSS OF BRAKING WITH THE PARKING BRAKE SET ENGINES RUNNING AT GATE. PLANE MOVED FORWARD 2-3 FEET. MEMORY ITEMS APPLIED AND PLANE CAME TO A STOP PARKING BRAKE HANDLE CYCLED AND BRAKE PRESSURE RESTORED. AIRCRAFT WAS REMOVED FROM SERVICE AS A RESULT OF THIS EVENTAug 8, 2024 · N341FR · Airbus A320251N · Landing Gear Brake SystemSDR F3LA2024042900060Shear Plate · crackedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SHCEDULED MX. DURING INSPECTION R/H SHEAR PLATE FR69-FR70 CRACKED REQUIRES REPLACEMENT AS PER SRM 51-72-11-911-001 REV 39. R/H SHEAR PLATE WAS REPLACED AS PER SRM 51-72-11-911-001 REV 39. MX ACTION IS ACCEPTABLE.Apr 12, 2024 · N341FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2024041900054Door Sill · corrodedREFERENCE LTPR NR 5001313422-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION ON LH DOOR SILL BEAM NUT PLATE HOLE IS BEYOND ADL WITH 100% MATERIAL LOSS WHICH REQUIRES REPAIR AS PER A320 NEO SRM TASK 53-41-14-283-002 REV. 39. LH DOOApr 12, 2024 · N341FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2024041900053Shear Plate · crackedREFERENCE LTPR NR 5001313403-0010 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION FOUND L/H SHEAR PLATE FR69-70 CRACKED REQUIRES REPLACEMENT AS PER SRM 51-72-11-911-001 REV. 39. L/H SHEAR PLATE WAS REPLACED AS PER SRM 51-72-11-9Apr 12, 2024 · N341FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2021081600059Seal · failedRT WING AIR LEAK. R/R #2 PACK OZONE CONVERTER SEAL AS REQUIRED. OPS CHECK & LEAK CHECK GOOD REF AMM 21-51-41-04.Aug 13, 2021 · N341FR · Airbus A320251N · Airfoil Anti/De-ice 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

Earlier aircraft with this N-number · 1

This aircraft carried N341FR before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.