Location
Columbia, MD
Owner type
Corporation
Serial number
8380
Year built
2018
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
October 26, 2018
Certificate issued
October 25, 2018
Expires
October 31, 2028
Mode S code
A3B05D

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 N337FRMatched 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 N337FRMatched 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 · 12

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

SDR F3LA2024072300111Check Valve · inoperativeLP481863 ITEM 1ENGINE #1 STALL ENROUTE TWICE AT FL 370, NO ABNORMAL ENGINE PARAMETERS OBSERVED. THIS AIRCRAFT WAS GROUNDED AS A RESULT OF THIS DEFECT. LP481863 ITEM 1. IAW TSM 77-11-00-810-815-A, REMOVED AND REPLACED IP CHECK VALVE IAW AMM TASK 36-11-41-200-Jul 19, 2024 · N337FR · Airbus A320251N · Engine (Turbine/Turboprop)SDR F3LA2024042500059Check Valve · defectiveDURING CRUISE LEVEL OFF AT FL380, ECAM ENG 1 STALL FOR APPROX 6-10 SECS. N1 WAS APPROX 74%. THIRD OCCURRENCE IN 7 DAYS. REF LP 388967 AND 388971. N1 WAS BEING COMMANDED TO HIGHER N1 (APPROXIMATELY 82%) AND N1 STUCK AT 74% FOR APPROX 10 SECONDS. FA'S REPORTED Apr 18, 2024 · N337FR · Airbus A320251N · Engine (Turbine/Turboprop)SDR F3LA2024032800041Shear Plate · crackedREFERENCE NR 5001308391-0040 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CRACK SHEAR PLATE FOUND DURING INSPECTION OF AFT CABIN FLOOR BET FR69-70 RH. REPLACE AS PER A320N SRM 51-72-11 REV39. INSTALLED NEW SHEAR PLATE ON AFT CABIN FLOOR BET FMar 24, 2024 · N337FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2024032800040Shear Plate · crackedREFERENCE NR 5001308391-0020 AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CRACK SHEAR PLATE FOUND DURING INSPECTION OF AFT CABIN FLOOR BET FR69-70 LH. REPLACE AS PER A320N SRM 51-72-11 REV39. INSTALLED NEW SHEAR PLATE ON AFT CABIN FLOOR BET FRMar 24, 2024 · N337FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2024040300045Door Sill · corrodedAIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. CORROSION FOUND ON RH DOOR SILL BEAM DURING INSPECTION OF AFT CABIN FLOOR STRUCTURES AT FR68. EVALUATE AS PER A320N SRM TASK 53-41-14-300-001 REV 39. PERFORMED INSTALLATION OF REPAIR PARTS ON AFT Mar 14, 2024 · N337FR · Airbus A320251N · Fuselage Miscellaneous StructureSDR F3LA2023082900150Valve · stuckREFERENCE LP 35036 ENG 1 STALL ECAM UPON REACHING CRUISE AT FL370. ECAM LASTED 3-5 SEC NO OTHER ECAM REMAINDER OF FLIGHT. REMOVED AND REPLACED IP VALVE IAW AMM 36-11-41-000 /400-803-A OPS CHECK GOOD NO FAULTS AT THIS TIME AC OK FOR SERVICE.Aug 27, 2023 · N337FR · Airbus A320251N · Engine (Turbine/Turboprop)SDR F3LA2022113000156Check Valve · damagedON LANDING ROLLOUT, AN ECAM FOR A NR 1 ENGINE STALL WITH LARGE SURGE FELT. TOWER HEARD AN AUDIBLE BANG FELT THE CONCUSSION. FOUND IP CHECK VALVE TO BE DAMAGED, REPLACED IAW AMM 36-11-41-000-040. PERFORMED ACCEL/DECCEL TEST IAW AMM 71-00-00-710-814 ALL PARNov 26, 2022 · N337FR · Airbus A320251N · Turbine Engine Compressor SectionSDR F3LA2021011400003Battery · dischargedUPON AIRCRAFT INSPECTION THE EMERGENCY POWER SUPPLY UNIT (EPSU BATTERY) FAILED TO TEST. CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY. OPERATIONS CHECK GOOD, REF AMM 33-51-00-710-050-B.Jan 13, 2021 · N337FR · Airbus A320251N · Emergency LightingSDR F3LA2020111700045Connector · looseDISCREPANCY: FWD FACING EXIT LIGHT OVER EXIT ROW 13 INOPERABLE. CORRECTIVE ACTION: GROUND CONNECTOR TO EXIT LIGHT ASSEMBLY LOOSE. SECURED GROUND CONNECTOR, OPERATIONS CHECK OF EMERGENCY LIGHT SYSTEM GOOD, REF AMM 33-51-00-710-805-A.Nov 14, 2020 · N337FR · Airbus A320251N · Light System WiringSDR F3LA2020090800034Relay · failed09/06/2020-CORRECTIVE ACTION: REMOVED AND REPLACED RELAY FIN#3PH, IAW TSM 24-24-00-810-806-A. OPS CHECK GOOD, AIRCRAFT OF FOR RETURN TO SERVICE. 09/05/2020-FAILS EMER GEN TEST, AS PER HEAVY SERVICE CHECK TASK CARD 281100-01 STEP 8 AMM REF 24-24-00-710-001-A,Sep 5, 2020 · N337FR · Airbus A320251N · External Power SystemSDR F3LA202007300032Actuator · leakingTHS ACTUATOR LEAKING AND SIGHT GLASS READS MIN. REMOVED AND REPLACED ACTUATOR PER A320 AMM 27-44-51-000-001-A & 27-44-51-400-001-A. OPS & LEAK CHECK GOOD.Jul 26, 2020 · N337FR · Airbus A320251N · Stabilizer ActuatorSDR F3LA201962600045Unknown · odorSTRONG SMELL OF BURNING RUBBER AROUND ROWS 9-10 ON DESCENT. AIRCRAFT WAS GROUNDED DUE TO DISCREPANCY. DISIPATED ON LANDING - NO DEFECT NOTED. CHECKED ROW 9 AND 10 FOR BURNING EVIDENCE. OK FOR SERVICE. REF AMM 05-50-00-PB001-00. MX INSPECTED BALLAST ON LEFT AJun 24, 2019 · N337FR · Airbus A320251N · Air 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