# Service difficulty reports: N480PX A list on [N480PX](https://openairdocs.org/aircraft/N480PX.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR REXA2026100601885](https://openairdocs.org/sdr/REXA2026100601885.md): Charger · inoperative · Sep 26, 2026 · N480PX · Cndair CL6002D24 · Emergency Lighting > AFT CABIN CEILING EMERGENCY LIGHTS INOP REMOVED + REPLACED AFT CHARGER IAW AMM 33-51-17. OPS CHK GOOD PN ON/OFF 11-0049 SN ON/ 2880 SN OFF 30716 - [SDR REXA2026092101851](https://openairdocs.org/sdr/REXA2026092101851.md): Retainer · damaged · Aug 18, 2026 · N480PX · Cndair CL6002D24 · Horizontal Stabilizer, Plate/Skin > AFTER SEAL REMOVAL ELONGATE SEAL RETAINER HOLES OF ACCESS PANEL 331AL WAS FOUND. SEAL RETAINER OF ACCESS PANEL 331AL WAS REPLACED AND MUST ME INSTALLED UNDER NRC 00217 PER CRJ-900 AMM 55-11-07-400-801 (CONFIG A01). - [SDR REXA2026092101850](https://openairdocs.org/sdr/REXA2026092101850.md): Floorbeam · cracked · Aug 15, 2026 · N480PX · Cndair CL6002D24 · Fuselage Main, Floor Beam > CRACKED CENTER COCKPIT FLOORBEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT CRACKED CENTER COCKPIT FLOORBEAM RBL 12 AT FS 280.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2248 R - [SDR REXA2026092101849](https://openairdocs.org/sdr/REXA2026092101849.md): Rib · cracked · Aug 15, 2026 · N480PX · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON MACHINED RIB OF LEADING EDGE BTW SS58.41 AT RH WING MACHINED RIB OF LEADING EDGE BTW SS58.41 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV-- - [SDR REXA2026092101848](https://openairdocs.org/sdr/REXA2026092101848.md): Floor Support · cracked · Aug 15, 2026 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50) FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STR - [SDR REXA2026092101847](https://openairdocs.org/sdr/REXA2026092101847.md): Bracket · cracked · Aug 15, 2026 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACK ON FWD OUTB SUPPORT TO ATTACH HYDRAULIC ACCUMULATOR AT NOSE HYDRAULICS COMPARTMENT SUPPORT OF ATTACH HYDRAULIC ACCUMULATOR WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01. - [SDR REXA2026092101846](https://openairdocs.org/sdr/REXA2026092101846.md): Rib · cracked · Aug 15, 2026 · N480PX · Cndair CL6002D24 · Wing, Rib/Bulkhead > CRACK ON LEADING EDGE RIB SS57.16 AT LH WING MACHINED RIB OF LEADING EDGE ON SS57.16 AT LH WING WAS PER REO 690-57-41-240 REV-- - [SDR REXA2026092101869](https://openairdocs.org/sdr/REXA2026092101869.md): Seat Track · corroded · Aug 14, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RT SIDE SEAT RAIL (1E/A) FROM BS 907 - 969 IN THE PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49. - [SDR REXA2026092101868](https://openairdocs.org/sdr/REXA2026092101868.md): Seat Track · corroded · Aug 14, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON THE RT SIDE SEAT TRACK, BS 661+101 - 847+14. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49 - [SDR REXA2026092101867](https://openairdocs.org/sdr/REXA2026092101867.md): Seat Track · corroded · Aug 14, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RT SIDE SEAT TRACK, BS 379 - 482. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49. - [SDR REXA2026092101866](https://openairdocs.org/sdr/REXA2026092101866.md): Seat Track · corroded · Aug 14, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LT SIDE SEAT TRACK, BS 744 - 761. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49 - [SDR REXA2026092101865](https://openairdocs.org/sdr/REXA2026092101865.md): Seat Track · corroded · Aug 14, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON RT SEAT TRACK, RBL 9 BTWN BS 349 - 677. THE SEAT TRACKS WAS REPLACED IAW AMM 53-00-49. - [SDR REXA2026092101863](https://openairdocs.org/sdr/REXA2026092101863.md): Seat Track · corroded · Aug 14, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON FLOOR SEAT TRACK FROM BS 374 TO 409, LBL 9 AT PAX CABIN. THE SEAT TRACK WAS REPLACED IAW AMM 53-00-49 - [SDR REXA2026092101864](https://openairdocs.org/sdr/REXA2026092101864.md): Seat Track · corroded · Aug 13, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON LT SEAT TRACK, LBL 9 BTWN BS 581 - 661+32 AND BTWN BS 661+32 - 677. THE SEAT TRACKS WERE REPLACED IAW AMM 53-00-49. - [SDR REXA2026092101862](https://openairdocs.org/sdr/REXA2026092101862.md): Bracket · corroded · Aug 13, 2026 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CORROSION ON MACHINED BRACKETS (4E/A) FROM FS501.00 TO FS661.00+32 AND BTW STGR 26LH AND STGR 26RH AT BAGGAGE BAY. MACHINED BRACKETS (4E/A) FROM FS501.00 TO FS661.00+32 AND BTW STGR 26LH AND STGR 26RH AT BAGGAGE BAY WERE REPLACED PER CRJ 900 SRM 51-42-06-001-0 - [SDR REXA2026092101870](https://openairdocs.org/sdr/REXA2026092101870.md): Support Angle · cracked · Aug 12, 2026 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > CRACKED SUPPORT ANGLE, STR 17R BTW BS 317 - 319. THE SUPPORT ANGLE WAS REPLACED IAW SRM 51-42-10-001-001-A01, & SRM 51-42-13-001-001-A01. - [SDR REXA2026092101861](https://openairdocs.org/sdr/REXA2026092101861.md): Plate · worn · Aug 10, 2026 · N480PX · Cndair CL6002D24 · Trailing Edge Flaps > "WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42- - [SDR REXA2026092101860](https://openairdocs.org/sdr/REXA2026092101860.md): Plate · worn · Aug 10, 2026 · N480PX · Cndair CL6002D24 · Trailing Edge Flaps > "WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42- - [SDR REXA2026092101859](https://openairdocs.org/sdr/REXA2026092101859.md): Fitting · worn · Aug 10, 2026 · N480PX · Cndair CL6002D24 · Trailing Edge Flaps > "WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42- - [SDR REXA2026092101858](https://openairdocs.org/sdr/REXA2026092101858.md): Fitting · worn · Aug 10, 2026 · N480PX · Cndair CL6002D24 · Trailing Edge Flaps > "WEAR ON FLAP FITTING AND PLATE SUPPORT OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES FLAP FITTING (2EAS) AND PLATE SUPPORT (2EAS) OF ""FLAP STUB FAIRING"" 171DL AND 172DR AT RH/LH SIDES WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01,SRM 51-42- - [SDR REXA2026092101842](https://openairdocs.org/sdr/REXA2026092101842.md): Web · corroded · Aug 10, 2026 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > WEAR AND CORROSION ON SETTLEMENT AREAS (4 LOCATIONS) OF MLG BINS AT LH/RH WHEEL WELL AREA MACHINED WEB LH ON MLG BINS AT LH WHEEL WELL AREA P/N CC670-39221-3 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-21-001-001-A01. - [SDR REXA2026092101841](https://openairdocs.org/sdr/REXA2026092101841.md): Angle · corroded · Aug 10, 2026 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > WEAR AND CORROSION ON SETTLEMENT AREAS (4 LOCATIONS) OF MLG BINS AT LH/RH WHEEL WELL AREA ANGLE PN: (SH670-36386-16) WAS REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01. - [SDR REXA2026092101840](https://openairdocs.org/sdr/REXA2026092101840.md): Angle · corroded · Aug 10, 2026 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > WEAR AND CORROSION ON SETTLEMENT AREAS (4 LOCATIONS) OF MLG BINS AT LH/RH WHEEL WELL AREA ANGLE PN: (SH670-36386-15) WAS REPLACED PER CRJ-900 SRM 51-42-10-001-001-A01. - [SDR REXA2026092101857](https://openairdocs.org/sdr/REXA2026092101857.md): Latch · cracked · Aug 9, 2026 · N480PX · Cndair CL6002D24 · Service Doors > FWD LAV SERVICING DOOR TOP HINGE AND BOTTOM LATCH BROKEN TOP HINGE AND BOTTOM LATCH AT FWD LAV SERVICING DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ9-00 SRM 51-41-02-001-001-A01. - [SDR REXA2026092101856](https://openairdocs.org/sdr/REXA2026092101856.md): Hinge · cracked · Aug 9, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Door Hinge > FWD LAV SERVICING DOOR TOP HINGE AND BOTTOM LATCH BROKEN TOP HINGE AND BOTTOM LATCH AT FWD LAV SERVICING DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ9-00 SRM 51-41-02-001-001-A01. - [SDR REXA2026092101853](https://openairdocs.org/sdr/REXA2026092101853.md): Plate · worn · Aug 6, 2026 · N480PX · Cndair CL6002D24 · Passenger/Crew Doors > WEAR ON FWD AND AFT PLATE (2EA) OF PASSENGER DOOR. FWD AND AFT NEW PLATE (2EA) OF PASSENGER DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01; CRJ-900 SRM 51-42-21-001-001-A01 AND CRJ-900 SRM 51-42-13-001-001-A01. - [SDR REXA2026092101852](https://openairdocs.org/sdr/REXA2026092101852.md): Plate · worn · Aug 6, 2026 · N480PX · Cndair CL6002D24 · Passenger/Crew Doors > WEAR ON FWD AND AFT PLATE (2EA) OF PASSENGER DOOR. FWD AND AFT NEW PLATE (2EA) OF PASSENGER DOOR WERE REPLACED PER SRM 51-42-06-001-001-A01; CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-42-13-001-001-A01. - [SDR REXA2026092101845](https://openairdocs.org/sdr/REXA2026092101845.md): Bracket · worn · Aug 6, 2026 · N480PX · Cndair CL6002D24 · Passenger/Crew Doors > WEAR ON BRACKET RETAINING (2EA) AND MISSING GROMMETS ON BRACKET RETAINING (4EA) OF PASSENGER DOOR. BRACKET RETAINING (2EAS) WERE REPLACED PER CRJ-900 SRM 51-42-21-001-001-A01,GROMMETS ON BRACKET RETAINING (4EA) WERE INSTALLED PER CRJ-900 AMM 52-11-05-350-801. - [SDR REXA2024103101258](https://openairdocs.org/sdr/REXA2024103101258.md): Retainer · chafed · Mar 15, 2024 · N480PX · Cndair CL6002D24 · Fuselage Main, Structure > CENTRAL BAGGAGE BAY DOOR - LOWER SEAL RETAINER IS CHAFED ON BOTH CORNERS. REMOVED CENTER BAGGAGE BAY DOOR LOWER SEAL RETAINER P/N LE670-39644-1 IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED SERVICEABLE LOWER SEAL RETAINER WITH P/N LE670-39644-1 - [SDR REXA2024080600636](https://openairdocs.org/sdr/REXA2024080600636.md): Panel · cracked · Mar 6, 2024 · N480PX · Cndair CL6002D24 · Passenger/Crew Doors > THE TOP PANEL ON PAX DOOR UNDER UPPERMOST STEP HAS 2EA CRACKS, PANEL REQUIRES REPLACEMENT OR REPAIR REMOVED DAMAGED TOP PANEL PAX DOOR STAIRS IAW CRJ-900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED AND DRILLED NEW TOP PANEL PAX DOOR STAIRS P/N - [SDR REXA2024080500617](https://openairdocs.org/sdr/REXA2024080500617.md): Floorbeam · corroded · Mar 5, 2024 · N480PX · Cndair CL6002D24 · Fuselage Main, Floor Beam > "FS 280 FWD J ANGLE IS CORRODED BETWEEN LBL 9 AND RBL 9 REMOVED AND REPLACED FS280 ""J"" ANGLE IAW CRJ900SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. " - [SDR REXA2024031300281](https://openairdocs.org/sdr/REXA2024031300281.md): Web · cracked · Mar 5, 2024 · N480PX · Cndair CL6002D24 · Fuselage Miscellaneous Structure > PASSENGER DOOR AFT WEB HAS 4 EACH CRACKS AT STEP LOCATIONS. REMOVED PAX DOOR AFT WEB IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01 AND INSTALLED NEW SERVICEABLE PAX DOOR AFT WEB P/N 601R317071-11S IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-00 - [SDR REXA2024031100252](https://openairdocs.org/sdr/REXA2024031100252.md): Panel · cracked · Mar 5, 2024 · N480PX · Cndair CL6002D24 · Passenger/Crew Doors > PASSENGER DOOR- FWD WEB CRACKED IN 4 EACH LOCATIONS AT STEP LOCATIONS. REQUIRES REPLACEMENT REPAIRED FWD WEB IAW CRJ 900 SRM 52-11-04-201-004-A01 REPAIR ZONE 2 AND ZONE 2 AND ZONE 3 REPAIR PARTS IAW CRJ-900 SRM 51-40-11-001-001-A01. ZONE 2 AND ZONE 3 CUTOUT R - [SDR REXA2024080500616](https://openairdocs.org/sdr/REXA2024080500616.md): Drag Angle · cracked · Mar 4, 2024 · N480PX · Cndair CL6002D24 · Passenger/Crew Doors > PASSENGER DOOR - CRACK ON THE AFT DRAG ANGLE. REPAIRED AFT DRAG ANGLE ON PASSENGER DOOR IAW CRJ-900 SRM 52-11-04-201-002-A01. - [SDR REXA2020081300614](https://openairdocs.org/sdr/REXA2020081300614.md): Battery Pack · failed · Aug 8, 2020 · N480PX · Cndair CL6002D24 · Emergency Lighting > REMOVED AND REPLACED EMERG BATT PACK AT PS38. WOULD NOT TEST IAW JOBCARD 33-900-701. REMOVED AND REPLACED BATT PACK AT PS38 IAW AMM 33-51-17 ALL CHECKS GOOD. - [SDR REXA2020081300613](https://openairdocs.org/sdr/REXA2020081300613.md): Charger · failed · Aug 8, 2020 · N480PX · Cndair CL6002D24 · Emergency Lighting > REMOVED AND REPLACED PS37 IAW JOB CARD 33-900-701 EMERGENCY LIGHTS WOULD NOT TEST. REMOVED AND REPLACED EMERG BATT PACK AT PS 37 NO FIX IAW CRJ900 AMM 33-51-17 NO FIX. REMOVED AND REPLACED CHARGER AT PS37 IAW AMM 33-51-17. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N480PX' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N480PX/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.