N546FF

Service difficulty reports · 80

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

Query with SQL
duckdb -csv -c "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 = 'N546FF' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA202610230005Skin · corrodedCORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNA2026F00010Skin · corrodedCORROSION ON STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT STRUCTURE INNER SKIN AREA WHERE MAIN AVIONICS COMPARTMENT DOOR SEAT WAS REPAIRED PER REO: 670-53-21-242 REV: - C.Oct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202610230004Strap · corrodedCORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT CORROSION ON STRUCTURE WHERE ACCESS PANEL 195AB SEAT WAS REMOVED PER CRJ 700 SRM 51-21-06-001-001-A01 AND EVALUATED (SEAT BTW FS 847) WITHIN OF LIMIT AND SEAT BTW FS 849 TO FS 879 WAS EVALUATED OUT OF LIMITSOct 23, 2026 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202610230003Support · corrodedCORROSION ON FAIRING SUPPORT (FRAMES) 2 EAS STA BS 629 AND 661 AND DIAFRAGMA 1EA BTW FS 629-FS 661 (SEATLEMENT AREA, UNDER ACCESS PANELS 191 AB, 191BB AND 192BB ) SUMMARY:CORROSION WAS REMOVED PER 51-42-06-001-001-A01 AREA WAS EVALUATE PER SRM 53-82-55-101-0Oct 23, 2026 · N546FF · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA202610230002Bracket · corrodedCORROSION ON ANTI-ROTATION BEAM ASSY ON LT FWD DOOR HINGE AT NLG W/W. CORROSION ON ANTI-ROTATION BEAM ASSY WAS REMOVED IAW SRM 51-21-06-001-001-A01. AND AREA IT IS OUT LIMITS PER SRM 53-00-00-101-001-A01 AND ANTI-ROTATION BEAM ASSY ON LT FWD DOOR HINGE AT NLGOct 23, 2026 · N546FF · Cndair CL6002C10 · Main Landing GearSDR VNAA202610230001Hinge · corroded"IN REF TASK TRFKE00AXBMU : AFTER REMOVAL OF BUSHINGS THE MOUNTING HOLES FOR HINGES ASSY # 3 (2EA) ON RH AILERON REAR SPAR WERE OVERSIZED AND AFTER REMOVAL OF BUSHINGS THE MOUNTING HOLES FOR HINGE ASSY 2# S (1EA) ON LH AILERON REAR SPAR WAS OVERSIZED ON HOLES Oct 23, 2026 · N546FF · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNAA2026050617501Steering Sys · faultedNOSE WHEEL STEERING INOP. JACK NOSE OF AIRCRAFT TO DUE NLG GEAR SWING IAW AMM 32-30-00-865-802-A01. OPS CHECK GOOD. DID STEERING BITE TEST IAW AMM 32-50-00-740-801-A01. OPS CHECK GOOD AT THIS TIME. OPS CHECK GOOD DURING TAXI NO ISSUES FAULT DIDN€™T RECUR.May 5, 2026 · N546FF · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2025122611101Transducer · leakingHYD SYSTEM 2 LOW PRESSURE CAUTION MSG. IN FLIGHT. EMER DECLARED. / UPON ARRIVAL TO AIRCRAFT CLEANED AFFECTED AREA AND FOUND LEAK COMING FROM THE SYSTEM #2 PRESSURE TRANSDUCER. FOUND THE PRESSURE TRANSDUCER TO BE LOOSE AND HAD A CRUSHED O-RING. REPLACED O-RING Dec 24, 2025 · N546FF · Cndair CL6002C10 · Hydraulic System, MainSDR VNAA2025091411101Safety Valve · faultedCABIN PRESSURIZATION FAILED IN DESCENT INTO BHM. APPROX 15000FT PRESSURIZATION BECAME ERRATIC AND CABIN ALT STARTED TO INCREASE. AT 8500FT AMBER CABIN ALT THEN RED CABIN ALT. RAN QRC/ARH FOR CABIN ALT. REMOVED AND REPLACED NR 2 SAFTEY VALVE IAW AMM 21-32-03-0Sep 10, 2025 · N546FF · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA2025072311101Duct · leakingL BLEED DUCT CAUTION MSG IN FLIGHT. / UPON LEAK CHECK FOUND LEAK AT LH CONNECTOR DUCT FWD OF FLOW CONTROL VALVE AND AT APU BLEED AIR CHECK VALVE. REMOVED AND REPLACED CONNECTOR DUCT IAW AMM 36-19-03-000/400. PERFORMED LEAK TEST IAW AMM 36-10-00-790-801. LEAK Jul 17, 2025 · N546FF · Cndair CL6002C10 · Pneumatic SystemSDR VNAA2025041411102Anti-Skid Sys · faultedA\SKID FAULT IN FLIGHT. PERFORMED HYDRAULIC SYS 1,2,AND 3 BLEED IAW AMM 29-10-00-870-801-A01 AND 29-10-00-870-802-A01. ACCOMPLISHED GVI OF BRAKE-UNIT ASSEMBLY WEAR-PIN INDICATOR IAW CRJ 700 AMM 32-43-26-210-801-A01. NO DEFECTS NOTED AT THIS TIME. FLT CREW COApr 13, 2025 · N546FF · Cndair CL6002C10 · Brake Anti-Skid SectionSDR VNAA202504140037Post · corrodedVERTICAL POST LBL12 IS CORRODED AT F.S.280 FRAME AND STRINGER 25L REMOVED VERTICLE POST AT LBL12 AND INSTALLED NEW SERVICEABLE VERTICLE POST P/N CC670-34180-7 AT LBL12 F.S 280 WITH NEW IAW CRJ 700 SRM 51-42-13-001-001-A01 AND 51-42-21-001-001-A01Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202504140036Lock Fastener · shearedLOCK FASTENER HEAD IS SHEARED AT RIGHT SLAT LEADING EDGE AT SLAT TRACK 1-1 POSITION. CORRECTIVE ACTION: REPLACED RH LE SLAT PANEL SHEARED RIVET AT SLAT TRACK 1-1 WITH A NEW SERVICEABLE HI-LITE PN: PLT1092-6 IAW MHIRJ CRJ 700 REO 670-57-42-2041 REV-- DATED 03/2Apr 7, 2025 · N546FF · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA202504140035Stringer Clip · corrodedGUSSET AT STR 20 FS 333 FOUND TO BE DAMAGED REQUIRES REPLACEMENT. FABRICATED NEW SERVICEABLE GUSSET P.O.#5-39394 IAW CRJ 700 SRM 51-24-36-001-001-A01. DRILLED AND LOCATED HOLES IN NEW SERVICEABLE GUSSET IAW CRJ 700 SRM 51-40-11-001-001-A01. PRIMED AND PAINTEApr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA202504140034Bulkhead Web · corrodedFS 280 LH LOWER WEB HAS CORRSION. REPAIRED LH LOWER WEB IAW CRJ 700 SRM 53-11-10-201-004-A01Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA202504140033Floorbeam · corrodedFS 280.00 FWD FLOOR SUPPORT J-ANGLE IS SEVERELY CORRODED. REQUIRES REPLACEMENT. ORIGINAL MATERIAL THICKNESS IS .063. REMOVED DAMAGE DEPTH IS .018. MAX ALLOWED IS .006. REMAINING THICKNESS IS .045. REMOVED AND REPLACE FS 280.00 FWD FLOOR SUPPORT J-ANGLE P/N CApr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202504140032Intercostal · corrodedHN00228605 DISCREPANCY: INTERCOSTAL AT STRINGER 20R BETWEEN F.S.319-F.S.333 HAS LIGHT CORROSION AROUND RIVET HEAD ADJACENT TO GS328. CORRECTIVE ACTION: REMOVE INTERCOSTAL AT STRINGER 20R BETWEEN F.S.319-333 IAW CRJ700 SRM 51-42-06-001-001-A01 & 51-42-21-001-00Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504140031Intercostal · corrodedHN00228604 DISCREPANCY: INTERCOSTAL AT STRINGER 20R IS CORRODED BETWEEN F.S.310-319 CORRECTIVE ACTION: REMOVE INTERCOSTAL AT STRINGER 20R BETWEEN F.S.310-319 AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-23-00-001-001-A01, Apr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202504140030Angle · corrodedCLIP/KLEAT (ANGLE) @ FS310.00 STGR 20, FOUND TO BE CHAFED, CORRODED, REQUIRES R&R CORRECTIVE ACTION: DRILLED, LOCATED, AND INSTALLED NEW SERVICEABLE P/N(SH670-32046-3) CLIP/KLEAT(ANGLE) @ FS310.00 STGR 20 IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-AApr 7, 2025 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2024051511101Selector Valve · unserviceableHAD GEAR DISAGREE WARNING MSG AT GEAR RETRACTION. RAN QRC\QRH . GEAR SUCCESSFULLY LOCKED IN DOWN POSITION / INTERROGATED MDC FOUND B1 005969. PREFORMED TROUBLESHOOTING IAW CRJ 700 FIM 32-31-00-810-804. PREFORMED OPERATIONAL CHECK IF THE LANDING GEAR EXTENSIOMay 13, 2024 · N546FF · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA202308311112Unknown · unknownSMOKE/ABNORMAL SMELL IN THE COCKPIT FIM FASK NEEDS TO BE C/W DUE TO POSSIBLE ARCING. PERFORMED SMOKE/ABNORMAL SMELL IN THE COCKPIT CHECK IAW CRJ700 FIM 21-21-00-810-806-A01 AND CHECK GOOD.NO SIGN OF SMOKE OR BURN.Aug 30, 2023 · N546FF · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202211209992Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL (SEVERAL LOCATIONS), PAX CABIN. (REF. FS661+13" TO FS708+5").Oct 17, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202211209991Skin Panel · nickedNICKS ON FWD CARGO CUT OUT SURROUND SKIN (FWD, REAR & UPPER FRAMES).Oct 17, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2022112099910Stringer Splice · corrodedAFTER REMOVAL OF STRINGER 21RH, CORROSION WAS FOUND ON STGR SPLICE 21R AT FS 333.00 ON MAIN AVIONICS COMPARTMENT INTERNAL STRUCTUREOct 16, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202211209998Seat Track · corrodedCORROSION ON SEAT RAIL RBL9 & BTW FS485 - FS581.. AT PAX CAB.Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202211209997Seat Track · corrodedCORROSION ON SEAT RAIL LBL9 & BTW FS485 - FS581. AT PAX CAB.Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202211209996Seat Track · corrodedCORROSION ON SEAT RAIL LBL27 & BTW FS581 - FS693. AT PAX CAB.Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202211209995Seat Track · corrodedCORROSION ON SEAT RAIL LBL27 & BTW FS485 - FS581. AT PAX CAB.Oct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202211209994Seat Track · corrodedCORROSION ON SEAT RAIL LBL27 & BTW FS364 - FS485. AT PAX CABOct 9, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202211209999Intercostal · corrodedCORROSION AT INTERCOSTAL (3 EAS) BETWEEN STRG 25L TO STRG 25R AND BETWEEN FS 349 TO FS364.Oct 8, 2022 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202211209993Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL BTW FS661+13" TO FS708+5”Oct 8, 2022 · N546FF · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2022112099918Frame · corrodedCORROSION ON FRAME AT FS 1015.00 BTW STGR 26LH AND 26RH ON AFT CARGO COMPARTMENT INTERNAL STRUCTUREOct 5, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2022112099917Frame · corrodedCORROSION ON FRAME AT FS 1047.00 BTW STGR 25LH AND 24LH ON AFT CARGO COMPARTMENT INTERNAL STRUCTUREOct 5, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2022112099915Frame · corrodedCORROSION ON FRAME FS 1088.20 BTW STGR 26LH AND 26RH ON AFT CARGO COMPARTMENT INTERNAL STRUCTUREOct 5, 2022 · N546FF · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2022030310111Windshield · unserviceableON DECENT INTO DCA CA SIDE WINDSHIELD ARCHED AND OVERHEATED. DECLARED EMERGENCY LANDED WITHOUT INCIDENT. TAXI TO GATE MX HAS BEEN CALLED. TRUCKES ROLLED AIRCRAFT CANNOT BE FERRIED. ORF ROAD TRIP IS BE PUT TOGETHER. / REPLACED CAPT WINDSHIELD IAW CRJ 700 AMM 56Mar 1, 2022 · N546FF · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA202105311112Windshield · sparksON APPROACH INTO CVG, CAPTAIN AND FO STARTED SEEING SPARKS COMING FROM THE FRONT RIGHT WINDSCREEN. RAN THE QRH AND DECLARED. LANDED SAFELY AND HAD FIRE AND RESCUE CHECK THEIR WINDSHIELD FOR HEAT. CREW NOTICED A VISIBLE CRACK. MX HAS BEEN ADVISED. REMOVED ANDMay 29, 2021 · N546FF · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2020041811101Cooling Fan · failedBURNING SMELL IN COCKPIT WITH DISPLAY COOL MSG. REMOVED AND REPLACED #2 DISPLAY COOLING FAN IAW CRJ-700 AMM. OPS CHECK GOOD.Apr 16, 2020 · N546FF · Cndair CL6002C10 · Air Distribution FanSDR VNAA2020041111101Hydraulic Line · damagedHYDRAULIC 3B LOW PRESSURE CAUTION JUST AFTER TAKING HIGH SPEED EXIT C10 36R. FIRE DEPARTMENT TRUCKS NEEDED TO ASSIST IN ENVIRONMENTAL FLUID SPILL. HAZMAT CLEANED UP ON C11. AIRCRAFT NEEDED TOW TEAM TO MAKE IT TO GATE IN CLT. REMOVED AND REPLACED FLEXIBLE HOSE Apr 9, 2020 · N546FF · Cndair CL6002C10 · Hydraulic System, MainSDR VNAA2020010951102Connector · dirtyON THE ARRIVAL AT FL060, STAB TRIM RUNAWAY. THE CREW RAN THE QRH AND DECIDED TO DIVERT TO IAD FOR THE LONGER RUNWAY. CREW DECLARED AN EMERGENCY. CABI DID NOT BRACE, TRUCKS DID ROLL. FLIGHT LANDED ON RWY 1C WITHOUT FURTHER INCIDENT AND WAS ABLE TO TAXI TO GAJan 5, 2020 · N546FF · Cndair CL6002C10 · Flight Control System WiringSDR VNAA2019032899901Door Sill · corrodedALT CARGO DOOR SILL CORRODED ON AFT END, UPPER SURFACE. REPLACED AFT CARGO BAY DOOR TOWER SILL.Mar 28, 2019 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2018122321102Filter · dirtyAFTER PUSHBACK, CREW REPORTED A BURNING SMELL. MAINTENANCE REPLACED BOTH RECIRC FAN FILTERS. OPS CHECK GOOD NO ODORS NOTED.Dec 22, 2018 · N546FF · Cndair CL6002C10 · Air Distribution SystemSDR VNAA2018101611102Acm · malfunctionedON GROUND EMERGENCY DECLARED IN DCA AFTER SMOKE PRESENT ON THE FLIGHTDECK AND REPORTS OF A BURNING PLASTIC SMELL. NO VISIBLE FIRE. MX WENT TO INSPECT AND FOUND THE LT PACK MAKING A GRINDING NOISE. MX R&R LH ACM. OPS CHECK GOOD.Oct 16, 2018 · N546FF · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2018090311101Unknown · malfunctionedDURING CLIMBOUT, CAPTAIN NOTICED THAT THE FLIGHT CONTROLS WERE ACTING SLUGGISH REQUIRING 3 TO 4 TIMES THE AMOUNT OF FORCE NEEDED TO MAKE THE AIRCRAFT TURN. DID NOT FOLLOW THE QRH AND THE STATION DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. Sep 3, 2018 · N546FF · Cndair CL6002C10 · Flight Control SystemSDR VNAA2017071411101Acm · failedON APU START THE CREW RECEIVED A RIGHT AIR CONDITIONING PACK AUTO FAILED WITH THE PACK TEMPERATURE GOING TO 99 DEGREES. CAUSING SMOKE AND FUMES TO FILL THE CABIN.Jul 14, 2017 · N546FF · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2016123000049Screw · strippedEMERGENCY EXIT LIGHT SIGN IS HANGING DOWN. REMOVED AND REPLACED STRIPPED SCREW.Dec 30, 2016 · N546FF · Cndair CL6002C10 · Emergency LightingSDR VNAA2016120200005Intercostal · crackedLEFT PACK WATER INJECTION LINE CLAMP BRACKET CRACKED. REPAIRED THE INTERCOSTAL AT STRINGER 9L, BS 1144 - 1154.48 AND PERFORMED CHECKS IAW THE AMM.Dec 2, 2016 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016120200004Bulkhead Web · corrodedRIGHT BS 280 BULKHEAD WEB CORRODED. MAINTENANCE REMOVED AND REPLACED BULKHEAD WEB AND PERFORMED CHECKS IAW THE AMM.Dec 2, 2016 · N546FF · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2016113000040Floor Support · crackedCOCKPIT FLOOR SUPPORT RIGHT SIDE IS CRACKED. MAINTENANCE PERFORMED A MAJOR REPAIR IAW AMM.Nov 30, 2016 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016113000039Floor Support · crackedCOCKPIT FLOOR SUPPORT LEFT SIDE IS CRACKED. MAINTENANCE PERFORMED A MAJOR REPAIR IAW THE AMM.Nov 30, 2016 · N546FF · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016112500036Drag Angle · crackedRIGHT FORWARD VERTICAL STABILIZER DRAG ANGLE CRACKED. MAINTENANCE REPAIRED THE DRAG ANGLE AND PERFORMED CHECKS IAW THE AMM.Nov 25, 2016 · N546FF · Cndair CL6002C10 · Vertical Stabilizer
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