N501BG

Service difficulty reports · 209

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 = 'N501BG' 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 VNAA2026040315701Coffeemaker · odorBURNING SMELL COMING FROM GALLEY / PERFORMED SEVERAL OPS CHECKS/BREW CYCLES OF BOTH COFFEE POTS IAW CRJ 700 AMM 25-32-06-710-801 AND WHILE BREWING, NOTICED ABNORMAL SMELL COMING FROM BOTH COFFEE POTS AND SUSPECT BOTH COFFEE MAKERS TO BE FAULTY. REMOVED AND REPApr 1, 2026 · N501BG · Cndair CL6002C10 · Buffet/GalleysSDR VNAA2025120111102Unknown · odorBURNING SMELL IN COCKPIT AFTER LANDING / C/W FDE SMOKE AND/OR ABNORMAL SMELL IN CABIN IAW FIM 21-22-00-810-806 NO DEFECTS OR SMELL NOTED AT THIS TIMENov 27, 2025 · N501BG · Cndair CL6002C10 · Air Distribution SystemSDR VNAA20251015093Intercostal · corrodedSTRINGER 20R INTERCOSTAL BETWEEN F.S. 319.70 AND F.S. 349.00 IS CORRODED AT MULTIPLE LOCATIONS. REMOVED AND REPLACED INTERCOSTAL BETWEEN IAW CRJ700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, AND 51-42-21-001-001-A01.Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20251015092Angle · corrodedWING TO FUSELAGE SUPPORT ANGLES AT RH SIDE AT FS939 PN SH670-39265-4 AND SH670-39265-6 HAS EXCESSIVE CORROSION REMOVED CORRODED ANGLES. LOCATED AND INSTALLED NEW ANGLES IAW REO 670-53-82-679 REV.--.Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Wing Attach FittingsSDR VNAA20251015091Fitting · damagedOTBD BUSHING OF THE OTBD LUG OF THE L/H FITTING FOUND TO BE DAMAGED UPON REMOVAL REPAIRED THE OUTBD LUG OF THE L/H MLG SIDE STAY FITTING IAW MHIRJ REO 670-57-11-321 REV. --, DWG CC670-10608Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Landing Gear Attach FittingsSDR VNAA20251015089Insert · damagedFOUND HOLES FOR UPPER AND LOWER IB RH THRUST REVERSER NYLON INSERTS ELONGATED. PERFORMED REPAIR OF THE R/H THRUST REVERSER HINGE BEAM - P/N: CN624-0103-001, S/N: SB/0034 BY COMPLYING WITH MHIRJ REO 670-54-22-109 REV-- DATED 4-01-2025. VERIFIED CUSTOMER IS MAOct 17, 2025 · N501BG · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA20251015088Seat Track · corrodedRIGHT SIDE SEAT RAIL [FS847.00] TO [FS863.00] AND REQUIRES REPLACMENT. UPON FURTHER EVALUATION SIDE SEAT RAIL (FS847.00 TO FS863.00) WAS FOUND TO BE CORRODED OUT OF LIMITS AND REQUIRES REPLACEMENT. : FABRICATED NEW SEAT TRACK (FS847.00 TO FS 863.00) FROM EXTRUOct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251015087Seat Track · corrodedRIGHT SIDE SEAT RAIL [FS573.00] TO [FS661.00] IS CORRODED REQUIRES REPLACMENT. REMOVED CORRODED SEAT RAIL. INSTALLED A NEW SEAT RAIL IAW CRJ AMM 53-00-49-001-801-A01.Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251015084Seat Track · corrodedSEAT TRACK RBL 9.00, FS836.55 TO FS850.45 REQUIRES REPLACEMENT DUE TO CORROSION. REMOVED AND REPLACED SEAT TRACK I.A.W. CRJ700 SRM 53-00-49-201-002-A01, 51-40-11-001-001-A01 AND 53-00-49-400-801-A01. PAINTED SEAT TRACK P/N (SH670-33425-3), IAW PSA T.O. NUMBEOct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251015083Seat Track · corrodedSEAT TRACK LBL 9.00 [FS693.00] TO [FS847.00] REQUIRES REPLACMENT. REPLACED SEAT TRACK LBL 9, FS 693 TO 847 (P/N SH670-35864-951) IAW CRJ 700 AMM 53-00-49-400-801-A01.Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251015082Seat Track · corrodedCORROSION FOUND TO BE OUT OF LIMITS ON LBL 9.00 [FS581.00] TO [FS677.00] REUIRES REPLACMENT. REPLACED SEAT TRACK LBL 9,00 FS581.00 TO FS677.00 (P/N SH670-33425-3) IAW CRJ 700 AMM 53-00-49-400-801-A01Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251015081Seat Track · corrodedSEAT TRACK AT RBL 9.00 [FS693.00] TO [FS847.00] FOUND TO BE OUT OF LIMITS DUE TO CORROSION EXTENDING ENTIRE LENGTH OF SEAT TRACK ON MULTIPLE ELEMENTS IAW CRJ700 SRM 53-41-49-101-001-A01. LOCATED AND DRILLED SEAT TRACK RBL9 [FS 693- FS 847] P/N (SH670-33425-3) Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20251015080Bracket · corrodedPAX DOOR BRACKET AT FORWARD INTERCOSTAL DD5 IS CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED AND REPLACED BRACKET I.A.W. CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. 601R31902-461Oct 17, 2025 · N501BG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20251015079Beam · chafedLEFT IB FLAP MOVABLE VANE BEAMS (ALL 4) HAVE SIGNS OF WEAR/CHAFING FROM ROLLER CONTACT. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ REO 670-57-52-257 REV -A DATED 2024-08-20. REPAIR HAS SDIR IMPLICATIONS THAT NEED CAPTURED-VERIFIED REQUIREMENTS ARE BEING Oct 17, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20251015078Intercostal · dentedPAX DOOR INTERCOSTAL FOWARD DD5 WAS FOUND TO BE DENTED AND BULGED. REMOVED AND REPLACED INTERCOSTAL I.A.W. MHIRJ REO 670-52-11-1459 REV.-.Oct 17, 2025 · N501BG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA20251015077Intercostal · corrodedFOUND PAX DOOR DD1 AFT INTERCOSTAL TO BE CRACKED. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01.Oct 17, 2025 · N501BG · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNA2025F00039Floor Support · corrodedDISCREPANCY: LBL 27 FLOOR BEAM IS CORRODED FROM FS 1000 TO FS 1015. CORRECTIVE ACTION: REPAIRED FLOOR BEAM IAW CRJ-700 SRM 53-00-41-201-001-A01. MM670-35302-005Oct 17, 2025 · N501BG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20251015076Cleat · corrodedAV SUPPORT CLEAT ON STR21R AT FS333.00 IS SEVERELY CORRODED. REMOVED AND REPLACED SUPPORT CLEAT IAW CRJ-700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.Oct 17, 2025 · N501BG · Cndair CL6002C10 · Navigation SystemSDR VNAA20251015075Stringer · corrodedDISCREPANCY: AV SUPPORT CLEAT ON STR21R AT FS333.00 IS SEVERELY CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED SUPPORT CLEAT IAW CRJ-700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01. SH670-32695-7Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20251015074Stringer · corrodedSTRINGER 21R SPLICE AT FS333.00 IS SEVERELY CORRODED. REMOVED AND REPLACED STRINGER SPLICE IAW CRJ-700 SRM'S 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20251015073Frame · damagedBS 295 FRAME REQUIRES SPLICE REPAIR TO REMOVE AND REPLACE STGR 18R AND 19R. PERFORMED A CUT AND SPLICE REPAIR TO THE FS 295 FRAME IAW MHIRJ REO 670-53-21-2553 REV-.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20251015072Stringer · corrodedSTRINGER 18 R IS CORRODED BETWEEN F.S. 280 TO F.S. 295. FOUND TO BE OUT OF LIMITS DUE TO CORROSION ON MULTIPLE ELEMENTS. REMOVED STGR 18 R BETWEEN F.S. 280 TO F.S. 295 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED, DRILLED, AND DEBURROct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20251015071Door · chafedFWD CARGO DOOR IS CHAFFED ON INNER DOOR SKIN AT/ABOVE IB DOOR STOP, FWD AND AFT. REMOVED DAMAGE AND COMPLIED WITH MHIRJ REO 670-52-35-528 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA20251015070Slat Track · damagedRIGHT SLAT TRACK 3-1 HAS WEAR DAMAGE IN MULTIPLE AREAS. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-57-42-1956 REV. -- DISPOSITION FOR BLENDED WEAR DAMAGE TO SLAT TRACK 3-1, RHS. REFERENCE HR00504995 AND HN00253015 FOR ASSOCIATED WORK PERFORMED.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015069Fairing · damagedFOUND ENLONGATED HOLE UNDER LH SIDE WING TO FUSELAGE FAIRING AT FS FS893. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-53-51-335 REV --.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA20251015068Slat Track · chafedRIGHT SLAT TRACK 3-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1961 REV-.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015067Slat Track · chafedRIGHT SLAT TRACK 3-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 3-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1961 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20251015066Slat Track · chafedRIGHT SLAT TRACK 2-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 2-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1954 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015065Slat Track · chafedRIGHT SLAT TRACK 2-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 2-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1951 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015064Slat Track · chafedRIGHT SLAT TRACK 2-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 2-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1939 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015063Slat Track · chafedRIGHT SLAT TRACK 1-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 1-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1940 REV-- DATED 2025-01-29. CC670-12030-1Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015062Slat Track · chafedRIGHT SLAT TRACK 1-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 1-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1935 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015061Slat Track · chafedRIGHT SLAT TRACK 1-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF RH SLAT TRACK 1-1 BY COMPLYING WITH MHIRJ REO 670-57-42-2008 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015060Skin · chafedDISCREPANCY:R/H AILERON LOWER SKIN CHAFED WS 348.00 TO WS 353.00 CORRECTIVE ACTION: SERVICEABLE PART P/N CC670-13054-2 DRILLED UP AND INSTALLED IAW CRJ 700 SRM TASK 51-42-06-001-001-A01, AND SRM TASK 51-42-21-001-001-A01 CC670-13054-2Oct 16, 2025 · N501BG · Cndair CL6002C10 · AileronsSDR VNAA20251015059Vane · gougedRIGHT OUTBOARD FLAP VANE LEADING EDGE HAS AN APPROXIMATELY 4" LONG GOUGE FROM CONTACT WITH BUCKTAIL ON TRAILING EDGE OF WING AT WS 231.23. COMPLIED WITH REO 670-57-53-395 REV --.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20251015058Slat Track · chafedLEFT SLAT TRACK 3-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 3-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1964 REV--.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015057Slat Track · chafedLH SLAT TRACK 2-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 2-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1953 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015056Slat Track · chafedLEFT SLAT TRACK 2-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 2-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1953 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015055Slat Track · chafedLEFT SLAT TRACK 2-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 2-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1943 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015054Slat Track · chafedLEFT SLAT TRACK 2-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 2-1 BY COMPLYING WITH MHIRJ REO 670-57-42-1941 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015053Slat Track · chafedLEFT SLAT TRACK 1-3 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LT SLAT TRACK 1-3 BY COMPLYING WITH MHIRJ REO 670-57-42-1938 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20251015052Slat Track · chafedLEFT SLAT TRACK 1-2 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 1-2 BY COMPLYING WITH MHIRJ REO 670-57-42-1936 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015051Slat Track · chafedDISCREPANCY: LH SLAT TRACK 1-1 HAS MULTIPLE CHAFES ALONG THE LENGTH OF THE TRACK. PERFORMED MAJOR REPAIR OF LH SLAT TRACK 1-1 BY COMPLYING WITH MHIRJ REO 670-57-42-2009 REV -.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20251015050Drag Angle · crackedVERTICAL STAB RH DRAG ANGLE IS CRACKED (PREVIOUSLY REPAIRED AREA) CORRECTIVE ACTION: REPAIRED RH DRAG ANGLE IAW MHIRJ REO 670-55-31-188 REV -- DATED: 2025-03-04 AND BOMBARDIER REO 670-55-31-018 REV -A DATED: 2016-11-10.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR VNAA20251015049Attach Angle · corrodedDISCREPANCY: INTERCOSTAL ATTACH ANGLES AT F.S 517-533 STR 26L ARE CORRODED AND HAVE OVERSIZE HOLES CORRECTIVE ACTION: INSTALLED NEW PN: SH670-33399-951 AND PN: SH670-33600-983 BETWEEN FS 517 - FS 533, STR 27 - STR 26L (LBL 2.6) IAW CRJ-700 SRM 51-42-06-001-001Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA20251015048Fitting · corrodedFITTING P/N SH670-33389-1 @ F.S 533 STR 25L IS CORRODED. INSTALLED NEW FITTING P/N SH670-33389-1 IAW CRJ 700 SRM 51-42-21-001-001-A01 & CRJ 700 SRM 51-45-00-001-001-A01 SH670-33389-1Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20251015047Frame · corrodedINTERCOSTAL FOR ACCESS TO FRAME CORROSION @ STR 25L F.S 517-F.S533 FOUND IT HAS INCOMING OVERSIZE RIVET HOLES. INSTALLED NEW INTERCOSTAL PN SH670-33568-5 IAW CRJ 700 SRM 51-42-06-001-001-A01 & CRJ 700 SRM 51-42-21-001-001-A01.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA20251015046Angle · corrodedFS280 J ANGLE IS CORRODED. NEW SERVICEABLE ANGLE DRILLED UP AND INSTALLED IAW CRJ 700 SRM TASK 51-42-21-001-001-A01, AND SRM TASK 51-42-06-001-001-A01.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20251015045Window Frame · chafedPILOT AND COPILOT'S WINDOW UPPER SILL IS GOUGED ABOVE THE LH AND RH WINDSHIELD SIDE POST. REPAIRED UPPER SILL IAW MHIRJ REO 670-53-11-2088 REV-.Oct 16, 2025 · N501BG · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20251015044Beam · chafedRH IB FLAP MOVABLE VANE BEAMS (ALL 4) HAVE SIGNS OF WEAR/CHAFING FROM ROLLER CONTACT. PERFORMED MAJOR REPAIR BY COMPLYING WITH MHIRJ REO 670-57-52-257 REV -A DATED 2024-08-20. REPAIR HAS SDIR IMPLICATIONS THAT NEED CAPTURED-VERIFIED REQUIREMENTS ARE BEING TROct 16, 2025 · N501BG · Cndair CL6002C10 · Trailing Edge Flaps
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