Bombardier CL-600-2C10
Service difficulty reports · 46,658
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'CL6002C10' 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.
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 aircraft_model_key = 'CL6002C10' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA202610230048Flex Hose · wornCHAFING BTW FIRE EXTINGUISHER DISCHARGE LINE (DISCONNECTED FLEX HOSE) AND AGB HOUSING AT LH ENGINE. CHAFING BTW FIRE EXTINGUISHER DISCHARGE LINE (DISCONNECTED FLEX HOSE) AND AGB HOUSING AT LH ENGINE WAS REPAIRED PER EA NO: 7264-2026-1055, REV -- , SECTION IISDR VNAA202610230047Skin · wornWEAR ON INBOARD EDGE OF SLAT 1 SS 57.16 AT RH WING. WEAR ON INBOARD EDGE OF SLAT 1 SS 57.16 AT RH WING WAS REPAIRED PER REO 670-57-42-2560 REV -.SDR VNAA202610230046Skin · wornWEAR ON SLAT LOWER SKIN (WEDGE) BTW SS 57.16 TO SS 337.66 AT RH WING. WEAR ON SLAT LOWER SKIN (WEDGE) BTW SS 57.16 TO SS 337.66 AT RH WING WAS REPAIRED PER PER REO 670-57-42-2574 REV-.SDR VNAA202610230045Skin · damagedTEMPORARY REPAIR FOR MULTIPLE LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN PANELS BETWEE FS409.00 - FS985.00 AND STR4R - STR9R THE REPORTED CONDITION IS STRUCTURALLY ACCEPTABLE FOR A MAXIMUM OF 1450 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS MULTIPLE LIGHSDR VNAA202610230044Skin · damagedTEMPORARY DISPOSITION FOR LIGHTNING STRIKE DAMAGE TO UPPER FUSELAGE SKIN PANEL AT FS830.40 AND STR7R THE SUBJECT CONDITION IS ACCEPTABLE FOR A MAXIMUM OF 1500 FLIGHT HOURS FROM THE INCORPORATION OF THIS REO. LIGHTNING STRIKE DAMAGE TO UPPER FUSELAGE SKIN PANESDR VNAA202610230043Skin · damagedLIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS AT FS855.40 AND AT STR7R. DAMAGE TO FUSELAGE SKINS AT FS855.40 AND AT STR7R WAS REPAIRED PER REO 670-53-00-836 REV -.SDR VNAA202610230042Skin · damagedLIGHTNING STRIKE DAMAGE - FUSELAGE SKIN PANEL FS169-FS193 PERM REPAIR WITHIN 8000 FH. REPLACE PANEL OR SUBMIT RFTS. LIGHTNING STRIKE DAMAGE - FUSELAGE SKIN PANEL FS169-FS193 WERE REPAIRED PER REO: 670-53-11-2369. REV: - -."SDR VNAA202610230041Skin · damagedLIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FS 661+16 AND BTW STGR 8RH TO STGR 9RH AT FUSELAGE. LIGHTNING STRIKE ON EXTERNAL FUSELAGE SKIN FS 661+16 AND BTW STGR 8RH TO STGR 9RH AT FUSELAGE WAS REPAIRED PER CRJ 900 SRM 53-00-00-201-003-A03.SDR VNAA202610230040Angle · gougedGOUGE ON FWD INTERCOSTAL ANGLE STGR15 RH FS 319.70.00 AT INTERNAL SURROUND STRUCTURE OF GALLEY SERVICE DOOR. GOUGE ON FWD INTERCOSTAL ANGLE STGR15 RH FS 319.70.00 AT INTERNAL SURROUND STRUCTURE OF GALLEY SERVICE DOOR WAS REPAIRED PER REO: 670-53-21-2962 REV-SDR VNAA202610230039Stiffener · bentBENT ON STABILIZER STIFFENER BTW FS 295.00 TO FS 333.00 RBL 27.0 AT CAB8N PAX FLOOR STRUCTURE. STABILIZER STIFFENER BTW FS 295.00 TO FS 333.00 RBL 27.0 AT CAB8N PAX FLOOR STRUCTURE WAS REPLACED PER SRM 51-42-10-001-001-A01.SDR VNAA202610230038Stop Pad · brokenBROKEN STOP PAD OF AFT LOWER FITTING AT LH EMERGENCY EXIT DOOR EXTERNAL SURROUND STRUCTURE. STOP PAD OF AFT LOWER FITTING AT LH EMERGENCY EXIT DOOR EXTERNAL SURROUND STRUCTURE. WAS REPLACED PER CRJ-700 AMM 53-41-23-000-801 (CONFIG A01) AND CRJ-700 AMM 53-41-SDR VNAA202610230037Skin · dentedTEMPORARY DISPOSITION FOR MULTIPLE DENTS TO MULTIPLE FUSELAGE SKINS DUE TO HAIL BETWEEN FS169.00 - FS235.00 THIS TEMPORARY DISPOSITION IS VALID FOR MAXIMUM 5200 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO. WITHIN 5200 FLIGHT HOURS REPAIR OR REPLACESDR VNAA202610230036Door · dentedDENT ON LH ENGINE LOWER FAN-COWL DOOR. DENT ON LH ENGINE LOWER FAN-COWL DOOR WAS REPAIRED PER REO 670-54-14-1012 REV B AND REO 670-54-14-1355, REV-.SDR VNAA202610230035Skin · dentedDENT ON LOWER EXTERNAL FUSELAGE AT APPROXIMATELY FS 270.00 BETWEEN STGR 24R - 25R. DENT ON LOWER EXTERNAL FUSELAGE AT APPROXIMATELY BS 270 BTWN STR 24R AND STR 25R WAS REPAIRED IAW REO 670-51-00-085 REV -B AND REO 670-53-11-2376. REV-.SDR VNAA202610230034Fan Cowl · dentedDENT IN THE LOWER FAN COWL, ENGINE 1. REPAIRED PER REO 670-54-14-1012. REV B.SDR VNAA202610230033Skin · dentedDENT TO ADG SKIN PANEL BELOW THE ADG DOOR BETWEEN FS177.00 AND FS185. DENT TO ADG SKIN PANEL BELOW THE ADG DOOR BETWEEN FS177.00 AND FS185.00 WAS REPAIRED PER REO 670-53-11-2365 REV -- "SDR VNAA202610230032Exhaust Duct · damagedAFTER THE REMOVAL OF THE SEAL ON AFT EXHAUST APU ,ENLOGATED RIVET HOLES (4EA) WERE FOUND BTW THE 6 O'CLOCK AND 12 O' CLOCK POSITION APROXIMATELLY AND AN ADITIONAL RIVET HOLE WAS FOUND AT THE 9 O' CLOCK POSITION APROXIMATELLY. ENLOGATED RIVET HOLES (4EA) WERE SDR VNAA202610230031Skin Panel · damagedGOUGES AT LEADING EDGE SKIN PANEL (SS337.66 TO SS446.86), LH WING. GOUGES AT LEADING EDGE SKIN PANEL (SS337.66 TO SS446.86), LH WING WERE REPAIRED PER EA NO. 5741-2026-1071. REV A AND EA 5741-2026-1096 REV A.SDR VNAA202610230030Winglet · damagedPERM REPAIR BEFORE 34,331.08 FH - WEDGE, WINGLET T/E (LH) WITHIN 7,220.45 FLIGHT HOURS (34,331.08 FH), REPAIR OR REPLACE OF THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. WINGLET T/E (LH TIP FAIRING) WAS REPAIRED PER REO 670-57-30-082 REV -"SDR VNAA202610230029Rivet · damagedDAMAGED ALIGNMENT RIVETS AT CAPT & FO'S SEAT TRACKS. SEAT TRACKS WAS REPAIRED PER REO: 670-53-11-210, REV D.SDR VNAA202610230028Floorbeam · cracked"CRACK ON FLOORBEAM BS 280 AND RBL 12 AT FLOOR STRUCTURE. CRACK ON FLOORBEAM FSTA 280 AND RBL 12 AT FLOOR STRUCTURE WAS REPAIRED PER SRM 53-11-43-201-003-A01.SDR VNAA202610230027Floorbeam · crackedCRACK ON FLOORBEAM BS 280, LBL 12.0 AT FLOOR STRUCTURE. CRACK ON FLOORBEAM BS 280, LBL 12.0 AT FLOOR STRUCTURE WAS REPAIRED IAW SRM 53-11-43-201-003-A01.SDR VNAA202610230026Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUSDR VNAA202610230025Web · crackedCRACK ON WEB BTWN BS 195 - 205, WL 79.50. ON LEFT INTERNAL STRUCTURE IN THE FWD EQUIPMENT BAY. THE WEB BTWN BS 195 TO BS 205, WL 79.50 WAS REPAIRED IAW REO 670-53-11-509, REV E.SDR VNAA202610230024Fitting · crackedCRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE. CRACK ON UPPER CASCADE ANGLE FITTING ON INNER BORDER AT 3 O'CLOCK, LT ENGINE WAS REPAIRED PER REO: 670-54-22-181 REV- A.SDR VNAA202610230023Hinge · corrodedIN REF TRFKE00AXBML: AFTER REMOVAL OF BUSHING AND BEARING, CORROSION AND WEAR IN THE INNER AREA OF THE LUGS OF FITTING INBD, L1, L2, L3 , L4 , L5 & L6 ON CENTER FITTING AND FITTING OUTBD ( UPPER / LOWER)AT LH AILERON LUGS L5 & L6 WERE CLEANED PER CRJ -700 SRM SDR VNAA202610230022Seat Track · corrodedCORROSION AT SEAT TRACK OF LBL 9 BTWN BS 677 TO BS 977 AT PAX CABIN. SEAT TRACK OF LBL 9 BTWN BS 677 TO 977 AT PAX CABIN WERE REPLACED IAW AMM 53-00-49.SDR VNAA202610230021Seat Track · corrodedCORROSION AT SEAT TRACK OF RBL 9 BTWN BS 677 TO 977 AT PAX CABIN. SEAT TRACK OF RBL 9 BETWEEN FS 677.00 TO FS 977.00 AT PAX CABIN WERE REPLACED PER AMM 53-00-49.SDR VNAA202610230020Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY1 WAS REPLACED IAW CMM 25-33-44, REV 3.SDR VNAA202610230019Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-44 REV 3.SDR VNAA202610230018Skin · corrodedCORROSION ON STR 26R, BTW BS 969 - 985 AT INTERNAL FUSELAGE SKIN. CORROSION ON STR 26R BTWN BS 969 - 985 AT INTERNAL FUSELAGE SKIN WAS REMOVED AND EVALUATED WHITIN LIMITS IAW REO 670-53-61-2762, REV -.SDR VNAA202610230017Skin · corrodedCORROSION ON BOTH FACES OF FRAME FS=909 BTW SGTR 25L TO SGTR 25R AT INTERNAL FUSELAGE SKIN. FRAME FS=909 BTW SGTR 25L TO SGTR 25R AT INTERNAL FUSELAGE SKIN WAS REPAIRED PER REO 670-53-51-407 REV -, AND REO: 670-53-31-1251 REV-.SDR VNAA202610230016Skin · corroded"CORROSION ON SGTR 26R BTW FS=847 TO FS=863 AT INTERNAL FUSELAGE SKIN. SGTR 26R BTW FS=847 TO FS=863 AT INTERNAL FUSELAGE SKIN WAS REPAIRED PER EA 5351-2026-1079 REV -.SDR VNAA202610230015Bracket · corroded"CORROSION ON BRACKET MACHINED 5EA BTW FS517.00-FS597.00, STGR 22L-24R AT FWD BAGGAGE COMPARTMENT. BRACKET MACHINED 5EA BTW FS517.00-FS597.00, STGR 22L-24R AT FWD BAGGAGE COMPARTMENT WERE BLENDED OUT AND FOUND WITHIN LIMITS PER REO NO: 5332-2026-1041. REV .--SDR VNAA202610230014Strap · corrodedCORROSION ON SETTLEMENT AREA OF HORIZONTAL STABILIZER TIP LH. LOWER STRAP WAS REPLACED ON SETTLEMENT AREA OF HORIZONTAL STABILIZER TIP FAIRING LH PER CRJ-700 SRM 51-42-10-001-001-A01"SDR VNAA202610230013Support · corrodedCORROSION INSIDE HOLE (8EAS) ON GALLEY SUPPORT FS 285.00 RBL17.0, FS 296.00 RBL 4.0, FS 310.00 RBL 4.0, FS 288.00 LBL 20, FS 310.00 LBL 20, FS 333.00 LBL 38.0, FS 333.00LBL 32.0 AND FS 349.00 LBL 17.0 AT CABIN PAX FLOOR STRUCTURE. CORROSION INSIDE HOLE (8EAS)SDR VNAA202610230012Seat Track · corrodedCORROSION ON SEAT RAILS ALONG PASSENGER CABIN 8 (E/AS) RH SIDE (BTW FS364 TO FS977 STGR 15R). SEAT RAILS ALONG PASSENGER CABIN 8 (E/AS) RH SIDE (BTW FS364 TO FS977 STGR 15R) WERE REPLACED PER CRJ-700 AMM 53-00-49"SDR VNAA202610230011Seat Track · corrodedCORROSION ON SEAT TRACK ALONG PASSENGER CABIN 7EA LH SIDE (BTW FS364 TO FS977 STGR 15L). SEAT TRACK ALONG PASSENGER CABIN 7EA LH SIDE (BTW FS364 TO FS977 STGR 15L) WERE REPLACED PER AMM 53-00-49.SDR VNAA202610230010Seat Track · corrodedCORROSION AT SEAT TRACK OF LBL9 BETWEEN FS 373.00 TO FS 677.00 AT PAX CABIN. CORROSION AT SEAT TRACK OF LBL9 BETWEEN FS 373.00 TO FS 677.00 AT PAX CABIN WERE REMOVED PER SRM 51-21-06-001-001-A01, WAS EVALUATED, DUE TO EXCESSIVE CORROSION DAMAGE PER CRJ 700 SDR VNAA202610230009Seat Track · corrodedCORROSION AT SEAT RAIL OF RBL9 BETWEEN FS 349.00 TO FS 677.00 AT PAX CABIN. CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS 349.00 TO FS 677.00 AT PAX CABIN WERE REMOVED IAW SRM 51-21-06-001-001-A01, WAS EVALUATED, DUE TO EXCESSIVE CORROSION DAMAGE AT SEAT TRACK OSDR VNAA202610230008Seat Track · corrodedCORROSION AT SEAT RAIL OF LBL27 BETWEEN FS 364.00 TO FS 485.00, FS 485 TO FS 581.00 AT PAX CABIN. CORROSION ON SEAT RAIL OF LBL27 BETWEEN FS 364.00 TO FS 485.00, FS 485 TO FS 581.00 AT PAX CABIN WERE REMOVED PER SRM 51-21-06-001-001-A01, WAS EVALUATED, DUE TOSDR VNA2026F00012Retainer · corrodedCORROSION RETAINER SEAL ON DOOR E/E COMPARTMENT (AVIONICS). RETAINERS SEAL (4EA) ON DOOR E/E COMPARTMENT (AVIONICS) WERE REPLACE PER SRM 51-42-06-001-001-A01.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.SDR 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.SDR 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 LIMITSSDR 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 53-82-55-101-0SDR 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 NLGSDR 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 SDR SWIA2026102277793Cartridge · warning messageIN IAD, DURING FLIGHT, NOTICED L AUTO XFLOW STAY ON FOR LONGER THAN NORMAL. FUEL IMBALANCE CONTINUED TO DEVELOP WITH THE LEFT SIDE LOW AND XFLOW RUNNING, TOTAL FUEL WAS NOT BELOW EXPECTED. DECLARED AN EMERGENCY AND LANDED WITH 600LB IMBALANCE. NO MESSAGES POSDR SWIA2026102277792A/C Pack · smokeWHITE SMOKE FILLED COCKPIT DURING CLIMB, WENT AWAY AND CLEARED ABOUT 5 MINUTES LATER ON FINAL, THE SMOKE REAPPEARED & CLEARED AGAIN AND ONE LAST TIME DURING TAXI IN, ON ARRIVAL TO GATE LT AUTO PACK FAIL CAUTION MESSAGE. APPEARED FLIGHT 4941. OPEN.
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