N652BR, cancelled Nov 3, 2023
Service difficulty reports · 155
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 = 'N652BR' AND deregistration_id = 'N652BR-2023-11-03' 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 n_number = 'N652BR' AND deregistration_id = 'N652BR-2023-11-03' 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 SWIA202266736None · failedD:GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR UP ABOVE SPEED 200KTS. GEAR RETRACTION SPEED LIMIT EXCEEDED. / C: MEL 32-30-1 / CAT A DUE WITHIN 1 FLIGHT DAY / NOTE: MX ACTION CW AND CAT II DOWNGRADED / GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR USDR SWIA2021091561081A/C Pack · failedWHILE CLIMBING THROUGH 23000 FT RIGHT PACK TURNED OFF. RAN CHECKLISTS AND DESCENDED TO 15000. DO TO THE TERRAIN AND NOT BEING ABLE TO GET LOWER THE PASSENGER MASKS DEPLOYED AND CABIN HIGH ALT OCCURRED. (FLIGHT 5488 - FILED CLOSED) THIS DISCREPANCY WAS TRSDR SWIA2021072659748Skin · damagedAIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN BETWEEN FS 265.00 - FS 280.00 BETWEEN STR 25L AND STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS265.00 - FS280.00 AND STR24L - STR25R IN REF TO REO 601R-53-11-3715, REV--, DATED 2021-07-21SDR SWIA202159747Skin · damagedAIRCRAFT SUSTAINED DAMAGE TO THE FUSELAGE SKIN AND REPAIR DOUBLER AT FS 235.00, BETWEEN STR 25L - STR 26L (FILED CLOSED) REPAIRED DAMAGE TO FUSELAGE SKIN BETWEEN FS227.74 - FS250.00 AND STR24R - STR24L IN REF TO REO 601R-53-11-3714, REV--, DATED 2021-07-SDR SWIA2021062591000Apu · shutdownAPU INFLIGHT SHUTDOWN WHILE ENROUTE. SINGLE GENERATOR. VERIFIED APU INTAKE DOOR CLOSED AND ALL MX ACTION HAS BEEN COMPLIED WITH. REACTIVATED APU PER MEL 49-10-1A TROUBLESHOT APU INFLIGHT SHUTDOWN IAW FIM 49-10-00. REMOVED AND REPLACED APU ECU IAW AMM 49-6SDR SWIA202158148Bracket · bentGEAR DISAGREE EMERGENCY MESSAGE. NOSE GEAR REMAINED DOWN. RAN QRH AND EXTENDED ALL GEAR SUCCESSFULLY AND COMPLETED RTF. (FLIGHT 5289 - FILED CLOSED) FOUND NOSE LANDING GEAR WOW SENSOR BRACKET BENT, REPLACED BRACKET AND ADJUSTED WOW SENSOR IN REFERENCE TOSDR SWIA202053019Heat Shield · crackedAPU HEAT EXHAUST SHIELD HAS A CRACK BETWEEN THE 7 O`CLOCK AND 8 O`CLOCK POSITION. FILED CLOSED RO 10/5/2020. REMOVED AND REPLACED APU HEAT EXHAUST SHIELD, IN REF TO CRJ200 AMM.SDR SWIA2020060950959Skin · dentedFUSELAGE SKIN DENT LABELED 18 BETWEEN FS654.50 & FS672.20 AND STR 1R - STR 2R REQUIRES REPAIR. (C-CHECK) RO 4/27/2020 REPAIRED FUSELAGE SKIN DENT LABELED 18 BETWEEN FS654.50 - FS672.20 AND STR 1R - STRG 2R REF REO.SDR SWIA2020060950958Bulkhead · damagedWHILE PERFORMING REPLACEMENT OF RBL 18 VERTICAL POSTS (INBOARD AND OUTBOARD) AT FS 409+128, FOUND 4 EACH HOLES ELONGATED ON BULKHEAD WEB AND 1 EACH DENT. (C-CHECK) RO 4/27/2020 REPAIR DAMGED AT RBL 18 VERTICAL POSTS (INBOARD AND OUTBOARD) AT FS 409+128 REF RESDR SWIA2020060950957Skin · dentedDENTS FOUND IN MULTIPLE LOCATIONS ON TOP SIDE OF FUSELAGE BETWEEN FS 621.00 AND FS 755.00 PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 4/27/2020 REWORKED AND REPAIRED SDR SWIA2020060950956Floor Support · wornFLOORBEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3) REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 REMOVED THE DAMAGED BEAM CAP FROM FS569 TO FS621 LBL27 (P/N 601R35031-3), REF SRM. INSTALLED NEW BEAM CAP P/N 601R35031-3 FROM FS569 TO FS621 LBL27 REF SRMSDR SWIA2020060950946Strap · wornRT STRAP FS559.0 RBL 40 AND 27 APPROX REQUIRES REPLACEMENT. (C-CHECK) RO 4/27/2020 ORDERED AND RECEIVED, DRILLED AND LOCATED NEW PART, INSTALLED NEW STRAP ON THE RT SIDE AT FS559.00 RBL 27 - 40. REF SRM, DRAWING. COMPLIED WITH TASK CARD.SDR SWIA2020060950955Post · crackedFS 409+128 LBL 18.0 OUTBD VERTICAL POST AFT RADIUS IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED 2 EA PLATES ATTACHED TO VERTICAL STIFFENER FS 409+128 LBL18 AT WL 65.90 & WL 53.42 FOM. REF SRM. REMOVED I/B STIFFENER AND O/B CRACKED STIFFENER OF OUTBOARD VERTICASDR SWIA2020060950954Stiffener · crackedFS 409+128 BL 0.0 RT VERTICAL POST UPPER STIFFENER IS CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED RT VERTICAL POST AT BL 0.0 FS 409.00+128 INSTALLED REF SRM AND DRAWING.SDR SWIA2020060950953Post · crackedFS 409+128 RBL 18.0 INBD AND OUTBD VERTICAL POST HAVE CRACKS IN AFT RADIUS. (C-CHECK) RO 4/27/2020 REMOVED AND INSTALLED NEW FS 409+128 RBL 18.0 INBD AND OUTBD VERTICAL POST. REF DWG, REO AND SRM. ALL CHECKS GOOD AT THIS TIME.SDR SWIA2020060950972Stop Fitting · chafedTHE AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING IS CHAFED. (C-CHECK) RO 4/27/2020 REPLACED AVIONICS BAY DOOR CUTOUT SURROUND FWD RT STOP FITTING REF SRM TUC4200 DUE:30-SEP-20 SEE CONTINUE CARD FOR WORK PERFORMED.SDR SWIA2020060950971Stop Fitting · chafedTHE AVIONICS BAY DOOR CUTOUT SURROUND FWD LT STOP FITTING IS CHAFFED. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT LIMITS REF SRM. REMOVED AND REPLACED NEW AVIONICS BAY DOOR CUTOUT SORROUND FWD LT STOP FITTING. REF SRM.SDR SWIA2020060950965Fitting · crackedTHE AVIONICS BAY DOOR SURROUND AFT LT GUIDE FITTING IS BROKEN/CRACKED. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED WITH NEW1 EACH AFT LT GUIDE FITTING ON AVIONICS BAY DOOR REF SRM.SDR SWIA2020060950952Frame · corrodedTHE FRAME AT FS349.00 HAS CORROSION FROM STRINGER 26R TO 26L. (C-CHECK) RO 4/27/2020 BLENDED OUT CORROSION ON LOWER FRAME SECTION AT FS349 FROM STR 26R TO 26L. REF SRM. ORIGINAL MATERIAL THICKNESS IS .063" PER SRM. MATERIAL LOSS IS .005 WITH .058" REMAININSDR SWIA2020060950974Strap · corrodedRT STRAP FS559.0 LBL 40 AND 27 APPROX HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION AND RT STRAP FS559.0 WAS FOUND TO BE OUT OF LIMITS REF SRM. REPLACED ON MX#20971547, JOB 2742971. SEE CONTINUTION CARD FOR DETAILS.SDR SWIA2020060950967Seat Track · corrodedTHE SEAT TRACK SECTION FROM APPROX FS559.00 TO FS559.00+80 AT RBL9.00 HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND REPLACED NEW PASSENGER FLOOR SEAT RAIL AY FS 559.00 TO 559.00+80 RBL 9.0 REF AMM ASDR SWIA2020060950966Seat Track · corrodedFS559.00+112 - 574.00 (APPROXIMATE) AT RBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM 53-61-49. REMOVED AND INSTALLED NEW CARGO SEAT TRACK INSTALLED ATFS 559.00+112 TO FS 574.00 AT RBL 9.0 REF AMM.SDR SWIA2020060950962Floor Skin · crackedTHE PRESSURE FLOOR SKIN BETWEEN LBL 9.00 AND BL 0 AT APPROX FS 461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.06LBS. WEIGHT OF REPAIR PARTS IS 2.42LBS. TOTAL WEIGHT ADDED = 2.36LB. PRESSURE CHECKS GOOD AT THIS TIMSDR SWIA2020060950951Panel · corrodedTHE RT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED RT PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 REF REO, SEE CONTINUATION CARD FOR DETAILS. LEAK CHECK GOOD AT THIS TISDR SWIA2020060950950Panel · corrodedTHE LT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION FROM FS409.00+128 TO FS559.00. (C-CHECK) RO 4/27/2020 REPAIRED LT PRESSURE FLOOR SILL BETWEEN FS409.00+128 TO FS559.00 REF REO, AND REO. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOSDR SWIA2020060950949Floor Skin · crackedTHE PRESSURE FLOOR SKIN BETWEEN RBL 9.00 AND BL 0 AT APPROX FS461.00 HAS 2EA CRACKS. (C-CHECK) RO 4/27/2020 REPAIRED REF REO. WEIGHT OF PARTS REMOVED IS 0.05LBS. WEIGHT OF REPAIR PARTS IS 2.42LBS. TOTAL WEIGHT ADDED = 2.37LB. PRESSURE CHECKS GOOD AT THIS TSDR SWIA2020060950947Crossbeam · corrodedTHE CROSSBEAM CAP AT FS559.00+48 BETWEEN RBL27.00 AND RBL9.00 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE FLOOR SUPPORT PLATE. REF SRM, DRAWING.SDR SWIA2020060950945Strap · corrodedLT STRAP FS559.0 LBL 35 AND 27 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED CORROSION ON LT STRAP AT FS559 BETWEEN LBL27 - LBL35 REF SRM. LT STRAP AT FS 559.00 BETWEEN LBL 27 AND LBL 35 HAS AN ORIGINAL THICKNESS OF 0.050? REF SRM 53-41-43 FIG 1. MIN REMAINISDR SWIA2020060950944Bracket · crackedLT FS 484 INBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 INBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT FS484 INBOARD PULLEY ANGLE BRACKET PART 601R-51-41-059-2 REF PREVIOUSLY INCORPERATED RE. INSTALLED LSDR SWIA2020060950943Bracket · crackedLT FS 484 OUTBRD PULLEY ANGLE BRACKET IS CRACKED UPPER CORNER. (C-CHECK) RO 4/27/2020 REMOVED AT LT FS 484 OUTBRD PULLEY ANGLE BRACKET. REF SRM. FABRICATED LT FS484 OUTBOARD PULLEY ANGLE BRACKET PART 601R-51-41-059-1 REF: PREVIOUSLY INCORPERATED REO. INSTASDR SWIA2020060950942Floor Support · corrodedRT FLOORBEAM FS 409.00+128 TO 599.0 RBL 9 HAS CORROSION. (C-CHECK) RO 4/27/2020 REMOVED THE CORROSION, ENSURED REMAINING MATERIAL THICKNESS (NDT) - FOUND OUT OF LIMITS. RECEIVED ENGINEERING SUPPORT, COMPLIED WITH REO - PART IN LIMITS. REF REO.SDR SWIA2020060950941Doubler · corrodedRT GALLEY INBRD FWD DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED FWD DOUBLER PLATE AT FS295 AND RBL 4.25 REF SRM AND DWG. SEE CONTINUATIO CARD FOR DETAILS.SDR SWIA2020060950940Doubler · corrodedRT GALLEY INBRD AFT DOUBLER PLATE HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED AFT DOUBLER PLATE AT FS324 AND RBL 4.25 REF SRM AND DWG. CONTINUATION CARD FOR DETAILS.SDR SWIA2020060950939Doubler · corrodedRT GALLEY OUTBRD DOUBLER PLATE APPROX FS 319 RBL 35 HAS CORROSION AROUND NUTPLATE HOLE. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED O/B DOUBLER PLATE AT FS319 AND RBL 35 REF SRM AND DWG. CONTINUATION CARD FOR DETAILS.SDR SWIA2020060950938Floorbeam · corrodedRT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 RBL 9. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED THE RT FLOORBEAM AT RBL 9 BETWEEN FS409.00+05 TO 409.00+121. REF REO.SDR SWIA2020060950937Floorbeam · corrodedLT FLOORBEAM HAS CORROSION FS409.00+05 TO 409.00+121 LBL 9. (C-CHECK) RO 4/27/2020 BLENDED CORROSION ON LT FLOOR BEAM AT FS409.00+05 TO FS409.00+121 REF. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO. COMPLIED WITH TASK CARD.SDR SWIA2020060950936Door Sill · corrodedSERVICE DOOR SILL HAS CORROSION RT FS 319- 349. (C-CHECK) RO 4/27/2020 FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND REPLACED NEW MID SUPPORT ANGLE P/N 601R38303-253 AT RT FS319.00 TO FS 349.00 REF SRM AND DRAWING.SDR SWIA2020060950935Seat Track · corrodedFS559.00+112 - 574.00 (APPROXIMATE) AT LBL9 SEAT TRACK CORRODED AROUND FASTENERS. (C-CHECK) RO 4/27/2020 REMOVED AND REPLACED SEAT TRACK FROM FS559+112 -FS574 LBL9 REF SRM.SDR SWIA2020060950934Seat Track · corrodedFS559.00+112 - 621.00 SEAT RAIL BEAM CAP AT LBL27 CORRODED IN NUMEROUS AREAS. (C-CHECK) RO 4/27/2020 REMOVED CORROSION FROM SEAT RAIL BEAM CAP AT LBL27 FS559.00+112 - 621.00. BLEND OUT AT FLOORBEAM FS559+112 - FS569.00, INBD LBL27 WAS FOUND TO BE WITHIN LIMISDR SWIA2020060950970Connecting Rod · chafedRT MLG LWR/OTBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF INBD END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REMOVED RT MLG DOOR STRUT. REF AMM - INSTALLED NEW RT MLG DOOR STRUT (WITH ONE EACH NEW BOLT, ONE NEW WASHER AND ONE NEW NUT ATSDR SWIA2020060950969Connecting Rod · chafedRT MLG UPPER/INBD DOOR CONNECTING ROD CHAFED ON AFT FACE OF LWR END OF ROD, AT PIVOT MEMBER CONNECTION POINT. (C-CHECK) RO 4/27/2020 REPLACED RT MLG DOOR PUSH/PULL ROD REF AMM. OPS TEST GOOD.SDR SWIA2020060950968Support · chafedCENTER VERTICAL SUPPORT POST (AFT SIDE) REAR PRESS BULKHEAD FS 621.00, BL 0.00, IS CHAFED FROM MECHANICAL CONTACT WITH 10TH STAGE BLEED AIR SOV APROX 10' FROM TOP OF POST. (C-CHECK) RO 4/27/2020 REPAIRED CENTER VERTICAL SUPPORT POST (AFT SIDE) REAR PRESS BULKSDR SWIA2020060950964Attach Fitting · crackedFOUND CRACKED ATTACHING (CLIP) AFT R/H SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14R LEVEL, AFT EQUIPMENT BAY. (C-CHECK) RO 4/27/2020 REMOVED, LOCATED, DRILLED, REPLACED AND RESTORED FINISH ON ATTACHSDR SWIA2020060950963Attach Fitting · crackedFOUND CRACKED ATTACHING (CLIP) AFT LT SIDE OF REAR PRESS BULKHEAD FS 621.00, THAT ATTACHES TO FS 625.00 BY COMMON INTERCOSTAL, AT APROX STR 14L LEVEL, AFT EQUIPMENT BAY. (C-CHECK) RO 4/27/2020 REMOVED, LOCATED, DRILLED, REPLACED AND RESTORED FINISH ON ATTACHISDR SWIA2020060950973Stringer · gougedSMALL SECTION OF STRINGER ATTACHED TO AFT PRESSURE BULKHEAD FS 621.00 THAT SPANS FROM THE AFT CARGO DOOR AFT TRACK OTBD TO FS 621.00, FOUND GOUGED/BENT FROM PROBABLE PREVIOUS MECHANICAL CONTACT WITH AFT CARGO DOOR AFT LOCK BOLT. (C-CHECK) RO 4/27/2020 REMOVEDSDR SWIA2020060950961Attach Angle · cracked(AFT) ATTACHING ANGLE (BOTTOM SIDE) AT FS 621.00 AND COMMON TO THE PRESSURE BULKHEAD, FOR ATTACHMENT OF THE CARGO DOOR CAM TRACK SUPPORT ASSY FOUND CRACKED. (C-CHECK) RO 4/27/2020 REPLACED CRACKED AFT ATTACHING ANGLE WITH NEW ONE P/N 601R35050-109 AT FS 621.0SDR SWIA2020060950933Skin · dentedRT FUSELAGE SKIN HAS DENT OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT APPROX FS 232 / BL 8 RT. (C-CHECK) RO 4/27/2020 REPAIRED THE DENT AT THE RT FUSELAGE SKIN, OUTBOARD OF NLG AFT GEAR DOOR HINGE POINT. REF REO. REFERENCE THE CONTINUE CARD FOR DETAILS.SDR SWIA2020060950932Skin · chafedLT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584FT. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E OUTBOARD SECTION WITH NEW PN 601R14303-43 PO# T-54677 REF DWG AND SRM. COMPLIED WITH CARD.SDR SWIA2020060950931Skin · chafedLT INBOARD FLAP VANE SKIN L/E IS CHAFED OUTBOARD OF PANEL 584ET. (C-CHECK) RO 4/27/2020 REPLACED LT INBOARD FLAP VANE SKIN L/E CENTER SECTION WITH NEW PN 601R14303-51 PO# 7426-00010 REF DWG AND SRM. COMPLIED WITH CARD.SDR SWIA2020060950930Skin · chafedRT INBOARD FLAP VANE SKIN IS CHAFED OUTBOARD OF PANEL 684FT. (C-CHECK) RO 4/27/2020 REPLACED RT INBOARD FLAP VANE SKIN OUTBOARD OF PANEL 684FT PN 601R14303-44S REF DWG SRM, SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD.
Back to N652BR, cancelled Nov 3, 2023