N983SW
Service difficulty reports · 200
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 = 'N983SW' 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.
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 = 'N983SW' AND registry_match = 'registration' 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 SWIA2020042350234Intercostal · crackedFS621-FS625 INTERCOSTAL AL STGR 13L, FLANGE NEXT TO SKIN IS CRACKED (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED FS621.00-FS625.00 INTERCOSTAL AT STGR 13L. REF BOMBARDIER DWG, BOMBARDIER REO, & CRJ200SRM. COMPLIED WITH TASK CARDSDR SWIA2020042350233Angle · crackedCRACKED ANGLE ATTACHED TO BATT RIB LOCATED ON THE RH SIDE WHEEL WELL AT WS 53.60. (C-CHECK) RO 4/21/2020 REPAIRED THE RHS BATT RIB ASSY AND NOTED CRACKED ANGLE, AT WS 53.60 REF BOMBARDIER REO, COMPLIED WITH SKY CARD FOR COMPLETE DETAILS OF WORK PERFORMED SDR SWIA2020042350232Stringer · cracked* STGR 3L CRACKED AT FS 379.00. (C-CHECK) RO 4/21/2020 COMPLETE STRINGER SPLICE REPAIR ON CRACKED STGR 3L AT FS379.00 REF CRJ 200 SRM, BOMBARDIER DWG. PRESSURE LEAK CHECKS CHECKED GOOD. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020042350231Stringer Clip · cracked* STGR 3L AT FS 282.00 HAS CRACKED ATTACHMENT ANGLE. (C-CHECK) RO 4/21/2020 REMOVED CLIP ON STR 3 LH FS 280.00 REF CRJ 200 SRM. REMOVED STR 3 LH FS 282.00 ATTACHMENT ANGLE REF CRJ 200 SRM. - INSTALLED NEW STR 3 LH FS 282.00 ATTACHMENT ANGLE REF CRJ 20SDR SWIA2020042350230Rib · crackedWS 53.60 BATT. RIB IS CRACXKED AT UPPER RADIUS IN LH WHEEL WELL. (RIB LOCATED AT AFT SPAR OF WING BOX) (C-CHECK) RO 4/21/2020 REPAIRED WS 53.6 BATT. RIB PER BOMBARDIER REO.SDR SWIA2020042350229Frame · cracked* THE FRAME AT FS333.00 BETWEEN STRINGER 0 AND 1 IS CRACKED. (MARKED) (C-CHECK) RO 4/21/2020 REPLACED FRAME FS333.00 BETWEEN STRINGER 0 AND 1 , REF. CRJ200 SRM, AND DRWG. COMPLIED WITH (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**), LEAK CHECK GOOD, NO LSDR SWIA2020042350228Angle · corroded* THE SERVICE DOOR SURROUND LOWER SILL ANGLE FROM FS319.00 TO FS349.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM SERVICE DOOR LOWER SILL ANGLEFROM FS319.00 TO FS349.00 REF CRJ 200 SRM. EVALUATED AND FOUND SDR SWIA202042350262Door Sill · corroded* THE LH FLOOR SILL BETWEEN FS295.00 AND FS310.00 HAS CORROSION. (MARKED) (C-CHECK) RO 4/21/2020 BLENDED CORROSION AT 2EA. LOCATIONS ON THE LH FLOOR SILL BETWEEN FS295.00 AND FS310.00 REF BOMBARDIER REO. EVALUATED AND FOUND THE BLEND LOCATION #1 AT FS303,SDR SWIA2020042350259Seat Track · corroded*RH FLOOR SEAT TRACK RBL9 AT FS559.00 €“ FS559.00+112, GOUGED AND CORRODED IN SEVERAL AREAS (MARKED) (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM SEAT TRACK RBL9.00 FROM FS559.00+80 TO APPROX. FS559.00+112. REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. FSDR SWIA2020042350258Seat Track · corroded*THE SEAT TRACK AT RBL9.00 FROM FS409.00 TO 409.00+112 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/21/2020 BLENDED OUT CORROSION ON RBL 9 TRACK FS 409 TO FS 409+112 REF CRJ 200 SRM AND FOUND OUT OF LIMITS REF CRJ 200 SRM, AND INSTALLED NEWSDR SWIA2020042350253Intercostal · cracked* INTERCOSTAL ABOVE PRESSURE FLOOR AT FS 484.00 BETWEEN RBL 27 AND RBL 36 HAS CRACKED ATTACHMENT CLIP AT INB END. (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED INTERCOSTAL ABOVE PRESSURE FLOOR AT FS 484.00 BETWEEN RBL 27 AND RBL 36 ATTACHMENT CLIP PN #601R3SDR SWIA2020042350252Bracket · cracked*FS461.00 RH SIDE ABOVE WING UNDER PANEL 162EL, PANEL BRACKET POSSIBLE CRACK (MARKED) (C-CHECK) RO 4/21/2020 REMOVED CRACKED PANEL 162EL BRACKET AT FS461.00 RH SIDE AND INSTALLED NEW FABRICATED BRACKET REF CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020042350251Bracket · cracked*FS461.00 LH SIDE ABOVE WING UNDER PANEL 161EL, PANEL BRACKET POSSIBLE CRACK (MARKED) (C-CHECK) RO 4/21/2020 INSTALLED NEW ANGLE BRACKET FS461.00 LH SIDE UNDER PANEL 161EL REF CRJ200 SRMSDR SWIA2020042350250Bracket · cracked*FS449.85 LH SIDE ABOVE WING UNDER PANEL 161EL, PANEL BRACKET POSSIBLE CRACK (MARKED) (C-CHECK) RO 4/21/2020 INSTALLED NEW ANGLE BRACKET AT LH SIDE ABOVE WING UNDER PANEL 161EL REF CRJ200 SRM.SDR SWIA2020042350227Doubler · chafed* FS 280.00 BUKHEAD AFT SIDE ABOVE FLOOR PREVIOUS REPAIR DOUBLER AT R/H SIDE OF BULKHEAD HAS TWO CHAFES AND DAMAGED RIVETS, (C-CHECK) RO 4/21/2020 REMOVED DAMAGE TO FS280 BULKHEAD AFT SIDE ABOVE FLOOR PREVIOUS REPAIR DOUBLER REF CRJ 200 SRM. EVALUATED AND SDR SWIA2020042350226Intercostal · cracked*FS 625 INTERCOSTAL AT STR 14L NEXT TO SKIN CRACKED (C-CHECK) RO 4/21/2020 REMOVED AND INSTALLED NEW INTERCOSTAL AT FS625.00 STGR14L. REF C RJ200 SRM AND DWG. COMPLIED WITH TASK CARD. SEE CONTINUATION FOR DETAILS.SDR SWIA2020042350225Post · defectiveF.S 409.0+128 RBL 18 OUTB AFT RADIUS OF VERTICAL POST DEFECT NOTED. (C-CHECK) RO 4/21/2020 REMOVED THE VERTICAL POST AT FS 409.00+128 RBL18 PER REF: CRJ200 SRM. - INSTALLED NEW VERTICAL POST AT FS 409-.00+128 RBL18 PER REF: BOMBARDIER DWG IN CONJUNCTION WSDR SWIA2020042350224Strap · chafed* FS 280.00 - FS 282.00 INTERNAL CIRCUMFERENTIAL JOINT STRAP CHAFED AND/OR PREVIOUSLY BLENDED AND EXPOSED OBD OF STGR 25R. (C-CHECK) RO 4/21/2020 BLENDED OUT FS 280.00 - FS 282.00 INTERNAL CIRCUMFERENTIAL JOINT STRAP CHAFE DAMAGE AND EVALUATED PER BOMBARDISDR SWIA2020042350223Frame · corroded* FS 333.00 FRAME CORRODED FWD SIDE BETWEEN STGR 22R AND STGR 23R. (C-CHECK) RO 4/21/2020 INSTALLED NEW FRAME AT FS 333.00 STGR 23R TO FLOOR SILL, REF. CRJ200 SRM, BOMBARDIER DWG, AND BOMBARDIER DWG. COMPLIED WITH STRUCTURAL MAJOR REPAIR (**RII**), PRESSUSDR SWIA2020042350222Door Sill · cracked*CARGO DOOR LOWER SILL HAS CORROSION AROUND NUTPLATE HOLES (C-CHECK) RO 4/21/2020 REMOVED CORROSION AT CARGO DOOR LOWER SILL AROUND NUTPLATES REF CRJ200 SRM. FOUND SILL TO BE CRACKED. REMOVED CRACKED CARGO DOOR SILL AND INSTALLED NEW SILL REF DWG, AND REO.SDR SWIA2020042350221Seat Track · corroded*SEAT TRACK AT FS 559+112-621 LBL 27 CORRODED (C-CHECK) RO 4/21/2020 REMOVED AND INSTALLED NEW SERVICEABLE SEAT TRACK AT LBL9.00 FROM FS559.00+112 TO FS621.00. REF: CRJ200 AMM TOOL TUC8607 CALDUE: 31-JAN-21SDR SWIA2020042350220Seat Track · corroded*SEAT TRACK FS 559+112-621 LBL 9 CORRODED (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM SEAT TRACK FS 559+112-621 LBL 9. REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. REF: CRJ-200 SRM AND BOMBARDIER STANDARDS MANUAL. FABRICATED SEAT TRAC REF BOMBARDIER REO.SDR SWIA2020042350219Seat Track · corroded*SEAT TRACK FS 559+112-621 RBL 9 CORRODED (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM SEAT TRACK FS 559+112-621 RBL 9. REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. REF: CRJ-200 SRM AND BOMBARDIER STANDARDS MANUAL. FABRICATED SEAT TRACK REF BOMBARDIER REOSDR SWIA2020042350218Floor Support · corroded*FLOOR BEAM CAP FS 570- 610 LBL 27 CORRODED AROUND NUTPLATE HOLES (C-CHECK) RO 4/21/2020 REMOVED CORROSION ON FLOOR BEAM CAP FS570 - FS610 LBL27 REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM AND BOMBARDIER STANDARDS MANUAL. REMOSDR SWIA2020042350217Door Sill · corroded*FLOOR EDGE MEMBER FROM FS 559+80 - 621 RH HAS CORROSION AROUND NUTPLATE HOLES (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM FLOOR EDGE MEMBER FROM FS559+80 TO FS621.00 RH. REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. REF: REO. REPLACED FLOOR SILL SECTIONSDR SWIA2020042350216Attach Fitting · cracked* INTERCOSTAL ABOVE PRESSURE FLOOR AT FS 484.00 BETWEEN LBL 27 AND LBL 36 HAS CRACKED ATTACHMENT CLIP AT OBD END. (C-CHECK) RO 4/21/2020 REMOVED CRACKED ATTACHMENT CLIP AT OTBD END OF INTERCOSTAL ABOVE PRESSURE FLOOR FS484.00 BETWEEN LBL 27 AND LBL 36. FABSDR SWIA2020042350215Attach Fitting · cracked* INTERCOSTAL ABOVE PRESSURE FLOOR AT FS 484.00 BETWEEN RBL 27 AND RBL 36 HAS CRACKED ATTACHMENT CLIP AT OBD END. (C-CHECK) RO 4/21/2020 REMOVED CRACKED ATTACHMENT CLIP AT OTBD END OF INTERCOSTAL ABOVE PRESSURE FLOOR FS484.00 BETWEEN RBL 27 AND RBL 36. FABSDR SWIA2020042350214Door Sill · corroded*FS559.00 RH STRAP FROM RBL27 TO FLOOR SILL IS CORRODED IN SEVERAL AREAS (MARKED) (C-CHECK) RO 4/21/2020 REMOVED CORROSION. ORIGINAL THICKNESS OF RH FLOOR STRAP RBL 27 AT FS 559 IS .050". REMAINING MATERIAL IS .036". REMOVED .014" WITH MAX ALLOWABLE 10%. SDR SWIA2020042350213Door Sill · corroded*FS559.00 LH STRAP FROM LBL27 TO FLOOR SILL IS CORRODED IN SEVERAL AREAS (MARKED) (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM FS559.00 LH STRAP FROM LBL27 TO FLOOR SILL REF CRJ200 SRM. ORIGINAL THICKNESS OF LH FLOOR STRAP AT LBL27 AND FS 559 IS .050" SDR SWIA2020042350212Attach Fitting · corroded* THE FLOOR BEAM ATTACHMENT TO THE REAR PRESSURE BULKHEAD AT LBL27.00 HAS CORROSION. (MARKED) (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM FLOOR BEAM ATTACHMENT TO REAR PRESSURE BULKHEAD REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS. COMPLETEDSDR SWIA2020042350211Seat Track · cracked* THE SEAT TRACK AT LBL9.00 FROM FS409.00 TO APPROX. FS409.00+112 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/21/2020 AFTER FURTHER EVALUATION, FOUND MULTIPLE CRACKS ON SEAT TRACK AT LBL9 FROM FS409.00 TO FS409.00+112, REMOVED CRACKED SEASDR SWIA2020042350210Seat Track · corroded* THE SEAT TRACK AT RBL9.00 HAS CORROSION FROM FS364.00 TO APPROX. FS394.00. (MARKED) (C-CHECK) RO 4/21/2020 COMPLIED W/STEP 1, 2, 3, 4, 5, 6 AND 8 (FABRICATED SEAT TRACK USING N126-2075, PO# TX8728) OF BOMBARDIER REO. INSTALLED NEW SERVICEABLE SEAT TRACSDR SWIA2020042350209Seat Track · corroded* THE SEAT TRACK AT LBL9.00 FROM FS364.00 TO APPROX FS394.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/21/2020 REMOVED CORROSION FROM SEAT TRACK FS 364.00 TP APPROX FS394.00 LBL 9. REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. REF: CRJ-2SDR SWIA2020042350208Support · cracked* THE LH WINDSHIELD SIDE POST SUPPORT IS CRACKED. (MARKED) (C-CHECK) RO 4/21/2020 ACCESSED AND REMOVED LH WINDSHIELD SIDE POST SUPPORT REF CRJ 200 SRM. - INSTALLED LH WINDSHIELD SIDE POST SUPPORT REF CRJ 200 SRM AND DRAWING. RESTORED ACCESS OPERATIONALSDR SWIA2020042350207Panel · corroded* THE RH FLOOR SILL PANEL HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 409+128 AND FS 559. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK) RO 4/21/2020 BLENDED AND NDT ALL LOCATIONS FOR THICKNESS AND CRACKS, EVALUATED AND REPAIRED RH FLOOR SILL PANEL BETWEEN FS4SDR SWIA2020042350257Spring · corroded*RH WING INBD FLAP #1 FLAP VANE ACTUATOR (MOST INBD) HAS A CORRODED SPRING AND ATTACHING HARDWARE (C-CHECK) RO 4/21/2020 REMOVED AND REPLACED WITH NEW I/B FLAP VANE ACTUATOR SPRING AND ATTACHING HARDWARE. REF. BOMBARDIER CMM. OPS CHECK GOOD AT THIS TIME. SSDR SWIA2020042350249Bracket · cracked*OTBD BRACKET TO MOUNT R/H WING CENTER LEADING EDGE INBD END IS CRACKED. BRACKET LOCATION IS AT APPROX WS149. (C-CHECK) RO 4/21/2020 REMOVED CRACKED BRACKET FOR RH LEADING EDGE APPRX WS 149 REF CRJ 200 SRM AND LOCATED AND DRILLED NEW BRACKET 600-12045-12 RSDR SWIA2020042350203Skin · dented*DENT ON RH INBD FLAP LOWER SKIN AT APPROX. WS 138.00, 8€? FWD OF TRAILING EDGE (C-CHECK) RO 4/21/2020 REPAIRED RH INBD FLAP LOWER SKIN AT APPROX. WS 138.00, 8€? FWD OF TRAILING EDGE. REF: CRJ200 SRM. COMPLIED WITH TASK CARD.SDR SWIA2020042350202Skin · chafed*RIGHT HAND AILERON UPPER LEADING EDGE IS CHAFED AT THE INBD, CTR, AND OTBD AREAS. (C-CHECK) RO 4/21/2020 BLENDED OUT DAMAGE ON RH AILERON UPPER LEADING EDGE. REF: CRJ-200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED RH AILERON UPPER LEADINSDR SWIA2020042350256Hinge Fitting · corroded*RIGHT OUTBOARD FLAP HINGE LUG FITTINGS HAVE CORRODED HARDWARE (692BB AND 697BB). (C-CHECK) RO 4/21/2020 REMOVED CORRODED AND INSTALLED 2 EA. NEW RH OB FLAP HINGE NUTS USING TORQUE WRECH TUC4198, CAL. DUE 5/31/21, REF. CRJ200 AMM.SDR SWIA2020042350201Skin · dented*LEFT INBOARD FLAP LOWER SKIN INBD IS DENTED. FLAGGED (C-CHECK) RO 4/21/2020 APPLIED DOUBLER REPAIR ON LH INBD FLAP LOWER SKIN. REF: CRJ200 SRM, REPAIR NO.3 AND CRJ200 SRM SEE CONTINUE CARD FOR FURTHER DETAILS. COMPLIED WITH TASK CARDSDR SWIA2020042350200Vane · chafed*LH INBD FLAP VANE UPPERSIDE CENTER HAS X2 AREA'S OF CHAFING. FLAGGED (C-CHECK) RO 4/21/2020 BLENDED OUT CHAFING DAMAGE IN 2EA LOCATIONS ON LH INBD FLAP VANE UPPER TRAILING EDGE REF: CRJ200 SRM. COMPLIED WITH REO. SEE CONTINUATION FOR DETAILS.SDR SWIA2020042350199Vane · chafed*LH WING INBD FLAP VANE, THERE ARE X3 AREA'S OF CHAFE ALONG LEADING EDGE. ( FROM BUMPER STOPS ) FLAGGED (C-CHECK) RO 4/21/2020 REMOVED DAMAGE AND EVALUATED REPAIRS. L/H INBOARD FLAP VANE LEANING EDGE INBOARD CAP, CENTER CAP, AND OUTBOARD CAPS ALL FOUND TSDR SWIA2020042350260Bracket · chafed*PAX DOOR AFT FRAME HAS A ROLLER BRACKET THATS CHAFED. FLAGGED (C-CHECK) RO 4/21/2020 REMOVED CHAFED PAX DOOR AFT FRAME ROLLER BRACKET AND INSTALLED NEW ROLLER BRACKET P/N 600-31471-9. RE-INSTALLED ROLLER ON NEW BRACKET. RE-INSTALLED BRACKET BY RE-INSTALLSDR SWIA2020042350198Pan · corroded*EXTERNAL LOWER SIDE OF SERVICE DOOR IS CORRODED. FLAGGED (C-CHECK) RO 4/21/2020 - REMOVED EXFOLIATED CORROSION FROM SERVICE DOOR PAN AT BOTTOM AFT OF SERVICE DOOR REF CRJ200 SRM. ORIGINAL THICKNESS OF SERVICE DOOR LOWER AFT PAN IS .063" REF CRJ 200 SRM, SDR SWIA2020042350197Skin Panel · dented*X2 DENTS ABOVE RH NLG DOOR CUT-OUT. (C-CHECK) RO 4/21/2020 EVALUATED 2EA. DENTS ABOVE RH NLG DOOR CUT OUT, NO REPAIR ALLOWED REF CRJ 200 SRM. REMOVED DENTED RH NLG SURROUND SKIN PANEL AND INSTALLED NEW SKIN PANEL, REF BOMBARDIER DWG AND CRJ 200 SRM. SEE SDR SWIA2020042350196Skin · dented*FWD PAX DOOR CUT-OUT THE OUTER SKIN IS DENTED APPROX 1/4 OF AN INCH. (C-CHECK) RO 4/21/2020 EVALUATED AND FOUND DENT OUT OF LIMITS DUE TO IN A NO DAMAGE ALLOWED AREA REF CRJ200 SRM. TRIMMED AWAY DAMAGE, FUSELAGE SKIN/STRUCTURE, NEAR LOWER FORWARD CORNER OSDR SWIA2020042350243Hinge Fitting · failedCOMPLY WITH SCHEDULED MAINTENANCE CODE: BACKLASH - ELEVATOR CONTROL SYSTEM FC - COMPLY WITH TASK CARD FUNCTIONAL CHECK OF EACH ELEVATOR PCU FOR BACKLASH AND DEFLECTION UNDER LOAD (MRB), PART NUMBER: - , SERIAL NUMBER: 7961, POSITION: (C-CHECK) RO 4/21/202SDR SWIA2020042350195Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL. (J)(2) MODIFYING THE RPB AND DSDR SWIA2019111246760Transducer · faultyON DEPARTURE FOS LOW SPEED CUE WAS STUCK ON THE GREEN LINE. FLIGHT # 5066 CLOSED REMOVED AND REPLACED RH AOA TRANSDUCER IAW AMM. PERFORMED AOA OPS CHECK IAW AMM. OPS CHECK GOOD AT THIS TIME. PERFORMED FUNCTIONAL TEST OF STALL PROTECTION COMPUTER (GREEN ACC
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