N980SW
Service difficulty reports · 202
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 = 'N980SW' 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 = 'N980SW' 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 SWIA2020041750162Hinge · damaged* THE PAX DOOR HINGE FUSELAGE SIDE HAS MULTIPLE LOCATIONS OF ELONGATED HOLES FOR LUGS FROM LUG 1 TO 27. (C-CHECK) RO 4/16/2020 INSTALLED THE PAX DOOR HINGE (FUSELAGE SIDE) REF. CRJ200 SRM AND BOMBARDIER REO AND BOMBARDIER DRAWING. PRESSURE CHECK IS GOOD.SDR SWIA2020041750161Door Sill · corroded* L/H SIDE FUSELAGE PRESSURE FLOOR SILL HAS AREAS OF CORROSION IN BETWEEN FS 409+128 TO 559.0. (C-CHECK) RO 4/16/2020 BLENDED 9 EA AREAS OF CORROSION ON L/H PRESSURE FLOOR SILL BETWEEN FS409+128 AND FS559 REF BOMBARDIER REO. ALL BLENDS EVALED IN LIMITS ANDSDR SWIA2020041750160Post · crackedF.S 409.0+128 BL 0 RH VERTICAL POST AFT RADIUS DEFECT NOTED. (C-CHECK) RO 4/16/2020 REMOVED CRACKED FS 409+128 BL 0.0 R/H UPPER RE-INFORCING ANGLE,REF CRJ-200 SRM. INSTALLED NEW FS409+128 BL 0.0 R/H UPPER REINFORCING ANGLE PN 601R32208-132 ,REF BOMBARDIERSDR SWIA2020041750159Vane · out of limitsRH WING INBD FLAP. L/E OUTBD FLAP VANE CAP FOUN OUT LIMITS REPLACE PART (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED WITH NEW RH INBD FLAP L/E OTBD FLAP VANE CAP REF CRJ-200-SRM AND BOMBARDIER DRAWING AND BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILSDR SWIA2020041750158Vane · out of limitsRH WING INBD FLAP. L/E CENTER FLAP VANE CAP FOUND OUT LIMITS REPLACE PART (C-CHECK) RO 4/16/2020 REMOVED AND INSTALLED RH WING INBD FLAP, NEW CENTER FLAP VANE CAP. REF BOMBARDIER DWG AMD CRJ 200 SRM.SDR SWIA2020041750157Vane · out of limitsLH WING INBD FLAP. L/E CENTER FLAP VANE CAP FOUND OF LIMITS REPALCE PART (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED LH INBD FLAP CENTER OTBD VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG.SDR SWIA2020041750156Vane · out of limitsLH WING INBD FLAP. L/E FLAP INBD VANE CAP FOUD OUT OF LIMITS REPALCE PART (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED LH WING INBD FLAP, INBD FLAP VANE CAP WITH A NEW ONE. REF BOMBARDIER DWG AND CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020041750189Fastener · corrodedRH WS178 INBOARD FLAP HINGE BOX HARDWARE IS CORRODED (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED CORRODED HARDWARE ON RH WS 178.00 TO INCLUDE 2EA BOLTS, 6EA WASHERS, 3EA BUSHINGS AND 3EA NUTS REF CRJ 200 AMM TUC 5802 CAL DUE 31 MAY 20SDR SWIA2020041750188Fastener · corrodedRH WS222.00 MID FLAP HINGE BOX HARDWARE IS CORRODED (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED CORRODED HARDWARE ON RH WS 220.00 TO INCLUDE 1EA BOLT, 5EA WASHERS, 3EA BUSHINGS AND 2EA NUTS REF CRJ 200 AMM TUC 5802 CAL DUE 31 MAY 20SDR SWIA2020041750187Fastener · corrodedRH WS264.00 OUTBOARD FLAP HINGE BOX HARDWARE IS CORRODED (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED CORRODED HARDWARE ON RH WS 264.00 TO INCLUDE 2EA BOLTS, 4EA WASHERS, 3EA BUSHINGS AND 2EA NUTS REF CRJ 200 AMM TUC 5802 CAL DUE 31 MAY 20SDR SWIA2020041750186Fastener · corrodedLH WS264.00 OUTBOARD FLAP HINGE BOX HARDWARE IS CORRODED (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED CORRODED HARDWARE ON LH WS 264.00 TO INCLUDE 2EA BOLTS, 4EA WASHERS, 3EA BUSHINGS AND 2EA NUTS REF CRJ 200 AMM TUC 5802 CAL DUE 31 MAY 20SDR SWIA2020041750185Fastener · corrodedLH WS222.00 MID FLAP HINGE BOX HARDWARE IS CORRODED (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED CORRODED HARDWARE ON LH WS 220.00 TO INCLUDE 1EA BOLT, 5EA WASHERS, 3EA BUSHINGS AND 2EA NUTS REF CRJ 200 AMM TUC 5802 CAL DUE 31 MAY 20SDR SWIA2020041750184Fastener · corrodedLH WS 178 INBOARD FLAP HINGE BOX HARDWARE IS CORRODED (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED CORRODED HARDWARE ON LH WS 178.00 TO INCLUDE 2EA BOLTS, 6EA WASHERS, 3EA BUSHINGS AND 3EA NUTS REF CRJ 200 AMM TUC 5802 CAL DUE 31 MAY 20SDR SWIA2020041750192Seat Track · corroded* THE SEAT TRACK AT LBL9.00 HAS CORROSION BETWEEN APPOX FS559.00 TO 559.00+80 IN MULTIPLE LOCATIONS. (MARKED) (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED WITH NEW SEAT TRACK AT LBL9 FS559 - FS559+80 REF CRJ200 AMM. TOOL ID: TUC8604, DUE 31-OCT-20. SEAT TRSDR SWIA2020041750191Leg Assy · cracked*PAX DOOR SUPPORT WHEEL LEG POSSIBLE CRACK OUTBD CENTER (MARKED) (C-CHECK) RO 4/16/2020 RECEIVED NEW SUPPORT WHEEL LEG PN 601R317092-1 AND INSTALLED ALL HARDWARE REF CRJ200 AMMSDR SWIA2020041750183Seat Track · corroded* THE LH SIDE SEAT TRACK FROM APPROX. FS544.00 TO FS559.00+80 HAS MULIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/16/2020 REMOVED CORRODED AND INSTALLED NEW LH SIDE SEAT-TRACK FROM FS544.00 TO FS559.00 +80 REF CRJ 200 AMM. SEE CONTINUATION CARD SDR SWIA2020041750182Seat Track · corroded* THE LH SIDE SEAT TRACK FROM APPROX. FS499.00 TO FS544.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/16/2020 NO ALLOWABLE MATERIAL LOSS PER CRJ-200 SRM . REMOVED AND INSTALLED NEW L/H SIDE SEAT TRACK FROM FS499, TO FS544. REF: CRJ200 ASDR SWIA2020041750181Seat Track · corroded* THE LH SIDE SEAT TRACK RETAINER TRIM HAS MULTIPLE LOCATIONS OF CORROSION BETWEEN APPROX. FS409.00+128 AND FS449.85. (MARKED) (C-CHECK) RO 4/16/2020 REMOVED CORRODED AND INSTALLED NEW LH SIDE SEAT-TRACK RETAINER BETWEEN APPROX. FS409.00+128 AND FS449.85.SDR SWIA2020041750180Seat Track · corroded* THE SEAT TRACK AT RBL9.00 BETWEEN APPROX. FS559.00 TO FS599.00+80 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/16/2020 ORDERED, RECEIVED AND INSTALLED NEW SEAT TRACK FS559 - FS559+80 RBL9 REF CRJ-200 AMM.SDR SWIA2020041750155Door Frame · corroded* PAX DOOR HAS LIGHT CORROSION ON MOST FWD FRAME INSIDE ACCESS PANEL AREA 832HL. (C-CHECK) RO 4/16/2020 CORROSION IS PRESENT ON 3EA ELEMENTS AND COVERS MORE THAN 30% OF THE LENGTH OF THE PART OUT OF LIMITS REF CRJ200 SRM. RPLACED FWD PASSENGER DOOR FORMER.SDR SWIA2020041750154Support Angle · cracked*RH WINDSHIELD SIDE POST SUPPORT POSSIBLE CRACK AT LWR END OUTBD (MARKED) (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED RH WINDSHIELD SIDE POST SUPPORT ANGLE AT LWR END OUTBD REF BOMBARDIER DWG AND CRJ-200 SRM. PRESSURIZATION LEAK ON THE WORK AREA WAS GOOD SDR SWIA2020041750153Support Angle · cracked*LH WINDSHIELD SIDE POST SUPPORT CRACKED AT LWR END OUTBD (MARKED) (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED LH WINDSHIELD SIDE POST SUPPORT ANGLE AT LWR END OUTBD REF BOMBARDIER DWG CRJ-200 SRM. PRESSURIZATION LEAK ON THE WORK AREA WAS GOOD NO LEAK NOTSDR SWIA2020041750152Seat Track · corroded* THE LH SIDE SEAT TRACK BETWEEN APPROX. FS449.85 AND FS499.00 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C-CHECK) RO 4/16/2020 REMOVED CORRODED AND INSTALLED NEW LH SIDE SEAT-TRACK FROM FS449.85 AND FS499.00. REF CRJ 200 AMM. SEE CONTINUATION CARD FSDR SWIA2020041750151Seat Track · corroded* THE LH SIDE SEAT TRACK HAS MULTIPLE LOCATIONS OF CORROSION FROM APPROX. FS409.00+128 TO FS449.85. (MARKED) (C-CHECK) RO 4/16/2020 REMOVED CORRODED AND INSTALLED NEW LH SIDE SEAT-TRACK FROM FS 409.00 +128 TO FS 449.00 +85 REF CRJ 200 AMM. SEE CONTINUATISDR SWIA2020041750150Floor Support · corrodedAFT FLOOR BEAM LH B27 FS 559+80 TO 621 APPROX. HAS CORROSION AROUND NUT PLATE AS MARKED (C-CHECK) RO 4/16/2020 PERFORMED PERMANENT REPAIR TO AFT FLOOR BEAM LH B27 FS 559+80 TO 621 APPROX. HAS CORROSION AROUND NUT PLATE. REF BOMBARDIER REO SEE CONTINUATIOSDR SWIA2020041750149Support Angle · crackedFS 621 FLOOR SUPPORT ANGLE RH BL 36 APPROX HAS POSSIBLE CRACK. (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED FS 621 FLOOR SUPPORT ANGLE RH BL 36 APPROX REF BOMBARDIER REO AND BOMBARDIER DWG.PRESSURIZATION LEAK WAS GOOD.SDR SWIA2020041750148Support Angle · corrodedFS 621 FLOOR SUPPORT ANGLE LH BL36 TO RH BL27 APPROX. HAS CORROSION AS MARKED (C-CHECK) RO 4/16/2020 BLENDED OUT CORROSION ON FS 621 FLOOR SUPPORT ANGLE, LBL36 TO RBL27. REF CRJ 200 SRM. ORIGINAL PART THICKNESS = .094" MATERIAL REMOVED AT FS 621.0 LBL 27SDR SWIA2020041750147Frame · cracked* INSIDE FUSELAGE CARGO COMPARTMENT FS 605.0 AT STR 9L THERE IS A CRACK AT LAST RIVET LOCATION ON FRAME FLANGE. LEFT HAD SIDE ABOVE AFT CARGO DOOR. (C-CHECK) RO 4/16/2020 REMOVED DAMAGED SECTION OF LOWER FRAME FLANGE AT FS605.0 STR 9L AND REPAIRED FRAME RESDR SWIA2020041750146Floorbeam · crackedFS 280.00 FLOORBEAM SUSPECTED CRACK ON FWD SIDE OF VERTICAL FLANGE INBOARD OF LBL 9.00. (MARKED) (C-CHECK) RO 4/16/2020 COMPLIED WITH ALL STEPS OF BOMBARDIER REO. REMOVED AND REPLACED CRACKED BEAM, ANGLES AND FLANGE AT FS280. RESTORED FINISH AND COMPLIED WSDR SWIA2020041750145Fitting · cracked* INTERNAL FUSELAGE AT FS 484 RBL 36 OUT BOARD CLIP IS CRACKED (R/H) SIDE (C-CHECK) RO 4/16/2020 REMOVED AND INSTALLED NEW CLIP AT FS 484.00 RBL 36 OUTBOARD CLIP REF REO. COMPLIED WITH TASK CARD. SEE CONTINUE CARD FOR DETAILS.SDR SWIA2020041750144Fitting · cracked* INTERNAL FUSELAGE AT FS 484 LBL 27 INBOARD L/H SIDE CLIP IS CRACKED (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED CLIP AT FS 484.00 LBL27. COMPLIED WITH REO. SEE CONTINUATION FOR DETAILS.SDR SWIA2020041750143Fitting · cracked* L/H SIDE INTERNAL FUSELAGE OUT BOARD CLIP IS CRACKED AT FS 484.0 LBL 36 (C-CHECK) RO 4/16/2020 REMOVED CRACKED CLIP AND INSTALLED NEW L/H SIDE INTERNAL FUSELAGE OUT BOARD CLIP AT FS 484.00 LBL36 REF: REO. SEE CONTINUATION CARD FOR DETAILS.SDR SWIA2020041750141Angle · corroded*PAX DOOR SURROUND LWR SILL ANGLE HAS SEVERAL AREAS OF CORROSION (MARKED) (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED WITH NEW LOWER SILL ANGLE REF CRJ200 SRM, BOMBARDIER DWG. SEE CONTINUE CARD FOR DETAILS OF INSTALLATION. OPS CHECK GOOD.SDR SWIA2020041750140Door Sill · cracked*PAX DOOR UPPER SILL IS CRACKED AT FS280.00 ATTACH POINT BETWEEN STGR 2LH -3LH (MARKED) (C-CHECK) RO 4/16/2020 REMOVED AND REPLACED PAX DOOR UPPER SILL ANGLE AT FS280.00 ATTACH POINT BETWEEN STGR 2LH -3LH REF CRJ-200 SRM AND BOMBARDIER DWG. PRESSURIZATIONSDR SWIA2020041750139Stop Fitting · chafed*FS364.00 RH STOP FITTING AT STGR 26RH ON SURROUND IS CHAFFED (MARKED) (C-CHECK) RO 4/16/2020 REMOVED CHAFED AVIONICS DOOR FWD R/H STOP FITTING AND INSTALLED NEW STOP FITTING PN# 601R38343-1 ASSY REF BOMBARDIER DWG, NO ALLOWABLE DAMAGE IS STATED IN SRM,RESDR SWIA2020041750138Striker · bent*PAX DOOR AFT UPPER SEAL STRIKER IS BENT (MARKED) (C-CHECK) RO 4/16/2020 REPAIRED PAX DOOR AFT UPPER SEAL STRIKER REFERENCE BOMBARDIER REO. PRESSURE CHECKS GOOD.SDR SWIA2020041750179Bracket · corrodedLH OUTBOARD BRACKET ASSY AT BL45 FS 345 APPROX. HAVE CORROSION AS MARKED. (C-CHECK) RO 4/16/2020 REPLACED L/H AFT CORRODED BRACKET ASSY AT BL45 FS345 WITH NEW BRACKET AND NEW HARDWARE PER CRJ-200 SRM.SDR SWIA2020041750136Seat Track · corrodedRH SEAT RAILS R BL9 FS 364 TO 409.128 APPROX HAS CORROSION AS MARKED (C-CHECK) RO 4/16/2020 BLENDED OUT CORROSION ON RH SEAT REAIL RBL9 FS 364 TO FS 409.128. REF CRJ 200 SRM. SEAT TRACK OUT OF LIMITS. REF CRJ. REMOVED AND REPLACED SEAT TRACK. REF BOMBARDISDR SWIA2020041750135Skin · corrodedRH WING UPPER PLANK OPENING FOR 640CT HAS CORROSION AROUND NUT PLATE (C-CHECK) RO 4/16/2020 BLENDED OUT CORROSION AROUND THE OPENING AT PANEL 640CT REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NEW REO. COMPLIED WITH ALL STEPS OF REO. BOND CHECK GOOSDR SWIA2020041750134Rib · crackedRH WING BATT RIB 53.60 FWD CHANNEL IS CRACKED. (C-CHECK) RO 4/16/2020 REPAIRED THE DAMAGED BATT RIB ASSY AT WS 53.60 PER REO (REPAIR NO. 3) STEPS 1 THRU 10.SDR SWIA2020041750133Skin · corrodedLH WING UPPER PLANK OPENING FOR 540CT HAS CORROSION AROUND NUT PLATE (C-CHECK) RO 4/16/2020 BLENDED OUT CORROSION AROUND THE OPENING AT PANEL 540CT REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. RECEIVED NEW REO. COMPLIED WITH ALL STEPS OF REO. BOND CHECK GOOSDR SWIA2020041750132Rib · crackedLH WING BATT RIB WS53.60 FWD CHANNEL IS CRACKED AND HAS CORROSION ON INBOARD ANGLE AROUND ELECTRICAL CONNECTORS. (C-CHECK) RO 4/16/2020 REPAIRED THE LHS BATT RIB ASSY AT WS 53.60 PER REO AND CRJ200.SDR SWIA2020041750131Skin · corroded*FS559.00 €“ FS559.00+32 STGR 26LH €“ 26RH EXTERNAL SKIN HAS SEVERAL FASTENERS WITH CORROSION AROUND THEM (MARKED) (C-CHECK) RO 4/16/2020 REPAIRED CORRODED SKIN AND FASTENERS @ FS559.00 €“ FS559.00+32 STGR 26LH €“ 26RH REF REO. LEAK CHECK GOOD AT THISSDR SWIA2020041750130Skin · chafed*CENTER WING PLANK AFT RH BOTTOM EDGE APPROXIMATELY RBL45.0 IS CHAFFED (MARKED) (C-CHECK) RO 4/16/2020 PERFORMED REPAIR CENTER WING PLANK AFT RH BOTTOM EDGE APPROXIMATELY RBL45.0 REF BOMBARDIER REO, DWG. PRESSURIZATION LEAK WAS GOOD .SDR SWIA2020041750129Skin · chafed*CENTER WING PLANK AFT LH BOTTOM EDGE APPROXIMATELY LBL45.0 IS CHAFFED (MARKED) (C-CHECK) RO 4/16/2020 PERFORMED REPAIR CENTER WING PLANK AFT LH BOTTOM EDGE APPROXIMATELY LBL45.0 REF BOMBARDIER REO, DWG. PRESSURIZATION LEAK WAS GOOD.SDR SWIA2020041750128Skin · gougedLH BOOST PUMP ACCESS HOLE HAS 4 GOUGES ON LANDING AND WING PLANK. (C-CHECK) RO 4/16/2020 BLENDED GAUGES ON L/H BOOST PUMP ACCESS HOLE, REF REO, REWORK NOT REQUIRED, RESTORED FINISH TO BLENDED AREAS.SDR SWIA2020041750178Spring · corroded*LH WING INBD FLAP HAS CORROSION ON FLAP VANE ACTUATOR SPRINGS AND ATTACHING HARDWARE LOCATED UNDER FLAP PANEL 584AB (MARKED) (C-CHECK) RO 4/16/2020 INSTALLED NEW HARDWARE AND SPRINGS ON THE LH INBOARD FLAP VANE ACTUATOR UNDER FLAP PANEL 584AB REF CRJ-200 SDR SWIA2020041750126Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODSDR SWIA2019073046100Pressure Switch · failedHYD 3 LOW PRESSURE ON CLIMB OUT. FLT 5283. REMOVED AND REPLACED THE HYD 3A LOW-PRESSURE SWITCH S9DB IAW AMM. OPS CHECK GOOD AND NO LEAKS FOUND.SDR SWIA201811045165Bracket · wornAT 12000 THE AIRCRAFT STARTED TO PRODUCE HEAVY UNUSUAL VIBRATION IN THE HULL THE AND A VERY LOUD VIBRATING NOISE. WE DECLARED EMERGENCY AND RETURNED TO FIELD. NO MASTER WARNING AND NO MASTER CAUTIONS MESSAGES AND ALL ENG VIBRATIONS WERE WITHIN NORMAL RANGE. (F
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