N917SW
Service difficulty reports · 309
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 = 'N917SW' 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 = 'N917SW' 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 SWIA20250103007Mount · crackedCARGO DOOR AFT BALANCE SPRING MOUNT BRACKET, CRACK EMANATING FROM MOUNT HOLE TO EDGE OF BRACKET. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET WITH REFERENCE TO SRM 51-42-22 AND WITH REFERENCE TO REO 601R-53-61-8262 REV SDR SWIA20250103115Mount · crackedCARGO DOOR FWD BALANCE SPRING MOUNT BRACKET, CRACKED AROUND MOUNT HOLE. (FILED OPEN) REMOVED AND REPLACED CARGO DOOR FWD BALANCE SPRING MOUNT BRACKET WITH REFERENCE TO SRM 51-42-06 AND SRM 53-61-15. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITSDR SWIA2025010601112Support · corroded2 SPOTS OF CORROSION FOUND ON THE LH SILL BETWEEN FS559.00 AND 559.00+16 (MARKED WITH TAPE) (FILED CLOSED) BLENDED CORROSION ON THE LH FLOOR SILL APPROX BETWEEN FS559.00 AND FS 559.00+16 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MSDR SWIA20250103112Floor Support · corroded2 SPOTS OF CORROSION FOUND ON THE LH SILL BETWEEN FS559.00 AND 559.00+16 (MARKED WITH TAPE) (FILED OPEN) BLENDED CORROSION ON THE LH FLOOR SILL APPROX BETWEEN FS559.00 AND FS 559.00+16 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASDR SWIA2025010601110Track · gougedAFT UPPER TRACK ON CARGO BAY DOOR GOUGED (FILED CLOSED) REMOVED AND REPLACED AFT CARGO DOOR TRACK WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.SDR SWIA20250103110Track · gougedAFT UPPER TRACK ON CARGO BAY DOOR GOUGED (FILED OPEN) REMOVED AND REPLACED AFT CARGO DOOR TRACK WITH REFERENCE TO SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.SDR SWIA202501061106Door Frame · crackedCARGO DOOR SURROUND, FORWARD LOWER CHANNEL CRACKED. FS574.00 (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR SURROUND FORWARD TRACK LOWER AFT CHANNEL AT FS 574.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 53-61-23. COMPLIED WITH TASK CARD 51-900-1003-SKY. SDR SWIA20250103106Channel · crackedCARGO DOOR SURROUND, FORWARD LOWER CHANNEL CRACKED. FS574.00 (FILED OPEN) REMOVED AND REPLACED CARGO DOOR SURROUND FORWARD TRACK LOWER AFT CHANNEL AT FS 574.00 WITH REFERENCE TO SRM 51-42-06 AND SRM 53-61-23. COMPLIED WITH TASK CARD 51-900-1003-SKY. COSDR SWIA2025010600801Skin · dentedCOMPLY WITH REPAIR AUTHORIZATION: RA90819-REO601R-53-11-3928 MXCODEID74488-PR - CW REO 601R-53-11-3928 TEMPORARY DISPOSITION TO FUSELAGE SKIN DENT BTWN FS220.00 - FS235.00 AND BTWN STRINGER 12L AND PILOT SIDE WINDOW LOWER SILL. PERMANENT REPAIR IS DUE WITH IN SDR SWIA202501030002Skin · dentedCOMPLY WITH REPAIR AUTHORIZATION: RA90819-REO601R-53-11-3928 MXCODEID74488-PR - CW REO 601R-53-11-3928 TEMPORARY DISPOSITION TO FUSELAGE SKIN DENT BTWN FS220.00 - FS235.00 AND BTWN STRINGER 12L AND PILOT SIDE WINDOW LOWER SILL. PERMANENT REPAIR IS DUE WITH IN SDR SWIA2023121900008Unknown · failedGEAR DISAGREE MASTER WARNING ON LANDING . MAP ACCOMPLISHED. QRH ACCOMPLISHED. BACK TO LAND . NORMAL LANDING. (FLIGHT 5762 - FILED CLOSED)THIS IS CURRENTLY A WORK IN PROGRESSSDR SWIA202266222None · damagedTRANSFER FROM EAML 963626 : WHILE PERFORMING BIRDSTRIKE INSPECTION, FOUND DAMAGE ON RH WINGLET LEADING EDGE BETWEEN FASTENERS #11-15 (SEE SRM 57-31-51 FIGURE 101 VIEW G FOR REF). DAMAGE EXTENDS APPROX. 8.5 INCHES IN LENGTH AND APPROX. 2 INCHES DEEP THROUGH WINSDR SWIA202158813Oil System · overtempDURING CLIMB OUT LEFT ENGINE OIL REACHED 178 IN THE RED. FOLLOWED QRH PROCEDURE AND COULD NOT GET OIL TEMPERATURE TO REDUCE BELOW 173 AND STAYED IN RED. PERFORMED IN FLIGHT ENGINE SHUT DOWN PROCEDURE AND RETURNED TO TUCSON. (FLIGHT 5583)SDR SWIA2021062258862Frame · twistedLH & RH FRAME SECTORS AT FS513.00 SHOWED TWISTING IN LATERAL SECTION AT APPROXIMATELY LBL33 & RBL33 WHILE ZERO LOAD FIXTURES WERE IN PLACE. (C-CHECK - RO 6/19/21) / REPAIRED FRAME SECTOR STN. 513.00 BETWEEN BL27.00 AND BL45.00 LOWER FLANGE RHS AND LHS PER SDR SWIA2021062258888Stiffener · crackedPAX DOOR FWD WEB STIFFENER PN# 601R317742-1 IS CRACKED (C-CHECK - RO 6/19/21) / PAX DOOR FWD WEB STIFFENER PN#601R317742-1 REMOVED AND REPLACED WITH NEW PN#601R317742-1 PO:T000055751/1 REF. CRJ200 SRM 51-42-06.SDR SWIA202158861Track · gouged*CARGO DOOR AFT TRACK IS WORN AND GOUGED AT 2EA LOCATION. (C-CHECK - RO 6/19/21) / REMOVED CARGO DOOR AFT TRACK FROM 621 BULKHEAD REF CRJ 200 SRM 51-42-06 AND REF CRJ 200 SRM 51-42-21 / . INSTALLED NEW CARGO DOOR AFT TACK REF CRJ 200 SRM 51-42-06 AND SRMSDR SWIA2021062258886Angle · crackedPAX DOOR LOWER STEP BOTTOM ANGLE IS CRACKED (C-CHECK - RO 6/19/21) / REMOVED DAMAGED PAX DOOR LOWER STEP BOTTOM ANGLE AND REPLACED. INSTALLED NEW ANGLE PN#601R317726-3 REF. CRJ200 SRM 51-42-10SDR SWIA202158885Plate · crackedPAX DOOR BOTTOM STEP MOUNTING PLATE AFT MOUNT BRACKET AT APPROX FS 340 IS CRACKED (C-CHECK - RO 6/19/21) / REMOVED PAX DOOR BOTTOM STEP MOUNTING PLATE AFT MOUNT BRACKET AT APPROX. FS340 REF. CRJ200 SRM 51-41-02. INSTALLED NEW STAIR SUPPORT MOUNT BRACKET PNSDR SWIA202158860Intercostal · corrodedCORROSION ON PAX DOOR INTERCOSTAL DD-3 (C-CHECK - RO 6/19/21) / DETERMINED CORROSION EXFOLIATED MATERIAL BEYOND 50% OF MATERIAL THICKNESS. FOUND TO BE OUT OF LIMITS REF. CRJ200 SRM 52-00-00. REMOVED INTERCOSTAL DD-3 REF. CRJ200 SRM 51-42-06, AND CRJ200 SRSDR SWIA202158859Intercostal · corrodedCORROSION ON PAX DOOR INTERCOSTAL DD-1 (C-CHECK - RO 6/19/21) / DETERMINED CORROSION EXFOLIATED MATERIAL BEYOND 50% OF MATERIAL THICKNESS. FOUND TO BE OUT OF LIMITS REF. CRJ200 SRM 52-00-00. REMOVED INTERCOSTAL DD-1 REF. CRJ200 SRM 51-42-06, AND CRJ200 SSDR SWIA202158858Frame · cracked*FRAME AT FS333 HAS SUSPECTED CRACK AT TOOLING HOLE BETWEEN STGR 0 AND STGR 1L. (C-CHECK - RO 6/19/21) / REMOVED AND INSTALLED NEW FRAME AT FS 333 BETWEEN STGR 0 AND STGR 3L REF CRJ200 SRM 51-42-06. INSTALLED NEW FRAME AT FS 333 BETWEEN STGR 0 AND STGR 3L,SDR SWIA202158857Frame · cracked*CRACK AT L/H FRAME AT FS235 BELOW WL110 (MARKED) (C-CHECK - RO 6/19/21) / REPAIRED FRAME FS235 WL110 BY COMPLYING WITH REO 601R-53-11-3687 REV-- DATED 2021-05-10. COMPLIED WITH 51-900-1003-SKY. REFERENCE THE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. SDR SWIA202158856Rib · crackedLH MLG BATT RIB WS 53.60, INBD CLIP P/N 601R10203-25 HAS CRACK. (C-CHECK - RO 6/19/21) / REMOVED AND REPLACED CLIP WITH NEW. REF. CRJ200 SRM 51-42-21 AND DWG 601R10203 REV. -G. COMPLIED WITH 51-900-1003-SKYSDR SWIA2021062258884Roller · chafed*PAX DOOR UPPER RH ROLER ON FUSELAGE SIDE CHAFFED (C-CHECK - RO 6/19/21) / REMOVED AND REPLACED PAX DOOR UPPER R/H (AFT) GIUDE ROLLER FITTING REF. CRJ 200 SRM 51-41-02.SDR SWIA2021062258855Intercostal · crackedRH INTERCOSTAL BETWEEN 621 AND 625 FRAMES APPROX STRG 14R IS CRACKED. (C-CHECK - RO 6/19/21) / REMOVED CRACKED INTERCOSTAL/CLIP AT STRINGER 14R AND FS 621-625 AND INSTALLED A NEW INTERCOSTAL/CLIP REF CRJ 200 SRM 51-42-06 AND DRAWING 601-35012 REVD, COMPLISDR SWIA202158854Bracket · cracked*BRACKET/CLIP CRACKED AT PILOT'S SIDE WINDSHIELD SIDE POST (MARKED) (C-CHECK - RO 6/19/21) / REMOVED PILOTS SIDE WINDSHIELD SIDE POST CLIP PER REFERENCE CRJ 200 SRM 51-42-21. INSTALLED A NEW PILOTS SIDE WINDSHIELD FITTING. REF CRJ 200 SRM 51-42-21 AND DRASDR SWIA2021062258853Window Frame · cracked*L/H FRAME 210 CRACKED UNDER PILOT'S SIDE WINDOW SILL (MARKED) (C-CHECK - RO 6/19/21) / REMOVED AND REPLACED WITH NEW 210 FRAME ANGLE REF CRJ200 SRM 51-42-06, DWG 601R34032 REV V . COMPLIED WITH 51-900-1003-SKY. PRESSURE CHECK GOOD.SDR SWIA202158883Pin · corroded*PASSENGER DOOR €“ SPRING RETAINING PINS ON THE LATCH CAM ARE CORRODED. (FLAGGED) (C-CHECK - RO 6/19/21) / REMOVED AND REPLACED CORRODED HARDWARE FOR THE PASSENGER DOOR €“ SPRING RETAINING PINS ON THE LATCH CAM (OPEN LOCK MECHANISM). REF: CRJ-200 AMM 20SDR SWIA2021062258882Handle · corroded*PASSENGER DOOR €“ OUTER HANDLE DETENT MECHANISM HAS CORRODED MOUNTING HARDWARE. (FLAGGED) (C-CHECK - RO 6/19/21) / REMOVED AND REPLACED PASSENGER DOOR €“ OUTER HANDLE DETENT MECHANISM CORRODED MOUNTING HARDWARE. REF: CRJ-200 AMM 52-11-03-000-804 AND CRJSDR SWIA2021062258878Skin · corroded*PASSENGER DOOR €“ CORROSION ON THE INNER SKIN AROUND THE FORWARD AND AFT ACCESS PANEL CUTOUTS. (MARKED) (C-CHECK - RO 6/19/21) / REMOVED AND REPLACED PAX DOOR INNER SKIN ASSEMBY PER REFERENCE DRAWING# 601R31702 REV N, AND CRJ 200 SRM 51-40-11, CRJ 200 SSDR SWIA2021062258877Fastener · corroded* SERVICE DOOR HAS MULTIPLE CORRODED FASTENERS ON UPPER SIDE OF DOOR( MARKED). (C-CHECK - RO 6/19/21) / NEW FASTENERS INSTALLED ON INNER UPPER SIDE OF SERVICE DOOR AS REQUIRED (MARKED LOCATIONS) REF CRJ 200 SRM 51-42-21SDR SWIA202158876Bolt · corroded* SERVICE DOOR UPPER MOUNT HINGE LOWER OB MOUNT BOLT CORRODED. (C-CHECK - RO 6/19/21) / REMOVED CORRODED HARDWARE AND INSTALLED NEW HARDWARE ( 1 EA. BOLT, NUT AND 2 EA. WASHERS) ON SERVICE UPPER HINGE SUPPORT FITTING. REF. CRJ200 SRM 51-41-02SDR SWIA2021062258875Receiver · corroded* SERVICE DOOR SURROUND AFT LOWER CAM ROLLER RECIEVER HAS CORRODED HARDWARE (MARKED). (C-CHECK - RO 6/19/21) / REMOVED CORRODED HARDWARE AND INSTALLED NEW HARDWARE ( 2 EA. BOLTS, NUTS AND 4 EA. WASHERS) ON SERVICE DOOR AFT LOWER ROLLER FITTING. REF. CRJ200SDR SWIA2021506228852Door Sill · corroded* SERVICE DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS BETWEEN APOX. FS 319.7 AND FS 349.00 (MARKED). (C-CHECK - RO 6/19/21) / REPLACED SERVICE DOOR LOWER SILL AND UPPER ANGLE REF CRJ200 SRM 51-42-10 AND CRJ200 SRM 51-42-21 AND DWG 601R38303 REV. AL. LEAK CHSDR SWIA2021062258874Seat Track · corroded*LBL 9 PAX SEAT TRACK FROM APPROX FS 409 +126 TO FS 559 +4 HAS THREE AREAS OF CORROSION AT APPROX FS 444, FS 474 AND FS 559 +4. (C-CHECK - RO 6/19/21) / BLENDED *LBL 9 PAX SEAT TRACK FROM APPROX FS 409 +126 TO FS 559 +4 REF CRJ 200 SRM 51-21-06. FOUND TO BSDR SWIA2021062258873Seat Track · corroded*LBL 9 PAX SEAT TRACK HAS EVIDENCE OF CORROSION AT APPROX FS 409 +54. (C-CHECK - RO 6/19/21) / BLENDED *LBL 9 PAX SEAT TRACK FROM APPROX FS 409 +54 REF CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-21-49. REMOVED AND INSTALLED AND FABSDR SWIA2021062258872Mount · corroded*CARGO DOOR AFT TRACK SPRING BALANCE MOUNT PLATE CRACKED AT SPRING BALANCE ATTACHMENT NUTPLATE. (C-CHECK - RO 6/19/21) / REMOVED BALANCE SPRING ASSY. TO FOM REF CRJ200 AMM 52-31-08-000-801.INSTALLED NEW BALANCE SPRING PART # B1780-5L REF CRJ200 AMM 52-31-0SDR SWIA2021062258871Cargo Track · cracked*CARGO DOOR FWD TRACK SPRING BALANCE MOUNT PLATE CRACKED AT SPRING BALANCE ATTACHMENT NUTPLATE. (C-CHECK - RO 6/19/21) / REMOVED AND INSTALLED NEW CARGO DOOR FWD TRACK BALANCE SPRING PLATE REF CRJ200 SRM 51-42-06. / REMOVED AND INSTALLED NEW CARGO DOOR FWDSDR SWIA202158870Floor Support · cracked*LH PRESSURE FLOOR SILL ANGLE HAS AREAS OF CORROSION AS MARKED FROM APPROX FS 420 TO FS 513. (C-CHECK - RO 6/19/21) / COMPLIED WITH REO 601R-53-41-666, REV -C, DATED 2012-11-06 AND REO 601R-53-41-2917 REV-- DATED 2021-05-04 TO REPAIR LH PRESSURE FLOOR SILSDR SWIA2021062258869Seat Track · corroded*LBL 9 PAX SEAT TRACK FROM APPROX FS 409+ 126 TO FS 559+ 4 HAS THREE AREAS OF CORROSION AT APPROX FS 344, FS 374 AND FS 559+ 4. (C-CHECK - RO 6/19/21) / LOCATION OF CORROSION INCORRECTLY IDENTIFIED. CAMP ENTERED IN ERROR. SEE CAMP #22613350 JOB 27641101 OPSDR SWIA2021062258868Seat Track · corroded*RBL 9 PAX SEAT TRACK FROM APPROX FS 409+126 TO FS 559+ 4 HAS EXFOLIATION CORROSION ALONG THE ENTIRE LENGTH. (C-CHECK - RO 6/19/21) / REMOVED AND REPLACED RBL 9 PAX SEAT TRACK FROM APPROX FS 409+126 TO FS 559+ 4 . REF: CRJ-200 AMM 53-01-11-000-802 AND CRJ-SDR SWIA2021062258867Seat Track · constricted*L/H SIDE SEAT RAIL HAS MULTIPLE SPOTS OF CORROSION ,SCRATCHES AND GOUGES FROM FS364.00-FS409.00+112 (C-CHECK - RO 6/19/21) / REMOVED CORROSION, SCRATCHES AND GOUGES FROM L/H SIDE SEAT RAIL FROM FS364.00-FS409.00+112. REF: CRJ-200 SRM 51-21-06 AND CRJ-200SDR SWIA2021062258851Floor Support · corroded*RH PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION AS MARKED FROM APPROX FS 440 TO FS 542. (C-CHECK - RO 6/19/21) / COMPLIED WITH REO 601R-53-41-666, REV -C, DATED 2012-11-06 AND REO 601R-53-41-2917 REV-- DATED 2021-05-04 TO REPAIR RH PRESSURE FLOOR SILSDR SWIA202158850Floor Support · corroded*LH PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION AS MARKED FROM APPROX FS 424 TO FS 556. (C-CHECK - RO 6/19/21) / COMPLIED WITH REO 601R-53-41-666, REV -C, DATED 2012-11-06 AND REO 601R-53-41-2917 REV-- DATED 2021-05-04 TO REPAIR LH PRESSURE FLOOR SILSDR SWIA202158849Floor Support · corroded*RBL 9 FLOOR BEAM HAS CORROSION ON TOP SURFACE INBOARD SIDE AT APPROX FS 409+ 128, FS 463, FS 493 AND FS 537. (C-CHECK - RO 6/19/21) / REMOVED CORROSION FROM RBL9 AT 4 PLACES AT FS 409+128 , FS 463, FS 493, FS 537 REF REO 601R-53-00-005 REV B DATED 2011/0SDR SWIA202158848Intercostal · corroded*INTERCOSTAL HAS CORROSION BETWEEN FS319.00-FS333.00 AT STRG20L (MARKED) (C-CHECK - RO 6/19/21) / REPLACED NEW INTERCORSTAL AT STR21L FROM FS333.0 - FS 310.0 REF CRJ200 SRM 51-42-06, BOMBARDIER DWG 601R31527 REV AM. COMPLIED WITH SKYWEST 51-900-1003-SKY. CSDR SWIA202158847Frame · corroded*CORROSION NOTED AT FRAME 310 BETWEEN STRG 26L-26R (MARKED) (C-CHECK - RO 6/19/21) / REMOVED COROSION FROM FRAME 310 BETWEEN STRG 26L-26R REF CRJ 200 SRM 51-21-06, CORROSION ON FRAME 310 BETWEEN STRG 26L AND STRG 26R FOUND TO BE OUT OF LIMITS IAW CRJ 200SDR SWIA202158846Frame · corroded*CORROSION NOTED AT FRAME 319 BETWEEN STRG 26L-27L (MARKED) (C-CHECK - RO 6/19/21) / REMOVED COROSION FROM FRAME 319 BETWEEN STRG 26L-27L REF CRJ 200 SRM 51-21-06 BLEND WITHIN LIMITS. ORIGINAL MATERIAL IAW CRJ-200 SRM 53-21-15 PAGE 9-10 IS 0.052, REMOVED SDR SWIA202158845Floorbeam · corrodedSUPPORT BEAM @ STA. 559.00 BTW LBL 27.0 AND L/H FLOOR SILL HAS EVIDENCE OF CORRISION. MARKED WITH TAPE (C-CHECK - RO 6/19/21) / REMOVED CORROSION FROM LBL27 TO FLOOR SILL AT FS 559 REF CRJ200 SRWM 51-21-06. FOUND THE STRAP ON THE FLOOR BEAM AT FS 559 LBL SDR SWIA2021062258866Skin · corroded*LH WING TOP SKIN PANEL 540BT HAS FRETTING CORROSION ON LANDING. (C-CHECK - RO 6/19/21) / REMOVED CORROSION FROM LH WING TOP PANE 540BT LANDING REF CRJ 200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 57-21-31. MEASURED THICKNESS .198. ORIGINAL
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