N915SW

Service difficulty reports · 248

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 = 'N915SW' 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.

SDR SWIA202266800None · crackedLH FRAME 605 FLANGE CRACKED ATSTGR 9 (C-CHECK RO 11/10/2022) REPAIRED LH FRAME 605.00 AT STGR 9 REF REO 601R-53-61-5214 REV -A DATE 2016-11-04. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.Sep 2, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266799None · corrodedLH INTERCOSTAL FS 333 TO 349 STGR 21 HAS CORROSION (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LH INTERCOSTAL FS 333 TO 349 STGR 21 P/N: 691R31527-19 REF DWG. 601R31527 REV. AM, CRJ-200 SRM 51-21-16, SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH 51-900Sep 2, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202266829None · corroded*MULTIPLE SPOTS OF CORROSION AT R/H FLOOR SILL BETWEEN FS559.00-FS559.00+16 (MARKED) (C-CHECK RO 11/10/2022) REMOVED AND INSTALLED NEW INTERCOSTAL AT R/H FLOOR SILL BETWEEN FS559.00-FS559.00+16. REF CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-42-06 AND DWG NO Sep 1, 2022 · N915SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266828None · corroded*CORROSION ON FRAME 349 BETWEEN STRG26L-STRG26R (MARKED) (C-CHECK RO 11/10/2022) REMOVED AND REPLACED NEW FRAME SECTION AT FS349 AT APPROX STGR 23L AND STGR 23R REF. CRJ-200 SRM, 51-42-06, CRJ-200 SRM, 51-42-21 AND DWG 601R32005 REV AR. COMPLIED WITH TASep 1, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266827None · crackedFS 484 AT LBL27 INNER CLIP IS CRACKED AT UPPER RADIUS INSIDE FUSELAGE (C-CHECK RO 11/10/2022) REMOVED AND REPLACED FS 484 AT LBL27 INNER CLIP IS CRACKED AT UPPER RADIUS INSIDE FUSELAGE. REF. DWG 601R31171, REV-E, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21Sep 1, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266826None · crackedFS 484.00 RBL 27 , INNER CLIP IS CRACKED AT UPPER RADIUS INSIDE FUSELAGE. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED CLIP P/N 601R31171-9 PER CRJ200 SRM 51-40-11, CRJ200 SRM. 51-42-06 AND CRJ200. SRM. 51-42-21, DWG. 601R31171. REV -E / COMPLIED WITH Sep 1, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266825None · crackedFS 460 RBL 9.0 THERE IS A SUSPECT CRACK ON UPPER RADIUS OF CASTING ON PRESSURE FLOOR BEAM. (C-CHECK RO 11/10/2022) LOCATED, DRILLED AND INSTALLED NEW 600-31068-19 FLOOR SUPPORT FITTING REF CRJ 200 SRM 51-42-21 CRJ-200 SRM 51-42-22 AND CRJ 200 SRM 51-42-Sep 1, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266824None · corrodedR/H SIDE PRESSURE FLOOR SILL HAS AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK RO 11/10/2022) EVALUATED AND BLENDED AREA, FOUND TO BE WITHIN LIMITS. REF. REO 601R-53-41-3077 REV. -- DATED: 2022-10-03 STEPS 1-7. COMPLIED WITH SKYWEST TASK CARDSep 1, 2022 · N915SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266823None · corrodedL/H SIDE INSIDE PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559.0 HAS AREAS OF CORROSION (C-CHECK RO 11/10/2022) BLENDED CORROSION WITHIN LIMITS ON L/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559.0 REF REO 601R-53-41-666 REV. -C DATED 2012-11-06, AND RESep 1, 2022 · N915SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202266822None · crackedRH ENGINE PYLON RIB AT FS 605.00 IS CRACKED ON LOWER FLANGE AT OUTBOARD EDGE (MARKED). (C-CHECK RO 11/10/2022) REPAIRED RIGHTHAND ENGINE PYLON RIB AT FS605.00 AT LOWER FLANGE AT OUTBOARD EDGE IAW REO 601R-54-61-138 REV -- DATE 2022-09-23 STEPS. 1-15 (SEAug 30, 2022 · N915SW · Cndair CL6002B19 · Nacelle/Pylon StructureSDR SWIA202266821None · corrodedDURING REMOVAL OF L/H ELEVATOR #1 HINGE FITTING BEARING, FOUND FITTING TO BE CORRODED IN BEARING BORE, FITTING REQUIRES REPLACEMENT. (C-CHECK RO 11/10/2022) REMOVED CORRODED L/H ELEVATOR #1 HINGE FITTING ASSY, AND INSTALLED 1 EA NEW FITTING ASSY P/N 600Aug 30, 2022 · N915SW · Cndair CL6002B19 · Elevator Tab, Attach FittingsSDR SWIA202266820None · corrodedAFT FORMER ON PAX DOOR HAS CORROSION MID AREA OF FORMER. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER REF DWG# 601R31702 REV N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SAug 30, 2022 · N915SW · Cndair CL6002B19 · DoorsSDR SWIA202266819None · corrodedFWD FORMER ON PAX DOOR HAS CORROSION MID AREA OF FORMER. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER REF. DRWG 601R31702 REV. N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003Aug 30, 2022 · N915SW · Cndair CL6002B19 · DoorsSDR SWIA202266818None · crackedCRACKED CLIP FROM THE AFT SIDE OF THE 621 BULKHEAD AT STGR.14 RIGHT. (MARKED) (C-CHECK RO 11/10/2022) REMOVED AND REPLACED CLIP AT AFT SIDE OF THE 621 BULKHEAD AT STGR 14 RIGHT PER REF CRJ200 SRM 51-42-21AND DWG 601-35012 REV D. FOR DETAIL SEE ATTACHED Aug 29, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202266817None · corrodedRH WHEEL WELL STRAP FS538.70 CORRODED AND CHAFED AS MARKED (C-CHECK RO 11/10/2022) REMOVED CHAFED RH WHEEL WELL STRAP. LOCATED AND DRILLED NEW GUSSET P/N 601R31058-392 TO MATCH EXISTING STRUCTURE, INSTALLED NEW GUSSET REF CRJ 200 SRM 51-42-06 AND DRAWIAug 27, 2022 · N915SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWIA202266816None · corrodedPASSENGER DOOR - DOUBLER ON THE INNERSIDE OF THE SILL DEPRESSOR AT THE FORWARD LOWER CORNER IS CORRODED. (MARKED) (C-CHECK RO 11/10/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED PARTS. REF. CRJAug 26, 2022 · N915SW · Cndair CL6002B19 · DoorsSDR SWIA202266815None · chafedLH OUTBOARD FLAP CENTER HINGE ARM SIDE PLATE HAS CHAFING DAMAGE (C-CHECK RO 11/10/2022) REMOVED AND REPLACED CHAFED LH OTBD FLAP CENTER HINGE ARM SIDE PLATE. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-15 & DWG 601R14699 REV B. ALL STEPS OF 51-900-1003-SAug 26, 2022 · N915SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202266814None · gougedL/H MLG UPLOCK STRUCTURE (GUSSET) IS GOUGED. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LEFTHAND MAIN LANDING GEAR UPLOCK STRUCTURE GUSSET P/N: 601R31058-81 IAW CRJ 200 SRM 51-42-06. (SEE CONTINUATION SHEET FOR FURTHER DETAILS). COMPLIED WITH 51-900-1Aug 26, 2022 · N915SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202266813None · corrodedPASSENGER DOOR- FLOOR SUPPORT ANGLE ON THE LOWER SILL IS CORRODED. (MARKED) (C-CHECK RO 11/10/2022) EVALUATED OUT OF LIMITS, REMOVED AND INSTALLED NEW REF CRJ200 SRM 51-42-06, REF CRJ200 SRM 51-42-21 AND DWG 601R31020 REV-F. COMPLIED WITH SKYWEST TASK Aug 25, 2022 · N915SW · Cndair CL6002B19 · DoorsSDR SWIA202266812None · chafedLH INBOARD FLAP OUTBOARD HINGE ARM SIDE PLATES HAVE CHAFING DAMAGE (C-CHECK RO 11/10/2022) BLENDED CHAFING DAMAGE FROM LH INBOARD FLAP OUTBOARD HINGE ARM SIDE PLATES. REF CRJ200 SRM 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050" PER CRJ200 SRM 57-54-00Aug 25, 2022 · N915SW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR SWIA202266811None · elongatedPAX DOOR HINGE FUSELAGE SIDE 4EA MOST AFT LUGS ARE ELONGATED WORN (C-CHECK RO 11/10/2022) EVALUATED OUT OF LIMITS, REMOVED AND INSTALLED NEW PAX DOOR HINGE REF DWG 601R31020 REV-F, REO 601R-53-21-656 REV-A DATED 2017-03-06 AND REF CRJ200 SRM 53-21-23,SRAug 25, 2022 · N915SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWIA202266810None · corrodedCORROSION AROUND BOTH DRAIN HOLES FS559.00+64 - FS559.0+80 STGR26L €“ STGR26R. (MARKED) (C-CHECK RO 11/10/2022) REPAIRED CORROSION AROUND DRAIN HOLES AT FS559.00+64 TO FS559.00+80 AND STR26L TO STR26R PER REO 601R-53-51-626 REV -- DATED 2022-09-17, CRJAug 24, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266809None · dentedEVALUATE DENT ON THE AFT FUSELAGE NEAR FS 700, STGR. 9 RIGHT. (MARKED) (C-CHECK RO 11/10/2022) REPAIRED AFT FUSELAGE SKIN BETWEEN FS690.00 TO FS700.00 BETWEEN STRINGER8R TO STRINGER9R IAW CRJ 200 SRM 53-00-31 STEP 4. (1-12) REPAIR 3 FIGURE 204 SHEET 1 .Aug 22, 2022 · N915SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202266808None · chafedLH ALIERON UPPER LEADING EDGE SKIN HAS CHAFING DAMAGE BETWEEN INBOARD AND MID HINGE POINTS AS MARKED. (C-CHECK RO 11/10/2022) LOCATED DRILLED AND INSTALLED NEW LH AILERON LEADING EDGE SKIN P./N CC670-13052-1 REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-06 Aug 18, 2022 · N915SW · Cndair CL6002B19 · Aileron TabsSDR SWIA202266807None · chafedLH INBOARD FLAP VANE LEADING EDGE HAS CHAFING DAMAGE OUTBOARD OF FLAP MID VANE ACTUATOR SLIDING BEAM APPROX WS 106.352 AS MARKED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LH INBD FLAP VANE LE OTBD OF FLAP MID VANE ACTUATOR SLIDING BEAM APPROX WS 106.Aug 18, 2022 · N915SW · Cndair CL6002B19 · AileronsSDR SWIA202266806None · none* MULTIPLE GOUGES FOUND AROUND THE UPPER AND LOWER END OF THE CARGO COMPARTMENT DOOR HANDLE CUT-OUT.( AREA MARKED) (C-CHECK RO 11/10/2022) REPLACED THE CARGO DOOR HANDLE HOUSING REF CRJ 200 SRM 51-42-21 AND DWG 601R35027 REV AY. M-337 AND SKYWEST TASK CAug 17, 2022 · N915SW · Cndair CL6002B19 · DoorsSDR SWIA2020062251140Window · crackedSEAT 3D EXTERNAL WINDOW PANE IS BROKEN AND CRACKED. FLIGHT 5283 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO ITEM 20919066 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED SEAT 3CD EXTERNAL WINDOW PANE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM.May 3, 2020 · N915SW · Cndair CL6002B19 · Passenger Compartment WindowsSDR SWIA2018112145268Skin · dentedDENT LOCATED AT WS 50.498 AND ABOVE 5.0€? FROM TRAILING EDGE OF R/H I/B FLAP. (C-CHECK) RO: 11/20/2018 PERFORMED PERMANENT DOUBLER REPAIR TO DENT LOCATED AT WS 50.498 AND ABOVE 5.0€? FROM TRAILING EDGE OF R/H I/B FLAP IAW SRM.Nov 7, 2018 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2018112145267Floorbeam · corrodedR/H CABIN FLOOR SUPPORT AT FS. 559 OUTBOARD OF RBL 36 HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 11/20/2018 REMOVED AND INSTALLED NEW FLOOR SUPPORT AT FS 559.00 BETWEEN RBL 36 AND RBL 56 IAW SRM. LEAK CHECK GOOD.Nov 2, 2018 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2018082345009Seal · failedLOUD SQUEAL THROUGH 10,000 FEET. PASSING 13,000 FEET SQUEAL BECAME LOW PITCHED AND CABIN ALTITUDE BEGAN TO CLIMB. DESCENDED, DECLARED AN EMERGENCY AND RETURNED TO FIELD. REMOVED AND REPLACED THE PASSENGER DOOR SEAL IAW AMM, OPS CHECKED GOOD. PERFORMED PRESSURAug 23, 2018 · N915SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201642749Closeout Panel · corrodedPAX DOOR CLOSEOUT PANEL 832GR HAS CORROSION AROUND FASTENERS. REPLACED THE CLOSEOUT PANEL IAW SRM.Oct 22, 2016 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642748Closeout Panel · corrodedPAX DOOR CLOSEOUT PANEL 832HL HAS CORROSION AROUND FASTENERS. REPLACED CLOSEOUT PANEL IAW SRM.Oct 22, 2016 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201642747Vane · chafedLEFT INBD FLAP OUTBOARD FLAP VANE CAP IS CHAFED. INSTALLED A NEW VANE CAP IAW SRM.Oct 6, 2016 · N915SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642746Vane · chafedLEFT INBD FLAP INBD VANE CAP IS CHAFED. INSTALLED A NEW VANE CAP IAW SRM.Oct 6, 2016 · N915SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201642745Floorbeam · corrodedFLOORBEAM TEE BS 615 LBL 27 HAS CORROSION. FLOORBEAM TEE WAS REPLACED IAW SRM.Oct 6, 2016 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201642744Panel · chafedRIGHT WING PANEL 699CB HAS CHAFED. REPLACED THE PANEL IAW SRM.Oct 2, 2016 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201642743Panel · chafedRIGHT WING PANEL 699AB CHAFED. REPLACED THE PANEL IAW SRM.Oct 2, 2016 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201541701Detector · failedFLAPS FAIL AT 14 DEGREES. REPLACED THE SKEW DETECTOR. COMPLIED WITH FULL FLAP AD IAW AMM.Dec 23, 2015 · N915SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA201540713Frame · puncturedFWD AREA OF THE PAX DOOR JUST ABOVE THE LOWER GREEN LOCK INDICATOR PANEL HAS A PUNCTURE. REPLACED INNER FRAME ON PAX DOOR AND COMPLIED WITH REO REPAIR ON FWD AREA OF THE PAX DOOR JUST ABOVE THE LOWER GREEN LOCK INDICATOR PANEL, PN 600-31902-260.Feb 4, 2015 · N915SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA201439642Access Panel · chafedLT WING FUEL ACCESS PANEL 550HB IS CHAFED ON INBD AFT MATING SURFACE. C-CHECK, REPAIRED IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439641Access Panel · chafedLT WING FUEL ACCESS PANEL 550EB IS CHAFED ON INBD MATING SURFACE. C-CHECK, REPAIRED IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439640Access Panel · chafedLT WING FUEL ACCESS PANEL 550AB IS CHAFED ON OTBD MATING SURFACE. C-CHECK, REPAIRED IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439639Access Panel · chafedLT WING FUEL ACCESS PANEL 540FB IS CHAFED ON INBD AFT MATING SURFACE. C-CHECK, REPAIRED IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439638Access Panel · chafedLEFT WING FUEL ACCESS PANEL 540BB IS CHAFED ON OTBD MATING SURFACE. C-CHECK, REPAIRED IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439637Access Panel · chafedLEFT WING ACCESS PANEL 540BB IS CHAFED ON INBD MATING SURFACE. C-CHECK, REPAIRED THE ACCESS PANEL IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439635Floorbeam · crackedBS 280 FLOORBEAM IS CRACKED AT RBL 9. C-CHECK, REPAIRED IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201439622Access Panel · chafedRT WING FUEL ACCESS PANEL 650HB IS CHAFED ON INBD AFT MATING SURFACE. C-CHECK, REPAIRED CHAFING ON RT WING ACCESS PANEL IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439621Access Panel · chafedRT WING FUEL ACCESS PANEL 640BB IS CHAFED ON INBD MATING SURFACE. C-CHECK, REPAIRED CHAFING ON RT WING ACCESS PANEL IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA201439619Bulkhead Web · crackedMULTIPLE CRACKS FOUND ON BS 280.0 BULKHEAD WEB. C-CHECK, BULKHEAD WEB REPAIR IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201439618Splice · crackedLOWER SPLICE ANGLE AT FS 280, LBL 9 IS CRACKED. C-CHECK, REPAIRED IAW REO.Oct 9, 2014 · N915SW · Cndair CL6002B19 · Fuselage Main, Structure
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