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 SWIA200617528Panel · crackedPAX DOOR AFT SIDE PANEL CRACKED BEHIND HAND RAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS OT AFT SIDE PAX DOOR BEHIND HAND RAIL SUPPORT AS PER REO 601R-52-11-702.Oct 9, 2006 · N915SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617527Structure · crackedCRACK AT AFT DOOR EDGE MEMBER LOWER PART OF DOOR UNDER FOLDING STEP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-52-11-279 NC REO AND RII52-900-1001.Oct 9, 2006 · N915SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617526Angle · crackedCRACK AT LOWER EDGE OF OTBD (DOOR OPEN) DOOR ASSIST Z ANGLE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW OTBD Z ANGLE PN 601R31-7745-7 PO 71461 PER CRJ200 SRM 51-42-06 PG 1-8.Oct 9, 2006 · N915SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200617525Floorbeam · crackedFS 280 FLOORBEAM CLIPS 2EA LBL CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPLACEMENT CLIPS PER CRJ200 DWG 601R3113 AND SRM 51-40-06/51-24-16 PG 1-7.Oct 9, 2006 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200617524Floorbeam · crackedFS 280 FLOORBEAM CLIPS 2EA RBL 9 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PARTS IAW CRJ 200 SRM 51-42-06 PG 18 AT FS 280 FLOORBEAM RBL INBD AND OTBD.Oct 9, 2006 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200617523Floorbeam · crackedFS 280 FLOORBOARD SUPPORT IS CRACKED AT LBL 9.0, ON UPPER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. REPAIR PARTS INSTALLED IAW REO 601R-53-11-138 REV-NC.Oct 9, 2006 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200617025Light · inoperativeEMERGENCY LIGHTS ARE INOP AT THE SERVICE DOOR. THE EMERGENCY LIGHTS JUST FORWARD OF THE SERVICE DOOR WERE RE-LAMPED. OPERATIONAL CHECKS REF 33-00-00.Aug 19, 2006 · N915SW · Cndair CL6002B19 · Emergency LightingSDR SWIA200616765Window · crackedCAPTAINS LEFT SIDE WINDOW CRACKED. REPLACED LEFT SIDE WINDOW PER RII 56-402 AND AMM 56-12-01.Jun 6, 2006 · N915SW · Cndair CL6002B19 · Flight Compartment WindowsSDR SWIA200616107Sensor · malfunctionedFLAPS DEGRADED MESSAGE (STATUS) COMES ON AND WILL NOT RESET. REPLACED LT SKEW DETECTOR SENSOR IAW AMM 27-51-15. OPERATIONAL CHECK GOOD.Jan 7, 2006 · N915SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200515669Control Unit · malfunctionedSTAB CH 2 WOULD NOT ENGAGE AFTER POWER UP. REPLACED MOTOR CONTROL UNIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD.Oct 10, 2005 · N915SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200515598Actuator · malfunctionedSTAB TRIM CH 2 INOP STATUS MSG. REPLACED HSTA, MCU IAW AMM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD IAW AMM 27-40-00, 27-41-00.Sep 24, 2005 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515576Trim Switch · inoperativeSTAB TRIM CH. 2 WILL NOT ENGAGE. REPLACED FO'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW 27-41-05 AND 27-41-30.Sep 21, 2005 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515504Trim Switch · inoperativeSTAB CH 2 WILL NOT ENGAGE. REPLACED PILOT STAB TRIM DISCONNECT SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD IAW 27-41-00.Sep 4, 2005 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515475Control Panel · malfunctionedSTAB TRIM CH 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM PANEL. OPERATIONAL CHECK GOOD IAW MM 27-41-25 AND 27-41-00.Aug 25, 2005 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200515364Pcu · malfunctionedDURING ROLL OUT IN DEN A "SPOILERONS FAULT" STATUS MESSAGE. REPLACED LEFT OUTBOARD SPOILERON PCU IAW CRJ 200 AMM 27-62-01. OPERATIONAL CHECK GOOD.Jul 31, 2005 · N915SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200515304Actuator · malfunctionedSTAB TRIM CHANNEL 2 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MCU IAW CRJ 200 MM 27-42-01. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 851.Jul 20, 2005 · N915SW · Cndair CL6002B19 · Stabilizer ActuatorSDR SWIA200515241Control Unit · malfunctionedON T/O STAB TRIM HAD MOVED SMALL AMOUNT FROM WHERE IT WAS SET. INSTALLED SERVICEABLE HSTCU IAW CRJ MM 27-41-01 AND REPLACED F/O AND CAPT TRIM SWITCHS IAW MM 27-41-05. OPERATIONAL CHECK GOOD.Jul 5, 2005 · N915SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200514859A/C Pack · smokeSMOKE IN CABIN. SMOKE ORIGINATED WHILE RUNNING PACKS ON FAULTY AIR WISCONSIN GROUND START CART. RAN LEFT AND RIGHT AIR CONDITIONER PACKS FOR TWENTY MINUTES TO CLEAR SMOKE FROM PACKS. OPERATIONAL CHECK GOOD.Apr 6, 2005 · N915SW · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA200515213Floor Support · crackedFS 621 FLOOR SUPPORT ANGLE RBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515212Floor Support · crackedFS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV B.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515211Intercostal · crackedFS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515210Support Fitting · crackedSUPPORT FITTING CRACKED AT FS 460, RBL 9, OUTBOARD SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUPPORT FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-41-02.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200515209Support Beam · crackedENGINE SUPPORT BEAM LHS LWR WEB LBL 38 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV E.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA200515208Intercostal · crackedINTERCOSTAL CRACKED, FS 484, LBL 36, ITEM FOUND AT C-CHECK INSPECTION. REPAIR CARRIED OUT IAW REO 601R-53-41-059 REV A.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200515207Attach Angle · crackedFS 280 RT FLOORBEAM RBL 9.0 IB AND OB ANGLES CRACKED ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 AND 51-21-11.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA200515206Floorbeam · crackedFS 280 L FLOORBEAM LBL 9.0 OB ATTACH ANGLE CRACKED (ITEM FOUND AT C-CHECK INSPECTION.) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 AND 51-21-11.Mar 21, 2005 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200414271Servo · stuckON SHORT APPROACH TO DEN AT 300 FT AGL, ON AUTO PILOT DISCONNECT THE ELEVATOR FROZE. AFTER PULLING HARD ON THE YOKE, CONTROL WAS RESTORED. REMOVED AND REPLACED ELEVATOR SERVO IAW 22-11-24-00. OPERATIONAL TEST GOOD OF ELEVATOR SERVO PER AMM 22-11-24-710-801.Dec 12, 2004 · N915SW · Cndair CL6002B19 · Autopilot Trim ServoSDR SWIA200413761Control Unit · malfunctionedSTAB TRIM CHANNEL 1 WILL NOT ENGAGE. INSTALLED A SERVICEABLE HSTCU. OPERATIONAL CHECK GOOD.Aug 24, 2004 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413665Wire Harness · damagedTRIM RUNAWAY ALARM AND TRIM INDICATOR ERRATIC, MACH TRIM MESSAGE. REMOVED AND REPLACED CHANNEL 1 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. REMOVED AND REPLACED CHANNEL 2 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONAug 1, 2004 · N915SW · Cndair CL6002B19 · Flight Control System WiringSDR SWIA200413589Actuator · malfunctionedSTAB TRIM AND MACH TRIM CAUTION MESSAGES JUST AFTER T/O AND REPEATED IN FLIGHT. REMOVED AND REPLACED HSTC ACTUATOR AND HRTCU MOTOR IAW CRJ MM 27-42-01 AND 27-42-05 RESPECTIVELY. OPERATIONAL CHECK GOOD. P/N: 7062-3, S/N ON: 602, S/N OFF: 138.Jul 16, 2004 · N915SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413528Control Unit · malfunctionedDURING LEVEL FLIGHT AP PITCH TRIM MESSAGE. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD.Jul 1, 2004 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200413453Actuator · malfunctionedSTAB TRIM CH 1 DISENGAGED IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR AND MOTOR CONTROL UNIT, IAW CRJ MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD.Jun 19, 2004 · N915SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200413438Wire · brokenWIRES PULLED OUT OF CONNECTOR OF FIRST OFFICER'S STICK SHAKER. REPAIRED CONNECTOR PER AWM 20-17-10. OPERATIONAL CHECK GOOD PER AMM 27-35-01.Jun 13, 2004 · N915SW · Cndair CL6002B19 · Navigation System WiringSDR SWIA200413136Proximity Sensor · malfunctionedFLAPS FAIL CAUTION MESSAGE APPROX 30 SEC. AFTER SELECTING 0 DEGREES AFTER DEPARTURE. FLIGHT CONTROL PAGE SHOWS FLAPS 0 DEGREES YELLOW OUTLINE. REMOVED AND REPLACED RIGHT BPSU AND RIGGED IAW CRJ MM CHAPTER 27-51-10. OPS CHECKS GOOD.Apr 11, 2004 · N915SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200413133Wire · brokenDURING STALL TEST -STALL FAIL- CAUTION MESSAGE APPEARED. REPAIRED BROKEN WIRE ON STICK SHAKER ON FIRST OFFICER'S YOKE AS REQUIRED. OPS CHECKED GOOD IAW MM 27-35-00.Apr 8, 2004 · N915SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200413092Warning Light · false indicationAFTER TAKEOFF, FLAPS FAILED TO COME UP. FLAPS STOPPED 6-8 DEGREES WITH ASSOCIATED FLAPS FAIL CAUTION MESSAGE. RETURNED TO FIELD. PERFORMED A POWER DOWN/POWER UP ON AIRCRAFT. ALL OPS CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY.Mar 26, 2004 · N915SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200413025Control Handle · malfunctionedPLACED FLAP HANDLE TO 20 FLAP POSITION INDICATED 8, RECEIVED FLAPS FAIL MESSAGE. REMOVED AND REPLACED FECU IAW MM 27-51-04. OPS CHECK GOOD.Mar 16, 2004 · N915SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200412826Switch · malfunctionedON CLIMBOUT LOST STAB AND MACH TRIM, WOULD NOT RE-ENGAGE. RETURNED TO FIELD. ON APPROACH MOMENTARILY GOT TRIM BACK THEN LOST IT AGAIN. REMOVED AND REPLACED CAPTAIN'S YOKE PITCH TRIM DISCONNECT SWITCH IAW CRJ AMM 27-41-30. P/N ON: 996-0013.Jan 27, 2004 · N915SW · Cndair CL6002B19 · Stabilizer Position IndicatingSDR SWIA200312742Fcu · malfunctionedEN ROUTE FLAPS FAIL CAUTION MESSAGE. REPLACED FECU. OPS CHECK GOOD.Dec 31, 2003 · N915SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200312539Ecu · malfunctionedFLIGHT SPOILERS STATUS MESSAGE ON TAXI OUT. REMOVED AND REPLACED NR 2 SECU PER AMM 27-61-05. OPS CHECK GOOD. P/N OFF: 49-164-05, S/N OFF: 01430.Oct 18, 2003 · N915SW · Cndair CL6002B19 · Drag Control SystemSDR SWIA200312495Actuator · malfunctionedFLAPS FAIL MESSAGE WHEN SELECTED TO 45 DEGREES. FLAPS STOPPED AT 33 DEGREES. QRH COMPLIED. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR AND RIGHT INBOARD FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-53-01 AND 27-53-05. P/N OFF: 852D100-11, S/N OFF: 3Oct 5, 2003 · N915SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA200312400Intercostal · crackedFS484 RT INTERCOSTAL OUTBOARD FLG, RBL36 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV ''A''.Sep 12, 2003 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312399Intercostal · crackedFS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.Sep 11, 2003 · N915SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312398Floorbeam · crackedFS 280 RT FLOORBEAM RBL 9.0 I/B ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11.Sep 11, 2003 · N915SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312505Handle · crackedPASSENGER DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE REMOVED AND REPLACED IAW CRJ MM 52-11-03. OPS CHECKS GOOD.Sep 10, 2003 · N915SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA200312372Actuator · failedFLAPS FAIL MESSAGE. FLAPS STOPPED AT 38 DEGREES. FLAPS WOULD NOT RAISE ON GROUND. REMOVED AND REPLACED LEFT INBOARD FLAP OUTBOARD ACTUATOR IAW MM 27-53-05. OPS CHECK GOOD.Sep 1, 2003 · N915SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA200311888Warning System · false activationFLAP FAIL MESSAGE APPEARED WITH FLAP SELECTED TO FLAPS 8. FLAP FAILED IN UP POSITION. RESET FLAP SYSTEM AND INSPECTED FLAP SURFACES. INSPECTION REVEALED NO IRREGULARITIES. RECORDED FLAP SYSTEM FAULT CODES. FLAPS OPS CHECKED NORMAL. RAN FLAPS UP AND DOWN Apr 14, 2003 · N915SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR SWIA200311840Control Unit · failedFLAP FAIL MESSAGE - PERFORMED NO FLAP LANDING. COMPLIED WITH OPS CHECK OF FLAP SYSTEM. CHECKED FECU, NO FAULTS FOUND. OPERATED FLAPS, ALL OPS CHECKS GOOD IAW CRJ MM 27-51-00.Mar 20, 2003 · N915SW · Cndair CL6002B19 · Trailing Edge Flap Control System
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