N778SK
Service difficulty reports · 208
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 = 'N778SK' 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 = 'N778SK' 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 SWIA2026092077223Windshield · crackedLEFT WINDSHIELD HEAT CAUTION MESSAGE. WINDSHIELD CRACKED A FEW MINUTES AFTER THE MESSAGE CAME ON. FLIGHT 4312. LT WINDSHIELD REMOVED AND REPLACED IAW TASK CARD 56-220-1000-SKY, OPS CHKD GOOD, PRESSURIZATION CHKD GOOD.SDR SWIA2026082876970Ballast · failedPASSENGER LIGHT OVER 1 A BEGAN FLICKERING AND SMOKE BEGAN TO COME OUT OF THE LIGHT AREA. (FLIGHT 4324)TROUBLESHOT SMOKE IN CABIN IAW FIM 21-22-00-810-806. PERFORMED OPS CHECK OF AC DISTRIBUTION SYSTEM IN REFERENCE TO AMM 21-51-00 PER FIM. NO SMOKE OR ABNORMALSDR SWIA2026050676003Wire Splice · damagedANTISKI INBOARD CAUTION, PARKING BRAKE SOV CAUTION, AND PARKING BRAKE WARNING MESSAGE ON UPWIND OUT OF DETROIT. (FLIGHT 3936)TROUBLESHOT IAW FIM 32-45-16. FOUND SPLICES TO MICROSWITCHES HAD PINS PULL OUT OF SPLICE SP62. REPLACED SPLICE SP62 AT PARKING BRAKE MSDR SWIA2026050475998Shutoff Valve · faultedPARKING BRAKE WARNING IN CRUISE. PERSISTED MOST OF FLIGHT. PERFORMED OPS TEST OF PARKING BRAKE IAW AMM 32-45-00. COULD NOT DUPLICATE FAULT WITH PARKING BRAKE RELEASED. INTERROGATED MDC FOUND FAULT CODE B1-007492 FLAGGING PARKING BRAKE SIGNAL DISAGREE & CODE BSDR SWIA2026020975235Landing Gear · warning messageGEAR DISAGREE ON DEPARTURE. RIGHT MLG RED. LEFT AND NOSEWHEEL UP AND LOCKED. RAN QRH. LANDING GEAR STAYED DOWN FOR REST OF THE FLIGHT. LANDING NORMALC:MEL 32-30-1CAT "A" DUE 1 FLT DAYMX ACTION COMPLIED WITH (FLIGHT 350)FEB 09, 2026 STATION: GRR--DEFERRED LASDR SWIA2026021075235Landing Gear · warning messageDUE TO ODI EVENT SMOD APPROVAL REQUIRED FOR RTS, CAT II DOWNGRADED. GEAR DISAGREE ON DEPARTURE. RIGHT MLG RED. LT AND NOSEWHEEL UP AND LOCKED. RAN QRH. LANDING GEAR STAYED DOWN FOR REST OF THE FLIGHT. LANDING NORMAL. MEL 32-30-1CAT A DUE 1 FLT DAY, MX ACTSDR SWIA2025040700004Oxygen System · warning messageCRUISING AT 370FL RECEIVED O2 LOW MSG OBSERVED O2 LEVEL 900 PSI DROPPING 10 LBS EVERY 40 SECS, LOWEST LEVEL WAS 500 PSI. ON THE GRD ITS SITTING AT 1660 PSI (FLIGHT 3676 - FILED CLOSED)PLEASE REFERENCE AML 1575104 TROUBLESHOT DISCREPANCY IN REF TO CRJ 700 FIM 3SDR SWI2025F00283Oxygen Bottle · low pressureOXYGEN LO PRESS CAUTION MESSAGE IN CRUISE. PRESSURE WENT AS LOW AS 600PSI. PRESSURE WENT BACK TO NORMAL AFTER LANDING. MEL 35-12-1ACAT C, SMOD RTS APPROVAL REQUIRED DUE TO ODI EVENT. OXYGEN LO PRESS CAUTION MESSAGE IN CRUISE. PRESSURE WENT AS LOW AS 600PSI.SDR SWIA20241220Bracket · chafedNLG, BEFORE INSTALLING SERVICEABLE GEAR, FOUND CHAFE ON AFT WALL BRACKET FOR THE LOCK LINK, HN00208689 (C-CHECK RO 1/29/2025) REMOVED CHAFE AT THE NLG AFT WALL BRACKET FOR THE LOCK LINK REF CRJ 700 SRM 51-12-00-001-001-A01 FOUND TO BE OUT OF LIMITS. RECSDR SWI2025F00089Floor Support · corrodedFLOOR BEAM ON TOP SURFACE HAVE CORROSION AT LBL9 BTW FS645 TO FS677 (MX 29228065) (C-CHECK RO 1/29/2025) --REPAIRED FLOOR BEAM SECTION AT LBL 9.0 BETWEEN F/S 639.00 TO F/S 686.00 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REF REO 670-53-31-983 REV -- DATSDR SWI2025F00081Stringer · corrodedSTRINGER 26L HAS CORROSION FROM APPROX FS280 - FS333 MX 29199537 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW STR 26L FROM FS280 TO FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV KCOMPLIED WITH SKYWESSDR SWI2025F00121Floorbeam · corrodedCORROSION ON LH CROSSBEAM AT FS 280.00 TRANS #29193959 (C-CHECK RO 1/29/2025) REMOVED LH CROSSBEAM AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01. INSTALLED NEW LH CROSSBEAM AT FS 28SDR SWIA20250130121Web · corrodedLH WEB AT FS 280.00 HAS CORROSION TRANS #29190182 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW LH LOWER WEB AT FS280 REF CRJ 700 SRM 53-11-10-201-004-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-10002-SKYSDR SWI2025F00120Floorbeam · crackedFOUND CRACK ON COCKPIT FLOORBEAM AT LBL12.00 FS 280.00. TRANS #29187421 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW SECTION FLOOR BEAM AT LBL 12.00, ITEM -35 INBOARD UPPER ANGLE, ITEM -37 INBOARD LOWER ANGLE, -ITEM 39 OUTBOARD WEB ANGLE AND ITEM -4SDR SWI2025F00119Floorbeam · crackedFOUND CRACK ON COCKPIT FLOORBEAM AT RBL12.00 FS 280.00. TRANS #29187403 (C-CHECK RO 1/29/2025) REMOVED RH FLOOR SUPPORT BETWEEN FS250.00 - FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01.INSTALLED SECTION FLOOR BEAM AT RBL 12.00, ITEM -36 INBOARD UPPER ASDR SWI2025F00118Frame · corrodedFRAME FS310 BETWEEN STGR25L & STGR25R IS CORRODED (C-CHECK RO 1/29/2025) INSTALLED NEW LOWER FRAME SECTOR FS310 BETWEEN STGR25L & STGR25R REF CRJ-700 SRM 53-00-06-201-006-A01. PERFORMED PRESSURE LEAK CHECK IAW CRJ700 AMM 21-31-00-910-801-A01. PRESSURE SDR SWIA2025013020Frame · corrodedFRAME FS295 BETWEEN STGR25L & STGR25R IS CORRODED (C-CHECK RO 1/29/2025) INSTALLED NEW LOWER FRAME SECTOR FS295 BETWEEN STGR25L & STGR25R REF CRJ-700 SRM 53-00-06-201-006-A01. PERFORMED PRESSURE LEAK CHECK IAW CRJ700 AMM 21-31-00-910-801-A01. PRESSURE SDR SWI2025F00097Slat Track · crackedLH SLAT TRACK CANISTER 1-3 IS CRACKED (C-CHECK RO 1/29/2025) REMOVED LH WING SLAT #1 REF CRJ 700 AMM 27-81-17-000-801-A01. PERFORMED ALL STEPS OF REO 670-57-42-577 REV -- DATED 2016-12-02 TO PERFORM REPAIR OF LH SLAT TRACK CANISTER 1-3. INSTALLED LH WINSDR SWI2025F00117Floor Support · crackedRIGHT HAND COCKPIT FLOOR BEAM AT APPROX. RBL 12 AND JUST AFT OF FS 202.00 IS CRACKED. HN00200833 (C-CHECK RO 1/29/2025) RECEIVED AND COMPLIED WITH REO 670-53-11-2052 REV -- DATED 2024-11-15 REPAIR TO COCKPIT FLOOR BEAM RBL12 BETWEEN FS.220-FS.226. COMPLSDR SWI2025F00116Hinge · gougedPAX DOOR PIANO HINGE (DOOR SIDE) HAS MULTIPLE GOUGES ON THE LUG LANDS, IN THE LUG TO LAND RADIUS AND ON THE SIDES OF THE LUGS. (C-CHECK RO 1/29/2025) BLENDED AND EVAL'D PAX DOOR PIANO HINGE LUG LANDS (DOOR SIDE), FOUND TO BE WITHIN LIMITS REF MHIRJ REOSDR SWI2025F00115Hinge · gougedPAX DOOR HINGE (FUSELAGE SIDE) LAST LAND LUG GOUGED FROM PROTRUDING ROLL PIN. (C-CHECK RO 1/29/2025) REMOVED, EVALUATED AND REPAIRED GOUGE AT PAX DOOR HINGE LAND LUG , WAS FOUND WITHIN LIMITS REF REO 670-53-21-582 REV-G DATE:2024-02-18. ALL STEPS OF RESDR SWI2025F00114Skin · damagedRH ICE DETECTOR SKIN CUT OUT, FASTENER HOLE HAS DRILL DAMAGE, EGG SHAPED AND OVERSIZED (MARKED) (C-CHECK RO 1/29/2025) REPAIRED PER MHIRJ REO 670-53-11-2053 REV -- 2024-11-23. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYPERFORMED PRESSURE LEAK CHECKSDR SWIA202501300013Floor Support · gougedR/H FLOOR SILL BETWEEN FS437.00 TO FS453.00 HAS GOUGED (MARKED) (C-CHECK RO 1/29/2025) BLENDED GOUGE AT R/H FLOOR SILL BETWEEN FS437.00 TO FS453.00 REF CRJ700 SRM 51-12-00-001-001-A01 EVALUATED BLEND AT R/H FLOOR SILL BETWEEN FS437.00 TO FS453.00, THE BSDR SWI2025F00113Intercostal · corrodedINTERCOSTAL HAS CORROSION, AFT OF FS661.00 STGR19R. (MARKED) (C-CHECK RO 1/29/2025) EVALUATED INTERCOSTAL (DIAPHRAGM) AT FS661.15+2" AND STGR19R. FOUND EXFOLIATION AND MATERIAL LOSS ON DIAPHRAGM, IS OUT OF LIMITS, MUST BE REPLACED PER CRJ700 SRM TASK 5SDR SWI2025F00112Floorbeam · crackedCRACKED ANGLE ATTACHED TO OTBD SIDE OF FLOOR BEAM LBL 12 AND AFT FACE OF FS 280.00 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW ANGLE AT OTBD SIDE OF FLOOR BEAM LBL 12 AND AFT FACE OF FS 280.00 REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG CC670-34010SDR SWI2025F00111Floorbeam · crackedCRACKED ANGLE ATTACHED TO OTBD SIDE OF FLOOR BEAM RBL 12 AND AFT FACE OF FS 280.00 (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW ANGLE ATTACHED TO OTBD SIDE OF FLOOR BEAM RBL 12 AND AFT FACE OF FS 280.00 REF CRJ700 SRM 51-42-21-001-001-A01. AND DWG CSDR SWI2025F00110Hinge · damagedFABRICATE R/H UPPER TRANSCOWL HINGE HALF CN624-2030-207 (C-CHECK RO 1/29/2025) FABRICATED HINGE HALF REF EO CL-600-2C10-53-L08541 REV A 2024-11-23 USING 15-5PH HT1025 PO# 5-42720 DWG CN624-2030 REV C COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWI2025F00109Bracket · corrodedCORROSION ON BRACKET AT FS364.0 STGR27 AS MARKED (C-CHECK RO 1/29/2025) REMOVED CORROSION ON STGR27 (NOT A BRACKET) ON SKIN FLANGE (AFT END OF STGR27) REF CRJ-700 SRM 51-21-06-001-001-A01. STGR LOSS 100% OF MATERIALREMOVED AND REPLACED STR 27 FROM FS333SDR SWIA20250130112Stringer · corrodedCORROSION ON STGR25R BETWEEN FS319.0 AND FS333.0 AS MARKED (C-CHECK RO 1/29/2025) INSTALLED NEW STR 25R FROM FS280 TO FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND SH670-31630 REV K. PERFORMED PRESSURE LEAK CHECK IAW CRJ700SDR SWI2025F00108Floor Support · corrodedCABIN FLOOR BEAM AT RBL9 BETWEEN FS1015.00 TO FS1051.30 HAS CORROSION AS MARKED (C-CHECK RO 1/29/2025) REMOVED CORROSION ON CABIN FLOOR BEAM AT RBL9 BETWEEN FS1015.00 TO FS1051.30 REF CRJ-700 SRM 51-21-06-001-001-A01FLOOR BEAM IS OUT OF LIMITS. NO DAMSDR SWI2025F00107Floor Support · corrodedCABIN FLOOR BEAM AT LBL27 BETWEEN FS1000.00 TO 1051.30 HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW FLOOR SECTION AT LBL27 BETWEEN FS1000.00 TO 1037.00 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND COMPLIED WITH SDR SWI2025F00106Stiffener · looseR/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE PULLED LOOSE (C-CHECK RO 1/29/2025) REPAIRED INNER SKIN COMMON TO ZED STIFFENER P/N CN624-2038-204 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-1687, REV. --, 2024-11-19 . COMPLIED WITH MAJOR REPAIR M-337 AND SKSDR SWI2025F00105Floor Support · corrodedCABIN FLOOR BEAM AT LBL9 BETWEEN FS1015.00 TO FS1051.30 HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 1/29/2025) REMOVED AND INSTALLED NEW FABRICATED FLOOR BEAM AND REPAIR PARTS AT LBL9 BETWEEN FS1015.00 AND FS1051.30 REF CRJ 700 SRM 53-00-41-2SDR SWIA2025013001Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 1/29/2025) INSTALLED 1 EA. NEW A-BRACKET P/N CN624-2082-201 ON INBD. SIDE OF THE L/H UPPER TRANSCOWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3, AND COMPLIEDSDR SWIA20250130109Slat Track · worn* L/H WING LEADING EDGE SLAT TRACK 1-1 NOTED WEAR MARKS TWO PLACES. FLAGGED. MX # 29127834 . (C-CHECK RO 1/29/2025) REMOVED 2EA DAMAGE AT L/H WING LEADING EDGE SLAT TRACK 1-1 REF CRJ700 SRM 51-12-00-001-001-A01 AND PERFORMED REPAIR PER REO 670-57-42-18SDR SWI2025F00104Skin · dentedRH INBD FLAP, THE BOTTOM INBD SKIN HAS SEVERAL DENTS (MARKED) (C-CHECK RO 1/29/2025) RH I/B FLAP BOTTOM I/B SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-802, SHEET 1 AND 2. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED FSDR SWI2025F00103Skin · dentedLH INBD FLAP, THE BOTTOM INBD SKIN HAS SEVERAL DENTS (MARKED) (C-CHECK RO 1/29/2025) L/H I/B FLAP, BOTTOM I/B SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG 57-52-01-995-802, SHEET 1 AND 2. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED SDR SWIA202501300002Skin · dentedFS1015.00- 1031.00 STRG 23LH - 24LH, 2EA DENTS ON FUSELAGE EXTERIOR SKIN (MARKED) (C-CHECK RO 1/29/2025) DENT #1- LENGTH: 3.745", WIDTH: 0.854", DEPTH: 0.003". DENT #2- LENGTH: 3.670", WIDTH: 0.795", DEPTH- 0.002". USED CALIBRATED TOOL 101030TUC CAL DUESDR SWIA202501300001Skin · crackedRH TRU DOOR CUT OUT, THE LOWER AFT CORNER OF THE FUSELAGE SKIN HAS POSSIBLE CRACK IN THE RADIUS (MARKED) (C-CHECK RO 1/29/2025) VERFIFIED CRACK ON RH FWD LOWER FUSELAGE SKIN UNDER TRU DOOR CUTOUT. REMOVED FWD SKIN PANEL ADG AT RIGHT SIDE REF CRJ700 SRMSDR SWIA20250130104Skin · dentedEVALUATE DENT ON EXTERNAL AIRCRAFT EXTERNAL SKIN AT FASTENER ON STGR 25R, FS 549.00 - 533.00 (C-CHECK RO 1/29/2025) PERFORMED ALL STEPS REO 670-53-31-974 REV--DATED 202412-03 FOR REPAIR. COMPLIED WITH TASK CAD 51-900-1002-SKY. THIS REO REPAIR ADRESSES 2SDR SWI2025F00102Bracket · bentAFT CARGO DOOR FWD TRACK ASSY BRACKET (P/N CC670-38813-1) ATTACHED TO UPPER ROLLER GUIDE IS BENT (C-CHECK RO 1/29/2025) REMOVED AND REPLACED AFT CARGO DOOR FWD TRACK ASSY BRACKET (P/N CC670-38813-1). REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 5SDR SWI2025F00101Track · wornAFT CARGO DOOR FWD TRACK ASSY LOWER ROLLER GUIDE HAS WEAR ALONG UPPER EDGE. MARKED (C-CHECK RO 1/29/2025) REMOVED AND REPLACED LOWER FWD. ROLLER GUIDE P/N CC670-38809-1SB. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWSDR SWI2025F00100Track · wornAFT CARGO DOOR FWD TRACK ASSY UPPER ROLLER GUIDE HAS WEAR ALONG LOWER EDGE. MARKED (C-CHECK RO 1/29/2025) REMOVED AND REPLACED UPPER FWD. ROLLER GUIDE P/N CC670-38810-1SB. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWSDR SWI2025F00099Track · wornAFT CARGO DOOR AFT TRACK ASSY LOWER ROLLER GUIDE HAS WEAR ALONG UPPER EDGE. MARKED (C-CHECK RO 1/29/2025) REMOVED AND REPLACED AFT CARGO DOOR AFT TRACK ASSY LOWER ROLLER GUIDE P/N CC670-38811-1. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-2SDR SWI2025F00098Skin · dentedEVALUATE 2EA DENTS ON EXTERNAL AIRCRAFT EXTERNAL SKIN, FS 501.00 - 517.00, STGR 25R - 26R (C-CHECK RO 1/29/2025) DRESSED BACK 2EA DENTS ON EXTERNAL AIRCRAFT SKIN AT FS501-FS517 STGR 25R-26R AND ADDRESSED PREVIOUS BLEND OUT PER REO 670-53-31-975 REV -- DSDR SWI2025F0000098Skin · dentedEVALUATE 2EA DENTS ON EXTERNAL AIRCRAFT EXTERNAL SKIN, FS 501.00 - 517.00, STGR 25R - 26R (C-CHECK RO 1/29/2025) DRESSED BACK 2EA DENTS ON EXTERNAL AIRCRAFT SKIN AT FS501-FS517 STGR 25R-26R AND ADDRESSED PREVIOUS BLEND OUT PER REO 670-53-31-975 REV -- DSDR SWIA20250130102Skin · dentedRHS OF FWD. FUSELAGE AT APPROXIMATELY FS202, ABOVE WL79.50, (ABOVE RVSM RED CORNER MARKING), THE SKIN APPEARS TO BE DENTED. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK RSDR SWIA2023062200019Windshield · crackedTRANSFER FROM EAML 1159516 : L WSHLD HEAT CAUTION MESSAGE IN FLIGHT. QRH COMPLETED AND MESSAGE CLEARED. L WSHLD HEAT CAUTION MESSAGE REAPPEARED. (FLT 3292 FILED CLOSED)REMOVED AND REPLACED LEFT WINDSHIELD IAW AMM 30-42-09 AND TASK CARD 56-220-1000-SKYSDR SWIA202301167115Windshield · crackedRIGHT WINDSHIELD OUTER LAYER CRACKED. REMOVED AND REPLACED RH WINDSHIELD IAW AMM 56-11-01. PERFORMED PRESSURIZE AND DEPRESSURIZE OF THE AIRCRAFT FOR MAINTENANCE IAW AMM 21-31-00. NO LEAKS FOUND , AIRCRAFT OK TO RETURN TO SERVICE.SDR SWIA202266442None · burnedD; DURING ARRIVAL WITH APU RUNNING FOR ASE, APU FAULT CAUTION MSG DISPLAYED FOLLOWED BY APU FIRE WARNING FOR A FEW SECONDS, WHICH DISAPPEARED SOON. THEN APU PUMP CAUTION DISPLAYED. RAN QRH AND SHUTDOWN APU IN THE AIR. / C; MEL 49-10-1A / CAT C DUE 9/16/22 / **
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