N724SK

Service difficulty reports · 119

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 = 'N724SK' 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 SWIA2026041475690Heater · odorPASSING THROUGH FL350 WE SMELLED A BURN IN SMELL SHORTY AFTER RECEIVED A L WSHLD HEAT CAUTION MESSAGE ALSO OBSERVED SMOKE (FLIGHT 6364) FOR CORRECTIVE ACTION PLS SEE CAMP 32077598.Apr 14, 2026 · N724SK · Cndair CL6002C10 · Windshield/Door Rain/Ice RemovalSDR SWIA2026041475689Windshield · cracked2 FOOT LONG CRACK IN THE LEFT WINDSHIELD (FLIGHT 6364) REMOVED AND REPLACED CA SIDE WINDSHEILD IAW AMM 53-12-01.Apr 14, 2026 · N724SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2024061300002A/C Pack · smokeDURING CLIMB TO CRUISE, R PACK AUTOFAIL, THEN R PACK TEMP. COMPLIED WITH QRH, SHUT DOWN R PACK, REMAINED BELOW 31,000 FT. ON FINAL TO DESTINATION, SMELL AND SIGHT OF SMOKE WAS OBSERVED BY FLIGHT ATTENDANTS, THEN AFTER LANDING, L PACK AUTOFAIL, L PACK TEMP, FOLJun 12, 2024 · N724SK · Cndair CL6002C10 · Cabin Cooling SystemSDR SWIA20230817Unknown · corrodedCAP ANGLE (MID) SILL CORRODED BETWEEN FS310-FS349 (C-CHECK RO 9/13/2023) CAP ANGLE SILL FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED CAP ANGLE REF DRAWING SH670-31810 REV AE, CRJ700 SRM 51-41-00-001-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-90Aug 17, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20230816Unknown · crackedCRACK FOUND AT GUSSET COMMON TO FLOOR SUPPORT ANGLE LBL12 FS280 (C-CHECK RO 9/13/2023) INSTALLED NEW GUSSET AT L/H COCKPIT FLOOR ANGLE AT LBL12.0 FWD OF FS 280.0 REF CRJ700 SRM 51-42-06-001-001-A01 AND DRWG CC670-33052 REV. -G. COMPLIED WITH SKY WEST TCAug 16, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20230814Unknown · crackedCRACK FOUND AT FLOOR SUPPORT ANGLE LH COCKPIT FLOOR BEAM LBL12 FS259 - FS280 (C-CHECK RO 9/13/2023) REPLACED THE FLOOR ANGLE AT L/H COCKPIT FLOOR BEAM AT BL12.0 FS 280.0 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV.-G. COMPLIED WITH SKY WAug 14, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20230811Unknown · crackedCRACK FOUND AT FLOOR SUPPORT ANGLE RH COCKPIT FLOOR BEAM RBL12 FS259 - FS280 (C-CHECK RO 9/13/2023) REPLACED CRACKED FLOOR ANGLE AT RIGHT-HAND COCKPIT FLOOR BEAM AT BL 12.0, FS280.0, WITH NEW FLOOR ANGLE. REF. CRJ700 SRM 53-11-43-201-003-A01 (TYPE -IV) Aug 11, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2023F00373Unknown · crackedR/H COCKPIT FLOOR BEAM AT BL12.0 CRACKED IN LOWER RADIUS AT FS 280.0 (C-CHECK RO 9/13/2023) PERFORMED A SPLICE REPAIR TO REMOVE DAMGED FLOOR BEAM BY REMOVING CRACKED FLOOR ANGLE AT R/H COCKPIT FLOOR BEAM AT BL12.0 FS 280.0 REF CRJ700 SRM 51-42-06-001-00Aug 1, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202300801Unknown · crackedL/H COCKPIT FLOOR BEAM AT BL12.0 CRACKED IN LOWER RADIUS AT FS 280.0 (C-CHECK RO 9/13/2023) PERFORMED A SPLICE REPAIR TO REMOVE DAMAGED FLOOR BEAM BY REMOVING CRACKED FLOOR ANGLE AT L/H COCKPIT FLOOR BEAM AT BL12.0 FS 280.0 REF CRJ700 SRM 51-42-06-001-0Aug 1, 2023 · N724SK · Cndair CL6002C10 · Fuselage Floor PanelSDR SWIA20230730Unknown · corrodedPAX DOOR CLIP COMMON TO INTERCOSTAL DD5 ON THE AFT SIDE OF FRAME 338 IS CORRODED (C-CHECK RO 9/13/2023) FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED PAX DOOR CLIP COMMON TO INTERCOSTAL DD5 ON THE AFT SIDE OF FRAME 338 IAW CRJ700 SRM 51-42-06-001-001-Jul 30, 2023 · N724SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2023F00372Unknown · gouged* EXTERNAL SKIN UNDER ADF ANTENNA HAS GOUGED AREAS, MARKED. (C-CHECK RO 9/13/2023) COMPLIED WITH MHIRJ REO 670-53-31-803, REV --, 2023-08-07, DISPOSITION STEPS 1 THRU 5. GOUGE DAMAGE COMPLETELY REMOVED REF CRJ700 SRM 51-12-00-001-001-A01. NDT - THICKNESJul 29, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2023010729Unknown · corroded* EXTERNAL SKIN UNDER ADF ANTENNA HAS AREAS OF CORROSION, MARKED. (C-CHECK RO 9/13/2023) COMPLIED WITH MHIRJ REO 670-53-31-803, REV --, 2023-08-07, DISPOSITION STEPS 1 THRU 5. CORROSION COMPLETELY REMOVED REF CRJ700 SRM 51-21-06-001-001-A01. NDT - THICKJul 29, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2023F00376Unknown · crackedR/H UPPER TRANSCOWL A-BRACKET CRACKED (C-CHECK RO 9/13/2023) REMOVED DAMAGED STAND-OFF ANGLE (A-BRACKET) & INSTALLED NEW STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. A, 2017-05-11. COMPLIED WITH SKY CARD 51-900Jul 26, 2023 · N724SK · Cndair CL6002C10 · Nacelle/Pylon StructureSDR SWI2023F00375Unknown · chafedR/H UPPER TRANSCOWL COAMING CHAFED THROUGH DISHING AND SKIN (C-CHECK RO 9/13/2023) REPAIRED R/H UPPER TRANSCOWL REF MHIRJ REO 670-54-21-1207 REV A 2015-08-27, AND REO670-54-21-1567 REV -- 2023-07-31.COMPLIED WITH SKYCARD 51-900-1002Jul 26, 2023 · N724SK · Cndair CL6002C10 · Nacelle/Pylon StructureSDR SWI2023F00374Unknown · corrodedSUPPORT ANGLE COMMON TO INTERCOSTAL DD4 AND AFT FORMER AT FS347 IS CORRODED (C-CHECK RO 9/13/2023) FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED PAX DOOR SUPPORT ANGLE COMMON TO INTERCOSTAL DD4 AND AFT FORMER AT FS347 IAW CRJ700 SRM 51-42-06-001-001-AJul 26, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20230726Unknown · crackedLEFT OVERWING APRON HAS SIGNS OF FRETTING. (C-CHECK RO 10/29/2023) REMOVED FRETTING AT LEFT OVERWING APRON REF CRJ200 SRM 51-12-00. AREA WAS BLENDED AND NDT PER REO 601R-53-41-341 REV C DATE 2009-JUN-10 PERMANENT REPAIR (REF ITEM 1A AND 2A), FROM FS 516.8Jul 26, 2023 · N724SK · Cndair CL6002C10 · Nacelle/Pylon StructureSDR SWI2023F00371Unknown · crackedPAX DOOR INTERCOSTAL DD1 BETWEEN FS347.250 & 338.963 IS CRACKED ON THE TOP FLANGE (C-CHECK RO 9/13/2023) REMOVED AND REPLACED INTERCOSTAL DD1 LOCATED BETWEEN FS347 & FS338 IAW CRJ700 SRM 51-42-06-001-001-A01 & DWG 601R31702 REV -N, COMPLIED WITH 51-900-Jul 24, 2023 · N724SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2023F00370Unknown · unknownPAX DOOR AFT FORMER, HAS A PREVIOUS REPAIR WITH CUT OUT AND OVER SIZED FASTENERS NOT COMMON TO NEW INNER SKIN (C-CHECK RO 9/13/2023) REMOVED AND REPLACED PAX DOOR AFT FORMER IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, & DWG 601Jul 24, 2023 · N724SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2023F00369Unknown · corrodedFLOOR BEAM LBL9 FROM FS1015 TO 1069.75 HAS SIGNS OF CORROSION. (C-CHECK RO 9/13/2023) PERFORMED SPLICE REPAR TO LBL.9 FLOOR BEAM FROM APROX FS.977-1069 REF CRJ 700 SRM 53-00-41-201-001-001-A01 FIG.53-00-41-991-803 , DWG MM670-35301 REV.H AND REO 670-53-Jul 24, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2023F00368Unknown · corrodedFLOOR BEAM LBL27 FROM FS1000 TO 1047 HAS SIGNS OF CORROSION. (C-CHECK RO 9/13/2023) REMOVED DAMAGED FLOORBEAM SECTION, FABRICATED AND INSTALLED ALL REPAIR PARTS FROM FS977 TO FS 1057. REF: CRJ-700 SRM 51-40-11-001-001-A01. M-337 AND SKYWESTTASK CARD 51Jul 24, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2023F00367Unknown · corrodedFLOOR BEAM RBL9 FROM FS1015 TO 1069.75 HAS SIGNS OF CORROSION. (C-CHECK RO 9/13/2023) REMOVED CORROSION FROM FLOOR BEAM AT FS1015.00 TO FS1069.75, RBL9 AND EVALUATED AS OUT-OF-LIMITS. REPAIRED FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01 REV 38 DATEDJul 24, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA20230000724Unknown · corrodedPAX DOOR INTERCOSTAL DD4 BETWEEN FS347.250 & 338.963 IS CORRODED ON THE TOP FLANGE (C-CHECK RO 9/13/2023) FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 BETWEEN FS347.250 & 338.963 IAW CRJ700 SRM 51-42-06-001-001-A01 & DWG 601RJul 24, 2023 · N724SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2023F0000367Unknown · corrodedFLOOR BEAM RBL9 FROM FS1015 TO 1069.75 HAS SIGNS OF CORROSION. (C-CHECK RO 9/13/2023) REMOVED CORROSION FROM FLOOR BEAM AT FS1015.00 TO FS1069.75, RBL9 AND EVALUATED AS OUT-OF-LIMITS. REPAIRED FLOOR BEAM IAW CRJ 700 SRM 53-00-41-201-001-A01 REV 38 DATEDJul 24, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2023F00351Unknown · wornPAX DOOR PIANO HINGE - DOOR SIDE - TOP PORTION - SURFACE AREA PRIOR TO FIRST LUG, LUGS 1-5, AND LUGS 15-27 ALL DISPLAY SOME AMOUNT OF WEAR, SCRATCHES, OR GOUGES (C-CHECK RO 9/13/2023) FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED PAX DOOR PIANO HINGEJul 20, 2023 · N724SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWI2023F00356Unknown · eroded*R/H INBD FLAP VANE LOWER EXTERNAL SKIN ERODED BETWEEN FLS15-FLS46 (MARKED) (C-CHECK RO 9/13/2023) REMOVED AND INSTALLED NEW FLAP LEADING EDGE VANE LOWER SKIN P/N CC670-14012-6. REF CRJ700 SRM 51-42-10-001-001-A01 AND BOMBARDIER DWG CC670-14010 REV F. Jul 19, 2023 · N724SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWI2023F00355Unknown · corroded*CORROSION NOTED AT MOUNTING POINT FOR BONDING JUMPER AT R/H INBD FLAP UNDER PANEL #648BB (MARKED) (C-CHECK RO 9/13/2023) COMPLIED WITH BLEND OUT REPAIR OF R/H INBD FLAP RIB P/N CC670-14086-8. REF. MHIRJ REO 670-57-52-540, REV. --, DATED 2023-08-22. M-3Jul 19, 2023 · N724SK · Cndair CL6002C10 · Wing System WiringSDR SWI2023F00354Unknown · unknown*DENT NOTED ON R/H INBD FLAP LOWER EXTERNAL SKIN AT APPROX. FLS33 AND 3" FROM T/E (MARKED) (C-CHECK RO 9/13/2023) PERFORMED AND COMPLIED WITH INBOARD FLAP LOWER SKIN REPAIR IAW ALL STEPS OF CRJ700 SRM 57-52-01-201-005-A01 SPLICE REPAIR FIGURE 57-52-01-9Jul 19, 2023 · N724SK · Cndair CL6002C10 · Trailing Edge FlapsSDR SWI2023F00366Unknown · corrodedCENTER FUSELAGE FS813.7 RIGHT ANGLE SILL CORROSION (C-CHECK RO 9/13/2023) COMPLIED WITH REO 670-53-41-632-REV-- DATED 2023-07-27 STEP 1 ENSURE BLENDING CORROSION DAMAGE IS SMOOTH CONTOUR, COMPLETE DAMAGE REMOVED, MINIMUM REMAINING THICNESS IS NOT LESS TJul 18, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2023F00365Unknown · corroded* STRINGER 20R AT APPROX. FS 364.00 TO FS 379.00 IS CORRODED. (C-CHECK RO 9/13/2023) COMPLIED WITH A SPLICE REPAIR PER REO 670-53-21-2310 REV -- DATED 2023-08-23, ALL STEPS CW. COMPLIED WITH TC 51-900-1002-SKY. PRESSURE CHECKED GOOD.Jul 18, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWI2023F00364Unknown · corrodedAFT BAGGAGE BAY UNDER FLOOR SKIN CORROSION FS1069.75-FS1088.2 STGR24LH-STGR25LH (MARKED) (C-CHECK RO 9/13/2023) REPAIRED SKIN CORROSION AT FS1069.75-FS1088.2 STGR24LH-STGR25LH REF. REO 670-53-61-2152 REV -- DATED 2023-08-12. SEE CONTINUATION CARD FOR WOJul 18, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2023F00363Unknown · corroded* INTERCOSTAL AT APPROX. FS 319.00 AND STGR 20L IS CORRODED. (C-CHECK RO 9/13/2023) INSTALLED NEW INTERCOSTAL P/N SH670-31822-1 AT STGR 20L BETWEEN FS310 - FS333. REF: CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, DWG SH670-31810, REJul 18, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2023071118Unknown · corroded* FRAME AT FS295.00 HAS AREAS OF CORROSION AT APPROX. STGR 27 AND BETWEEN STGR 23L AND 24L. (C-CHECK RO 9/13/2023) BLENDED AND EVALUATED F.S 295 FRAME STRG 27 AND BETWEEN STGR 23L AND 24L, LOCATIONS WERE FOUND TO BE WITHIN ALLOWABLE LIMITS. FOUND ADDITIJul 18, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI2023F00360Unknown · corroded* COCKPIT FLOOR BOARD SUPPORT ANGLE CONNECTED TO FS 280.00 BEAM IS CORRODED. (C-CHECK RO 9/13/2023) REMOVED REPLACED FLOOR SUPPORT ANGLE PN CC670-34095-1SB PER CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-06-001-001-A01, DWG CC670-33052 REV -G, CJul 17, 2023 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2023F00361Unknown · crackedLH WING INTERNAL TANK SLAT TRACK CANISTER 1-3 HAS POSSIBLE A CRACK IN MOUNTING FLANGE AS MARKED (C-CHECK RO 9/13/2023) REPAIRED LH WING TANK SLAT CANISTER REF. REO N0. 670-57-42-577, REV-- DATED 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAKJul 13, 2023 · N724SK · Cndair CL6002C10 · Wing StructureSDR SWIA20230701Unknown · corrodedPAX DOOR - SURROUND STRUCTURE - SILL CORRODED BTWN FS'S 310/349 (C-CHECK RO 9/13/2023) REMOVED AND REPLACED PAX DOOR LOWER KICK PLATE REF DRAWING SH670-31810 REV AE CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01. OPS CHECK GOOD AT THISJul 1, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2023F00362Unknown · groovedPILOTS SEAT INBOARD RAI SEAT ISL GROOVED (C-CHECK RO 9/13/2023) REMOVED & REPLACED PILOTS SEAT INBOARD RAIL REF. CRJ700 SRM 51-42-21-001-001-A01 & DWG CC670-40010 REV-B. COMPLIED WITH ALL STEPS OF REO 670-53-11-1877 REV. -- DATED 2023-08-23 REF. CRJ700 Jun 29, 2023 · N724SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2023060129Unknown · damagedCOPILOTS SEAT INBOARD RAIL IS GROOVED (C-CHECK RO 9/13/2023) COPILOT'S I/B SEAT RAIL EXCEEDS MAXIMUM ALLOWABLE DIMENSION OF .290". ACTUAL DIMENSION .303". CALIPER USED: TUC9237, CAL: 19-JUL-22, DUE: 31-JUL-23. OUT OF LIMITS REF CRJ700 SRM 53-11-49-101-0Jun 29, 2023 · N724SK · Cndair CL6002C10 · Fuselage, Powerplant Attach FittingsSDR SWIA20230421Unknown · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA74228-670-53-21-2167 N724SK MXCODEID59543-PR - ONE BURN MARK ON FUSELAGE SKIN LOCATED .25" FROM RIVET ON STGR-5L AFT OF FS295. BURN MARK IS .023" DEEP. REO. 670-53-21-2167 REV --, DATED 2021-10-14. COMPLIED WITH TEMPOApr 21, 2023 · N724SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202266148None · delaminatedREMOVAL OF RH SIDE WINDOW REQUIRED DUE TO DELAMINATION (FILED CLOSED) REMOVED RH SIDE WINDOW AS REQUIRED. REFERENCE APPLICABLE STEPS IN AMM 56-12-01Jul 24, 2022 · N724SK · Cndair CL6002C10 · Window/Windshield SystemSDR SWIA202266147None · delaminatedD: PLEASE REPLACE FIRST OFFICER'S WINDOW AT NEXT MX BASE OVERNIGHT VISIT IF PARTS ARE AVAILABLE DUE TO FWD UPPER CORNER DELAMINATION NEARING MX ALLOWABLE LIMIT OF 4 INCHES PER CRJ700 AMM 56-12-01-210-801 , TO AVOID IN SERVICE MAINTENANCE INTERRUPTION. / C: MCIJul 23, 2022 · N724SK · Cndair CL6002C10 · Window/Windshield SystemSDR SWIA202162752None · damagedFOUND DAMAGE TO PAX DOOR INNER SKIN AT DOOR ASSIST MOTOR PULLEY ON AFT SIDE OF DOOR TO BE OUT OF LIMITS PER SRM 52-11-01, THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR PER GMM 3-26. SEE CP 23892009 FOR DETERMINATION OF MAJOR OR MINOR REPAIR. (FILED - CLOSEDNov 24, 2021 · N724SK · Cndair CL600* · Fuselage Structure (General)SDR SWIA202161791None · damagedDAMAGE AREA AT FS 677.00 €“ 693.00, STR 3L-4L HAS EXCESSIVE MATERIAL BLENDED FROM THE AREA. THE DIMENSIONS OF THE BLENDED AREA ARE 1.8€? LONG, 2.3€? WIDE, AND .045€? DEEP. (FILE - CLOSED) COMPLIED WITH DOUBLER REPAIR TO FUSELAGE SKIN BETWEEN FS677.00-Oct 16, 2021 · N724SK · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA2019091946334Door Sill · corrodedFRAME AT FS 1051 AT RT FLOOR SILL HAS CORROSION. (C-CHECK) RO: 09/17/19 REMOVED CORROSION AT FS1051 AT RT FLOOR SILL AT THE SEAM OF THE CROSSBEAM. PERFORMED REPAIR IAW REO. NO FURTHER DEFECTS NOTED.Aug 21, 2019 · N724SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2019091946332Lug · gougedWING TRAILING EDGE - LT AILERON - NR 3 HINGE IB LUG - UPON AILERON REMOVAL - FOUND GOUGED. (C-CHECK) RO: 09/17/19 REMOVED GOUGE ON LT AILERON NR 3 HINGE IB LUG IAW REO.Aug 21, 2019 · N724SK · Cndair CL6002C10 · AileronsSDR SWIA2019091946333Door · gougedPAX DOOR, "PRESSURE VALVE" ICE BREAKER DOOR. IS GOUGE ON THE BACK-SIDE. (C-CHECK) RO: 09/17/19 BLENDED OUT DAMAGE ON PAX DOOR, "PRESSURE VALVE" ICE BREAKER DOOR. REMOVED AND INSTALLED NEW DOOR IAW AMM. ALL CHECKS GOOD.Aug 19, 2019 · N724SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA201642428Pin · chafedWHILE DOING HORIZONTAL PIVOT PIN LUBE TASK, FOUND PIN HAD ROTATED AND IS CHAFING THE TANG. PERFORMED REO REPAIR ON HORIZONTAL STAB PIVOT. REPAIRED IAW REO.Aug 9, 2016 · N724SK · Cndair CL6002C10 · Horizontal Stabilizer StructureSDR SWIA201642141Door · damagedPERFORM REPAIR TO PAX DOOR LINTEL, STR 3 AT FS 280. COMPLIED WITH ALL STEPS OF REPAIR OF PAX DOOR LINTEL AT F/S 280 ON STR 3 IAW REO. PERFORMED FUSELAGE PRESSURIZATION CHECK ON FUSELAGE COMMON TO THE REPAIRED AREA IAW AMM. PRESSURE CHECKED GOOD.Apr 21, 2016 · N724SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA201642140Frame · corrodedBS 319 LOWER FRAME CORRODED. REPAIRED IAW REO.Apr 8, 2016 · N724SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201642139Frame · corrodedBS 310 LOWER FRAME CORRODED. REPAIRED THE FRAME IAW REO.Apr 8, 2016 · N724SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA201642138Frame · corrodedBS 349 LOWER FRAME CORRODED OUT OF LIMITS. REMOVED AND INSTALLED NEW LOWER FRAME SECTION AT BS 349 FROM STR 23L TO 24R IAW SRM.Apr 8, 2016 · N724SK · Cndair CL6002C10 · Fuselage Main, Frame
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