N804SK

Service difficulty reports · 289

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 = 'N804SK' 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 SWIA2026081976927Elevator · faultedELEVATOR SPLIT CAUTION MESSAGE CAME ON IN FLIGHT. HAS STAYED ON AFTER ENGINE SHUTDOWN. REF CP 32892245 FOR LT ELEVATOR POSITION TRANSMITTER, R & R IAW CP 32882985 FOR LT FOR NR 2 ELEVATOR PCU REPLACEMENT. REF CP 32882986 FOR LT NR 3 ELEVATOR PCU REPLACEMENT,Aug 19, 2026 · N804SK · Cndair CL6002D24 · Elevator Control SystemSDR SWIA2026063076356Warning Message · illuminatedRECEIVED A GEAR DISAGREE WARNING MESSAGE ON TAKEOFF AT AROUND 3000 FT AND 200 KNOTS. RIGHT MLG SHOWED IN TRANSIT. RAN QRH AND RETURNED TO FIELD. (FLIGHT 4130). THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 32557612 WITH THE FOLLOWING CORRECTIVE ACTION: REFERJun 30, 2026 · N804SK · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR SWIA2026062576311Warning Message · illuminatedGEAR DISAGREE AFTER BRINGING GEAR UP. LEFT GEAR AND NOSE CAME UP, RIGHT SIDE HAD BLANK INDICATION. AFTER QRH, ALL THREE GEAR SHOWED DOWN WITH GEAR HANDLE DOWN. (FLIGHT 4464).Jun 25, 2026 · N804SK · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR SWIA2025111400002Warning Message · illuminatedGEAR DISAGREE WARNING ON TAKEOFF WITH GEAR HANDLE SELECTED UP. ALL 3 GEAR STAYED DOWN AND LOCKED. RAN QRH AND RETURNED TO DEPARTURE POINT. (FLIGHT 4062) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31180672. REFERENCE CP 31182373 AND CP 31182349 FOR CNov 12, 2025 · N804SK · Cndair CL6002D24 · Landing Gear Door ActuatorSDR SWIA20251113002Landing Gear · faultedGEAR DISAGREE WARNING ON TAKEOFF WITH GEAR HANDLE SELECTED UP. ALL 3 GEAR STAYED DOWN AND LOCKED. RAN QRH AND RETURNED TO DEPARTURE POINT. OPEN.Nov 12, 2025 · N804SK · Cndair CL6002D24 · Landing Gear Retraction/Extension SystemSDR SWIA2025082500011Window · crackedLH PILOTS SIDE WINDSHIELD CRACKED DURING APU PRESSURIZATION RUNS (C-CHECK RO 8/21/2025) INSTALLED NEW LH SIDE WINDOW (PN:NP139322-13 SN: 25170H8031) REF CRJ900 AMM 56-12-01-400-801-A01 (OPS TEST AND LEAK TEST GOOD AT THIS TIME)Aug 11, 2025 · N804SK · Cndair CL6002D24 · Flight Compartment WindowsSDR SWIA2025082500720Attach Fitting · corrodedL/H ELEVATOR ATTACH FITTING LOCATED ON ELEVATOR L/E AT RIB# 13 WAS FOUND TO HAVE PITTING ON THE INNER SURFACE. THIS CONDITION WILL REQUIRE A FITTING CHANGE. (C-CHECK RO 8/21/2025) REMOVED & INSTALLED NEW #3 L/H ELEVATOR HINGE FITTING (PN AV670-24136-009Jul 20, 2025 · N804SK · Cndair CL6002D24 · Elevator StructureSDR SWIA2025082500624Door Frame · crackedFOUND CRACK UNDER RIGHT TRU DOOR LANDING. (C-CHECK RO 8/21/2025) INSTALLED REPAIR TO UPPER FLANGE ON SUPPORT INTERCOSTAL AT ELECTRONIC BAY FLOOR ON RIGHT TRU DOOR LANDINGCOMPLIED WITH THE ALL STEPS OF REO 690-53-11-2032 REV. --. DATED 2025-07-04.COMPLIEJun 24, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025082500610Frame · corrodedCORROSION ON FRAME F/S 613 BETWEEN STRG 18 R/H AND STRG 20 R/H (C-CHECK RO 8/21/2025) INSTALLED NEW FLANGE ANGLE(-1) FOR REPAIR ON FRAME F/S 613 BETWEEN STRG 18 R/H AND STRG 20 R/H IAW CRJ-900 SRM TASK 53-00-06-201-001-A03 FIGURE 53-00-06-991-881 (SHEEJun 10, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F01108Stringer · damagedPROVIDE ACCESS FOR F/S 645.FRAME REMOVAL BETWEEN STRG 20 R/H AND STRG 16 R/H FOR STRINGER REPAIR STRG 18 R/H FOR CAMP #30042715 JOB # HN00238242 (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED FRAME F/S 645 BETWEEN STRG 16 R/H AND FACTORY SPLICE AT STRG 2Jun 5, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWI2025F01107Intercostal · corrodedEXFOLIATED CORROSION FOUND ON PAX DOOR AFT INTERCOSTAL DD7. (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD7 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUJun 5, 2025 · N804SK · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2025082500605Intercostal · corrodedEXFOLIATED CORROSION FOUND ON PAX DOOR AFT INTERCOSTAL DD7 CLEAT. (C-CHECK RO 8/21/2025) REMOVED AN INSTALLED NEW PAX DOOR AFT INTERCOSTAL DD7 CLEAT IAW CRJ900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEJun 5, 2025 · N804SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025082500603Bracket · corrodedEXFOLIATED CORROSION FOUND ON BRACKET BETWEEN FWD INTERCOSTAL DD4 AND FORMER 311.75. (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW PAX DOOR BRACKET BETWEEN FWD INTERCOSTAL DD4 AND FORMER 311.75 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42Jun 3, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR SWIA2025082500601Frame · corrodedEXFOLIATED CORROSION FOUND ON BRACKET BETWEEN FRAME 338.963 AND AFT INTERCOSTAL DD6. (C-CHECK RO 8/21/2025) INSTALLED NEW PAX DOOR BRACKET BETWEEN FRAME 338.963 AND AFT INTERCOSTAL DD6. IAW. CRJ900 SRM 51-42-06-001-001-A01. AND DWG 601R31702 REV. N.COMPJun 1, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2025082500528Stringer · corrodedSTGR23R BETWEEN FS364-FS349 IS CORRODED (C-CHECK RO 8/21/2025) INSTALLED NEW STRINGER 23R BETWEEN FS333 AND FS379 P/N SH670-31380-1 REF CRJ 900 SRM 51-42-06-001-001-A01 USING DRAWING SH690-31350 REV M ,COMPLIED WITH 51-900-1002-SKY,PRESSURIZATION LEAK May 28, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2025082500515Attach Angle · corrodedCORROSION FOUND AT ATTACHMENT ANGLE 26R BETWEEN FS349 - FS364 30149114 (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW ATTACHMENT ANGLE 26R BETWEEN FS349 - FS364 REF CRJ-900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-21-001-001-A01 AND DWG SH670-3205May 15, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR SWI2025F01114Door Frame · crackedRIGHT TRU DOOR LANDING AFT LATCH CATCH CRACKED AS MARKED (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW RH TRU DOOR LANDING. P/N CC670-33151-6S REF CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-22-001-001-A01 REV 38 DATED JUL 25/2020 & REO 690-May 9, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025082500509Door Frame · crackedLEFT TRU DOOR LANDING AFT LATCH CATCH CRACKED AS MARKED (C-CHECK RO 8/21/2025) REPLACED L/H TRU DOOR LANDING IAW CRJ 900 SRM 51-42-06-001-001-A01, CRJ 900 SRM 51-42-13-001-001-A01. CRJ 900 SRM 51-42-22-001-001-A01. AND ACCOMPLISHED REO 690-53-11-2027 RMay 9, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025082500501Door Frame · damagedLAND 27 ON THE FUSELAGE SIDE HAS FURTHER DAMAGE FROM FURTHER PIN MIGRATION. (C-CHECK RO 8/21/2025) REMOVED AND EVALD DAMAGE ON THE PAX DOOR LAND 27 ON FUSELAGE SIDE. FOUND TO BE WITHIN LIMITS REF DWG SH670-31875 REV. G AND CRJ 900 SRM 52-11-01-201-007-AMay 1, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01115Hinge · chafedPASSENGER DOOR HINGE, ON FUSELAGE, HAS SCRATCHES/CHAFING IN LANDS 1 THRU 26. (C-CHECK RO 8/21/2025) REPAIRED DAMAGE ON PAX DOOR HINGE IN 19 SPOTS OF THE LUG LANDS FWD TO AFT (SPOTS 6-10, 12-25, MARKED) , FUSELAGE SIDE REF CRJ900 SRM 53-21-23-201-010-A01May 1, 2025 · N804SK · Cndair CL6002D24 · Fuselage, Door HingeSDR SWI2025F01105Transcowl · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/21/2025) INSTALLED L/H UPPER TRANSCOWL INBD "A" BRACKET (PN CN624-2082-201). REF REO 670-54-21-971 REV B DATED 2023-11-28. COMPLIED FULLY WITH SKYCARD 51-900-1002-SKY.Apr 29, 2025 · N804SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWI2025F01104Plate · corrodedDURING AUDIT OF 6YR TASK CARD 53-230-500(DETAILED INSPECTION OF THE GALLEY SERVICE DOOR (FORWARD) SURROUND STRUCTURE, ABOVE FLOOR, INTERNAL - FS319.70 TO FS349.00 (EES)) FOUND AFT LOWER JOINT PLATE AT FS 349.00 - WL 72.00 APPEARS TO BE CORRODED. (C-CHECK RApr 29, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01103Plate · corrodedDURING AUDIT OF 6YR TASK CARD 53-230-500(DETAILED INSPECTION OF THE GALLEY SERVICE DOOR (FORWARD) SURROUND STRUCTURE, ABOVE FLOOR, INTERNAL - FS319.70 TO FS349.00 (EES)) FOUND FWD LOWER JOINT PLATE AT FS 319.70 - WL 72.00 APPEARS TO BE CORRODED. (C-CHECK RApr 29, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01102Transcowl · crackedL/H LWR TRANSCOWL INBD A BRACKET IS CRACKED (C-CHECK RO 8/21/2025) INSTALLED L/H LWR TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.Apr 29, 2025 · N804SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWI2025F01101Transcowl · shearedR/H LOWER TRANSCOWL Z STIFFENER RIVETS ARE SHEARED (C-CHECK RO 8/21/2025) R/H LOWER TRANSCOWL INNER SKIN UNDER "Z" STIFFENER LOCATION HAS BEEN REPAIRED REF REO# 690-54-21-561, REV --, DATED 5/23/25. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED FULApr 29, 2025 · N804SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA2025082500429Transcowl · wornLEFT UPEPR TRANSCOWL FWD & AFT LATCH BEARING PADS ARE WORN THROUGH AND INTO UNDERLYING STRUCTURE. REPAIRED LT UPPER TRANS COWL FWD & AFT LATCH BEARING PADS IAW CRJ-900 51-42-06-001-001-A01 AND REO 690-54-21-564 REV -- DATED 2025-05-29. COMPLIED WITH ALL STEPSApr 29, 2025 · N804SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWI2025F01100Door · corrodedLEFT AFT EMER. EXIT DOOR HAS SPOTS OF CORROSION AROUND SCREW HOLE AT LOWER AFT END (MARKED). (C-CHECK RO 8/21/2025) REPAIRED CORROSION ON LH AFT EMER. EXIT DOOR AROUND SCREW HOLE AT LOWER AFT END. COMPLIED WITH ALL STEPS OF REO 690-52-21-200 REV A DATEDApr 28, 2025 · N804SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F01099Door · chafedLEFT FWD EMER. EXIT DOOR CHAFED ON LOWER AFT END (MARKED). (C-CHECK RO 8/21/2025) REMOVED DAMAGE ON FWD LH EMER DOOR LOWER AFT END REF CRJ900 SRM 51-12-00-001-001-A01. RESTORED FINISH. COMPLIED WITH ALL STEPS OF REO 690-52-21-197 REV -A DATE 2025-06-10Apr 28, 2025 · N804SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F01098Stringer · corrodedCORROSION ON STGR25R AS MARKED BETWEEN FS280.00 - FS295.00 (C-CHECK RO 8/21/2025) REMOVED STR 25R FROM FS280 TO FS333 REF CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND INSTALLED NEW STR 25R FROM FS280 TO FS333 REF CRJ-900 SRM 51-42-Apr 28, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2025082500428Structure · corrodedLH FWD EMER. EXIT DOOR HAS SPOTS OF CORROSION AROUND SCREW HOLE AT LOWER AFT END (MARKED). (C-CHECK RO 8/21/2025) COMPLIED WITH REPAIR TO LH FWD EMMER EXIT DOOR CORROSION AROUND SCREW HOLE AT LOWER AFT END REF REO 690-52-21-197 REV -A DATED 2025-06-10 CApr 28, 2025 · N804SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F01097Fitting · chafedPAX DOOR SURROUND STRUCTURE FWD MID LOCK PIN, SHOOT BOLT FITTING CHAFED. (C-CHECK RO 8/21/2025) REPAIRED PAX DOOR SURROUND STRUCTURE FORWARD MID LOCK PIN FITTING IAW REO 690-53-21-1971 REV-- DATED 2025-06-10. COMPLIED WITH ALL STEPS OF REO 690-53-21-19Apr 27, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01096Skin · gougedAVIONICS BAY DOOR SURROUND STRUCTURE EDGE SKIN GOUGED ON LH AFT SIDE (C-CHECK RO 8/21/2025) BLENDED AVIONICS BAY DOOR SURROUND STRUCTURE EDGE SKIN ON LH AFT SIDE REF. CRJ-900 SRM 51-12-00-001-001-A01 AND EVALUATED REF. CRJ900 SRM 53-21-01-101-006-A02. AApr 27, 2025 · N804SK · Cndair CL6002D24 · Electrical/Electronic Compartment DoorsSDR SWI2025F01095Stringer · corrodedCORROSION ON STGR 26R AT FS349.00 (C-CHECK RO 8/21/2025) REMOVED STR 26R FROM FS333 TO FS364 REF CRJ-900 SRM 51-42-06-001-001-A01 AND INSTALLED NEW STR 26R FROM FS333 TO FS364 REF CRJ-900 SRM 51-42-06-001-001-A01 AND DWG SH670-32050 REV J, COMPLIED WITHApr 27, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWI2025F01094Gusset · corrodedGUSSET ON THE AFT SIDE OF FS661+90 AT STR 19R IS CORRODED (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW GUSSET ON THE AFT SIDE OF FS661+90 AT STR 19R IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01 AND DWG SH690-39100 REV. GApr 27, 2025 · N804SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01093Former · corrodedPASSENGER DOOR FS329.41, DD5 AND DD6, FORMER CORRODED (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW PAX DOOR FORMER 329.41 BETWEEN INTERCOSTALS DD5 AND DD6 IAW CRJ900 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-10Apr 27, 2025 · N804SK · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWI2025F01092Floorbeam · corrodedSTR 18R IS CORRODED FS629 €“ 645 (C-CHECK RO 8/21/2025) COMPLIED WITH ALL THE STEPS OF THE REO 690-53-31-1023 REV -- DATE:2025-06-25 .INSTALLED HI-LITES AND SOLID RIVETS PER SRM, ENSURED HOLE SIZE ARE WITHIN SRM LIMITS, WET INSTALLED ALL PARTS, FILL GAApr 27, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F01091Stringer · corrodedSTR 24L IS CORRODED FS501 €“ 517 (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW STGR 24L BETWEEN FS501-FS517, PN: SH690-33207-3B. PER CRJ900 SRM TASK 51-42-06-001-001-A01 . AND DWG:SH690-33207 REV.A. AND DWG SH690-33200 REV. N SHEET1 COMPLIED WITH 51Apr 27, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWIA2025082500427Door Frame · corrodedCORROSION ON INTERNAL SURROUND STRUCTURE FWD AVIONICS BAY DOOR LANDING. REMOVED CORROSION ON INTERNAL SURROUND STRUCTURE FWD AVIONICS BAY DOOR LANDING. NOMINAL THICKNESS OF 0.120" REMAINING THICKNESS OF 0.110". MATERIAL LOSS OF 0.010" IS WITHIN LIMITS OF GApr 27, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F01112Floor Support · corrodedINTERNAL STRUCTURE, FLOOR BEAM RBL9 HAS CORROSION AND SCRATCHES BETWEEN FS1015 TO FS1088, HN00238047 (C-CHECK RO 8/21/2025) REMOVED FLOOR BEAM SECTION FROM F/S 1006 TO F/S 1088 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND INSTALLED NEW FLOOR BEAM SECTIOApr 26, 2025 · N804SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01111Floor Support · corrodedINTERNAL STRUCTURE, FLOOR BEAM LBL9 HAS CORROSION AND SCRATCHES BETWEEN FS1000 TO FS1088, HN00238046 (C-CHECK RO 8/21/2025) REMOVED AND INSTALLED NEW FLOOR BEAM SECTION FROM F/S 1006 TO F/S 1080 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND REO 690-53-61-Apr 26, 2025 · N804SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01110Floor Support · corrodedINTERNAL STRUCTURE, FLOOR BEAM LBL27 HAS CORROSION AND SCRATCHES BETWEEN FS1000 TO FS1088, HN00238044 (C-CHECK RO 8/21/2025) REMOVED FLOOR BEAM SECTION FROM F/S 977 TO F/S 1060 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND INSTALLED NEW (-16) FLOOR BEAMApr 26, 2025 · N804SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F01109Floor Support · corrodedRIGHT FLOOR SILL IS CORRODED FS280 €“ 319 (C-CHECK RO 8/21/2025) INSTALLED NEW R/H FLOOR SILL BETWEEN F/S 280 TO F/S 319 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-13-001-001-A01 AND DWG SH690-32170 REV. AD ,COMPLIED WITH 51-900-1002-SKApr 26, 2025 · N804SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025082500426Floorbeam · corrodedINTERNAL STRUCTURE, CROSS BEAM FS1031, BETWEEN LBL27 AND LBL9 HAS CORROSION, HN00238049 (C-CHECK RO 8/21/2025) INTERNAL STRUCTURE, CROSS BEAM FS1031, BETWEEN LBL27 AND LBL9 HAS CORROSION PERFORMED A REPAIR PER THE REO 690-53-61-1586 REV. --. DATED 20Apr 26, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F01090Door Frame · crackedRIGHT FORWARD OVERWING EMERGENCY EXIT DOOR FRAME IS CRACKED ON THE TOP WEB AT THE FORWARD MICROSWITCH TAB. (C-CHECK RO 8/21/2025) PERFORMED REPAIR ON R/H FORWARD OVERWING EMERGENCY EXIT DOOR FRAME ON THE TOP WEB AT THE FORWARD MICROSWITCH TAB IAW REO 6Apr 25, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025082500425Web · crackedLEFT FORWARD OVERWING EMERGENCY EXIT DOOR FRAME IS CRACKED ON THE TOP WEB AT THE FORWARD MICROSWITCH TAB. REPAIRED L/H FORWARD OVERWING EMERGENCY EXIT DOOR FRAME CRACK ON THE TOP WEB AT THE FORWARD MICROSWITCH TAB REF REO 670-52-21-103 REV -- DATED 2024-11Apr 25, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWIA2025082500419Shaft · dentedLEFT INBOARD FLAP, SECOND FROM INBOARD VANE ACTUATOR SHAFT HAS INDENT. (C-CHECK RO 8/21/2025) REMOVED INDENTATION ON LEFT INBOARD FLAP, SECOND FROM INBOARD VANE ACTUATOR SHAFT IAW CRJ700 SRM 51-12-00-001-001-A01 AND EVALUATED WITH IN LIMITS REF REO 67Apr 19, 2025 · N804SK · Cndair CL6002D24 · Trailing Edge Flap ActuatorSDR SWI2025F01113Skin · dentedRIGHT INBOARD FLAP, SECOND FROM OUTBOARD VANE ACTUATOR SHAFT HAS DENT. REMOVED INDENTATION ON RH INBOARD FLAP, SECOND FROM OUTBOARD VANE ACTUATOR SHAFT. FOUND TO BE STRUCTURALLY ACCEPTABLE PER REO 670-57-52-257 REV -A DATED 2024-08-20. SEE CONTINUATION CARDApr 19, 2025 · N804SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWIA2025082500418Skin · dentedEXTERNAL FUSELAGE FS394 @ APPROXIMATLY STG17L DENTED, HN235814 (C-CHECK RO 8/21/2025) INSTALLED REPAIR PARTS ON EXTERNAL FUSELAGE FS394 @ APPROXIMATLY STG17L REF CRJ 900 SRM 51-42-21-001-001-A01 AND REO 690-53-21-1979, REV --, DATED ON 2025-07-07,PRApr 18, 2025 · N804SK · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025082500416Drag Angle · crackedTHE RH VERTICAL FWD DRAG ANGLE IS CRACKED. (C-CHECK RO 8/21/2025) REPAIRED RH VERTICAL FORWARD DRAG ANGLE BY INSTALLING -3 DOUBLER ANGLE AND -4 ANGLE FILLER ON VERTICAL STABILIZER TO FUSELAGE FWD ATTACHMENT PER REF CRJ 900 SRM 55-31-00-201-001-A01. COMApr 16, 2025 · N804SK · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR SWI2025F01106Drag Angle · crackedTHE LH VERTICAL FWD DRAG ANGLE IS CRACKED. (C-CHECK RO 8/21/2025) REPAIRED LH VERTICAL FORWARD DRAG ANGLE BY INSTALLING -1 DOUBLER ANGLE AND -2 ANGLE FILLER ON VERTICAL STABILIZER TO FUSELAGE FWD ATTACHMENT PER REF CRJ 900 SRM 55-31-00-201-001-A01. COApr 16, 2025 · N804SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure
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