N800SK

Service difficulty reports · 325

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 = 'N800SK' 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 SWIA2026061476221Hydraulic Line · leakingHYD 1 LOW PRESS CAUTION AT CRUISE. QUANTITY 0 PERCENT PRESSURE 2700, 18 DEGREES C. RAN QRH THEN HAD HYD EDP 1A CAUTION MESSAGE AND RAN QRH, NO CHANGE. (FLIGHT 4024) FOUND PINHOLE IN HYD SYS NR 1 RETURN LINE IN MAIN LANDING GEAR NR1 WHEEL BIN. REPAIRED HYDRAUJun 14, 2026 · N800SK · Cndair CL6002D24 · Hydraulic System, MainSDR SWIA2025070100623Buttstrap · damagedREPAIR FS 280 LOWER BUTT-STRAP BETWEEN STR25L (C-CHECK RO 06/29/2025)PERFORMED REPAIR FS 280 LOWER BUTT-STRAP BETWEEN STR25L BY COMPLYING WITH REO 690-53-21-1936 REV-- DATED 2025-06-27, COMPLIED WITH 51-900-1002-SKY, LEAK CHECK PASSEDJun 23, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F00772Skin · chafedAFT FUSELAGE EXTERNAL LOWER SKIN PANEL CHAFED BETWEEN FS897 AND FS913 STR27 (MARKED). 30056481 (C-CHECK RO 06/29/2025)REPAIRED AFT FUSELAGE EXTERNAL LOWER SKIN PANEL CHAFED BETWEEN FS897 AND FS913 STR27 PER REO 690-53-51-467 REV-- DATE 2025-05-20. SEE CONTINUApr 29, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025070100429Skin · damagedLIGHTNING STRIKE BURN MARK ON THE SKIN BETWEEN FS661+16 AND FS661+32 BETWEEN STR 18R AND 19R. REPAIRED LIGHTNING STRIKE AT FUSELAGE SKIN BETWEEN FS661+16 AND FS661+32 BETWEEN STR 18R AND 19R. REMOVING ALL DAMAGE REF CRJ900 SRM 53-00-00-201-003-A03 AND CRJ90Apr 29, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025070100425Hinge · gougedMULTIPLE GOUGES ON THE PASSENGER DOOR PIANO HINGE(DOOR SIDE). CAMP # 30038062. (C-CHECK RO 06/29/2025)INSPECTED PASSENGER DOOR PIANO HINGE FOR MULTIPLE GOUGES. REMAINING THICKNESS OF LUG #1 IS 0.109" , REMAINING THICKNESS OF LUG #2 IS 0.113", REMAINING THICKNApr 25, 2025 · N800SK · Cndair CL6002D24 · Fuselage, Door HingeSDR SWIA2025070100415Skin · corrodedCORROSION ON EXTERNAL SKIN BETWEEN FS1031 - FS1051 STR26R - STR26L ( 29979184 ) (C-CHECK RO 06/29/2025)REPAIRED CORROSION ON EXTERNAL SKIN BETWEEN FS1031- FS1051, STR 26L REF REO 690-53-61-1558, REV:--, DATED 2025-04-21 AND CRJ900 SRM 51-21-06-001-001-A01, SEApr 15, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SWIA2025070200414Roller · wornLH SLAT TRACK 3-3 UPPER OUTBOARD AFT ROLLER WORN. REMOVED AND REPLACED LH SLAT TRACK 3-3 TOP OUTBOARD AFT ROLLER REF AMM 27-81-43-000-806-A01 AND 27-81-43-400-806-A01.Apr 14, 2025 · N800SK · Cndair CL6002D24 · Leading Edge DevicesSDR SWI2025F00774Beam · damagedLH INBOARD FLAP FLS 140.40 VANE ACTUATOR BEAM HAS ROLLER INDENTIONS (C-CHECK RO 06/29/2025)LH INBOARD FLAP FLS 140.40 VANE ACTUATOR BEAM PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. OPERATIONAL TEST PASSED. COMPLIED WITH M-337 ANDApr 9, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWI2025F00773Frame · corrodedCORROSION FOUND ON REINFORCING ANGLE OF FRAME FS549.00 BETWEEN STGR 17L AND 18L. (29947227). (C-CHECK RO 06/29/2025)REMOVED AND REPLACED CLEAT PN: SH670-33796-1 AT FS549 BETWEEN STGR 17 AND STGR 18 PER CRJ 900 SRMS 51-42-06-001-001-A01 AND 51-42-22-001-001-A0Apr 9, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA2025070100409Roller · damagedLH INBOARD FLAP FLS 24.0 VANE ACTUATOR BEAM HAS ROLLER INDENTIONS (C-CHECK RO 06/29/2025)LH INBOARD FLAP FLS 24.0 VANE ACTUATOR BEAM REPAIRED PER REO 670-57-52-257 REV -A DATED 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 AND TASK CARD 51-900-10Apr 9, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWI2025F00785Rod · damagedRH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 102.90. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR ROD AT APPROX FLS 102.90. REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. OPERATIONAL TEST PASSED. COMPLIED WITHApr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWI2025F00784Fitting · chafedRH FWD EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS CHAFFED. CAMP # 29942099. (C-CHECK RO 06/29/2025)PERFORMED BLEND OUT REPAIR ON RH FWD EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS. REF. REO 690-52-21-192 REV.-- DATED 2025-04-21. COMPLIED WITH TASK CARD Apr 8, 2025 · N800SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F00783Rod · groovedRH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 140.40. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR AT APPROX FLS 140.40 REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 AND TASK CAApr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWI2025F00782Rod · damagedRH INBD FLAP VANE ACTUATOR AT APPROX FLS 24.00 HAS A GROOVE ON THE ACTUATOR ROD. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR AT APPROX FLS 24.00 REPAIRED PER REO 670-57-52-257, REV -A, DATE 2024-08-20. WITHIN LIMITS. NO DEFECTS. COMPLIED WITH M-337 ANApr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWI2025F00781Frame · corrodedCORROSION FOUND ON FRAME FS533.00 BETWEEN STGR 17L AND 18L WEB PORTION AND ATTACHING FLANGE. (29941771) (C-CHECK RO 06/29/2025)PERFORMED SPLICE REPAIR ON FRAME FS533.00 BETWEEN STGR 17L AND 18L. REF CRJ-900 SRM 53-00-06-201-001-A03, CRJ-900 SRM 51-42-06-001-Apr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00780Rod · groovedRH INBD FLAP HAS GROOVE ON FLAP VANE ACTUATOR ROD AT APPROX FLS 65.50. (C-CHECK RO 06/29/2025)RH INBD FLAP VANE ACTUATOR ROD AT APPROX FLS 65.50 REPAIRED PER REO 670-57-52-257 REV-A DATE 2024-08-20. WITHIN LIMITS. OPERATIONAL TEST PASSED. COMPLIED WITH M-337 Apr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWI2025F00779Angle · corrodedANGLE FOR LH TIRE BURST PANEL 542AZ IS CORRODED. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED LH TIRE BURST PANEL 542AZ ANGLE REF CRJ900 SRM 51-42-21-001-001-A01 REVISION 38,DATED JULY 25/2020 AND DWG CC670-10320 REV FCOMPLIED WITH SKYWEST TASK CARD 51-900-100Apr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F00778Fitting · chafedRIGHT AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS CHAFFED. PERFORMED BLEND OUT REPAIR ON RH AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS. REF. REO 690-52-21-193 REV.-- ISSUED 2025-04-21.COMPLIED WITH TASK CARD 51-900-1002-SKY.Apr 8, 2025 · N800SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F00777Fitting · chafedLH AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS CHAFFED. CAMP # 29942073. (C-CHECK RO 06/29/2025)PERFORMED BLEND OUT REPAIR ON LH AFT EMERGENCY EXIT DOOR I/B AND O/B HOOK FITTINGS. REF REO 690-52-21-194 REV -- DATED 2025-04-21. COMPLIED WITH TASK CARD 51Apr 8, 2025 · N800SK · Cndair CL6002D24 · Emergency ExitsSDR SWI2025F00776Angle · corrodedANGLE FOR RH TIRE BURST PANEL 642AZ IS CORRODED. REMOVED AND REPLACED RH TIRE BURST PANEL 642AZ ANGLE REF CRJ 200 SRM 51-42-21-001-001-A01 AND DWG CC670-10320 REV. F. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOODApr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F00775Repair · crackedCRACK IN THE RADIUS OF THE REPAIR DOUBLER ON THE TRU BAY FLOOR, RIGHT SIDE UNDER THE ADG PUMP, AT FS193 .00 FRAME INBOARD AFT CORNER. REPLACED THE REPAIR DOUBLER ON THE RIGHT TRU BAY FLOOR. REF REO 670-53-11-509 REV-E DATE 2018-02-08.Apr 8, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2025070100408Track · damagedRH INBD FLAP HAS GROOVES ON THE VANE ACTUATOR CAM TRACKS AT APPROX FLS 102.90. REPAIRED RH INBD FLAP ON THE VANE ACTUATOR CAM TRACKS AT APPROX FLS 102.90 BY COMPLYING WITH ALL STEPS OF REO 670-57-52-259 REV -.Apr 8, 2025 · N800SK · Cndair CL6002D24 · Trailing Edge FlapsSDR SWIA2025070100407Frame · corrodedCORROSION ON FRAME IN MULTIPLE LOCATIONS AT FS613 BETWEEN STGR 26L AND STGR 26R. (C-CHECK RO 06/29/2025)PERFORMED FRAME FLANGE SPLICE REPAIR ON FS613 BETWEEN STRG27 AND STRG26R REF CRJ900 SRM 53-00-06-201-001-A03 AND CRJ-900 SRM 51-42-06-001-001-A01. COMPLIEApr 7, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00790Frame · corrodedCORROSION ON FRAME AT FS613 BETWEEN STGR 18L AND STGR 19L. (MARKED) (C-CHECK RO 06/29/2025)REMOVED CORRODED FRAME AT FS613- BETWEEN STGR18L AND STGR19L REF CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 INSTALLED NEW FRAME AT FS613- BETWEEN STGRApr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00789Frame Angle · corrodedCORROSION ON FRAME ANGLE AT APPROX FS645 STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)REMOVED AND REPLACED FRAME ANGLE/CLEAT PN SH670-33796-1 AT FS 645.00 STGR 18L PER CRJ900 SRMS 51-42-06-001-001-A01 AND 51-42-22-001-001-A01 USING DWG NO SH690-33750 REV AF. COApr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00788Frame · corrodedCORROSION ON FRAME AT FS661+32 BETWEEN STGR 18L AND STGR 19L. (MARKED) (C-CHECK RO 06/29/2025)REMOVED DAMAGE STUB FRAME AND INSTALLED NEW STUB FRAME AT FS661+32 BETWEEN STR 18L AND STR19L REF DWG# SH690-33750 REV: AF AND CRJ900 SRM 51-42-06-001-001-A01; 51-42Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00787Stringer · corrodedCORROSION ON STR 26R ATTACH FLANGE BETWEEN FS1015 €“ 1031 (C-CHECK RO 06/29/2025)REPAIRED CORROSION DAMAGE ON STR 26R ATTACH FLANGE BETWEEN FS1015 AND FS1031 BY COMPLETING ALL STEPS (1-13) OF REO 690-53-61-1555, REV --, DATED 2025-05-01. LEAK CHECK GOOD. SEApr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWI2025F00786Frame Angle · corrodedCORROSION ON FRAME ANGLE AT APPROX FS613 STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)PERFORMED FRAME SPLICE REPAIR PERCRJ900 SRM 53-00-06-201-001-A03, CRJ900 SRM 51-42-06-001-001-A01AND CRJ900 SRM 51-42-21-001-001-A01. SEE CONTINUE CARD FOR DETAILS. COMPLIED WApr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00799Door Sill · corrodedSERVICE DOOR SILL BOTTOM ANGLE HAS MULTIPLE LOCATIONS OF CORROSION. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED MOUNTING ANGLE IAW CRJ900 SRM 51-42-06-001-001-A01 AND DRAWING# SH670-31950, REV Y. AND REMOVED AND REPLACED 4 EA WEB FLOOR PROTECTORS ON SERVICE Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F00798Frame · corrodedCORROSION ON FRAME AT FS645 BETWEEN STGR 17L AND STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)REPLACED FRAME SECTION FS645 STGR16L-18L REF CRJ 900 SRM 53-00-06-201-001-A03 AND CRJ900 SRM 51-42-06-001-001-A01.SEE CONTINUE CARD FOR WORK PERFORMED. COMPLIED WITH Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00797Frame · corrodedCORROSION ON FRAME AT FS501 BETWEEN STGR 27 AND STGR 26L. (C-CHECK RO 06/29/2025)BLENDED OUT CORROSION ON FRAME FS501 BETWEEN STGR 27 AND 26L. FOUND WITHIN LIMITS. REF. REO 690-53-31-959 REV.-- ISSUED 2025-04-18.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKApr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00796Plate · corrodedFWD CARGO FWD H-PLATE ON OPEINING SILL HAS CORROSION AT APPROX FS517 STGR 24L .(MARKED) (C-CHECK RO 06/29/2025)BLENDED CORRODED AREA ON FWD CARGO FWD H-PLATE FS517 STGR 24L. REF CRJ-900 SRM 51-21-06-001-001-A01. COMPLIED WITH REO 690-53-31-960 REV -- DATE: 2Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F00795Floorbeam · corrodedAVIONICS BAY FLOOR SUPPORT ANGLE AT FS.280.00 CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 06/29/2025)REMOVED AND REPLACED WITH NEW AVIONICS BAY FLOOR SUPPORT ANGLE AT FS280.00 IAW CRJ900 SRM 51-42-06-001-001-A01 AND CRJ900 SRM 51-42-21-001-001-A01 AND DWApr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F00794Floor Support · corrodedRH FLOOR SILL IS CORRODED FS280 €“ 319 (C-CHECK RO 06/29/2025)REPAIRED RH FLOOR SILL CORROSION AT FS280-FS319 REF CRJ 900 SRM TASK 51-40-06-001-001-A01 , CRJ 900 SRM TASK 51-42-21-001-001-A01 , CRJ 900 SRM TASK 51-42-06-001-001-A01 , CRJ 900 SRM TASK 51-42-1Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWI2025F00793Floorbeam · corrodedLBL9 FLOOR BEAM IS CORRODED FS1031 (C-CHECK RO 06/29/2025)REPAIRED FLOOR BEAM NEW SECTION AT LBL 9.0 BETWEEN F/S 1025 TO F/S 1037 IAW CRJ 900 SRM 53-00-41-201-001-A03 AND CRJ 900 SRM 51-42-21-001-001-A01.COMPLIED WITH 51-900-1002-SKY.Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F00792Frame Angle · corrodedCORROSION ON FRAME ANGLE AT APPROX FS581 STGR 18L. (MARKED) (C-CHECK RO 06/29/2025)PERFORMED FRAME SPLICE REPAIR REF CRJ900 SRM 53-00-06-201-001-A03, CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01 AND BOMBARDIER DRAWING SH690-33100, REV N. Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWI2025F00791Frame · corrodedCORROSION ON FRAME AT FS581 BETWEEN STGR 27 AND STGR 26R. (C-CHECK RO 06/29/2025)REPAIRED CORROSION ON FRAME AT FS581 BETWEEN STGR 27 AND STGR 26R. CRJ900 SRM 53-00-06-201-001-A03 AND 51-42-06-001-001-A01. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARApr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWIA20250701406Stringer · corrodedCORROSION ON STGR 24R IN MULTIPLE LOCATIONS BETWEEN FS581 AND FS597. PERFORMED STRINGER SPLICE REPAIR AND INSTALLED ALL REPAIR PARTS AT STGR 24R BETWEEN FS565 AND FS661+32. REF. CRJ900 SRM 53-00-03-201-001-A02 FIGURE 53-00-03-995-806 SHEET 1, REO 690-53-31-95Apr 6, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR SWI2025F00806Floorbeam · crackedRBL12 FS280 CLIP IS CRACKED (C-CHECK RO 06/29/2025)REMOVED AND REPLACED CLIP P/N CC670-34099-2 AT RBL 12 FS,280 REF. CRJ900 SRM 51-42-21-001-001-A01 AND DWG# KBA670-30026 REV. J SHT 7. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2D24) STRUCTURAL MApr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F00805Floorbeam · corrodedCOCKPIT FLOOR BOARD SUPPORT ANGLE ON THE FWD SIDE OF FS280 IS CORRODED (C-CHECK RO 06/29/2025)FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED COCKPIT FLOOR BOARD SUPPORT ANGLE ON THE FWD SIDE OF FS280 REF DWG CC670-33052 REV G, CRJ900 SRM 51-42-21-001-001-A01Apr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F00804Door Sill · corrodedPAX DOOR LOWER SILL LOWER ANGLE HAS CORROSION IN MULITPLE LOCATIONS. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED NEW PAX DOOR LOWER SILL LOWER ANGLE REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG# SH670-31810 REV AE. LEAK CHECK GOOD. ( SEE CONTINUE CARD FOR WOApr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F00803Striker · chafedPAX DOOR SEAL STRIKER IS CHAFED AT FS310 APPROX STGR 9L. (C-CHECK RO 06/29/2025)REPAIRED PAX DOOR STRIKER REF CRJ 900 SRM 53-21-23-201-006-A01. SEE CONTINUE CARD FOR DETAILS.COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.Apr 5, 2025 · N800SK · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWI2025F00802Floorbeam · crackedLBL12 FS280 CLIP IS CRACKED (C-CHECK RO 06/29/2025)REMOVED AND REPLACED CLIP P/N CC670-34099-1 REF CRJ 900 SRM 51-42-21-001-001-A01 WITH DRAWING BA670-31057 REV -L FOR FASTENER CALL-OUT. COMPLIED WITH TASK CARD 51-900-1002-SKY, SEE CONTINUE CARD FOR WORK DETApr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SWI2025F00801Striker · corrodedSERVICE DOOR LOWER SEAL STRIKER HAS CORROSION AROUND MULTIPLE FASTENER HOLES. REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SEAL STRIKER REF CRJ900 SRM 51-42-06-001-001-A01, AND DRAWING SH670-31950, REV Y. LEAK CHECK GOOD. SEE CONTINUE CARD FOR MORE DETAILApr 5, 2025 · N800SK · Cndair CL6002D24 · Service DoorsSDR SWI2025F00800Fitting · chafedPAX DOOR FWD AND AFT CAM FITTINGS ON FUSELAGE SIDE ARE CHAFED. CHAFES FOUND TO BE OUT OF LIMITS REF RJ 900 SRM 53-21-23-101-001-A02 . INSTALLED NEW FWD AND AFT PAX DOOR CAM FITTINGS ON FUSELAGE SIDE IAW CRJ900 SRM 53-21-27-001-001-A01 AND CRJ900 SRM 51-42-21-Apr 5, 2025 · N800SK · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWIA2025070100405Door Frame · gouged4EA GOUGES ON UPPER PAX DOOR SURROUND AT APPROX STGR 4L BEHIND NUTPLATE BRACKETS. COMPLETED REO 690-53-21-1925 REV.--, DATED 2025-04-21 FOR GOUGE DAMAGE TO UPPER LINTEL DOUBLER ABOVE PAX DOOR BETWEEN FS333.00-FS337.50 AT STR 3L. (#3 DOUBLER BLEND). ENSURED GApr 5, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, StructureSDR SWI2025F00811Bracket · crackedL/H LWR TRANSCOWL OTBD "A" BRACKET IS CRACKED (C-CHECK RO 06/29/2025)REMOVED AND INSTALLED NEW L/H LWR TRANSCOWL O/B BRACKET REF REO# 670-54-21-971, REV B, DATED 11/28/23 AND CRJ900 AMM 78-33-03-400-801-A01. OPS CHECK GOOD AT THIS TIME. SEE CONTINUE CARD FORApr 4, 2025 · N800SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWIA2025070100404Transcowl · shearedL/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE SHEARED. REPAIRED LEFT UPPER TRANSCOWL AT SHEARED RIVETS ON INNER SKIN COMMON TO ZED STIFFENER, REF. REO 690-54-21-552, REV. --, COMPLIED WITH MAJOR REPAIR M-337, SKY CARD 51-900-1002-SKY.Apr 4, 2025 · N800SK · Cndair CL6002D24 · Engine Thrust ReverserSDR SWI2025F00810Structure · corrodedS/N 0462BETWEEN FS1069.75 AND FS1088.20 INTERNAL OF LH PYLON (LUNCH BOX), THEIRS A FUEL LINE THAT LEAKED AND AREA HAS CORROSION. FLAGGED (C-CHECK RO 06/29/2025)REMOVED CORROSION BETWEEN FS1069.75 AND FS1088.20 INTERNAL OF LH PYLON (LUNCH BOX) PER CRJ900 SRM Apr 3, 2025 · N800SK · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR SWI2025F00809Receiver · crackedS/N 0444EXTERNAL INSPECTION OF THE RH AFT FUSELAGE TRU BAY LATCH RECEIVER HAS A POSSIBLE CRACK. FLAGGED (C-CHECK RO 06/29/2025)REMOVED AND REPLACED RH TRU LATCH RECEIVER (LANDING PN CC670-33151-6) PER DWG CC670-33040 REV-G, CRJ 900 SRM 51-42-06-001-001-A01 REApr 3, 2025 · N800SK · Cndair CL6002D24 · Fuselage Main, Structure
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