# Service difficulty reports: N805SK A list on [N805SK](https://openairdocs.org/aircraft/N805SK.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 5 · 221 reports - [SDR SWIA202507170602](https://openairdocs.org/sdr/SWIA202507170602.md): Bushing · damaged · Jun 2, 2025 · N805SK · Cndair CL6002D24 · Engine Mount Section > PITTING ON INTERIOR LANDINGS OF LH ENGINE TIE BAR BUSHING OPENINGS 30245106 (C-CHECK RO 07/16/2025)REPAIRED PITTING ON INTERIOR LANDINGS OF THE LH ENGINE TIE BAR BUSHING OPENINGS REF CRJ900 SRM 51-21-06-001-001-A01, CRJ900 SRM 51-12-00-001-001-A01, DWG# CN624 - [SDR SWIA202507170529](https://openairdocs.org/sdr/SWIA202507170529.md): Landing · cracked · May 29, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RH TRU BAY LANDING HAS A CRACK NEXT TO THE ADG PUMP (C-CHECK RO 07/16/2025)REPAIRED THE CRACK ON THE RHS TRU BAY FLOOR PER CRJ900 SRM 53-11-43-201-001-A01 TYPE 2 PROCEDURE STEPS 1-4.A PARAS (C) THRU (N) FOR THE CRACK REPAIR ON THE RHS AT FS193.00 ELECTRICAL B - [SDR SWIA202507170525](https://openairdocs.org/sdr/SWIA202507170525.md): Beam · cut · May 25, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > WHILE PERFORMING INSTALLATION OF THE AFT CARGO BAY DOOR PROXIMITY SENSOR PX102, FOUND AFT BAGGAGE BAY STRUCTURE BEAM CUT INTO FROM AFT BALANCE SPRING CABLE CAUSING BROKEN STRANDS AND FOUND CARGO DOOR AFT LOWER PULLEY BROKEN AT APPROX. FS1000.00. (C-CHECK RO 0 - [SDR SWIA202507170509](https://openairdocs.org/sdr/SWIA202507170509.md): Stringer · corroded · May 9, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > UPON PROVIDING ACCESS TO FOM REMOVAL OF STGR24L FOUND CORROSION ON FS501 BETWEEN STGR25L-STGR24L. (C-CHECK RO 07/16/2025)REPLACED FRAME FS501 BETWEEN STGR 25L-STGR24L REF CRJ900 SRM 51-42-06-001-001-A01, CRJ900 SRM 51-42-20-001-001-A01, DWG SH690-33750 REV. A - [SDR SWI2025F00969](https://openairdocs.org/sdr/SWI2025F00969.md): Hinge · damaged · May 9, 2025 · N805SK · Cndair CL6002D24 · Ailerons > UPON THE REMOVAL OF THE L/H NO.1, INBOARD AILERON HINGE BUSHING. FOUND A RIDGE NEAR THE EDGE OF THE BORE. (C-CHECK RO 07/16/2025)REPAIRED THE L/H AILERON, NO.1 INBD HINGE BUSHING BORE REF REO 690-57-51-432 REV--A, DATED 2025-06-06 AND DWG# CC670-18002 REV-C, - [SDR SWIA202507170508](https://openairdocs.org/sdr/SWIA202507170508.md): Access Door · damaged · May 8, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > UPPON REMOVAL OF CRACKED R/H LWR LANDING FOR FWD AVIONICS BAY ACCESS DOOR 212AR FOUND ELONGATED FASTENERS HOLES AND MISSING PIECE OF INTERCOASTAL FLANGE AT FS.173. (C-CHECK RO 07/16/2025)REPAIRED ELONGATED FASTENER HOLES AND MISSING PIECE OF INTERCOSTAL FLA - [SDR SWI2025F00970](https://openairdocs.org/sdr/SWI2025F00970.md): Angle · corroded · May 7, 2025 · N805SK · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR KICKPLATE ANGLE HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 07/16/2025)REMOVED CORROSION IN MULTIPLE SPOTS ON PAX DOOR KICKPLATE ANGLE. REF: CRJ 900 SRM 51-21-06-001-001-A01 REMOVED AND INSTALLED NEW PAX DOOR KICKPLATE ANGLE REF CRJ900 SRM 51-42-06-0 - [SDR SWIA202507170507](https://openairdocs.org/sdr/SWIA202507170507.md): Angle · corroded · May 7, 2025 · N805SK · Cndair CL6002D24 · Passenger/Crew Doors > PAX DOOR MID CAP ANGLE HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 07/16/2025)REPLACED PAX DOOR MID CAP ANGLE REF CRJ900 SRM 51-41-02-001-001-A01 AND DWG SH670-31810 REV. AE. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. - [SDR SWIA202507170504](https://openairdocs.org/sdr/SWIA202507170504.md): Stringer · corroded · May 4, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > CORROSION FOUND ON STRINGER 26L BETWEEN FS 349.0 - FS 364.0. (C-CHECK RO 07/16/2025)REPLACED STRINGER 26L BETWEEN FS349.0-FS364.0 REF CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH670-31350 REV. A. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. - [SDR SWIA202507170422](https://openairdocs.org/sdr/SWIA202507170422.md): Hinge · damaged · Apr 22, 2025 · N805SK · Cndair CL6002D24 · Fuselage, Door Hinge > THE PAX DOOR HINGE ON THE DOOR SIDE AFT LUG UPPER PIN HOLE IS ELONGATED AND LUG IS GOUGED. (C-CHECK RO 07/16/2025)REPLACED PAX DOOR HINGE(DOOR SIDE) REF CRJ900 SRM 52-11-01-201-A01 AND DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. - [SDR SWIA202507170421](https://openairdocs.org/sdr/SWIA202507170421.md): Doubler · chafed · Apr 21, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin > THE FWD ATG ANTENNA ETERNAL DOUBLER WHERE ANTENNA ATTACHES IS CHAFED. (C-CHECK RO 07/16/2025)PERFORMED FWD ATG ANETNNA DOUBLER. REF CRJ900 SRM 51-40-06-001-001-A01, REF CRJ900 SRM 51-42-20-001-001-A01 AND PER GOGO D12938-20210 REV D. COMPLIED WITH TASK CARD - [SDR SWI2025F00949](https://openairdocs.org/sdr/SWI2025F00949.md): Housing · gouged · Apr 14, 2025 · N805SK · Cndair CL6002D24 · Cargo/Baggage Doors > AFT CARGO DOOR EXTERIOR HANDLE HOUSING IS GOUGED IN MULTIPLE AREAS. (C-CHECK RO 07/16/2025)REPLACED AFT CARGO DOOR EXTERIOR HANDLE HOUSING ASSY. REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG CC670-38702 REV. F. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. O - [SDR SWIA2025071700413](https://openairdocs.org/sdr/SWIA2025071700413.md): Floor Support · corroded · Apr 13, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AFT BAGGAGE DOOR FLOOR SILL INNER CHORD P/N MM670-35656-001 AND P/N MM670-35669-001 AND P/N MM670-35670-001 ARE CORRODED BETWEEN FS1000.00 - FS1051.30. ( MX 29971167) (C-CHECK RO 07/16/2025)REPAIRED DOOR FLOOR SILL INNER CHORD P/N MM670-35656-001 AND P/N MM6 - [SDR SWI2025F00971](https://openairdocs.org/sdr/SWI2025F00971.md): Door Frame · corroded · Apr 8, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > AVIONICS BAY DOOR SURROUND DOOR CUTOUT BETWEEN FS364.00 €“ FS394.00 AND STRGR25R €“ STGL25L HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 07/16/2025)REPAIRED AVIONICS BAY DOOR SURROUND CUTOUT BETWEEN FS360-FS394 AND STGR25R-STGR25L REF REO 690-53-21- - [SDR SWIA2025071700408](https://openairdocs.org/sdr/SWIA2025071700408.md): Door · cracked · Apr 8, 2025 · N805SK · Cndair CL6002D24 · Emergency Exits > R/H AFT EMERGENCY EXIT DOOR HAS CRACKED NEXT TO AFT HOOK FITTING (MARKED) (C-CHECK RO 07/16/2025)REPAIRED CRACK ON THE R/H AFT EMERGENCY EXIT DOOR, NEXT TO AFT HOOK FITTING REF REO 670-52-21-103 REV--, DATED 2024-11-06, COMPLIED WITH ALL STEPS. COMPLIED WITH - [SDR SWI2025F00953](https://openairdocs.org/sdr/SWI2025F00953.md): Frame · corroded · Apr 3, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Frame > CORROSION NOTED ON FRAME AT FS349.00, BTWN STRG27 AND STRG26R (C-CHECK RO 07/16/2025)REPLACED FS349.00 FRAME BETWEEN STRG27 AND STRG26R REF CRJ900 SRM 51-42-06-001-001-A01, AND DWG SH690-31350 REV. M. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. - [SDR SWIA202507170402](https://openairdocs.org/sdr/SWIA202507170402.md): Door Sill · gouged · Apr 2, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > PAX DOOR SURROUND LOWER SILL HAS MULTIPLE GOUGES ALONG THE LENGTH OF THE PART FROM APROX. FS.310.00 TO FS.349.00. REMOVED AND REPLACED NEW PAX DOOR SURROUND LOWER SILL BETWEEN FS 310.00 - FS 349.00 REF CRJ900 SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV - - [SDR SWI2025F00972](https://openairdocs.org/sdr/SWI2025F00972.md): Plate · bent · Apr 2, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > PLATE BENT FS661+74 STGR2627. REMOVED AND INSTALLED NEW FABRICATED PLATE AT FS661+74 REF. CRJ900 SRM 51-42-06-001-001-A01 AND DWG SH690-33600, REV. -AH. COMPLIED WITH 51-900-1002-SKY - [SDR SWI2025F00980](https://openairdocs.org/sdr/SWI2025F00980.md): Mount · corroded · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings > MACHINED MOUNT CORRODED FS565.00 STGR26L - 27. REMOVED AND REPLACED MACHINED MOUNT BRACKET P/N SH670-33389-2 AT FS565.00 BETWEEN STGR26L - 27 REF CRJ900 SRM TASK 51-42-22-001-001-A01, CRJ900 SRM TASK 51-42-20-001-001-A01, CRJ900 SRM TASK 51-45-00-001-001-A01 - [SDR SWI2025F00979](https://openairdocs.org/sdr/SWI2025F00979.md): Frame · corroded · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Frame > FRAME LOWER FLANGE CORRODED FS581.00 BETWEEN STGR26L - 26R. COMPLIED WITH REPAIR REO 690-53-31-970 REV -- DATE 2025-04-26 FOR CORROSION ON FRAME LOWER FLANGE FS581.00 STGR26L - 26R. COMPLIED WITH 51-900-1002-SKY NO WEIGHT CHANGE BLEND ONLY. - [SDR SWI2025F00978](https://openairdocs.org/sdr/SWI2025F00978.md): Nut Plate · corroded · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Emergency Exits > CORROSION NOTED AROUND NUTPLATE AT R/H FWD EMER DOOR LOWER STRUCTUE AT INNER AND OUTER SIDES. REPAIRED RH FWD EMER DOOR LOWER STRUCTURE AT INNER AND OUTER SIDES REF REO 690-52-21-189 REV.-- DATED 2025-06-07. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. - [SDR SWI2025F00977](https://openairdocs.org/sdr/SWI2025F00977.md): Angle · corroded · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Wing Miscellaneous Structure > ANGLE FOR RH TIRE BURST PANEL 642AZ IS CORRODED. REPLACED ANGLE FOR RH TIRE BURST PANEL 642AZ REF CRJ900 SRM 51-42-21-001-001-A01, DWG CC670-10320 REV. -F. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY AND 28-900-1000-SKY. SEE CONTINUATION FOR DETAILS. COMPL - [SDR SWI2025F00976](https://openairdocs.org/sdr/SWI2025F00976.md): Skin · ground damage · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Cargo/Baggage Doors > IMPACT DAMAGE NOTED AT CENTER BAG BAY DOOR INNER SKIN AT LOCATIONS. REPAIRED IMPACT DAMAGE ON CENTER BAG BAY DOOR INNER SKIN REF MHIRJ R.E.O. 690-52-35-517 REV.-- DATED 2025-05-19. COMPLIED WITH ALL STEPS, COMPLIED WITH 51-900-1002-SKY(CL600-2D24) STRUCTURAL - [SDR SWI2025F00975](https://openairdocs.org/sdr/SWI2025F00975.md): Stringer · corroded · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STGR24L BETWEEN FS501.00 - 517.00 IS CORRODED. (MARKED) (C-CHECK RO 07/16/2025)REPLACED STGR 24L BETWEEN FS501.00 - 517.00 REF REO 690-53-31-1009 REV.-- DATED 2025-06-13. LEAK CHECK GOOD. COMPLIED WITH 51-900-1002-SKY. - [SDR SWI2025F00974](https://openairdocs.org/sdr/SWI2025F00974.md): Stringer · corroded · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer > STGR27 FS661.00+16 - 661.00+32 HAS THREE RIVETS WITH CORROSION AROUND THE BUCK TAIL. (MARKED) (C-CHECK RO 07/16/2025)BLENDED STGR 27 FS661.00+16 - 661.00+32 IN LIMITS AND RESTORED REF REO 690-53-31-982 REV.-- DATED 2025-05-07. LEAK CHECK GOOD. COMPLIED WITH 5 - [SDR SWI2025F00973](https://openairdocs.org/sdr/SWI2025F00973.md): Door · cracked · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Emergency Exits > LH AFT EMER EXIT DOOR HAS CRACK NEXT TO AFT MICROSWITICH BRACKET. (C-CHECK RO 07/16/2025)REPAIRED LH AFT EMER DOOR CRACK ON AFT MICROSWITCH BRACKET AREA REF REO 670-52-21-103 REV.-- DATED 2024-11-06.C/W 51-900-1002-SKY - [SDR SWIA20250717401](https://openairdocs.org/sdr/SWIA20250717401.md): Mount · corroded · Apr 1, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Attach Fittings > MACHINED MOUNT CORRODED FS533.00 - 549.00 STGR25R - 24R. (MARKED) (C-CHECK RO 07/16/2025)REMOVED CORROSION ON THE MACHINED MOUNT AT FS533.00 - FS549.00 STGR25L - 24L, AND EVALUATED AS 'OUT-OF-LIMITS'. REPLACED MACHINED MOUNT WITH NEW MOUNT. REF. CRJ900 SRM 51 - [SDR SWI2025F00987](https://openairdocs.org/sdr/SWI2025F00987.md): Floor Support · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > RIGHT FLOOR SILL FROM FS280 TO FS319 HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 07/16/2025)REPLACED RIGHT FLOOR SILL FROM FS280 TO FS319 REF CRJ900 SRM 51-42-0-001-001-A01, CRJ900 SRM 51-42-21-001-001-A01, CRJ900 SRM 51-42-13-001-001-A01 AND DWG SH - [SDR SWI2025F00986](https://openairdocs.org/sdr/SWI2025F00986.md): Intercostal · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AVIONICS BAY DOOR SURROUND INTERCOSTAL ON FWD SIDE BETWEEN FS.349.00 FS.364.00 AT 26L HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK RO 07/16/2025) INTERCOSTAL ORIGINAL MATERIAL THICKNESS IS 0.063" IAW CRJ900 SRM 53-21-23-001-003-A01. CORROSION IS ON TWO E - [SDR SWI2025F00985](https://openairdocs.org/sdr/SWI2025F00985.md): Floor Support · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LBL27.00 CORRODED IN MULTIPLE LOCATIONS ON UPPER SURFACE BETWEEN APPROXIMATELY FS1005.00 - FS1069.75 AS MARKED (C-CHECK RO 07/16/2025)REMOVED AND INSTALLED NEW REPAIR FLOOR BEAM SECTION AT LBL 27 BETWEEN F/S 1005 TO F/S 1038 IAW CRJ 900 SRM 53-00-41-201-001-A - [SDR SWI2025F00984](https://openairdocs.org/sdr/SWI2025F00984.md): Stringer · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Floor Beam > BELOW FLOOR NEAR INTERCOSTAL AT STR.20R BETWEEN FS.333.00 AND FS.349.00 HAS CORROSION IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 07/16/2025)REPLACED BELOW FLOOR INTERCOSTAL AT STR.20R BETWEEN FS.333.00 AND FS.349.00CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 S - [SDR SWI2025F00983](https://openairdocs.org/sdr/SWI2025F00983.md): Intercostal · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AVIONICS BAY DOOR SURROUND INTERCOSTAL ON FWD SIDE BETWEEN FS.349.00 FS.364.00 AT 27L HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 07/16/2025)REPLACED AVIONICS BAY DOOR SURROUND INTERCOSTAL FWD SIDE BETWEEN FS349-FS364 AT 27L REF CRJ900 SRM 51-42-06-0 - [SDR SWI2025F00982](https://openairdocs.org/sdr/SWI2025F00982.md): Floor Support · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > LBL9.00 CORRODED IN MULTIPLE LOCATIONS ON UPPER SURFACE BETWEEN FS1031.00 - FS1088.2. REPAIRED CORROSION AT MULTIPLE LOCATIONS ON THE UPPER SURFACE OF THE LBL 9 FLOORBEAM BETWEEN FS 1031.30 - FS 1088.20 REF CRJ900 SRM 53-00-41-201-001-A03 REV 38 JUL 25/2020 - [SDR SWI2025F00981](https://openairdocs.org/sdr/SWI2025F00981.md): Intercostal · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Miscellaneous Structure > AVIONICS BAY DOOR SURROUND INTERCOSTAL ON FWD SIDE OF DOOR BETWEEN FS.349.00 FS.364.00 AT 27R HAS MULTIPLE SPOTS OF CORROSION (MARKED) (C-CHECK RO 07/16/2025)REPLACED AVIONICS BAY DOOR SURROUND INTERCOSTAL ON FED SIDE OF DOOR BETWEEN FS349-FS364 AT 27R REF CR - [SDR SWIA202507140330](https://openairdocs.org/sdr/SWIA202507140330.md): Door Sill · corroded · Mar 30, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > AFT BAGGAGE BAY DOORSILL HAS CORROSION AND CHAFFING BETWEEN FS1000.00 - FS1051.30 AS MARKED (C-CHECK RO 07/16/2025)CORROSION PRESENT ON MORE THAN 75% OF SURFACE. FOUND OUT OF LIMITS. REF. CRJ900 SRM 53-61-23-201-001-A01. REMOVED AND  INSTALLED NEW AFT CARGO - [SDR SWI2025F00991](https://openairdocs.org/sdr/SWI2025F00991.md): Floorbeam · corroded · Mar 29, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Floor Beam > FS280, THE COCKPIT FLOOR PANEL ANGLE THAT IS ATTACHED TO THE FS280 BEAMS IS CORRODED (MARKED) (C-CHECK RO 07/16/2025)REPLACED FS280, THE CORRODED COCKPIT FLOOR PANEL ANGLE THAT IS ATTACHED TO THE FS280 BEAMS WITH NEW PN CC670-34095-1 PO# 5-31209 PERF CRJ 900 S - [SDR SWI2025F00990](https://openairdocs.org/sdr/SWI2025F00990.md): Landing · cracked · Mar 29, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > R/H LWR LAND FOR THE ACCESS DOOR 212AR FOR THE FORWARD EQUIPMENT COMPARTMENT HAS A CRACK AT THE CUTOUT FOR THE AFT LATCH. REMOVED AND REPLACED THE R/H LOWER LANDING (P/N CC670-33151-6) FOR ACCESS DOOR 212AR FOR THE FORWARD EQUIPMENT COMPARTMENT REF REO 690-5 - [SDR SWI2025F00989](https://openairdocs.org/sdr/SWI2025F00989.md): Landing · cracked · Mar 29, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Structure > L/H LWR LAND FOR THE ACCESS DOOR 211AL FOR THE FORWARD EQUIPMENT COMPARTMENT HAS A CRACK AT THE CUTOUT FOR THE AFT LATCH. REMOVED AND REPLACED THE LH SIDE FWD AVIONICS BAY DOOR LANDING FOR PANEL 211AL REF CRJ900 SRM TASK 51-42-06-001-001-A01, CRJ900 SRM TASK - [SDR SWI2025F00988](https://openairdocs.org/sdr/SWI2025F00988.md): Floorbeam · cracked · Mar 29, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Floor Beam > FS280.00 RBL 9, FLOORBEAM TO CROSS BEAM OUTBD ATTACH ANGLE IS CRACKED. REMOVED AND INSTALLED NEW OUTBD ATTACH ANGLE TO FS280-00 RBL9 FLOORBEAM REF CRJ900 SRM 51-42-21-001-001-A01 & DWG CC670-34010 REV-K. COMPLIED WITH 51-900-1002-SKY - [SDR SWIA202507170329](https://openairdocs.org/sdr/SWIA202507170329.md): Floorbeam · cracked · Mar 29, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Floor Beam > FS280.00 LBL 9, FLOOR BEAM TO CROSS BEAM OUTBD ATTACH ANGLE IS CRACKED (MARKED) (C-CHECK RO 07/16/2025)REMOVED AND INSTALLED NEW OUTBD ATTACH ANGLE TO FS280-00 LBL9 FLOOR BEAM REF CRJ900 SRM 51-42-21-001-001-A01 & DWG CC670-34010 REV-K. COMPLIED WITH 51-900-1 - [SDR SWIA2025071700327](https://openairdocs.org/sdr/SWIA2025071700327.md): Stand Off · cracked · Mar 27, 2025 · N805SK · Cndair CL6002D24 · Engine Thrust Reverser > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 07/16/2025)REMOVED AND REPLACED INBD STANDOFF P/N CN624-2082-201 ON R/H UPPER TRANSCOWL REF. REO 670-54-21-971 REV. B, 2023-11-28.COMPLIED WITH SKY CARD 51-900-1002-SKY. - [SDR SWIA202507170319](https://openairdocs.org/sdr/SWIA202507170319.md): Skin · chafed · Mar 19, 2025 · N805SK · Cndair CL6002D24 · Leading Edge Devices > LEFT WING INBOARD SLAT #1 AFT TRAILING EDGE SKIN IS CHAFED AT THE INBOARD END. HN00227627 (C-CHECK RO 07/16/2025)REPAIRED LH WING INBD SLAT #1 AFT TRAILING EDGE SKIN. PER REO 670-57-42-1207 REV -- DATED 2025-05-12. COMPLIED WITH TASK CARD 51-900-1002-SKY. - [SDR SWI2025F00994](https://openairdocs.org/sdr/SWI2025F00994.md): Beam · gouged · Mar 17, 2025 · N805SK · Cndair CL6002D24 · Trailing Edge Flaps > LH INBD FLAP INBD VANE ACTUATOR BEAM IS GOUGED. (MARKED) (C-CHECK RO 07/16/2025)REPAIRED LH INBD FLAP VANE ACTUATOR BEAM. PER REO 670-57-52-257 REV -A DATED 2024-08-20. OPS CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY. - [SDR SWI2025F00993](https://openairdocs.org/sdr/SWI2025F00993.md): Skin · gouged · Mar 17, 2025 · N805SK · Cndair CL6002D24 · Cargo/Baggage Doors > FWD CARGO CENTER DOOR HAS MULTIPLE GOUGES ON AFT SEAL STICKER. (MARKED) (C-CHECK RO 07/16/2025)REMOVED AND REPLACED NEW AFT SEAL STRIKER AT FWD CARGO CENTER DOOR REF CRJ900 SRM 51-41-02-001-001-A01 AND DWG# SH670-33750 REV -AA ( SEE CONTINUE CARD FOR WORK DET - [SDR SWI2025F00992](https://openairdocs.org/sdr/SWI2025F00992.md): Beam · gouged · Mar 17, 2025 · N805SK · Cndair CL6002D24 · Trailing Edge Flaps > LH INBD FLAP OTBD FLAP VANE ACTUATOR BEAM IS GOUGED. (MARKED) (C-CHECK RO 07/16/2025)COMPLIED WITH REO 670-57-52-257 REV A DATE 2024-08-20 OPS CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY - [SDR SWIA202507170317](https://openairdocs.org/sdr/SWIA202507170317.md): Beam · gouged · Mar 17, 2025 · N805SK · Cndair CL6002D24 · Wing Main, Frame Structure > LH INBD FLAP MIDDLE FLAP VANE ACTUATOR BEAM IS GOUGED. (MARKED) (C-CHECK RO 07/16/2025)COMPLIED WITH REO 670-57-52-257 REV A DATE 2024-08-20 OPS CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY - [SDR SWIA202507170303](https://openairdocs.org/sdr/SWIA202507170303.md): Skin · dented · Mar 3, 2025 · N805SK · Cndair CL6002D24 · Fuselage Main, Plate/Skin > DENT DAMAGE ON LH HYDRAULIC BAY SKIN PANEL BETWEEN FS169.00 - FS173.00 AND STR21L - STR23L. THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1250 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV €Œ--€?., PART NUMBER: -, SERIAL NUMBER: 15069, - [SDR SWI2025F01001](https://openairdocs.org/sdr/SWI2025F01001.md): Roller · out of limits · Dec 27, 2024 · N805SK · Cndair CL6002D24 · Leading Edge Devices > TRACK ROLLER SLAT 2-2 900 RH - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 2-2, TOP FORWARD - SLAT 2 (PN CC670-12272-1). (MRB 27-81-43-725), PART NUMBER: -, SERIAL NUMBER: 15069, POSITION: (C-CHECK RO 07/16/2025)REMOVED AND REPLACED RH - [SDR SWI2025F01000](https://openairdocs.org/sdr/SWI2025F01000.md): Roller · out of limits · Dec 27, 2024 · N805SK · Cndair CL6002D24 · Leading Edge Devices > TRACK ROLLER SLAT 2-2 900 LH - COMPLY WITH TASK CARD 27-530-809 LH TRACK ROLLER SEALED, TRACK 2-2, TOP FORWARD - SLAT 2 (PN CC670-12272-1). (MRB 27-81-43-725), PART NUMBER: -, SERIAL NUMBER: 15069, POSITION: (C-CHECK RO 07/16/2025)REMOVED AND REPLACED L/H - [SDR SWI2025F00999](https://openairdocs.org/sdr/SWI2025F00999.md): Roller · out of limits · Dec 27, 2024 · N805SK · Cndair CL6002D24 · Leading Edge Devices > TRACK ROLLER SLAT 1-3 900 RH - COMPLY WITH TASK CARD 27-630-809 RH TRACK ROLLER SEALED, TRACK 1-3, TOP FORWARD - SLAT 1 (PN CC670-12272-1). (MRB 27-81-43-718), PART NUMBER: -, SERIAL NUMBER: 15069, POSITION: (C-CHECK RO 07/16/2025)REMOVED AND REPLACED R/H Next page: https://openairdocs.org/aircraft/N805SK/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N805SK' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N805SK/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.