# Service difficulty reports: N604SK A list on [N604SK](https://openairdocs.org/aircraft/N604SK.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 4 · 174 reports - [SDR SWI2025F00634](https://openairdocs.org/sdr/SWI2025F00634.md): Skin · chafed · Mar 19, 2025 · N604SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin > FWD BAG BAY FUSELAGE SKIN CHAFING UNDER DOOR TOP AFT CORNER (C-CHECK RO 05/08/2025)REPAIRED DAMAGE TO FUSELAGE SKIN AT FWD BAG BAY TOP AFT CORNER IAW REO 670-53-31-1028 REV-- DATE 2025-04-18 AND CRJ700 SRM 51-12-00, 53-31-01, AMM 21-31-00. NDT PERFORMED BY BA - [SDR SWI2025F00633](https://openairdocs.org/sdr/SWI2025F00633.md): Slat Track · worn · Mar 19, 2025 · N604SK · Cndair CL6002C10 · Leading Edge Devices > SLAT TRACK #1 HAS WARE MARK ON LWR SIDE (C-CHECK RO 05/08/2025)REPAIRED DAMAGE ON SLAT TRACK #1 IAW REO 670-57-42-2054 REV-- DATE 2025-04-14 AND CRJ700 SRM 51-10-06, 51-12-00. - [SDR SWIA20250508319](https://openairdocs.org/sdr/SWIA20250508319.md): Slat Track · worn · Mar 19, 2025 · N604SK · Cndair CL6002C10 · Leading Edge Devices > SLAT TRACK #9 HAS WEAR MARK ON LWR SIDE (C-CHECK RO 05/08/2025)REPAIRED DAMAGED SLAT TRACK #9 RHS IAW REO 670-57-42-2068 REV-- DATE 2025-04-29 AND CRJ700 SRM 51-10-06 AND 51-12-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S042425-1, P.O# 176 - [SDR SWI2025F00637](https://openairdocs.org/sdr/SWI2025F00637.md): Slat Track · corroded · Mar 18, 2025 · N604SK · Cndair CL6002C10 · Leading Edge Devices > SLAT TRACK #4 HAS EVIDANCE OF PITTING CORROCION ON UPPER SURFACE (C-CHECK RO 05/08/2025)PERFORMED BLENDED OUT AND EVALUATED AREA ON SLAT TRACK #4 OF FITTING UPPER SURFACE, MEASUREMENTS ARE: ORIGINAL THICKNESS #1 IS: 0.256", MATERIAL LOSS: 0.002", REMAINING MA - [SDR SWI2025F00636](https://openairdocs.org/sdr/SWI2025F00636.md): Slat Track · corroded · Mar 18, 2025 · N604SK · Cndair CL6002C10 · Leading Edge Devices > SLAT TRACK #2 HAS EVIDANCE OF PITTING CORROCION ON LWR SURFACE (C-CHECK RO 05/08/2025)PERFORMED REPAIR AT SLAT TRACK 1-2 LHS,REWORKED AREA IS STRUCTURALLY AND FUNCTIONALLY ACCEPTABLE,FOUND TO BE WITH IN LIMITS IAW REO 670-57-42-2052 REV -- DATED 2025-04-14,CR - [SDR SWI2025F00635](https://openairdocs.org/sdr/SWI2025F00635.md): Slat Track · worn · Mar 18, 2025 · N604SK · Cndair CL6002C10 · Leading Edge Devices > SLAT TRACK #1 HAS WEAR ON LWR SIDE (C-CHECK RO 05/08/2025)PERFORMED REPAIR ON SLAT TRACK # 1 LOWER SIDE PER MHIJR REO 670-57-42-2055. REV.--. DATE: 2025-04-14. CRJ-700 SRM 51-12-00, 51-10-06 CRJ-700 AMM 57-42-26. - [SDR SWIA20250508318](https://openairdocs.org/sdr/SWIA20250508318.md): Slat Track · corroded · Mar 18, 2025 · N604SK · Cndair CL6002C10 · Leading Edge Devices > SLAT TRACK #5 HAS EVIDANCE OF PITTING CORROCION ON LWR SURFACE (C-CHECK RO 05/08/2025)PERFORMED REPAIR AT SLAT TRACK #5 L/H SIDE ON LOWER SURFACE IAW REO 670-57-42-2058 REV -- DATED 2025-04-14,CRJ 700 SRM 51-21-06,AMM 57-42-26PERFORMED NDT PT INSPECTION BY BA - [SDR SWIA20250508314](https://openairdocs.org/sdr/SWIA20250508314.md): Skin · chafed · Mar 14, 2025 · N604SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin > BOTTOM FUSELAGE SKIN CHAFFED AFT OF FS977.00 AT STR27 (C-CHECK RO 05/08/2025)PERFORMED REPAIR AREA ON BOTTOM FUSELAGE SKIN FS977.00 STR27 IAW MHI RJ REO 670-53-00-290 REV-F DATE: 2019-04-26, CRJ700 SRM 51-25-01. PERFORMED INSPECTION BY BARON NDT, LLC FAA CRS - [SDR SWIA20250808313](https://openairdocs.org/sdr/SWIA20250808313.md): Structure · cracked · Mar 13, 2025 · N604SK · Cndair CL6002C10 · Wing Main, Frame Structure > RH WING SLAT #1, #3 SLAT TRACK BOX CRACKED. (C-CHECK RO 05/08/2025)PERFORMED REPAIR ON R/H WING SLAT # 1, # 3 SLAT TRACK BOX PER BOMBARDIER REO 670-57-42-577. REV. --. DATE: 2016-12-02. NDT PERFORMED BY BARON NDT,LLC FAA CRS# 5NDR545D. REPORT # S040125-3. P.O. - [SDR SWIA20250508306](https://openairdocs.org/sdr/SWIA20250508306.md): Pulley Bracket · chafed · Mar 6, 2025 · N604SK · Cndair CL6002C10 · Passenger/Crew Doors > PASSENGER DOOR POWER ASSIST MOTOR CABLE PULLEY BRACKET IS CHAFFED FROM THE CABLE (C-CHECK RO 05/08/2025)PERFORMED REPAIR ON PASSENGER DOOR POWER ASSIST MOTOR CABLE PULLEY BRACKET IAW MHI RJ REO- 670-52-11-1470 REV -- DATED 2025-04-16, IAW CRJ700 SRM 53-00-00, - [SDR SWIA20250508115](https://openairdocs.org/sdr/SWIA20250508115.md): Skin · damaged · Jan 15, 2025 · N604SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA68951-670-57-00-083 604SK BL45.00 WS29.76 STR29-STR30 MXCODEID56025-PR - LIGHTNING STRIKE @ BL 45.00 WS 29.76 BETWEEN STR 29 & STR 30. DAMAGE REPAIRED PER REO 670-57-00-083 REV B. PERMANENT REPAIR DUE IN 8000 FH. DUE - [SDR SWIA202411150930](https://openairdocs.org/sdr/SWIA202411150930.md): Stringer · damaged · Sep 30, 2024 · N604SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > FOUND DAMAGED TO RH STRS 6R AND 7R BETWEEN FS1144.00-FS1162.00. (FILED CLOSED)REPAIRED DAMAGED STRINGERS AND DAMAGED SKIN FOUND ON CP 28924642 PER REO 670-53-61-2381 REV-- DATED 10-23-24. FORM 337 AND MAJOR REPAIR 51-900-1002-SKY CARD COMPLETED. - [SDR SWIA20241030930](https://openairdocs.org/sdr/SWIA20241030930.md): Stringer · damaged · Sep 30, 2024 · N604SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > FOUND DAMAGED TO RH STRS 6R AND 7R BETWEEN FS1144.00-FS1162.00. (FILED OPEN)REPAIRED DAMAGED STRINGERS AND DAMAGED SKIN FOUND ON CP 28924642 PER REO 670-53-61-2381 REV-- DATED 10-23-24. FORM 337 AND MAJOR REPAIR 51-900-1002-SKY CARD COMPLETED. - [SDR SWIA202401290006](https://openairdocs.org/sdr/SWIA202401290006.md): Heater · warning message · Jan 26, 2024 · N604SK · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal > AT NEXT MX OPPORTUNITY TROUBLESHOOT R WINDOW HEAT CAUTION DUE TO REPEAT WRITE UPS MCI TYPE: TROUBLESHOOTING PRIORITY 1 (FILED CLOSED)REMOVED AND REPLACED R COCKPIT WINDOW IN REFERENCE TO CRJ 700 AMM 56-12-01 AND COMPLIED WITH TASK CARD 56-220-1000-SKY. PERFORM - [SDR SWIA202161781](https://openairdocs.org/sdr/SWIA202161781.md): None · malfunctioned · Oct 16, 2021 · N604SK · Cndair CL6002C10 · Landing Gear Door Actuator > GEAR DISAGREE WARNING MESSAGE AFTER SELECTING GEAR UP. COMPLIED WITH QRH PROCEDURE. GEAR INDICATED DOWN AND LOCKED. ( 9906 - FILE CLOSED)INVESTIGATED NOSE GEAR HARNESS, FOUND PROXIMITY SENSORS PX22 AND PX21 TO BE OUT OF LIMITS. ADJUSTED PROXIMITY SENSORS P - [SDR SWIA202156824](https://openairdocs.org/sdr/SWIA202156824.md): Panel · cracked · Feb 27, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Structure > BOTTOM PART OF DOOR SURROUND SIDE PANEL 151FLW WHERE THE NUT PLATES GO IS CRACKED (C-CHECK) RO 3/10/2021 RECIEVED NEW SERVICEABLE FWD CARGO DOOR SURROUND PANEL 151FLW. LOCATED AND DRILLED UP NEW SERVICEABLE PANEL IAW CRJ 700 SRM 51-40-11-001-001-A01. RE - [SDR SWIA202156802](https://openairdocs.org/sdr/SWIA202156802.md): Frame · damaged · Feb 11, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Frame > DAMAGE @ F.S.280.00 CIRCUMFRENTIAL JOINT BETWEEN STRINGER23R - 18R REQUIRES REPAIR (C-CHECK) RO 3/10/2021 REPAIRED DAMAGE @ F.S.280.00 CIRCUMFRENTIAL JOINT BETWEEN STRINGER23R - 18R IAW REO 670-53-21-1952 REV -- DATED 2021-02-10. ATTACHED STRUCTURAL MAJO - [SDR SWIA202156801](https://openairdocs.org/sdr/SWIA202156801.md): Frame · damaged · Feb 11, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Frame > DAMAGE @ F.S. 280.00 CIRCUMFRENTIAL JOINT STRINGER 23L-25L & 23R-25R REQUIRES REPAIR (C-CHECK) RO 3/10/2021 REPAIRED DAMAGE @ F.S. 280.00 CIRCUMFRENTIAL JOINT STRINGER 23L-25L & 23R-25R IAW REO 670-53-21-1943 REV -- DATED 2021-02-04. ATTACHED STRUCTURAL - [SDR SWIA202156800](https://openairdocs.org/sdr/SWIA202156800.md): Frame · damaged · Feb 11, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Frame > DAMAGE @ F.S. 208.00 CIRCUMFRENTIAL JOINT BETWEEN STRINGERS 18L - 22L REQUIRES REPAIR (C-CHECK) RO 3/10/2021 REPAIRED DAMGE @ F.S. 208.00 CIRCUMFRENTIAL JOINT BETWEEN STRINGERS 18L - 22L IAW REO 670-53-21-1953 REV -- DATED 2021-02-10. ATTACHED STRUCTURA - [SDR SWIA202156823](https://openairdocs.org/sdr/SWIA202156823.md): Angle · cracked · Feb 3, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > L/H LBL 9 ANGLE FS 265 TO 280 IS CRACK (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED L/H LBL 9 J ANGLE AT FS 265 TO 280 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 - [SDR SWIA202156822](https://openairdocs.org/sdr/SWIA202156822.md): Angle · cracked · Feb 3, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > R/H RBL 9 ANGLE FS 265 TO 280 IS CRACK (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED R/H RBL 9 J ANGLE AT FS 265 TO 280 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 - [SDR SWIA202156834](https://openairdocs.org/sdr/SWIA202156834.md): Stop Fitting · corroded · Jan 28, 2021 · N604SK · Cndair CL6002C10 · Trailing Edge Flaps > L/H WING INBD TRAILING EDGE STOPPER WS24.50 IS CHAFFED OUT OF LIMITS (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED L/H WING INBOARD FLAP VANE INBOARD STOP FITTING IAW CRJ-700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01 AND 51-42-13-001-001-A01. - [SDR SWIA202156819](https://openairdocs.org/sdr/SWIA202156819.md): Frame · corroded · Jan 28, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Frame > FS235 BULKHEAD FRAME IS CORRODED ON AFT SIDE AT LBL5 WL51.5 (C-CHECK) RO 3/10/2021 FS235 BULKHEAD FRAME IS CORRODED ON AFT SIDE AT LBL5 WL51.5. REPAIRED IAW REO 670-53-11-1644 REV -- DATED 2021-02-02 AND REO 670-53-11-1645 REV -- DATED 2021-03-05. OP AND - [SDR SWIA202156812](https://openairdocs.org/sdr/SWIA202156812.md): Frame · corroded · Jan 28, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Frame > FS235 BULKHEAD FRAME IS CORRODED ON AFT SIDE AT RBL5 WL51.5 (C-CHECK) RO 3/10/2021 FS235 BULKHEAD FRAME IS CORRODED ON AFT SIDE AT RBL5 WL51.5 WAS REPAIRED IAW MHIRJ REO 670-53-11-1645 REV -- DATED 2021-03-05 AND REO 670-53-11-1644 REV -- DATED 2021-02-02 - [SDR SWIA202156833](https://openairdocs.org/sdr/SWIA202156833.md): Angle · corroded · Jan 27, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PAX DOOR SILL UPPER ANGLE CORRODED (C-CHECK) RO 3/10/2021 REPLACED PAX DOOR UPPER SILL ANGLE IAW CRJ 700 SRM 51-41-02-001-001-A01. OPS CHECKS GOOD. REF CONT CARD FOR WORK PERFORMED. - [SDR SWIA202156818](https://openairdocs.org/sdr/SWIA202156818.md): Intercostal · corroded · Jan 27, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > INTERCOSTAL AT STRGR 20R CORRODED BETWEEN F.S. 319.00 AND F.S 349.00 (C-CHECK) RO 3/10/2021 REMOVED CORRODED INTERCOSTAL AT STRINGER 20R FROM F.S. 319.00 TO F.S. 349.00 AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42- - [SDR SWIA202156762](https://openairdocs.org/sdr/SWIA202156762.md): Plate · chafed · Jan 25, 2021 · N604SK · Cndair CL6002C10 · Passenger/Crew Doors > CHAFE ON PAX DOOR AFT CEBTERING PLATE ON AFT FORMER AT FS 347 (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR AFT CENTERING PLATE WITH SERVICEABLE CENTERING PLATE IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. COMPLETED AND ATTACHED - [SDR SWIA202156769](https://openairdocs.org/sdr/SWIA202156769.md): Floorbeam · corroded · Jan 22, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Floor Beam > CROSSBEAM CAP AT FS 280 R/H SIDE HAS HEAVY CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED RH 280 CROSSBEAM CAP IAW CRJ 700 SRM 51-42-06-001-001-A01.. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY AND FORM M-337.WEIGHT NOT AFFECTED. REF; CO - [SDR SWIA202156768](https://openairdocs.org/sdr/SWIA202156768.md): Web · corroded · Jan 22, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FS 280 R/H LOWER WEB AT FLOOR LEVEL IS CORRODED (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED 280 RH LOWER WEB AT FLOOR LEVEL IAW CRJ 700 SRM 53-11-10-201-004-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY AND FORM M-337.WEIGHT NOT AFFECTED. RE - [SDR SWIA202156767](https://openairdocs.org/sdr/SWIA202156767.md): Web · corroded · Jan 22, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > FS 280 LOWER WEB L/H HAS HEAVY CORROSION AT FLOOR LEVEL (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED F.S. 280 LH LOWER WEB IAW CRJ 700 SRM 53-11-10-201-004-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY AND FORM M-337.WEIGHT NOT AFFECTED. REF - [SDR SWIA202156766](https://openairdocs.org/sdr/SWIA202156766.md): Crossbeam · corroded · Jan 22, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Structure > CROSSBEAM CAP AT FS 280 L/H SIDE HAS HEAVY CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED LH CROSSBEAM CAP AT F.S. 280 IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY AND FORM M-337..WEIGHT NOT AFFECTED. - [SDR SWIA202156803](https://openairdocs.org/sdr/SWIA202156803.md): Stringer Splice · corroded · Jan 21, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STRINGER SPLICE AT FS 333.00 STGR 25R CORRODED (C-CHECK) RO 3/10/2021 REPLACED STRINGER SPLICE AT FS 333.00 STGR 25R IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY,SDR AND FORM M-337. WEIGHT NOT AFFECTED. RE - [SDR SWIA202156808](https://openairdocs.org/sdr/SWIA202156808.md): Frame · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Frame > CORROSION FOUND ON PAX DOOR FORWARD FORMER AT FS 311. (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR FORWARD FORMER AT F.S. 311 WITH SERVICEABLE FORMER IAW CRJ 700 SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-06-001-001-A01. ATTACHED - [SDR SWIA202156807](https://openairdocs.org/sdr/SWIA202156807.md): Door Frame · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Structure > CORROSION FOUND ON PAX DOOR AFT FORMER AT FS347.25 (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR FORMER AT F.S. 347.25 WITH SERVICEABLE FORMER IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-9 - [SDR SWIA202156806](https://openairdocs.org/sdr/SWIA202156806.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD3 AFT LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD3 AFT LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. SEE ATTACHED CONTINUATION CARD FOR WORK PE - [SDR SWIA202156805](https://openairdocs.org/sdr/SWIA202156805.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL ATDD1 AFT LOCATION FORWARD OF FS 347 (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD1 AFT LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. SEE ATTACHED CONTINUATION - [SDR SWIA202156798](https://openairdocs.org/sdr/SWIA202156798.md): Frame · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Main, Frame > CORROSION FOUND ON PAX DOOR FRAME AT FS 313.56 BETWEEN DD4 AND DD5 FORWARD LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT F.S. 313.5 BETWEEN DD4 AND DD5 LLOCATIONS WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001 - [SDR SWIA202156797](https://openairdocs.org/sdr/SWIA202156797.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD3 FORWARD LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD3 FORWARD LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR T - [SDR SWIA202156796](https://openairdocs.org/sdr/SWIA202156796.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD2 FORWARD LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD2 FORWARD LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK - [SDR SWIA202156795](https://openairdocs.org/sdr/SWIA202156795.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Passenger/Crew Doors > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD5 FORWARD LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD5 FORWARD LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR T - [SDR SWIA202156794](https://openairdocs.org/sdr/SWIA202156794.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD6 FORWARD LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD6 LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51- - [SDR SWIA202156793](https://openairdocs.org/sdr/SWIA202156793.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL DD1 AT AFT LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD1 AFT LOCATION IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY,SDR AND FORM M- - [SDR SWIA202156792](https://openairdocs.org/sdr/SWIA202156792.md): Hinge · gouged · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage, Door Hinge > PAX DOOR HINGE (FUSELAGE SIDE) AFT LANDING HAS GOUGE FROM HINGE PIN ROLL PIN. (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR HINGE IAW CRJ 700 SRM 53-21-23-201-007-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY,SDR AND FORM M-337. WEIGH - [SDR SWIA202156791](https://openairdocs.org/sdr/SWIA202156791.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD4 AFT LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD4 AFT LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51- - [SDR SWIA202156790](https://openairdocs.org/sdr/SWIA202156790.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD5 AFT LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD5 AFT LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51- - [SDR SWIA202156789](https://openairdocs.org/sdr/SWIA202156789.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND IN PAX DOOR INTERCOSTAL DD7A (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD7A WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51-900-1002-SKY,SDR AND FORM M-3 - [SDR SWIA202156788](https://openairdocs.org/sdr/SWIA202156788.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD6 MID LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR FORMER AT F.S. 329 BETWEEN DD5 AND DD6 WITH SERVICEABLE FORMER IAW CRJ 700 SRM 51-42-06-001-001-A01. ATTACHED STRUCTURAL MAJOR REPAIR TASK 51 - [SDR SWIA202156787](https://openairdocs.org/sdr/SWIA202156787.md): Intercostal · corroded · Jan 20, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CORROSION FOUND ON PAX DOOR INTERCOSTAL AT DD3 MID LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD3 MID LOCATION WITH SERVICEABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. ATTACHED STRUCTUR - [SDR SWIA202156832](https://openairdocs.org/sdr/SWIA202156832.md): Angle · corroded · Jan 19, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > PAX DOOR SILL ANGLE HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO 3/10/2021 INSTALLED PAX DOOR LOWER ANGLE IAW CRJ 700 SRM 51-42-21-001-001A01 AND 51-42-06-001-001-A01. REF CONT CARD FOR WORK PERFORMED. - [SDR SWIA202156831](https://openairdocs.org/sdr/SWIA202156831.md): Intercostal · corroded · Jan 19, 2021 · N604SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure > INTERCOSTAL AT STRGR 20L CORRODED FROM F.S. 333.00 TO 349.00 (C-CHECK) RO 3/10/2021 FOUND STR 20L AT F.S 333.00-349.00 TO BE OUT OF LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01. REMOVED.015 MATERIAL ORIGINAL THICKNESS.050 FOUND REMIAING THICKNESS TO BE Next page: https://openairdocs.org/aircraft/N604SK/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 = 'N604SK' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N604SK/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.