# Service difficulty reports: N787SK

A list on [N787SK](https://openairdocs.org/aircraft/N787SK.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 3 · 120 reports

- [SDR SWIA2026100777528](https://openairdocs.org/sdr/SWIA2026100777528.md): Unknown · odor · Oct 7, 2026 · N787SK · Cndair CL6002C11 · Air Distribution System
  > TROUBLESHOOT FOR FA & PAX IN LAST ROW, BOTH REPORTED SMELLING A STRONG OIL OR FUEL TYPE ODOR IN FLT, & THE PERIOD IMMEDIATELY AFTER ENG SHUTDOWN. NO SUCH ODOR OBSERVED IN FLIGHT DECK, OR IN CABIN AFTER DEPLANING. VERIFIED WITH CAPTAIN THAT APU WAS NOT USED
- [SDR SWIA2026080576738](https://openairdocs.org/sdr/SWIA2026080576738.md): Skin · damaged · Aug 5, 2026 · N787SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > AIRCRAFT FUSELAGE SUSTAINED DAMAGE DURING MAINTENANCE BETWEEN BS 265 AND BS 280 AND BETWEEN STR 27L AND STR 26L. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN BTWN BS 265 & BS 280, STR 26 - 27L IAW REO 670-53-11-2354. ALSO COMPLETED CARD ST 51-900-1002-SKY.
- [SDR SWIA2026072076664](https://openairdocs.org/sdr/SWIA2026072076664.md): Doubler · demodification · Jul 20, 2026 · N787SK · Cndair CL6002C11 · Standard Practices/Structures
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581 - 597 AND STR 24R - 25R,DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO
- [SDR SWIA2026072076663](https://openairdocs.org/sdr/SWIA2026072076663.md): Skin · demodification · Jul 20, 2026 · N787SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 1000 - 1015, STR 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (MAJOR REPAIR).
- [SDR SWIA2026072076662](https://openairdocs.org/sdr/SWIA2026072076662.md): Skin · demodification · Jul 20, 2026 · N787SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13L - 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (MAJOR REPAIR).
- [SDR SWIA2026072076661](https://openairdocs.org/sdr/SWIA2026072076661.md): Skin · demodification · Jul 20, 2026 · N787SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM ( MAJOR REPAIR).
- [SDR SWIA2026072076660](https://openairdocs.org/sdr/SWIA2026072076660.md): Skin · demodification · Jul 20, 2026 · N787SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847, STRG 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (MAJOR REPAIR).
- [SDR SWIA2026031675510](https://openairdocs.org/sdr/SWIA2026031675510.md): Window · cracked · Mar 13, 2026 · N787SK · Cndair CL6002C10 · Flight Compartment Windows
  > LEFT WINDOW SHATTERED, IN CRUISE AT FL370, HEARD A LOUD POP, FOLLOWED BY VISUALLY SEEING THE LT WINDOW CRACK AND THEN SHATTER ON AN OUTER LAYER. DELTA P 8.1, CABIN ALTITUDE 8100. NO PRESSURIZATION LOSSES. FOLLOWED QRH. (FLIGHT 5142) REMOVED AND REPLACED LH W
- [SDR SWIA202505120007](https://openairdocs.org/sdr/SWIA202505120007.md): Window · failed · May 7, 2025 · N787SK · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT SIDE WINDSHIELD SHATTERED ON CLIMB OUT. RAN QRH. RETURNED TO FIELD. (FLIGHT 5795 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30102635 WITH THE FOLLOWING CORRECTIVE ACTION: "UPON FURTHER INSPECTION FOUND RIGHT SIDE WINDOW TO BE SHATTERED.
- [SDR SWIA2024111500003](https://openairdocs.org/sdr/SWIA2024111500003.md): Sensor · out of adjust · Nov 13, 2024 · N787SK · Cndair CL6002C10 · Landing Gear Position and Warning
  > GEAR DISAGREE AFTER TAKEOFF. RETURNED TO FIELD PER QRH. GEAR UP DISAGREE. (FLIGHT 5202 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29149338 WITH THE FOLLOWING CORRECTIVE ACTION: "INTERROGATED MDC AND FOUND B1 CODES 065386(L MLG ACT PR
- [SDR SWI2024F01200](https://openairdocs.org/sdr/SWI2024F01200.md): Frame · corroded · Oct 14, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 319.00 HAS EVIDENCE OF CORROSION ON THE LOWER FLANGE BETWEEN 26L AND 26R. (S/N#00574) (C-CHECK RO 11/6/2024) INSTALLED NEW SECTION FRAME AND SPLICES ON FRAME FS 319.00 BETWEEN STGR 25L - STGR 24R REF CRJ700 SRM 53-00-06-201-006-A01. LEAK CHECKED G
- [SDR SWIA2024110814](https://openairdocs.org/sdr/SWIA2024110814.md): Frame · corroded · Oct 14, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 310.00 HAS EVIDENCE OF CORROSION ON THE LOWER FLANGE BETWEEN 26L AND 26R. (S/N00571) (C-CHECK RO 11/6/2024) INSTALLED NEW FRAME AT FS 310.00 BETWEEN STGR 23LH - 24RH REF. CRJ700 SRM 53-00-06-201-006-A01. COMPLIED WITH TC 51-900-1002-SKY. LEAK CHEC
- [SDR SWI2024F01173](https://openairdocs.org/sdr/SWI2024F01173.md): Angle · cracked · Oct 9, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS280 CLIP IS CRACKED RBL9 OTBD SIDE CAMP # 28969192 (C-CHECK RO 11/6/2024) REMOVED AND REPLACED WITH NEW ATTACHMENT BRACKET. REF. CRJ700 SRM 51-42-21-001-001-A01 REV 38 DATED 25 JULY 2020 AND DWG CC670-34010 REV. K SEE CONTINUATION CARD FOR DETAILS. CO
- [SDR SWI2024F01177](https://openairdocs.org/sdr/SWI2024F01177.md): Crossbeam · corroded · Oct 4, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON RH CROSSBEAM AT F.S 280.00 BULKHEAD #28943546 (C-CHECK RO 11/6/2024) RH CROSSBEAM AT F.S 280.00 FOUND OUT OF LIMITS, REPLACED WITH NEW CROSSBEAM. REF. CRJ700 SRM SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51
- [SDR SWI2024F01176](https://openairdocs.org/sdr/SWI2024F01176.md): Crossbeam · corroded · Oct 4, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LH CROSSBEAM AT FS 280.00 HAS CORROSION TRANS# 28943506 (C-CHECK RO 11/6/2024) REPLACED THE CROSSBEAM AT FS 280.00 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 REV 38 JUL 25/2020 AND DWG CC670-340
- [SDR SWI2024F01199](https://openairdocs.org/sdr/SWI2024F01199.md): Web · corroded · Oct 3, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > R/H WEB AT FS280.00, RBL12 HAS CORROSION. TRANS # 28939631 (C-CHECK RO 11/6/2024) PERFORMED CUT OUT REF. CRJ700 SRM 53-11-10-201-004-A01. C/W NDT INSP REF CRJ-700 NDTM PT1 51-20-006-250-A01. NO DEFECTS NOTED AT THIS TIME. TUC9452 CAL DUE 31 OCT 2024.
- [SDR SWI2024F01175](https://openairdocs.org/sdr/SWI2024F01175.md): Web · corroded · Oct 2, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > L/H WEB AT FS280.00 HAS CORROSION. TRANS # 28934862 (C-CHECK RO 11/6/2024) LH WEB FOUND OF LIMITS. REPAIRED PER CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWI2024F01174](https://openairdocs.org/sdr/SWI2024F01174.md): Post · corroded · Oct 2, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LH LOWER POST AT LBL9 FS 280.00 HAS CORROSION TRANS #28932511 (C-CHECK RO 11/6/2024) PERFORMED LH LOWER POST CUTOUT REPAIR AT LBL9 FS 280.00 PER CRJ700 SRM 53-11-10-201-006-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR
- [SDR SWI2024F01157](https://openairdocs.org/sdr/SWI2024F01157.md): Stand Off · cracked · Sep 26, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/6/2024) INSTALLED 1 EA. NEW "A"-BRACKET P/N CN624-2082-201 ON INBD. SIDE OF L/H UPPER TRANS COWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3, AND COMPLIED
- [SDR SWI2024F01156](https://openairdocs.org/sdr/SWI2024F01156.md): Stand Off · cracked · Sep 26, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/6/2024) INSTALLED 1 EA. NEW "A"-BRACKET P/N CN624-2082-201 ON OTBD. SIDE OF L/H UPPER TRANS COWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3. AND COMPLIED
- [SDR SWI2024F01155](https://openairdocs.org/sdr/SWI2024F01155.md): Stand Off · cracked · Sep 26, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/6/2024) REMOVED CRACKED INBD "A" BRACKET STANDOFF, AND WET-INSTALLED 1 EA NEW INBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF MHIRJ GREO #670-54-21-971 REV (-
- [SDR SWI2024F01154](https://openairdocs.org/sdr/SWI2024F01154.md): Hinge · nicked · Sep 26, 2024 · N787SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > NICKS AND SCRATCHES NOTED ON PAX DOOR HINGE (PAX DOOR SIDE) ON FWD TO AFT LUGS 1,2,6,7,8, AND 19-27 (MARKED) (C-CHECK RO 11/6/2024) BLENDED OUT DAMAGES ON PAX DOOR HINGE (PAX DOOR SIDE). FOUND WITHIN LIMITS. REF. CRJ700 SRM 52-11-01-201-007-A01 AND REO
- [SDR SWI2024F01153](https://openairdocs.org/sdr/SWI2024F01153.md): Stand Off · cracked · Sep 26, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/6/2024) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-S
- [SDR SWIA20240926](https://openairdocs.org/sdr/SWIA20240926.md): Stand Off · cracked · Sep 26, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/6/2024) REMOVED CRACKED OUTBD "A" BRACKET STANDOFF, AND WET-INSTALLED 1 EA NEW OUTBD "A" BRACKET STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANSCOWL REF MHIRJ GREO #670-54-21-971 REV
- [SDR SWIA2024110867](https://openairdocs.org/sdr/SWIA2024110867.md): Slider · grooved · Sep 25, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > THE RH ENGINE UPPER TR OUTBD SLIDER IS GROOVED ALONG ENTIRE LENGTH. (C-CHECK RO 11/6/2024) PERFORMED A BLEND REPAIR AND FOUND WITHIN LIMITS PER REO# 670-54-21-1670, REV --, DATED 10/8/24. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2024F01168](https://openairdocs.org/sdr/SWI2024F01168.md): Slider · damaged · Sep 25, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > THE RH ENGINE LOWER TR OUTBD SLIDER IS GROOVED ALONG ENTIRE LENGTH. (C-CHECK RO 11/6/2024) PERFORMED A BLEND REPAIR AND FOUND WITHIN LIMITS PER REO 670-54-21-1673, REV. --, 2024-10-14. SKYWEST TASK CARD 51-900-1002-SKY COMPLIED WITH.
- [SDR SWI2024F01167](https://openairdocs.org/sdr/SWI2024F01167.md): Slider · grooved · Sep 25, 2024 · N787SK · Cndair CL6002C10 · Engine Thrust Reverser
  > THE RH ENGINE UPPER TR OUTBD SLIDER IS GROOVED ALONG ENTIRE LENGTH. (C-CHECK RO 11/6/2024) PERFORMED A BLEND REPAIR AND FOUND WITHIN LIMITS PER REO# 670-54-21-1670, REV --, DATED 10/8/24. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI2024F01152](https://openairdocs.org/sdr/SWI2024F01152.md): Tire · failed · Sep 23, 2024 · N787SK · Cndair CL6002C10 · Tire
  > RH MLG TIRE BURST PANEL ATTACHING ANGLE FOR PANEL 642AZ HAS CORROSION CAMP 28886419 (C-CHECK RO 11/6/2024) REMOVED AND REPLACED R/H TIRE BURST ANGLE P/N CC670-10338-2. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# CC670-10320 REV. F. COMPLIED WITH SKYWE
- [SDR SWI2024F001151](https://openairdocs.org/sdr/SWI2024F001151.md): Channel · corroded · Sep 23, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON CHANNEL FOR DRAIN MAST LOCATED IN CABIN UNDERFLOOR BETWEEN FS 333.00 - 349.00, STGR 24R - 25R (C-CHECK RO 11/6/2024) REMOVED AND REPLACED DRAIN MAST CHANNEL P/N SH670-32270-1. REF. CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 A
- [SDR SWI2024F01151](https://openairdocs.org/sdr/SWI2024F01151.md): Drain Mast · corroded · Sep 23, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON CHANNEL FOR DRAIN MAST LOCATED IN CABIN UNDERFLOOR BETWEEN FS 333.00 - 349.00, STGR 24R - 25R (C-CHECK RO 11/6/2024) REMOVED AND REPLACED DRAIN MAST CHANNEL P/N SH670-32270-1. REF. CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 A
- [SDR SWIA20241108922](https://openairdocs.org/sdr/SWIA20241108922.md): Striker · dented · Sep 22, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR SEAL STRIKER HAS A DENT AT FS 310.00, APPROX STGR 13L (C-CHECK RO 11/6/2024) REPAIRED PAX DOOR SEAL STRIKER AT FS310.00 APPROX STGR 13L REF REO 670-53-22-001 REV -J DATED 2016-11-10 ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-90
- [SDR SWI2024F01150](https://openairdocs.org/sdr/SWI2024F01150.md): Floorbeam · corroded · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM FITTING AT FS 349.00, STGR 18L, LBL36 - LBL45 (C-CHECK RO 11/6/2024) CORROSION ON FLOOR BEAM FITTING AT FS349.00 AND STRINGER 18L, LBL36 - LBL45 REPAIRED IAW REO 670-53-21-2466 REV.--, DATED 2024-09-27. SEE CONTINUATION CARD FOR D
- [SDR SWI2024F01149](https://openairdocs.org/sdr/SWI2024F01149.md): Door Sill · corroded · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AREAS OF CORROSION ON AFT CARGO DOOR SILL. MARKED (C-CHECK RO 11/6/2024) REMOVED AFT CARGO DOOR LOWER SILL BETWEEN FS 1000.00 - FS 1050.00 REF CRJ700 SRM 51-42-06-001-001-A01, REF CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-13-001-001-A01. INS
- [SDR SWI2024F01148](https://openairdocs.org/sdr/SWI2024F01148.md): Frame · corroded · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON AFT SIDE OF FS863 FRAME BETWEEN STR 26R AND 26L (C-CHECK RO 11/6/2024) REMOVED CORROSION ON AFT SIDE OF FS863 FRAME BETWEEN STR 26R AND 26 L REF CRJ700 SRM 51-12-00-001-001-A01. RECEIVED AND COMPILED WITH REO 670-53-51-316 REV.-- ISSUED 20
- [SDR SWI2024F01147](https://openairdocs.org/sdr/SWI2024F01147.md): Floorbeam · corroded · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL27 FLOOR BEAM IS CORRODED AT FS 1031 (C-CHECK RO 11/6/2024) LBL27 FOUND OUT OF LIMITS REF CRJ700 SRM 53-61-43-101-001-A01. PERFORMED FLOOR BEAM SPLICE REPAIR REF CRJ700 SRM 53-00-41-201-001-A01 AND COMPLIED WITH REO 670-53-61-2376 REV-- DATED 2024-09
- [SDR SWI2024F01146](https://openairdocs.org/sdr/SWI2024F01146.md): Floorbeam · cracked · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 CLIP IS CRACKED LBL9 OTBD SIDE (C-CHECK RO 11/6/2024) REMOVED CRACKED ANGLE CLIP ON LBL 9 OUTBOARD SIDE AT FS 280.00 REF CRJ700 SRM 51-42-21-001-001-A01. RECEIVED, LOCATED AND DRILLED NEW OUTBOARD ANGLE P/N CC670-34099-1SB REF CRJ700 SRM 51-40-11
- [SDR SWI2024F01145](https://openairdocs.org/sdr/SWI2024F01145.md): Fitting · corroded · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM FITTING AT FS 310.00, STGR 18L, LBL36 - LBL45 (C-CHECK RO 11/6/2024) CORROSION ON FLOOR BEAM FITTING AT FS310.00 STRINGER 18L, LBL36 - LBL45 REPAIRED IAW REO 670-53-21-2466 REV.--, DATED 2024-09-27. COMPLIED WITH SKYWEST TASK CARD
- [SDR SWI2024F01144](https://openairdocs.org/sdr/SWI2024F01144.md): Skin · gouged · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > *LWR EXTERNAL FUSELAGE SKIN IS GOUGED AT STGR 27 BETWEEN FS 972 AND FS 981. (C-CHECK RO 11/6/2024) BLENDED DAMAGE AND FOUND OUT OF LIMITS. REPAIRED LOWER SKIN PER BOMBARDIER REO 670-53-00-290 REV -F DATE 2019/04/26. SEE CONTINUATION CARD FOR DETAILS. CO
- [SDR SWI2024F01143](https://openairdocs.org/sdr/SWI2024F01143.md): Attach Angle · corroded · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON FS879 FRAME ATTACH FLANGE BETWEEN STR26R AND STR 26L (C-CHECK RO 11/6/2024) REPAIRED CORROSION ON FS879 FRAME ATTACH FLANGE BETWEEN STGR 26R AND STR 26L REF MHIRJ REO 670-53-51-313 REV -- DATED 2024-09-30 LEAK CHECK GOOD. COMPLIED WITH SKYW
- [SDR SWIA20240921](https://openairdocs.org/sdr/SWIA20240921.md): Intercostal · corroded · Sep 21, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON INTERCOSTAL ATTACHED TO STGR 21L BETWEEN FS 333.00 - 349.00 (C-CHECK RO 11/6/2024) REMOVED AND REPLACED WITH NEW BACK-UP SILL BETWEEN FS. 333 AND FS. 349 STGR 21L (SEE CONTINUATION CARD FOR DETAILS) REF. CRJ 700 SRM 51-42-06-001-001-A01, 5
- [SDR SWI2024F01193](https://openairdocs.org/sdr/SWI2024F01193.md): Door Sill · corroded · Sep 20, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT OVER WING EMERGENCY EXIT SURROUND STRUCTURE - THE LOWER SILL DIAPHRAGM FS785.15 - FS797.00 IS CORRODED, (MARKED IN RED) (C-CHECK RO 11/6/2024) REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS REF REO 670-53-41-688, REV --, DATED 2024-09-30. SEE CON
- [SDR SWI2024F01192](https://openairdocs.org/sdr/SWI2024F01192.md): Door Sill · corroded · Sep 20, 2024 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT OVER WING EMERGENCY EXIT SURROUND STRUCTURE - THE LOWER SILL DIAPHRAGM FSI752.50 - FS761.85 IS CORRODED, (MARKED IN RED) (C-CHECK RO 11/6/2024) REMOVED CORROSION, FOUND TO BE WITHIN LIMITS REF REO 670-53-41-688, REV --, DATED 2024-09-30. COMPLIED W
- [SDR SWI2024F01191](https://openairdocs.org/sdr/SWI2024F01191.md): Seal Depressor · damaged · Sep 20, 2024 · N787SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SEAL DEPRESSOR ON FS349.00 BETWEEN STGR4L - 5L IS DAMAGED. (MARKED) (C-CHECK RO 11/6/2024) REPAIRED PASSENGER DOOR SEAL DEPRESSOR ON FS349.00 BETWEEN STGR4L -5L REF REO 670-53-22-001 REV -J DATE 2016-11-10 SHEET 3, REPAIR TYPE 1. ALL STEP
- [SDR SWI2024F01202](https://openairdocs.org/sdr/SWI2024F01202.md): Fairing · chafed · Sep 14, 2024 · N787SK · Cndair CL6002C10 · Trailing Edge Flaps
  > MX: 28845399 S/N 0137 RIGHT WING INBOARD FLAP, OUTBOARD FLAP FAIRING (686BB) HAS DONE SOME CHAFING ON FLAP. FLAGGED (C-CHECK RO 11/6/2024) PERFORMED A BLEND OUT REPAIR PER AND FOUND WITHIN LIMITS PER REO 670-57-52-568 REV -- DATED 2024-10-03 AND CRJ7
- [SDR SWIA202411080914](https://openairdocs.org/sdr/SWIA202411080914.md): Fairing · chafed · Sep 14, 2024 · N787SK · Cndair CL6002C10 · Trailing Edge Flaps
  > MX: 28845384 S/N 0136RIGHT WING INBOARD FLAP, INBOARD FLAP FAIRING (683BB) HAS DONE SOME CHAFING ON FLAP. FLAGGED (C-CHECK RO 11/6/2024) PERFORMED A BLEND OUT REPAIR PER AND FOUND WITHIN LIMITS PER REO 670-57-52-568 REV -- DATED 2024-10-03 AND CRJ700 S
- [SDR SWIA202264680](https://openairdocs.org/sdr/SWIA202264680.md): None · failed · Feb 25, 2022 · N787SK · Cndair CL6002C10 · Leading Edge Slat Position Indicating System
  > SLATS FAIL MESSAGE ON FINAL FROM FLAP 0 TO 1. RAN QRH. SLATS NEVER DEPLOYED. (FLIGHT 5627 - FILED CLOSED) CLEARED SLAT/FLAP INHIBITS. PERFORMED FLAP/SLAT OPERATIONAL CHECK PER FIM 27-81-03. PERFORMED FLAP/SLAT GVI WITH FLAPS EXTENDED. NO DEFECTS NOTED. RE
- [SDR SWIA202054931](https://openairdocs.org/sdr/SWIA202054931.md): Skin · nicked · Dec 2, 2020 · N787SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > NICKS ON FUSELAGE SKIN AROUND GROUND AIR SERVICE DOOR FS 1015-FS 1051 STGR 22R-STGR 27. C-CHECK RO 12/28/2020. REPAIRED SKIN AROUND GROUND AIR SERVICE DOOR AT FS 1015.00-FS 1051, STRG 22R-STRG 27, REF REO. LEAK CHECK GOOD.
- [SDR SWIA202054940](https://openairdocs.org/sdr/SWIA202054940.md): Stiffener · cracked · Dec 1, 2020 · N787SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STIFFENER ON AFT WEB FOR PAX DOOR MOTOR IS CRACKED. C-CHECK RO 12/28/2020. REMOVED AND REPLACED STIFFENER P/N 601R317745-7 ON AFT WEB ASSEMBLY, REF CRJ-700 SRM AND DRAWING.
- [SDR SWIA202054930](https://openairdocs.org/sdr/SWIA202054930.md): Frame · corroded · Nov 29, 2020 · N787SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 333.00 IS CORRODED BETWEEN STRG 21L & STRG 20L. C-CHECK RO 12/28/2020. REPLACED 333.00 FRAME SECTION BETWEEN STGR 18L AND STGR 21L WITH NEW FROM STOCK, REF DWG CRJ-700 SRM. COMPLIED WITH SKYWEST TASK CARD.
- [SDR SWIA202054929](https://openairdocs.org/sdr/SWIA202054929.md): Intercostal · cracked · Nov 23, 2020 · N787SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 BETWEEN FS 338.00 AND FS 347.25 IS CRACKED. C-CHECK RO 12/28/2020. REMOVED DAMAGED INTERCOSTAL DD1 BETWEEN FS 338.00 AND FS 347.00, REF CRJ-700 SRM. INSTALLED NEW INTERCOSTAL DD1, P/N 601R31902-318S, REF CRJ-700 SRM AND DRAWING. LEA

Next page: https://openairdocs.org/aircraft/N787SK/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 = 'N787SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N787SK/reports

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