# Service difficulty reports: N785SK

A list on [N785SK](https://openairdocs.org/aircraft/N785SK.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 2 · 90 reports

- [SDR SWIA2025110400923](https://openairdocs.org/sdr/SWIA2025110400923.md): Floorbeam · no discrepancy · Sep 23, 2025 · N785SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > REQUEST TO PERFORM SPLICE REPAIR ON FLOOR BEAM BS 280, RBL12 FOR FOM. PERFORMED REPAIR ON FLOOR BEAM BS 280 RBL12 IAW REO 670-53-11-896 REV-, AND AMM 20-70-00.
- [SDR SWIA2025110400829](https://openairdocs.org/sdr/SWIA2025110400829.md): Slat Track · damaged · Aug 29, 2025 · N785SK · Cndair CL6002C11 · Leading Edge Devices
  > RIGHT SLAT TRACK HAS MULTIPLE GROOVES ON UPPER AND LOWER SIDE. REPAIRED DAMAGE ON THE SLAT TRACK IAW MHIRJ REO 670-57-42-2186 REV-P1, REV--, SRM 51-12-00, AMM 27-81-41, 27-81-00, 27-81-39. INSTALLATION OF SLAT TRACK TO BE ACCOMPLISHED.
- [SDR SWI2025F01508](https://openairdocs.org/sdr/SWI2025F01508.md): Striker · gouged · Aug 6, 2025 · N785SK · Cndair CL6002C11 · Passenger/Crew Doors
  > PASSENGER DOOR SURROUND FWD UPPER SIDE THE SEAL STRIKER IS GOUGED. REPAIRED DAMAGE ON PASSENGER DOOR SURROUND SEAL STRIKER FWD UPPER SIDE IAW SRM 53-21-23, 51-41-02, 51-21-11, 51-25-06, 51-42-06, 51-25-16, AMM 20-70-00.
- [SDR SWIA2025110400806](https://openairdocs.org/sdr/SWIA2025110400806.md): Frame · corroded · Aug 6, 2025 · N785SK · Cndair CL6002C11 · Fuselage Main, Frame
  > FLOOR PANEL 131ALF FRAME LANDING AT FS280 HAS SIGNS OF CORROSION. PERFORMED REPAIR FRAME ON FLOOR PANEL 131ALF LANDING AT FS280.00 STR23L TO STR23R IAW SRM 51-42-15, 51-21-06, MHI RJ REO 670-53-11-2171 REV--(P1), REO 670-53-11-896 REV--, AND REO 670-53-11-21
- [SDR SWIA2025110400730](https://openairdocs.org/sdr/SWIA2025110400730.md): Track · broken · Jul 30, 2025 · N785SK · Cndair CL6002C11 · Engine Thrust Reverser
  > LEFT ENGINE TRANS COWL TRACK LOWER NYLON INSERT SCREW BROKEN AND HAVE GOUGE AND HOLE ELONGATED. REPAIRED HOLES FOR NYLON ATTACH SCREWS ON LH ENGINE LOWER TRANSCOWL IAW SRM 54-21-00 AND REO 670-78-30-921 REV-B DATE 2014-07-02.
- [SDR SWIA202505050002](https://openairdocs.org/sdr/SWIA202505050002.md): Windshield · cracked · May 2, 2025 · N785SK · Cndair CL6002C11 · Flight Compartment Windows
  > LEFT SIDE WINDSHIELD CRACKING DURING FLIGHT, L WSHLD HEAT CAUTION MESSAGE OCCURRED AFTER NOTICING THE CRACKING. FOLLOWED QRH CRACKING STOPPED. (FLIGHT 5336 - FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30075796 WITH THE FOLLOWING CORRECTIVE ACTI
- [SDR SWI2025F00072](https://openairdocs.org/sdr/SWI2025F00072.md): Structure · damaged · Jan 17, 2025 · N785SK · Cndair CL6002C11 · Fuselage Main, Structure
  > DUE TO EXISTING PILOT HOLES THERE ARE TWO OVERSIZE HOLES COMMON TO THE LH PRESSURE BOX AND LBL18, MARKED. (FILED CLOSED) COMPLIED WITH ALL STEPS OF THIS REO 670-53-41-712 REV. - - DATED 2025-01-22 FOR INSTALLATION OF INSTALL TWO HI- LITE PIN AT FS838.00
- [SDR SWI2025F00320](https://openairdocs.org/sdr/SWI2025F00320.md): Angle · damaged · Jan 10, 2025 · N785SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > FWD LH SILL SEALING ANGLE AT FS693 AND LBL36 HAS TWO MISDRILLED HOLES. MARKED (FILED CLOSED) INSTALLED NEW FWD LH SILL SEALING ANGLE AT FS693 AND LBL36 IAW DWG SH670-35920 REV M AND REF CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD WITH NO LEAKS NOTE
- [SDR SWI2025F00069](https://openairdocs.org/sdr/SWI2025F00069.md): Door Sill · damaged · Jan 10, 2025 · N785SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > FWD LH SILL SEALING ANGLE AT FS693 AND LBL36 HAS TWO MISDRILLED HOLES. MARKED (FILED OPEN) INSTALLED NEW FWD LH SILL SEALING ANGLE AT FS693 AND LBL36 IAW DWG SH670-35920 REV M AND REF CRJ700 SRM 51-42-06-001-001-A01. LEAK CHECK GOOD WITH NO LEAKS NOTED.
- [SDR SWIA202265875](https://openairdocs.org/sdr/SWIA202265875.md): None · shutdown · Jun 4, 2022 · N785SK · Cndair CL6002C10 · Ice/Rain Protection System
  > R COWL A/I DUCT WARNING MESSAGE ON CLIMB-OUT. COMPLIED WITH QRH PROCEDURE, WARNING MESSAGE PERSISTED, DIVERTED TO BNA. (FLIGHT 5772 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 24937741 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT
- [SDR SWIA202156551](https://openairdocs.org/sdr/SWIA202156551.md): Drain Valve · misinstalled · Feb 15, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING INCORPORATION OF SB 670BA-53-057 FUSELAGE - CENTER FUSELAGE - MODIFICATION OF THE DRAIN VALVES IN THE CENTER FUSELAGE BETWEEN FS280.00 AND FS333.00. FORWARD LH AND RH DRAIN DOUBLERS BETWEEN FS280 - FS295 FOUND TO BE INSTALLED AT INCORRECT LOCATIONS (C
- [SDR SWIA202156549](https://openairdocs.org/sdr/SWIA202156549.md): Intercostal · cracked · Feb 11, 2021 · N785SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1 (UPPER AFT CORNER) HAS VISUALLY IDENTIFIED CRACK ON FLANGE (C-CHECK) RO 3/2/2021 REPLACED PAX DOOR INTERCOSTAL DD1. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV -N. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-S
- [SDR SWIA202156568](https://openairdocs.org/sdr/SWIA202156568.md): Seat Track · corroded · Feb 10, 2021 · N785SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON R/H SIDE SEAT TRACK P/N SH670-36261 BETWEEN F.S.784.00 AND F.S. 855.00 AT NUMEROUS LOCATIONS (C-CHECK) RO 3/2/2021 NEW SIDE SEAT TRACK P/N SH670-36261-5 FABRICATED USING EXTRUSION P/N 20276-288-0-0A, P/O# T58082 PER CRJ700 SRM 53-00-49-2
- [SDR SWIA202156548](https://openairdocs.org/sdr/SWIA202156548.md): Angle · corroded · Feb 10, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFTER REMOVAL OF PAX DOOR LOWER SILL AREA, MID CAP ANGLE, FOUND THE KICKPLATE ANGLE TO BE EXFOLIATED (C-CHECK) RO 3/2/2021 REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED PAX DOOR SURROUND KICKPLATE ANGLE IAW CRJ700 SRM 51-42-06-001-001-
- [SDR SWIA202156547](https://openairdocs.org/sdr/SWIA202156547.md): Intercostal · corroded · Feb 10, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE ACCESSING FOR 320.00 FRAME DD0 INTERCOSTAL FOUND TO BE CORRODED. (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND INTERCOSTAL TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV -N. COMPLIED WITH TASK
- [SDR SWIA202156546](https://openairdocs.org/sdr/SWIA202156546.md): Bracket · corroded · Feb 8, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE ACCESSING 320.00 FRAME FOUND BRACKET COMMON TO INTERCOSTAL DD7 ATTACHING TO FWD FORMER CORRODED. (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND BRACKET TO BE OUT OF LIMITS. REPLACED BRACKET REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG: 601R31702 R
- [SDR SWIA202156545](https://openairdocs.org/sdr/SWIA202156545.md): Bracket · corroded · Feb 8, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE ACCESSING 320.00 FRAME FOUND BRACKET COMMON TO INTERCOSTAL DD6 ATTACHING TO FWD FORMER CORRODED. (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND BRACKET TO BE OUT OF LIMITS. REPLACED BRACKET REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 RE
- [SDR SWIA202156544](https://openairdocs.org/sdr/SWIA202156544.md): Bracket · corroded · Feb 8, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE ACCESSING 320.00 FRAME FOUND BRACKET COMMON TO INTERCOSTAL DD3 CORRODED. (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND BRACKET TO BE OUT OF LIMITS. REPLACED BRACKET REF DWG 601R31702 REV-N AND CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK
- [SDR SWIA202156543](https://openairdocs.org/sdr/SWIA202156543.md): Floorbeam · corroded · Feb 5, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFTER REMOVING COCKPIT FLOOR AFT SUPPORT FOUND RH FS280 CROSSBEAM TO HAVE CORROSION (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED RH FS 280.00 NEW CROSSBEAM P/N CC670-34094-2S REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-3401
- [SDR SWIA202156542](https://openairdocs.org/sdr/SWIA202156542.md): Floorbeam · corroded · Feb 5, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFTER REMOVING COCKPIT FLOOR AFT SUPPORT FOUND LH FS280 CROSSBEAM TO HAVE CORROSIONREMOVED AND REPLACED LH FS 280.00 NEW CROSSBEAM P/N CC670-34094-1S REF CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010 REV -K, COMPLIED WITH TAS
- [SDR SWIA202156541](https://openairdocs.org/sdr/SWIA202156541.md): Intercostal · corroded · Feb 5, 2021 · N785SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR DD6 INTERCOSTAL FOUND TO BE CORRODED (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND INTERCOSTAL TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWIA202156540](https://openairdocs.org/sdr/SWIA202156540.md): Door Frame · corroded · Feb 5, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FS320.00 FRAME FOUND TO BE CORRODED (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND FRAME TO BE OUT OF LIMITS. REPLACED FRAME REF CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWIA202156539](https://openairdocs.org/sdr/SWIA202156539.md): Bulkhead Web · cracked · Feb 3, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > AFTER REMOVAL OF RH FS280 LOWER BULKHEAD WEB FOUND CRACK IN ANGLE, BL26.00 FS280.00 (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED NEW ANGLE P/N CC670-34117-6 ON RH FS280 LOWER BULKHEAD WEB REF CRJ700 SRM 51-42-06-001-001-A01 AND DGW CC670-34010 REV-K CO
- [SDR SWIA202156567](https://openairdocs.org/sdr/SWIA202156567.md): Door Frame · corroded · Feb 2, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H EMER DOOR FRAME - AFT DOOR STOP - FS'S 785 - BTWN STGRS 10/11L - HDWR CORRODED AS MARKED (C-CHECK) RO 3/2/2021 INSTALLED 2EA NEW BOLTS, WASHERS AND NUTS. REF CRJ 700 AMM 20-21-00-910-801 (CONFIG A01) TOOL: 8612 CAL DUE: 31 OCT '21
- [SDR SWIA202156566](https://openairdocs.org/sdr/SWIA202156566.md): Door Frame · corroded · Feb 2, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Structure
  > L/H EMER DOOR FRAME SILL - AFT SPIGOT RETAINER - AFT OTBD RETAINING HDWR CORRODED (C-CHECK) RO 3/2/2021 INSTALLED NEW HARDWARE. REF CRJ 700 AMM 20-21-00-910-801 (CONFIG A01) / TOOL: 8612 CAL DUE:31OCT21
- [SDR SWIA202156538](https://openairdocs.org/sdr/SWIA202156538.md): Bulkhead Web · corroded · Feb 2, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > AFTER REMOVAL OF RH FS280 CROSSBEAM FOUND RH FS280 LOWER BULKHEAD WEB TO HAVE PITTING CORROSION (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED RH FS 280.00 LOWER WEB AND RH FS280.00 BUTTSTRAP REF CRJ700 SRM 53-11-10-201-004-A01 REV 38 JUL 25/2020. COMPLIED W
- [SDR SWIA202156537](https://openairdocs.org/sdr/SWIA202156537.md): Bulkhead Web · corroded · Feb 2, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > AFTER REMOVAL OF LH FS280 CROSSBEAM FOUND LH FS280 LOWER BULKHEAD WEB TO HAVE PITTING CORROSION (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED LH FS280.00 LOWER WEB AND LH FS 280.00 BUTTSTRAP REF CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-90
- [SDR SWIA202156553](https://openairdocs.org/sdr/SWIA202156553.md): Attach Angle · cracked · Jan 30, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > ATTACHMENT CLIP AT STRG (24L) AND F.S. 1098.20 (AFT) SIDE OF REAR PRESSURE BULKHEAD, FOUND (CRACKED) IN RADIUS (MARKED). (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED WITH NEW PART: MM670-35192-001 REF CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.
- [SDR SWIA202156536](https://openairdocs.org/sdr/SWIA202156536.md): Bracket · cracked · Jan 30, 2021 · N785SK · Cndair CL6002C10 · Wing, Attach Fittings
  > * LH 1-3 FUEL TANK SLAT TRACK CANISTER MOUNT BRACKET CRACKED. (C-CHECK) RO 3/2/2021 PERFORMED REPAIR TO SLAT CANSITER NO. 3, SLAT TRACK 1-3, LHS REF REO 670-57-42-577 REV -- 2016-12-02. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202156535](https://openairdocs.org/sdr/SWIA202156535.md): Bracket · cracked · Jan 30, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > RH 1-3 FUEL TANK SLAT TRACK CANISTER MOUNT BRACKET CRACKED. (C-CHECK) RO 3/2/2021 PERFORMED REPAIR TO SLAT CANISTER NO. 3, SLAT TRACK 1-3, RHS REF REO 670-57-42-577 REV -- 2016-12-02. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202156534](https://openairdocs.org/sdr/SWIA202156534.md): Skin · dented · Jan 29, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > THE EXTERNAL FWD FUSELAGE AT FS411.0 ABOVE 2.00 IN OF STGR 15L HAS A DENT (C-CHECK) RO 3/2/2021 REPAIRED FUSELAGE SKIN BETWEEN FS394.00 - FS421.00 AND STR 14L - STR16L REF REO 670-53-21-1947 REV -- 2021-02-09. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900
- [SDR SWIA202156574](https://openairdocs.org/sdr/SWIA202156574.md): Link · chafed · Jan 26, 2021 · N785SK · Cndair CL6002C10 · Aileron Control System
  > RH AILERON - OUTBOARD POWER CONTROL UNIT OUTPUT LINK CHAFED (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED RH AILERON OUTBOARD POWER CONTROL UNIT LINK / REF CRJ700 AMM 27-14-15-000-801 A01 AND CRJ700 AMM 27-14-15-400-801 A01 / CHECKS GOOD, SEE CONTINUATION CA
- [SDR SWIA202156573](https://openairdocs.org/sdr/SWIA202156573.md): Link · chafed · Jan 26, 2021 · N785SK · Cndair CL6002C10 · Aileron Control System
  > RH AILERON - INBOARD POWER CONTROL UNIT OUTPUT LINK CHAFED (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED RH AILERON INBOARD POWER CONTROL UNIT LINK / REF CRJ700 AMM 27-14-15-000-801 A01 AND CRJ700 AMM 27-14-15-400-801 A01 / CHECKS GOOD, SEE CONTINUATION CARD
- [SDR SWIA202156572](https://openairdocs.org/sdr/SWIA202156572.md): Link · chafed · Jan 26, 2021 · N785SK · Cndair CL6002C10 · Aileron Control System
  > LH AILERON - INBOARD POWER CONTROL UNIT OUTPUT LINK CHAFED (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED LH AILERON INBOARD POWER CONTROL UNIT LINK / REF CRJ700 AMM 27-14-15-000-801 A01 AND CRJ700 AMM 27-14-15-400-801 A01 / CHECKS GOOD, SEE CONTINUATION CARD
- [SDR SWIA202156565](https://openairdocs.org/sdr/SWIA202156565.md): Hinge · corroded · Jan 26, 2021 · N785SK · Cndair CL6002C10 · Ailerons
  > RH AILERON - HINGE 1-2-3 & 4 WITH THE WASHERS & BOLTS CORRORED AT ALL THE RETAINING PLATES (C-CHECK) RO 3/2/2021 ORDERED AND RECEIVED WASHERS AND BOLTS FOR ALL RETAINING PLATES AT RH AILERON HINGES 1-2-3 & 4, HARDWARE INSTALLED ON CAMP # 22032683 JOB 7102
- [SDR SWIA202156564](https://openairdocs.org/sdr/SWIA202156564.md): Hinge · corroded · Jan 26, 2021 · N785SK · Cndair CL6002C10 · Ailerons
  > LH AILERON - HINGE 1-2-3 & 4 WITH THE WASHERS & BOLTS CORRORED AT ALL THE RETAINING PLATES (C-CHECK) RO 3/2/2021 ORDERED AND RECEIVED WASHERS AND BOLTS FOR ALL RETAINING PLATES AT LH AILERON HINGES 1-2-3 & 4, HARDWARE INSTALLED ON CAMP # 22032682 JOB 7102
- [SDR SWIA202156563](https://openairdocs.org/sdr/SWIA202156563.md): Seat Track · corroded · Jan 26, 2021 · N785SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL MOUNTING EXTRUSION CORRODED IN MULTIPLE SPOTS FROM F.S.785.00 TO F.S.797.00 AT STR.15R (MARKED). (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED RH SEAT TRACK TRIM RETAINER REF SNIEO SH670-300
- [SDR SWIA202156577](https://openairdocs.org/sdr/SWIA202156577.md): Skin · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD WEB CORRODED AROUND FASTENER HOLES. (C-CHECK) RO 3/2/2021 REMOVED CORROSION FROM PAX DOOR FWD WEB REF CRJ 700 SRM 51-21-06-001-001-A01. EVALUATED AND FOUND TO BE OUT OF LIMITS. ORDERED AND RECEIVED NEW PAX DOOR FWD WEB. INSTALLATION OF PAX DOO
- [SDR SWIA202156575](https://openairdocs.org/sdr/SWIA202156575.md): Stop Fitting · broken · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD BAGGAGE BAY DOOR - FWD INBOARD STOP BOLT ASSY HAS BROKEN SAFETY AS MARKED (C-CHECK) RO 3/2/2021 INSTALLED FWD BAGGAGE BAY DOOR- FWD INBOARD STOP BOLT SAFETY CABLE. CRJ 700 AMM 20-51-00-400-802 A01
- [SDR SWIA202156562](https://openairdocs.org/sdr/SWIA202156562.md): Angle · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER ANGLE IS CORRODED AROUND FASTENER HOLES. (C-CHECK) RO 3/2/2021 REMOVED AND REPLACED PAX DOOR LOWER ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01
- [SDR SWIA202156561](https://openairdocs.org/sdr/SWIA202156561.md): Web · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT WEB CORRODED AROUND FASTENER HOLES AND MARKED SPOT BETWEEN TO ACESS POINTS.. (C-CHECK) RO 3/2/2021 REMOVED CORROSION FROM PAX DOOR AFT WEB REF CRJ 700 SRM 51-21-06-001-001-A01. EVALUATED AND FOUND TO BE OUT OF LIMITS. ORDERED AND RECEIVED NEW
- [SDR SWIA202156552](https://openairdocs.org/sdr/SWIA202156552.md): Track · cracked · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > *AFT CARGO DOOR - AFT DOOR TRACK LOWER SUPPORT BRACKET IS CRACKED. (MARKED) (C-CHECK) RO 3/2/2021 REMOVED AND INSTALLED NEW CHANNEL P/N-MM670-35552-005 ON AFT CARGO DOOR - AFT DOOR LOWER TRACK. REF CRJ-700 SRM-51-42-06-001-001-A01 & SRM 51-42-21-001-001-A0
- [SDR SWIA202156533](https://openairdocs.org/sdr/SWIA202156533.md): Door Sill · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR LOWER SILL FWD TOP CAP ANGLE FOUND TO BE CORRODED (C-CHECK) RO 3/2/2021 REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED FWD CAP ANGLE IAW CRJ 700 SRM 51-42-06-001-A01, 51-42-21-001-001-A01, AND DWG SH670-31810 REV AE, COMPLIED W
- [SDR SWIA202156532](https://openairdocs.org/sdr/SWIA202156532.md): Door Sill · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *AFT CARGO DOOR - DOOR SILL IS CORRODED ACROSS MULTIPLE ELEMENTS. (MARKED) (C-CHECK) RO 3/2/2021 REMOVED OLD DOOR SILL, AND REPLACED WITH NEW SILL PER DWG: MM670-35085 REV L & CRJ-700 SRM 51-41-06-001-001-A01 & CRJ-700 SRM 51-41-21-001-001A01. COMPLIED WITH
- [SDR SWIA202156531](https://openairdocs.org/sdr/SWIA202156531.md): Intercostal · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > PAX DOOR INTERCOSTAL DD6 CORRODED. (MARKED) (C-CHECK) RO 3/2/2021 REMOVED CORROSION AND FOUND INTERCOSTAL TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD
- [SDR SWIA202156530](https://openairdocs.org/sdr/SWIA202156530.md): Intercostal · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > PAX DOOR INTERCOSTAL DD3 CORRODED AT NUT PLATE. REMOVED CORROSION AND FOUND INTERCOSTAL TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV-N. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202156529](https://openairdocs.org/sdr/SWIA202156529.md): Intercostal · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR SURROUND FWD LATCH PIN INTERCOSTAL AT 27R, FS364 - FS349 FOUND TO BE CORRODED AT ATTACH FLANGE (C-CHECK) RO 3/2/2021 REPLACED THE AVIONICS BAY DOOR SURROUND LATCH PIN INTERCOSTAL AT FS349.00 - FS364.00 STGR 27R. REF CRJ700 SRM 51-42-06-00
- [SDR SWIA202156528](https://openairdocs.org/sdr/SWIA202156528.md): Intercostal · corroded · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR SURROUND FWD LATCH PIN INTERCOSTAL AT 27L, FS364 - FS349 FOUND TO BE CORRODED AT ATTACH FLANGE (C-CHECK) RO 3/2/2021 REMOVED AND REPLCED AVIONICS BAY DOOR FWD LATCH PIN INTERCOSTAL. REF CRJ700 SRM 51-42-06-001-001-A01, REF CRJ700 SRM 51-4
- [SDR SWIA202156527](https://openairdocs.org/sdr/SWIA202156527.md): Fitting · damaged · Jan 25, 2021 · N785SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > R/H WING TO BODY MOUNT - FS 797 - AFT SIDE - INBOARD WEB HAS EVIDENCE OF IMPACT DAMAGE - AS MARKED (C-CHECK) RO 3/2/2021 BLENDED CHAFE ON RH WING TO BODY MOUNT FITTING FS797 AFT INBD LOCATION AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO 670-57-11
- [SDR SWIA202156576](https://openairdocs.org/sdr/SWIA202156576.md): Seat Track · gouged · Jan 23, 2021 · N785SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES WITH HIGH METAL FOUND ON L/H FLOOR SEAT TRACK (LBL 27.00), AT SEAT LOCK DOWN LOCATIONS (AFT) OF F.S. 364.00 AND (FWD) OF F.S. 409.00 (MARKED). (C-CHECK) RO 3/2/2021 CORROSION ON L/H FLOOR SEAT TRACK LBL 27.00, FS 364.00 TO FS 409.00, FOUND TO BE OU

Next page: https://openairdocs.org/aircraft/N785SK/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 = 'N785SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N785SK/reports

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