# Service difficulty reports: N630SK

A list on [N630SK](https://openairdocs.org/aircraft/N630SK.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 · 86 reports

- [SDR SWIA2024122301381](https://openairdocs.org/sdr/SWIA2024122301381.md): Floorbeam · corroded · Nov 6, 2024 · N630SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > TOP FLANGE OF FS280 CROSSBEAM AT LBL12 IS CORRODED. (29112136) (C-CHECK RO 12/20/2024) INSTALLED NEW LHS FS280 CROSSBEAM W/L 72.00 REF CRJ700 SRM 51-42-10-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG NO. CC670-34010 REV -K. SE
- [SDR SWIA2024122301380](https://openairdocs.org/sdr/SWIA2024122301380.md): Hinge · damaged · Nov 6, 2024 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > FABRICATE R/H UPPER TRANSCOWL HINGE HALF CN624-2030-207 (C-CHECK RO 12/20/2024) FABRICATED HINGE HALF REF EO NO: CL-600-2C10-54-L08531 REV.A DATE 2024.11.22 USING 15-5 PH HT1025 PO# 5-42720 DRWG CN624-2030 REV-C. COMPLIED WITH SKYWEST TASK CARD: 51-90
- [SDR SWIA202412231106](https://openairdocs.org/sdr/SWIA202412231106.md): Hinge · damaged · Nov 6, 2024 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > FABRICATE L/H LWR TRANSCOWL HINGE HALF CN624-2030-207 (C-CHECK RO 12/20/2024) FABRICATED AND INSTALLED HINGE HALF REF EO NO: CL-600-2C10-54-L08530 REV. A DATE 2024.11.22 USING 15-5 PH HT1025 PO# 5-42720 DRWG CN624-2030 REV-C. COMPLIED WITH SKYWEST
- [SDR SWIA2024122301379](https://openairdocs.org/sdr/SWIA2024122301379.md): Vane · chafed · Nov 5, 2024 · N630SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP, NUMBER TWO VANE ACTUATOR SHAFT IS CHAFED, HN00198352 (C-CHECK RO 12/20/2024) REPAIRED RH INBD FLAP VANE ACTUATOR NO. 2 PER MHIRJ REO# 670-57-52-257, REV -A, 2024-08-20. PERFORMED ELECTRICAL RETRACTION & EXTENSION OF THE FLAPS
- [SDR SWIA202412231105](https://openairdocs.org/sdr/SWIA202412231105.md): Vane · chafed · Nov 5, 2024 · N630SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP, NUMBER ONE VANE ACTUATOR SHAFT IS CHAFED, HN00198345 (C-CHECK RO 12/20/2024) REPAIRED INBOARD FLAP NUMBER ONE VANE ACTUATOR SHAFT, COMPLIED WITH REO 670-57-52-257 REV A DATED 2024-08-20. STEP 5, PERFORMED ELECTRICAL EXTENSION AND
- [SDR SWIA2024122301378](https://openairdocs.org/sdr/SWIA2024122301378.md): Stand Off · cracked · Nov 4, 2024 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 12/20/2024) INSTALLED 1 EA. NEW "A"-BRACKET P/N CN624-2082-201 ON INBD. SIDE OF R/H LOWER TRANSCOWL. REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH STEPS 1-3, AND COMPLIED WI
- [SDR SWIA2024122301377](https://openairdocs.org/sdr/SWIA2024122301377.md): Beam · chafed · Nov 4, 2024 · N630SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > LH INBOARD FLAP FLS24.00 VANE ACTUATOR BEAM CHAFFED (C-CHECK RO 12/20/2024) REPAIRED LH INBOARD FLAP FLS24.00 VANE ACTUATOR BEAM COMPLIED WITH REO 670-57-52-257 REV A DATED 2024-08-20. PERFORMED ELECTRICAL EXTENSION AND RETRACTION OF THE SLATS AND FLAPS
- [SDR SWIA202412231104](https://openairdocs.org/sdr/SWIA202412231104.md): Skin · chafed · Nov 4, 2024 · N630SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH OUTBOARD FLAP INBOARD LOWER LEADING EDGE CHAFFED (C-CHECK RO 12/20/2024) PERFORMED REPAIR ON LH OUTBOARD FLAP PER MHIRJ REO # 670-57-53-388 REV. -- DATED 2024-11-26 AND TASK CARD SKY 51-900-1000 SKY DATE 15 FEB 23. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2024122301376](https://openairdocs.org/sdr/SWIA2024122301376.md): Floorbeam · cracked · Nov 3, 2024 · N630SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACK FOUND @RBL12 COCKPIT FLOOR BEAM FWD OF FS280. (C-CHECK RO 12/20/2024) REMOVED AND INSTALLED NEW FABRICATED RBL12 COCKPIT FLOOR BEAM FS280 - FS265 REF CRJ700 SRM 53-11-43-201-003-A01. COMPLIED WITH SKYWEST TASK CARD: 51-900-1002-SKY.
- [SDR SWIA2024122301375](https://openairdocs.org/sdr/SWIA2024122301375.md): Floor Support · corroded · Nov 3, 2024 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CRAWLWAY FLOOR SUPPORT ANGLE IS CORRODED @ FS280. (C-CHECK RO 12/20/2024) REMOVED AND REPLACED AVIONICS BAY CRAWLWAY FLOOR SUPPORT ANGLE WITH NEW ANGLE ( P/N CC670-34256-3) AT FS 280.00 REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A
- [SDR SWIA202412231103](https://openairdocs.org/sdr/SWIA202412231103.md): Skin · gouged · Nov 3, 2024 · N630SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AFT LOWER EXTERNAL SKIN GOUGED BETWEEN FS977.00 & FS985.00 (C-CHECK RO 12/20/2024) PERFORMED REPAIR OF AFT LOWER EXTERNAL SIN GOUGE BETWEEN FS977.00 AND FS985.00 BY COMPLYING WITH ALL STEPS OF REO 670-53-00-290 REV -F DATE 2019/04/26. PRESSURE LEAK CHEC
- [SDR SWIA202412231102](https://openairdocs.org/sdr/SWIA202412231102.md): Floor Skin · cracked · Nov 2, 2024 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD EQUIPMENT COMPARTMENT, TRU BAY, FLOOR ON THE LEFT SIDE HAS A CRACK EMANATING FROM THE PASS THRU CUT OUT FOR THE FS192.00 FRAME. (C-CHECK RO 12/20/2024) COMPLIED WITH REO 670-53-11-509 REV -E DATE 2018-02-08 FOR LH REPAIR AT TRU BAY FLOOR AT FS 192.
- [SDR SWIA2024122301374](https://openairdocs.org/sdr/SWIA2024122301374.md): Stringer · corroded · Nov 1, 2024 · N630SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 26L BETWEEN FS295 AND FS310 MX TRANS 29087059 (C-CHECK RO 12/20/2024) CORROSION ON STGR26L FORM FS295.00-FS310.00 IS OUT OF LIMITS PER CRJ700SRM 53-21-03-101-002-A01. REMOVED AND INSTALLED 1EA NEW STGR26L FS280.00-FS333.00 PER CRJ700SRM
- [SDR SWIA2024122301373](https://openairdocs.org/sdr/SWIA2024122301373.md): Canister · cracked · Nov 1, 2024 · N630SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK CANISTER 1-3 IS CRACKED (C-CHECK RO 12/20/2024) REPAIRED R/H SLAT TRACK 1-3 CANISTER PER REO 670-57-42-577 REV -- DATE 2016-12-02. FUEL LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA2024122301372](https://openairdocs.org/sdr/SWIA2024122301372.md): Mount · corroded · Nov 1, 2024 · N630SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON ANTENNA MOUNTING PLATE BETWEEN FS295.0 AND FS310.0 STGR27 AND STGR26L (C-CHECK RO 12/20/2024) ANTENNA MOUNTING PLATE BETWEEN FS295 - FS310 IS FOUND TO BE IN A NO DAMAGE ALLOWED AREA THEREFORE IT IS OUT OF LIMITS REF CRJ-700 SRM 53-21-01-101
- [SDR SWIA2024122301371](https://openairdocs.org/sdr/SWIA2024122301371.md): Stringer · corroded · Nov 1, 2024 · N630SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR26R BETWEEN FS280.0 AND FS295.0 AS MARKED (C-CHECK RO 12/20/2024) CORROSION ON STGR26R FS280.00-FS295.00 IS IN A NO DAMAGE ALLOWED AREA PER CRJ700SRM 53-21-03-101-002-A01. REMOVED AND INSTALLED 1EA NEW STGR26R FS280.00-FS333.00 PER CRJ7
- [SDR SWIA20241223101](https://openairdocs.org/sdr/SWIA20241223101.md): Bracket · corroded · Nov 1, 2024 · N630SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR FORWARD FIRE BLANKET BRACKET AT FS1000.00 HAS CORROSION AT LOWER NUT PLATE AS MARKED (C-CHECK RO 12/20/2024) INSTALLED NEW FABRICATED LOWER BRACKET P/N MM670-34120-007, REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING MM670-36021 REV H.
- [SDR SWIA202412231031](https://openairdocs.org/sdr/SWIA202412231031.md): Bulkhead Web · corroded · Oct 31, 2024 · N630SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > EVIDENCE OF CORROSION ON FS280 BLKHD WEB, LBL9 UNDER VERTICAL LEG OF CORROSION CAP. REMOVED DAMAGED AREA AND PERFORMED LHS FS280 LOWER BULKHEAD WEB REPAIR REF. CRJ700 SRM 53-11-10-201-004-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY (CL600-2C10) S
- [SDR SWIA2024122301370](https://openairdocs.org/sdr/SWIA2024122301370.md): Drag Angle · cracked · Oct 22, 2024 · N630SK · Cndair CL6002C10 · Vertical Stabilizer, Plate/Skin
  > RIGHT VERTICAL STAB TO FUSELAGE, AFT DRAG ANGLE POSSIBLY CRACKED. COMPLIED WITH VERTICAL STAB RT AFT DRAG ANGLE REPAIR REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202412230012](https://openairdocs.org/sdr/SWIA202412230012.md): Drag Angle · cracked · Oct 22, 2024 · N630SK · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > LEFT VERTICAL STAB TO FUSELAGE, AFT DRAG ANGLE POSSIBLY CRACKED. LT V-STAB AFT DRAG ANGLE CRACK VERIFIED. REPAIRED CRACKED DRAG ANGLE PER CRJ700SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA2020061251092](https://openairdocs.org/sdr/SWIA2020061251092.md): Stringer · corroded · May 19, 2020 · N630SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > EVALUATE CORROSION ON STR 26R BETWEEN FS280 AND 265. (C-CHECK) RO 6/8/2020 REPAIRED THE STRINGER 26R BETWEEN FS250 TO FS280 REF SRM. LEAK CHECK GOOD COMPLIED WITH TASK CARD.
- [SDR SWIA2020061251091](https://openairdocs.org/sdr/SWIA2020061251091.md): Support Angle · corroded · May 19, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SEVERE CORROSION FOUND ON FS280 FLOOR SUPPORT ANGLE. (C-CHECK) RO 6/8/2020 BLENDED AND EVALUATED FS280 FLOOR SUPPORT ANGLE. FOUND TO BE OUT OF LIMITS. REMOVED AND WET INSTALLED "NEW" FLOOR SUPPORT ANGLE LOCATED AT FS280 AS REQ'D REF DRWG, SRM COMPLIED WITH.
- [SDR SWIA2020061251090](https://openairdocs.org/sdr/SWIA2020061251090.md): Frame · corroded · May 18, 2020 · N630SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS319.00 CORRODED IN MULTIPLE LOCATIONS. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED CORRODED FRAME WITH NEW ( P/N SH670-31891-3) AT FS319.00 BETWEEN STR 17L AND STR 21L, REF DWG AND SRM. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FURTHER DETAILS. CO
- [SDR SWIA2020061251123](https://openairdocs.org/sdr/SWIA2020061251123.md): Seat Track · corroded · May 16, 2020 · N630SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT SEAT TRACK BETWEEN FS 677 AND 863 LBL 9 HAS CORROSION. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED SEAT TRACK WITH FABRICATING SEAT TRACK AT RBL9 FS677-863 REF AMM.
- [SDR SWIA2020061251122](https://openairdocs.org/sdr/SWIA2020061251122.md): Seat Track · corroded · May 16, 2020 · N630SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RT SEAT TRACK BETWEEN FS 677 AND 863 RBL 9 HAS CORROSION. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED SEAT TRACK WITH FABRICATING SEAT TRACK AT RBL9 FS677-863 REF AMM.
- [SDR SWIA2020061251121](https://openairdocs.org/sdr/SWIA2020061251121.md): Seat Track · corroded · May 16, 2020 · N630SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK BETWEEN FS 863. - 988. HAS EVIDENCE OF SURFACE CORROSION AT FS 876, FS 891 AND FS 920. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED REPLACED SEAT TRACK WITH FABRICATING ONE AT RBL9 FS 863.00-FS988.00 REF AMM.
- [SDR SWIA2020061251120](https://openairdocs.org/sdr/SWIA2020061251120.md): Seat Track · corroded · May 16, 2020 · N630SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK BETWEEN FS 863. - 972. HAS EVIDENCE OF SURFACE CORROSION AT FS 890, FS 920 AND FS 935. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED SEAT TRACK WITH FABRICATING ONE AT LBL9 FS 863.00-FS972.00 REF AMM.
- [SDR SWIA2020061251119](https://openairdocs.org/sdr/SWIA2020061251119.md): Seat Track · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 FS597-677 HAS CORROSION. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED SEAT TRACK WITH FABRICATING SEAT TRACK AT LBL9 FS597-677. REF AMM.
- [SDR SWIA2020061251118](https://openairdocs.org/sdr/SWIA2020061251118.md): Seat Track · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL9 FS533-581 HAS CORROSION. (C-CHECK) RO 6/8/2020 REPLACED SEAT TRACK WITH FABRICATING SEAT TRACK AT LBL9 FS533-581. REF AMM.
- [SDR SWIA2020061251117](https://openairdocs.org/sdr/SWIA2020061251117.md): Seat Track · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT RBL9 FS581-677 HAS CORROSION. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED SEAT TRACK WITH FABRICATING SEAT TRACK AT RBL9 FS581-677 REF AMM.
- [SDR SWIA2020061251113](https://openairdocs.org/sdr/SWIA2020061251113.md): Intercostal · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STR 21L FS333-349 IS CORRODED. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED CORRODED INTERCOSTAL/BACK UP SILL WITH NEW ( P/N SH670-31823-1) AT STR 21L BETWEEN FS333.00 AND FS349.00, REF DWG AND SRM. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FURT
- [SDR SWIA2020061251112](https://openairdocs.org/sdr/SWIA2020061251112.md): Intercostal · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STR 21L FS310 333 IS CORRODED. (C-CHECK) RO 6/8/2020 REMOVED AND REPLACED CORRODED INTERCOSTAL/BACK UP SILL WITH NEW ( P/N SH670-31822-1) AT STGR 21L BETWEEN FS310.00 AND FS333.00, REF DWG AND SRM. ALL CHECKS GOOD. SEE CONTINUATION CARD FOR FU
- [SDR SWIA2020061251111](https://openairdocs.org/sdr/SWIA2020061251111.md): Intercostal · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT INTERCOSTAL AT FWD JACK FITTING IS CORRODED. (C-CHECK) RO 6/8/2020 REMOVED CORROSION FROM RT INTERCOSTAL LOWER FLANGE AT FWD JACK FITTING REF SRM. COMPLIED WITH ALL STEPS OF REO. LEAK CHECK GOOD, COMPLIED WITH TASK CARD.
- [SDR SWIA2020061251110](https://openairdocs.org/sdr/SWIA2020061251110.md): Intercostal · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT INTERCOSTAL AT FWD JACK FITTING IS CORRODED. (C-CHECK) RO 6/8/2020 REMOVED CORROSION FROM LT INTERCOSTAL LOWER FLANGE AT FWD JACK FITTING REF SRM. COMPLIED WITH ALL STEPS REO. LEAK CHECK GOOD COMPLIED WITH TASK.
- [SDR SWIA2020061251109](https://openairdocs.org/sdr/SWIA2020061251109.md): Door Sill · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON RT FLOOR SILL AT FS282. (C-CHECK) RO 6/8/2020 PERFORMED ALL STEPS OF PERMANENT DOUBLER REPAIR TO CORROSION ON RT FLOOR SILL AT FS282. REF REO, SEE CONTINUATION CARD FOR DETAILS. LEAKAGE TEST GOOD.
- [SDR SWIA2020061251108](https://openairdocs.org/sdr/SWIA2020061251108.md): Stringer · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STR 27 AT FS296. (C-CHECK) RO 6/8/2020 INSTALLED NEW SERVICEABLE STRINGER 27 BETWEEN FS280 - FS305 REF DRAWING, SRM. COMPLIED WITH PRESSURIZATION OF THE THE AIRCRAFT FOR LEAK CHECK IN REF TO AMM. NO LEAKS NOTED. COMPLIED WITH TASK CARD.
- [SDR SWIA2020061251107](https://openairdocs.org/sdr/SWIA2020061251107.md): Frame · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 313.56 BETWEEN DD4 AND DD5 FWD SIDE CORRODED. (C-CHECK) RO 6/8/2020 REPLACED CORRODED FRAME WITH NEW P/N: 601318086-1 REF DWG AND SRM. TASK CARD COMPLIED WITH. ALL CHECKS GOOD.
- [SDR SWIA2020061251106](https://openairdocs.org/sdr/SWIA2020061251106.md): Door Sill · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT SILL BELOW FLOOR BOARD HAS CORROSION FS1000.00 TO 1051.30 AFT BAGGGAGE BAY DOOR CUT-OUT. (C-CHECK) RO 6/8/2020 DISCARDED DAMAGED PART AND INSTALLED NEW AFT CARGO FLOOR SILL REF SRM, DWG. COMPLIED WITH TASKCARD.
- [SDR SWIA2020061251105](https://openairdocs.org/sdr/SWIA2020061251105.md): Floor Support · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT FLOORBEAM LBL 27 HAS CORROSION FWD AND AFT OF FS1031.00. (C-CHECK) RO 6/8/2020 REPAIRED LT FLOORBEAM LBL 27 LOCATED AT PROXIMATELY FS977.00 TO FS1037.00 REF SRM. COMPLIED WITH TASKCARD.
- [SDR SWIA2020061251104](https://openairdocs.org/sdr/SWIA2020061251104.md): Cleat · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CLEAT ON FWD SIDE INTERCOSTAL AFT DD4 CORRODED. (C-CHECK) RO 6/8/2020 REPLACED CORRODED CLEAT WITH NEW P/N: 600-31902-269 REF DWG AND SRM. TASK CARD COMPLIED WITH.
- [SDR SWIA202061251103](https://openairdocs.org/sdr/SWIA202061251103.md): Intercostal · corroded · May 15, 2020 · N630SK · Cndair CL6002C10 · Passenger/Crew Doors
  > INTERCOSTAL ON FWD SIDE DD4 CORRODED MARKED WITH GREEN TAPE (C-CHECK) RO 6/8/2020. REPLACED CORRODED INTERCOSTAL WITH NEW P/N: 601R318093-1 REF DWG AND SRM. TASK CARD COMPLIED WITH. ALL CHECKS GOOD.
- [SDR SWIA2020061251116](https://openairdocs.org/sdr/SWIA2020061251116.md): Bolt · corroded · May 14, 2020 · N630SK · Cndair CL6002C10 · Rudder Structure
  > FOUND 2EA BOLTS AND 2EA WASHERS CORRODED ON BOTTOM HINGE ANTI-ROTATION LEVERS DURING REMOVAL OF RUDDER. (C-CHECK) RO 6/8/2020 ORDERED AND RECIEVED 2EA BOLTS, 2EA WASHERS AND 9EA COTTER PINS FOR INSTALLATION DETAILS SEE JOB 71032860.
- [SDR SWIA2020061251102](https://openairdocs.org/sdr/SWIA2020061251102.md): Track · damaged · May 14, 2020 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LT UPPER C-DUCT, I/B T/R NYLON SLIDER TRACK, 2 EA SLIDER MOUNTING HOLES FOUND TO BE ELONGATED. (C-CHECK) RO 6/8/2020 COMPLIED WITH REPAIRED ON LT UPPER C-DUCT, I/B T/R NYLON SLIDER TRACK, 2 EA SLIDER MOUNTING HOLES REF REO. FUNCTIONAL TEST GOOD. COMPLIED WTI
- [SDR SWIA2020061251101](https://openairdocs.org/sdr/SWIA2020061251101.md): Lug · chafed · May 10, 2020 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RIGHT ENGINE UPPER THRUST REVERSER HINGE BEAM HINGE LUGS FOR THE FLOATING TIE-BAR ARE CHAFED. (C-CHECK) RO 6/8/2020 REMOVED DAMAGE ON RIGHT ENGINE UPPER THRUST REVERSER HINGE BEAM HINGE LUGS FOR THE FLOATING TIE-BAR REF SRM. RECEIVED ENGINEERING DISPOSITION R
- [SDR SWIA2020061251100](https://openairdocs.org/sdr/SWIA2020061251100.md): Lug · chafed · May 10, 2020 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RIGHT ENGINE LOWER THRUST REVERSER HINGE BEAM HINGE LUGS FOR THE FLOATING TIE-BAR ARE CHAFED. (C-CHECK) RO 6/8/2020 REMOVED DAMAGE ON RIGHT ENGINE LOWER THRUST REVERSER HINGE BEAM HINGE LUGS FOR THE FLOATING TIE-BAR REF SRM. RECEIVED ENGINEERING DISPOSITION R
- [SDR SWIA2020061251099](https://openairdocs.org/sdr/SWIA2020061251099.md): Mount · chafed · May 10, 2020 · N630SK · Cndair CL6002C10 · Engine Mount Section
  > LEFT ENGINE FORWARD MOUNT HAS CHAFING ON THE UPPER AND LOWER SURFACES AT THE COWL HINGE LINE. (C-CHECK) RO 6/8/2020 REMOVED CHAFING FROM THE UPPER AND LOWER SURFACE AT THE COWL HINGE LT ENGINE FWD MOUNT REF SRM. COMPLIED WITH ALL STEPS OF REO. COMPLIED WITH
- [SDR SWIA2020061251098](https://openairdocs.org/sdr/SWIA2020061251098.md): Beam · chafed · May 10, 2020 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT ENGINE UPPER THRUST REVERSER HINGE BEAM UPPER SURFACE IS CHAFED. (C-CHECK) RO 6/8/2020 REMOVED DAMAGE ON LEFT ENGINE UPPER THRUST REVERSER HINGE BEAM UPPER SURFACE REF SRM. RECEIVED ENGINEERING DISPOSITION REO FOR LT UPPER TRANSCOWL HINGE BEAM. COMPLIED S
- [SDR SWIA2020061251097](https://openairdocs.org/sdr/SWIA2020061251097.md): Lug · chafed · May 10, 2020 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT ENGINE UPPER THRUST REVERSER BOX BEAM HINGE LUGS FOR THE FLOATING TIE-BAR ARE CHAFED. (C-CHECK) RO 6/8/2020 COMPLIED WITH THE REPAIRED ON LEFT ENGINE UPPER THRUST REVERSER BOX BEAM HINGE LUGS FOR THE FLOATING TIE-BAR ARE CHAFED PER REO. COMPLIED WITH TAS
- [SDR SWIA2020061251096](https://openairdocs.org/sdr/SWIA2020061251096.md): Lug · chafed · May 10, 2020 · N630SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT ENGINE LOWER THRUST REVERSER BOX BEAM HINGE LUGS FOR THE FLOATING TIE-BAR ARE CHAFED. (C-CHECK) RO 6/8/2020 COMPLIED WITH THE REPAIRED ON LEFT ENGINE LOWER THRUST REVERSER BOX BEAM HINGE LUGS FOR THE FLOATING TIE-BAR CHAFED PER REO AND SRM. COMPLIED WITH
- [SDR SWIA2020061251115](https://openairdocs.org/sdr/SWIA2020061251115.md): Support · corroded · May 9, 2020 · N630SK · Cndair CL6002C10 · Aerodynamic Fairings
  > AFT WING TO BODY FAIRING SUPPORT STRUCTURE SPLICE ANGLE AT FS939 IS CORRODED. (C-CHECK) RO 6/8/2020 AFT WING TO BODY FAIRING SUPPORT STRUCTURE SPLICE ANGLE AT FS939 REPLACED. REF: SRM AND DWG.

Next page: https://openairdocs.org/aircraft/N630SK/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 = 'N630SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N630SK/reports

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