# Service difficulty reports: N611SK

A list on [N611SK](https://openairdocs.org/aircraft/N611SK.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 9 · 414 reports

- [SDR SWIA2026071477503](https://openairdocs.org/sdr/SWIA2026071477503.md): Slat Track · corroded · Jul 14, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE RIGHT SLAT TRACK 3-2. REMOVED AND INSTALLED NEW SERVICEABLE RT SLAT TRACK 3-2 IAW AMM27-81-41-000-802-A01, AND AMM27-81-41-400-802-A01.
- [SDR SWIA2026071477502](https://openairdocs.org/sdr/SWIA2026071477502.md): Slat Track · corroded · Jul 14, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE RIGHT SLAT TRACK 3-1. REMOVED AND INSTALLED NEW SERVICEABLE RT SLAT TRACK 3-1 IAW AMM27-81-41-000-801-A01 AND AMM 27-81-41-400-801-A01.
- [SDR SWIA2026071477501](https://openairdocs.org/sdr/SWIA2026071477501.md): Slat Track · corroded · Jul 14, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE RIGHT SLAT TRACK 2-3. REMOVED AND INSTALLED SERVICEABLE, RT SLAT TRACK 2-3 USING NEW COTTER PINS IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01OPS TEST GOOD.
- [SDR SWIA2026071377500](https://openairdocs.org/sdr/SWIA2026071377500.md): Slat Track · corroded · Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE RIGHT SLAT TRACK 2-2. REMOVED AND INSTALLED SERVICEABLE, RT SLAT TRACK 2-2 USING NEW COTTER PINS AND SAFETY CABLES IAW AMM 27-81-41-000-802 A01 AND AMM 27-81-41-400-802 A01.
- [SDR SWIA2026071377499](https://openairdocs.org/sdr/SWIA2026071377499.md): Slat Track · corroded · Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE RIGHT HAND SLAT TRACK 2-1. REMOVED AND INSTALLED SERVICEABLE SLAT TRACK 2-1 USING NEW COTTER PINS AND SAFETY CABLE IAW AMM 27-81-41-000-801 A01, AND AMM 27-81-41-400-801 A01.
- [SDR SWIA2026071377496](https://openairdocs.org/sdr/SWIA2026071377496.md): Slat Track · corroded · Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE LT SLAT TRACK 3-2. REMOVED AND INSTALLED A NEW SLAT TRACK 3-2 IAW AMM 27-81-41-400-802-A01.
- [SDR SWIA2026071377495](https://openairdocs.org/sdr/SWIA2026071377495.md): Slat Track · corroded · Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE LT SLAT TRACK 2-3. INSTALLED A NEW LT SLAT TRACK 2-3, IAW AMM 27-81-41-400-801-A01.
- [SDR SWIA2026071377494](https://openairdocs.org/sdr/SWIA2026071377494.md): Slat Track · corroded · Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE LT SLAT TRACK 2-2. REMOVED AND INSTALLED A NEW LT SLAT TRACK 2-2 IAW AMM 27-81-41-400-802-A01.
- [SDR SWIA2026071377436](https://openairdocs.org/sdr/SWIA2026071377436.md): Slat Track · not reported · Jul 13, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE LH SLAT TRACK 3-3. REMOVED AND INSTALLED THE LH SLAT TRACK 3-3 AT LT WING, IAW AMM27-81-41-000-803-A01 AND AMM27-81-41-400-803-A01
- [SDR SWIA2026071277504](https://openairdocs.org/sdr/SWIA2026071277504.md): Slat Track · corroded · Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVED AND REPLACED LH SLAT TRACK 1-2. REMOVED AND INSTALLED NEW SLAT TRACK 1-2 IAW AMM 27-81-41-400-802-A01.
- [SDR SWIA2026071277498](https://openairdocs.org/sdr/SWIA2026071277498.md): Slat Track · corroded · Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE RIGHT HAND SLAT TRACK 1-3. REMOVED AND INSTALLED SERVICEABLE, PN, RH SLAT TRACK 1-3 USING NEW COTTER PINS IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01.
- [SDR SWIA2026071277497](https://openairdocs.org/sdr/SWIA2026071277497.md): Slat Track · corroded · Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE RIGHT HAND SLAT TRACK 1-1. REMOVED AND INSTALLED A NEW,, RT WING SLAT TRACK 1-1 IAW AMM 27-81-41-000-801 A01 AND AMM 27-81-41-400-801 A01.
- [SDR SWIA2026071277492](https://openairdocs.org/sdr/SWIA2026071277492.md): Slat Track · corroded · Jul 12, 2026 · N611SK · Cndair CL6002C10 · Leading Edge Devices
  > REMOVE AND REPLACE LT SLAT TRACK 1-3. INSTALLED A NEW LT SLAT TRACK 1-3 IAW AMM 27-81-41-400-801-A01.
- [SDR SWIA2026050777454](https://openairdocs.org/sdr/SWIA2026050777454.md): Skin · corroded · May 7, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN FS310 AND FS319, STR25L TO STR26L. REPAIRED INNER SKIN IAW REO 670-53-21-2887 REV-.
- [SDR SWIA2026050677414](https://openairdocs.org/sdr/SWIA2026050677414.md): Support · damaged · May 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUR ELONGATED HOLES FOUND IN BACKUP SILL ON STGR21L FROM FS333 TO FS349. REPLACED BACKUP SILL ON STGR21 AT FS333 TO FS349 WITH NEW PART REF SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV AE
- [SDR SWIA2026050277509](https://openairdocs.org/sdr/SWIA2026050277509.md): Angle · damaged · May 2, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING INSTALLATION OF FASTENERS EDGE DAMAGE CREATED ON REINFORCEMENT ANGLE BS 333, BETWEEN STR 21R TO 22R. REPAIRED REINFORCEMENT ANGLE IAW REO 670-53-21-2883, REV -.
- [SDR SWIA2026042477437](https://openairdocs.org/sdr/SWIA2026042477437.md): Skin · dented · Apr 24, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > PROTRUDING DENT FOUND ON FUSELAGE SKIN BETWEEN FS 333 AND FS 349, AND BETWEEN STR23L AND STR24L. PERFORMED CUTOUT OF DENT AND APPLIED DOUBLER AT FUSELAGE SKIN BETWEEN FS333 - FS349, STGR 23L - 24L REF REO 670-53-21-2876 REV --.
- [SDR SWIA2026042077463](https://openairdocs.org/sdr/SWIA2026042077463.md): Stringer Splice · corroded · Apr 20, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE 22L, BS 477. REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, & DWG SH670-30006, REV A.
- [SDR SWIA2026041677346](https://openairdocs.org/sdr/SWIA2026041677346.md): Stringer Splice · corroded · Apr 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRG 21 RT SPLICE AT CIRCUMFERENTIAL JOINT AT FS 477.4. REPLACED STRINGER SPLICE AT STGR21R, FS477 REF SRM 51-42-06-001-001-A01 AND DWG SH670-30006 REV A.
- [SDR SWIA2026041377369](https://openairdocs.org/sdr/SWIA2026041377369.md): Fitting · chafed · Apr 13, 2026 · N611SK · Cndair CL6002C10 · Main Landing Gear
  > LEFT MLG SIDE STAY FITTING HAS A MULTIPLES CHAFES AND GOUGES. REMOVED THE CHAFED AREAS ON LT MLG SIDE STAY FITTING IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS 1-5 REF REO 670-57-11-261, REV --.
- [SDR SWIA2026040977419](https://openairdocs.org/sdr/SWIA2026040977419.md): Skin · corroded · Apr 9, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN BS 280 & 295, STR 24R -25R. PERFORMED A CUT OUT OF THE CORRODED FUSELAGE SKIN BTWN BS 280 - 310, STR 24R - 26R AND APPLIED DOUBLER IAW REO 670-53-21-2866, REV -.
- [SDR SWIA2026040877489](https://openairdocs.org/sdr/SWIA2026040877489.md): Seat Track · corroded · Apr 8, 2026 · N611SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK, BS 847 - 879, SCRATCHED AND CORRODED. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A01.
- [SDR SWIA2026040877440](https://openairdocs.org/sdr/SWIA2026040877440.md): Frame · fom · Apr 8, 2026 · N611SK · Cndair CL6002C10 · Standard Practices/Structures
  > REMOVE AND SPLICE FRAME FS 485, STR20R FROM STR26R TO FOM. PERFORMED SPLICE REPAIR OF FRAME AT FS485, STGR26R - STGR20R REF REO 670-53-31-1193 REV -, SRM 53-00-06-201-001-A03, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-33200 REV G.
- [SDR SWIA2026040877435](https://openairdocs.org/sdr/SWIA2026040877435.md): Frame · fom · Apr 8, 2026 · N611SK · Cndair CL6002C10 · Standard Practices/Structures
  > REMOVE AND SPLICE FRAME FS 469, STR20L FROM STR23L TO FOM C-CHECK RO 09302026REMOVED AND SPLICED FRAME FS469, FROM STR20L TO STR23L BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2857 REV -, SRM 53-00-06-201-001-A03, SRM 51-42-21-001-001-A01, 51-42-06-001-001
- [SDR SWIA2026040677472](https://openairdocs.org/sdr/SWIA2026040677472.md): Angle · damaged · Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TWO ELONGATED HOLES FOUND IN REINFORCEMENT ANGLE AT BS 333, STR 21L. REPLACED REINFORCEMENT ANGLE AT BS 333, STRINGER 21L IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31810, REV AE.
- [SDR SWIA2026040677464](https://openairdocs.org/sdr/SWIA2026040677464.md): Support · damaged · Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TWO ELONGATED HOLES FOUND IN BACKUP SILL ON STR 21L FROM BS 295 - 333. REPLACED THE BACKUP SILL ON STR 21L BTWN BS 295 - 333 IAW SRM 51-42-06-001-001-A01, REV 38, & DWG SH670-31810, REV AE.
- [SDR SWIA2026040677434](https://openairdocs.org/sdr/SWIA2026040677434.md): Frame · damaged · Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Frame
  > TWO ELONGATED HOLES FOUND IN FRAME AT FS 333 STR 21L. REPLACED FRAME AT BS 333, STR 21L IAW SRM 51-42-21-001-001-A01, & DWG SH670-31810, REV AE.
- [SDR SWIA2026040677376](https://openairdocs.org/sdr/SWIA2026040677376.md): Frame Splice · damaged · Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Frame
  > TWO ELONGATED HOLES FOUND IN FRAME SPLICE AT BS 333, STR 21L. REPLACED THE FRAME SPLICE IAW SRM 51-42-06-001-001-A01, AND DWG SH670-31810, REV AE.
- [SDR SWIA2026040677351](https://openairdocs.org/sdr/SWIA2026040677351.md): Stringer Splice · damaged · Apr 6, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > TWO ELONGATED HOLES FOUND UPPER STRINGER SPLICE 21L, BS 333. REPLACED UPPER STRINGER SPLICE 21L, BS 333 IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.
- [SDR SWIA2026040477396](https://openairdocs.org/sdr/SWIA2026040477396.md): Floor Support · corroded · Apr 4, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ON REMOVAL OF THE LT FLOOR SUPPORT, BS 533 - 581 FOUND TO BE CORRODED. REPAIRED THE FLOOR SUPPORT, BTWN BS 333 - 581, IAW REO 670-53-21-2855, REV -. AND DWG SH670-32170, REV V.
- [SDR SWIA2026040377388](https://openairdocs.org/sdr/SWIA2026040377388.md): Cleat · corroded · Apr 3, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON 3EA CLEATS ON STR20L AT FS 453, FS 364, FS 379. REMOVED AND REPLACED WITH NEW CLEATS 3EA ON STGR20L AT FS364, FS379 AND FS453 PER CRJ700 SRM 51-42-06-001-001-A01, DWG SH670-32050 REV J AND DWG SH670-31401 REV A COMPLIED WITH TASK CARD 51-9
- [SDR SWIA2026040377370](https://openairdocs.org/sdr/SWIA2026040377370.md): Stringer Splice · corroded · Apr 3, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE 20L, BS 477. REPLACED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, AND DWG SH670-30006, REV A.
- [SDR SWIA2026040277412](https://openairdocs.org/sdr/SWIA2026040277412.md): Bulkhead · corroded · Apr 2, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS280 BULKHEAD RH DOOR POST AT WL795 RBL9 HAS CORROSION. PERFORMED REPAIR ON FS280 BULKHEAD RH DOOR POST AT WL795 RBL9 IAW REF 53-11-10-201-006-A01 REV 38, SRM 51-42-10-001-001-A01 REV 38 AND SRM 51-42-13-001-001-A01 REV 38
- [SDR SWIA2026033177474](https://openairdocs.org/sdr/SWIA2026033177474.md): Bracket · damaged · Mar 31, 2026 · N611SK · Cndair CL6002C10 · Wing Miscellaneous Structure
  > REAR SPAR LARTERAL BEAM, LT & RT AFT OTBD HOLE IN FITTING HAVE TWO DEFECTS IN EACH LT AFT OTBD HOLE IN SPAR HAS ONE DEFECT. REAMED DEFECTS IN LT & RT SIDE STAY BRACKETS FRAME SECTOR BETWEEN LBL45, RBL 45 UNTIL NO DEFECTS NOTED. INSTALLED OVERSIZE FASTENERS
- [SDR SWIA2026032677457](https://openairdocs.org/sdr/SWIA2026032677457.md): Angle · cracked · Mar 26, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING AUDIT OF TASK CARD 32-710-125 IT WAS FOUND THAT THE NLG WHEEL WELL, AFT BULKHEAD FS 235, CANTED BULK HEAD BACK UP ANGLE SHOWING SIGNS OF A CRACK. REPLACED REF CRJ-700 SRM 51-42-21-001-001-A01, DWG PLCC670-32106 REV A, DWG CC670-32030 REV H COMPLIED WI
- [SDR SWIA2026032677360](https://openairdocs.org/sdr/SWIA2026032677360.md): Stringer Splice · corroded · Mar 26, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND AT STR19R SPLICE BS 477. REMOVED AND REPLACED STRINGER SPLICE WITH A NEW STR19R, BS 477 IAW SRM 51-42-06-001-001-A01, & DWG SH670-30006, REV A.
- [SDR SWIA2026032577425](https://openairdocs.org/sdr/SWIA2026032577425.md): Stringer · corroded · Mar 25, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 21R, BS 394 - 477. REPLACED THE STRINGER IAW DWG SH670-31350, REV A, AND SRM 51-42-06-001-001-A01.
- [SDR SWIA2026032577382](https://openairdocs.org/sdr/SWIA2026032577382.md): Stringer Splice · corroded · Mar 25, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER 18L SPLICE, BTWN BS 469 - 485. REMOVED AND REPLACED WITH A NEW SPLICE ON STRINGER 18L, BS 469 - 485 PER SRM 51-42-06-001-001-A01, AND DWG SH670-30006, REV A.
- [SDR SWIA2026032477423](https://openairdocs.org/sdr/SWIA2026032477423.md): Bulkhead · corroded · Mar 24, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > CORROSION FOUND ON BS 280 BULKHEAD AT STR 26L UNDER CRAWL WAY SUPPORT ANGLE. REMOVED CORROSION ON THE BS 280 BULKHEAD IAW SRM 51-21-06-001-001-A01,COMPLIED WITH ALL STEPS 1-9 OF REO 670-53-11-2298, REV -.
- [SDR SWIA2026032377354](https://openairdocs.org/sdr/SWIA2026032377354.md): Floor Support · cracked · Mar 23, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT COCKPIT AT APPROX BS 202.75 - 280, RBL12 WAS CRACKED. REMOVED NEW COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, AND DWG CC670-34010, REV -K.
- [SDR SWIA2026032077407](https://openairdocs.org/sdr/SWIA2026032077407.md): Web · corroded · Mar 20, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LH LOWER WEB AT FS 280 HAS CORROSION 31921541 C-CHECK RO 09302026REPAIRED LH LOWER WEB AT FS 280 REF CRJ700 SRM 53-11-10-201-003-A01 REPAIR B
- [SDR SWIA2026031877381](https://openairdocs.org/sdr/SWIA2026031877381.md): Frame · corroded · Mar 18, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Frame
  > LOWER FRAME SECTOR AT BS 863, STR 25L - 25R WAS CORRODED OUT OF SCOPE. REPLACED LOWER FRAME SECTOR AT BS 863, STR 20R - 20L IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, AND DWG SH670-37060, REV F.
- [SDR SWIA2026031877350](https://openairdocs.org/sdr/SWIA2026031877350.md): Bulkhead Web · corroded · Mar 18, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > RIGHT LOWER WEB AT FS 280 HAS CORROSION. REPAIRED RT LOWER WEB AT FS 280 IAW SRM 53-11-10-201-003-A01 REPAIR B.
- [SDR SWIA2026031777458](https://openairdocs.org/sdr/SWIA2026031777458.md): Angle · corroded · Mar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SURROUND STRUCTURE LOWER SILL ANGLE, MOUNTING HAS CORROSION ON BOTH SIDES. REMOVED AND REPLACED LOWER SILL ANGLE MOUNTING REF SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV Y.
- [SDR SWIA2026031777402](https://openairdocs.org/sdr/SWIA2026031777402.md): Floorbeam · cracked · Mar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOORBEAM AT APPROX FS 28000 LBL12 HAS CRACK TRANS 31900501 C-CHECK RO 09302026REPARED COCKPIT FLOORBEAM AT LBL1200 REF CRJ700 SRM 53-11-43-201-003-A01 AND COMPLIED WITH FORM M337 AND TASK CARD 51-900-1002-SKY,SEE CONTINUE CARD FORE MORE DETAILS
- [SDR SWIA2026031777387](https://openairdocs.org/sdr/SWIA2026031777387.md): Floorbeam · cracked · Mar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOORBEAM AT APPROX FS 28000 RBL12 HAS CRACK. INSTALLED REPAIR PARTS FOR COCKPIT FLOORBEAM AT RBL1200 REF SRM 53-11-43-201-003-A01
- [SDR SWIA2026031777357](https://openairdocs.org/sdr/SWIA2026031777357.md): Attach Angle · cracked · Mar 17, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > ATTACH ANGLE AT BS 280, RBL12 HAS CRACK. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-42-21-001-001-A1 AND DWG CC670-34010 REV -K,
- [SDR SWIA2026031677470](https://openairdocs.org/sdr/SWIA2026031677470.md): Stringer Splice · corroded · Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE 24R AT BS 333. REPLACED STRINGER SPLICE AT FS333, STGR24R REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.
- [SDR SWIA2026031677447](https://openairdocs.org/sdr/SWIA2026031677447.md): Floorbeam · corroded · Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LEFT CROSSBEAM AT BS 280 HAS CORROSION. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010, REV -K.
- [SDR SWIA2026031677444](https://openairdocs.org/sdr/SWIA2026031677444.md): Stringer Splice · corroded · Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE AT FS333 STR25R. REPLACED STRINGER SPLICE AT FS333 STGR25R IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.

Next page: https://openairdocs.org/aircraft/N611SK/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 = 'N611SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N611SK/reports

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