# Service difficulty reports: N614SK

A list on [N614SK](https://openairdocs.org/aircraft/N614SK.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 7 · 326 reports

- [SDR SWIA2026082576961](https://openairdocs.org/sdr/SWIA2026082576961.md): Wire · nicked · Aug 25, 2026 · N614SK · Cndair CL6002C10 · Equipment/Furnishings Wiring
  > SPARKS COMING FROM BEHIND CAPTAIN`S CHART LIGHT HOLDER. DURING STALL TEST THERE WAS VISIBLE ARCING WITH SMOKE. MEL 25-18-2 CAT: D DUE DATE: 23 DEC 2026. (FLIGHT 6466) DEFERRED CAPTAIN`S SIDE CHART HOLDER/LIGHT ASSY IAW MEL 25-18-2, MX ACTION COMPLIED WITH.
- [SDR SWIA202509020009](https://openairdocs.org/sdr/SWIA202509020009.md): Tie Bar · bent · Jul 18, 2025 · N614SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RH ENGINE PYLON - AFT OF PYLON TIE BAR FRAME - UPR AND LWR FIREWALL SEAL RETAINERS AND SUPPORT STRUCTURE BENT. REPLACED RH ENGINE PYLON - AFT OF PYLON TIEBAR FRAME - UPR AND LWR FIREWALL SEAL RETAINERS AND SUPPORT STRUCTURE REF.DWG: MM670-37001 REV: AH AND S
- [SDR SWIA202509020024](https://openairdocs.org/sdr/SWIA202509020024.md): Fitting · gouged · Jun 23, 2025 · N614SK · Cndair CL6002C10 · Wing, Control Surface Attach Fittings
  > RIGHT WING AILERON HINGE FITTING NR 2 (WING SIDE) OUTBOARD LUG GOUGED. REPAIRED RT WING AILERON HINGE FITTING NR 2 (WING SIDE) REF REO 670-57-51-615 REV--.
- [SDR SWIA202509020008](https://openairdocs.org/sdr/SWIA202509020008.md): Rib · cracked · Jun 2, 2025 · N614SK · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > RIGHT INBD GROUND SPOILER INBD FITTING ASSY AT SPS0.00 FOUND TO BE CRACKED AT AFT LOWER FASTENER HOLE LOCATION. FABRICATED NEW RIB. REMOVED OLD AND INSTALLED NEW GROUND SPOILER RIB ASSEMBLY. COMPLIED WITH TASK CARD 51-900-1002-SKY. REF DWG# CC670-16150 REV:
- [SDR SWIA20250902001](https://openairdocs.org/sdr/SWIA20250902001.md): Seal · torn · May 11, 2025 · N614SK · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL-STABILIZER LT TRAILING-EDGE SEAL IS TORN NEAR AFT FAIRING 326CT. REPAIRED HORIZONTAL STABIULIZER LT TRAILING EDGE SEAL NEAR AFT FAIRING 326CT IAW REO 670-55-10-017, REV --, DWG BA670-23107, REV --, AND DWG KBA670-23001, REV C. COMPLIED WITH TASK 5
- [SDR SWI2025F01175](https://openairdocs.org/sdr/SWI2025F01175.md): Intercostal · damaged · May 1, 2025 · N614SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES FOUND ON INTERCOSTAL SILL AT STGR 21L, FS333.00 TO FS349.00 UPON REMOVAL. REMOVED AND INSTALLED NEW INTERCOSTAL SILL AT STGR 21L, FS333.00 TO FS349.00 IAW SRM 51-42-06-001-001 A01 & DWG SH670-31810 REV AE. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWIA202509020020](https://openairdocs.org/sdr/SWIA202509020020.md): Stringer · damaged · May 1, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVAL OF INTERCOSTAL SILL ON STRINGER STGR 21L FS333.00 TO FS349.00 FOUND ELONGATED HOLES ON VERTICAL FLANGE OF STRINGER. REPAIRED FOR OVERSIZED HOLE ON STRINGER 21L AT FS333.00 REF-CRJ-700 REO 670-53-21-2629 REV --, LEAK CHECK PASSED. COMPLIED WITH
- [SDR SWI2025F01154](https://openairdocs.org/sdr/SWI2025F01154.md): Hinge · cracked · Apr 30, 2025 · N614SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE #1 LUG CRACKED (C-CHECK RO 08/30/2025) REPLACED PASSENGER DOOR HINGE. REF: SRM TASK-52-11-01-201-002-A01 AND DWG: 601R31702 REV: N. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202509020007](https://openairdocs.org/sdr/SWIA202509020007.md): Hinge · gouged · Apr 30, 2025 · N614SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PASSENGER DOOR PIANO HINGE ON THE FUSELAGE HAS GOUGES ON: #6 LUG, #7 LUG AND #27 LANDING PASSENGER DOOR PIANO HINGE ON THE FUSELAGE SIDE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED PAX DOOR FUSELAGE HINGE REF CRJ 700 REO 670-53-21-2627 -A DATED 2025-06
- [SDR SWIA202509030002](https://openairdocs.org/sdr/SWIA202509030002.md): Window Post · cracked · Apr 19, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Structure
  > CO-PILOTS SIDE WINDSHIELD POST UPPER ATTACH SUPPORTING STRUCTURE, IN THE CEILING, IS CRACKED. REMOVED AND INSTALLED NEW FRAME, WINDSHIELD SUPPORT, WAS CRACKED STRUCTURE, IAW SRM 51-42-06-001-001 A01, SRM 51-42-21-001-001 A01 AND DWG CC670-33010 REV G, INSTALL
- [SDR SWIA202509030001](https://openairdocs.org/sdr/SWIA202509030001.md): Seat Track · corroded · Apr 17, 2025 · N614SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > AFTER REMOVAL OF SEAT TRACK FOUND HEAVY CORROSION AT LBL9, APPROX FS480 - FS485. REPAIRED FLOOR BEAM AT LBL9, FS485 - FS517 REF REO 670-53-31-1032 REV -- 2025-05-09, SRM 53-00-41-201-001-A01, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01 AND DWG: SH
- [SDR SWIA20250902005](https://openairdocs.org/sdr/SWIA20250902005.md): Fitting · gouged · Apr 16, 2025 · N614SK · Cndair CL6002C10 · Horizontal Stabilizer Structure
  > HORIZONTAL STAB LT SCREW JACK FITTING HAS NUMEROUS GOUGES, OTBD UPPER MOUNT FLANGES, INBD UPPER MOUNT FLANGES, LUG FORWARD OTBD SIDE & LUG FORWARD INBOARD SIDE. REMOVED GOUGES ON LH HORIZ STAB FITTING IAW SRM 51-12-00-001-001-A01, COMPLIED WITH STEPS 1-5. ENS
- [SDR SWI2025F01153](https://openairdocs.org/sdr/SWI2025F01153.md): Cradle · gouged · Apr 15, 2025 · N614SK · Cndair CL6002C10 · Wing, Attach Fittings
  > RIGHT INBD FLAP VANE ACTUATOR SYSTEM- CRADLE ASSEMBLY AT WS65.50 GOUGED. COMPLIED WITH REPAIR TO RT INBD FLAP VANE ACTUATOR SYSTEM- CRADLE ASSEMBLY AT WS65.50 REF REO 670-57-52-609 REV -- DATED 2025-05-16 AND SRM-51-21-16-001-001-A01. ALL CHECKS GOOD. COMPL
- [SDR SWI2025F01152](https://openairdocs.org/sdr/SWI2025F01152.md): Cradle · gouged · Apr 15, 2025 · N614SK · Cndair CL6002C10 · Wing, Attach Fittings
  > LEFT INBD FLAP VANE ACTUATOR SYSTEM- CRADLE ASSEMBLY AT WS65.50 GOUGED. REPAIRED LT INBD FLAP VANE ACTUATOR SYSTEM, CRADLE ASSEMBLY AT WS65.50 IAW REO 670-57-52-608 REV -- DATE 2025-05-16 AND SRM 51-12-00-001-001 A01. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01151](https://openairdocs.org/sdr/SWI2025F01151.md): Angle · corroded · Apr 15, 2025 · N614SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL MOUNTING ANGLE HAS CORROSION. REMOVED AND REPLACED WITH NEW SERVICE DOOR SILL MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV Y. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA20250902003](https://openairdocs.org/sdr/SWIA20250902003.md): Cradle · gouged · Apr 15, 2025 · N614SK · Cndair CL6002C10 · Wing, Attach Fittings
  > RIGHT INBD FLAP VANE ACTUATOR SYSTEM, CRADLE ASSEMBLY AT WS24.00 GOUGED. COMPLIED WITH REPAIR TO RH IB FLAP VANE CRADLE ASSY AT WS24 REF REO 670-57-52-609 REV -- AND SRM-51-21-16-001-001-A01. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01163](https://openairdocs.org/sdr/SWI2025F01163.md): Stringer Splice · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR21R STRINGER SPLICE AT FS333. REMOVED AND INSTALLED NEW STRINGER 21R SPLICE AT FS333 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-32420 REV E, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01162](https://openairdocs.org/sdr/SWI2025F01162.md): Stringer · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON ATTACH FLANGE OF STR21R FS280 - FS333. REMOVED AN DINSTALLED NEW STRINGER 21R FROM FS280 TO FS333 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-31630 REV K, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01161](https://openairdocs.org/sdr/SWI2025F01161.md): Stringer · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON ATTACH FLANGE OF STR22R FROM FS280 - FS333. REMOVED AND INSTALLED NEW STRINGER 22R FROM FS280 TO FS333 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-31630 REV K, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01160](https://openairdocs.org/sdr/SWI2025F01160.md): Stringer Splice · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR24R SPLICE AT FS333. REMOVED AND INSTALLED NEW STRINGER 24R SPLICE AT FS333 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-32420 REV E, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01159](https://openairdocs.org/sdr/SWI2025F01159.md): Stringer · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON ATTACH FLANGE STR24R FS333 TO FS477. REMOVED AND INSTALLED NEW STRINGER 24R FROM FS333 TO FS477 IAW SRM 53-00-03-201-001 A01, SRM 51-42-06-001-001 A01 AND DWG SH670-31350 REV A, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01158](https://openairdocs.org/sdr/SWI2025F01158.md): Stringer · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON ATTACH FLANGE OF STR24R FS280 - FS333. REMOVED AND INSTALLED NEW STRINGER 24R FS280-FS333 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-31630 REV K. LEAK CHECK PASSED. COMPLIED WITH THA TASK 51-900-1002-SKY.
- [SDR SWI2025F01157](https://openairdocs.org/sdr/SWI2025F01157.md): Stringer Splice · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STR23R SPLICE AT FS333. REMOVED AND INSTALLED NEW STRINGER SPLICE 23R AT FS333 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-32420 REV E, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01156](https://openairdocs.org/sdr/SWI2025F01156.md): Attach Angle · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION FOUND ON ATTACH FLANGE OF STR23R FS280 - FS 333. REMOVED AND INSTALLED NEW STRINGER 23R FROM FS280 TO FS333 REF SRM 51-42-06-001-001 A01 AND DWG SH670-31630 REV K, LEAK CHECK PASSED.COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWIA2025090200011](https://openairdocs.org/sdr/SWIA2025090200011.md): Stringer Splice · corroded · Apr 13, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON S22R STRINGER SPLICE AT FS 333 CAMP. REMOVED AND INSTALLED NEW STRINGER 22R SPLICE AT FS333 REF SRM 51-42-06-001-001 A01 AND DWG SH670-32420 REV E, LEAK CHECK PASSED.COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01177](https://openairdocs.org/sdr/SWI2025F01177.md): Stringer · corroded · Apr 12, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON ATTACH FLANGE OF STR22R FS333-FS349. REMOVED AND INSTALLED NEW STRINGER 22R BETWEEN FS333 TO FS349 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-31350 REV A. LEAK CHECK GOOD. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWIA202509020022](https://openairdocs.org/sdr/SWIA202509020022.md): Stringer · corroded · Apr 12, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > HEAVY CORROSION FOUND ON ATTACH FLANGE. STR21R FS364 - FS379. REMOVED AND INSTALLED NEW STRINGER 21R BEWTEEN FS333-FS379 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-31350 REV A, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01174](https://openairdocs.org/sdr/SWI2025F01174.md): Stringer Splice · corroded · Apr 10, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER SPLICE AT FS.477 STGR26L. REMOVED AND INSTALLED NEW STRINGER 26L SPLICE AT FS477 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-30006 REV A, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWIA202509020019](https://openairdocs.org/sdr/SWIA202509020019.md): Stringer Splice · corroded · Apr 10, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON STRINGER SPLICE AT FS333 STR24L. REMOVED AND INSTALLED NEW STRINGER SPLICE AT STGR24L FS333 IAW SRM 51-42-06-001-001 A01, AND DWG SH670-32420 REV E, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWIA2025090200013](https://openairdocs.org/sdr/SWIA2025090200013.md): Lintel · cracked · Apr 7, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR LINTEL (STGR3L) BETWEEN FS280.00 AND FS295.00 CRACKED. COMPLIED WITH SB 670BA-53-040 REV-C PART A & B AND ALL STEPS OF REO 670-53-21-493 REV-D, REPAIR OF PASSENGER DOOR LINTEL AT STGR 3LSERVICE BULLETIN 670BA-53-040, REVISION C, BS 280 TO BS.
- [SDR SWI2025F01182](https://openairdocs.org/sdr/SWI2025F01182.md): Stringer · corroded · Apr 4, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON ATTACH FLANGE OF LONGERON AT STR25L FS333 - FS349. REMOVED AND INSTALLED NEW LONGERON AT STGR25L BETWEEN FS333 AND FS349 IAW DWG# SH670-32050 REV J, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEAL CHECK PASSED. COMPLIED WITH TA
- [SDR SWIA202509020027](https://openairdocs.org/sdr/SWIA202509020027.md): Stringer · corroded · Apr 4, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON ATTACH FLANGE OF STR24L BETWEEN FS333 - FS349. REMOVED AN INSTALLED NEW STRINGER 24L BETWEEN FS333-FS385 IAW SRM 51-42-06-001-001 A01 AND SRM 53-00-00-201-001 A01, LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01173](https://openairdocs.org/sdr/SWI2025F01173.md): Bracket · bent · Apr 3, 2025 · N614SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BRACKET, IS BENT ON FRAMES, BS 565.00 AT STGR27. REMOVED 1 EACH DAMAGE BRACKETS AT BS 565, S27 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW BRACKET P/N SH670-34082-3 AT FS565.00 STGR27 IAW SRM 51-42-06-001-001-A01 AND DWG SH670-33600 REV-AD.
- [SDR SWIA2025090200017](https://openairdocs.org/sdr/SWIA2025090200017.md): Bracket · bent · Apr 3, 2025 · N614SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BRACKET, IS BENT ON FRAMES, FS 581.00 AT STGR27. REMOVED 1 EACH DAMAGE BRACKETS AT 581.00 AT STGR27 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW BRACKET AT FS581.00 STGR27 IAW SRM 51-42-06-001-001-A01 AND DWG SH670-33600 REV- AD. COMPLIED
- [SDR SWI2025F01142](https://openairdocs.org/sdr/SWI2025F01142.md): Frame · corroded · Apr 1, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CIRCUMFERENTIAL JOINT HAS CORROSION AT FS333 BETWEEN STGR 25L - STGR 27, FWD AND AFT OF FRAME. REMOVED CORROSION AT CIRCUMFERENTIAL JOINT FS333 BETWEEN STGR 25L - STGR 27, FWD AND AFT OF FRAME REF-CRJ-700 SRM 51-21-06-001-001 A01, REO 670-53-21-2613 REV --,
- [SDR SWI2025F01141](https://openairdocs.org/sdr/SWI2025F01141.md): Stringer Splice · corroded · Apr 1, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 22L SPLICE BETWEEN BS 333 - 349 HAS CORROSION. REMOVED AND INSTALLED NEW STRINGER SPLICE 22L BETWEEN FS333-FS349 REF SRM 51-42-06-001-001 A01 AND DWG SH670-32420 REV E, LEAK CHECK PASSED.COMPLIED WITH TASK 51-900-1002-SKY
- [SDR SWIA2025090200026](https://openairdocs.org/sdr/SWIA2025090200026.md): Stringer · corroded · Mar 30, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION VISIBLE UNDER STGR 22L BETWEEN FS349 - FS364. REPAIRED STGRINGER 22L SPLICE BETWEEN FS349-FS364 IAW SRM 53-00-03-201-001 A01 AND SRM 51-42-06-001-001 A01, LEAK CHECK PASSED.COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01155](https://openairdocs.org/sdr/SWI2025F01155.md): Frame · corroded · Mar 25, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS333 HAS HEAVY CORROSION BETWEEN STGR21L - STGR 25L. REMOVED AND INSTALLED NEW FRAME AT FS333 REF SRM 51-42-06-001-001 A01, SRM 51-42-21-001-001 A01 AND DWG SH670-32420 REV E. LEAK CHECK PASSED.COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWIA202509020010](https://openairdocs.org/sdr/SWIA202509020010.md): Frame · damaged · Mar 25, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Frame
  > UPON REMOVAL OF FS333 FRAME FOUND ELONGATED HOLES (2 EA) ON FRAME SUPPORT ANGLE BETWEEN STGR 21L - STGR 22L. REPLACED FRAME SUPPORT ANGLE OF FRAME FS333 BETWEEN STGR 21L - STGR22L WITH NEW FABRICATED FRAME SUPPORT ANGLE.REF DWG SH670-31810 REV: AE AND SRM
- [SDR SWI2025F01178](https://openairdocs.org/sdr/SWI2025F01178.md): Stringer · corroded · Mar 22, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON THE ATTACH FLANGE OF STR23R FS364 - FS 379. REMOVED AND INSTALLED NEW STRINGER 23R BETWEEN FS333 AND FS379 IAW SRM 51-42-06-001-001 A01 AND DWG SH670-31350 REV A. LEAK CHECK PASSED. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWIA202509020023](https://openairdocs.org/sdr/SWIA202509020023.md): Skin · cracked · Mar 22, 2025 · N614SK · Cndair CL6002C10 · Rudder, Plate/Skin
  > RUDDER LEADING EDGE SKIN, LOWER RT, CRACKED. REMOVED AND INSTALLED NEW RUDDER LEADING EDGE SKIN LOWER RT IAW SRM 51-42-06-001-001 A01 AND DWG CC670-22002 REV -B. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01166](https://openairdocs.org/sdr/SWI2025F01166.md): Beam · chafed · Mar 21, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > RIGHT INBD FLAP VANE ACTUATOR BEAM AT WS65 (NO.2) IS CHAFED. REPAIRED RT INBD FLAP VANE ACTUATOR BEAM AT WS65 (NO.2) AND COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV - A DATED 2024-08-20. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01165](https://openairdocs.org/sdr/SWI2025F01165.md): Beam · chafed · Mar 21, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > RIGHT INBD FLAP VANE ACTUATOR BEAM AT WS24 (NO.1) IS CHAFED. REPAIRED RH IB FLAP VANE ACTUATOR BEAM AT WS24 (NO.1) AND COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV-A DATED 2024-08-20. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01164](https://openairdocs.org/sdr/SWI2025F01164.md): Beam · chafed · Mar 21, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > RIGHT INBD FLAP VANE ACTUATOR BEAM AT WS140 (NO.4) IS CHAFED. REPAIRED RT INBD FLAP VANE ACTUATOR BEAM AT WS140 (NR 4) AND COMPLIED WITH ALL STEPS REO 670-57-52-257 REV-A. COMPLIED WITH TASK CARD 51-900-1002-SKY..
- [SDR SWIA2025090200014](https://openairdocs.org/sdr/SWIA2025090200014.md): Beam · chafed · Mar 21, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > RIGHT INBD FLAP VANE ACTUATOR BEAM AT WS102 (NO.3) IS CHAFED. REPAIRED RT INBD FLAP VANE ACTUATOR BEAM AT WS102 (NR 3) AND COMPLIED WITH ALL STEPS OF REO 670-57-52-257 REV - A. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01181](https://openairdocs.org/sdr/SWI2025F01181.md): Beam · chafed · Mar 20, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > LEFT INBOARD FLAP VANE ACTUATOR BEAM AT WS65.50 CHAFED. REPAIRED LH I/B FLAP VANE ACTUATOR BEAM AT WS65.50 IAW REO 670-57-52-257 REV -A DATE 2024-08-20. OPS TESTED GOOD. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01180](https://openairdocs.org/sdr/SWI2025F01180.md): Beam · chafed · Mar 20, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > LEFT INBD FLAP VANE ACTUATOR BEAM AT WS140 CHAFED. REPAIRED LT INBD FLAP VANE ACTUATOR BEAM AT WS140 IAW REO 670-57-52-257 REV-A DATED: 2024-08-20 OPS TEST GOOD. COMPLIED WITH TASK 51-900-1002-SKY.
- [SDR SWI2025F01179](https://openairdocs.org/sdr/SWI2025F01179.md): Beam · chafed · Mar 20, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > LH IB FLAP VANE ACTUATOR BEAM AT WS102 CHAFED. REPAIRED LH I/B FLAP VANE ACTUATOR AT WS102 REF-CRJ-700 REO 670-57-52-257 REV -B DATE 2024-08-20. SEE CONTINUATION CARD FOR DETAILS. OPS TEST GOOD.COMPLIED WITH TASK 51-900-1002-SKY
- [SDR SWIA202509020025](https://openairdocs.org/sdr/SWIA202509020025.md): Beam · chafed · Mar 20, 2025 · N614SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > LEFT INBOARD FLAP VANE ACTUATOR BEAM AT WS24.00 CHAFED. REPAIRED LT INBOARD FLAP VANE ACTUATOR BEAM AT WS24.00 IAW REO 670-57-52-257 REV-A. OPS TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWI2025F01172](https://openairdocs.org/sdr/SWI2025F01172.md): Skin · damaged · Mar 18, 2025 · N614SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FORWARD BAGGAGE BAY SURROUND STRUCTURE JOINT PLATE ON THE INNER SKIN AT FS533 STGR25L HAS A FASTENER HOLE WITH DAMAGE AROUND THE INNER EDGE OF THE HOLE. REMOVED AND INSTALLED NEW FORWARD BAGGAGE BAY SURROUND STRUCTURE JOINT PLATE ON THE INNER SKIN AT FS533 ST

Next page: https://openairdocs.org/aircraft/N614SK/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 = 'N614SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N614SK/reports

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