# Service difficulty reports: N685SK

A list on [N685SK](https://openairdocs.org/aircraft/N685SK.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SWIA2026042276025](https://openairdocs.org/sdr/SWIA2026042276025.md): Skin · damaged · Apr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN F
- [SDR SWIA2026042276024](https://openairdocs.org/sdr/SWIA2026042276024.md): Skin · damaged · Apr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLA
- [SDR SWIA2026042276023](https://openairdocs.org/sdr/SWIA2026042276023.md): Skin · damaged · Apr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO
- [SDR SWIA2026042276022](https://openairdocs.org/sdr/SWIA2026042276022.md): Skin · damaged · Apr 22, 2026 · N685SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED
- [SDR SWIA2026020475192](https://openairdocs.org/sdr/SWIA2026020475192.md): Skin · corroded · Dec 22, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON RIGHT EXTERIOR FUSELAGE AROUND BS 630 FOR PANEL 192BB. REMVOED CORROSION ON RT EXTERIOR FUSELAGE AROUND BS 629 TO BS 708 IAW SRM 51-21-06-001-001-A01, AND REPAIRED BY COMPLYING WITH ALL STEPS OF REO 670-53-00-806, REV -. COMPLIED WITH TASK CARD
- [SDR SWIA2026020475181](https://openairdocs.org/sdr/SWIA2026020475181.md): Skin · corroded · Dec 22, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON LEFT EXTERIOR FUSELAGE AROUND BS 630 FOR PANEL 191BB. REMOVED CORROSION ON THE LT EXTERIOR FUSELAGE, BS 629 TO 693 IAW SRM 51-21-06-001-001-A01 AND REPAIRED DAMAGE BY COMPLYING WITH ALL STEPS OF REO 670-53-00-804, REV -. COMPLIED WITH TASK CARD
- [SDR SWIA2025091775180](https://openairdocs.org/sdr/SWIA2025091775180.md): Rib · corroded · Sep 17, 2025 · N685SK · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > LEFT WING, TRAILING EDGE RIB AT WS 398, WAS CORRODED AROUND 13 FASTENER HOLES. REMOVED AND REPLACED THE LT WING, T/E RIB IAW SRM 51-42-21-001-001-A01 AND DWG CC670-15010 REV: B. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2025090875191](https://openairdocs.org/sdr/SWIA2025090875191.md): Angle · cracked · Sep 8, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Structure
  > ANGLE COMMON TO LANDING LATCH CUT OUT FOR PANEL 212AR AT APPROXIMATELY BS 173 CRACKED. REMOVED AND REPLACED THE ANGLE COMMON TO LANDING LATCH CUT OUT FOR PANEL 212AR AT APPROXIMATELY BS 173 IAW SRM 51-42-06-001-001-A01, AND DWG CC670-33040, REV G, COMPLIED WI
- [SDR SWIA2025082375209](https://openairdocs.org/sdr/SWIA2025082375209.md): Roller · worn · Aug 23, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUR LT SLAT TRACK SIDE ROLLERS AT 3-2 ARE WORN. REMOVED AND REPLACED FOUR LT WING SLAT TRACK SIDE ROLLERS AT 3-2, IAW AMM:27-81-44-400-803-A01. OPS TESTED GOOD.
- [SDR SWIA2025082375208](https://openairdocs.org/sdr/SWIA2025082375208.md): Roller · worn · Aug 23, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUR LT WING SLAT TRACK SIDE ROLLERS AT 2-2 ARE WORN. REMOVED AND REPLACED THE LT WING FOUR SIDE ROLLERS AT 2-2, IAW AMM:27-81-44-400-802-A01. OPS TESTED GOOD.
- [SDR SWIA2025082375207](https://openairdocs.org/sdr/SWIA2025082375207.md): Roller · worn · Aug 23, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUR LT WING SIDE TRACK ROLLERS AT 1-2 ARE WORN. REMOVED AND REPLACED LT WING FOUR SIDE ROLLERS AT 1-2, IAW AMM:27-81-44-400-801-A01. EXTENSION & RETRACTION OF SLATS GOOD.
- [SDR SWIA2025082275206](https://openairdocs.org/sdr/SWIA2025082275206.md): Roller · worn · Aug 22, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUR RT SLAT TRACK SIDE ROLLERS AT 3-2 ARE WORN REMOVED AND REPLACED FOUR RT WING SLAT TRACK SIDE ROLLERS AT 3-2, IAW AMM:27-81-44-400-803-A01. EXTENSION AND RETRACTION OF SLATS GOOD AND OPERATING SMOOTHLY.
- [SDR SWIA2025082275205](https://openairdocs.org/sdr/SWIA2025082275205.md): Roller · worn · Aug 22, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > ALL FOUR RT WING SLAT TRACK SIDE ROLLERS AT 2-2 ARE WORN. REMOVED AND REPLACED FOUR RT WING SLAT TRACK SIDE ROLLERS AT 2-2, IAW AMM:27-81-44-400-802-A01. OPS TESTED GOOD.
- [SDR SWIA2026020475200](https://openairdocs.org/sdr/SWIA2026020475200.md): Fitting · chafed · Aug 22, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FLOOR AFT CLOSING FITTING EXFOLIATED. REPLACED PAX DOOR FLOOR AFT CLOSING FITTING IAW DWG SH670-31810, REV AE, SRM 51-42-06-001-001-A01, & SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025082175210](https://openairdocs.org/sdr/SWIA2025082175210.md): Roller · worn · Aug 21, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > FOUR RT SIDE SLAT TRACK ROLLERS AT THE 1-2 ARE WORN. REMOVED AND REPLACED THE FOUR RT WING SLAT TRACK SIDE ROLLERS AT 1-2, IAW AMM:27-81-44-400-801-A01. OPS TESTED GOOD.
- [SDR SWIA2026020475179](https://openairdocs.org/sdr/SWIA2026020475179.md): Angle · corroded · Aug 21, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR MID CAP ANGLE IS CORRODED. INSTALLED NEW PAX DOOR FLOOR MID CAP ANGLE IAW DWG SH670-31810 REV AE AND SRM 51-41-02-001-001-A01. COMPLIED WITH 51-900-1002-SKY. OP TEST GOOD..
- [SDR SWIA2026020475199](https://openairdocs.org/sdr/SWIA2026020475199.md): Stringer · corroded · Aug 12, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R HAS CORROSION IN MULTIPLE AREAS BETWEEN BS 469 AND 485. REPLACED THE STRINGER IAW DWG SH670-30006, REV A, SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025081075198](https://openairdocs.org/sdr/SWIA2025081075198.md): Former · cracked · Aug 10, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER BS 320.163 SUSPECTED CRACKED. INSTALLED NEW PAX DOOR FORMER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. PRESSURIZATION LEAK CHECK OF THE REPAIR AREA PASSED IAW AMM 21-31-00-
- [SDR SWIA2026020475190](https://openairdocs.org/sdr/SWIA2026020475190.md): Intercostal · cracked · Aug 10, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD1A AFT CRACKED. INSTALLED A NEW PAX DOOR AFT DD1A INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2025081075189](https://openairdocs.org/sdr/SWIA2025081075189.md): Door Frame · cracked · Aug 10, 2025 · N685SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FRAME BS 320 CRACKED. INSTALLED A NEW DOOR FRAME IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2026020475188](https://openairdocs.org/sdr/SWIA2026020475188.md): Intercostal · dented · Aug 10, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD1 INTERCOSTAL DENTED AT THE BEND RADIUS. INSTALLED A NEW PAX DOOR AFT DD1 INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2026020475197](https://openairdocs.org/sdr/SWIA2026020475197.md): Angle · corroded · Aug 9, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DOOR FLOOR ANGLE IS CORRODED. FLAGGED. REMOVED CORRODED AND INSTALLED NEW PAX DOOR FLOOR ANGLE IAW DWG SH670-31810, REV AE, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01, REV 38. OPS TESTED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026020475196](https://openairdocs.org/sdr/SWIA2026020475196.md): Former · cracked · Aug 9, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT FORMER IS CRACKED. INSTALLED NEW PAX DOOR AFT FORMER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY900080.
- [SDR SWIA2025080975187](https://openairdocs.org/sdr/SWIA2025080975187.md): Intercostal · cracked · Aug 9, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DD7 INTERCOSTAL IS CRACKED. INSTALLED NEW PAX DOOR AFT DD7 INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV N. COMPLIED WITH 51-900-1002-SKY. LEAK CHECK GOOD AT THIS TIME.
- [SDR SWIA2025080975186](https://openairdocs.org/sdr/SWIA2025080975186.md): Intercostal · corroded · Aug 9, 2025 · N685SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID DD6 INTERCOSTAL IS CORRODED. INSTALLED NEW PAX DOOR MID DD6 INTERCOSTAL IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702 REV N. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025080875178](https://openairdocs.org/sdr/SWIA2025080875178.md): Floor Support · damaged · Aug 8, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT LBL27 IS PITTED AND CORRODED FROM BS 985 - 1098.2. REPAIRED THE LT FLOOR SUPPORT IAW SRM 53-00-41-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
- [SDR SWIA2025080775185](https://openairdocs.org/sdr/SWIA2025080775185.md): Landing · cracked · Aug 7, 2025 · N685SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SUSPECTED CRACK IN THE AFT A-BAY LANDING LATCH CUT OUT FOR PANEL 212AR. REMOVED AND REPLACED CRACKED LANDING LATCH CUT OUT FOR PANEL 212AR IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, DWG CC670-33040 REV -G, & REO 670-53-11-2178 REV-, COMPLIED WIT
- [SDR SWIA2026020475177](https://openairdocs.org/sdr/SWIA2026020475177.md): Hinge · damaged · Aug 7, 2025 · N685SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE DOOR SIDE AFT LUG ROLL PIN HOLE IS ELONGATED. INSTALLED NEW PAX DOOR HINGE DOOR SIDE IAW SRM 52-11-01-201-002-A01 STEPS R AND T AND DWG 601R31702 REV. N AND SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. LEAK CHECK GOOD. COMPLIED
- [SDR SWIA2025080675195](https://openairdocs.org/sdr/SWIA2025080675195.md): Skin · gouged · Aug 6, 2025 · N685SK · Cndair CL6002C10 · Aerodynamic Fairings
  > EXTERNAL LOWER SKIN GOUGED FROM WING-TO-BODY FAIRING AT STRG27, BS 977 - BS 985. BLENDED OUT DAMAGE ON EXTERNAL LOWER SKIN AT STGR27, BS 977 - 985 IAW SRM 51-12-00-001-001-A01 AND COMPLIED WITH NOTES A., B., AND C. OF GREO 670-53-00-290, REV F. LEAK CHECKED G
- [SDR SWIA2025080675194](https://openairdocs.org/sdr/SWIA2025080675194.md): Rivet · loose · Aug 6, 2025 · N685SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT OTBD FLAP OUTER SKIN HAD SMOKING RIVETS. FOUND AT NUMEROUS LOCATIONS ALONG FLAP. REMOVED 10 SMOKING RIVETS AT RT OTBD FLAP OUTER SKIN AT NUMEROUS LOCATIONS ALONG FLAP IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-13-001-001-A01. INSTALLED 10 EACH FASTENE
- [SDR SWIA2025073075193](https://openairdocs.org/sdr/SWIA2025073075193.md): Stand Off · cracked · Jul 30, 2025 · N685SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT UPPER TRANSCOWL INBD -A- BRACKET STAND OFF CRACKED. REMOVED CRACKED STAND OFF FROM LT UPPER TRANSCOWL AND INSTALLED ONE NEW STAND OFF ON LT UPPER TRANSCOWL IAW GREO 670-54-21-971, REV B, STEPS 1-3. COMPLIED WITH SKY CARD 51-900-1002-SKY.
- [SDR SWIA2025073075184](https://openairdocs.org/sdr/SWIA2025073075184.md): Stand Off · cracked · Jul 30, 2025 · N685SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LEFT LOWER TRANSCOWL INBD -A- BRACKET STAND OFF IS CRACKED. STAND OFF REPAIRED IAW REO 670-54-21-971, REV B. COMPLIED WIT 51-900-1002-SKY.
- [SDR SWIA2025072575183](https://openairdocs.org/sdr/SWIA2025072575183.md): Helicoil · damaged · Jul 25, 2025 · N685SK · Cndair CL6002C10 · Wing Miscellaneous Structure
  > LEFT WING JACKING POINT HELI-COIL IS DAMAGED. INSTALLED NEW LEFT WING JACK FITTING IAW SRM 51-42-21-001-001-A01, DWG CC670-10126, REV NC, AND DWG CC670-10038, REV NC..COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2025061975204](https://openairdocs.org/sdr/SWIA2025061975204.md): Roller · out of limits · Jun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 RT - DISCARD THE RT SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3. REMOVE AND REPLACE IAW TASK CARD 27-630-824. COMPLIED WITH SCHEDULED MAINTENANCE ON TRACK ROLLER SLAT 3-3 700
- [SDR SWIA2025061975203](https://openairdocs.org/sdr/SWIA2025061975203.md): Roller · out of limits · Jun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 700 RT - DISCARD THE RT SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2. REMOVE AND REPLACE IAW TASK CARD 27-630-809 (MRB 27-81-43-717), COMPLIED WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER S
- [SDR SWIA2025061975202](https://openairdocs.org/sdr/SWIA2025061975202.md): Roller · out of limits · Jun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 3-3 700 LH - DISCARD THE LH SLAT TRACK ROLLER SEALED, ECCENTRIC LOCATED AT TOP FORWARD 3-3 (REQUIRES QTY 2 OF PN CC670-12567-1). REMOVE AND REPLACE IAW TASK CARD 27-530-824 (MRB 27-81-43-713), COMPLIED
- [SDR SWIA2025061975201](https://openairdocs.org/sdr/SWIA2025061975201.md): Roller · out of limits · Jun 19, 2025 · N685SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 1-2 700 LH - DISCARD THE LH SLAT TRACK SEALED ROLLER LOCATED AT TOP FORWARD 1-2 (P/N CC670-12272-1. REMOVE AND REPLACE IAW TASK CARD 27-530-809 (MRB 27-81-43-717), COMPLIED WITH SCHEDULED MAINTENANCE C
- [SDR SWIA2026020475182](https://openairdocs.org/sdr/SWIA2026020475182.md): Skin · scratched · Jun 19, 2025 · N685SK · Cndair CL6002C10 · Trailing Edge Flaps
  > PERFORMED TEMPORARY REPAIR TO SCRATCH DAMAGE ON RT OTBD FLAP VANE UPPER SKIN BETWEEN FLAP STN. 235.84 - FLAP STN. 254.96. COMPLETE PERMANENT REPAIR 650 HOURS FROM THE TIME OF INCORPERATION., REPAIRD SCRATCH DAMAGE ON RT OTBD FLAP VANE UPPER SKIN BETWEEN FLAP
- [SDR SWIA202163029](https://openairdocs.org/sdr/SWIA202163029.md): None · out of tolerance · Dec 6, 2021 · N685SK · Cndair CL600* · Fuselage Main, Frame
  > MOUNTING HOLES IN GALLEY AREA ABOVE GALLEY SERVICE DOOR ON RH FRAME AT FS333.00 AND FS349.00 BETWEEN STRINGERS 5R AND 6R DUE TO EA7RJ3519-25 BRACKET REMOVAL (8 HOLES TOTAL) ARE OUT OF LIMITS AND REQUIRE REPAIR. REFERENCE CP 23948264 FOR INITIAL DISCREPANCY. TH
- [SDR SWIA202163028](https://openairdocs.org/sdr/SWIA202163028.md): None · out of tolerance · Dec 6, 2021 · N685SK · Cndair CL600* · Fuselage Main, Frame
  > MOUNTING HOLES IN FLIGHT DECK ON RH FRAME AT FS250.00 AND INTERCOSTAL AT FS243.125 JUST ABOVE STRINGER 12A DUE TO EA7RJ3519-25 BRACKET REMOVAL (4 HOLES TOTAL) ARE OUT OF LIMITS AND REQUIRE REPAIR. REFERENCE CP 23948260 FOR INITIAL DISCREPANCY. THIS IS A €ŒMAJ
- [SDR SWIA202163027](https://openairdocs.org/sdr/SWIA202163027.md): None · out of tolerance · Dec 6, 2021 · N685SK · Cndair CL600* · Fuselage Main, Frame
  > MOUNTING HOLES IN FLIGHT DECK ON LH FRAME AT FS250.00 AND INTERCOSTAL AT FS243.125 JUST ABOVE STRINGER 12A DUE TO EA7RJ3519-25 BRACKET REMOVAL (4 HOLES TOTAL) ARE OUT OF LIMITS AND REQUIRE REPAIR. REFERENCE CP 23948257 FOR INITIAL DISCREPANCY. THIS IS A €ŒMAJ
- [SDR SWIA202165167](https://openairdocs.org/sdr/SWIA202165167.md): None · damaged · Dec 4, 2021 · N685SK · Cndair CL6002C10 · Fuselage Main, Frame
  > DAMAGE/HOLES FOUND OUT OF LIMITS IN FLIGHT DECK ON LH FRAME AT FS250.00 AND INTERCOSTAL AT FS243.125 JUST ABOVE STRINGER 12A DUE TO EA7RJ3519-25 BRACKET REMOVAL (FILED - CLOSED) MOUNTING HOLES IN FLIGHT DECK ON LH FRAME AT FS250.00 AND INTERCOSTAL AT FS243
- [SDR SWIA202165168](https://openairdocs.org/sdr/SWIA202165168.md): None · cracked · Dec 2, 2021 · N685SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND CRACKED SUPPORT ANGLE CLEAT ON FORWARD SIDE OF FS 349 FLOOR CROSS BEAM AT LBL27.00 (FILED - CLOSED) REMOVED AND REPLACED SUPPORT ANGLE CLEAT ON FORWARD SIDE OF FS 349 FLOOR CROSS BEAM AT LBL27.00, REF CRJ 700 SRM 51-42-06 AND 53-21-43.
- [SDR SWIA202165166](https://openairdocs.org/sdr/SWIA202165166.md): None · damaged · Nov 17, 2021 · N685SK · Cndair CL6002C10 · Doors
  > RIGHT EMERGENCY EXIT DOOR WINDOW SCUFFED. (FILED - CLOSED) REMOVED AND REPLACED RH OVERWING EMERGENCY EXIT DOOR IAW TASK CARD 56-200-1000-SKY. LEAK CHECK GOOD. OLD DATE:08-02
- [SDR SWIA202165165](https://openairdocs.org/sdr/SWIA202165165.md): None · damaged · Nov 17, 2021 · N685SK · Cndair CL6002C10 · Doors
  > LEFT EMERGENCY EXIT DOOR WINDOW SCUFFED. (FILED - CLOSED) REMOVED AND REPLACED LH OVERWING EMERGENCY EXIT DOOR IAW TASK CARD 56-200-1000-SKY. LEAK CHECK GOOD. OLD DATE:08-02

## 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 = 'N685SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N685SK/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.