# Service difficulty reports: N710SK

A list on [N710SK](https://openairdocs.org/aircraft/N710SK.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 4 · 191 reports

- [SDR SWIA20250417003](https://openairdocs.org/sdr/SWIA20250417003.md): Wire · damaged · Apr 3, 2025 · N710SK · Cndair CL6002C10 · Electrical Power System Wiring
  > CONNECTOR JSIS/PSIS BACKSHELL BROKEN. (C-CHECK RO 04/16/2025)REPAIRED WIRE TO THE BACKSHELL ON J512 IAW CRJ 700 REO 670-20-12-131. NO WEIGHT CHANGE, TASK CARD 51-900-1002-SKY COMPLETED, M-337 ATTACHED.DN 909542
- [SDR SWIA20250417320](https://openairdocs.org/sdr/SWIA20250417320.md): Roller · excess play · Mar 20, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 1-2 BOTH IB AND OB AFT TRACK ROLLER HAS EXCESSIVE PLAY. (C-CHECK RO 04/16/2025)REMOVED AND REPLACED BOTH I/B AND O/B AFT SLAT TRACK 1-2 ROLLERS AS REQUIRED IAW CRJ 700 AMM 27-81-42.
- [SDR SWIA2025F00472](https://openairdocs.org/sdr/SWIA2025F00472.md): Roller · excess play · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H SLAT TRACK 1-2 BOTH IB AND OB FWD TRACK ROLLERS HAS EXCESSIVE PLAY. (C-CHECK RO 04/16/2025)REMOVED AND REPLACED R/H SLAT TRACK 1-2 BOTH IB AND OB FWD TRACK ROLLERS IAW CRJ 700 AMM:27-81-44-000-801(AO1), AMM:27-81-44-400-801(AO1)
- [SDR SWIA2025F00471](https://openairdocs.org/sdr/SWIA2025F00471.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H SLAT TRACK 2-2 OB FWD TRACK ROLLER HAS OUT OF LIMIT FLAT SPOTS. (C-CHECK RO 04/16/2025)REMOVED AND REPLACED R/H SLAT TRACK 2-2 OB FWD TRACK ROLLER IAW CRJ700 AMM:27-81-44-000-801(AO1), AMM:27-81-44-400-801(AO1)
- [SDR SWIA2025F00470](https://openairdocs.org/sdr/SWIA2025F00470.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H SLAT TRACK 2-2 IB FWD TRACK ROLLER HAS EXCESSIVE PLAY AND OUT OF LIMIT FLAT SPOTS. (C-CHECK RO 04/16/2025)REMOVED AND REPLACED R/H SLAT TRACK 2-2 IB FWD TRACK ROLLER IAW CRJ700 AMM:27-81-44-000-801(AO1), AMM:27-81-44-400-801(AO1)
- [SDR SWIA2025F00469](https://openairdocs.org/sdr/SWIA2025F00469.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H SLAT TRACK 2-2 IB AFT TRACK ROLLER HAS OUT OF LIMIT FLAT SPOTS AND EXCESSIVE PLAY. (C-CHECK RO 04/16/2025)REMOVED,REPLACE AND AJUSTED R/H SLAT TRACK 2-2 IB AFT TRACK ROLLER IAW CRJ 700 AMM 27-81-44
- [SDR SWIA2025F00468](https://openairdocs.org/sdr/SWIA2025F00468.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > R/H SLAT TRACK 3-2 HAS 2 TRACK ROLLERS OUT OF LIMIT FLAT SPOTS. IB AND OB FWD ROLLERS. (C-CHECK RO 04/16/2025)REMOVED AND REPLACED BOTH I/B AND O/B FWD SIDE ROLLERS ON SLAT RECK 3-2 AS REQUIRED IAW CRJ 700 AMM 27-81-44-400-801-A01.
- [SDR SWI2025F00467](https://openairdocs.org/sdr/SWI2025F00467.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 1-2 IB FWD ROLLER HAS OUT OF LIMITS FLAT SPOT AND EXCESSIVE PLAY (C-CHECK RO 04/16/2025)REMOVED AND REPLACED L/H SLAT TRACK 1-2 I/B FWD ROLLER AS REQUIRED IAW CRJ 700 AMM 27-81-44-400-801-A01.
- [SDR SWI2025F00466](https://openairdocs.org/sdr/SWI2025F00466.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 1-2 IB AFT ROLLER HAS OUT OF LIMITS FLAT SPOTS AND EXCESSIVE PLAY (C-CHECK RO 04/16/2025)IAW CRJ 700 AMM 27-81-44 400-801-A01, REPLACED LH SLAT TRACK 1-2 IB AFT ROLLER. EMP#: JM 8097
- [SDR SWIA20250417002](https://openairdocs.org/sdr/SWIA20250417002.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 2-2 IB AFT ROLLER HAS OUT OF LIMITS FLAT SPOTS (C-CHECK RO 04/16/2025)I.A.W CR 700 AMM 27-81-44 000-802 WAS REPLACED LH SLAT TRACK 2-2 IB AFT ROLLER EMP#: JM 8097
- [SDR SWIA202504170219](https://openairdocs.org/sdr/SWIA202504170219.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 1-2 OB FWD ROLLER HAS OUT OF LIMITS FLAT SPOTS AND EXCESSIVE PLAY (C-CHECK RO 04/16/2025)REMOVED AND REPLACED L/H SLAT TRACK 1-2 O/B FWD ROLLER AS REQUIRED IAW CRJ 700 AMM 27-81-44-400-801-A01.
- [SDR SWIA202504170218](https://openairdocs.org/sdr/SWIA202504170218.md): Support · loose · Feb 18, 2025 · N710SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH WING, OB FLAP, VANE FLAP SUPPORT #3 LOOSE ATTACHMENT HI-LOCK (C-CHECK RO 04/16/2025)ACCOMPLISHED INSTALLED NEW HI-LOCK ON THE RH WING O/B FLAP SUPPORT # 3 IAW CRJ 700 REO #670-57-53-402, TASK CARD 51-900-1002-SKY COMPLETE, M-337 ATTACHED
- [SDR SWIA202504170212](https://openairdocs.org/sdr/SWIA202504170212.md): Door Sill · corroded · Feb 12, 2025 · N710SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SURROUND INTERCOSTAL HAS CORROSION BETWEEN FS 349.00 - FS 333.00 STGR 21 L (C-CHECK RO 04/16/2025)REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 333.00 AND FS 349 STGR 21 L IAW CRJ700 SRM 51-42-20 AND CRJ700 SRM 51-42-06
- [SDR SWIA202504170211](https://openairdocs.org/sdr/SWIA202504170211.md): Striker · corroded · Feb 11, 2025 · N710SK · Cndair CL6002C10 · Service Doors
  > GALLEY SERVICE DOOR AT LWR SEAL AREA SEAL STRIKER HAS CORROSION (C-CHECK RO 04/16/2025)REMOVED AND REPLACED LWR ANGLE AND SEAL STRIKER I.A.W CRJ700 SRM 51-42-06 AND KBA670-31407. TASK CARD 51-900-1002-SKY COMPLETED, M-337 ATTACHED
- [SDR SWI2025F00465](https://openairdocs.org/sdr/SWI2025F00465.md): Angle · corroded · Feb 11, 2025 · N710SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LWR SEAL AREA ANGLE KICK PLATE HAS CORROSION AROUND OF THE NUT PLATE. (C-CHECK RO 04/16/2025)REMOVED AND INTALLED PAX DOOR ANGLE KICK PLATE I.A.W CRJ700 SRM 51-42-06. TASK CARD 51-900-1002-SKY COMPLETED, M-337 ATTACHED.
- [SDR SWI2024F00288](https://openairdocs.org/sdr/SWI2024F00288.md): Acm · seized · Apr 16, 2024 · N710SK · Cndair CL6002C10 · Cabin Cooling System
  > D:L PACK AUTOFAIL CAUTION MESSAGE ON TAXI IN. UPON ARRIVAL TO A/C FOUND #1 ACM TO BE SEIZED. DEFERRED #1 TEMP CONTROL SYSTEM PER MEL 21-61-1A. NO MX ACTION REQ. PLEASE REFERENCE AML 1332508 FOR LEFT PACK MELC: MEL 21-61-1ACAT C DUE BY 04/26/24L PACK AUTOFA
- [SDR SWIA202402270003](https://openairdocs.org/sdr/SWIA202402270003.md): Warning Message · illuminated · Feb 23, 2024 · N710SK · Cndair CL6002C10 · Landing Gear Position and Warning
  > D: RECEIVED MASTER WARNING AURAL WARNING SOON AFTER GEAR UP AFTER TAKEOFF. RECEIVED A BRAKE OVHT WARNING MESSAGE PLUS ASSOCIATED AURAL ?BRAKES?. LEFT INBOARD BRAKE INDICATION VARIED IN RED FROM 1 TO 20 WHILE ALL OTHER INDICATIONS WERE GREEN AND 0 OR 1. SOUND A
- [SDR SWIA202402260003](https://openairdocs.org/sdr/SWIA202402260003.md): Warning Message · false indication · Feb 23, 2024 · N710SK · Cndair CL6002C10 · Landing Gear Brake System
  > D: RECEIVED MASTER WARNING AURAL WARNING SOON AFTER GEAR UP AFTER TAKEOFF. RECEIVED A BRAKE OVHT WARNING MESSAGE PLUS ASSOCIATED AURAL ?BRAKES?. LEFT INBOARD BRAKE INDICATION VARIED IN RED FROM 1 TO 20 WHILE ALL OTHER INDICATIONS WERE GREEN AND 0 OR 1. SOUND A
- [SDR SWIA20230404](https://openairdocs.org/sdr/SWIA20230404.md): Windshield · cracked · Apr 4, 2023 · N710SK · Cndair CL6002C10 · Flight Compartment Windows
  > TRANSFER FROM EAML 1115011: LEFT WINDSHIELD WAS ARCING ON FINAL APPROACH. TURNED WSHLD HEAT OFF AND COMPLIED WITH QRH PROCEDURE BEFORE LANDING WITHOUT ISSUE. THERE IS A LONG SOLID CRACK WITH BURN DAMAGE FROM THE TOP THROUGH THE MIDDLE OF THE WINDSHIELD (FLI
- [SDR SWIA202264156](https://openairdocs.org/sdr/SWIA202264156.md): None · corroded · Jan 18, 2022 · N710SK · Cndair CL600* · Fuselage Structure (General)
  > *LOWER SILL JUST FWD OF THE AFT CARGO DOOR ENTRANCE HAS CORROSION AT APPROX. FS.985 TO FS.1000 (MARKED) (C CHECK RO 02-03-22) REPLACED AND MODIFIED LH LOWER SILL FROM APPROX. F.S 985 TO F.S 1000 REF. REO 670-53-61-2048 REV -- DATED 2022-01-22. COMPLIED WI
- [SDR SWIA202264155](https://openairdocs.org/sdr/SWIA202264155.md): None · damaged · Jan 16, 2022 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > CUT AND REPAIR FS 319.00 FRAME BETWEEN STR 25L TO STR 25R TO PERFORM REMOVE AND REPLACE STR 25R BETWEEN FS280.00 TO FS333.00 (C CHECK RO 02-03-22) REPAIRED FS 319.00 FRAME BETWEEN STR 25L TO STR 25R IAW CRJ 700 SRM 53-00-06-201-006-A01. COMPLIED WI
- [SDR SWIA202264194](https://openairdocs.org/sdr/SWIA202264194.md): None · failed · Jan 12, 2022 · N710SK · Cndair CL600* · Flight Control System
  > AFTER RUDDER #3 PCU REPLACEMENT, #3 SYSTEM FAILED BACKLASH. (C CHECK RO 02-03-22) REMOVED AND INSTALLED RUDDER WITH 10 EA. NEW BUSHINGS AND 2 EA. NEW NUTS, REF. CRJ700 AMM 27-24-01-400-801-A01. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 27-320-1000-SKY
- [SDR SWIA202264182](https://openairdocs.org/sdr/SWIA202264182.md): None · corroded · Jan 11, 2022 · N710SK · Cndair CL600* · Fuselage Structure (General)
  > ANGLE SUPPORT, CRAWLWAY FLOOR FS280.00 P/N CC670-34256-3 CORRODED (C CHECK RO 02-03-22) REMOVED AND INSTALLED NEW ANGLE SUPPORT, CRAWLWAY FLOOR FS280.00 P/N CC670-34256-3 REF CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202264154](https://openairdocs.org/sdr/SWIA202264154.md): None · damaged · Jan 10, 2022 · N710SK · Cndair CL600* · Fuselage Structure (General)
  > 9 INCH CREASE FOUND ON FUSELAGE SKIN AT F.S 319-333 BETWEEN STRINGER 25L-26L (C CHECK RO 02-03-22) REPAIR TO FUSELAGE SKIN BETWEEN FS310.00 TO FS349.00 AND STR 24 & 27 LHS. COMPLIED WITH REO 670-53-21-2218 REV -- DATED 2022-01-17. COMPLIED WITH TASK CAR
- [SDR SWIA202264153](https://openairdocs.org/sdr/SWIA202264153.md): None · worn · Jan 8, 2022 · N710SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL FS 333-349 AT STR 26L HAS AROUND FASTENER HOLES (C CHECK RO 02-03-22) REPLACED INTERCOSTAL FS333 - FS349 AT STR 26L. REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32050 REV J. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202264189](https://openairdocs.org/sdr/SWIA202264189.md): None · corroded · Jan 6, 2022 · N710SK · Cndair CL600* · Fuselage Structure (General)
  > CORROSION FOUND ON STIFFENER BETWEEN FS985.00 AND FS1000.00, BETWEEN STGR25L AND STGR26L COMMON TO FUEL-SYSTEM AFT DRAIN MAST (C CHECK RO 02-03-22) REPLACED STIFFENER BETWEEN FS985 - FS1000 STR 25L - 26L. REF CRJ700 SRM 51-40-11-001-001-A01 AND REF CRJ700
- [SDR SWIA202264152](https://openairdocs.org/sdr/SWIA202264152.md): None · corroded · Jan 5, 2022 · N710SK · Cndair CL600* · Fuselage Main, Keel
  > FS 333.00 - 349.00, STGR 26L. / STRINGER HAS SUSPECTED CORROSION. (MARKED) (C CHECK RO 02-03-22) CORROSION ON STRINGER 26L FS333 - FS364 FOUND TO BE OUT OF LIMITS. REPLACED STRINGER REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31350 REV A. COMPLIED
- [SDR SWIA202264151](https://openairdocs.org/sdr/SWIA202264151.md): None · corroded · Jan 5, 2022 · N710SK · Cndair CL600* · Fuselage Main, Keel
  > FS 319.70 - 333.00, STGR 25R. / STRINGER AND STRINGER SPLICE HAVE SUSPECTED CORROSION. (MARKED) (C CHECK RO 02-03-22) / REMOVED AND REPLACED STR 25R BETWEEN FS280.00 TO FS 333.00 REF CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-06-001-001-A01, RE
- [SDR SWIA202164181](https://openairdocs.org/sdr/SWIA202164181.md): None · cracked · Dec 22, 2021 · N710SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > THE CHANNEL BRACKET COMMON TO CENTER INTERCOSTAL DD1 IS CRACKED (C CHECK RO 02-03-22) INSTALLED THE CHANNEL BRACKET COMMON TO CENTER INTERCOSTAL DD1 REF. CRJ700 SRM 51-42-21-001-001-A01
- [SDR SWIA202164150](https://openairdocs.org/sdr/SWIA202164150.md): None · cracked · Dec 22, 2021 · N710SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > RH 1-3 SLAT TRACK CANISTER INSIDE RH WING FUEL TANK HAS CRACKED WELD (C CHECK RO 02-03-22) COMPLIED WITH R/H WING SLAT TRACK CANISTER REPAIR REF REO 670-5742-577 REV-- DATED 2016-12-02. SEE CONTINUE CARD FOR WORK PERFORMED. COMPLIED WITH SKY CARDS 51-900-1
- [SDR SWIA202164149](https://openairdocs.org/sdr/SWIA202164149.md): None · corroded · Dec 22, 2021 · N710SK · Cndair CL600* · Fuselage Main, Keel
  > STRINGER AT FS 1000, LBL26 HAS EXFOLIATED CORROSION. (C CHECK RO 02-03-22) CORROSION ON STRINGER 26L BETWEEN FS985 AND FS1000 FOUND TO BE OUT OF LIMITS. REPAIRED STRINGER REF REO 670-53-61-2034 REV -- 2022-01-13. COMPLIED WITH TASK CARD 51-900-1002-SKY. LE
- [SDR SWIA202164148](https://openairdocs.org/sdr/SWIA202164148.md): None · corroded · Dec 16, 2021 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > FRAME AT FS1047 BETWEEN STR 23L - 27 IS CORRODED. (C CHECK RO 02-03-22) REPAIRED FRAME AT FS1047.00 STGR23L - STGR27 REF REO 670-53-61-2031 REV -- DATED 2022-01-17.. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202164188](https://openairdocs.org/sdr/SWIA202164188.md): None · cracked · Dec 15, 2021 · N710SK · Cndair CL600* · Fuselage Structure (General)
  > FOUND CRACK ON Z STIFFENER ANGLE @ PAX DOOR AFT WEB. REPLACE. (C CHECK RO 02-03-22) REPLACED PAX DOOR AFT WEB Z STIFFENER. REF CRJ700 SRM 51-42-06-001-001-A01.
- [SDR SWIA202164180](https://openairdocs.org/sdr/SWIA202164180.md): None · elongated · Dec 15, 2021 · N710SK · Cndair CL600* · Fuselage, Door Hinge
  > FOUND ELONGATED HOLES ON ATTACHMENT ANGLE @ AFT PAX DOOR WEB. (C CHECK RO 02-03-22) REMOVED AND REPLACED THE AFT DRAG ANGLE PART # 601R31772-5 COMMON TO THE PAX DOOR AFT STAIR WEB REF. CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-40-11-001-001-A01
- [SDR SWIA202164147](https://openairdocs.org/sdr/SWIA202164147.md): None · cracked · Dec 15, 2021 · N710SK · Cndair CL600* · Powerplant System
  > LH UPPER TRANSCOWL CRACKED ON INNER SKIN UNDER Z-STIFFENERS FOR LATCH DOOR COAMING (C CHECK RO 02-03-22) PERFORMED REO REPAIR ON LH UPPER TRANSCOWL Z-STIFFENER FOR LATCH DOOR COAMING. PER REO 670-54-21-1495 REV -A DATED 2022-01-27 / COMPLIED WITH TASK CARD
- [SDR SWIA202164146](https://openairdocs.org/sdr/SWIA202164146.md): None · chafed · Dec 13, 2021 · N710SK · Cndair CL600* · Powerplant System
  > LH UPPER TRANSCOWL LATCH DOOR COAMING CHAFED AT LATCH DOOR MATING SURFACES NEAR ALIGNMENT PIN OPINING AND ON LEADING EDGE IB SIDE (C CHECK RO 02-03-22) REMOVED AND REPLACED LATCH DOOR COAMING ON LEFTHAND UPPER TRANSCOWL IAW CRJ 700 SRM 51-42-06-001-001-A0
- [SDR SWIA202164179](https://openairdocs.org/sdr/SWIA202164179.md): None · corroded · Dec 8, 2021 · N710SK · Cndair CL600* · Fuselage, Door Hinge
  > HANDRAIL BRACKETS ON FWD PAX DOOR WEB IS DAMAGE NEED TO BE REPLACE. (C CHECK RO 02-03-22) REMOVED AND REPLACED HANDRAIL BRACKETS ON FWD PAX DOOR WEB REF CRJ700 SRM 51-42-21-001-001-A01
- [SDR SWIA202164145](https://openairdocs.org/sdr/SWIA202164145.md): None · cracked · Dec 8, 2021 · N710SK · Cndair CL600* · Powerplant System
  > LH LOWER TRANSCOWL FWD LATCH COAMING APPEARS CRACKED FROM FWD LATCH CUTOUT FORWARD TO THE LEADING EDGE. (C CHECK RO 02-03-22) PERFORMED LH LOWER TRANSCOWL FWD LATCH COAMING REPLACEMENT IAW REO670-54-21-1207 REV. A DATE: 2015-08-27. COMPLIED WITH TASK CARD
- [SDR SWIA202164144](https://openairdocs.org/sdr/SWIA202164144.md): None · corroded · Dec 7, 2021 · N710SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT STA 1031 LBL 27 IS CORRODED. (C CHECK RO 02-03-22) REPAIRED FLOOR BEAM AT STATION 1031 LBL 27 IAW CRJ 700 SRM 53-00-41-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202164143](https://openairdocs.org/sdr/SWIA202164143.md): None · corroded · Dec 7, 2021 · N710SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT STA 1031 LBL 9 IS CORRODED. (C CHECK RO 02-03-22) REPAIRED FLOOR BEAM AT STA 1031 LBL 9 IAW CRJ700 SRM 53-00-41-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202164142](https://openairdocs.org/sdr/SWIA202164142.md): None · corroded · Dec 6, 2021 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > FWD FRAME FS313.56 BETWEEN DD4 AND DD5 HAS CORROSION. (C CHECK RO 02-03-22) CORROSION ON PAX DOOR FWD FRAME AT FS313.56 BETWEEN DD4 AND DD5 FOUND TO BE OUT OF LIMITS. REPLACED FRAME REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG: 601R31702 REV N. COMPLIED WI
- [SDR SWIA202164187](https://openairdocs.org/sdr/SWIA202164187.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PAX DOOR INTERCOSTAL AFT DD6 (C CHECK RO 02-03-22) REMOVED CORROSION ON PAX DOOR INTERCOSTAL AFT DD6. ORIGINAL MATERIAL THICKNESS IS 0.050 NDT REPORTS MINIMUM MATERIAL THICKNESS MEASURED AT 0.049 WITH 0.01 MATERIAL LOSS INTERCOSTAL FOUND TO B
- [SDR SWIA202164141](https://openairdocs.org/sdr/SWIA202164141.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION ON PAX DOOR AFT FRAME AT FS338 (C CHECK RO 02-03-22) REMOVED CORROSION ON PAX DOOR AFT FRAME AT FS338. ORIGINAL MATERIAL THICKNESS OF AFT FRAME WAS 0.063". REMOVED MATERIAL THICKNESS IS 0.003", REMAINING MATERIAL THICKNESS IS 0.060". FOUND TO BE
- [SDR SWIA202164140](https://openairdocs.org/sdr/SWIA202164140.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION ON PAX DOOR FWD FRAME AT FS338 710170114$M127 (C CHECK RO 02-03-22) REMOVED CORROSION ON PAX DOOR FWD FRAME. ORIGINAL MATERIAL THICKNESS OF FWD FRAME WAS 0.063". REMOVED MATERIAL THICKNESS IS 0.002", REMAINING MATERIAL THICKNESS IS 0.061". FOUND
- [SDR SWIA202164139](https://openairdocs.org/sdr/SWIA202164139.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION ON PAX DOOR FRAME AT FS327 (C CHECK RO 02-03-22) CORROSION ON PAX DOOR FRAME AT FS327 FOUND TO BE OUT LIMITS. REPLACED FRAME REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DWG: 601R31702 REV N. COMPLIED WITH TASK CAR
- [SDR SWIA202164138](https://openairdocs.org/sdr/SWIA202164138.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION ON PAX DOOR FRAME AT FS320, THE AFT FRAME ATTACH FLANGE AND BETWEEN THE FRAMES (C CHECK RO 02-03-22) CORROSION ON PAX DOOR FRAME AT FS320 FOUND TO BE OUT OF LIMITS. REPLACED FRAME REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-00
- [SDR SWIA202164137](https://openairdocs.org/sdr/SWIA202164137.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PAX DOOR INTERCOSTAL DD7 BETWEEN FS320 AND FS327 (C CHECK RO 02-03-22) CORROSION ON PAX DOOR INTERCOSTAL DD7 BETWEEN FS320 AND FS327 FOUND TO BE OUT OF LIMITS. REPLACED INTERCOSTAL REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG: 601R31702 REV N
- [SDR SWIA202164136](https://openairdocs.org/sdr/SWIA202164136.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PAX DOOR INTERCOSTAL AFT DD5 (C CHECK RO 02-03-22) CORROSION ON PAX DOOR INTERCOSTAL AFT DD5 FOUND 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-SK
- [SDR SWIA202164135](https://openairdocs.org/sdr/SWIA202164135.md): None · corroded · Dec 4, 2021 · N710SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION ON PAX DOOR AFT FORMER FS347 (C CHECK RO 02-03-22) CORROSION ON PAX DOOR AFT FORMER AT FS347 FOUND TO BE OUT OF LIMITS. REPLACED FORMER REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND
- [SDR SWIA202164186](https://openairdocs.org/sdr/SWIA202164186.md): None · corroded · Dec 3, 2021 · N710SK · Cndair CL600* · Fuselage Structure (General)
  > FWD INNER CORD ON AFT CARGO DOOR SILL FS 1000 HAS CORROSION. (C CHECK RO 02-03-22) REMOVED AND REPLACED FWD INNER CORD ON AFT CARGO DOOR SILL IAW CRJ700 SRM 51-42-06-001-001-A01

Next page: https://openairdocs.org/aircraft/N710SK/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 = 'N710SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N710SK/reports

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