# Service difficulty reports: N715SK

A list on [N715SK](https://openairdocs.org/aircraft/N715SK.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 3 · 144 reports

- [SDR SWIA2026071576655](https://openairdocs.org/sdr/SWIA2026071576655.md): Unknown · odor · Jul 15, 2026 · N715SK · Cndair CL6002C10 · Air Distribution System
  > FUME EVENT. EXTREMELY STRONG DIRTY SOCK ODOR, EYES BURNED. SMELLED THROUGHOUT FLIGHT DECK AND CABIN. FLIGHT 6396. OPEN
- [SDR SWIA2026032875600](https://openairdocs.org/sdr/SWIA2026032875600.md): Skin · damaged · Mar 28, 2026 · N715SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA110660-REO 670-53-31-1164 N715SK MXCODEID120995-TR - COMPLY WITH TEMPORARY REPAIR ON RA ID: 110660 BLENDED LIGHTNING STRIKE DAMAGE TO CENTER FUSELAGE LOWER SKIN BTW BS 565 - 581 STR24L - STR25L PER REO 670-53-31-1164
- [SDR SWIA2025080500001](https://openairdocs.org/sdr/SWIA2025080500001.md): Ballast · failed · Aug 1, 2025 · N715SK · Cndair CL6002C10 · Passenger Compartment Lighting
  > BURNING ELECTRICAL SMELL THROUGH OUT THE AIRPLANE. (FLIGHT 6240) UPON ARRIVAL TO AC, INTERROGATED EVIDENCE OF ELECTRICAL BURNING SMELL AND COULD NOT SMELL OR SEE ANY EVIDENCE OF SAID ELECTRICAL SMELLS IN AC. HAD SERVAL MXS COME ON BOARD TO VERIFY, AND EVERY M
- [SDR SWIA2025073000512](https://openairdocs.org/sdr/SWIA2025073000512.md): Hinge Arm · gouged · May 12, 2025 · N715SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD CARGO DOOR, AFT HINGE ARM AT OPEN LOCK LEVER IS GOUGED. REPAIRED DAMAGED ON FWD CARGO DOOR AFT HINGE ARM AT OPEN LOCK LEVER IAW REO-670-52-35-558 REV -. NDT PERFORMED.
- [SDR SWIA20250505](https://openairdocs.org/sdr/SWIA20250505.md): Slat Track · corroded · May 5, 2025 · N715SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 SHOWING SIGNS OF CORROSION AND WEAR. REMOVED CORROSION ON ROLLING SURFACE AT RT SLAT TRACK 2-2 FOUND TO BE IN LIMITS IAW REO 670-57-42-2116 REV- AND IAW SRM 51-12-00. PERFORMED NDT PT INSPECTION, NO DEFECTS NOTED AT TIME OF INSPECTION.
- [SDR SWIA2025073000503](https://openairdocs.org/sdr/SWIA2025073000503.md): Slat Track · corroded · May 3, 2025 · N715SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 HAS SIGNS OF CORROSION ON THE UPPER SURFACE. REMOVED DAMAGE AND EVALUATED REWORKED AREA ON SLAT TRACK 1-2 LT UPPER SURFACE, THE SUBJECT REWORKED CONDITION IS STRUCTURALLY AND FUNCTIONALLY ACCEPTABLE, COMPLETE DAMAGE HAS BEEN REMOVED, THE
- [SDR SWIA2024101510003](https://openairdocs.org/sdr/SWIA2024101510003.md): Bracket · detached · Oct 3, 2024 · N715SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR POWER-ASSIST MOTOR CABLE BRACKET PULLED FROM FRAME. (FILED CLOSED)PERFORMED A TEMPORARY REPAIR TO THE PASSENGER DOOR IN REFERENCE TO REO 670-52-11-1413 REV -- DATED 13OCT2024. COMPLIED WITH TASK CARD 51-900-1002-SKY. THIS TEMPORARY REPAIR IS ON
- [SDR ICRR202408270001](https://openairdocs.org/sdr/ICRR202408270001.md): Link · cracked · Aug 27, 2024 · N715SK · Cndair CL6002C10 · Fuselage Structure (General)
  > FAILED EDDY CURRENT PER NDT MANUAL PART 6, CRJ 700 71-21-101-250
- [SDR SWIA2024070300630](https://openairdocs.org/sdr/SWIA2024070300630.md): Plate · gouged · Jun 30, 2024 · N715SK · Cndair CL6002C10 · Horizontal Stabilizer Structure
  > HSTA LH UPPER FITTING HAS GOUGES ON THE LOCKING PLATE (FILED CLOSED) REFERENCE CP 28466575, OUT OF LIMITS GOUGES FOUND ON HSTA L/H UPPER BEARING ATTACH FITTING ANTI-ROTATION PLATE SURFACE DETERMINED TO BE MAJOR REPAIR. COMPLY WITH TEMPORARY REPAIR/BLEND O
- [SDR SWIA2024070300627](https://openairdocs.org/sdr/SWIA2024070300627.md): Attach Fitting · gouged · Jun 27, 2024 · N715SK · Cndair CL6002C10 · Horizontal Stabilizer Structure
  > THE HSTA RT HAND TOP ATTACHMENT HAS GOUGES ON THE INNER RACE (FILED CLOSED) REFERENCE CP 28466355, OUT OF LIMITS GOUGES FOUND ON HSTA R/H UPPER BEARING ATTACH FITTING INNER RACE SURFACE DETERMINED TO BE MAJOR REPAIR. COMPLIED WITH REO 670-55-11-396 DATED 20
- [SDR SWIA2024022600175](https://openairdocs.org/sdr/SWIA2024022600175.md): Window Post · cracked · Feb 20, 2024 · N715SK · Cndair CL6002C10 · Fuselage Main, Structure
  > DURING REMOVAL OF RH SIDE WINDSHIELD FOUND CRACK ON THE UPPERMOST BARREL NUT OF THE RH WINDOW/WINDSHIELD SIDE POST. (FILED CLOSED)REMOVED AND REPLACED RH SIDE POST. IN REFERENCE TO SRM REF: 53-11-35 / 51-42-21 AND INSTALLATION DWG # CC670-33055 REV F. SEE ATTA
- [SDR SWIA2023010567074](https://openairdocs.org/sdr/SWIA2023010567074.md): Fire Detector · false activation · Jan 2, 2023 · N715SK · Cndair CL6002C10 · Fire Detection
  > APU FIRE GOING INTO ASE, DIVERT TO GJT. APU SHUT ITSELF DOWN. (FLIGHT 3077 - FILED CLOSED) OPENED APU ACCESS DOORS AND VISUALLY INSPECTED APU AREA FOR EVIDENCE OF SMOKE, FIRE OR HEAT DAMAGE. NO DEFECTS NOTED. INSPECTED WIRING HARNESS'S AND APU GEN CONNECTI
- [SDR SWIA202266462](https://openairdocs.org/sdr/SWIA202266462.md): None · failed · Sep 12, 2022 · N715SK · Cndair CL6002C10 · Stabilizer Position Indicating
  > AFTER TAKEOFF DURING NORMAL TRIM OPERATION, THE TRIM CLACKER SOUNDED. AIRCRAFT WAS SPEEDING UP THROUGH ABOUT 190 KNOTS. FLIGHT DIRECTOR WAS ON IN SPEED MODE AND NAV MODE WITH AUTOPILOT DISENGAGED. CAPTAIN MOVED TRIM SWITCH BOTH DIRECTION AND TRIM CONTINUED MOV
- [SDR SWIA202265346](https://openairdocs.org/sdr/SWIA202265346.md): None · none · Mar 6, 2022 · N715SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > WHILE INSTALLING THE PAX DOOR FOUND THE PAX DOOR HINGE PIN SPRING PIN HOLE TO BE OVERSIZED APROX.128 IN. IN THE PAX DOOR HINGE HALF. (C-CHECK RO 4/9/2022) COMPLIED WITH REO 670-52-11-1287 REV-- DATED 2022-03-06 AND SKYCARD 51-900-1002-SKY FOR REPAIR O
- [SDR SWIA202265345](https://openairdocs.org/sdr/SWIA202265345.md): None · damaged · Mar 3, 2022 · N715SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR BEAM REPAIR TRANSFERED FROM PARENT CAMP # 24158512 / JOB: 910179104 OP: 89 FROM CONTINUATION CARD LINE ITEM #2 PERFORM FLOOR BEAM REPAIR PER CRJ 700 SRM 53-00-41-201-001-A01 AT FS 978 TO FS 1037. (C-CHECK RO 4/9/2022) REPAIRED FLOOR BEAM AT
- [SDR SWIA202265344](https://openairdocs.org/sdr/SWIA202265344.md): None · corroded · Feb 21, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PAX DOOR AFT CLOSEOUT FITTING IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PASSENGER DOOR AFT CLOSEOUT FITTING IAW CRJ 700 SRM 51-42-06-001-001-A01 REV38B DAT
- [SDR SWIA202265343](https://openairdocs.org/sdr/SWIA202265343.md): Fitting · corroded · Feb 21, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWDCLOSEOUT FITTING IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR FWD CLOSE OUT FITTING IAW CRJ-700 SRM 51-42-06-001-001-A01 REVISION 38B - 1
- [SDR SWIA202265342](https://openairdocs.org/sdr/SWIA202265342.md): None · corroded · Feb 21, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PAX DOOR UPPER AFT SILL ANGLE IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR UPPER AFT SILL ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01 REV38B DATED 14
- [SDR SWIA202265341](https://openairdocs.org/sdr/SWIA202265341.md): None · corroded · Feb 21, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD UPPER SILL ANGLE IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REPAIRED PAX DOOR FWD UPPER SILL ANGLE BY REPLACEMENT IAW SRM 51-42-06-001-001-AO1, COMPLETED TASK CAR
- [SDR SWIA202265340](https://openairdocs.org/sdr/SWIA202265340.md): None · corroded · Feb 19, 2022 · N715SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FOUND CORROSION AT LBL 9 FS549 ON FLOOR BEAM CAP (C-CHECK RO 4/9/2022) REMOVED AND REPLACED FLOOR BEAM SECTION FROM LBL 9 FS544 TO FS570 IAW CRJ700 SRM 53-00-41-201-001-A01. TASK CARD 51-900-1002-SKY AND M-337 ATTACHED WITH NO SIGNIFICANT CHANGE TO WEI
- [SDR SWIA202265339](https://openairdocs.org/sdr/SWIA202265339.md): None · corroded · Feb 6, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Keel
  > FOUND STRINGER 25L FROM F.S.280.00 TO F.S.333.00 AND 25L SPLICE AT F.S.333.00 TO BE CORRODED. (C-CHECK RO 4/9/2022) REMOVED DAMAGED STRINGER 25L FROM FS 280.00 TO 333.00 AND INSTALLED A NEW STRINGER AND SPLICE IAW CXRJ 700 SRM 51-42-06-001-001-A01 AND
- [SDR SWIA202265338](https://openairdocs.org/sdr/SWIA202265338.md): None · corroded · Jan 25, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > WHILE WORKING STR 26R CORROSION. FOUND INTERCOSTAL AT STR 26R FROM FS349.00 TO FS364.00 TO BE CORRODED. (C-CHECK RO 4/9/2022) INTERCOSTAL AT STR 26R FROM FS349.00 TO FS364.00 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-00
- [SDR SWIA202265337](https://openairdocs.org/sdr/SWIA202265337.md): None · gouged · Jan 18, 2022 · N715SK · Cndair CL6002C10 · Doors
  > AFT BAGGAGE BAY DOOR OUTER HANDLE HOUSING GOUGED. (C-CHECK RO 4/9/2022) REMOVED OUTER HANDLE HOUSING AND INSTALLED A NEW SERVICE A HANDLE HOUSING IAW CRJ 700 AMM 52-31-03-400-801-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. REFERENCE CONTINUATION CARD FOR
- [SDR SWIA202265336](https://openairdocs.org/sdr/SWIA202265336.md): None · cracked · Jan 17, 2022 · N715SK · Cndair CL6002C10 · Elevator Tab, Attach Fittings
  > RH ELEVATOR LEADING EDGE CLOSING RIB BRACKET FOR ACCESS PANEL CRACKED. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED R/H ELEVATOR LEADING EDGE INBD CLOSING RIB IAW CRJ700 SRM 51-42-06-001-001-A01 REV. 38B DATED 14 DEC 2020 AND REO 670-55-21-146 REV-- DATE
- [SDR SWIA202265335](https://openairdocs.org/sdr/SWIA202265335.md): None · corroded · Jan 17, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PAX DOOR DD5 INTERCOSTAL CORRODED. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR DD5 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLE
- [SDR SWIA202265334](https://openairdocs.org/sdr/SWIA202265334.md): None · corroded · Jan 17, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PAX DOOR FWD FORMER CORRODED AT FS311.75 (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER AT FS311.75 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD AND FORM M-337 COMPLETED
- [SDR SWIA202265333](https://openairdocs.org/sdr/SWIA202265333.md): None · corroded · Jan 17, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > PAX DOOR DD4 INTERCOSTAL CORRODED BETWEEN FS320 AND FS338.963. (C-CHECK RO 4/9/2022) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT DD3 INTERCOSTAL BETWEEN FS320 AND FS338.963. REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD3 FS320-FS338.963 IAW CR
- [SDR SWIA202265332](https://openairdocs.org/sdr/SWIA202265332.md): None · corroded · Jan 17, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PAX DOOR DD4 INTERCOSTAL CORRODED BETWEEN FS311.75 AND FS320. (C-CHECK RO 4/9/2022) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT DD3 INTERCOSTAL AT FS311-FS320. REMOVED AND REPLACED PAX DOOR DD3 INTERCOSTAL AT FS311 AND 320 I.A.W. CRJ-700 SRM 51
- [SDR SWIA202265331](https://openairdocs.org/sdr/SWIA202265331.md): None · corroded · Jan 15, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND MULTIPLE AREAS OF CORROSION ON RBL 27 FS 1031-1051 (C-CHECK RO 4/9/2022) REPAIRED FLOORBEAM ON RBL 27 FROM FS 1031-1051 IAW CRJ 700 SRM 53-00-41-201-001-A01. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM 337 COMPLETED AND ATTACHED. WEIGHT CHANG
- [SDR SWIA202265330](https://openairdocs.org/sdr/SWIA202265330.md): Skin · chafed · Jan 15, 2022 · N715SK · Cndair CL6002C10 · Ailerons
  > L/H INBD. FLAP VANE HAS MULTIPLE LONG LEADING EDGE CHAFFES (AS MARKED) (C-CHECK RO 4/9/2022) L/H INBD FLAP VANES WERE REPAIRED AND REPLACED AS REQUIRED IAW CRJ 700 SRM 51-42-13-001-001-A01 & REO 670-57-52-521 REV-- DATED: 2022-03-07 COMPLETED SKYCARD
- [SDR SWIA202265329](https://openairdocs.org/sdr/SWIA202265329.md): None · chafed · Jan 15, 2022 · N715SK · Cndair CL6002C10 · Ailerons
  > R/H INBD. FLAP VANE HAS MULTIPLE LONG LEADING EDGE CHAFFES ( AS MARKED) (C-CHECK RO 4/9/2022) REMOVED AND REPLACED R/H FLAP VANE CAP, INBD MID L/E SKIN AND O/B MID L/E SKIN IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-13-001-001-A01
- [SDR SWIA202265328](https://openairdocs.org/sdr/SWIA202265328.md): None · corroded · Jan 11, 2022 · N715SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT FS 978-1088 LBL 27 HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 4/9/2022) FLOOR BEAM AT FS 978-1088 LBL 27 WAS REPAIRED IAW REO 670-53-61-2063 REV -- DATED 2022-03-07. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHE
- [SDR SWIA202265327](https://openairdocs.org/sdr/SWIA202265327.md): None · corroded · Jan 11, 2022 · N715SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT FS 978-1088 LBL 9 HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 4/9/2022) REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 670-53-61-2058 REV --DATED 2022-02-14. TASK CARD 51-900-1002-SKY AND M-337 ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.
- [SDR SWIA202265326](https://openairdocs.org/sdr/SWIA202265326.md): None · corroded · Jan 11, 2022 · N715SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR BEAM AT FS 978-1088 RBL 9 HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK RO 4/9/2022) REPAIRS WERE ACCOMPLISHED IAW MHIRJ REO 670-53-61-2061 REV -- DATED 2022-02-22 WITH NO CHANGE TO WEIGHT AND BALANCE. TASK CARD 51-900-1002-SKY AND M-337 ATTACHED
- [SDR SWIA202265325](https://openairdocs.org/sdr/SWIA202265325.md): None · corroded · Jan 11, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 1000 IS CORRODED BETWEEN STGR 27-26L (C-CHECK RO 4/9/2022) REPAIRED FS1000 FRAME IAW MHIRJ REO 670-53-61-2059 REV-- DATED 2022-02-14. SKYWEST MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLIED WITH. REFERENCE CONTINUATION CARD FOR WORK PERFORME
- [SDR SWIA202265324](https://openairdocs.org/sdr/SWIA202265324.md): None · bent · Jan 11, 2022 · N715SK · Cndair CL6002C10 · Doors
  > FWD. CARGO DOOR LOWER SEAL RETANIER BENT AND BUCKELED IN MULTIPLE AREAS AND CHAFFED ON CORNER END (C-CHECK RO 4/9/2022) REMOVED AND REPLACED FWD. CARGO DOOR LOWER SEAL RETAINER I.A.W. CRJ-700 SRM 51-42-06-001-001-A01 REV.38B, DATED 12/14/2020. SKYWEST T
- [SDR SWIA202265323](https://openairdocs.org/sdr/SWIA202265323.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 364 FRAME IS CORRODED BETWEEN STGR 26L TO 25L. (C-CHECK RO 4/9/2022) REPAIRED FRAME AT F.S 364 BETWEEN STGR26L TO 25L IAW MHI REO # 670-53-21-687 REV-A DATED 2016/06/06 AND SKYCARD 51-900-1002-SKY.NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION
- [SDR SWIA202265322](https://openairdocs.org/sdr/SWIA202265322.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVI DOOR INTERCOSTAL IS CORRODED AT STGR 27. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED BOTH LATCH PIN INTERCOSTALS AT STGR 27 FORM FS349-FS364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CA
- [SDR SWIA202265321](https://openairdocs.org/sdr/SWIA202265321.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVI BAY DOOR INTERCOSTAL IS CORRODED AT STGR 26L. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STGR 26L FROM FS349-FS364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FO
- [SDR SWIA202265320](https://openairdocs.org/sdr/SWIA202265320.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 349 FRAME IS CORRODED BETWEEN STGR 27 TO 26R. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED FS 349 LOWER FRAME SEGEMENT IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND
- [SDR SWIA202265319](https://openairdocs.org/sdr/SWIA202265319.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Keel
  > STGR 26R IS CORRODED BETWEEN F.S. 333 TO F.S. 364. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STGR 26R FROM FS 333-FS 364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AN
- [SDR SWIA202265318](https://openairdocs.org/sdr/SWIA202265318.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Keel
  > STGR 26L IS CORRODED BETWEEN F.S. 333 TO 364. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STR 26L FROM FS 333- FS 364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FOR
- [SDR SWIA202265317](https://openairdocs.org/sdr/SWIA202265317.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Keel
  > STGR 25R IS CORRODED BETWEEN F.S. 319 TO F.S. 333. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STRINGER 25R AND SPLICE FROM FS280- FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASKS CARD 51-
- [SDR SWIA202265316](https://openairdocs.org/sdr/SWIA202265316.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 319 FRAME IS CORRODED BETWEEN STGR 26L TO 26R. (C-CHECK RO 4/9/2022) REPAIRED F.S. 319 FRAME BETWEEN STR 25L AND STR 23R IAW CRJ 700 SRM 53-00-06-201-006-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETE
- [SDR SWIA202265315](https://openairdocs.org/sdr/SWIA202265315.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Galley Doors
  > SERVICE DOOR SEAL RETAINER ON THE FUSELAGE IS CORRODED ON THE AFT SIDE AROUND SCREW HOLES AT THE BOTTOM. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED THE SERVICE DOOR SEAL STRIKER RETAINER IAW CRJ-700 SRM 51-42-06-001-001-A01 REV.38B, DATED 12/14/2020. C
- [SDR SWIA202265314](https://openairdocs.org/sdr/SWIA202265314.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Structure (General)
  > ATENNA DOUBLER IS CORRODED BETWEEN F.S. 295 TO F.S. 310 STGR 26R TO 26L. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED ANTENNA DOUBLER BETWEEN F.S. 295 TO F.S. 310 STGR 26R TO 26L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATE
- [SDR SWIA202265313](https://openairdocs.org/sdr/SWIA202265313.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > F.S. 310 FRAME IS CORRODED BETWEEN STGR 25L TO 26R. (C-CHECK RO 4/9/2022) FS 310.00 FRAME WAS REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01, NO CHANGE TO WEIGHT ANDE BALANCE. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED
- [SDR SWIA202265312](https://openairdocs.org/sdr/SWIA202265312.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 1051 STRG 27 IS CORRODED (C-CHECK RO 4/9/2022) REPAIRED FRAME AT FS 1051.30 BETWEEN STR24L-STR24R IAW REO 670-53-61-2060 REV.-- DATED 2022-03-14. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE
- [SDR SWIA202265311](https://openairdocs.org/sdr/SWIA202265311.md): None · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Doors
  > PASSENGER DOOR UPPER SILL ANGLE IS CORRODED. (C-CHECK RO 4/9/2022) DISCREPANCY SHOULD HAVE READ PAASENGER DOOR UPPER MID SILL CORRODED. REMOVED AND REPLACED PAX DOOR MID UPPER SILL ANGLE WITH A SERVICEABLE PART IAW CRJ 700 AMM 20-21-00-910-801-A01. MAJ
- [SDR SWIA202265310](https://openairdocs.org/sdr/SWIA202265310.md): Frame · corroded · Jan 10, 2022 · N715SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS1051 IS CORRODED BETWEEN STRG 26L-26R (C-CHECK RO 4/9/2022) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT FS 1015.00 BETWEEN 26L-26R. COMPLIED WITH MHIRJ REO 670-53-61-2062 REV.-- DATED 2022-02-22 FOR FRAME SPLICE REPAIR ON FRAME 1015.0

Next page: https://openairdocs.org/aircraft/N715SK/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 = 'N715SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N715SK/reports

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