# Service difficulty reports: N706SK

A list on [N706SK](https://openairdocs.org/aircraft/N706SK.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 5 · 239 reports

- [SDR SWIA2025091500013](https://openairdocs.org/sdr/SWIA2025091500013.md): Hose · faulted · Sep 13, 2025 · N706SK · Cndair CL6002C10 · Hydraulic System, Main
  > HYD 3 LO PRESS CAUTION MSG. CHECKED HYDRAULICS PAGE AND SHOWED 0 % FLUID REMAINING. RAN QRH AND DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. TOWED INTO GATE. (FLIGHT 6510 - FILED CLOSED) PLEASE REFERENCE AML 1703109 FOUND HYD HOSE IN BELLEY FARING NO.320 ON
- [SDR SWIA202411271013](https://openairdocs.org/sdr/SWIA202411271013.md): Angle · cracked · Oct 13, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > CRACK FOUND AT BULKHEAD ANGLE BL26.00 FS280.00 (HN00194250) (C-CHECK RO 11/26/2024) REMOVED AND REPLACED ANGLE RBL26.00 FS280.00 REF CRJ700 SRM51-42-06-001-001-A01, SRM51-42-13-001-001-A01 AND DWG NO. CC670-34010 REV -K. COMPLIED WITH TASK CARD 51-900-
- [SDR SWIA2024112701305](https://openairdocs.org/sdr/SWIA2024112701305.md): Stringer Splice · corroded · Oct 11, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER SPLICE STR 26R AT FS333 HAS DEEP CORROSION (C-CHECK RO 11/26/2024) REPLACED STRINGER SPLICE AT FS333 AND STGR 26R REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2024112701011](https://openairdocs.org/sdr/SWIA2024112701011.md): Stringer · corroded · Oct 11, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R FROM FS280 TO FS333 HAS SEVERE CORROSION (C-CHECK RO 11/26/2024) REPLACED STRINGER 26R AT FS280 - FS333 CRJ-700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020, CRJ-700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020 AND DWG SH670-31630 REV K. LEA
- [SDR SWIA2024112701304](https://openairdocs.org/sdr/SWIA2024112701304.md): Floorbeam · corroded · Oct 7, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION FOUND AT RH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 (C-CHECK RO 11/26/2024) REMOVED AND REPLACED RH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 REF CRJ700 SRM51-42-06-001-001-A01, SRM51-42-10-001-001-A01, SRM51-42-22-001-001-A01 REV 38 D
- [SDR SWIA202411271007](https://openairdocs.org/sdr/SWIA202411271007.md): Floorbeam · corroded · Oct 7, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION FOUND AT LH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 (C-CHECK RO 11/26/2024) REMOVED AND REPLACED LH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 REF CRJ700 SRM51-42-06-001-001-A01, SRM51-42-10-001-001-A01 AND SRM51-42-22-001-001-A01 REV
- [SDR SWIA2024112701301](https://openairdocs.org/sdr/SWIA2024112701301.md): Handle · gouged · Oct 4, 2024 · N706SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR HANDLE HOUSING HAS NUMEROUS GOUGES (C-CHECK RO 11/26/2024) AFT CARGO DOOR HANDLE HOUSING IS OUT OF LIMITS PER REO 670-52-31-031 REV -B DATE 2016-12-07. REMOVED AND INSTALLED 1EA NEW AFT CARGO DOOR HANDLE HOUSING PER CRJ700SRM 51-42-
- [SDR SWIA2024112701300](https://openairdocs.org/sdr/SWIA2024112701300.md): Slat Track · damaged · Oct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT WING - SLAT TRACK 3-3 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) COMPLIED WITH REO 670-57-42-1788 REV-- DATED 2024-10-18, BLEND WAS PERFORMED CORRECTLY AND MADE SMOOTH. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-S
- [SDR SWIA2024112701299](https://openairdocs.org/sdr/SWIA2024112701299.md): Slat Track · damaged · Oct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT WING - SLAT TRACK 2-3 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) COMPLIED WITH REO 670-57-42-1787 REV-- DATED 2024-10-18, BLEND WAS PERFORMED CORRECTLY AND MADE SMOOTH. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SK
- [SDR SWIA2024112701298](https://openairdocs.org/sdr/SWIA2024112701298.md): Slat Track · damaged · Oct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING - SLAT TRACK 3-2 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) REMOVED GROOVING DAMAGE FROM LH SLAT TRACK 3-2 AND FOUND ACCEPTABLE AT THIS TIME REF REO 670-57-42-1795 REV -- 2024-10-21. COMPLIED WITH TASK CARD 51-900-1002-
- [SDR SWIA2024112701297](https://openairdocs.org/sdr/SWIA2024112701297.md): Slat Track · grooved · Oct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING - SLAT TRACK 1-1 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) COMPLIED WITH REPAIR OF WEAR DAMAGE TO LH SLAT TRACK 1-1 REF REO 670-57-42-1786 REV-- DATED 2024-10-17 ALL STEPS COMPLIED WITH. CLEARANCE CHECK GOOD. COMPLIE
- [SDR SWIA202411271004](https://openairdocs.org/sdr/SWIA202411271004.md): Slat Track · grooved · Oct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT WING - SLAT TRACK 2-1 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) REMOVED GROOVING DAMAGE FROM LH SLAT TRACK 2-1 AND FOUND ACCEPTABLE AT THIS TIME REF REO 670-57-42-1789 REV -- 2024-10-21. COMPLIED WITH TASK CARD 51-900-1002-S
- [SDR SWI2024112701296](https://openairdocs.org/sdr/SWI2024112701296.md): Striker · dented · Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PASSENGER DOOR SURROUND STRUCTURE FS349.00 SILL STRIKER BETWEEN IS DENTED STGR4L & STGR5L. (MARKED IN RED) (C-CHECK RO 11/26/2024) PERFORMED REPAIR OF PASSENGER DOOR SURROUND STRUCTURE FS349.00 SILL STRIKER BETWEEN STGR4L & STGR5L BY COMPLYING WITH ALL
- [SDR SWIA2024112701295](https://openairdocs.org/sdr/SWIA2024112701295.md): Stringer · corroded · Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > GALVANIC CORROSION ON STGR25R FS295.00 - 310.00 (MARKED IN RED) (C-CHECK RO 11/26/2024) REPLACE STRINGER AT 25R FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. LEAK CHECK GOOD. COMPLIED WITH TAS
- [SDR SWIA2024112701294](https://openairdocs.org/sdr/SWIA2024112701294.md): Stringer · corroded · Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > GALVANIC CORROSION THE FULL LENGTH ON STGR25R STRINGER SPLICE AT FS333.00. (MARKED IN RED) (C-CHECK RO 11/26/2024) REPLACED STRINGER SPLICE AT 25R. FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG: SH670-32420 REV E. LEAK CHECK GOOD. COMPLIED WITH TAS
- [SDR SWIA2024112701293](https://openairdocs.org/sdr/SWIA2024112701293.md): Stringer · corroded · Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > GALVANIC CORROSION ON STGR26R FS333.00 - 349.00. (MARKED IN RED) (C-CHECK RO 11/26/2024) REPLACED STRINGER AT 26R, FS333 - FS364 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31350 REV A. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202411271292](https://openairdocs.org/sdr/SWIA202411271292.md): Skin · gouged · Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LOWER EXTERNAL SKIN PANEL HAS 4 DEEP GOUGES FORWARD AND AFT OF FS977 (C-CHECK RO 11/26/2024) COMPLIED WITH ALL STEPS OF SOLUTION 2 OF REO 670-53-00-290 REV - F 2019/04/26. LEAK CHECK GOOD, COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202411571003](https://openairdocs.org/sdr/SWIA202411571003.md): Seat Track · corroded · Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SEAT RAIL BEAM AT LBL9 BETWEEN FS572.00 TO FS685.00 SEVERAL AREAS ARE CORROSION (MARKED) (C-CHECK RO 11/26/2024) REPAIRED CORROSION DAMAGE ON LH SEAT RAIL BEAM FLANGE AT LBL 9, BETWEEN F.S. 572 AND F.S. 685 TO REO 670-53-31-954 REV -- DATED 2024-10-
- [SDR SWAI2024112701291](https://openairdocs.org/sdr/SWAI2024112701291.md): Transcowl · cracked · Oct 1, 2024 · N706SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/26/2024) INSTALLED A NEW R/H LWR TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY
- [SDR SWIA202411271001](https://openairdocs.org/sdr/SWIA202411271001.md): Transcowl · cracked · Oct 1, 2024 · N706SK · Cndair CL6002C10 · Engine Thrust Reverser
  > R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/26/2024) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY C
- [SDR SWIA202411270926](https://openairdocs.org/sdr/SWIA202411270926.md): Floor Support · corroded · Sep 26, 2024 · N706SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > COCKPIT FLOORBOARD SUPPORT ANGLE IS CORRODED. FWD SIDE OF FS280 BEAM (C-CHECK RO 11/26/2024) REMOVED AND REPLACED COCKPIT FLOORBOARD SUPPORT ANGLE REF CRJ 700 SRM51-42-06-001-001-A01 REV 38 DATE JUL 25/2020, DWG NO. CC670-34010 REV -K AND DWG NO. CC670-
- [SDR SWIA2024112701302](https://openairdocs.org/sdr/SWIA2024112701302.md): Door · cracked · Sep 22, 2024 · N706SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > LH TRU DOOR (211AL) LANDING HAS A POSSIBLE CRACK BY AFT LATCH (C-CHECK RO 11/26/2024) REMOVED AND REPLACED LH TRU DOOR (211AL) LANDING REF REO NO. 670-53-11-2026 REV -- DATED 2024-10-04 AND DWG NO. CC670-33040 REV -G. COMPLIED WITH TASK CARD 51-900-100
- [SDR SWIA202411270922](https://openairdocs.org/sdr/SWIA202411270922.md): Door · cracked · Sep 22, 2024 · N706SK · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > RH TRU DOOR (212AR) LANDING HAS A POSSIBLE CRACK BY AFT LATCH (C-CHECK RO 11/26/2024) REMOVED CRACKED DOOR LANDING FROM STGR 16R BETWEEN FS172-FS193 AND INSTALLED A NEW ONE PER REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01, CRJ
- [SDR 2023FA0000253](https://openairdocs.org/sdr/2023FA0000253.md): Fire Bottle · abnormal · May 10, 2023 · N706SK · Cndair CL6002C10 · Fire Protection System
  > FIRE EXTINGUISHER WAS RECEIVED WITH FOD INSIDE OF THE CYLINDER. THE FOD WAS A BROWN RESIDUE AND GRANULAR SUBSTANCE LOCATED ON RESTRICTED FLOW ORIFICES AND ON THE CYLINDER WALLS. FOD WAS FOUND DURING THE SERVICE OF THE FIRE EXTINGUISHER. THE RECOMMENDED SERVICE
- [SDR SWIA2023011367111](https://openairdocs.org/sdr/SWIA2023011367111.md): Stringer · deformed · Nov 12, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 19L FOUND DEFORMED NEAR FRAME SPLICE AT BS 1015. REPAIRED THE STRINGER IAW REO 670-53-61-2096, REV.C.
- [SDR SWIA2023011367114](https://openairdocs.org/sdr/SWIA2023011367114.md): Frame · not reported · Sep 2, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > REMOVED FRAME SEGMENT FROM FS 1047 STR19L-27L. LOCATED DRILLED AND INSTALLED NEW LOWER FRAME SEGMENT PN MM670-36064-003 REF CRJ 700 SRM 51-40-11 AND 51-42-06. ORIG SUBMISSION DATE: 1/13/2023
- [SDR SWIA2023011367113](https://openairdocs.org/sdr/SWIA2023011367113.md): Support Bracket · deformed · Aug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SUPPORT BRACKET DEFORMED AT BS 1047, STGR 19 LEFT. REMOVED, FABRICATED, AND INSTALLED A NEW SUPPORT BRACKET IAW SRM 51-42-06-001-001, 51-24-21-001-001, 53-61-03 AND DWG MM670-36485. ORIG SUBMISSION DATE: 1/13/2023
- [SDR SWIA2023011367112](https://openairdocs.org/sdr/SWIA2023011367112.md): Frame Splice · deformed · Aug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SPLICE SUPPORT BRACKET DEFORMED AT BS 1015, STGR 19L. REMOVED CLEAT AND FABRICATED A NEW CLEAT. INSTALLED THE NEW CLEAT IAW SRM 51-42-06-001-001, 51-24-21-001-001, 53-61-03 AND DWG MM670-36483. ORIG SUBMISSION DATE: 1/13/2023
- [SDR SWIA2023011367110](https://openairdocs.org/sdr/SWIA2023011367110.md): Frame Splice · deformed · Aug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME SPLICE BS 1015, S19L DEFORMED. REMOVED FRAME SPLICE, AND FABRICATED A NEW FRAME SPLICE. INSTALLED IAW SRM 51-42-06-001-001, 51-24-21-001-001-A01, DWG MM670-36402, AND REO 670-53-61-2096 REV C. ORIG SUBMISSION DATE: 1/13/2023
- [SDR SWIA2023011367109](https://openairdocs.org/sdr/SWIA2023011367109.md): Frame · damaged · Aug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 1015.00 TORN AND DEFORMED AT THE INTERSECTION OF FRAME BS 1015, S18L. REMOVED DAMAGED FRAME. NEW FRAME SEGMENT PN MM670-36123-003 LOCATED, DRILLED, AND INSTALLED IAW SRM TASK 51-40-11-001-001, 51-42-06-001-001 AND REO 670-53-61-2096, REV C. ORIG SUBM
- [SDR SWIA202162060](https://openairdocs.org/sdr/SWIA202162060.md): None · cracked · Oct 2, 2021 · N706SK · Cndair CL6002C10 · Doors
  > PAX DOOR AFT FORMER IS CRACKED. (C-CHECK RO 10/29/2021) REMOVED AND REPLACED PAX DOOR FORMER AFTER FORMER PER CRJ 700 SRM 51-42-06-001-001-A01 AND PERFORMED PRESSURE LEAK CHECK TO PAX DOOR AFT FORMER PER CRJ 700 AMM 21-31-00-910-801-A01 NO LEAKS. COMPL
- [SDR SWIA202162062](https://openairdocs.org/sdr/SWIA202162062.md): None · wrinkled · Oct 1, 2021 · N706SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach Fittings
  > WITH AIRCRAFT POWER ON AN UNCOMMANDED FLAP DEPLOYMENT CAUSED WRINKLING OF THE RH OUTBOARD FLAP PANEL (C-CHECK RO 10/29/2021) REPLACED RH OUTBD FLAP PANEL WITH SERVICABLE PANEL REF CRJ-700 AMM 27-52-29-400-801-A02. OPS AND RIG CHECK GOOD SEE CONTINUATION
- [SDR SWIA202162059](https://openairdocs.org/sdr/SWIA202162059.md): None · damaged · Oct 1, 2021 · N706SK · Cndair CL6002C10 · Wing Structure
  > EVALUATE DAMAGE TO RH AILERON CAUSED BY UNCOMMANDED DEPLOYMENT OF RH OUTBOARD FLAP (C-CHECK RO 10/29/2021) BLENDED AILERON EDGE IAW CRJ 700 SRM 51-12-00-001-001-A01 FOUND OUT OF LIMITS INSTALLED NON FLUSH PATCH REPAIR IAW CRJ 700 SRM 57-61-01-201-001-A0
- [SDR SWIA202162058](https://openairdocs.org/sdr/SWIA202162058.md): None · corroded · Sep 23, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON INTERCOSTAL DD4 BETWEEN FS 311-327 ON FWD PAX DOOR (C-CHECK RO 10/29/2021) - INSTALLED NEW PAX DOOR INTERCOSTAL DD4 BETWEEN FS311 AND FS327 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH TASK CARD 51-900-100
- [SDR SWIA202162057](https://openairdocs.org/sdr/SWIA202162057.md): None · gouged · Sep 23, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Keel
  > STGR AT AFT CARGO DOOR THRESHOLD (ADJACENT TO COAMING) HAS GOUGES AND FRETTING IN MULTIPLE LOCATIONS. (C-CHECK RO 10/29/2021) BLENDED OUT FRETTING/GOUGING ON STGR 17L AT AFT CARGO DOOR THRESHOLD, REF CRJ 700 SRM 51-12-00-001-001-A01 / BLENDED WITHIN LI
- [SDR SWIA202162056](https://openairdocs.org/sdr/SWIA202162056.md): None · corroded · Sep 23, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON REINFORCEMENT ANGLE OF FRAME FS549 BETWEEN STGR18L/17L (C-CHECK RO 10/29/2021) REMOVED AND REPLACED ANGLE REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-33100 REV K / FS549 STGR18L-STGR17L, COMPLIED WITH SKY CARD 51-900-1002 SK
- [SDR SWIA202162055](https://openairdocs.org/sdr/SWIA202162055.md): None · cracked · Sep 16, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 320 ON PAX DOOR HAS A CRACK AT RIVET HOLE AND MULTIPLE SPOTS OF CORROSION (C-CHECK RO 10/29/2021) INSTALLED INTERCOSTAL DDA BETWEEN FS 311-320 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, AND REO 670
- [SDR SWIA202162054](https://openairdocs.org/sdr/SWIA202162054.md): None · elongated · Sep 15, 2021 · N706SK · Cndair CL6002C10 · Engine Exhaust System
  > RIGHT ENG. LOWER TRANSCOWL DOUBLER HAS AN ELONGATED HOLE. (C-CHECK RO 10/29/2021) INSTALLED NEW RH ENG. LOWER TRANSCOWL DOUBLER CRJ-700 SRM 51-42-13-001-001-A01, SRM 51-42-06-001-001-A01, REO 670-54-21-1207 REV A DATED 2015-08-27 / COMPLIED WITH SKY CAR
- [SDR SWIA202162053](https://openairdocs.org/sdr/SWIA202162053.md): None · corroded · Sep 15, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL DD6 HAS CORROSION ON IT ON FLANGE AND FWD ANGLE HAS A CRACK IN IT (C-CHECK RO 10/29/2021) INSTALLED NEW INTERCOSTAL REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06 AND 51-42-21-001-001-A01. / COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202162052](https://openairdocs.org/sdr/SWIA202162052.md): None · gouged · Sep 15, 2021 · N706SK · Cndair CL6002C10 · Engine Exhaust System
  > RIGHT ENG. LOWER TRANSCOWL LATCH COAMING WORN AND GAUGED (C-CHECK RO 10/29/2021) INSTALLED NEW RIGHT ENG. LOWER TRANSCOWL LATCH COAMING REF, CRJ-700 SRM 51-42-13-001-001-A01, SRM 51-42-06-001-001-A01, REO 670-54-21-1207 REV A DATED 2015-08-27 / COMPLIED
- [SDR SWIA202162051](https://openairdocs.org/sdr/SWIA202162051.md): None · corroded · Sep 13, 2021 · N706SK · Cndair CL6002C10 · Doors
  > FWD AND AFT CAP ANGLES CORRODED ON PAX DOOR MID CAP ANGLE FLOOR SILL/THRESHOLD AREA. (C-CHECK RO 10/29/2021) REPLACED FWD AND AFT CAP ANGLES CORRODED ON PAX DOOR MID CAP ANGLE FLOOR SILL/THRESHOLD AREAREF: CRJ-700 S.R.M.51-42-06-001-001-A01 DWG-SH670-3
- [SDR SWIA202162050](https://openairdocs.org/sdr/SWIA202162050.md): None · corroded · Sep 10, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CLIP( 601R318058-1) ON INTERCOSTAL DD7A IS CORRODED AFT SIDE (C-CHECK RO 10/29/2021) REMOVE AND REPLACED CLIP IN INTERCOSTAL DD7 AFT SIDE REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202162049](https://openairdocs.org/sdr/SWIA202162049.md): None · corroded · Sep 10, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FORMER FS320 (601R318038-3) HAS CORROSION OROUND SEVERAL FASTENERS THROUGH THE SKIN (C-CHECK RO 10/29/2021) INSTALLED NEW FORMER REF DWG 601R31702 REV N CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-9
- [SDR SWIA2021110262048](https://openairdocs.org/sdr/SWIA2021110262048.md): Support Angle · corroded · Sep 9, 2021 · N706SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORWARD SUPPORT ANGLE HAS CORROSION IN 2 PLACES AND A GOUGE IN LOWER END (C-CHECK RO 10/29/2021) INSTALLED NEW PAX DOOR FOWARD SUPPORT ANGLE REF CRJ700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-20-001-001-A01, AND DWG 601R31702 REV N / C
- [SDR SWIA202162047](https://openairdocs.org/sdr/SWIA202162047.md): None · worn · Sep 5, 2021 · N706SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > LEFT HAND WING ZONE 500 SLAT TRACK 1-1 SHOWS SIGNS OF WEAR ON LWR SIDE (MARKED WITH RED) (C-CHECK RO 10/29/2021) BLENDED WEAR ON LH WING SLAT TRACK 1-1 LOWER SIDE, MATERIAL LOSS FOUND TO BE WITHIN LIMITS REF MHIRJ REO 670-57-42-1190 REV--, DATED 2021-0
- [SDR SWIA202162046](https://openairdocs.org/sdr/SWIA202162046.md): None · cracked · Sep 3, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CRACK FOUND AT ANGLE ASSY LBL12 WL 72.10 BETWEEM FS280 AND FS265 (C-CHECK RO 10/29/2021) REMOVED AND REPLACED ANGLE ASSY (P/N CC670-33199-3) AT LBL 12 WL 72.10 BETWEEN F.S. 280 AND F.S. 265, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV -
- [SDR SWIA202162045](https://openairdocs.org/sdr/SWIA202162045.md): Intercostal · corroded · Sep 2, 2021 · N706SK · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION FOUND ONPAX DOOR INTERCOSTAL DD7A BETWEEN FS 323-335 INSTALLED NEW INTERCOSTAL DD7A BETWEEN FS 323-335 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.LEAK CHECK GOOD. / COMPLIED WITH SKYWEST FORM M-337 / COMPLIE
- [SDR SWIA202162044](https://openairdocs.org/sdr/SWIA202162044.md): None · corroded · Sep 2, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON INTERCOSTAL DD2 BETWEEN FS 311-327 (C-CHECK RO 10/29/2021) INSTALLED NEW INTERCOSTAL DD2 BETWEEN FS311-327 REF DWG 601R31702 REV N, CRJ700 SRM 51 -42-06-001-001-A01 AND 51-42-21-001-001-A01, DWG 601R31702 REV N. COMPLIED WITH TASK
- [SDR SWIA2021110262043](https://openairdocs.org/sdr/SWIA2021110262043.md): Intercostal · corroded · Sep 2, 2021 · N706SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON INTERCOSTAL DD1A BETWEEN FS 338 AND 320 (C-CHECK RO 10/29/2021) REMOVED AND REPLACED INTERCOSTAL DD1A BETWEEN FS 338 AND 320 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-40-11-001-001-A01, LEAK CHECK G
- [SDR SWIA202162042](https://openairdocs.org/sdr/SWIA202162042.md): None · corroded · Sep 2, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
  > EVIDENCE OF CORROSION FOUND ON CROSS BEAM AT FS1051.30 COMMON TO RBL27.00 UNDER R/H FLOOR SILL. (C-CHECK RO 10/29/2021) COMPLIED WITH BEAM REPAIR PER REO 670-53-61-1955 REV-- DATED 2021-10-14. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD

Next page: https://openairdocs.org/aircraft/N706SK/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 = 'N706SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N706SK/reports

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