# Service difficulty reports: N782SK

A list on [N782SK](https://openairdocs.org/aircraft/N782SK.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 · 112 reports

- [SDR SWIA2026072376942](https://openairdocs.org/sdr/SWIA2026072376942.md): Skin · demodification · Jul 23, 2026 · N782SK · Cndair CL6002C11 · Standard Practices/Structures
  > 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) (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR IN
- [SDR SWIA2026072376941](https://openairdocs.org/sdr/SWIA2026072376941.md): Skin · demodification · Jul 23, 2026 · N782SK · Cndair CL6002C11 · Standard Practices/Structures
  > 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 (DETERMINED TO BE A MAJOR REPAIR) (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR I
- [SDR SWIA2026072376940](https://openairdocs.org/sdr/SWIA2026072376940.md): Skin · demodification · Jul 23, 2026 · N782SK · Cndair CL6002C11 · Standard Practices/Structures
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH 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 (DETERMINED TO BE A MAJOR REPAIR) (FILED CLOSED)PERFORMED PERMANENT DOUBLER REP
- [SDR SWIA2026072376939](https://openairdocs.org/sdr/SWIA2026072376939.md): Skin · demodification · Jul 23, 2026 · N782SK · Cndair CL6002C11 · Standard Practices/Structures
  > 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) (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPA
- [SDR SWIA2026072376938](https://openairdocs.org/sdr/SWIA2026072376938.md): Skin · demodification · Jul 23, 2026 · N782SK · Cndair CL6002C11 · Standard Practices/Structures
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847, STR 1L - STR 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATE
- [SDR SWIA2026070476442](https://openairdocs.org/sdr/SWIA2026070476442.md): Window · cracked · Jul 4, 2026 · N782SK · Cndair CL6002C10 · Flight Compartment Windows
  > VISIBLE CRACK IN RIGHT COCKPIT WINDOW. (FLIGHT 5791) COMPLIED WITH TASK CARD 56-220-1000-SKY REMOVAL AND INSTALLATION OF SERVICEABLE RT WINDOW.
- [SDR SWIA202411261028](https://openairdocs.org/sdr/SWIA202411261028.md): Attach Angle · cracked · Oct 28, 2024 · N782SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FOUND CRACK ON LOWER SIDE OF LEFT FWD UPLOCK ATTACHMENT ANGLE. (FILED CLOSED) REMOVED AND REPALCED ATTACHEMENT ANGLE PN SH670-36394-1 POI # 5000015864 PER CRJ 700 SRM 51-42-21-001-001-A01 REV 38B DATED 14DEC2020AND DWG SH670-36290 REV U COMPLIED WITH TASK
- [SDR SWIA2023052211](https://openairdocs.org/sdr/SWIA2023052211.md): Skin · damaged · May 1, 2023 · N782SK · Cndair CL6002C10 · Wing, Plate/Skin
  > WHILE DRILLING OUT A STUCK SCREW ON PANEL 672AB MISDRILLED AND DAMAGED UNDERLYING STRUCTURE. (C-CHECK RO 5/18/2023) REPAIRED DAMAGE TO RH WINGLET CLOSING RIB REF MHIRJ EO # CL-600-2C10-57-L07462 DATED 5/2/2023. COMPLIED WITH SKYWEST TASK CARD 51-900-100
- [SDR SWIA2023052215](https://openairdocs.org/sdr/SWIA2023052215.md): Seat Track · corroded · Apr 25, 2023 · N782SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH FITTING ASSY SEAT TRACK AT RBL9.0 BETWEEN FS939.00 AND FS953.00 HAS CORROSION (C-CHECK RO 5/18/2023) INSTALLED FITTING ASSY SEAT TRACK AT RBL9.0 BETWEEN FS939.00 AND FS953.00 REF CRJ-700 SRM 51-41-02-001-001-A01.
- [SDR SWIA2023052210](https://openairdocs.org/sdr/SWIA2023052210.md): Intercostal · corroded · Apr 24, 2023 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD4 FS311.75 - FS320.00 IS CORRODED (C-CHECK RO 5/18/2023) INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS311.75 - FS320.00 PER CRJ 700 SRM 51-42-06-001-001-A01 AND INSTALLATION DRAWING DWG 601R31702 REV -N. LEAK CHECKED GOOD. COMPLIED WI
- [SDR SWIA202305229](https://openairdocs.org/sdr/SWIA202305229.md): Cleat · corroded · Apr 24, 2023 · N782SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > PAX DOOR CLEAT @ FS320.00 THAT ATTACHES TO INTERCOSTAL DD6 FS311.75 - FS320.00 IS CORRODED (C-CHECK RO 5/18/2023) REMOVED AND REPLACED PAX DOOR CLEAT @ FS320.00 THAT ATTACHES TO INTERCOSTAL DD6 FS311.75 - FS320.00. REF: CRJ-700 SRM 51-42-06-001-001-A
- [SDR SWIA202305228](https://openairdocs.org/sdr/SWIA202305228.md): Intercostal · corroded · Apr 24, 2023 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR INTERCOSTAL DD6 FS311.75 - FS320.00 AND BRACKET ARE CORRODED (C-CHECK RO 5/18/2023) INSTALLED NEW INTERCOSTAL DD6 FS311.75 - FS320.00 AND BRACKET. REF: CRJ-700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N. LEAK CHECKED GOOD. COMPLIED WI
- [SDR SWIA2023052214](https://openairdocs.org/sdr/SWIA2023052214.md): Seat Track · corroded · Apr 21, 2023 · N782SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SEAT TRACK AT LBL27 BETWEEN FS364.00 TO FS453.00 SEVERAL AREAS HAS CORROSION (MARKED) (C-CHECK RO 5/18/2023) REMOVED CORROSION ON LH SEAT TRACK AT LBL27.00 BETWEEN FS364.00 TO FS453.00 PER CRJ-700 SRM 51-21-06-001-001-A01. INSTALLED NEW LH SEAT TRA
- [SDR SWIA202305227](https://openairdocs.org/sdr/SWIA202305227.md): Pad · worn · Apr 20, 2023 · N782SK · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > UPON REMOVAL OF R/H LWR TRANSCOWL AFT LATCH BEARING PAD ON JOB 71027881 OP 144 CAMP #26469813, FOUND WEAR DAMAGE ON UNDERLYING CHANNEL. (C-CHECK RO 5/18/2023) REPAIRED DAMAGE TO R.H LOWER TRANS COWL AFT C CHANNEL REF MHIRJ REO 670-54-21-1550 REV --
- [SDR SWIA202305226](https://openairdocs.org/sdr/SWIA202305226.md): Former · corroded · Apr 20, 2023 · N782SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FWD FORMER FS311.75 IS CORRODED (C-CHECK RO 5/18/2023) INSTALLED NEW FORMER FS311.75. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N. LEAK CHECKED GOOD. COMPLIED WITH TASK CARD 51-900-1002-S
- [SDR SWIA202305225](https://openairdocs.org/sdr/SWIA202305225.md): Post · cracked · Apr 19, 2023 · N782SK · Cndair CL6002C10 · Fuselage Structure (General)
  > CO-PILOT SIDE POST UPPER BARREL POSSIBLE CRACK. FLAGGED (C-CHECK RO 5/18/2023) REPLACED CO-PILOT WINDOW SIDE POST REF CRJ-700 SRM 51-42-21-001-001-A01 AND DWG: 601R33007 REV U. ALL CHECKS GOOD. COMPLIED WITH TASK CARDS 51-900-1002-SKY & 56-220-1000-SKY
- [SDR SWIA202305224](https://openairdocs.org/sdr/SWIA202305224.md): Hinge · gouged · Apr 18, 2023 · N782SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (FUSELAGE SIDE) HAS CHAFFING ON LANDS #14 - #26 AND GOUGED ON LAND #27 (C-CHECK RO 5/18/2023) BLENDED CHAFFING ON PAX DOOR HINGE (FUSELAGE SIDE) LANDS #14 - #26 AND GOUGED ON LAND #27. MATERIAL LOSS OF 0.065" MEASURED WITH CALIPER TUC939
- [SDR SWIA202305223](https://openairdocs.org/sdr/SWIA202305223.md): Support · cracked · Apr 18, 2023 · N782SK · Cndair CL6002C10 · Wing Structure
  > *LH WING UNDER FUEL PANEL 551AB, SLAT TRACK 1-3 CANISTER SUPPORT STRAP CRACKED (MARKED) OUT OF SCOPE (C-CHECK RO 5/18/2023) REPAIRED CRACKED 1-3 SLAT CANISTER SUPPORT STRAP PER REO 670-57-42-577 REV -- DATED 2016-12-02 AND MHIRJ REO 670-57-42-1410 REV -
- [SDR SWIA202305222](https://openairdocs.org/sdr/SWIA202305222.md): Bracket · cracked · Apr 17, 2023 · N782SK · Cndair CL6002C10 · Nacelle/Pylon Structure
  > L/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 5/18/2023) REMOVED AND REPLACED INBD STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF. REO 670-54-21-971 REV. A, 2017/05/11 AND BOMBARDIER DWG CN624-2005 REV. T. COMPLIED WITH SKYCARD 51
- [SDR SWIA202305221](https://openairdocs.org/sdr/SWIA202305221.md): Bracket · cracked · Apr 17, 2023 · N782SK · Cndair CL6002C10 · Nacelle/Pylon Structure
  > R/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 5/18/2023) R/H UPPER TRANSCOWL INBD CRACKED A" BRACKET HAS BEEN REMOVED AND REPLACED BY COMPLYING FULLY W/REO# 670-54-21-971, REV A, DATED 5/11/17 AS WELL AS SKYCARD 51-900-1002-SKY.
- [SDR SWIA2023052213](https://openairdocs.org/sdr/SWIA2023052213.md): Seat Track · corroded · Apr 16, 2023 · N782SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAIL AT RBL9 FROM FS485 TO FS581. (C-CHECK RO 5/18/2023) CORROSION FOUND ON FLOOR SEAT RAIL AT RBL 9 BETWEEN FS485 TO FS581 IS OUT OF LIMITS DUE TO MORE THAN ONE TYPE OF DAMAGE AT SEVERAL CROSS-SECTIONS.INSTALLED NEW RH SEAT TRAC
- [SDR SWIA2023052206](https://openairdocs.org/sdr/SWIA2023052206.md): Door Sill · cracked · Apr 16, 2023 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD EQUIPMENT COMPARTMENT - R/S DOOR SILL CRACKED @ AFT LATCH RECEPTICLE (C-CHECK RO 5/18/2023) REPAIRED FWD EQUIPMENT COMPARTMENT - R/S DOOR SILL REF CRJ-700 SRM 51-42-06-001-001-A01 REV 38 JUL 25 2020, REO 670-53-11-1845 REV -- 2023-04-21, DWG: CC670
- [SDR SWIA2023052212](https://openairdocs.org/sdr/SWIA2023052212.md): Panel · chafed · Apr 9, 2023 · N782SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH WING FLAP PANEL 584HT CHAFE (C-CHECK RO 5/18/2023) REMOVED AND REPLACED LH WING FLAP PNL 584HT REF-CRJ-700 SRM 51-40-11-001-001 A01 AND PANEL INSTALLED ON CAMP # 26307786 M-212 FORM, JOB 0 OP 7005
- [SDR SWIA202154933](https://openairdocs.org/sdr/SWIA202154933.md): Windshield · cracked · Jan 4, 2021 · N782SK · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT WINDSHIELD SHATTERED IN CRUISE FLIGHT, DIVERTED TO FSD. FOUND WINDOW CRACKED DUE TO ELECTRICAL ARCING. REMOVED AND REPLACED RIGHT WINDSHIELD, REF AMM.
- [SDR SWIA2020021848745](https://openairdocs.org/sdr/SWIA2020021848745.md): Spring · inoperative · Feb 13, 2020 · N782SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD CARGO DOOR FWD LATCH LEVER SPRING INOP. (C-CHECK) RO:2/14/2020REPLACED SPRING ON FWD CARGO DOOR FWD LATCH ASSY PER LATECOERE CMM.
- [SDR SWIA2020021848720](https://openairdocs.org/sdr/SWIA2020021848720.md): Floorbeam · corroded · Feb 6, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > OUTBOARD ANGLE P/N: CC670-34269-4 AT RBL 9 AT FS 280.00 CORRODED THROUGH. (C-CHECK) RO:2/14/2020REPLACED NEW ANGLE P/N: CC670-34269-4 AT RBL 9 AT FS 280.00 REF CRJ-700 SRM
- [SDR SWIA2020021848719](https://openairdocs.org/sdr/SWIA2020021848719.md): Support Bracket · corroded · Jan 26, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DUCT SUPPORT BRACKET COMMON TO CROSS BEAM AT FS1000.00 LBL29 & FRAME 1000.00 BETWEEN STRG21L AND STRG 22L IS CORRODED. (C-CHECK) RO:2/14/2020REPLACED DUCT SUPPORT BRACKET COMMON TO CROSS BEAM AT FS 1000.00 LBL 29 BETWEEN STRG 21L AND 22L AS PER CRJ 700
- [SDR SWIA2020021848682](https://openairdocs.org/sdr/SWIA2020021848682.md): Floorbeam · cracked · Jan 22, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL12 CRACKED @ 280 (C-CHECK) RO:2/14/2020NEW L/H CENTER COCKPIT FLOOR BEAM SEGMENT AND REPAIR PARTS AT 280 LBL 12.0 INSTALLED REF CRJ 700 SRM / COMPLIED WITH SKY CARD (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337
- [SDR SWIA2020021848681](https://openairdocs.org/sdr/SWIA2020021848681.md): Floorbeam · cracked · Jan 22, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 12 CRACKED @ 280 (C-CHECK) RO:2/14/2020REPLACED CENTER COCKPIT FLOOR BEAM AT RBL 12 F.S. 280 TO FOM REF. CRJ 700 SRM TASK / COMPLIED WITH SKY CARD STRUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337
- [SDR SWIA2020021848679](https://openairdocs.org/sdr/SWIA2020021848679.md): Intercostal · cracked · Jan 17, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CRACKED FS 280 LBL 39 (C-CHECK) RO:2/14/2020REMOVED AND REPLACED INTERCOSTAL FS 280 LBL 39 REF CRJ 700 SRM AND COMPLIED WITH SKYCARD CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) AND COMPLIED WITH M-337
- [SDR SWIA2020021848728](https://openairdocs.org/sdr/SWIA2020021848728.md): Attach Angle · cracked · Jan 16, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > ATTACH ANGLE CRACKED FS 280 LBL12 COMMON TO CROSS BEAM AND INTERCOSTAL (C-CHECK) RO:2/14/2020REMOVED AND REPLACED ANGLE, REF CRJ700 SRM AND CRJ700 SRM RESTORED FINISH, REF. CRJ700 SRM AND REAPPLIED CIC, REF. CRJ700 SRM
- [SDR SWIA2020021848717](https://openairdocs.org/sdr/SWIA2020021848717.md): Angle · corroded · Jan 16, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ARROUND FASTENER HOLES ON MID CAP ANGLE P.N. SH670-31825-7 AT PAX DOOR ENTRANCE SURROUND STRUCTURE. (C-CHECK) RO:2/14/2020BLENDED CORROSION PER CRJ 700 SRM. ORIGINAL MATERIAL THICKNESS.060€?, MATERIAL REMOVED.036€? MATERIAL REMAIN
- [SDR SWIA2020021848716](https://openairdocs.org/sdr/SWIA2020021848716.md): Angle · corroded · Jan 16, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ARROUND FASTENER HOLES ON FORWARD CAP ANGLE P.N.SH670-31821-3 AT BOTTOM OF PAX DOOR ENTRANCE SURROUND STRUCTURE. (C-CHECK) RO:2/14/2020REPLACED FWD CAP ANGLE P.N SH670-31-821-3 AT BOTTOM OF PAX DOOR ENTRANCE SURROUND REF CRJ 700 SRM
- [SDR SWIA2020021848677](https://openairdocs.org/sdr/SWIA2020021848677.md): Floorbeam · corroded · Jan 16, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON LONG BEAM FS 295 LBL9 (C-CHECK) RO:2/14/2020INSTALLED NEW LONG BEAM AT F.S. 295.00 LBL9 REF BOMBARDIER REO / COMPLIED WITH SKY CARD CL600-2C10) STUCTURAL MAJOR REPAIR (**RII**) / COMPLIED WITH FORM M-337
- [SDR SWIA2020021848676](https://openairdocs.org/sdr/SWIA2020021848676.md): Bulkhead · corroded · Jan 16, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > CORROSION ON LH 280 BULKHEAD LOWER WEB LBL 12 (C-CHECK) RO:2/14/2020CORROSION DETERMINED TO BE OUT OF LIMITS, REMOVED AND REPLACED LH 280 BULKHEAD, LOWER WEB, REF CRJ700 SRM AND REO SEE CONTINUATION FOR DETAIL. WEIGHT UNCHANGED AS PART AND FASTENERS WE
- [SDR SWIA2020021848743](https://openairdocs.org/sdr/SWIA2020021848743.md): Panel · bent · Jan 15, 2020 · N782SK · Cndair CL6002C10 · Wing Main, Frame Structure
  > PANEL 684GT IS BENT. (C-CHECK) RO:2/14/2020BEND IN PANEL 684GT OUT OF LIMITS. ORDERED AND RECEIVED NEW PANEL. REF CRJ 700 SRM.
- [SDR SWIA2020021848714](https://openairdocs.org/sdr/SWIA2020021848714.md): Floor Support · corroded · Jan 15, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR FLOOR SILL HAS EVIDENCE OF CORROSIO ON THE I/B FACE OF THE FWD CUP RECESS ATTACH POINT. (C-CHECK) RO:2/14/2020REMOVED CORROSION FROM PAX DOOR FLOOR SILL I/B FACE OF THE CUP RECCESS ATTACH POINT. ORIGINAL MATERIAL THICKNESS.063€?, MATERIAL
- [SDR SWIA2020021848675](https://openairdocs.org/sdr/SWIA2020021848675.md): Floorbeam · corroded · Jan 11, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON LH 280 BEAM (C-CHECK) RO:2/14/2020 REMOVED AND REPLACED LH 280 BEAM REF CRJ 700 SRM AND DWG REV NC DATED 2009-11-26. COMPLIED WITH SKYCARD (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) AND M-337
- [SDR SWIA2020021848727](https://openairdocs.org/sdr/SWIA2020021848727.md): Attach Angle · cracked · Jan 10, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > ATTACH ANGLE CRACKED FS 280 RBL12 COMMON TO CROSS BEAM AND INTERCOSTAL (C-CHECK) RO:2/14/2020REPLACED NEW ANGLE AT FS 280.00 AT RBL 12 REF CRJ-700 SRM.
- [SDR SWIA2020021848725](https://openairdocs.org/sdr/SWIA2020021848725.md): Vertical Support · cracked · Jan 10, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > VERTICLE ANGLE CRACKED AT LOWER TWO HOLES COMMON TO FS 280 BULKHEAD LOWER WEB RBL18 (C-CHECK) RO:2/14/2020REMOVED AND REPLACED ANGLE FS 280 RBL 18 REF CRJ 700 SRM.
- [SDR SWIA2020021848673](https://openairdocs.org/sdr/SWIA2020021848673.md): Floorbeam · corroded · Jan 10, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON LONG BEAM UPPER FLANGE FS 295 RBL 9 (C-CHECK) RO:2/14/2020 INSTALLED (1EA) NEW RBL 9.0 FLOOR BEAM AND ALL SPLICE REPAIR PARTS (1EA)(-7) LOWER FLANGE,(1EA)(-11) CLEAT,(2EA)(-13) SPLICE ANGLE, AND (2EA)(-15)UPPER ANGLE ON RBL 9.0 BETWEEN FS
- [SDR SWIA2020021848738](https://openairdocs.org/sdr/SWIA2020021848738.md): Intercostal · dented · Jan 9, 2020 · N782SK · Cndair CL6002C10 · Trailing Edge Flaps
  > WHILE PERFORMING DENT REPAIR OF LH INBD FLAP, MIDDLE SPAR INTERCOSTAL P/N CC670-14120-1 FOUND TO HAVE DENT DAMAGE. (C-CHECK) RO:2/14/2020REMOVED AND REPLACED WITH NEW PART REF CRJ 700 SRM.
- [SDR SWIA2020021848672](https://openairdocs.org/sdr/SWIA2020021848672.md): Floorbeam · corroded · Jan 9, 2020 · N782SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH 280 BEAM CORRODED (C-CHECK) RO:2/14/2020REMOVED AND REPLACED RH 280 BEAM REF CRJ 700 SRM AND DWG COMPLIED WITH SKYCARD (CL600-2C10) STRUCTURAL MAJOR REPAIR (**RII**) AND M-337
- [SDR SWIA2020021848739](https://openairdocs.org/sdr/SWIA2020021848739.md): Roller · bent · Jan 8, 2020 · N782SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > * AFT BAG DOOR SURROUND STRUCTURE, HAS "BENT" (LWR/AFT) DOOR TRACK GUIDE "PLATE" (FLAGGED). (C-CHECK) RO:2/14/2020REMOVED & REPLACED ROLLER GUIDE PLATE P/N-CC670-38810-2SB REF: CRJ-700 SRM.
- [SDR SWIA2020021848712](https://openairdocs.org/sdr/SWIA2020021848712.md): Door Sill · corroded · Jan 8, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL HAS CORROSION (C-CHECK) RO:2/14/2020REMOVED & REPLACED SERVICE DOOR SILL REF CRJ 700 SRM & DWG.
- [SDR SWIA2020021848711](https://openairdocs.org/sdr/SWIA2020021848711.md): Floor Support · corroded · Jan 8, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FLOOR SUPPORT HAS CORROSION (C-CHECK) RO:2/14/2020REMOVED AND REPLACED SERVICE DOOR FLOOR SUPPORT IAW CRJ700 SRM.
- [SDR SWIA2020021848709](https://openairdocs.org/sdr/SWIA2020021848709.md): Floor Support · corroded · Jan 8, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * CORROSION DETECTED ON R/H FLOOR "SILL" AT F.S. 1088.00, ON FWD SIDE OF FLT CONTROL PULLEY CAGE COVER (MARKED). (C-CHECK) RO:2/14/2020BLENDED DETECTED CORROSION ON R/H FLOOR SILL AT F.S. 1088.00 ON FWD SIDE OF FLT CONTROL PULLEY CAGE COVER REF CRJ SRM
- [SDR SWIA2020021848708](https://openairdocs.org/sdr/SWIA2020021848708.md): Striker · corroded · Jan 8, 2020 · N782SK · Cndair CL6002C10 · Service Doors
  > SERVICE DOOR LOWER SEAL STRIKER AIRCRAFT SIDE HAS CORROSION AROUND SEVERAL SCREW HOLES. (C-CHECK) RO:2/14/2020REPLACED SERVICE DOOR LOWER SEAL STRIKER AS PER CRJ 700 SRM.
- [SDR SWIA2020021848706](https://openairdocs.org/sdr/SWIA2020021848706.md): Floor Support · corroded · Jan 8, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * CORROSION DETECTED ON RH FLOOR "SILL" AFT BAG BAY, BETWEEN F.S. 1000.00 AND F.S. 1088.00 AROUND FLOOR BOARD NUT PLATE HOLES (MARKED). (C-CHECK) RO:2/14/2020REPAIRED RH FLOOR SILL AT FS 1000.00 AND 1088.00 AS PER REO.
- [SDR SWIA2020021848704](https://openairdocs.org/sdr/SWIA2020021848704.md): Floor Support · corroded · Jan 8, 2020 · N782SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > * CORROSION DETECTED ON L/H FLOOR "SILL" AFT BAG BAY, BETWEEN F.S. 985.00 AND F.S. 1000.00 AROUND FLOOR BOARD NUT PLATE HOLES (MARKED). (C-CHECK) RO:2/14/2020COMPLIED WITH BOMBARDIER REO.

Next page: https://openairdocs.org/aircraft/N782SK/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 = 'N782SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N782SK/reports

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