# Service difficulty reports: N796SK

A list on [N796SK](https://openairdocs.org/aircraft/N796SK.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 · 103 reports

- [SDR SWIA2026071076872](https://openairdocs.org/sdr/SWIA2026071076872.md): Floorbeam · corroded · Jul 10, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > UPON REMOVAL LH CROSSBEAM FOUND SIGNS OF CORROSION ON LH SIDE FLOOR BEAM AT FS295 LBL9. PERFORMED REPAIR LH CROSSBEAM AT FS295 IAW REO 670-53-21-2941 REV.--(P2), SRM 53-00-00, AMM 20-70-00 AND REO 670-53-21-2941 REV.--(P1). REO 670-53-21-2941 REV--.
- [SDR SWIA2026052876871](https://openairdocs.org/sdr/SWIA2026052876871.md): Striker · gouged · May 28, 2026 · N796SK · Cndair CL6002C11 · Passenger/Crew Doors
  > PAX DOOR FS310 FWD DOOR SEAL STREAKER GOUGE BETWEEN STR7-8. PERFORMED REPAIR OF FWD DOOR SEAL STREAKER FS.310 BETWEEN STGR7-8 OF PAX DOOR IAW CRJ700 550 SERIES SRM 53-21-23, 51-21-11, 51-25-06, 51-42-06, 51-25-16N
- [SDR SWIA2026052376874](https://openairdocs.org/sdr/SWIA2026052376874.md): Skin · eroded · May 23, 2026 · N796SK · Cndair CL6002C11 · Engine Air Intake System
  > RH ENG INLET LEADING EDGE ERODED. REMOVED AND REPLACED NOSE COWL LIPSKIN AT RT ENG INLET LEADING EDGE IAW SRM 54-11-05, AMM 71-61-01, SRM 51-42-06, REO 670-54-11-1456 REV -, REO 670-54-11-1456 REV -A AND SRM 51-21-11.
- [SDR SWIA2026052276878](https://openairdocs.org/sdr/SWIA2026052276878.md): Bulkhead Web · corroded · May 22, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Bulkhead
  > R/H FS280 BULKHEAD WEB AT FLOOR HAS SIGNS OF CORROSION. REMOVED AND REPLACED RH BUTTSTRAP AND RH LOWER WEB ON RH FS 280 BULKHEAD WEB IAW SRM 51-25-16, 51-42-06, 51-42-13, 53-00-00, AMM 20-70-00, REO 670-53-11-594, REV -A,
- [SDR SWIA2026052276870](https://openairdocs.org/sdr/SWIA2026052276870.md): Bulkhead Web · corroded · May 22, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Bulkhead
  > L/H FS 280 BULKHEAD WEB AT FLOOR HAS SIGNS OF CORROSION (C-CHECK RO 08/17/2026)PERFORMED REPAIR LH LOWER WEB FS280. FOUND TO BE WITHIN LIMITS IAW BOMBARDIER REO 670-53-11-594 REV -A, DATED 2015-06-26, CRJ 550 AMM 20-70-00, SRM 51-42-06, 51-42-13, 53-00-00.
- [SDR SWIA2026052076875](https://openairdocs.org/sdr/SWIA2026052076875.md): Floor Panel · gouged · May 20, 2026 · N796SK · Cndair CL6002C11 · Fuselage Floor Panel
  > ON FWD EQUIPMENT BAY FLOOR JUST AFT OF ACCESS DOOR 211AL THERE IS A GOUGE (C-CHECK RO 08/17/2026)PERFORMED REPAIR ON FWD EQUIPMENT BAY FLOOR JUST AFT OF ACCESS DOOR 211AL, IAW CRJ-550, SRM 51-42-06, BOMBARDIER REO 670-53-11-509, REV -E, DATE: 2018-02-08 AND
- [SDR SWIA2026051876877](https://openairdocs.org/sdr/SWIA2026051876877.md): Drag Angle · cracked · May 18, 2026 · N796SK · Cndair CL6002C11 · Fuselage, Stabilizer Attach Fittings
  > VERT STAB LH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AT VERT STAB LH AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018, REV -A, DATE: 2016-11-10.
- [SDR SWIA2026051876876](https://openairdocs.org/sdr/SWIA2026051876876.md): Drag Angle · cracked · May 18, 2026 · N796SK · Cndair CL6002C11 · Fuselage, Stabilizer Attach Fittings
  > VERT STAB RH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AFT DRAG ANGLE AT RH VERT STAB IAW BOMBARDIER REO 670-55-31-018 DATE: 2016-11-10, CRJ550 SRM 51-26-01, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S072326-2 DATE INS
- [SDR SWIA2026051376873](https://openairdocs.org/sdr/SWIA2026051376873.md): Skin · dented · May 13, 2026 · N796SK · Cndair CL6002C11 · Passenger/Crew Doors
  > ADM N796SK-9240 MCD TWO DENTS ON OUTER SKIN 24.5" FROM TOP, 11" FROM FRONT LEADING EDGE. 1ST DENT IS 11.5" FROM LEADING EDGE OF DOOR.750" TALL,.187" WIDE,.025" DEEP. 2ND DENT IS 11.0" FROM LEADING EDGE OF DOOR 1.250" TALL,.375" WIDE,.115" DEEP. SRM 52-11
- [SDR SWIA2026020675218](https://openairdocs.org/sdr/SWIA2026020675218.md): Skin · demodification · Feb 6, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - FS 409 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEE
- [SDR SWIA2026020675214](https://openairdocs.org/sdr/SWIA2026020675214.md): Skin · reversed · Feb 6, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581 - 597, S24R - 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 581 - 597, S24R - 25R I
- [SDR SWIA2026020675219](https://openairdocs.org/sdr/SWIA2026020675219.md): Skin · demodification · Feb 6, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - FS 409 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 BETWEE
- [SDR SWIA2026020975218](https://openairdocs.org/sdr/SWIA2026020975218.md): Skin · demodification · Feb 6, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394 - FS 409 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM.
- [SDR SWIA2026020675217](https://openairdocs.org/sdr/SWIA2026020675217.md): Skin · demodification · Feb 6, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. REPAIRED IAW DWG 601-2365-02-343, REV IR, AND STRUCTUAL MAJOR REPAIR CARD 51-900-1002
- [SDR SWIA2026020675216](https://openairdocs.org/sdr/SWIA2026020675216.md): Skin · demodification · Feb 6, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000 - FS 1015 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. REPAIRED IAW DWG 601-2365-02-343, REV IR AND STRUCTUAL MAJOR REPAIR CARD 51-900-1002-SKY.
- [SDR SWIA2026020975214](https://openairdocs.org/sdr/SWIA2026020975214.md): Skin · demodification · Feb 6, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581 - FS 597 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM. OPEN
- [SDR SWIA2026020376869](https://openairdocs.org/sdr/SWIA2026020376869.md): Skin · dented · Feb 3, 2026 · N796SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA94171-670-53-11-2025 MXCODEID104885-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 94171TEMP REPAIR FOR DENT DAMAGE TO CANOPY SKIN PANEL BETWEEN FS247.30-FS254.68 STR1R-STR2R (ON RH SIDE) IS VALID FOR 2700 FH FROM THE TIM
- [SDR SWIA202163654](https://openairdocs.org/sdr/SWIA202163654.md): None · broken · Dec 3, 2021 · N796SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > LH ACM WATER INJECTOR LINE HAS TWO BROKEN SUPPORT BRACKETS BETWEEN FS 1144.00 AND FS 1162.00. (C CHECK RO 01-05-2022) COMPLETED A MAJOR REPAIR TO LH ACM WATER INJECTOR LINE SUPPORTS AND INTERCOSTAL IAW REO 670-53-61-2021 REV--, DATED 12/10/2021 AND MAJOR R
- [SDR SWIA202163691](https://openairdocs.org/sdr/SWIA202163691.md): None · shifted · Nov 30, 2021 · N796SK · Cndair CL600* · Engine Exhaust System
  > DURING INSTALL OF THE R/H UPPER TRANSCOWL, FOUND OUTBOARD SLIDER TRACK INSERT TO HAVE SHIFTED FORWARD. (C CHECK RO 01-05-2022) REMOVED AND REPLACED R/H UPER TRANSCOWL OUTBOARD TRACK INSERT IAW CRJ 700 78-33-05-960-801-A02
- [SDR SWIA202163697](https://openairdocs.org/sdr/SWIA202163697.md): None · cracked · Nov 16, 2021 · N796SK · Cndair CL600* · Fuselage, Door Hinge
  > PAX DOOR FWD WEB IS CRACKED IN MULTIPLE LOCATIONS (C CHECK RO 01-05-2022) REMOVED DAMAGED FWD WEB AND INSTALLED A NEW WEB IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01
- [SDR SWIA202163653](https://openairdocs.org/sdr/SWIA202163653.md): None · cracked · Nov 16, 2021 · N796SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL AT DD1 IS CRACKED (C CHECK RO 01-05-2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD1 IAW CRJ 700 SRM 51-42-06-001-001-A01. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM 337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE C
- [SDR SWIA202163690](https://openairdocs.org/sdr/SWIA202163690.md): None · corroded · Nov 1, 2021 · N796SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > PAX DOOR INTERCOSTAL CORRODED BETWEEN FS320.163 AND FS338.63 AT DD6. (C CHECK RO 01-05-2022) REMOVED AND REPLACED CLIP ATTACHED TO INTERCOSTAL DD6 IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202163689](https://openairdocs.org/sdr/SWIA202163689.md): None · missing · Nov 1, 2021 · N796SK · Cndair CL600* · Ailerons
  > RH AILERON CAT TRACKS MISSING ON WING SIDE ABOVE AILERON PULLY AT APPROX WS314.50 (C CHECK RO 01-05-2022) REPLACED CAT TRACK ON RH WING AT WS 314.50 IAW CR 700 SRM 51-22-00-001-001-A01
- [SDR SWIA202163688](https://openairdocs.org/sdr/SWIA202163688.md): None · worn · Oct 26, 2021 · N796SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > ON THE RH WING, SLAT TRACK 3-2 AT THE I/B AFT POSITION, THE SIDE SUPPORT ROLLER IS WORN AND REQUIRES REPLACEMENT. (C CHECK RO 01-05-2022) REMOVED AND REPLACED RH WING SLAT TRACK 3-2 SIDE SUPPORT ROLLER AT THE I/B AFT POSITION IAW CRJ 700 AMM 27-81-44-400-8
- [SDR SWIA202163687](https://openairdocs.org/sdr/SWIA202163687.md): None · worn · Oct 26, 2021 · N796SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > ON THE RH WING, SLAT TRACK 2-2 AT THE O/B AFT AND THE I/B AFT POSITIONS, THE SIDE SUPPORT ROLLERS ARE WORN AND REQUIRE REPLACEMENT. (C CHECK RO 01-05-2022) REMOVED AND REPLACED RH WING SLAT TRACK 2-2 SIDE SUPPORT ROLLERS AT THE O/B AFT AND I/B AFT POSITION
- [SDR SWIA202163686](https://openairdocs.org/sdr/SWIA202163686.md): None · worn · Oct 26, 2021 · N796SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > ON THE RH WING, SLAT TRACK 1-2 AT THE O/B AFT POSITION, THE SIDE SUPPORT ROLLER IS WORN AND REQUIRES REPLACEMENT. (C CHECK RO 01-05-2022) REMOVED AND REPLACED RH WING SLAT TRACK 1-2 SIDE SUPPORT ROLLER AT THE O/B AFT POSITION IAW CRJ 700 AMM 27-81-44-400-8
- [SDR SWIA202163685](https://openairdocs.org/sdr/SWIA202163685.md): None · worn · Oct 25, 2021 · N796SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > ON THE LH WING, SLAT TRACK 2-2 SIDE ROLLER I/B FWD LOCATION IS OUT OF LIMITS AND REQUIRES REPLACEMENT. (C CHECK RO 01-05-2022) REMOVED AND REPLACED WITH A NEW SERVICEABLE SLAT TRACK 2-2 SIDE ROLLER (P/N: CC670-12048-3) AT THE I/B FWD LOCATION IAW CRJ700 AM
- [SDR SWIA202163684](https://openairdocs.org/sdr/SWIA202163684.md): None · worn · Oct 25, 2021 · N796SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > ON THE LH WING, SLAT TRACK 1-2 SIDE ROLLER O/B FWD LOCATION IS OUT OF LIMITS AND REQUIRES REPLACEMENT. (C CHECK RO 01-05-2022) REMOVED AND REPLACED WITH A NEW SERVICEABLE SLAT TRACK 1-2 SIDE ROLLER (P/N: CC670-12048-3) AT THE O/B FWD LOCATION IAW CRJ700 A
- [SDR SWIA202163652](https://openairdocs.org/sdr/SWIA202163652.md): None · gouged · Oct 22, 2021 · N796SK · Cndair CL600* · Fuselage, Equipment Attach Fittings
  > PAX DOOR PIANO HINGE HALF (FUSELAGE SIDE) HAS APPROX. (16) GOUGED HINGE LANDS LOOKING FROM AFT TO FRONT. (C CHECK RO 01-05-2022) REPAIRED AREAS IAW CRJ-700-SRM-53-21-23-201-010-A01 REPAIR TYPEE IV. AREA REQUIRES DETAILED VISUAL INSPECTION RE-INSPECT EVERY
- [SDR SWIA202163683](https://openairdocs.org/sdr/SWIA202163683.md): None · worn · Oct 21, 2021 · N796SK · Cndair CL600* · Ailerons
  > 3EA. ROLLERS ARE WORN FOR RIGHT SIDE TRAILING EDGE BUTE DOORS. (C CHECK RO 01-05-2022) REMOVED AND REPLACED WORN ROLLERS FROM TRAILING EDGE BUTE DOORS ON THE RIGHT HAND SIDE IAW CRJ 700 AMM 27-54-20-960-801-A01
- [SDR SWIA202163682](https://openairdocs.org/sdr/SWIA202163682.md): None · worn · Oct 21, 2021 · N796SK · Cndair CL600* · Ailerons
  > 3EA. ROLLERS ARE WORN FOR LEFT SIDE TRAILING EDGE BUTE DOORS. (C CHECK RO 01-05-2022) REMOVED 3EA. ROLLERS THAT WERE WORN ON LEFT SIDE TRAILING EDGE BUTE DOORS BY REMOVING OLD COTTER PIN, REMOVING ROLLER PIN, THEN REMOVING THE OLD ROLLER. INSTALLED 3EA. SE
- [SDR SWIA202163681](https://openairdocs.org/sdr/SWIA202163681.md): None · chafed · Oct 21, 2021 · N796SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > LEFT SLAT TRACK 1-1 HAS A CHAFE ON FWD OUTBOARD SIDE. (C CHECK RO 01-05-2022) REMOVED AND REPLACED THE LH 1-1 SLAT TRACK IAW CRJ-700 AMM 27-81-41-000-801-A01, 27-81-41-400-801-A01. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.
- [SDR SWIA202163651](https://openairdocs.org/sdr/SWIA202163651.md): None · cracked · Oct 21, 2021 · N796SK · Cndair CL600* · Fuselage Floor Panel
  > COCKPIT FLOOR BEAM AT RBL 9.00 IS CRACKED ON THE OUTBOARD SIDE AT F.S. 280.00. (C CHECK RO 01-05-2022) REPAIRED COCKPIT FLOOR BEAM AT RBL 9.00 IAW CRJ 700 SRM 53-11-43-201-003-A01. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED.
- [SDR SWIA202163696](https://openairdocs.org/sdr/SWIA202163696.md): None · corroded · Oct 20, 2021 · N796SK · Cndair CL600* · Wing Structure
  > RH OB GROUND SPOILER, ACTUATOR / CENTER HINGE HARDWARE CORRODED. (C CHECK RO 01-05-2022) REMOVED AND REPLACED R/H OB GROUND SPOILER/ CENTER HINGE HARDWARE IAW CRJ700 AMM 27-63-01-000/400-801-A01. REFERENCE ATTACHED SIGNED CONTINUATION CARD FOR DOCUMENTAT
- [SDR SWIA202163650](https://openairdocs.org/sdr/SWIA202163650.md): None · corroded · Oct 20, 2021 · N796SK · Cndair CL600* · Fuselage Main, Frame
  > FRAME SECTION AT F.S. 319 BETWEEN STR 20L AND 19L FOUND TO BE CORRODED. (C CHECK RO 01-05-2022) REMOVED DAMAGED FRAME SECTION AT FS 319 AND INSTALLED A NEW FRAME SECTION IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. TASK CARD 51-900-1002-SKY
- [SDR SWIA202163700](https://openairdocs.org/sdr/SWIA202163700.md): None · worn · Oct 19, 2021 · N796SK · Cndair CL600* · Elevator, Spar/Rib
  > RH ELEVATOR PCU TO ELEVATOR BOLTS DONT LINE UP WITH COTTER PIN HOLE WITHIN REQUIRED TOURQE VALUE AND NEED REPLACED WITH NEW HARDWARE (C CHECK RO 01-05-2022) RH ELEVATOR PCU TO ELEVATOR HARDWARE WAS REPLACED AS REQUIRED IAW CRJ 700 AMM 27-33-01-000-400-801
- [SDR SWIA202163680](https://openairdocs.org/sdr/SWIA202163680.md): None · corroded · Oct 19, 2021 · N796SK · Cndair CL600* · Doors
  > FWD BAGGAGE BAY DOOR LOWER STABILIZER GOUGED AND BENT. (C CHECK RO 01-05-2022) REMOVED AND REPLACED STABILIZER IAW CRJ-700-SRM-51-42-06-001-001-A01
- [SDR SWIA202163649](https://openairdocs.org/sdr/SWIA202163649.md): None · gouged · Oct 19, 2021 · N796SK · Cndair CL600* · Fuselage Structure (General)
  > FWD BAGGAGE BAY DOOR UPPER AFT CORNER OF GOUGED INTO DOOR SKIN. (C CHECK RO 01-05-2022) REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 670-52-35-436 REV-- DATED 2021-11-11 AND TASK CARD 51-900-1002-SKY, FORM M-337 ATTACHED, NO CHANGE TO WEIGHT AND BALANCE
- [SDR SWIA202163695](https://openairdocs.org/sdr/SWIA202163695.md): None · corroded · Oct 18, 2021 · N796SK · Cndair CL600* · Doors
  > RH OVERWING EMERGENCY EXIT PIVIOT BRACKET HAS CORRODED HARDWARE (C CHECK RO 01-05-2022) REMOVED DAMAGED HARDWARE AND INSTALLED NEW HARDWARE IAW CRJ 700 AMM 52-21-02-400-801
- [SDR SWIA202163679](https://openairdocs.org/sdr/SWIA202163679.md): None · corroded · Oct 18, 2021 · N796SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > FLOOR SEAT TRACK AT LBL9 CORRODED FROM FS677 TO FS863 (C CHECK RO 01-05-2022) REMOVED DAMAGED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW CRJ 700 AMM 53-00-49-000400-801-A03 AT LBL 9 FS 677- 863
- [SDR SWIA202163678](https://openairdocs.org/sdr/SWIA202163678.md): None · corroded · Oct 18, 2021 · N796SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > FLOOR SEAT TRACK AT RBL9 CORRODED FROM FS677 TO FS863 (C CHECK RO 01-05-2022) REMOVED AND REPLACED WITH NEW SEAT TRACK AT RBL9 FROM FS677 TO FS863 IAW CRJ 700 AMM 53-00-49-000/400-801-A03
- [SDR SWIA202163677](https://openairdocs.org/sdr/SWIA202163677.md): None · corroded · Oct 18, 2021 · N796SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > FLOOR SEAT TRACK AT LBL9 CORRODED FROM FS565 TO FS677 (C CHECK RO 01-05-2022) REMOVED AND REPLACED LBL 9 FLOOR SEAT TRACK FROM CORRECTED FS 570 TO FS 677 IAW CRJ 700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03
- [SDR SWIA202163676](https://openairdocs.org/sdr/SWIA202163676.md): None · corroded · Oct 18, 2021 · N796SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > FLOOR SEAT TRACK AT RBL9 CORRODED FROM FS565 TO FS677 (C CHECK RO 01-05-2022) REMOVED AND REPLACED RBL 9 FLOOR SEAT TRACK FROM FS 570 TO FS 677 IAW CRJ 700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03
- [SDR SWIA202163675](https://openairdocs.org/sdr/SWIA202163675.md): None · corroded · Oct 18, 2021 · N796SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL AT STGER 20L CORRODED BETWEEN FS310 AND FS349. (C CHECK RO 01-05-2022) REMOVED DAMAGED INTERCOSTAL AND INSTSALLECD A NEW INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR SWIA202201063648](https://openairdocs.org/sdr/SWIA202201063648.md): Floor Support · corroded · Oct 18, 2021 · N796SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL CORRODED BETWEEN FS349 TO FS364. (C CHECK RO 01-05-2022) ACCOMPLISHED A PERMANENT REPAIR IAW MHIRJ REO 670-53-21-2174 REV A DATED 2021-11-29. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, TASK CARD 51-900-1002-SKY AND M-337 COMPLETED AND ATTA
- [SDR SWIA202163647](https://openairdocs.org/sdr/SWIA202163647.md): None · corroded · Oct 18, 2021 · N796SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > MAIN AVIONICS SURROUND STRUCTURE, INTERCOSTAL CORRODED AT STGR26R BETWEEN FS349 AND FS364 (C CHECK RO 01-05-2022) REMOVED AND REPLACED INTERCOSTAL IAW CRJ-700-SRM-51-42-06-001-001-A01 AND 51-42-21-001-001-A01. COMPLIED WITH SKYCARD 51-900-1002-SKY AND M337
- [SDR SWIA202163694](https://openairdocs.org/sdr/SWIA202163694.md): None · cracked · Oct 17, 2021 · N796SK · Cndair CL600* · Fuselage, Door Hinge
  > PAX DOOR MOTOR MOUNT STIFFENER LOCATED ON AFT WEB CRACKED. (C CHECK RO 01-05-2022) REMOVED DAMAGED STIFFENER AND INSTALLED A NEW STIFFENER IAW CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202163693](https://openairdocs.org/sdr/SWIA202163693.md): None · corroded · Oct 17, 2021 · N796SK · Cndair CL600* · Fuselage, Door Hinge
  > PAX DOOR AFT STAIR WEB CORRODED. (MARKED WITH TAPE) (C CHECK RO 01-05-2022) REMOVED DAMAGED AFT STAIR WEB AND INSTALLED A NEW WEB IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01
- [SDR SWIA202163692](https://openairdocs.org/sdr/SWIA202163692.md): None · corroded · Oct 17, 2021 · N796SK · Cndair CL600* · Fuselage Structure (General)
  > FWD CARGO FLOOR BOARD SUPPORT ANGLE FWD OF FS 533.00 AT STGR 26L IS CORRODED. (C CHECK RO 01-05-2022) PART NUMBER SH670-33379-3 WAS REMOVED IAW CRJ 700 SRM 51-42-06-001-001-A01, NEW PART FABRICATED IAW CRJ 700 SRM 51-40-11-001-001-A01 WITH DWG SH670-33379
- [SDR SWIA202163674](https://openairdocs.org/sdr/SWIA202163674.md): None · corroded · Oct 17, 2021 · N796SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > SIDE SEAT TRACK FROM FS 863.00 TO FS 969.00 STGR 15R IS CORRODED. (C CHECK RO 01-05-2022) REMOVED AND REPLACED SIDE SEAT TRACK FROM FS 863.00 TO FS 969.00 IAW CRJ 700 AMM 53-00-49-000/400-801-A03

Next page: https://openairdocs.org/aircraft/N796SK/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 = 'N796SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N796SK/reports

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