# Service difficulty reports: N794SK

A list on [N794SK](https://openairdocs.org/aircraft/N794SK.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 · 119 reports

- [SDR SWIA2026080577141](https://openairdocs.org/sdr/SWIA2026080577141.md): Floorbeam · cracked · Aug 5, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > CENTER COCKPIT FLOORBEAM AT LBL 1200, FOUND CRACKED REPAIR IAW GREO 670-53-11-896, REV-. REPAIR PERFORMED CENTER COCKPIT FLOORBEAM LBL 12 IAW REO 670-53-11-896, REV-, SRM 51-42-06, 51-42-21, AMM 20-70-00,
- [SDR SWIA2026072377146](https://openairdocs.org/sdr/SWIA2026072377146.md): Intercostal · corroded · Jul 23, 2026 · N794SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF INTERCOSTAL FWD CARGO COMPARTMENT STR 23L HAS SIGNS OF CORROSION ON THE AFT FLANGE FOOT AT BS 517-533. REPAIR PERFORMED STR 23LT ON FWD CARGO COMPARTMENT FS517-FS533 IAW REO 670-53-31-1231, REV--, REO 670-53-31-1231 REV-P1, REO 670-53-31-1231,
- [SDR SWIA2026070577147](https://openairdocs.org/sdr/SWIA2026070577147.md): Rib · cracked · Jul 5, 2026 · N794SK · Cndair CL6002C11 · Wing, Rib/Bulkhead
  > LEFT WING SLAT 1 FIX LE RIB CRACKED AT WING BS 5841. PERFORMED REPAIR AREA ON SLAT 1 FIX RIB OF LT WING AT WS 5841 IAW SRM 51-42-10, 51-42-13, 51-42-06, REO 670-57-41-715, REV -,
- [SDR SWIA2026062977143](https://openairdocs.org/sdr/SWIA2026062977143.md): Bulkhead Web · corroded · Jun 29, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Bulkhead
  > SIGNS OF CORROSION ON 280 WEB AT BL 10, WL 725 APPROXIMATELY C-CHECK RO 09102026PERFORMED REPAIR BULKHEAD LOWER WEB ON FS280 AT BL10 WL725 IAW CRJ550 SRM 51-42-13, 51-42-06, 51-42-24, 53-00-00, 51-42-21, 51-41-02, 53-11-10, 51-21-11, 51-25-06, 51-25-16, AMM
- [SDR SWIA2026061577152](https://openairdocs.org/sdr/SWIA2026061577152.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 2 SKIN BURN MARKS NEAR STGR 25R AND BETWEEN FS32200-FS37400 2 SKIN BURN MARKS NEAR STGR 25R AND BETWEEN FS32200-FS37400 REF TABLE 1 OF REO 670-53-00-719 REV-, TABLE 1 DAMAGE 23, 26 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATED CPS REO
- [SDR SWIA2026061577151](https://openairdocs.org/sdr/SWIA2026061577151.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 7 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS28200-FS29600 7 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS28200-FS29600 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 11, 13, 14, 15, 16, 17, 19 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF D
- [SDR SWIA2026061577150](https://openairdocs.org/sdr/SWIA2026061577150.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 5 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS24100-FS27900 5 SKIN BURN MARKS NEAR STGR 25R AND 26R AND BETWEEN FS24100-FS27900 REF TABLE 1 OF REO 670-53-00-719 REV- TABLE 1 DAMAGE 2, 4, 7, 9, 10 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127
- [SDR SWIA2026061577149](https://openairdocs.org/sdr/SWIA2026061577149.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 5 RIVETS ON STGR 25R BETWEEN FS37000 AND 40200 5 BURNT RIVETS LOCATED ON STGR 25R BETWEEN FS37000-FS40200 REF TABLE 1 OF REO 670-53-00-719 REV- TABLE 1 DAMAGE 24, 25, 27, 28, 29 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATED CPS REO 670-
- [SDR SWIA2026061577148](https://openairdocs.org/sdr/SWIA2026061577148.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 5 RIVETS ON STGR 25R AND 26R BETWEEN FS23350 AND FS27400 5 BURNT RIVETS LOCATED ON STGR 25R AND 26R BETWEEN FS23350-FS27400 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 1, 3, 5, 6, 8 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATE
- [SDR SWIA2026061577145](https://openairdocs.org/sdr/SWIA2026061577145.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 6 RIVETS ON STGR 24R BETWEEN FS44550 AND FS45700 6 BURNT RIVETS LOCATED ON STGR 24R FS44550-FS45700 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 43, 44, 45, 46, 465, 47 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 27769127 FOR ASSOCIATED CPS REO 670-
- [SDR SWIA2026061577144](https://openairdocs.org/sdr/SWIA2026061577144.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 5 SKIN BURN MARKS NEAR STGR 24R AND 25R AND BETWEEN FS43525-FS44550 5 SKIN BURN MARKS NEAR STGR 24R AND 25R AND BETWEEN FS43525-FS44550 REF TABLE 1 OF REO 670-53-00-719 REV-- TABLE 1 DAMAGE 39, 40, 41, 42, 48 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN 2776
- [SDR SWIA2026061577142](https://openairdocs.org/sdr/SWIA2026061577142.md): Skin · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 9 RIVETS ON STGR 25R BETWEEN FS42200 AND FS43700 9 BURNT RIVETS LOCATED ON STGR 25R BETWEEN FS42200-FS43700 REF TABLE 1 OF REO 670-53-00-719 REV-- DATED 2024-02-15 TABLE 1 DAMAGE 30, 31, 32, 33, 34, 35, 36, 37, 38 FOR SPECIFIC LOCATIONS AND DIMENSIONS REF DIN
- [SDR SWIA2026061577140](https://openairdocs.org/sdr/SWIA2026061577140.md): Stringer · damaged · Jun 15, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer
  > 6 BURNED RIVETS LOCATED ON STR 25R AND 26R BTWN BS 282 - 319.70, REF TABLE 1 OF REO 670-53-00-719 REV--, TABLE 1, DAMAGE 12, 18, 20, 21, 22, 225. PERFORMED REPAIR OF DAMAGE HOLE 12,18,20,21,22,225, IAW SRM 51-42-13, 51-11-00, 53-00-00, AMM 20-30-00,21-3
- [SDR SWIA2026041375997](https://openairdocs.org/sdr/SWIA2026041375997.md): Skin · damaged · Apr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 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 (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED
- [SDR SWIA2026041375996](https://openairdocs.org/sdr/SWIA2026041375996.md): Skin · damaged · Apr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 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 (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATE
- [SDR SWIA2026041375995](https://openairdocs.org/sdr/SWIA2026041375995.md): Skin · damaged · Apr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 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 (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE
- [SDR SWIA2026041375994](https://openairdocs.org/sdr/SWIA2026041375994.md): Skin · damaged · Apr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > 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 (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE
- [SDR SWIA2026041375993](https://openairdocs.org/sdr/SWIA2026041375993.md): Skin · damaged · Apr 13, 2026 · N794SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847 AND STRINGERS 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS
- [SDR SWIA2026012000013](https://openairdocs.org/sdr/SWIA2026012000013.md): Overheat Loop · faulted · Jan 13, 2026 · N794SK · Cndair CL6002C10 · Overheat Detection
  > ANTI ICE DUCT WARNING ON CLIMB OUT OF DEN. QHR CLEARED THE MSG AND WE DIDN€™T NEED TO USE THE ANTI ICE AFTER THAT. (FLIGHT 5366) INTERROGATED MDC AND FOUND B1 CODES 007309 (L WING LOOP B) AND 007180 (L BLEED LOOP A). TROUBLESHOT L BLEED LOOP A PER FIM 36-2
- [SDR SWI2026F00076](https://openairdocs.org/sdr/SWI2026F00076.md): Warning Message · illuminated · Jan 13, 2026 · N794SK · Cndair CL6002C10 · Ice/Rain Protection System
  > ANTI ICE DUCT WARNING ON CLIMB OUT OF DEN. QHR CLEARED THE MSG AND WE DIDN`T NEED TO USE THE ANTI ICE AFTER THAT. (FLIGHT 5366) OPEN
- [SDR SWIA202511281025](https://openairdocs.org/sdr/SWIA202511281025.md): Floor Support · damaged · Oct 25, 2025 · N794SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DAMAGE HOLE TP RBL9.00 FLOOR SUPPORT LOWER FLANGE BTWN FS 677.00 & FS692.00. DAMAGE HOLE TP RBL9.00 FLOOR SUPPORT LOWER FLANGE BTWN FS 677.00 & FS692.00 COMPLIED ALL STEPS IAW REO670-53-31-1109 REV.--
- [SDR SWIA2025102700025](https://openairdocs.org/sdr/SWIA2025102700025.md): Floorbeam · damaged · Oct 25, 2025 · N794SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > DAMAGE HOLE TP RBL9.00 FLOOR BEAM LOWER FLANGE BTWN FS 677.00 & FS692.00. (FILED OPEN)
- [SDR SWIA20251128007](https://openairdocs.org/sdr/SWIA20251128007.md): Stringer · mechanic error · Oct 7, 2025 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CLIPCC670-24229-1 & -2 TO STRINGER 13A (LH & RH) WERE MISTAKENLY REMOVED ACCORDING PART A OF SB 044. PART A OF SB IS NOT APPLICABLE TO OUR AIRCRAFT SERIAL NUMBER. PARTS ARE SCRAP. NEW PARTS WILL BE REQUIRED. (FILED CLOSED)PERFORMED ALL STEPS PER REO 670-53-1
- [SDR SWIA202511281004](https://openairdocs.org/sdr/SWIA202511281004.md): Beam · damaged · Oct 4, 2025 · N794SK · Cndair CL6002C10 · Fuselage Main, Structure
  > DAMAGE WAS CAUSED TO THE FWD BULKHEAD BEAM AT RBL9, FS 693.00, NEW BULKHEAD BEAM WILL BE REQUIRE REPLACEMENT. FWD BULKHEAD BEAM AT RBL9 FS693, PN SH670-35885-6 REPLACED WITH NEW IAW SRM CRJ 700 51-42-21-001-001-A01, SRM CRJ 700 51-42-06-001-001-A01 AND SB 6
- [SDR SWIA2025100600004](https://openairdocs.org/sdr/SWIA2025100600004.md): Beam · damaged · Oct 4, 2025 · N794SK · Cndair CL6002C10 · Fuselage Main, Structure
  > DAMAGE WAS CAUSED TO THE FWD BULKHEAD BEAM AT RBL9, FS 693.00, PN SH670-35885-6. NEW BULKHEAD BEAM WILL BE REQUIRE REPLACEMENT.
- [SDR SWIA202512020928](https://openairdocs.org/sdr/SWIA202512020928.md): Stringer · chafed · Sep 28, 2025 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CHAFING FOUND UNDER FUSELAGE SKIN ON STRIGER 27, BS 977 - 989. CHAFE BLEND-OUT & FOUND WITHIN LIMITS IAW SRM 53-00-01-101-001-A01, L:3" W:2" D:0.016",SURFACE REPROTECTED IAW SRM 51-25-01-001-A01.
- [SDR SWIA2025092900028](https://openairdocs.org/sdr/SWIA2025092900028.md): Stringer · chafed · Sep 28, 2025 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CHAFING FOUND UNDER FUSELAGE SKIN ON STRG 27, FS 977.00 TO 989.00. (FILED OPEN)
- [SDR SWIA20240322001](https://openairdocs.org/sdr/SWIA20240322001.md): Landing Gear · warning message · Mar 21, 2024 · N794SK · Cndair CL6002C10 · Landing Gear Position and Warning
  > GEAR DISAGREE UP WARNING MESSAGE ON DEPARTURE (FLIGHT 5325 FILED CLOSED)UPON ARRIVAL TO AIRCRAFT FOUND GEAR PIN TO BE INSTALLED IN RIGHT HAND MLG. PERFORMED A GVI OF THE RIGHT MLG AREA AND FOUND NO DISCREPANCIES REF AMM 32-10-00. INTERROGATED PSEU AND FOUND A
- [SDR SWIA2023041800012](https://openairdocs.org/sdr/SWIA2023041800012.md): Stiffener · cracked · Apr 12, 2023 · N794SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT SKIN HAS A 2 INCH CRACK BEHIND THE COUNTERBALANCE BRACKET. (FILED CLOSED)REPAIRED DAMAGED PAX DOOR AFT SKIN IAW SRM 52-11-04-201-004-A01
- [SDR SWIA202266612](https://openairdocs.org/sdr/SWIA202266612.md): None · gouged · Oct 14, 2022 · N794SK · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > OUT OF LIMITS GOUGE DAMAGE TO HSTA UPPER RH ATTACHMENT FITTING HAS BEEN DETERMINED TO BE A MAJOR REPAIR IN REFERENCE TO GMM 3-26. / SEE CP 25653192 FOR DETERMINATION OF MAJOR/MINOR REPAIR TO THE HSTA UPPER RH ATTACHMENT FITTING. (FILED CLOSED) PERFORMED
- [SDR SWIA202266611](https://openairdocs.org/sdr/SWIA202266611.md): None · gouged · Oct 14, 2022 · N794SK · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > OUT OF LIMITS GOUGE DAMAGE TO HSTA UPPER LH ATTACHMENT FITTING HAS BEEN DETERMINED TO BE A MAJOR REPAIR IN REFERENCE TO GMM 3-26. / SEE CP 25653171 FOR DETERMINATION OF MAJOR/MINOR REPAIR TO THE HSTA UPPER LH ATTACHMENT FITTING. (FILED CLOSED PERFORMED
- [SDR SWIA202266610](https://openairdocs.org/sdr/SWIA202266610.md): None · gouged · Oct 14, 2022 · N794SK · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > OUT OF LIMITS GOUGE DAMAGE TO HSTA LH UPPER INBOARD, LH UPPER OUTBOARD AND RH UPPER INBOARD FITTINGS HAS BEEN DETERMINED TO BE A MAJOR REPAIR IN REFERENCE TO GMM 3-26. / SEE CP 25653199-1 FOR DETERMINATION OF MAJOR/MINOR REPAIR TO THE HSTA UPPER LH UPPER INBO
- [SDR SWIA202163525](https://openairdocs.org/sdr/SWIA202163525.md): None · damaged · Dec 4, 2021 · N794SK · Cndair CL6002C10 · Fuselage Main, Keel
  > PERFORM 953 FRAME SPLICE AT STRG25L AND STRG25R TO PROVIDE REPLACEMENT OF STRG25L REPAIR SECTION ON JOB: 71029874 OP: 69 MX TRANS #23682006 (C-CHECK RO 1/7/2022) PERFORMED FRAME 953 SPLICE REPAIR AT STRG25L AND STRG25R IAW REO 670-53-51-243 REV-A DATED
- [SDR SWIA202163524](https://openairdocs.org/sdr/SWIA202163524.md): None · cracked · Dec 1, 2021 · N794SK · Cndair CL6002C10 · Doors
  > AFT CARGO DOOR SURROUND BRACKET CC670-38814-1 IS CRACKED (C-CHECK RO 1/7/2022) FABRICATED NEW AFT CARGO DOOR SURROUND BRACKET PN: CC670-38814-1 FROM PN: S6144-16 PO: T000056550/2 IAW DWG CC670-38814 REV --, AND REPLACED IAW CRJ700 SRM 51-42-06-001-001-A
- [SDR SWIA202163523](https://openairdocs.org/sdr/SWIA202163523.md): None · cracked · Nov 28, 2021 · N794SK · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT FLOOR SUPPORT ANGLE LOCATED AT RBL12.00 FS259 TO FS280 IS CRACKED (C-CHECK RO 1/7/2022) REMOVED AND REPLACED COCKPIT FLOOR SUPPORT ANGLE LOCATED AT RBL12.00 FS259 TO FS280 IAW CRJ700 SRM 51-42-06-001-001-A01 & DWG CC670-33052 REV -G, COMPLIED W
- [SDR SWIA202163522](https://openairdocs.org/sdr/SWIA202163522.md): None · corroded · Nov 18, 2021 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON INTERCOSTAL P/N 601R31902-317 COMMON TO FORMER FS347.25 (C-CHECK RO 1/7/2022) REMOVED AND REPLACED INTERCOSTAL P/N 601R31902-317 COMMON TO FORMER AT FS347.25 PER CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. CO
- [SDR SWIA202163521](https://openairdocs.org/sdr/SWIA202163521.md): None · cracked · Nov 18, 2021 · N794SK · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT BEAM AT RBL12.00 JUST FWD OF FS280 IS CRACKED. (C-CHECK RO 1/7/2022) REMOVED AND INSTALLED NEW COCKPIT RBL 12.00 FLOOR BEAM SECTION -34, AND REINSTALLED PRE EXISTING REPAIR PARTS -36, -38, -40, -42 IAW CRJ700 SRM 53-11-43-201-003-A01 TYPE 4 REP
- [SDR SWIA202163520](https://openairdocs.org/sdr/SWIA202163520.md): None · corroded · Nov 15, 2021 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON BRACKET AND INTERCOSTAL DD7 COMMON TO FORMER FS347.25 (C-CHECK RO 1/7/2022) REMOVED AND REPLACED DD7 INTERCOSTAL AND BRACKET COMMON TO FORMER AT FS347.25 PER CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. COMPL
- [SDR SWIA202163519](https://openairdocs.org/sdr/SWIA202163519.md): None · corroded · Nov 15, 2021 · N794SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON BRACKET AND INTERCOSTAL DD6 COMMON TO FORMER FS347.25 (C-CHECK RO 1/7/2022) REMOVED AND REPLACED DD6 INTERCOSTAL AND BRACKET COMMON TO FORMER AT FS347.25 PER CRJ700SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. COMPLIED
- [SDR SWIA202163518](https://openairdocs.org/sdr/SWIA202163518.md): None · corroded · Nov 14, 2021 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL JUST RIGHT OF STR 27 CORRODED ON ATTACHING FLANGE (C-CHECK RO 1/7/2022) REPLACED INTERCOSTAL JUST RIGHT OF STGR27 PER CRJ-700 SRM 51-42-06-001-001-A01 REV-38, DATED JUL25/2020, CRJ 700 SRM 51-42-21-001-001-A01 REV-38 DATED JUL 25/2020 AND D
- [SDR SWIA202163517](https://openairdocs.org/sdr/SWIA202163517.md): None · corroded · Nov 14, 2021 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL JUST LEFT OF STR 27 CORRODED ON ATTACHING FLANGE (C-CHECK RO 1/7/2022) REMOVED AND REPLACED INTERCOSTAL ON L/H SIDE OF STGR27 PER CRJ700SRM 51-42-06-001-001-A01 AND CRJ700SRM 51-42-21-001-001-A01 AND DWG SH670-32050 REV J. SEE CONTINUATION
- [SDR SWIA202163516](https://openairdocs.org/sdr/SWIA202163516.md): None · corroded · Nov 11, 2021 · N794SK · Cndair CL6002C10 · Doors
  > CORROSION FOUND ON PAX DOOR FORMER, FS320.163 CLOSE TO THE HINGE (C-CHECK RO 1/7/2022) REMOVED AND REPLACED PAX DOOR FORMER AT FS320.163 PER CRJ700SRM 51-42-06-001-001-A01 AND CRJ700SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. COMPLIED
- [SDR SWIA202163515](https://openairdocs.org/sdr/SWIA202163515.md): None · corroded · Nov 11, 2021 · N794SK · Cndair CL6002C10 · Doors
  > CORROSION FOUND ON PAX DOOR FORMER FS311.75 (C-CHECK RO 1/7/2022) REMOVED AND REPLACED PAX DOOR FORMER FS311.75 P/N 601R318031-5S IAW CRJ700 SRM 51-42-06-001-001-A01 REVISION 38: JUL 25/2020, CRJ700 SRM 51-42-21-001-001-A01 REVISION 38 JUL 25/2020, AND
- [SDR SWIA202163514](https://openairdocs.org/sdr/SWIA202163514.md): None · corroded · Nov 9, 2021 · N794SK · Cndair CL6002C10 · Doors
  > CORROSION FOUND AT FASTENERS ROW ON PAX DOOR FORMER, FS338.963 CLOSE TO THE HINGE. (C-CHECK RO 1/7/2022) REMOVED AND REPLACED PAX DOOR FORMER FS338.963 P/N 601R318037-3 WITH A NEW UNIT IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01
- [SDR SWIA202163513](https://openairdocs.org/sdr/SWIA202163513.md): None · corroded · Nov 9, 2021 · N794SK · Cndair CL6002C10 · Doors
  > CORROSION FOUND ON PAX DOOR INTERCOSTAL DD3 COMMON TO FORMER FS311.75 (C-CHECK RO 1/7/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 PER CRJ700SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY. SE
- [SDR SWIA202163512](https://openairdocs.org/sdr/SWIA202163512.md): None · corroded · Nov 8, 2021 · N794SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION FOUND ON FRAME FS313.56, DD4 AND DD5 ON FASTENERS ROW. (C-CHECK RO 1/7/2022) REMOVED AND REPLACED FRAME AT FS313.56 DD4 AND DD5 PER CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. S
- [SDR SWIA202163511](https://openairdocs.org/sdr/SWIA202163511.md): None · corroded · Nov 8, 2021 · N794SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON INTERCOSTAL DD2 COMMON TO FORMER FS347.25. (C-CHECK RO 1/7/2022) REMOVED AND REPLACED INTERCOSTAL DD2 P/N 601R318052-1 COMMON TO FORMER FS347.25 WITH A NEW ONE IAW CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV. N. C
- [SDR SWIA202163510](https://openairdocs.org/sdr/SWIA202163510.md): None · corroded · Nov 8, 2021 · N794SK · Cndair CL6002C10 · Galley Doors
  > CORROSION FOUND ON PAX DOOR INTERCOSTAL DD6 COMMON TO FORMER FS311.75. (C-CHECK RO 1/7/2022) REMOVED, REPLACED AND INSTALLED PAX DOOR INTERCOSTAL DD6 P/N 601R31902-485S IAW CRJ700 SRM 51-42-06-001-001-A01 REVISION 38: JUL 25/2020, AND DRAWING 601R31702
- [SDR SWIA202163509](https://openairdocs.org/sdr/SWIA202163509.md): None · corroded · Nov 8, 2021 · N794SK · Cndair CL6002C10 · Doors
  > CORROSION FOUND ON PAX DOOR INTERCOSTAL DD2 COMMON TO FORMER FS311.75 (C-CHECK RO 1/7/2022) REMOVED AND REPLACED INTERCOSTAL DD2 P/N 601R318051-1S WITH A NEW UNIT IAW CRJ700 SRM 51-42-06-001-001-A01 REVISION 38: JUL 25/2020, AND BOMBARDIER DRAWING 601R3
- [SDR SWIA202163508](https://openairdocs.org/sdr/SWIA202163508.md): None · cracked · Nov 6, 2021 · N794SK · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > * R/H SLAT TRACK CANISTER 1-3 HAS A CRACKED ATTACHMENT BRACKET ON AFT END, MARKED. (C-CHECK RO 1/7/2022) COMPLIED WITH REPAIR OF R/H SLAT TRACK CANISTER 1-3 REF REO 670-57-42-577 REV-- DATE 2016-12-02 LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD

Next page: https://openairdocs.org/aircraft/N794SK/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 = 'N794SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N794SK/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.