# Service difficulty reports: N744SK

A list on [N744SK](https://openairdocs.org/aircraft/N744SK.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 · 209 reports

- [SDR SWIA202504240009](https://openairdocs.org/sdr/SWIA202504240009.md): Buss · failed · Apr 9, 2025 · N744SK · Cndair CL6002C10 · AC Power Distribution System
  > AC BUS 1 FAIL ACCOMPANIED BY GEN 1 OFFLINE AND AC ESSENTIAL BUS FAIL AFTER TAKEOFF, RAN QRH, RETURN TO FIELD (FLIGHT 6534 - FILED CLOSED)FOUND TERMINAL T3 ON THE LH IDG DAMAGED AND SIGNS OF OVER HEATING. REPLACED #1 IDG REF. CRJ700 AMM 24-11-01, AND REPLACED #
- [SDR SWI2025F00444](https://openairdocs.org/sdr/SWI2025F00444.md): Generator · warning message · Apr 9, 2025 · N744SK · Cndair CL6002C10 · AC Generator-Alternator
  > AC BUS 1 FAIL ACCOMPANIED BY GEN 1 OFFLINE AND AC ESSENTIAL BUS FAIL AFTER TAKEOFF, RAN QRH, RETURN TO FIELD (FLIGHT 6534 - FILED OPEN)FOUND TERMINAL T3 ON THE LH IDG DAMAGED AND SIGNS OF OVER HEATING. REPLACED #1 IDG REF. CRJ700 AMM 24-11-01, AND REPLACED #1
- [SDR SWIA202411200019](https://openairdocs.org/sdr/SWIA202411200019.md): A/C Pack · faulted · Nov 19, 2024 · N744SK · Cndair CL6002C10 · Cabin Cooling System
  > DIVERTED TO ICT DUE TO DIFF PRESS MESSAGE, LEFT PACK CYCLING ON CLIMBOUT, DIFF PRESS MESSAGE APPROX FLT LEVEL 240, EMERGENCY DECENT TO 10,000 FEET, LT PACK CONTINUED TO CYCLE, EMERGENCY MESSAGE EXTINGUISHED, PRESSURE STABALIZED, CABIN MASK DID NOT DEPLOY, DIVE
- [SDR SWIA2024032500016](https://openairdocs.org/sdr/SWIA2024032500016.md): Skin · gouged · Mar 16, 2024 · N744SK · Cndair CL6002C10 · Leading Edge Devices
  > L/H #1 SLAT WAS GOUGED ON THE LOWER SURFACE AT APPX. SLAT STATION 119. (C-CHECK RO 3/23/2024) REPAIRED L/H #1 SLAT, GOUGE ON THE LOWER SURFACE AT APPX. SLAT STATION 119. BY COMPLYING WITH REO 670-57-42-1501 REV -- DATED 2024-03-17, COMPLIED WITH 51-900-100
- [SDR SWIA2024032500221](https://openairdocs.org/sdr/SWIA2024032500221.md): Skin · damaged · Feb 21, 2024 · N744SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP HAS SMOKING RIVITS ON THE OUTTER SKIN (C-CHECK RO 3/23/2024) REMOVED AND REPLACED 10EA SMOKING FASTENERS ON RH OUTBOARD FLAP PER MHIRJ REO 670-57-53-347, REV: --, DATED 2024-02-24. ALL STEPS OF REO COMPLIED WITH IN THEIR ENTIRETY.SKYCA
- [SDR SWIA20240325219](https://openairdocs.org/sdr/SWIA20240325219.md): Skin · damaged · Feb 19, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Structure
  > THE LH APRON SKIN HAS MULTIPLE SMOKED RIVETS. (MARKED) (C-CHECK RO 3/23/2024) REMOVED SMOKING FASTENERS AS REQUIRED FROM L/H APRON SKIN. COMPLIED WITH REO 670-53-42-077, REV --, DATED ON 2024-02-22. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202403250263](https://openairdocs.org/sdr/SWIA202403250263.md): Drag Angle · cracked · Feb 10, 2024 · N744SK · Cndair CL6002C10 · Vertical Stabilizer
  > RH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE IS CRACKED (MARKED) CAMP # 27802535 (C-CHECK RO 3/23/2024) REPAIRED R/H AFT ANGLE ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT REF CRJ 700 SRM 55-31-00-201-001-A01. M-337 AND SKYWEST TASK CARD 51-900-1002-SKY CO
- [SDR SWIA20240325210](https://openairdocs.org/sdr/SWIA20240325210.md): Window Post · cracked · Feb 10, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Structure
  > PILOT'S SIDE WINDSHIELD POST. SUSPECT CRACKED AT THE TOP OF THE POST ON BOTH SIDES. (MARKED WITHIN RED GREASE PENCIL AND FLAGGED.) (C-CHECK RO 3/23/2024) REMOVED AND INSTALLED NEW PILOT SIDE WINDSHIELD POST REF CRJ 700 SRM 51-42-21-001-001-A01 / BOMBARDIER
- [SDR SWIA202403250268](https://openairdocs.org/sdr/SWIA202403250268.md): Seat Track · gouged · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL FS677-FS708, STGR15R HAS NICKS, GOUGES AND CORRODED HARDWARE, HN00137297 (C-CHECK RO 3/23/2024) REPLACED SIDE SEAT RAIL, P/N SH670-36255-3, AT APPROXIMATELY FS 677- FS 708, STGR 15 RH, REF CRJ 700, SRM 51-41-02-001-001-A01.
- [SDR SWIA2024032500267](https://openairdocs.org/sdr/SWIA2024032500267.md): Seat Track · gouged · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL FS485-FS565, STGR15R HAS SEVERAL AREAS OF NICKS AND GOUGES, HN00137290 (C-CHECK RO 3/23/2024) REMOVED OLD SIDE SEAT RAIL & INSTALLED NEW SIDE SEAT RAIL AT FS. 485-FS565, STGR15R REF. CRJ700 AMM 53-00-49-000-801-A03 & REF. CRJ700 AMM 53-00
- [SDR SWIA2024032500266](https://openairdocs.org/sdr/SWIA2024032500266.md): Seat Track · gouged · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL FS379-FS469, STGR15R HAS SEVERAL AREAS OF NICKS AND GOUGES, HN00137289 (C-CHECK RO 3/23/2024) SIDE SEAT RAIL FS379-FS469, STGR15R IS OUT OF LIMITS DUE TO HAVING DAMAGE/ CORROSION AT MULTIPLE CROSS-SECTIONS AND WITHIN 3.00" APART REF CRJ-70
- [SDR SWIA2024032500265](https://openairdocs.org/sdr/SWIA2024032500265.md): Seat Track · gouged · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL FS581-FS661, STGR15L HAS SEVERAL AREAS OF NICKS AND GOUGES, HN00137287 (C-CHECK RO 3/23/2024) SIDE SEAT RAIL FS581-FS661, STGR15L IS OUT OF LIMITS DUE TO HAVING MULTIPLE DAMAGES WITHIN 3.00" FROM EACH OTHER, NOT ALLOWED REF CRJ-700 SRM 53
- [SDR SWIA202403250264](https://openairdocs.org/sdr/SWIA202403250264.md): Seat Track · gouged · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL FS485-FS565, STGR15L HAS SEVERAL AREAS OF NICKS AND GOUGES, HN00137286 (C-CHECK RO 3/23/2024) REMOVED AND REPLACED WITH NEW SIDE SEAT RAIL FS485-FS565, STGR15L REF CRJ700 AMM 53-00-49-400-801-A03. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2024032500269](https://openairdocs.org/sdr/SWIA2024032500269.md): Seat Track · gouged · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL FS379-FS469, STGR15L HAS SEVERAL AREAS OF NICKS AND GOUGES, HN00137285 (C-CHECK RO 3/23/2024) REMOVED AND REPLACED WITH NEW SIDE SEAT RAIL AT LH SIDE, FS379 - FS469 REF CRJ700 AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.
- [SDR SWIA2024032500205](https://openairdocs.org/sdr/SWIA2024032500205.md): Seat Track · corroded · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL FS379-FS469 RBL9 HAS CORROSION THROUGH OUT IN VARIOUS AREAS, HN00137278 (C-CHECK RO 3/23/2024) REPLACED SEAT RAIL AT FS379-FS477.4 RBL9 WITH NEW REF. CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA2024032500264](https://openairdocs.org/sdr/SWIA2024032500264.md): Seat Track · gouged · Feb 5, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL FS485-FS565, STGR15L HAS SEVERAL AREAS OF NICKS AND GOUGES, HN00137286 (C-CHECK RO 3/23/2024) REMOVED AND REPLACED WITH NEW SIDE SEAT RAIL FS485-FS565, STGR15L REF CRJ700 AMM 53-00-49-400-801-A03. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA20240325201](https://openairdocs.org/sdr/SWIA20240325201.md): Hinge · gouged · Feb 1, 2024 · N744SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > LAST FLAT ON THE PASSENGER DOOR PIANO HINGE ON THE FUSELAGE SIDE IS GOUGED AND THE ROLL PIN IS MISSING. (C-CHECK RO 3/23/2024) REMOVED AND REPLACED PAX DOOR PIANO HINGE ON THE FUSELAGE SIDE REF CRJ 700 SRM 53-21-23-201-007-A01. COMPLIED WITH 51-900-1002-S
- [SDR SWIA202403250262](https://openairdocs.org/sdr/SWIA202403250262.md): Floorbeam · cracked · Jan 31, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR BEAM RBL12.00 AT FS280.00 IS FOUND CRACK (C-CHECK RO 3/23/2024) REMOVED AND INSTALLED NEW COCKPIT FLOOR BEAM RBL12.00 FS280.00 REF (TYPE IV REPAIR) REF CRJ700 SRM 53-11-43-201-003-A01. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202403250261](https://openairdocs.org/sdr/SWIA202403250261.md): Floorbeam · cracked · Jan 31, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > COCKPIT FLOOR BEAM LBL12.00 AT FS280.00 IS FOUND CRACK (C-CHECK RO 3/23/2024) REMOVED AND INSTALLED NEW COCKPIT FLOOR BEAM LBL12.00 FS280.00 REF (TYPE IV REPAIR) REF CRJ700 SRM53-11-43-201-003-A01. COMPLIED WITH 51-900-1002-SKY
- [SDR SWI202403250260](https://openairdocs.org/sdr/SWI202403250260.md): Drag Angle · cracked · Jan 31, 2024 · N744SK · Cndair CL6002C10 · Vertical Stabilizer
  > RH VERTICAL STAB TO FUSELAGE DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 3/23/2024) REPAIRED RH VERTICAL STAB TO FUSELAGE DRAG ANGLEREF CRJ 700 SRM 55-31-00-201-001-A01.COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2024032500131](https://openairdocs.org/sdr/SWIA2024032500131.md): Landing · cracked · Jan 31, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TRU PANEL 212AR LOWER LANDING ANGLE ON FUSELAGE HAS POSSIBLE CRACK AT THE AFT LATCH CUT OUT RADIUS (MARKED) (C-CHECK RO 3/23/2024) INSTALLED NEW LANDING ANGLE CC670-33151-6 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DRAWING CC670-33040 REV G AND REO 670-53-
- [SDR SWIA202403250259](https://openairdocs.org/sdr/SWIA202403250259.md): Landing · cracked · Jan 30, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TRU PANEL 211AL LOWER LANDING ANGLE ON FUSELAGE HAS POSSIBLE CRACK AT THE AFT LATCH CUT OUT RADIUS (MARKED) (C-CHECK RO 3/23/2024) PERFORMED DVI ON UPPER ELECTRICAL LH ACCESS LOWER LANDING ANGLE AT AFT LATCH CUT OUT RADIUS, IT WAS FOUND A VISIBLE CRACK OF
- [SDR SWIA202403250258](https://openairdocs.org/sdr/SWIA202403250258.md): Skin · cracked · Jan 30, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > POSSIBLE CRACK ON THE RH SIDE OF THE FUSELAGE SKIN AT TRU PANEL 212AR LOWER AFT CORNER AREA (MARKED) (C-CHECK RO 3/23/2024) ON THE RH SIDE OF THE FUSELAGE SKIN AT TRU PANEL CRACK LENGTH = 0.250", CRACK LENGTH PERMITTED = 0.5D = 0.081" (WHERE D IS THE NEARE
- [SDR SWIA202403250257](https://openairdocs.org/sdr/SWIA202403250257.md): Skin · cracked · Jan 30, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > POSSIBLE CRACK ON THE LH SIDE OF THE FUSELAGE SKIN AT TRU PANEL 211AL LOWER AFT CORNER AREA (MARKED) (C-CHECK RO 3/23/2024) INSTALLED NEW SKIN PANEL ON AIRCRAFT FROM FS169 TO FS202, BETWEEN STGR 24L TO STGR 16L PER REF CRJ 700 SRM 51-42-06-001-001-A01, CR
- [SDR SWIA2024032600256](https://openairdocs.org/sdr/SWIA2024032600256.md): Stringer · corroded · Jan 30, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Keel
  > AREAS OF CORROSION ON STGR 26R BETWEEN FS 1031.00 - 1049.00 (C-CHECK RO 3/23/2024) BLENDED AREAS OF CORROSION. FOUND OUT OFF LIMITS REF CRJ700 SRM 53-61-03-101-003-A01.REPAIRED CORROSION ON STGR 26R BETWEEN FS 1031.00 - 1049.00 PER REO 670-53-61-2237 REV -
- [SDR SWI20240326000255](https://openairdocs.org/sdr/SWI20240326000255.md): Seal · torn · Jan 30, 2024 · N744SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SURROUND LOWER FORWARD SEAL SURROUND CRACKED/BENT AND TORN LOOSE FROM STRUCTURE (C-CHECK RO 3/23/2024) REMOVED AND INSTALLED LOWER FORWARD SEAL SURROUND AND LOWER FWD CORNER SEAL STRIKER REF CRJ700 SRM 51-42-06-001-001-A01 AND DRW. SH670-318
- [SDR SWIA2024032600130](https://openairdocs.org/sdr/SWIA2024032600130.md): Door Sill · gouged · Jan 30, 2024 · N744SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR SURROUND LOWER SILL ANGLE HAS GOUGES (C-CHECK RO 3/23/2024) REMOVED BAD AND INSTALLED NEW GALLEY SERVICE DOOR SURROUND LOWER SILL ANGLE REF CRJ700 SRM 51-42-06-001-001-A01 AND DRAWING SH670-31950 REV Y, COMPLIED WITH SKYCARD 51-900-1002
- [SDR SWI20240326000254](https://openairdocs.org/sdr/SWI20240326000254.md): Door Sill · corroded · Jan 29, 2024 · N744SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AREAS OF CORROSION ON AFT CARGO DOOR LOWER SILL (C-CHECK RO 3/23/2024) AFT CARGO DOOR SILL FOUNT TO BE OUT OF LIMITS. REMOVED AND REPLACED THE AFT CARGO DOOR LOWER SILL REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-
- [SDR SWI20240326000253](https://openairdocs.org/sdr/SWI20240326000253.md): Striker · damaged · Jan 29, 2024 · N744SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR SEAL DEPRESSOR IS DAMAGED, FS349.00 BETWEEN STGR4L & 5L. (MARKED) (C-CHECK RO 3/23/2024) REMOVED AND REPLACED WITH NEW SEAL STRIKER (P/N SH670-31887-5) ON UPPER FRAME AT FS349.00 REF BOMBARDIER DWG# SH670-31810 REV AE AND CRJ700 SRM'S 51-42
- [SDR SWIA2024032600129](https://openairdocs.org/sdr/SWIA2024032600129.md): Transcowl · chafed · Jan 29, 2024 · N744SK · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH. (C-CHECK RO 3/23/2024) REMOVED DAMAGED COAMING ON LH LOWER TRANSCOWL AND PERFORMED REPAIR IAW ALL STEPS OF REO 670-54-21-1615 REV--, DATED 2024-02-05. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2024032600128](https://openairdocs.org/sdr/SWIA2024032600128.md): Slat Track · damaged · Jan 28, 2024 · N744SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT WING SLAT TRACK 1-1 SECTOR GEAR ROLLER SURFACE GROOVED. (C-CHECK RO 3/23/2024) REPAIRED RIGHT WING SLAT TRACK 1-1 SECTOR GEAR ROLLER SURFACE REF REO 670-57-42-1484 REV- STEPS 1-9.
- [SDR SWIA2024032600125](https://openairdocs.org/sdr/SWIA2024032600125.md): Skin · damaged · Jan 25, 2024 · N744SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN DAMAGED ALONG THE EDGE OF NOSE LANDING GEAR BOX CUT OUT, LEFT SIDE APPX. FS210.00. (C-CHECK RO 3/23/2024) BLENDED OUT EXTERNAL SKIN DAMAGE ALONG THE EDGE OF NOSE LANDING GEAR BOX CUT OUT, LEFT SIDE APPX. FS210.00. REF: CRJ-700 SRM 51-12-00-001-
- [SDR SWIA2024032600123](https://openairdocs.org/sdr/SWIA2024032600123.md): Housing · gouged · Jan 23, 2024 · N744SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR EXTERNAL HANDLE HOUSING HAS GOUGES ON HANDLE CUTOUT EDGES (C-CHECK RO 3/23/2024) REMOVED AND REPLACED WITH NEW AFT CARGO DOOR HANDLE HOUSING REF CRJ700 SRM 51-42-21-001-001-A01 AND DWG:600-35027, REV -M ALL CHECKS GOOD.SKYCARD 51-900-1002-S
- [SDR SWIA2024032600121](https://openairdocs.org/sdr/SWIA2024032600121.md): Skin · chafed · Jan 21, 2024 · N744SK · Cndair CL6002C10 · Rudder, Plate/Skin
  > RUDDER LEADING EDGE SKINS ARE CHAFFED. (C-CHECK RO 3/23/2024) REMOVED DAMAGE AT MULTIPLE LOCATIONS ON L/H AND R/H RUDDER LEADING EDGE SKINS REF CRJ700 SRM 51-12-00-001-001-A01COMPLIED WITH ALL STEPS 1-4 REF REO 670-55-41-134 REV --, DATED 2024-02-09. COMPL
- [SDR SWIA2024032601019](https://openairdocs.org/sdr/SWIA2024032601019.md): Skin · damaged · Oct 19, 2023 · N744SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DAMAGE ON LT SIDE OF FUSELAGE BETWEEN FS 349 AND FS 364 AND BETWEEN STRG 16L AND STGR 14L AND ON STRGR 15L. DAMAGE MEASURES 6" IN DIAMETER 3" BELOW STGR 14L AND 6.5" FWD OF FS 364.0. DAMAGE MEASURES.125" DEEP AT DEEPEST POINT WITH 2 SHEARED RIVETS ON STGR 15L
- [SDR SWIA20230907006](https://openairdocs.org/sdr/SWIA20230907006.md): Unknown · cracked · Sep 6, 2023 · N744SK · Cndair CL6002C10 · Flight Compartment Windows
  > F/O WINDSHIELD SHATTERED AT AROUND FL 250 CLIMBING TO FL260. RAN QRH AND DIVERTED TO KFWA (FLT 3063 FILED CLOSED)REMOVED AND REPLACED F/O'S WINDSHIELD IN REFERENCE TO AMM 56-11-01. COMPLETED TASK CARD 56-220-1000-SKY. PERFORMED OPS CHECK OF FO'S WINDSHIELD WI
- [SDR SWIA2023050100426](https://openairdocs.org/sdr/SWIA2023050100426.md): Window Post · damaged · Apr 26, 2023 · N744SK · Cndair CL6002C10 · Fuselage Main, Structure
  > WHILE REPLACING RH WINDSHIELD, FOUND A CRACK IN THE UPPER MOST BOLT HOLE OF THE RH SIDE POST. (FILED CLOSED)REMOVED AND REPLACED RH WINDSHIELD/WINDOW SIDEPOST P/N 601R33223-2 IAW. SRM 51-42-21-001-001-A01 REV 38 JULY-25-2020, DRAWING CC670-33055 REV F DATED 2
- [SDR SWIA2023042700002](https://openairdocs.org/sdr/SWIA2023042700002.md): Unknown · cracked · Apr 26, 2023 · N744SK · Cndair CL6002C10 · Flight Compartment Windows
  > WHILE REPLACING RH WINDSHIELD, FOUND A CRACK IN THE UPPER MOST BOLT HOLE OF THE RH SIDE POST. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2023042700001](https://openairdocs.org/sdr/SWIA2023042700001.md): Unknown · damaged · Apr 26, 2023 · N744SK · Cndair CL6002C10 · Flight Compartment Windows
  > FOUND RH WINDSHIELD Z-STRAP SEAL DAMAGED BEYOND LIMITS, WINDSHIELD REQUIRES REPLACEMENT. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2023010967084](https://openairdocs.org/sdr/SWIA2023010967084.md): Warning Message · illuminated · Jan 6, 2023 · N744SK · Cndair CL6002C10 · Landing Gear Position and Warning
  > ODI EVENT - PROX SYSTEM CAUTION MSG RETURN TO FIELD WITH DECLARED EMERGENCY REQUIRES SMOD APPROVAL BEFORE AIRCRAFT CAN BE PUT BACK IN SERVICE. REQUEST MCC REVIEW FOR APPROVAL WHEN TROUBLESHOOTING/ WORK IS COMPLETE / MCI TYPE: TROUBLESHOOTING PRIORITY 1 (FLIGH
- [SDR SWIA202266461](https://openairdocs.org/sdr/SWIA202266461.md): None · odor · Sep 12, 2022 · N744SK · Cndair CL6002C10 · Air Conditioning System
  > FLIGHT ATTENDANT REPORTED SEAT 6&7 CD CEILING LIGHT NOT WORKING AND HAS A BURNING SMELL WITHIN IT€™S AREA. (FLIGHT #3202 FILED CLOSED) REMOVED AND REPLACED CEILING LIGHT BULBS AT ROW 6/7 CD IN REFERENCE TO CRJ AMM 33-21-01. OPS CHECK GOOD AT THIS TIME. NO
- [SDR SWIA202265825](https://openairdocs.org/sdr/SWIA202265825.md): None · damaged · May 12, 2022 · N744SK · Cndair CL6002C10 · Doors
  > DURING DETAILED INSPECTION FOUND FWD BAGGAGE BAY DOOR SEALS TO BE DAMAGED. (FILED - CLOSED) REMOVED AND REPLACED FWD BAGGAGE BAY DOOR SEAL PER AMM 52-35-07. SEE CP 24814672 FOR LEAK CHECK.
- [SDR SWIA202265824](https://openairdocs.org/sdr/SWIA202265824.md): None · damaged · May 12, 2022 · N744SK · Cndair CL6002C10 · Doors
  > DURING INSPECTION OF LH OVERWING EMERGENCY EXIT DOOR PRESSURE SEAL FOUND SEAT TO BE DAMAGED BEYOND LIMITS. (FILED CLOSED) REMOVED AND REPLACED LH OVERWING EMERGENCY EXIT DOOR PRESSURE SEAL IAW AMM 52-21-07. SEE CP 24814561 FOR LEAK TEST.
- [SDR SWIA202005190762](https://openairdocs.org/sdr/SWIA202005190762.md): Structure · damaged · May 17, 2020 · N744SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CREATE A CHILD WRITE-UP TO COMPLY WITH FORM M-337, "REPORT OF AIRCRAFT MAJOR REPAIR", OR FORM M-337A "REPORT OF AIRCRAFT COMPONENT MAJOR REPAIR, ALTERATION, OR AD". / *REPAIR OF DAMAGE ON LT SIDE OF FUSELAGE BETWEEN FS 349 AND FS 364 AND BETWEEN STRG 16L AND
- [SDR SWIA2020040149841](https://openairdocs.org/sdr/SWIA2020040149841.md): Link Assy · corroded · Mar 18, 2020 · N744SK · Cndair CL6002C10 · Passenger/Crew Doors
  > "LOCKED "INDICATOR LINK ASSY FOR PAX DOOR IS CORRODED (MARKED) (C-CHECK) RO:3/29/2020REMOVED AND INSTALLED NEW SERVICEABLE PAX DOOR LOCKED INDICATOR LINK ASSEMBLY WITH EXISTING ROD-END. REF CRJ700 AMM. OPERATIONAL TEST GOOD.
- [SDR SWIA2020040149825](https://openairdocs.org/sdr/SWIA2020040149825.md): Intercostal · corroded · Mar 12, 2020 · N744SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD5- FWD HAS SIGN OF CORROSION (C-CHECK) RO:3/29/2020REMOVED AND INSTALLED PAX DOOR INTERCOSTAL DD5- FWD REF CRJ-700 SRM, CRJ-700 SRM AND BOMBARDIER DRAWING COMPLIED WITH SKYWEST TASKCARD, LEAK CHECK GOOD.
- [SDR SWIA2020040149840](https://openairdocs.org/sdr/SWIA2020040149840.md): Fitting · corroded · Mar 11, 2020 · N744SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SURROUND PROX SENSOR PX36 SLIDE FITTING CORRODED (C-CHECK) RO:3/29/2020REPLACED THE PX36 SENSOR BRACKET AND SLIDE ASSEMBLY ALONG WITH ASSOCIATED HARDWARE THAT WAS CORRODED IN THE SERVICE DOOR SURROUND. REF. CRJ700 AMM. OPS TEST PASSED.
- [SDR SWIA2020040149851](https://openairdocs.org/sdr/SWIA2020040149851.md): Coaming · cracked · Mar 9, 2020 · N744SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RH LOWER TRANSCOWL LATCH DOOR COAMING CRACKED (C-CHECK) RO:3/29/2020REPLACED RH LOWER TRANSCOWL LATCH DOOR COAMING REF REO. LATCH RIGGING GOOD
- [SDR SWIA2020040149872](https://openairdocs.org/sdr/SWIA2020040149872.md): Yoke · gouged · Mar 8, 2020 · N744SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR POWER ASSIST PULLEY BRACKET YOKE WAS GOUGE (C-CHECK) RO:3/29/2020REMOVED THE P/N 601R317107-13 PAX DOOR POWER ASSIST CABLE PULLEY YOKE, AND REPLACE IT WITH P/N 601R317107-21 AND WASHER B0202026U1724-63 AS A SET. REF CRJ700 AMM. PAX DOOR POWER
- [SDR SWIA2020040149850](https://openairdocs.org/sdr/SWIA2020040149850.md): Mount · cracked · Mar 4, 2020 · N744SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > AFT LAVATORY, FLOOR MOUNTS, BOTH (2EA) AFT MOUNTS ARE VISIBLY CRACKED AT THE BOLT HOLES (C-CHECK) RO:3/29/2020REMOVED 2 EA CRACKED AFT LAV, FLOOR MOUNTS AND INSTALLED 2 EA NEW AFT LAV FLOOR MOUNTS REF. CRJ700 SRM.

Next page: https://openairdocs.org/aircraft/N744SK/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 = 'N744SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N744SK/reports

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