# Service difficulty reports: N773SK

A list on [N773SK](https://openairdocs.org/aircraft/N773SK.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 4 · 160 reports

- [SDR SWIA2026012675098](https://openairdocs.org/sdr/SWIA2026012675098.md): Rib · damaged · Jan 26, 2026 · N773SK · Cndair CL6002C11 · Wing, Rib/Bulkhead
  > DAMAGE ON THE LT WING CANTED RIB LOCATED AT WS398.93 WAS FOUND TO BE OUT OF LIMITS PER SRM 57-21-12. DAMAGE IS OUT OF LIMITS AND THE REPLACEMENT OF THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR REPAIR. REMOVED AND REPLACED THE LT CANTED RIB AT
- [SDR SWIA2025102000017](https://openairdocs.org/sdr/SWIA2025102000017.md): Hinge · damaged · Oct 17, 2025 · N773SK · Cndair CL6002C11 · Fuselage, Door Hinge
  > FOUND PAX DOOR HINGE (FUSELAGE SIDE) HAS SEVERAL LUGS WITH INNER SURFACE WEAR DAMAGE. (FILED CLOSED)COMPLIED WITH REO 670-53-21-2718 DATED: 2025-10-17 REV -- TEMPORARY DISPOSITION FOR WEAR DAMAGE TO PASSENGER DOOR HINGE LUGS (FUSELAGE SIDE). COMPLIED WITH T
- [SDR SWIA20250813007](https://openairdocs.org/sdr/SWIA20250813007.md): Windshield · cracked · Aug 7, 2025 · N773SK · Cndair CL6002C11 · Flight Compartment Windows
  > CAPTAIN WINDSHIELD CRACKED (FLIGHT 5844 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 30628908 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH TASK CARD 56-220-1000-SKY (CL600-2C11) CRJ-550 COCKPIT WINDSHIELD/SIDE WINDOW INSTALLATION. OPS
- [SDR SWIA2025080800007](https://openairdocs.org/sdr/SWIA2025080800007.md): Windshield · cracked · Aug 7, 2025 · N773SK · Cndair CL6002C11 · Flight Compartment Windows
  > CAPTAIN WINDSHIELD CRACKED (FLIGHT 5844) THIS IS CURRENTLY A WORK IN PROGRESS.
- [SDR SWIA202265905](https://openairdocs.org/sdr/SWIA202265905.md): None · cracked · Jun 7, 2022 · N773SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > WHILE PERFORMING DETAILED VISUAL INSPECTION OF THE BULKHEAD WEBS FS202.75 AND FS235, THE FLOOR WEBBING DIRECTLY BELOW THE ADG RESTOW PUMP WAS FOUND TO BE CRACKED BEYOND LIMITS OF SRM 53-11-43, AND HAS BEEN DETERMIND TO BE A MAJOR REPAIR. REF CP 24911707 FOR O
- [SDR SWIA202265835](https://openairdocs.org/sdr/SWIA202265835.md): None · cracked · May 31, 2022 · N773SK · Cndair CL6002C10 · Ventral Structure
  > CRACK FOUND ON THE RH AFT DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT FWD EDGE OF RH AFT DRAG ANGLE AND EXTENDS APROX. 0.281" AFT IN THE CORNER OF THE ANGLE. DAMAGE IS OUT OF LIMITS PER SRM 55-31-00. / HAS BEEN DETERMINED TO BE A M
- [SDR SWIA202265834](https://openairdocs.org/sdr/SWIA202265834.md): None · cracked · May 31, 2022 · N773SK · Cndair CL6002C10 · Ventral Structure
  > CRACK FOUND ON THE LH AFT DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT FWD EDGE OF LH AFT DRAG ANGLE AND EXTENDS APROX. 0.7515" AFT IN THE CORNER OF THE ANGLE. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 55-31-00. / IT HAS BEEN DETERMI
- [SDR SWIA202265833](https://openairdocs.org/sdr/SWIA202265833.md): None · cracked · May 31, 2022 · N773SK · Cndair CL6002C10 · Ventral Structure
  > CRACK FOUND ON THE LH FWD DRAG ANGLE ON THE VERTICAL STAB TO EMPENAGE ATTACHMENT. CRACK STARTS AT AFT EDGE OF THE LH FWD DRAG ANGLE AND EXTENDS APROX. 2.115" FWD IN THE CORNER OF THE ANGLE. DAMAGE IS OUT OF LIMITS PER SRM 55-31-00. IT HAS BEEN DETERMINED TO BE
- [SDR SWIA202265924](https://openairdocs.org/sdr/SWIA202265924.md): None · cracked · May 30, 2022 · N773SK · Cndair CL6002C10 · Fuselage Structure (General)
  > DURING GVI AFTER A HIGH LOAD LANDING EVENT ( AMM 05-51-01) SUBTASK B., FOUND LH OVERWING WING TO FUSELAGE FAIRING PANEL 171CL TO HAVE A CRACK IN THE PANEL RUNNING THROUGH A RIVET HOLE OF THE LOWER AFT STIFFNER. (FILED CLOSED)REMOVED AND REPLACED LH OVERWING
- [SDR SWIA202163278](https://openairdocs.org/sdr/SWIA202163278.md): None · blocked · Dec 7, 2021 · N773SK · Cndair CL600* · Fuselage Main, Frame
  > REMOVE LOWER SECTOR FRAME AT FS319.70 TO F.O.M (C-CHECK RO 12/26/2021) REMOVED LOWER SECTOR FRAME AT FS319.70 BETWEEN STRG 25L TO STGR 23R TO FOM. REF CRJ-700 SRM 51-42-06-001-001-A01. / AND INSTALLED SAME LOWER SECTOR FRAME WITH NEW SPLICE AT FS319.7
- [SDR SWIA202163277](https://openairdocs.org/sdr/SWIA202163277.md): None · gouged · Dec 6, 2021 · N773SK · Cndair CL600* · Wing Spar
  > * LEFT WING REAR SPAR AT APPROX. WS 58.00, HAS GOUGE ( PREVIOUS DAMAGE) ON SPAR INBOARD OF INBOARD GROUND SPOILER ACTUATOR ROD ATTACHMENT POINT. (C-CHECK RO 12/26/2021) COMPLIED WITH REO MHIRJ REO 670-57-51-469 REV --, DATED: 2021-12-12 REPAIR FOR LH W
- [SDR SWIA2021122963276](https://openairdocs.org/sdr/SWIA2021122963276.md): Channel · corroded · Dec 5, 2021 · N773SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > TCAS OMNIDIRECTIONAL ANTENNA CHANNEL IS CORRODED (C-CHECK RO 12/26/2021) REMOVED AND REPLACED TCAS OMNIDIRECTIONAL ANTENNA CHANNEL WITH NEW SERVICEABLE CHANNEL ASSY. P/N:SH670-32364-5 REF DRAWING SH670-30023 REV G DATED 2017/06/14 AND CRJ 700 SRM 51-42
- [SDR SWIA202163275](https://openairdocs.org/sdr/SWIA202163275.md): None · corroded · Dec 5, 2021 · N773SK · Cndair CL600* · Fuselage Structure (General)
  > A-BAY STGR 27 FS280-FS310 CORRODED (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW A-BAY NEW STGR 27 FS280-FS310 REF CRJ700 SRM 51-42-21-001-001-A01,CRJ700 SRM 51-42-06-001-001-A01,DWG#SH670-31630 REV K COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SK
- [SDR SWIA202163274](https://openairdocs.org/sdr/SWIA202163274.md): None · corroded · Dec 2, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL AT STRINGER 20R FS349.00 €“ 364.00 HAS CORROSION. (C-CHECK RO 12/26/2021) EVALUATED CORROSION ON INTERCOSTAL AT STRINGER 20R FS349.00 €“ FS364.00 FOUND TO BE OUT OF LIMITS, CORROSION EXCEEDS 30% OF OVERALL LENGTH REF. CRJ700 SRM 53-00-00-
- [SDR SWIA202163273](https://openairdocs.org/sdr/SWIA202163273.md): None · dented · Dec 1, 2021 · N773SK · Cndair CL600* · Fuselage Structure (General)
  > UPON REMOVAL OF STRINGER FOUND DENT PROTRUDING ON FUSELAGE SKIN AT FS319.70 TO FS333.00 STRINGER 25R. (C-CHECK RO 12/26/2021) EVALUATED DENT AT STRINGER 25R BETWEEN FS319.70 TO FS333.00. DENT MEASURES 6.20€? L 0.013€? D AND 0.20€? W. WITH A W/D RA
- [SDR SWIA202163272](https://openairdocs.org/sdr/SWIA202163272.md): None · corroded · Nov 24, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 INTERCOSTAL (C-CHECK RO 12/26/2021) PAX DOOR FRAME FS313.56 BETWEEN DD4 AND DD5 INTERCOSTAL HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV.
- [SDR SWIA202163271](https://openairdocs.org/sdr/SWIA202163271.md): None · corroded · Nov 23, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > RH FLOOR SILL BETWEEN FS 280-FS319.70 HAS SEVERAL SPOTS OF CORROSION (C-CHECK RO 12/26/2021) INSTALLED NEW RH FLOOR SILL BETWEEN FS 280-FS319.70 REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND D
- [SDR SWIA2021122963270](https://openairdocs.org/sdr/SWIA2021122963270.md): Support · corroded · Nov 22, 2021 · N773SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT HAND NOSE JACKING SUPPORT AT APPROX. FS 265.00 TO FS 280.00 IS CORRODED. (C-CHECK RO 12/26/2021) EVALUATED CORROSION ON RIGHT HAND NOSE JACKING SUPPORT FS265.00 - FS280.00. OUT OF LIMITS. DAMAGE IS ON MORE THAN ONE ELEMENT. SKIN ATTACH ELEMENT AND
- [SDR SWIA202163269](https://openairdocs.org/sdr/SWIA202163269.md): None · gouged · Nov 21, 2021 · N773SK · Cndair CL600* · Fuselage Main, Frame
  > APPROXIMATELY FS333 & FS349 BETWEEN STGR 21R AND STGR 19R BELOW SERVICE DOOR HAS PREVIOUS POSSIBLE DENT/GOUGED PAINTED REQUIRES EVALUATION AND REPAIR (C-CHECK RO 12/26/2021) COMPLIED WITH DOUBLER REPAIR TO SKIN LAP JOINT BETWEEN FS333-FS364 AND STG 18
- [SDR SWIA202163268](https://openairdocs.org/sdr/SWIA202163268.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION ON UNION SPLICE AT STR 25R BETWEEN FS 319.70 AND FS 349.00 (C-CHECK RO 12/26/2021) REPLACED UNION SPLICE AT STR 25R BETWEEN FS 319.70 AND FS 349.00 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. COMPLIED WITH SKYWEST TASK CAR
- [SDR SWIA202163267](https://openairdocs.org/sdr/SWIA202163267.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Keel
  > CORROSION ON STR 25R BETWEEN FS 319.70 AND FS 333.00 (C-CHECK RO 12/26/2021) INSTALLED NEW STRINGER 25R PN SH670-31212-2 FS280.00 - FS333.00 CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 & DRAWING SH670-31630 REV. K, DATED 2017/11/2
- [SDR SWIA202163266](https://openairdocs.org/sdr/SWIA202163266.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Keel
  > CORROSION ON STRG 26L BETWEEN FS 319.70 TO FS 333.00 (C-CHECK RO 12/26/2021) REPLACED STRG 26L FROM FS 280.00 TO FS333.00 REF DWG SH670-31630 REV K,CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 LEAK CHECK GOOD COMPLIED WITH SKYWE
- [SDR SWIA202163265](https://openairdocs.org/sdr/SWIA202163265.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Structure (General)
  > CORROSION ON PAX DOOR FRAME FS327.763 BETWEEN INTERCOSTAL DD6 AND DD7A (C-CHECK RO 12/26/2021) PAX DOOR FRAME FS327.763 BETWEEN INTERCOSTAL DD6 AND DD7A HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010
- [SDR SWIA202163264](https://openairdocs.org/sdr/SWIA202163264.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL DD7A (C-CHECK RO 12/26/2021) REMOVED CORRODED PAX DOOR INTERCOSTAL DD7A AND INSTALLED NEW PAX DOOR INTERCOSTAL DD7A REF CRJ 700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG 601R31702 REV N. COMPLIED WITH SKYWEST TASK CARD 51-900-
- [SDR SWIA202163263](https://openairdocs.org/sdr/SWIA202163263.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL DD6 MID (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL MID DD6 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED PAX DOOR INTERCOSTAL DD6 MID REF
- [SDR SWIA202163262](https://openairdocs.org/sdr/SWIA202163262.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION IN INTERCOSTAL DD4 AFT (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL AFT DD4 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DD
- [SDR SWIA202163260](https://openairdocs.org/sdr/SWIA202163260.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL DD4 FWD (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL FWD DD4 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DD
- [SDR SWIA202163259](https://openairdocs.org/sdr/SWIA202163259.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL DD3 AFT (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL AFT DD3 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DD
- [SDR SWIA202163258](https://openairdocs.org/sdr/SWIA202163258.md): None · corroded · Nov 19, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOTAL DD2 MID (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL MID DD2 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED FS 329.50 CORRODED INTERCOSTAL D
- [SDR SWIA202163257](https://openairdocs.org/sdr/SWIA202163257.md): None · corroded · Nov 18, 2021 · N773SK · Cndair CL600* · Doors
  > PAX DOOR LOWER SILL CLOSING FITTING AT FS314.00 HAS INTERGRANULAR CORROSION IN MULTIPLE LOCATIONS. (C-CHECK RO 12/26/2021) FOUND PAX DOOR LOWER SILL CLOSING FITTING OUT OF LIMIT, REPLACED WITH NEW PN SH670-31840-3 PO# T-62897 REF CRJ 700 SRM 51-42-06-0
- [SDR SWIA2021122963256](https://openairdocs.org/sdr/SWIA2021122963256.md): Angle · corroded · Nov 18, 2021 · N773SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER SILL KICKPLATE ANGLE HAS INTERGRANULAR CORROSION IN SEVERAL LOCATIONS. (C-CHECK RO 12/26/2021) FOUND PAX DOOR LOWER SILL KICKPLATE ANGLE OUT OF LIMIT, REPLACED WITH NEW PN SH670-31875-7 PO# T-62190 REF CRJ 700 SRM 51-42-06-001-001-A01 AN
- [SDR SWIA202163255](https://openairdocs.org/sdr/SWIA202163255.md): None · corroded · Nov 18, 2021 · N773SK · Cndair CL600* · Doors
  > PAX DOOR LOWER SILL MID CAP ANGLE HAS INTERGRANULAR CORROSION AROUND SEVERAL SCREW HOLES. (C-CHECK RO 12/26/2021) FOUND PAX DOOR LOWER SILL MID CAP ANGLE OUT OF LIMIT, REPLACED WITH NEW PN SH670-31825-9 PO# 10236-0015 REF CRJ 700 SRM 51-41-02-001-001-A
- [SDR SWIA202163254](https://openairdocs.org/sdr/SWIA202163254.md): None · cracked · Nov 17, 2021 · N773SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > RH WING SLAT TRACK CANISTER 1-3 CRACKED (C-CHECK RO 12/26/2021) COMPLIED WITH REPAIR ON THE RH SLAT TRACK CANISTER 1-3 PER BOMBARDIER REO 670-57-42-577 REV -- DATED 2016-12-02, COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY, LEAK CHECK GOOD AND OPS TES
- [SDR SWIA202163253](https://openairdocs.org/sdr/SWIA202163253.md): None · damaged · Nov 16, 2021 · N773SK · Cndair CL600* · Rudder, Spar/Rib
  > R/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING BORE IS PITTED (C-CHECK RO 12/26/2021) REMOVED AND REPLACED R/H AILERON AFT SPAR #2 I/B HINGE FITTING BUSHING. COMPLIED WITH REO 670-57-51-464 REV-- DATED 2021-11-24. / COMPLIED WITH SKYWEST TASKCARD 51-
- [SDR SWIA202163252](https://openairdocs.org/sdr/SWIA202163252.md): None · cracked · Nov 16, 2021 · N773SK · Cndair CL600* · Doors
  > PAX DOOR AFT FORMER FS347.25 CRACK (C-CHECK RO 12/26/2021) REMOVED CRACK AFT FORMER FS347.25 REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED NEW PAX DOOR AFT FORMER AT FS 347.7 PN 601R318034 -5 REF CRJ 700 SRM 51-42
- [SDR SWIA202163251](https://openairdocs.org/sdr/SWIA202163251.md): None · worn · Nov 13, 2021 · N773SK · Cndair CL600* · Rudder/Tab, Attach Fittings
  > RUDDER VERTICAL STABILIZER CENTER UPPER HINGE BEARING WORN (C-CHECK RO 12/26/2021) REMOVED CENTER RUDDER HINGE, UPPER HINGE AND DISASSEMBLED FITTING BY REMOVING FASTENERS AND REMOVED OLD BEARING, REASSEMBLED FITTING WITH NEW FASTENERS AND INSTALLED NEW
- [SDR SWIA202163250](https://openairdocs.org/sdr/SWIA202163250.md): None · corroded · Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Main, Frame
  > * FITTING AT APPROX. STGR18R FS319.70 CORRODED (C-CHECK RO 12/26/2021) REPLACED OUT OF LIMITS FITTING WITH NEW FITTING AT APPROX STGR 18R FS319.70 REF. CRJ700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-31950 REV Y COMPLIED WITH SKYWEST TASK CARD 51-900
- [SDR SWIA202163249](https://openairdocs.org/sdr/SWIA202163249.md): None · corroded · Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > * BACK UP SILL AT STGR21L FS333-FS349 CORRODED (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW REPLACEMENT BACK UP SILL (P/N SH670-31823-1S) ONTO STGR21L BETWEEN FS333.00 AND FS349.00 USING ALL NEW HARDWARE. REF BOMBARDIER DWG# SH670-31810 REV Y AND
- [SDR SWIA202163248](https://openairdocs.org/sdr/SWIA202163248.md): None · corroded · Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > * BACK UP SILL AT STGR21L FS310-FS333 CORRODED (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW REPLACEMENT BACK UP SILL (P/N SH670-31822-1S) ONTO STGR21L BETWEEN FS310.00 AND FS333.00 USING ALL NEW HARDWARE. REF BOMBARDIER DWG# SH670-31810 REV Y AND
- [SDR SWIA202163247](https://openairdocs.org/sdr/SWIA202163247.md): None · corroded · Nov 13, 2021 · N773SK · Cndair CL600* · Fuselage Main, Frame
  > * FS319.70 FRAME BETWEEN STGR18L-STGR21L CORRODED (C-CHECK RO 12/26/2021) REMOVED CORRODED FRAME AT FS319.70 BETWEEN STGR'S 18L AND 21L. REF CRJ700 SRM'S 51-42-06-001-001 A01 AND 51-42-21-001-001 A01.INSTALLED NEW REPLACEMENT FRAME (P/N# SH670-31891-3S)
- [SDR SWIA202163246](https://openairdocs.org/sdr/SWIA202163246.md): None · dented · Nov 12, 2021 · N773SK · Cndair CL600* · Aileron Tabs
  > *DENT ON LH OTBD FLAP LOWER EXTERNAL SKIN, LOCATED ON LOWER OTBD CORNER (C-CHECK RO 12/26/2021) REPAIRED DENT DAMAGE ON LH OTBD FLAP LOWER EXTERNAL SKIN, LOCATED ON LOWER OTBD CORNER PER CRJ 700 SRM 57-53-01-201-001-A01 REV 38 DATED JUL 25 2020 TYPE II
- [SDR SWIA202163245](https://openairdocs.org/sdr/SWIA202163245.md): None · corroded · Nov 12, 2021 · N773SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > *FLOOR PANEL SUPPORT ANGLE IS CORRODED. LOCATED @FS280.00, WL72.50 BETWEEN LBL9.00 AND RBL9.00 (C-CHECK RO 12/26/2021) INSTALLED NEW FLOOR SUPPORT ANGLE PN CC670-34095-1 AT FS280 BETWEEN LBL9 - RBL9 REF BOMBARDIER DWG CC670-33052 REV -G, CRJ700 SRM 51-
- [SDR SWIA202163244](https://openairdocs.org/sdr/SWIA202163244.md): None · worn · Nov 11, 2021 · N773SK · Cndair CL600* · Engine Exhaust System
  > *RH UPPER TRANSCOWL HAS WEAR ON COAMING. AREAS MARKED (C-CHECK RO 12/26/2021) REMOVED WORN COAMING FROM THE RH UPPER TRANSCOWL, REF CRJ700 SRM 51-42-13-001-001 A01. INSTALLED NEW REPLACEMENT COAMING (P/N CN624-2061-205) ONTO RH UPPER TRANSCOWL USING ALL
- [SDR SWIA202163243](https://openairdocs.org/sdr/SWIA202163243.md): None · corroded · Nov 11, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *CORROSION ON INTERCOSTAL MID DD4 (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL MID DD4 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR DD4 MID SECTI
- [SDR SWIA202163242](https://openairdocs.org/sdr/SWIA202163242.md): None · corroded · Nov 11, 2021 · N773SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *CORROSION ON INTERCOSTAL FWD DD3 (C-CHECK RO 12/26/2021) PAX DOOR INTERCOSTAL FWD DD3 HAS CORROSION ON MORE THAN ONE ELEMENT. OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO 670-52-11-010 REV. NC DATED 2002-02-25. REMOVED CORRODED PAX DOOR INTERCOSTAL DD
- [SDR SWIA202163241](https://openairdocs.org/sdr/SWIA202163241.md): None · corroded · Nov 11, 2021 · N773SK · Cndair CL600* · Doors
  > *AREAS OF CORROSION ON PAX DOOR FWD FRAME FS 311.75 (C-CHECK RO 12/26/2021) PAX DOOR FWD FRAME/FORMER FS311.75 HAS CORROSION ON MORE THAN ONE ELEMENT AT A GIVEN CROSS-SECTION. FOUND OUT OF LIMIT REF CRJ 200 SRM 52-00-00 AND REO670-52-11-010 REV.NC DATED
- [SDR SWIA202163240](https://openairdocs.org/sdr/SWIA202163240.md): None · worn · Nov 10, 2021 · N773SK · Cndair CL600* · Engine Exhaust System
  > *LH LOWER TRANSCOWL HAS WEAR ON COAMING LEADING EDGE (C-CHECK RO 12/26/2021) REMOVED WORN COAMING FROM LH LOWER TRANSCOWL. REF CRJ700 SRM 51-42-13-001-001 A01. INSTALLED WITH NEW COAMING (P/N CN624-2061-205) ONTO LH LOWER TRANSCOWL USING NEW HARDWARE R
- [SDR SWIA202163239](https://openairdocs.org/sdr/SWIA202163239.md): None · worn · Nov 10, 2021 · N773SK · Cndair CL600* · Engine Exhaust System
  > *LH LOWER TRANSCOWL HAS WEAR ON OTBD LEADING EDGE INNER SKIN (C-CHECK RO 12/26/2021) COMPLIED WITH REO 670-54-21-1485 REV -- DATED 2021-11-30 REPAIR TO LH LOWER TRANSCOWL WEAR ON OTBD LEADING EDGE INNER SKIN COMPLIED WITH SKYWEST TACK CARD 51-900-1002-S
- [SDR SWIA202163238](https://openairdocs.org/sdr/SWIA202163238.md): None · cracked · Nov 6, 2021 · N773SK · Cndair CL600* · Doors
  > AFT CARGO DOOR HANDLE HOUSING HAS SUSPECT CRACK (MARKED) (C-CHECK RO 12/26/2021) REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE ASSY (PN H3415-13) IN REF TO CRJ700 AMM 52-31-03-400-801-A01 AND DWG CC670-38702 REV -C. OPS TEST GOOD. HEALTH MONITORING CH
- [SDR SWIA202163279](https://openairdocs.org/sdr/SWIA202163279.md): None · chafed · Nov 5, 2021 · N773SK · Cndair CL600* · Ailerons
  > *LEFT WING INBOARD FLAP VANE €“ PANEL 584ET IS CHAFED. (C-CHECK RO 12/26/2021) LH WING INBD FLAP VANE PANEL 584ET DAMAGE BLENDED TO A SMOOTH CONTOUR UPON EVALUATION PANEL WAS FOUND TO BE OUT OF LIMITS PANEL WAS REPLACED WITH NEW PART.CRJ700 SRM 51-12-0

Next page: https://openairdocs.org/aircraft/N773SK/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 = 'N773SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N773SK/reports

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