# Service difficulty reports: N772SK

A list on [N772SK](https://openairdocs.org/aircraft/N772SK.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 · 165 reports

- [SDR SWIA202503240126](https://openairdocs.org/sdr/SWIA202503240126.md): Support Angle · cracked · Jan 26, 2025 · N772SK · Cndair CL6002C10 · Aerodynamic Fairings
  > CRACK AT BOTTOM OF CORNER ANGLE SUPPORT BRACKET FOR AFT FAIRING AT FS909.0 STGR 25LH. (C-CHECK RO 03/22/2024)PERFORMED REPAIR AT AFT FAIRING SUPPORT FS 909.00 LBL 17.63 IAW REO 670-53-82-478 REV -A DATED 2014-11-12PERFORMED NDT ET INSPECTION BY BARON NDT,LLC F
- [SDR SWIA202503240121](https://openairdocs.org/sdr/SWIA202503240121.md): Slat Track · damaged · Jan 21, 2025 · N772SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-1 HAS GROOVING WEAR (C-CHECK RO 03/22/2024)REPAIRED DAMAGED SLAT TRACK 3-1 ON LH WING IAW REO 670-57-42-1997 REV-- DATE 2025-02-14 AND CRJ700 SRM 51-12-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S012725-5, P.O# 175296, DATE
- [SDR SWIA202503240118](https://openairdocs.org/sdr/SWIA202503240118.md): Rib · cracked · Jan 18, 2025 · N772SK · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > LH WING LEADING EDGE RIB AT WS58.41 IS CRACKED (C-CHECK RO 03/22/2024)REPAIRED DAMAGED RIB ON LH WING LEADING EDGE AT WS58.41 IAW REO 670-57-41-610 REV-P1 DATE 2025-03-06 AND REV-- DATE 2025-03-19 AND CRJ700 SRM 57-00-01. NDT PERFORMED BY BARON NDT LLC, FAA CR
- [SDR SWIA202503240112](https://openairdocs.org/sdr/SWIA202503240112.md): Floorbeam · cracked · Jan 12, 2025 · N772SK · Cndair CL6002C10 · Fuselage Floor Panel
  > COCKPIT FLOOR BEAM AT LBL12 IS CRACKED AT F.S.280 BEAM ATTACH POINT. (C-CHECK RO 03/22/2024)PERFORMED REPAIR ON COCKPIT FLOOR BEAM LBL 12 AT FS 280.00 BEAM PER BOMBARDIER REO 670-53-11-896. REV.--. DATE 2015-03-17. CRJ-700 AMM 20-70-00. NDT PERFORMED BY BARON
- [SDR SWIA202503241205](https://openairdocs.org/sdr/SWIA202503241205.md): Skin · gouged · Dec 5, 2024 · N772SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA75762-670-53-21-2207 N772SK MXCODEID60308-PR - TEMPORARY DISPOSITION FOR BLENDED GOUGE AND DENT DAMAGE TO THE FUSELAGE UPPER SKIN AT FS349.00 AND BETWEEN STR 4L -STR 5L. COMPLIED WITH REINSPECT PER REO 670-53-21-2207.
- [SDR SWIA20241110](https://openairdocs.org/sdr/SWIA20241110.md): Actuator · failed · Nov 10, 2024 · N772SK · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > LEFT OTBD FLAP INBD FLAP ACTUATOR DUE TO L3 INDICATOR TRIPPED.(FLIGHT 6216 - FILED CLOSED) INTERROGATED MDC FOUND NO CURRENT FAULTS, IN HISTORY FOUND B1-006551 MECHANICAL JAM OF FLAP SYSTEM PER FIM 27-52-09-810-802, NO HISTORY IN LAST 30 DAYS, PERFORMED CLEAR
- [SDR SWI202409230858](https://openairdocs.org/sdr/SWI202409230858.md): Detection Sys · false indication · Sep 20, 2024 · N772SK · Cndair CL6002C10 · Fire Protection System
  > D:FOUND MT141 LEAK DETECTION LOOP TO BE DEFECTIVE AND CAUSING THE L BLEED DUCT WARNING MESSAGE. DEFERRED LOOPS A AND B OF THE LEFT BLEED AIR DETECTION LEAK SYSTEMC:MEL 36-21-6ECAT:"C" DUE 10/02/2024**** DUE TO ODI EVENT****MANAGEMENT APPROVAL IS REQUIRED VIA M
- [SDR SWIA202409230001](https://openairdocs.org/sdr/SWIA202409230001.md): Duct · warning message · Sep 20, 2024 · N772SK · Cndair CL6002C10 · Pneumatic System
  > DURING CLIMB AROUND FL 220 RECEIVED L BLEED DUCT WARNING MESSAGE (FLIGHT 4841 - FILED CLOSED) TROUBLESHOT L BEED DUCT WARNING MESSAGE PER CRJ-700 FIM 36-21-01, B1 CODE: 349537 (LOOP B 142, 29% AND 43%), 007181 (LOOP A 141, 0%). FOUND CBP-1 D7 POPPED UPO
- [SDR SWI2023F00567](https://openairdocs.org/sdr/SWI2023F00567.md): Unknown · unknown · Dec 11, 2023 · N772SK · Cndair CL6002C10 · Flight Compartment Windows
  > DURING CLIMB OUT OF SAF PASSING 16,000 THE CAPT LEFT SIDE WINDOW CRACKED, APPEARS TO BE THE OUTER PANE. RAN QRH AND PRESSURE HELD DURING FLIGHT. (FLIGHT 6348 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27543060 WITH THE FOLLOWING CORRECTIVE ACTI
- [SDR SWIA202308310027](https://openairdocs.org/sdr/SWIA202308310027.md): Unknown · uncontrollable · Aug 27, 2023 · N772SK · Cndair CL6002C10 · Stabilizer Position Indicating
  > STAB TRIM RUNAWAY IN FLIGHT. CLACKER SOUNDED, QRC / QRH RAN TROUBLESHOOT STAB TRIM SYSTEM DUE TO STAB TRIM RUNAWAY ISSUES AT NEXT MX BASE OVERNIGHT. REF EAML 1201099, 1201412,1201098.***** SMOD APPROVEL REQUIRED FOR RTS****MCI TYPE: TROUBLESHOOTING PRIORITY
- [SDR SWIA20230828007](https://openairdocs.org/sdr/SWIA20230828007.md): Unknown · uncontrollable · Aug 27, 2023 · N772SK · Cndair CL6002C10 · Stabilizer Position Indicating
  > STAB TRIM RUNAWAY IN FLIGHT. CLACKER SOUNDED, QRC / QRH RAN (FLT 4956 FILED OPEN) PLEASE REFERENCE AML 1201098 PLEASE REFERENCE AML 1201099
- [SDR SWIA202266903](https://openairdocs.org/sdr/SWIA202266903.md): Windshield · shorted · Nov 15, 2022 · N772SK · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal
  > ON CLIMB OUT AN ELECTRICAL SHORT APPEARED TO OCCUR AT THE BASE ON THE LEFT WINDSHIELD. WE HEARD A SHORTING SOUND AND SAW THICK GREY SMOKE IMMEDIATELY FROM THE BASE OF THE LEFT WINDOW. (FLIGHT 9897) FOUND LT WINDSHIELD RESISTANCE BETWEEN THE HEATER POWER TE
- [SDR SWIA202266727](https://openairdocs.org/sdr/SWIA202266727.md): None · smoke · Nov 3, 2022 · N772SK · Cndair CL6002C10 · Air Conditioning System
  > DURING DEPARTURE, HAD A FUNNY SMELL IN THE COCKPIT AND CABIN FOR ABOUT 2 MINUTES. SMELL RETURNED DURING DESCENT, ONLY STRONGER. A COUPLE OF MINUTES LATER, I SAW A SMALL PLUM OF SMOKE NEAR THE UTILITY LIGHT. WE WERE ON FINAL DECENT, AND CONTINUED TO LAND. SMELL
- [SDR SWIA202162531](https://openairdocs.org/sdr/SWIA202162531.md): None · damaged · Oct 24, 2021 · N772SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > FLOOR SEAT TRACK FROM 17AB TO 13AB AT LBL 9.0 REQUIRES REPLACEMENT TO COMPLY WITH PAX SEAT INSTALLATION. (CANNOT ENGAGE AFT INBD LEG INTO TRACK DUE TO MISSING LUGS) (C-CHECK RO 11/10/2021) REPLACED FLOOR SEAT TRACK WITH NEW (FABRICATED) TRACK REF CRJ-70
- [SDR SWIA202162518](https://openairdocs.org/sdr/SWIA202162518.md): None · corroded · Oct 11, 2021 · N772SK · Cndair CL600* · Fuselage Structure (General)
  > GUSSETT LOCATED AT APPROXIMATELY WL71, FS280 CROSSBEAM, AND LBL11 IS CORRODED (C-CHECK RO 11/10/2021) REMOVED AND REPLACED WITH NEW GUSSETT AT APPROX. WL 71.00 FS280.00 LBL11.00. REF CRJ 700 SRM 51-42-06-001-001-A01, DRAWING # CC670-33052 REV -G COMPLIED
- [SDR SWIA202162530](https://openairdocs.org/sdr/SWIA202162530.md): None · corroded · Oct 6, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *FS280 CROSSBEAM SPLICE STRIP BETWEEN APPROXIMATELY LBL12 & RBL12 IS CORRODED(MARKED) (C-CHECK RO 11/10/2021) REMOVED AND REPLACED THE CROSSBEAM SPLICE STRIP AT FS280.00 BETWEEN LBL12.00 ABD RBL 12.00. REF CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-0
- [SDR SWIA202162517](https://openairdocs.org/sdr/SWIA202162517.md): None · cracked · Oct 6, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > STRINGER CLEAT LOCATED AT FS1015, STGR18L IS CRACKED (C-CHECK RO 11/10/2021) REMOVED AND REPLACED STGR CLEAT AT FS1015 STGR18L REF CRJ700 SRM 51-42-21-001-001-A01 AND SRM 51-42-06-001-001-A01 DWG MM670-36022 REV-C. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202162516](https://openairdocs.org/sdr/SWIA202162516.md): None · cracked · Oct 6, 2021 · N772SK · Cndair CL600* · Fuselage Floor Panel
  > THE LBL 12.00, BETWEEN FS235.00 AND FS280.00 - COCKPIT FLOOR SUPPORT ANGLE IS CRACKED NEAR THE 290.00 BULKHEAD (C-CHECK RO 11/10/2021) / REMOVED AND REPLACED THE COCKPIT FLOOR SUPPORT ANGLE LBL12 BETWEEN FS235 - FS280 REF CRJ 700 SRM 51-42-06-001-001-A01
- [SDR SWIA202162515](https://openairdocs.org/sdr/SWIA202162515.md): None · cracked · Oct 6, 2021 · N772SK · Cndair CL600* · Fuselage Floor Panel
  > RBL 12.00 - COCKPIT FLOOR BEAM ANGLE IS CRACKED AT THE AFT END NEAR THE 280 B/H. (C-CHECK RO 11/10/2021) REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE AT RBL 12.00. REF: CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH STRUCTURAL MAJOR REPAIR TASK
- [SDR SWIA202162514](https://openairdocs.org/sdr/SWIA202162514.md): None · corroded · Oct 6, 2021 · N772SK · Cndair CL600* · Fuselage Main, Frame
  > *DOOR POST LOCATED AT APPROXIMATELY FS280 RBL11 CORRODED ON LOWER SECTION (MARKED) (C-CHECK RO 11/10/2021) REMOVED LIGHT CORROSION ON DOOR POST LOCATED AT APPROXIMATELY FS280 RBL11 LOWER SECTION. REF: CRJ-700 SRM 51-21-06-001-001-A01. NO MATERIAL LOSS,AND
- [SDR SWIA202162513](https://openairdocs.org/sdr/SWIA202162513.md): None · corroded · Oct 6, 2021 · N772SK · Cndair CL600* · Fuselage Main, Frame
  > *DOOR POST LOCATED AT APPROXIMATELY FS280 LBL11 CORRODED ON LOWER SECTION (MARKED) (C-CHECK RO 11/10/2021) REMOVED DAMAGED SECTION - INSTALLED NEW PORTION OF THE DOOR POST AT APPROX FS280.00 LBL11.00 LOWER MEMBER. REF CRJ 700 SRM 53-11-10-201-006-A01. COM
- [SDR SWIA2021111162512](https://openairdocs.org/sdr/SWIA2021111162512.md): Floorbeam · corroded · Oct 6, 2021 · N772SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > *CLIP LOCATED AT APPROXIMATELY WL71, FS280 CROSSBEAM, AND LBL11 IS CORRODED (MARKED) (C-CHECK RO 11/10/2021) REMOVED AND REPLACED WITH A NEW CLIP AT APPROX. WL71.00 FS 280.00 CROSSBEAM, LBL11.00 REF CRJ 700 SRM 51-42-10-001-001-A01. COMPLIED WITH STRUCTUR
- [SDR SWIA202162511](https://openairdocs.org/sdr/SWIA202162511.md): None · corroded · Oct 6, 2021 · N772SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > *FS280 FLOOR PANEL SUPPORT ANGLE CORRODED (MARKED) (C-CHECK RO 11/10/2021) REMOVED AND REPLACED WITH NEW ANGLE AT FS280.00 FOR FLOOR PANEL SUPPORT. REF CRJ 700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 BOMBARDIER DRAWING CC670-34010 REV K, DWG CC670-
- [SDR SWIA202162510](https://openairdocs.org/sdr/SWIA202162510.md): None · bent · Oct 5, 2021 · N772SK · Cndair CL600* · Fuselage Main, Keel
  > STR18L BETWEEN FS1000 - FS1015 BENT (C-CHECK RO 11/10/2021) REPLACED STGR18L SECTION P/N MM670-35118-001 REF REO 670-53-61-1971 REV --, DATED 2021-10-19, CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 551-900-
- [SDR SWIA202162509](https://openairdocs.org/sdr/SWIA202162509.md): None · cracked · Oct 5, 2021 · N772SK · Cndair CL600* · Fuselage Main, Frame
  > FRAME FS1015 LOWER FLANGE CRACKED JUST ABOVE STR18L (C-CHECK RO 11/10/2021) REPLACED FRAME FS1015 WITH NEW FRAME BETWEEN STGR19L AND FLOOR SILL REF CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG# MM670-35005 REV-AJ. NO LEAKS NOTED. COMPLIE
- [SDR SWIA202162508](https://openairdocs.org/sdr/SWIA202162508.md): None · corroded · Oct 4, 2021 · N772SK · Cndair CL600* · Fuselage Main, Bulkhead
  > AFT SIDE OF FS235 BULKHEAD MID SECTION HAS CORROSION AROUND FASTENERS AT TWO LOCATIONS. MARKED IN RED. (C-CHECK RO 11/10/2021) REMOVED CORROSION. REF CRJ 700 SRM 51-21-06-001-001-A01. PART OUT OF LIMITS. COMPLIED WITH ALL STEPS OF FINAL REO 670-53-11-174
- [SDR SWIA202162507](https://openairdocs.org/sdr/SWIA202162507.md): None · cracked · Sep 28, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > FLOOR BEAM CLIP IS CRACKED AT RBL 12, FS280 (C-CHECK RO 11/10/2021) REMOVED AND REPLACED THE CRACKED FLOOR BEAM CLIP WITH NEW PART. REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV G. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202162506](https://openairdocs.org/sdr/SWIA202162506.md): None · corroded · Sep 25, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON PASSENGER DOOR CENTER INTERCOSTAL DD6. (C-CHECK RO 11/10/2021) REMOVED AND REPLACED PAX DOOR DD6 AFT P/N: 601R318057-1 REF DRAWING# 601R31702 REV -N & CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA202162505](https://openairdocs.org/sdr/SWIA202162505.md): None · cracked · Sep 24, 2021 · N772SK · Cndair CL600* · Fuselage Floor Panel
  > COCPIT RBL 12.0 FLOOR SUPPORT BEAM POSIBLE CRACK AT FS 280. (C-CHECK RO 11/10/2021) REMOVED AND REPLACED THE SECTION OF THE FLOOR SUPPORT BEAM AT RBL12, FS280 WITH A NEW DRILLED AND LOCATED PART SECTION. REF CRJ 700 SRM 53--11-43-201-003-A01. COMPLIED
- [SDR SWIA202162535](https://openairdocs.org/sdr/SWIA202162535.md): None · damaged · Sep 17, 2021 · N772SK · Cndair CL600* · Nacelle/Pylon Structure
  > COMPLY WITH REO 670-52-11-104 REV-H DATED: 2016-08-14 / TRANSFER REPAIR DOUBLER ON NEW PAX DOOR AFT WEB (C-CHECK RO 11/10/2021) COMPLIED REO 670-52-11-104 REV-H DATED: 2016-08-14 / REMOVED AND INSTALLED REPAIR DOUBLER ON NEW PAX DOOR AFT WEB
- [SDR SWIA202162504](https://openairdocs.org/sdr/SWIA202162504.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON PASSENGER DOOR CENTER INTERCOSTAL DD2 P/N: 601R318053-3. (C-CHECK RO 11/10/2021) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD2 REF. CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG#601R31702 REV. N. COMPLIED WITH TA
- [SDR SWIA202162503](https://openairdocs.org/sdr/SWIA202162503.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON PASSENGER DOOR CENTER INTERCOSTAL DD4 P/N: 601R318081-1. (C-CHECK RO 11/10/2021) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 REF. CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG#601R31702 REV. N. COMPLIED WITH TA
- [SDR SWIA202162502](https://openairdocs.org/sdr/SWIA202162502.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION FOUND ON PASSENGER DOOR AFT FORMER AT FS347.27. P/N: 601R318034-5. (C-CHECK RO 11/10/2021) REMOVED AND REPLACED PAX DOOR AFT FORMER P/N: 601R318034-5 REF DRAWING# 601R31702 REV -N & CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK
- [SDR SWIA202162501](https://openairdocs.org/sdr/SWIA202162501.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION FOUND ON PASSENGER DOOR FRAME AT FS338.96300. P/N: 601R318033-5 (C-CHECK RO 11/10/2021) REMOVED AND REPLACED PASSENGER DOOR FRAME AT FS338.96300. P/N: 601R318033-5 REF CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-
- [SDR SWIA202162500](https://openairdocs.org/sdr/SWIA202162500.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION FOUND ON PASSENGER DOOR FWD FORMER AT FS323.00. P/N: 601R318035-5 (C-CHECK RO 11/10/2021) REMOVED AND REPLACED FWD FORMER AT S323.00 P/N 601R318035-5 REF CRJ700 SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01 AND DWG601R31702 REV -N PRESSURE
- [SDR SWIA202162499](https://openairdocs.org/sdr/SWIA202162499.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Frame
  > CORROSION FOUND ON PASSENGER DOOR FWD FORMER AT FS311.75. P/N: 601R318031-5. (C-CHECK RO 11/10/2021) REPLACED PAX DOOR FWD FORMER WITH NEW FORMER REF CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND DWG 601R31702 REV -N. NO LEAKS NOTED. COMPLIE
- [SDR SWIA202162498](https://openairdocs.org/sdr/SWIA202162498.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PASSENGER DOOR INTERCOSTAL DD2 FWD P/N: 601R318051-1. (C-CHECK RO 11/10/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD2 FWD REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# 601R31702 REV -N COMPLIED WITH TASK CARD 51-900-1002-SKY PRESSURE LE
- [SDR SWIA202162497](https://openairdocs.org/sdr/SWIA202162497.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PASSENGER DOOR INTERCOSTAL DD3 FWD P/N: 601R318054-1. (C-CHECK RO 11/10/2021) REPLACED PAX DOOR INTERCOSTAL DD3 WITH NEW INTERCOSTAL REF CRJ-700 SRM 51-42-06-001-001-A01, AND DWG 601R31702 REV -N. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-9
- [SDR SWIA202162496](https://openairdocs.org/sdr/SWIA202162496.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PASSENGER DOOR INTERCOSTAL DD5 AFT P/N: 601R31902-317. (C-CHECK RO 11/10/2021) REMOVED AND REPLACED PAX DOOR DD5 AFT P/N: 601R31902-317 REF DRAWING# 601R31702 REV -N & CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-90
- [SDR SWIA202162495](https://openairdocs.org/sdr/SWIA202162495.md): None · corroded · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > CORROSION ON PASSENGER DOOR INTERCOSTAL DD4 AFT P/N: 601R31902-317. (C-CHECK RO 11/10/2021) REMOVED AND REPLACED PAX DOOR DD4 AFT P/N: 601R31902-317 REF DRAWING# 601R31702 REV -N & CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-90
- [SDR SWIA202162494](https://openairdocs.org/sdr/SWIA202162494.md): None · cracked · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR INTERCOSTAL DD1 P/N 601R31902-318 IS CRACK ON TOP FLANGE.REMOVED AND REPLACED PAX DOOR AFT INTERCOSTAL DD1 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG# 601R31702 REV -N COMPLIED WITH TASK CARD 51-900-1002-SKY PRESSURE LEAK CHECK OF REPAIR AREA G
- [SDR SWIA202162493](https://openairdocs.org/sdr/SWIA202162493.md): None · cracked · Sep 16, 2021 · N772SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > PASSENGER DOOR INTERCOSTAL DD7 P/N 601R318825-1 IS CRACK ON TOP FLANGE. (C-CHECK RO 11/10/2021) REMOVED AND REPLACED PASSENGER DOOR INTERCOSTAL DD7 P/N 601R318825-1 REF DRAWING# 601R31702 REV -N & CRJ 700 SRM 51-42-06-001-001-A01. COMPLIED WITH SKYWEST T
- [SDR SWIA202162492](https://openairdocs.org/sdr/SWIA202162492.md): None · cracked · Sep 16, 2021 · N772SK · Cndair CL600* · Ice/Rain Protection System
  > UPON FURTHER INSPECTION FOUND L/H AFT DRAG ANGLE JUST BELOW VERT. STAB. FS1220 - 67.5% CRACKED (MARKED) (C-CHECK RO 11/10/2021) REMOVED CRACKED AND INSTALLED NEW LH AFT DRAG ANGLE JUST BELOW VERTICAL STAB FS1220-67.5%, REF CRJ 700 SRM 51-42-13-001-001-A01
- [SDR SWIA202162491](https://openairdocs.org/sdr/SWIA202162491.md): None · cracked · Sep 16, 2021 · N772SK · Cndair CL600* · Empennage Structure
  > UPON FURTHER INSPECTION FOUND R/H AFT DRAG ANGLE JUST BELOW VERT. STAB. FS1220 - 67.5% CRACKED (MARKED) (C-CHECK RO 11/10/2021) REMOVED AND REPLACED THE RH AFT DRAG ANGLE ON THE VERT STAB FS1220 - 67.5% REF DRAWING AV670-21186 REV F, CRJ700 SRM 51-42-22-0
- [SDR SWIA202162534](https://openairdocs.org/sdr/SWIA202162534.md): None · cracked · Sep 14, 2021 · N772SK · Cndair CL600* · Fuselage Structure (General)
  > SUSPECTED CRACK ON PASSENGER DOOR AFT DRAG ANGLE NEAR POWER ASSIST MOTOR BRACKET ASSY. (C-CHECK RO 11/10/2021) FABRICATED AND REPLACED ANGLE SECTION OF THE CRACKED AFT DRAG ANGLE ON THE PAX DOOR REF CRJ700 SRM 52-11-04-201-002-A01 REPAIR TYPE 2. RESTORED
- [SDR SWIA202162529](https://openairdocs.org/sdr/SWIA202162529.md): None · worn · Sep 13, 2021 · N772SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > SLAT TRACK 3-2 FWD INBD, AFT INBD, FWD OUTBD, AND AFT OUTBD SIDE ROLLERS WORN/STIFF. (C-CHECK RO 11/10/2021) INSTALLED NEW SERVICEABLE LH WING SLAT TRACK 3-2 FWD INBD, AFT INBD, FWD OUTBD, AND AFT OUTBD SIDE ROLLERS REF CRJ700 AMM 27-81-44-400-803-A01 CH
- [SDR SWIA202162528](https://openairdocs.org/sdr/SWIA202162528.md): None · worn · Sep 13, 2021 · N772SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > SLAT TRACK 2-2 FWD INBD, AFT INBD, FWD OUTBD, AND AFT OUTBD SIDE ROLLERS WORN/STIFF. (C-CHECK RO 11/10/2021) INSTALLED NEW SERVICEABLE LH WING SLAT TRACK 2-2 FWD INBD, AFT INBD, FWD OUTBD, AND AFT OUTBD SIDE ROLLERS REF CRJ700 AMM 27-81-44-400-802-A01, CH
- [SDR SWIA202162527](https://openairdocs.org/sdr/SWIA202162527.md): None · worn · Sep 13, 2021 · N772SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > SLAT TRACK 1-2 FWD INBD, AFT INBD, FWD OUTBD, AND AFT OUTBD SIDE ROLLERS WORN/STIFF. (C-CHECK RO 11/10/2021) INSTALLED NEW SERVICEABLE LH SLAT TRACK 1-2 FWD INBD, AFT INBD, FWD OUTBD, AND AFT OUTBD SIDE ROLLERS, REF. CRJ700 AMM 27-81-44-400-801-A01, CHEC
- [SDR SWIA202162526](https://openairdocs.org/sdr/SWIA202162526.md): None · worn · Sep 13, 2021 · N772SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > RH WING SLAT TRACK 3-2 FWD INBOARD AND AFT INBOARD SIDE ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11/10/2021) INSTALLED NEW RH WING SLAT TRACK 3-2 FWD I/B AND AFT I/B SIDE ROLLERS PER CRJ 700 AMM 27-81-44-400-803-A01, ALL CHECKS GOOD AT THIS TIME.
- [SDR SWIA202162525](https://openairdocs.org/sdr/SWIA202162525.md): None · worn · Sep 13, 2021 · N772SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > RH WING SLAT TRACK 2-2 FWD OUTBOARD AND AFT OUTBOARD SIDE ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11/10/2021) RH WING SLAT TRACK 2-2 FWD OUTBOARD AND AFT OUTBOARD SIDE ROLLERS REMOVED & INSTALLED NEW SERVICEABLE PARTS. REF CRJ 700 AMM 27-81-44-400-802 A01,

Next page: https://openairdocs.org/aircraft/N772SK/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 = 'N772SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N772SK/reports

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