# Service difficulty reports: N774SK

A list on [N774SK](https://openairdocs.org/aircraft/N774SK.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 · 145 reports

- [SDR SWI2025F00615](https://openairdocs.org/sdr/SWI2025F00615.md): Slat Track · grooved · Mar 10, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 1-3 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)PERFORMED REPAIR ON LH SLAT TRACK 1-3 PER MHIRJ REO 670-57-42-2044. REV.--. DATE: 2025-04-07. CRJ-700 SRM 51-12-00. CRJ-700 AMM 12-20-27. NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D. R
- [SDR SWI2025F00614](https://openairdocs.org/sdr/SWI2025F00614.md): Slat Track · grooved · Mar 10, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 1-1 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)REPAIRED DAMAGE TO LH SLAT TRACK 1-1 IAW CRJ700 SRM 51-12-00 AND REO 670-57-42-2061 REV-- DATE 2025-04-15. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S032525-3, P.O# 176016, DA
- [SDR SWI2025F00613](https://openairdocs.org/sdr/SWI2025F00613.md): Slat Track · grooved · Mar 10, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 1-1 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)PERFORMED REPAIR ON RH SLAT TRACK 1-1 PER MHIRJ REO 670-57-42-2046. REV.--. DATE: 2025-04-07. CRJ-700 SRM 51-12-00. NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D. REPORT # S041125-9. P.
- [SDR SWIA20250430010](https://openairdocs.org/sdr/SWIA20250430010.md): Slat Track · grooved · Mar 10, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 1-3 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)REPAIRED DAMAGED ON RH SLAT TRACK 1-3 IAW CRJ700 SRM 51-12-00, AMM 12-20-27 AND REO 670-57-42-2049 REV-- DATE 2025-04-09. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S041125-13,
- [SDR SWIA20250430009](https://openairdocs.org/sdr/SWIA20250430009.md): Angle · cracked · Mar 9, 2025 · N774SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE FAIRING DIAPHRAM AT FS909.00 ON LH SIDE IS CRACKED (C-CHECK RO 04/30/2025)REPAIRED DAMAGE ON AFT FUSELAGE FAIRING DIAPHRAGM AT FS909.00 ON L/H SIDE IAW BOMBARDIER REO 670-53-82-478 REV.-A DATE: 2014-11-12, CRJ700 SRM 51-40-11, 51-21-11, 51-25-06,
- [SDR SWI2025F00621](https://openairdocs.org/sdr/SWI2025F00621.md): Slat Track · grooved · Mar 6, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 3-1 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)PERFORMED REPAIR AT SLAT TRACK 3-1 RH WING,REWORKED AREA OF SLAT TRACK 3-1 FOUND TO BE WITH IN LIMITS IAW REO 670-57-42-2057 REV -- DATED 2025-04-14,CRJ 700 AMM 57-42-26,SRM 51-12-00PERFORMED
- [SDR SWI2025F00620](https://openairdocs.org/sdr/SWI2025F00620.md): Slat Track · grooved · Mar 6, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 2-2 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)PERFORMED REPAIR ON R/H SLAT TRACK 2-2 PER MHIRJ REO-670-57-42-2060 REV- - DATED 2025-04-14, CALIBRATED TOOL: DIGITAL CALIPER AV-7805 DUE DATE JAN-26, DEPTH GAUGE AJ-1511 DUE DATE SEP-2025 AND
- [SDR SWI2025F00619](https://openairdocs.org/sdr/SWI2025F00619.md): Slat Track · grooved · Mar 6, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 2-1 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)PERFORMED REPAIR AREA ON RH SLAT TRACK2-1 IAW MHI RJ REO 670-57-42-2059 REV-- DATE: 2025-01-21, CRJ700 AMM 57-42-26, CRJ700 SRM 51-12-00, PERFORMED INSPECTION BY BARON NDT, LLC FAA CRS#5NDR545
- [SDR SWI2025F00618](https://openairdocs.org/sdr/SWI2025F00618.md): Slat Track · grooved · Mar 6, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-1 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)PERFORMED REPAIR AT SLAT TACK 3-1,FOUND TO BE WITH IN LIMITS IAW REO 670-57-42-2064 REV -- DATED 2025-04-21,CRJ 700 SRM 51-12-00PERFORMED NDT PT INSPECTION BY BARON NDT,LLC FAA CRS#5NDR545D,RE
- [SDR SWI2025F00617](https://openairdocs.org/sdr/SWI2025F00617.md): Slat Track · grooved · Mar 6, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-2 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)REPAIRED DAMAGED LH SLAT TRACK 3-2 IAW CRJ700 SRM 51-12-00 AND REO 670-57-42-2045 REV-- DATE 2025-04-08. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S042325-2, P.O# 176374, DATE
- [SDR SWI2025F00616](https://openairdocs.org/sdr/SWI2025F00616.md): Slat Track · grooved · Mar 6, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-3 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)REPAIRED DAMAGE TO LH SLAT TRACK 3-3 IAW CRJ700 SRM 51-12-00 AND REO 670-57-42-2047 REV-- DATE 2025-04-08. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S041425-3, P.O# 176374, DAT
- [SDR SWIA20250430006](https://openairdocs.org/sdr/SWIA20250430006.md): Slat Track · grooved · Mar 6, 2025 · N774SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 3-2 HAS GROOVE MARKS (CHAFFE) (C-CHECK RO 04/30/2025)REPAIRED DAMAGED SLAT TRACK RH 3-2 IAW CRJ700 AMM 57-42-26, SRM 51-12-00 AND REO 670-57-42-2063 REV-- DATE 2025-04-21. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, REPORT# S042325-5, P.
- [SDR SWIA20250430003](https://openairdocs.org/sdr/SWIA20250430003.md): Hinge Arm · gouged · Mar 3, 2025 · N774SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH IB FLAP HIMGE ARM GOUGED EVAL (WS 128.00) (C-CHECK RO 04/30/2025)PERFORMED REPAIR ON RH IB FLAP HINGE WS128.00 LUG FOUND TO BE STRUCTURRALLY ACCEPTABLE IAW REO 670-57-52-604 REV -- DATE 2025-04-03, CRJ 700 SRM 57-52-27, 51-12-00, NDT PERFORMED BY BARON DNT
- [SDR SWIA2024071800004](https://openairdocs.org/sdr/SWIA2024071800004.md): Skin · cracked · Jul 14, 2024 · N774SK · Cndair CL6002C10 · Passenger/Crew Doors
  > TRANSFER FROM EAML 1388599: TRANSFERRED FROM CAMP 28522574. MCD CABLE PULLEY BRACKET AND INNER SKIN FASTENERS PULLED UP FROM AFT EDGE WHERE THE PULLEY ATTACHES TO THE DOOR. DAMAGE BEGINS 38.75 INCHES FROM THE BOTTOM OF THE DOOR AND ENDS 36€? UP FROM THE BOTT
- [SDR SWIA2024031800008](https://openairdocs.org/sdr/SWIA2024031800008.md): Windshield · cracked · Mar 8, 2024 · N774SK · Cndair CL6002C10 · Flight Compartment Windows
  > RT SIDE POST BOLT HOLE #26 HAS TWO CRACKS FROM BOLT HOLE TO NUTPLATE.REO FROM MRJ REAQUESTED. (FILED CLOSED)REMOVED AND REPLACED COCKPIT RH WINDOW/WINDSHIELD SIDE POST IN REF TO SRM 51-42-21, 51-45-00, AND DWG CC670-33055. COMPLETED TASK CARD 51-900-1002-SKY A
- [SDR SWIA2024011231211](https://openairdocs.org/sdr/SWIA2024011231211.md): Unknown · warning message · Dec 11, 2023 · N774SK · Cndair CL6002C10 · Flight Control System
  > ON TAKEOFF STAB CH1 INOP STATUS FOLLOWED BY STAB FAULT STATUS. STAB TRIM RUNAWAY, PERFORMED ASSOCIATED MEMORY ITEMS. (FLIGHT 3074 FILED CLOSED)INTERROGATED MDC AND FOUND HISTORY OF B1 FAULT CODE 007959. TROUBLESHOT STAB CH1 INOP PER FIM TASK 27-42-03-810-803
- [SDR SWIA2023050900003](https://openairdocs.org/sdr/SWIA2023050900003.md): Unknown · dented · May 3, 2023 · N774SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 1132488: CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1132169FOUND THREE DENTS IN SKIN FWD OF LT TRU DOOR. ONE DENT IS 3.25"BY 2.25" BY.016" DEEP. THE NEXT DENT IS 1.5" BY 2.75" BY.094" DEEP WITH THE UNDERLYING STRINGER DEFORMED
- [SDR SWIA202263822](https://openairdocs.org/sdr/SWIA202263822.md): None · none · Jan 15, 2022 · N774SK · Cndair CL6002C10 · Window/Windshield System
  > LEFT CAPT SIDE WINDOW EXPERIENCED MULTIPLE POPPING FRACTURES AT 2,000 10,000 AND 18,000 FEET DURING CLIMB OUT. RETURN TO FIELD RIC. (FLIGHT 3131 - FILED CLOSED)REMOVED AND INSTALLED LH SIDE WINDOW IN REFERENCE WITH AMM 56-12-01. COMPLIED WITH TASK CARD 56-22
- [SDR SWIA202162727](https://openairdocs.org/sdr/SWIA202162727.md): None · misaligned · Oct 23, 2021 · N774SK · Cndair CL600* · Rudder, Spar/Rib
  > VERTICAL STABILIZER TRAILING EDGE RUDDER MIDDLE LOWER HINGE DOES NOT LINE UP CORRECTLY. (C-CHECK RO 11-20-2021) REMOVED MIDDLE LOWER HINGE ON VERTICAL STABILIZER TRAILING EDGE REF. CRJ700 SRM 51-42-21-001-001-A01 AND INSTALLED MIDDLE LOWER HINGE ON VERTIC
- [SDR SWIA202162726](https://openairdocs.org/sdr/SWIA202162726.md): None · corroded · Oct 12, 2021 · N774SK · Cndair CL600* · Fuselage Main, Frame
  > FRAME AT FS319.70 LH BETWEEN STGR'S 18L AND 21L HAS INTERGRANULAR CORROSION. (C-CHECK RO 11-20-2021) REMOVED AND REPLACED CORRODED FRAME WITH NEW FRAME (P/N SH670-31891-3) AT FS319.70 LH BETWEEN STGR'S 18L AND 21L USING ALL NEW HARDWARE. REF BOMBARDIER DW
- [SDR SWIA202162725](https://openairdocs.org/sdr/SWIA202162725.md): None · gouged · Oct 11, 2021 · N774SK · Cndair CL600* · Fuselage, Equipment Attach Fittings
  > PAX DOOR HINGE (FUSELAGE SIDE) HAS 3EA GOUGES AT LUG LAND #25,26, AND #27 (C-CHECK RO 11-20-2021) REPAIRED 3 EA GOUGES AT LUG LANDS #25, #26 AND #27 ON FUSELAGE SIDE OF PAX DOOR HINGE REF CRJ700 SRM 53-21-23-201-010-A01, DISPOSITON TYPE IV. FOUND TO BE WI
- [SDR SWIA202162724](https://openairdocs.org/sdr/SWIA202162724.md): None · cracked · Oct 8, 2021 · N774SK · Cndair CL600* · Engine Air Baffle Section
  > WHILE COMPLETING REPAIR ON R/H UPPER TRANSCOWL COAMING, FOUND CRACK IN METAL PERFORATE INNER SKIN UNDER ZED STIFFENER. (C-CHECK RO 11-20-2021) REPAIRED R/H UPPER TRANSCOWL INNER SKIN UNDER "Z" STIFFENER REF REO 670-54-21-1472 REV (--) 2021-10-18 STEPS 1-16
- [SDR SWIA202162723](https://openairdocs.org/sdr/SWIA202162723.md): None · cracked · Oct 3, 2021 · N774SK · Cndair CL600* · Fuselage Structure (General)
  > FORWARD EQUIPMENT COMPARTMENT, HAS A CRACK ON RIGHT SIDE WHERE THE FLOOR AND FRAME MEET @FS193.00. (C-CHECK RO 11-20-2021) REPAIRED F.S 193 FORWARD EQUIPMENT COMPARTMENT CRACK REF. BOMBARDIER REO 670-53-11-509 REV.E DATED 2018-02-08. COMPLIED WITH TASK
- [SDR SWIA202162722](https://openairdocs.org/sdr/SWIA202162722.md): None · cracked · Oct 2, 2021 · N774SK · Cndair CL600* · Fuselage Structure (General)
  > FORWARD EQUIPMENT COMPARTMENT, HAS A CRACK ON LEFT SIDE WHERE THE FLOOR AND FRAME MEET @FS193.00. (C-CHECK RO 11-20-2021) RE-INSTALLED HYDRAULIC SYSTEM 2 AND 3 CHARGE VALVE AND GAUGES TO PLACE AT FWD EQUIPMENT COMPARTMENT LH REF CRJ 700 AMM 32-43-30-400
- [SDR SWIA202162744](https://openairdocs.org/sdr/SWIA202162744.md): None · corroded · Oct 1, 2021 · N774SK · Cndair CL600* · Elevator, Plate/Skin
  > RH ELEVATOR TO H/ STAB HINGES 1,2,3 AND 4 HAVE CORRODED HARDWARE INSTALL. (C-CHECK RO 11-20-2021) REMOVED AND REPLACED RH ELEVATOR TO H/STAB HINGES 1,2,3 AND 4 WITH NEW HARDWARE. REF CRJ 700 AMM 27-34-01-000-801-A04. REF CRJ 700 AMM 27-34-01-400-801-A04.
- [SDR SWIA202162743](https://openairdocs.org/sdr/SWIA202162743.md): None · corroded · Oct 1, 2021 · N774SK · Cndair CL600* · Elevator, Plate/Skin
  > LH ELEVATOR TO H/ STAB HINGES 1,2,3 AND 4 HAVE CORRODED HARDWARE INSTALL. (C-CHECK RO 11-20-2021) REMOVED AND REPLACED LH ELEVATOR TO H/STAB HINGES 1,2,3 AND 4 WITH NEW HARDWARE. REF CRJ 700 AMM 27-34-01-000-801-A04. REF CRJ 700 AMM 27-34-01-400-801-A04.
- [SDR SWIA202162742](https://openairdocs.org/sdr/SWIA202162742.md): None · corroded · Sep 29, 2021 · N774SK · Cndair CL600* · Fuselage, Powerplant Attach Fittings
  > RH FLOOR SEAT TRACK AT RBL9 BETWEEN FS.379.00 TO FS.485.00 CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 11-20-2021) REMOVED AND INSTALLED NEW RBL9 SIDE SEAT TACK AT APPROX. FS379-FS485 CRJ-700 AMM 53-00-49-400-801-A17
- [SDR SWIA202162721](https://openairdocs.org/sdr/SWIA202162721.md): None · cracked · Sep 29, 2021 · N774SK · Cndair CL600* · Standard Practices/Structures
  > REPLACE THE CRACKED RH AFT DRAG ANGLE FOR VERTICAL STABILIZER REAR SPAR. (C-CHECK RO 11-20-2021) REPAIRED THE RH AFT DRAG ANGLE FOR THE VERTICAL STABILIZER BY CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS REF CRJ700 SRM 55-31-00-201-001-A01
- [SDR SWIA202162746](https://openairdocs.org/sdr/SWIA202162746.md): None · cracked · Sep 25, 2021 · N774SK · Cndair CL600* · Powerplant System
  > *RH UPPER TRANSCOWL MOST INBD €ŒA€? FITTING IS CRACKED (C-CHECK RO 11-20-2021) REMOVED DAMAGED R/H UPPER TRANSCOWL INBD "A" FITTING, AND INSTALLED 1 EA NEW "A" FITTING P/N CN624-2082-201 REF REO 670-54-21-971 REV (A) 2017-05-11 STEPS 1-3.
- [SDR SWIA202162745](https://openairdocs.org/sdr/SWIA202162745.md): None · cracked · Sep 25, 2021 · N774SK · Cndair CL600* · Powerplant System
  > *LH UPPER TRANSCOWL MOST INBD €ŒA€? FITTING IS CRACKED (C-CHECK RO 11-20-2021) REMOVED AND REPLACED INBD STAND OFF ANGLE ( A-FITTING) P/N CN624-2082-201 ON LH UPPER TRANSCOWL IAW ALL STEPS OF REO 670-54-21-971 REV -A, DATED 2017-05-11. WEIGHT REMOVED =
- [SDR SWIA202162720](https://openairdocs.org/sdr/SWIA202162720.md): None · worn · Sep 25, 2021 · N774SK · Cndair CL600* · Engine Cowl Flaps
  > *RH UPPER TRANSCOWL HAS WEAR ON COAMING. AREA MARKED (C-CHECK RO 11-20-2021) REPAIRED DAMAGE ON R/H UPPER TRANSCOWL COAMING REF REO 670-54-21-1028 REV (NC) 2009-06-15 STEPS 1-9. FUCNTIONAL CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202162719](https://openairdocs.org/sdr/SWIA202162719.md): None · worn · Sep 25, 2021 · N774SK · Cndair CL600* · Powerplant System
  > *LH UPPER TRANSCOWL LATCH DOOR COAMING HAS WEAR. AREA MARKED. (C-CHECK RO 11-20-2021) REPAIRED WEAR DAMAGE ON LH UPPER TRANSCOWL LATCH DOOR COAMING IAW ALL STEPS OF REO 670-54-21-1028 REV -NC, DATED 2009-06-15. COMPLIED WITH SKY CARD 51-900-1002-SKY. FUNCT
- [SDR SWIA202162718](https://openairdocs.org/sdr/SWIA202162718.md): None · cracked · Sep 25, 2021 · N774SK · Cndair CL600* · Empennage Structure
  > RH VERTICAL STABILIZER 67.5% REAR SPAR DATUM APPROX DRAG ANGLE HAS POSSIBLE CRACK AS MARKED (C-CHECK RO 11-20-2021) REPAIRED THE RH FWD DRAG ANGLE FOR THE VERTICAL STABILIZER BY CUTTING AWAY DAMAGE, FABRICATING AND INSTALLING REPAIR PARTS REF CRJ700 SRM 5
- [SDR SWIA202162741](https://openairdocs.org/sdr/SWIA202162741.md): None · worn · Sep 23, 2021 · N774SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > RH WING SLAT TRACK 3-2 FWD O/B AND AFT O/B ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11-20-2021) REMOVED AND REPLACED R/H SLAT TRACK 3-2 FWD O/B AND AFT O/B ROLLERS. REF CRJ700 AMM 27-81-44-400-803-A01. OPERATIONAL TEST GOOD.
- [SDR SWIA202162740](https://openairdocs.org/sdr/SWIA202162740.md): None · worn · Sep 23, 2021 · N774SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > RH WING SLAT TRACK 2-2 FWD I/B, FWD O/B, AFT I/B AND AFT O/B ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11-20-2021) REMOVED AND REPLACED RH WING SLAT TRACK 2-2 FWD I/B, FWD O/B, AFT I/B AND AFT O/B ROLLERS REF CRJ700 AMM 27-81-44-400-802-A01, CHECKS GOOD.
- [SDR SWIA202162739](https://openairdocs.org/sdr/SWIA202162739.md): None · worn · Sep 23, 2021 · N774SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > RH WING SLAT TRACK 1-2 FWD I/B, FWD O/B, AFT I/B AND AFT O/B ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11-20-2021) REMOVED AND REPLACED R/H SLAT TRACK 1-2 FWD I/B, FWD O/B, AFT I/B AND AFT O/B ROLLERS. REF CRJ700 AMM 27-81-44-400-801-A01, ALL CHECKS GOOD AT
- [SDR SWIA202162738](https://openairdocs.org/sdr/SWIA202162738.md): None · worn · Sep 23, 2021 · N774SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH WING SLAT TRACK 3-2 FWD O/B, FWD I/B, AFT O/B AND AFT I/B ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11-20-2021) INSTALLED NEW LH WING SLAT TRACK 3-2 FWD O/B, FWD I/B, AFT O/B AND AFT I/B ROLLERS WITH P/N CC670-12459-3 AND CC670-12459-4 REF CRJ700 AMM 27-81
- [SDR SWIA202162737](https://openairdocs.org/sdr/SWIA202162737.md): None · worn · Sep 23, 2021 · N774SK · Cndair CL600* · Wing, Nacelle/Pylon Attach Fittings
  > LH WING SLAT TRACK 2-2 FWD O/B, FWD I/B, AND AFT O/B ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11-20-2021) REMOVED AND REPLACED THE LH WING SLAT TRACK 2-2 FWD O/B, FWD I/B, AND AFT O/B ROLLERS REF CRJ700 AMM 27-81-44-400-802 (CONFIG A01), OP CHECKS GOOD.
- [SDR SWIA202162736](https://openairdocs.org/sdr/SWIA202162736.md): None · worn · Sep 23, 2021 · N774SK · Cndair CL600* · Wing, Fuselage Attach Fittings
  > LH WING SLAT TRACK 1-2 FWD O/B, FWD I/B, AFT O/B AND AFT I/B ROLLERS WORN BEYOND LIMITS (C-CHECK RO 11-20-2021) REMOVED AND REPLACED LH WING SLAT TRACK 1-2 FWD O/B, FWD I/B, AFT O/B AND AFT I/B ROLLERS WITH NEW ROLLERS P/N CC670-12027-3 AND CC670-12048-3 R
- [SDR SWIA202162717](https://openairdocs.org/sdr/SWIA202162717.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Floor Panel
  > *FORWARD BAGGAGE BAY DOOR SURROUNDING STRUCTURE MACHINED BRACKET HAS EVIDENCE OF CORROSION @LBL 24 BETWEEN FS581 TO FS597. MARKED (C-CHECK RO 11-20-2021) LOCATED DRILLED AND INSTALLED NEW MACHINED BRACKET P/N SH670-33390-2 AT THE AFT SIDE OF THE FWD BAG B
- [SDR SWIA202162716](https://openairdocs.org/sdr/SWIA202162716.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Main, Keel
  > *CORROSION ON STGR 19R BETWEEN FS 453.00 €“ 437.00 (C-CHECK RO 11-20-2021) REMOVED CORROSION ON STRINGER 19R BETWEEN FS437.00 TO FS453.00 IN FORWARD CABIN. EVALUATED A OUT-OF-LIMITS. COMPLIED WITH CRJ700 SRM 53-00-03-201-001-A01 REPAIR PROCEDURE STEP 5. A
- [SDR SWIA202162715](https://openairdocs.org/sdr/SWIA202162715.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Main, Keel
  > *CORROSION ON STGR 27, BETWEEN FS 349.00 €“ 364.00 (C-CHECK RO 11-20-2021) REMOVED AND INSTALLED NEW STRINGER 27 FROM BETWEEN FS333 AND FS364 REF. CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 AND DWG SH670-31350 REV -A. COMPLIED WIT
- [SDR SWIA202162714](https://openairdocs.org/sdr/SWIA202162714.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *CORROSION ON INTERCOSTAL AT STGR21L BETWEEN FS 310.00 €“ 333.00 (C-CHECK RO 11-20-2021) REMOVED AND REPLACED CORRODED INTERCOSTAL WITH NEW REPLACEMENT ONE (P/N SH670-31822-1S) ON STGR21L BETWEEN FS310.00 AND 333.00LH USING ALL NEW HARDWARE, REF BOMBARDIE
- [SDR SWIA202162713](https://openairdocs.org/sdr/SWIA202162713.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Structure (General)
  > *CORROSION ON ATTACHING ANGLE AT FS 319.00/STGR23R (C-CHECK RO 11-20-2021) REMOVED AND REPLACED ANGLE P/N SH670-35625-1 ON FS319 AND STRINGER 23R REF CRJ 700 SRM 51-42-06-001-001-A01 AND DRAWING SH670-31950 REV Y. COMPLIED WITH ST 51-900-1002-SKY
- [SDR SWIA202162712](https://openairdocs.org/sdr/SWIA202162712.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *CORROSION ON ATTACHING ANGLE AT FS 319.00/STGR22R (C-CHECK RO 11-20-2021) REMOVED AND REPLACED ANGLE P/N SH670-35625-1 ON FS319 AND STRINGER 22R REF CRJ 700 SRM 51-42-06-001-001-A01 AND DRAWING SH670-31950 REV Y. SEE CONTINUATION CARD FOR DETAILS. COMPL
- [SDR SWIA202162711](https://openairdocs.org/sdr/SWIA202162711.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Main, Keel
  > *CORROSION ON STGR 26R BETWEEN FS 295.00 €“ 310.00 (C-CHECK RO 11-20-2021) REMOVED CORROSION ON STGR 26RH BETWEEN FS 295.00 AND FS 310.00 REF CRJ700 SRM 51-21-06-001-001-A01. ALLOWABLE DAMAGE IS 10% (.006€?) FOUND OUT OF LIMITS. REF. DRAWING # SH60-3163
- [SDR SWIA202162710](https://openairdocs.org/sdr/SWIA202162710.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > *CORROSION ON STGR 27 TOP FLANGE BETWEEN FS280.00 €“ 295.00 (C-CHECK RO 11-20-2021) REMOVED CORROSION FROM STGR 27 TOP FLANGE BETWEEN FS280.00 €“ 295.00 PER CRJ700 SRM 51-21-06-001-001-A01. NO DAMAGE ALLOWED ON STGR 27 TOP FLANGE BETWEEN FS280.00 €“ 295
- [SDR SWIA202162709](https://openairdocs.org/sdr/SWIA202162709.md): None · corroded · Sep 23, 2021 · N774SK · Cndair CL600* · Fuselage Main, Longeron/Stringer
  > *MULTIPLE AREAS OF CORROSION ON FS280.00 JOINT STRAP BETWEEN STGR 23L €“ 23R (C-CHECK RO 11-20-2021) REMOVED CORROSION ON JOINT STRAP OF FS280.00 BETWEEN STGR23L AND 23R REF CRJ700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS PER CRJ700 SRM 53-00-
- [SDR SWIA202162750](https://openairdocs.org/sdr/SWIA202162750.md): None · chafed · Sep 22, 2021 · N774SK · Cndair CL600* · Nacelle/Pylon Structure
  > *RIGHT ENGINE €“ T/R COWLING DISHING FORWARD CHANNEL AND DOUBLER ARE CHAFED. (MARKED) (C-CHECK RO 11-20-2021) REMOVED AND INSTALLED NEW DOUBLER ON THE RH ENGINE UPPER T/R COWLING REF: CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH. UPON REMOVAL AND INST
- [SDR SWIA202162749](https://openairdocs.org/sdr/SWIA202162749.md): None · chafed · Sep 22, 2021 · N774SK · Cndair CL600* · Nacelle/Pylon Structure
  > *RIGHT ENGINE - T/R COWLING DISHING AFT CHANNEL AND DOUBLER ARE CHAFED. (MARKED) (C-CHECK RO 11-20-2021) REMOVED AND INSTALLED NEW DOUBLER ON THE RH ENGINE UPPER T/R COWLING REF: CRJ700 SRM 51-42-06-001-001-A01. RESTORED FINISH.UPON REMOVAL AND INSTALLATIO

Next page: https://openairdocs.org/aircraft/N774SK/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 = 'N774SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N774SK/reports

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