N706SK

Service difficulty reports · 239

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N706SK' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2025091500013Hose · faultedHYD 3 LO PRESS CAUTION MSG. CHECKED HYDRAULICS PAGE AND SHOWED 0 % FLUID REMAINING. RAN QRH AND DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. TOWED INTO GATE. (FLIGHT 6510 - FILED CLOSED) PLEASE REFERENCE AML 1703109 FOUND HYD HOSE IN BELLEY FARING NO.320 ONSep 13, 2025 · N706SK · Cndair CL6002C10 · Hydraulic System, MainSDR SWIA202411271013Angle · crackedCRACK FOUND AT BULKHEAD ANGLE BL26.00 FS280.00 (HN00194250) (C-CHECK RO 11/26/2024) REMOVED AND REPLACED ANGLE RBL26.00 FS280.00 REF CRJ700 SRM51-42-06-001-001-A01, SRM51-42-13-001-001-A01 AND DWG NO. CC670-34010 REV -K. COMPLIED WITH TASK CARD 51-900-Oct 13, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2024112701305Stringer Splice · corrodedSTRINGER SPLICE STR 26R AT FS333 HAS DEEP CORROSION (C-CHECK RO 11/26/2024) REPLACED STRINGER SPLICE AT FS333 AND STGR 26R REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKYOct 11, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2024112701011Stringer · corrodedSTRINGER 26R FROM FS280 TO FS333 HAS SEVERE CORROSION (C-CHECK RO 11/26/2024) REPLACED STRINGER 26R AT FS280 - FS333 CRJ-700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020, CRJ-700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020 AND DWG SH670-31630 REV K. LEAOct 11, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2024112701304Floorbeam · corrodedCORROSION FOUND AT RH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 (C-CHECK RO 11/26/2024) REMOVED AND REPLACED RH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 REF CRJ700 SRM51-42-06-001-001-A01, SRM51-42-10-001-001-A01, SRM51-42-22-001-001-A01 REV 38 DOct 7, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA202411271007Floorbeam · corrodedCORROSION FOUND AT LH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 (C-CHECK RO 11/26/2024) REMOVED AND REPLACED LH FLOOR STRUCTURE CROSSBEAM FS280.00 W/L 72.00 REF CRJ700 SRM51-42-06-001-001-A01, SRM51-42-10-001-001-A01 AND SRM51-42-22-001-001-A01 REVOct 7, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2024112701301Handle · gougedAFT BAGGAGE BAY DOOR HANDLE HOUSING HAS NUMEROUS GOUGES (C-CHECK RO 11/26/2024) AFT CARGO DOOR HANDLE HOUSING IS OUT OF LIMITS PER REO 670-52-31-031 REV -B DATE 2016-12-07. REMOVED AND INSTALLED 1EA NEW AFT CARGO DOOR HANDLE HOUSING PER CRJ700SRM 51-42-Oct 4, 2024 · N706SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA2024112701300Slat Track · damagedRIGHT WING - SLAT TRACK 3-3 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) COMPLIED WITH REO 670-57-42-1788 REV-- DATED 2024-10-18, BLEND WAS PERFORMED CORRECTLY AND MADE SMOOTH. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SOct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2024112701299Slat Track · damagedRIGHT WING - SLAT TRACK 2-3 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) COMPLIED WITH REO 670-57-42-1787 REV-- DATED 2024-10-18, BLEND WAS PERFORMED CORRECTLY AND MADE SMOOTH. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKOct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2024112701298Slat Track · damagedLEFT WING - SLAT TRACK 3-2 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) REMOVED GROOVING DAMAGE FROM LH SLAT TRACK 3-2 AND FOUND ACCEPTABLE AT THIS TIME REF REO 670-57-42-1795 REV -- 2024-10-21. COMPLIED WITH TASK CARD 51-900-1002-Oct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2024112701297Slat Track · groovedLEFT WING - SLAT TRACK 1-1 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) COMPLIED WITH REPAIR OF WEAR DAMAGE TO LH SLAT TRACK 1-1 REF REO 670-57-42-1786 REV-- DATED 2024-10-17 ALL STEPS COMPLIED WITH. CLEARANCE CHECK GOOD. COMPLIEOct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA202411271004Slat Track · groovedLEFT WING - SLAT TRACK 2-1 HAS ONE AREA OF GROOVING. (MARKED IN RED) (C-CHECK RO 11/26/2024) REMOVED GROOVING DAMAGE FROM LH SLAT TRACK 2-1 AND FOUND ACCEPTABLE AT THIS TIME REF REO 670-57-42-1789 REV -- 2024-10-21. COMPLIED WITH TASK CARD 51-900-1002-SOct 4, 2024 · N706SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024112701296Striker · dentedPASSENGER DOOR SURROUND STRUCTURE FS349.00 SILL STRIKER BETWEEN IS DENTED STGR4L & STGR5L. (MARKED IN RED) (C-CHECK RO 11/26/2024) PERFORMED REPAIR OF PASSENGER DOOR SURROUND STRUCTURE FS349.00 SILL STRIKER BETWEEN STGR4L & STGR5L BY COMPLYING WITH ALL Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2024112701295Stringer · corrodedGALVANIC CORROSION ON STGR25R FS295.00 - 310.00 (MARKED IN RED) (C-CHECK RO 11/26/2024) REPLACE STRINGER AT 25R FS280 - FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. LEAK CHECK GOOD. COMPLIED WITH TASOct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2024112701294Stringer · corrodedGALVANIC CORROSION THE FULL LENGTH ON STGR25R STRINGER SPLICE AT FS333.00. (MARKED IN RED) (C-CHECK RO 11/26/2024) REPLACED STRINGER SPLICE AT 25R. FS333 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG: SH670-32420 REV E. LEAK CHECK GOOD. COMPLIED WITH TASOct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2024112701293Stringer · corrodedGALVANIC CORROSION ON STGR26R FS333.00 - 349.00. (MARKED IN RED) (C-CHECK RO 11/26/2024) REPLACED STRINGER AT 26R, FS333 - FS364 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31350 REV A. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKYOct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202411271292Skin · gougedLOWER EXTERNAL SKIN PANEL HAS 4 DEEP GOUGES FORWARD AND AFT OF FS977 (C-CHECK RO 11/26/2024) COMPLIED WITH ALL STEPS OF SOLUTION 2 OF REO 670-53-00-290 REV - F 2019/04/26. LEAK CHECK GOOD, COMPLIED WITH TASK CARD 51-900-1002-SKYOct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202411571003Seat Track · corrodedL/H SEAT RAIL BEAM AT LBL9 BETWEEN FS572.00 TO FS685.00 SEVERAL AREAS ARE CORROSION (MARKED) (C-CHECK RO 11/26/2024) REPAIRED CORROSION DAMAGE ON LH SEAT RAIL BEAM FLANGE AT LBL 9, BETWEEN F.S. 572 AND F.S. 685 TO REO 670-53-31-954 REV -- DATED 2024-10-Oct 3, 2024 · N706SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWAI2024112701291Transcowl · crackedR/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/26/2024) INSTALLED A NEW R/H LWR TRANSCOWL I/B "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED FULLY Oct 1, 2024 · N706SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202411271001Transcowl · crackedR/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 11/26/2024) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY COct 1, 2024 · N706SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202411270926Floor Support · corrodedCOCKPIT FLOORBOARD SUPPORT ANGLE IS CORRODED. FWD SIDE OF FS280 BEAM (C-CHECK RO 11/26/2024) REMOVED AND REPLACED COCKPIT FLOORBOARD SUPPORT ANGLE REF CRJ 700 SRM51-42-06-001-001-A01 REV 38 DATE JUL 25/2020, DWG NO. CC670-34010 REV -K AND DWG NO. CC670-Sep 26, 2024 · N706SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2024112701302Door · crackedLH TRU DOOR (211AL) LANDING HAS A POSSIBLE CRACK BY AFT LATCH (C-CHECK RO 11/26/2024) REMOVED AND REPLACED LH TRU DOOR (211AL) LANDING REF REO NO. 670-53-11-2026 REV -- DATED 2024-10-04 AND DWG NO. CC670-33040 REV -G. COMPLIED WITH TASK CARD 51-900-100Sep 22, 2024 · N706SK · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR SWIA202411270922Door · crackedRH TRU DOOR (212AR) LANDING HAS A POSSIBLE CRACK BY AFT LATCH (C-CHECK RO 11/26/2024) REMOVED CRACKED DOOR LANDING FROM STGR 16R BETWEEN FS172-FS193 AND INSTALLED A NEW ONE PER REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-13-001-001-A01, CRJSep 22, 2024 · N706SK · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR 2023FA0000253Fire Bottle · abnormalFIRE EXTINGUISHER WAS RECEIVED WITH FOD INSIDE OF THE CYLINDER. THE FOD WAS A BROWN RESIDUE AND GRANULAR SUBSTANCE LOCATED ON RESTRICTED FLOW ORIFICES AND ON THE CYLINDER WALLS. FOD WAS FOUND DURING THE SERVICE OF THE FIRE EXTINGUISHER. THE RECOMMENDED SERVICEMay 10, 2023 · N706SK · Cndair CL6002C10 · Fire Protection SystemSDR SWIA2023011367111Stringer · deformedSTRINGER 19L FOUND DEFORMED NEAR FRAME SPLICE AT BS 1015. REPAIRED THE STRINGER IAW REO 670-53-61-2096, REV.C.Nov 12, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2023011367114Frame · not reportedREMOVED FRAME SEGMENT FROM FS 1047 STR19L-27L. LOCATED DRILLED AND INSTALLED NEW LOWER FRAME SEGMENT PN MM670-36064-003 REF CRJ 700 SRM 51-40-11 AND 51-42-06. ORIG SUBMISSION DATE: 1/13/2023Sep 2, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2023011367113Support Bracket · deformedSUPPORT BRACKET DEFORMED AT BS 1047, STGR 19 LEFT. REMOVED, FABRICATED, AND INSTALLED A NEW SUPPORT BRACKET IAW SRM 51-42-06-001-001, 51-24-21-001-001, 53-61-03 AND DWG MM670-36485. ORIG SUBMISSION DATE: 1/13/2023Aug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2023011367112Frame Splice · deformedFRAME SPLICE SUPPORT BRACKET DEFORMED AT BS 1015, STGR 19L. REMOVED CLEAT AND FABRICATED A NEW CLEAT. INSTALLED THE NEW CLEAT IAW SRM 51-42-06-001-001, 51-24-21-001-001, 53-61-03 AND DWG MM670-36483. ORIG SUBMISSION DATE: 1/13/2023Aug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2023011367110Frame Splice · deformedFRAME SPLICE BS 1015, S19L DEFORMED. REMOVED FRAME SPLICE, AND FABRICATED A NEW FRAME SPLICE. INSTALLED IAW SRM 51-42-06-001-001, 51-24-21-001-001-A01, DWG MM670-36402, AND REO 670-53-61-2096 REV C. ORIG SUBMISSION DATE: 1/13/2023Aug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2023011367109Frame · damagedFRAME 1015.00 TORN AND DEFORMED AT THE INTERSECTION OF FRAME BS 1015, S18L. REMOVED DAMAGED FRAME. NEW FRAME SEGMENT PN MM670-36123-003 LOCATED, DRILLED, AND INSTALLED IAW SRM TASK 51-40-11-001-001, 51-42-06-001-001 AND REO 670-53-61-2096, REV C. ORIG SUBMAug 27, 2022 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202162060None · crackedPAX DOOR AFT FORMER IS CRACKED. (C-CHECK RO 10/29/2021) REMOVED AND REPLACED PAX DOOR FORMER AFTER FORMER PER CRJ 700 SRM 51-42-06-001-001-A01 AND PERFORMED PRESSURE LEAK CHECK TO PAX DOOR AFT FORMER PER CRJ 700 AMM 21-31-00-910-801-A01 NO LEAKS. COMPLOct 2, 2021 · N706SK · Cndair CL6002C10 · DoorsSDR SWIA202162062None · wrinkledWITH AIRCRAFT POWER ON AN UNCOMMANDED FLAP DEPLOYMENT CAUSED WRINKLING OF THE RH OUTBOARD FLAP PANEL (C-CHECK RO 10/29/2021) REPLACED RH OUTBD FLAP PANEL WITH SERVICABLE PANEL REF CRJ-700 AMM 27-52-29-400-801-A02. OPS AND RIG CHECK GOOD SEE CONTINUATIONOct 1, 2021 · N706SK · Cndair CL6002C10 · Wing, Nacelle/Pylon Attach FittingsSDR SWIA202162059None · damagedEVALUATE DAMAGE TO RH AILERON CAUSED BY UNCOMMANDED DEPLOYMENT OF RH OUTBOARD FLAP (C-CHECK RO 10/29/2021) BLENDED AILERON EDGE IAW CRJ 700 SRM 51-12-00-001-001-A01 FOUND OUT OF LIMITS INSTALLED NON FLUSH PATCH REPAIR IAW CRJ 700 SRM 57-61-01-201-001-A0Oct 1, 2021 · N706SK · Cndair CL6002C10 · Wing StructureSDR SWIA202162058None · corrodedCORROSION FOUND ON INTERCOSTAL DD4 BETWEEN FS 311-327 ON FWD PAX DOOR (C-CHECK RO 10/29/2021) - INSTALLED NEW PAX DOOR INTERCOSTAL DD4 BETWEEN FS311 AND FS327 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01 COMPLIED WITH TASK CARD 51-900-100Sep 23, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202162057None · gougedSTGR AT AFT CARGO DOOR THRESHOLD (ADJACENT TO COAMING) HAS GOUGES AND FRETTING IN MULTIPLE LOCATIONS. (C-CHECK RO 10/29/2021) BLENDED OUT FRETTING/GOUGING ON STGR 17L AT AFT CARGO DOOR THRESHOLD, REF CRJ 700 SRM 51-12-00-001-001-A01 / BLENDED WITHIN LISep 23, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, KeelSDR SWIA202162056None · corrodedCORROSION FOUND ON REINFORCEMENT ANGLE OF FRAME FS549 BETWEEN STGR18L/17L (C-CHECK RO 10/29/2021) REMOVED AND REPLACED ANGLE REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-33100 REV K / FS549 STGR18L-STGR17L, COMPLIED WITH SKY CARD 51-900-1002 SKSep 23, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202162055None · crackedFRAME 320 ON PAX DOOR HAS A CRACK AT RIVET HOLE AND MULTIPLE SPOTS OF CORROSION (C-CHECK RO 10/29/2021) INSTALLED INTERCOSTAL DDA BETWEEN FS 311-320 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, AND REO 670Sep 16, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202162054None · elongatedRIGHT ENG. LOWER TRANSCOWL DOUBLER HAS AN ELONGATED HOLE. (C-CHECK RO 10/29/2021) INSTALLED NEW RH ENG. LOWER TRANSCOWL DOUBLER CRJ-700 SRM 51-42-13-001-001-A01, SRM 51-42-06-001-001-A01, REO 670-54-21-1207 REV A DATED 2015-08-27 / COMPLIED WITH SKY CARSep 15, 2021 · N706SK · Cndair CL6002C10 · Engine Exhaust SystemSDR SWIA202162053None · corrodedINTERCOSTAL DD6 HAS CORROSION ON IT ON FLANGE AND FWD ANGLE HAS A CRACK IN IT (C-CHECK RO 10/29/2021) INSTALLED NEW INTERCOSTAL REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06 AND 51-42-21-001-001-A01. / COMPLIED WITH TASK CARD 51-900-1002-SKYSep 15, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202162052None · gougedRIGHT ENG. LOWER TRANSCOWL LATCH COAMING WORN AND GAUGED (C-CHECK RO 10/29/2021) INSTALLED NEW RIGHT ENG. LOWER TRANSCOWL LATCH COAMING REF, CRJ-700 SRM 51-42-13-001-001-A01, SRM 51-42-06-001-001-A01, REO 670-54-21-1207 REV A DATED 2015-08-27 / COMPLIEDSep 15, 2021 · N706SK · Cndair CL6002C10 · Engine Exhaust SystemSDR SWIA202162051None · corrodedFWD AND AFT CAP ANGLES CORRODED ON PAX DOOR MID CAP ANGLE FLOOR SILL/THRESHOLD AREA. (C-CHECK RO 10/29/2021) REPLACED FWD AND AFT CAP ANGLES CORRODED ON PAX DOOR MID CAP ANGLE FLOOR SILL/THRESHOLD AREAREF: CRJ-700 S.R.M.51-42-06-001-001-A01 DWG-SH670-3Sep 13, 2021 · N706SK · Cndair CL6002C10 · DoorsSDR SWIA202162050None · corrodedCLIP( 601R318058-1) ON INTERCOSTAL DD7A IS CORRODED AFT SIDE (C-CHECK RO 10/29/2021) REMOVE AND REPLACED CLIP IN INTERCOSTAL DD7 AFT SIDE REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKYSep 10, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202162049None · corrodedFORMER FS320 (601R318038-3) HAS CORROSION OROUND SEVERAL FASTENERS THROUGH THE SKIN (C-CHECK RO 10/29/2021) INSTALLED NEW FORMER REF DWG 601R31702 REV N CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. COMPLIED WITH TASK CARD 51-9Sep 10, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2021110262048Support Angle · corrodedPAX DOOR FORWARD SUPPORT ANGLE HAS CORROSION IN 2 PLACES AND A GOUGE IN LOWER END (C-CHECK RO 10/29/2021) INSTALLED NEW PAX DOOR FOWARD SUPPORT ANGLE REF CRJ700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-20-001-001-A01, AND DWG 601R31702 REV N / CSep 9, 2021 · N706SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202162047None · wornLEFT HAND WING ZONE 500 SLAT TRACK 1-1 SHOWS SIGNS OF WEAR ON LWR SIDE (MARKED WITH RED) (C-CHECK RO 10/29/2021) BLENDED WEAR ON LH WING SLAT TRACK 1-1 LOWER SIDE, MATERIAL LOSS FOUND TO BE WITHIN LIMITS REF MHIRJ REO 670-57-42-1190 REV--, DATED 2021-0Sep 5, 2021 · N706SK · Cndair CL6002C10 · Wing, Fuselage Attach FittingsSDR SWIA202162046None · crackedCRACK FOUND AT ANGLE ASSY LBL12 WL 72.10 BETWEEM FS280 AND FS265 (C-CHECK RO 10/29/2021) REMOVED AND REPLACED ANGLE ASSY (P/N CC670-33199-3) AT LBL 12 WL 72.10 BETWEEN F.S. 280 AND F.S. 265, REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG CC670-33052 REV -Sep 3, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202162045Intercostal · corrodedCORROSION FOUND ONPAX DOOR INTERCOSTAL DD7A BETWEEN FS 323-335 INSTALLED NEW INTERCOSTAL DD7A BETWEEN FS 323-335 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.LEAK CHECK GOOD. / COMPLIED WITH SKYWEST FORM M-337 / COMPLIESep 2, 2021 · N706SK · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA202162044None · corrodedCORROSION FOUND ON INTERCOSTAL DD2 BETWEEN FS 311-327 (C-CHECK RO 10/29/2021) INSTALLED NEW INTERCOSTAL DD2 BETWEEN FS311-327 REF DWG 601R31702 REV N, CRJ700 SRM 51 -42-06-001-001-A01 AND 51-42-21-001-001-A01, DWG 601R31702 REV N. COMPLIED WITH TASK Sep 2, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021110262043Intercostal · corrodedCORROSION FOUND ON INTERCOSTAL DD1A BETWEEN FS 338 AND 320 (C-CHECK RO 10/29/2021) REMOVED AND REPLACED INTERCOSTAL DD1A BETWEEN FS 338 AND 320 REF DWG 601R31702 REV N, CRJ700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-40-11-001-001-A01, LEAK CHECK GSep 2, 2021 · N706SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202162042None · corrodedEVIDENCE OF CORROSION FOUND ON CROSS BEAM AT FS1051.30 COMMON TO RBL27.00 UNDER R/H FLOOR SILL. (C-CHECK RO 10/29/2021) COMPLIED WITH BEAM REPAIR PER REO 670-53-61-1955 REV-- DATED 2021-10-14. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARDSep 2, 2021 · N706SK · Cndair CL6002C10 · Fuselage Main, Frame
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