N770SK

Service difficulty reports · 253

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 = 'N770SK' 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 SWIA2026050476406Floor Support · crackedBS 193 RT FORWARD EQUIPMENT COMPARTMENT FLOOR IS CRACKED AT THE FRAME-TO-FLOOR CUTOUT, BY THE ADG PUMP AREA BS 193 RT FORWARD EQUIPMENT COMPARTMENT FLOOR REPAIRED IAW SRM 53-11-43-201-001-A01 ALREADY INCORPORATED TO THIS AIRCRAFT , FOUND EXISTING REPAIR DOUBLEMay 4, 2026 · N770SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026050476405Bracket · corrodedBRACKET IN FORWARD BAGGAGE BAY AT APPROX STGR 23L, BS 533 HAS MULTIPLE AREAS OF CORROSION. REMOVED AND INSTALLED NEW BRACKET AT FORWARD BAGGAGE BAY AT APPROX. STGR 23L, BS 533 IAW SRM 51-42-21-001-001-A01 AND DWG SH670-33600 REV AD COMPLIED WITH SKYWEST TASK May 4, 2026 · N770SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026050476404Bracket · corrodedBRACKET IN FORWARD BAGGAGE BAY AT APPROX STGR 27, BS 581 CORRODED IN MULTIPLE LOCATIONS. REMOVED AND REPLACED NEW ANCHOR FITTING (BRACKET) AT FORWARD BAGGAGE BAY AT APPROX. STGR 27, BS 581 IAW SRM 51-42-21-001-001-A01 AND DWG SH670-33600 REV AD. COMPLIED WITH May 4, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA2026050476378Angle · corrodedAVIONICS BAY FLOOR PANEL FWD LANDING AT FS.280.00 HAS SPOTS OF CORROSION. REMOVED AND REPLACED CORRODED SUPPORT ANGLE WITH NEW SUPPORT ANGLE ON AVIONICS BAY FLOOR PANEL FWD LANDING AT FS.280.00 REF CRJ700 SRM 51-42-21-001-001-A01, REF SRM 51-42-13-001-001-A01May 4, 2026 · N770SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026050476364Cup · corrodedPAX DOOR UNDERFLOOR FWD HAND RAIL CUP HAS SPOTS OF CORROSION. EVALUATED PAX DOOR UNDERFLOOR FWD FITTING IS EXFOLIATED AND HAS CORROSION IN MORE THAN ONE ELEMENT. DAMAGE IS ALLOWED ONLY IN ONE ELEMENT AT A GIVEN CROSS SECTION REF. SRM 53-21-23-101-001-A01. REMMay 4, 2026 · N770SK · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026050476363Angle · crackedRIGHT TRU DOOR LOWER LANDING ANGLE, THE AFT LATCH CUT CRACKED. REPLACED CRACKED RH TRU DOOR LOWER LANDING ANGLE WITH NEW PN CC670-33151-6S PO# 5-56391 REF SRM 51-42-06-001-001-A01 AND DWG CC670-33040 REV G. COMPLIED WITH SKY CARD 51-900-1002-SKY STRUCTURAL MMay 4, 2026 · N770SK · Cndair CL6002C10 · Electrical/Electronic Compartment DoorsSDR SWIA2026050376418Floorbeam · crackedFS280.00 RBL 12, RH COCKPIT FLOOR BEAM IS CRACKED WHERE IS ATTACHES TO THE FS280.00 FLOOR CROSSBEAM. REMOVED AND REPLACED CRACKED COCKPIT FLOORBEAM AT RBL 12 AND FS280.00 WITH NEW FABRICATED FLOOR BEAM,USING ALL NEW FASTENERS ON ITEM 36 INBOARD ANGLE, ITEM -3May 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026050376408Floorbeam · crackedBS 280 FLOORBEAM TO RBL 9 FLOORBEAM, THE THE AFT SIDE OUTBD ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED OUTBD ATTACH ANGLE ON THE AFT SIDE OF RBL 9.0 AT BS280 WITH NEW ANGLE USING ALL NEW FASTENERS IAW SRM 51-42-21-001-001-A01 AND DWG CC670-34010 REMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026050376401Fitting · wornAFT BAGGAGE-BAY DOOR SURROUND STRUCTURE, STOP FITTINGS WORN, REPAIRED AFT CARGO DOOR SURROUND STOP FITTINGS. PER REO 670-53-61-2721 REV --. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY.May 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026050376400Bulkhead · damagedRIGHT BS 280 BULKHEAD APPROXIMATELY RBL13-14, THE AFT SIDE LOWER FLOOR-TO-BULKHEAD ANGLE HAS FASTENER HOLE WITH DRILL DAMAGE. REMOVED AND REPLACED RT BS 280 BULKHEAD CROSSBEAM REF SRM 51-42-06-001-001-A01, SRM 51-42-22-001-001-A01, SRM 51-42-21-001-001-A01 ANDMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SWIA2026050376376Hinge · gougedFORWARD BAGGAGE BAY DOOR SURROUND, FORWARD HINGE FUSELAGE SIDE IS GOUGED, REMOVED AND REPLACED GOUGED FWD BAGGAGE BAY DOOR, FWD HINGE WITH NEW SERVICEABLE HINGE USING NEW HARDWARE, REF REF CRJ 700 SRM 51-41-02-001-001-A01 AND DWGSH670-33750 REV AA. . CALIBRAMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2026050376373Floor Panel · corrodedCOCKPIT ENTRANCE FLOOR PANEL AFT ATTACH ANGLE ON THE FS280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED CORRODED COCKPIT ENTRANCE FLOOR PANEL AFT ATTACH ANGLE AT FS280.00 BETWEEN RBL 9.0 AND LBL 9.0 WITH NEW AFT ATTACH ANGLE (P/N CC670-34095-1SB) USING ALL NEWMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Floor PanelSDR SWIA2026070276371Floorbeam · crackedBS 280, LBL 12, LT COCKPIT FLOORBEAM IS CRACKED WHERE IS ATTACHES TO THE BS 280 FLOORBEAM. REMOVED AND REPLACED CRACKED COCKPIT FLOORBEAM AT LBL 12 AND BS 280 WITH NEW FABRICATED FLOOR BEAM,USING ALL NEW FASTENERS ON ITEM 36 INBOARD ANGLE, ITEM -38 INBOARD LOMay 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026050376365Floorbeam · crackedFS280.00 FLOORBEAM TO LBL 9 FLOOR BEAM, THE THE AFT SIDE OUTBD ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED CRACKED OTBD ATTACH ANGLE ON THE AFT SIDE OF LBL 9.0 AT BS 280 WITH NEW ANGLE (P/N CC670-34099-1SB) USING ALL NEW FASTENERS, REF SRM 51-42-21-001-001-May 3, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026050276425Door Sill · corrodedSERVICE DOOR SURROUND LOWER SILL CORRODED AT FORWARD DOOR STOP FITTING. REMOVED AND INSTALLED NEW ONE MOUNTING ANGLE AND SEAL STRIKER IAW SRM 51-42-06-001-001-A01 AND DWG. SH670-31950 REV Y. COMPLIED WITH TASK CARD 51-900-1002-SKY.May 2, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026043076374Repair · corrodedEXTERNAL FUSELAGE STATION 985 STG27, REPAIR PATCH HAS CORROSION IN VARIOUS AREAS, BLENDED AND TREATED CORROSION ON REPAIR PATCH ON EXTERNAL SKIN AT FS985.00 AND STGR27 PER MHIRJ REO 670-53-51-395 REV-- DATED 2026-05-06, REO 670-53-00-290 REV. -F DATED 2019-0Apr 30, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026042776429Stand Off · crackedLH LWR TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. INSTALLED NEW LT LOWER TRANSCOWL INBD -A- BRACKET REF REO# 670-54-21-971, REV B. COMPLIED WITH TASK CARD 51-900-1002-SKY.Apr 27, 2026 · N770SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026042776426Stand Off · crackedRIGHT LOWER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED CRACKED INBD -A- BRACKET STANDOFF FROM RT LOWER TRANSCOWL AND INSTALLED 1 EA NEW INBD -A- BRACKET STANDOFF ON RT LOWER TRANSCOWL REF GREO #670-54-21-971, REV (-B), STEP 1-3. COMPLIED WITH SKApr 27, 2026 · N770SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026042776421Stand Off · crackedRT UPPER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. INSTALLED NEW RT UPPER TRANSCOWL INBD -A- BRACKET REF REO# 670-54-21-971, REV B, DATED 11/28/23. SEE CONTINUATION SHEET FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKYApr 27, 2026 · N770SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026042776370Bracket · crackedLEFT LOWER TRANSCOWL OTBD -A- BRACKET STANDOFF IS CRACKED. INSTALLED NEW LT LWR TRANSCOWL O/B -A- BRACKET REF REO# 670-54-21-971, REV B, COMPLIED WITH TASK CARD 51-900-1002-SKY.Apr 27, 2026 · N770SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026042776368Rivet · looseLEFT UPPER TRANSCOWL ZEE STIFFENER RIVETS ARE PULLED LOOSE. REPAIRED UNDERLYING HOLES COMMON TO ZEE STIFFENER AND INNER PERFORATED SKIN ON LT UPPER TRANSCOWL, REF. REO 670-54-21-1824, REV. --.Apr 27, 2026 · N770SK · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2026042376410Slat Track · damagedLEFT SLAT TRACK 1-2 HAS FRETTING MARKS ON THE TRACK. PERFORMED REPAIR OF LT SLAT TRACK 1-2 PER REO 670-57-42-2496 REV --. OPS CHECKS GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.Apr 23, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026042376389Slat Track · wornRIGHT HAND SLAT TRACK 3-2 HAS WEAR MARKS ON THE LOWER SURFACE AND UPPER INNER SIDE. COMPLIED WITH ALL STEPS OF REO 670-57-42-2502 REV -- FOR REPAIR OF RH SLAT TRACK 3-2 OPS AND RIG CHECK GOOD SEE CONTINUE CARD FOR DETAILS.COMPLIED WITH 51-900-1002-SKY.Apr 23, 2026 · N770SK · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2026042276431Support · crackedAFT CARGO DOOR TRACK LOWER SUPPORT IS CRACKED THROUGH FASTNERS. REMOVED & INSTALLED AFT CARGO DOOR TRACK LOWER SUPPORT NEW CHANNEL IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 REV.38 & DWG MM670-35060 REV. W. IN RESTORED FINISH. COMPLIED WITH ALApr 22, 2026 · N770SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA2026042276385Guide · chafedAFT CARGO DOOR TRACK GUIDE IS CHAFED AND NICKED. (C-CHECK RO 07/01/2026)REMOVED AND INSTALLED NEW AFT CARGO DOOR TRACK GUIDE BRACKET ROLLER GUIDE AFT PN: CC670-38814-1SB (01 EA.), ROLLER GUIDE LOW AFT PN: CC670-38811-1 (01 EA.) AND ROLLER GUIDE UP AFT PN: CC6Apr 22, 2026 · N770SK · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA2026042176430Drag Angle · crackedLH FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED LT FUSELAGE TO VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Apr 21, 2026 · N770SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA2026042176379Drag Angle · crackedRIGHT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED RT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Apr 21, 2026 · N770SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA2026042076417Skin · crackedLEFT TRU BAY DOOR CUT-OUT, AFT LOWER CORNER POSSIBLE FUSELAGE SKIN CRACKED AT THE RADIUS. REPLACED LT HYDRAULIC BAY SKIN PANEL, JUST BELOW TRU BAY DOOR CUT OUT, REF SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001-A01 & DWG CC670-33040 REV G AND DWG CC670-320Apr 20, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026042076415Housing · chafedSERVICE DOOR EXTERIOR HANDLE HOUSING IS CHAFFED AT THE FORWARD RADIUS. REMOVED AND REPLACED CHAFFED SERVICE DOOR EXTERIOR HANDLE HOUSING WITH NEW HOUSING USING ALL NEW HARDWARE INTO THE SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND DWG CC670-38103 REV -C. ALApr 20, 2026 · N770SK · Cndair CL6002C10 · Service DoorsSDR SWIA2026042076377Skin · crackedRH TRU BAY DOOR CUT-OUT, AFT LOWER CORNER POSSIBLE FUSELAGE SKIN CRACKED AT THE RADIUS. REPLACED ADG SKIN WITH SERVICEABLE SKIN PANEL REF. DWG CC670-33040 REV-G, DWG CC670-32010 REV-F, SRM 51-42-06-001-001-A01 REV. 38, SRM 51-42-21-001-001-A01 REV. 38, SRM 5Apr 20, 2026 · N770SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026022675355Actuator · warning messageSTEERING INOPERTIVE CAUTION MESSAGE IMMEDIATELY AFTER GEAR DOWN HANDLE MOVEMENT. BROUGHT THE GEAR BACK UP. RAN QRH AND LANDED AND STOPPED ON RUNWAY WITH NO FURTHER ISSUES. (FLIGHT 4993) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31784729. SEE CP 31786397 Feb 25, 2026 · N770SK · Cndair CL6002C10 · Landing Gear Steering SystemSDR SWIA2026021775291Windshield · crackedR WINDSHIELD HEAT CAUTION..RAN QRH IT FIXED BUT WE HAVE MULTIPLE CRACKS ON FO WINDSHIELD AND SOME BURN/SCORCH MARKS (FLIGHT 6403) REMOVED CRACKED RH WINDSHIELD AND INSTALLED SERVICEABLE RH WINDSHIELD PER THE CRJ 700 AMM 56-11-01 AND TASK CARD 56-220-1000-SKY.Feb 17, 2026 · N770SK · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2024051308Warning Message · illuminatedPASSENGER DOOR WARNING IN FLIGHT (FLIGHT 3174 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28208488 WITH THE FOLLOWING CORRECTIVE ACTION: "SEE CP-28208491 AND CP-28208492 FOR CORRECTIVE ACTION"May 8, 2024 · N770SK · Cndair CL6002C10 · Door Warning SystemSDR SWIA2024050900008Warning Message · illuminatedPASSENGER DOOR WARNING IN FLIGHT (FLIGHT 3174 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.May 8, 2024 · N770SK · Cndair CL6002C10 · Door Warning SystemSDR SWI2024F00284Seat Track · missingSEAT TRACK EXTRUSION MISSING AT SEAT 12B. (FILED CLOSED)INSTALLED SERVICEABLE SEAT TRACK EXTRUSION AT SEAT12B. REFERENCE APPLICABLE STEPS IN CRJ700AMM 25-21-01Apr 9, 2024 · N770SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00283Seat Track · wrong partSEAT TRACK AT SEAT10B IS THE WRONG COLOR. (FILED CLOSED)INSTALLED SERVICEABLE SEAT TRACK EXTRUSION AT SEA10B. REFERENCE APPLICABLE STEPS IN CRJ700AMM 25-21-01Apr 9, 2024 · N770SK · Cndair CL6002C10 · Fuselage, Powerplant Attach FittingsSDR SWI2024F00282Seat Track · wrong partSEAT TRACK AT SEAT 8B IS THE WRONG COLOR. (FILED CLOSED)INSTALLED SERVICEABLE SEAT TRACK EXTRUSION AT SEAT 8B. REFERENCE APPLICABLE STEPS IN CRJ700AMM 25-21-01Apr 9, 2024 · N770SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2024F00281Seat Track · damagedSEAT TRACK EXRUSION AT SEAT 6C IS DAMAGED. (FILED CLOSED)INSTALLED SERVICEABLE SEAT TRACK EXRUSION AT SEAT 6C, REFERENCE APPLICABLE STEPS IN CRJ700AMM 25-21-01Apr 9, 2024 · N770SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202404090001Seat Track · missingSEAT TRACK MISSING AT SEAT 4C. (FILED CLOSED)INSTALLED SERVICEABLE SEAT TRACK EXTRUSIONS AT SEATS 4C. REFERENCE APPLICABLE STEPS IN AMM 25-21-01Apr 9, 2024 · N770SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWI2023F00595Unknown · smokeD: RT PACK AUTO FAIL-SUSPECT ACM FAILUREC:MEL 21-51-1BCAT:"C" DUE 01/07/2024LIGHT SMOKE IN THE CABIN ON PUSH BACK BUT BEFORE ANY ENGINE STARTUP. (FLIGHT 3200 FILED CLOSED)DEC 28, 2023 STATION: PHX--PLEASE REFERENCE AML 1269896T/S SMOKE IN CABIN PER CRJ700 SL-Dec 28, 2023 · N770SK · Cndair CL6002C10 · Air Distribution SystemSDR SWIA202308154Unknown · delaminatedTRANSFER FROM EAML 1192174 : DURING WALK AROUND FOUND DELAMINATION DAMAGE ON NOSE RADOME, DETERMINED THE DAMAGED TO BE OUT OF LIMITS. (FILED CLOSED)REMOVED AND REPLACED NOSE RADOME IN REFERENCE WITH CRJ AMM 53-81-80.Aug 14, 2023 · N770SK · Cndair CL6002C10 · Aerodynamic FairingsSDR SWIA20230207Not Reported · damagedHSTA R/H UPPER FITTING IS DAMAGED. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 WILL BE REQUIRED. (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSFeb 7, 2023 · N770SK · Cndair CL6002C10 · Horizontal Stabilizer, Plate/SkinSDR SWIA20230206Not Reported · dentedLEFT FUSELAGE STRUCTURE DENTED BY FS169.00 IN BETWEEN RADOME AND ACCESS PANEL 121 AL HAS BEEN EVALUATED AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-31. REFERENCE FOR CP 26143452 FOR INITAL DISCREPANCY. THIS IS A "MAJOR REPAIR". FORM M-337 INITIATED. (FILED CLOFeb 6, 2023 · N770SK · Cndair CL6002C10 · Horizontal Stabilizer, Tab StructureSDR SWIA20230130Not Entered · warning messageRIGHT FADEC CAUTION MESSAGE APPEARED IN CRUISE. COMPLIED WITH QRH (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26148679 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED RH FADEC IAW CRJ 700 AMM 73-21-01. PERFORMED MULTIPLE ENGINE RUNSJan 30, 2023 · N770SK · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR SWIA202266428None · noneCAPTAIN SIDE WINDSHIELD BEGAN ARCING IN THE OUTER GLASS LAYER THEN SHATTERED (FLIGHT #3083 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25440295 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED CAPTAIN WINSHIELD REFERENCING AMM 56Sep 5, 2022 · N770SK · Cndair CL6002C10 · Window/Windshield SystemSDR SWIA202163869None · failedBINDING NOISES ON ELEVATOR DURING OPS CHECK. (C CHECK RO 1/16/2022) INSTALLED NEW R/H ELEVATOR NO.2 PCU ROD END HARDWARE IAW CRJ700 AMM 27-33-01-400-801-A01. TUC6233 CAL DUE 31-AUG-22.Dec 27, 2021 · N770SK · Cndair CL600* · Elevator Tab, Attach FittingsSDR SWIA202163859None · damagedFLOOR 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 1/16/2022) REMOVED AND REPLACED FLOOR SEAT TRACK FROM 17AB TO 13AB AT LBL9.0 RDec 22, 2021 · N770SK · Cndair CL600* · Fuselage, Powerplant Attach FittingsSDR SWIA202163850None · distortedBRACKET AT F.S. 1000.0 STGR 23L (P/N MM670-43600-003) IS DISTORTED. (C CHECK RO 1/16/2022) REPLACED BRACKET AT FS1000 STGR 23L WITH NEW BRACKET REF CRJ-700 SRM 51-42-06-001-001-A01, DWG MM670-43600 REV NC. COMPLIED WITH TASK CARD 51-900-1002-SKY.Dec 9, 2021 · N770SK · Cndair CL600* · Fuselage Structure (General)SDR SWIA202163864None · crackedWHILE PERFORMING FUSELAGE SKIN DENT REPAIR AT FS1015 FOUND INNER CHORD BTWN FS1015-1031 TO BE CRACKED (C CHECK RO 1/16/2022) REMOVED AND REPLACED INNER CHORD FROM FS1015 TO FS1031 WITH NEW P/N MM670-35669-001 IAW CRJ700 SRM 51-42-21-001-001-A01Dec 7, 2021 · N770SK · Cndair CL600* · Fuselage Main, KeelSDR SWIA202163849None · wornLH UPPER TRANSCOWL LATCH DOOR CHANNELS WORN ( PN CN624-2048-201 AND PN CN624-2049-201) (C CHECK RO 1/16/2022) REMOVED AND INSTALLED NEW CHANNEL P/N CN624-2048-201, AND NEW CHANNEL P/N CN624-2049-201 REF. CRJ700 SRM 51-42-10-001-001-A01 & REO 670-54-21-1494Dec 2, 2021 · N770SK · Cndair CL600* · Powerplant System
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