N445SW

Service difficulty reports · 275

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 = 'N445SW' 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 SWIA2020090452217Pressure Panel · corrodedLT PRESSURE FS PANEL HAS SEVERAL AREAS OF CORROSION. C-CHECK RO 9/1/2020. REMOVED CORROSION FROM LT PRESSURE FS PANEL REF CRJ 200 SRM. BLENDED AREA FOUND TO BE WITHIN LIMITS REF REO. SEE CONTINUATION CARD FOR DETAILS.Jul 27, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020090452216Strap · corrodedTOP CAP @ FS 559.0 RBL 27 TO SILL HAS CORROSION. C-CHECK RO 9/1/2020. REPLACED FLOOR STRAP AT RBL 27 & FS.559.00, FLOOR STRAP P/N 601R31025-29 WITH NEW FASTENERS PER CRJ200 SRM REF. BOMBARD. DRAWING. COMPLIED WITH SKYWEST TASK CARD, LEAK CHECK GOOD NO DEFEJul 27, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452215Strap · corrodedTOP STRAP @ FS 559.0 LBL 27 TO SILL HAS CORROSION. C-CHECK RO 9/1/2020. REPLACED 559 LBL27 TOP STRAP, REF. CRJ200 SRM AND BOMBARDIER DRAWING. NO LEAKS DETECTED ON PRESSURE LEAK CHECK. COMPLIED WITH SKYWEST TASK CARD.Jul 27, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452279Intercostal · corrodedLT OVERWING EMERGENCY EXIT DOOR INTERCOSTAL BELOW THE LATCH HANDLE HAS 11 RUSTY NUT PLATES AND CORROSION ON THE FLANGE. LT OVERWING EMERGENCY EXIT DOOR INTERCOSTAL BELOW THE LATCH HANDLE REPLACED 11 NUT PLATES REF CRJ 200 SRM.Jul 24, 2020 · N445SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA2020090452214Skin · dentedRT INBOARD FLAP UPPER SKIN HAS DENTS AT WS 73 10" FROM TRAILING EDGE AND WS 76 14" FROM TRAILING EDGE. EVALUATE AND REMOVE DAMAGE, OR FILL AND PAINT. C-CHECK RO 9/1/2020. REPAIRED RT INBOARD FLAP UPPER SKIN, REF CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAJul 24, 2020 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090452308Bulkhead · scratchedFS 621 BULKHEAD HAS A 9? SCRATCH AT APPROXIMATELY LBL 24. BLENDED DAMAGE ON FS 621 BULKHEAD AT APPROXIMATELY LBL 24, REF CRJ-200-SRM. BLENDED AREA WAS FOUND TO BE OUT OF LIMITS, REF REO. REPAIRED FS 621 BULKHEAD AT APPROXIMATELY LBL 24, REF REO.Jul 23, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020090452278Angle · bentLT INBOARD FLAP FWD RIB, BOTTOM RIB ANGLE BENT UP AND NOT SECURED. RIB IS ON THE INBOARD SIDE OF THE OUTER HINGE ARM. REMOVED AND INSTALLED SERVICEABLE LT INBOARD FLAP, REF CRJ 200 AMM. PERFORMED OPERATIONAL TEST OF THE FLAPS IAW CRJ 200 AMM, TEST GOOD.Jul 23, 2020 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090452213Bulkhead Web · dentedFS621 BULKHEAD HAS A DENT AND CHAFE MARK 3" ABOVE FLOOR AT APPROXIMATELY LBL32. C-CHECK RO 9/1/2020. REPAIRED FS621 BULKHEAD 3" ABOVE FLOOR AT APPROXIMATELY. LBL32, REF REO. SEE CONTINUATION CARD FOR DETAILS COMPLIED WITH SKYWEST TASK CARD.Jul 23, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020090452273Attach Bracket · crackedFS449.85 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED. REMOVED AND REPLACED PANEL 162EL ATTACH BRACKET WITH NEW P/N 601R31037-48 AT FS 449.85, REF CRJ200 SRM.Jul 22, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020090452272Attach Bracket · crackedFS461.00 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED (MARKED). C-CHECK RO 9/1/2020. INSTALLED NEW OVER WING PANEL 162EL ATTACH BRACKET P/N, REF CRJ200 SRM.Jul 22, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020090452271Attach Bracket · crackedAFT OF FS473.15 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED ANGLE AT FS473.15, REF CRJ-200-SRM. SEE CONTINUATION CARD FOR DETAILS.Jul 22, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020090452270Attach Bracket · crackedFWD OF FS473.15 AND UNDER OVERWING PANEL 162EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED. REMOVED AND REPLACED OVER WING PANEL ATTACH BRAKET FWD OF FS473.15, REF CRJ200 SRM.Jul 22, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020090452269Attach Bracket · crackedFWD OF FS473.15 AND UNDER OVERWING PANEL 161EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED. REMOVED AND INSTALLED NEW ATTACH BRACKET FWD OF FS473.15 AND UNDER OVERWING PANEL 161EL, REF CRJ-200-SRM.Jul 22, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020090452212Skin · chafedRT AILERON EXTERIOR SKIN CHAFFED ON BOTTOM INBOARD AND OUTBOARD LEADING EDGES (MARKED). C-CHECK RO 9/1/2020. REMOVED CHAFE DAMAGE FROM THE RT AILERON OUTBOARD LEADING EDGE SKIN, EVALUATED AND FOUND TO BE WITHIN LIMITS, REF.CRJ200 SRM. REMOVED RT AILERON LOWJul 22, 2020 · N445SW · Cndair CL6002B19 · AileronsSDR SWIA2020090452211Skin · chafedRIGHT WING LOWER PLANK CHAFE FROM FAIRING AT RBL 45. C-CHECK RO 9/1/2020. REPAIRED RIGHT WING LOWER PLANK AT RBL 45, REF REO. SEE CONTINUATION CARD FOR DETAILS.Jul 22, 2020 · N445SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202052210Attach Fitting · gougedRT OUTBOARD FLAP AFT HINGE BOX ATTACH FITTING, OUTBOARD ATTACH POINT INBOARD LUG GOUGED. C-CHECK RO 9/1/2020. BLENDED RT OUTBOARD FLAP, AFT HINGE BOX, OUTBOARD ATTACH POINT, INBOARD LUG REF CRJ-200 SRM. SUBMITTED TO ENGINEERING. RECEIVED AND COMPLIED WITH MJul 22, 2020 · N445SW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR SWIA2020090452209Attach Bracket · crackedAFT OF FS473.15 AND UNDER OVERWING PANEL 161EL THE PANEL ATTACH BRACKET ANGLE IS CRACKED (MARKED). C-CHECK RO 9/1/2020. REMOVED AND REPLACED BRACKET ANGLE, P/N 601R31037-33, AT AFT OF FS473.15 AND UNDER OVERWING PANEL 161EL, REF CRJ200 SRM AND DWG. C/W ATTAJul 22, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2020090452277Linkage · corrodedRUDDER POSITION TRANSMITTER LINKAGE HAS CORRODED HARDWARE. C-CHECK RO 9/1/2020. REMOVED AND REPLACED CORRODED HARDWARES ON THE RUDDER TRANSMITTER LINKAGE PER REF CRJ 200 AMM AND CRJ 200 AMM.Jul 21, 2020 · N445SW · Cndair CL6002B19 · Rudder Control SystemSDR SWIA2020090452276Link · corrodedRT OUTBOARD GROUND SPOILER PCU LINK HARDWARE IS CORRODED. C-CHECK RO 9/1/2020. INSTALLED NEW HARDWARE ON RT OUTBOARD GROUND SPOILER PCU LINK, REF CRJ 200 AMM.Jul 21, 2020 · N445SW · Cndair CL6002B19 · AileronsSDR SWIA2020090452275Link · corrodedRT INBOARD GROUND SPOILER PCU LINK HARDWARE IS CORRODED. INSTALLED NEW HARDWARE ON RT INBOARD GROUND SPOILER PCU LINK, REF CRJ 200 AMM. OPERATIONS CHECK GOOD.Jul 21, 2020 · N445SW · Cndair CL6002B19 · AileronsSDR SWIA2020090452208Hinge Fitting · gougedRT ELEVATOR HINGE FITTING ON THE HORIZONTAL STABILIZER, CENTER POSITION, HAS A GOUGE (MARKED). C-CHECK RO 9/1/2020. BLENDED GOUGE FROM RT ELEVATOR HINGE FITTING ON THE HORIZONTAL STABILIZER, CENTER POSITION, REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OFJul 21, 2020 · N445SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2020090452207Window Post · crackedRT WINDSHIELD SIDE POST LOWER OUTBOARD CLIP CRACKED. C-CHECK RO 9/1/2020. REMOVED RT WINDSHIELD SIDE POST LOWER OUTBOARD CLIP (FITTING), REF CRJ200 SRM & INSTALLED NEW CLIP (FITTING) AT RT WINDSHIELD SIDE POST LOWER OUTBOARD, REF CRJ200 SRM AND BOMBARDIER DWJul 21, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020090452206Support · gougedCARGO DOOR TACK SUPPORT STRUCTURE OUTBOARD BEAM MEMBER IS GOUGED AT THE FWD END BELOW THE CABLE PULLEY (MARKED). C-CHECK RO 9/1/2020. REPLACED AND INSTALLED NEW OUTBOARD BEAM MEMBER, P/N 601R35050-64 PO:T000055969/1, AT CARGO TRACK SUPPORT STRUCTURE FS574.00Jul 21, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452205Support · crackedCARGO DOOR TACK SUPPORT STRUCTURE CLIP ANGLE AT THE FORWARD END OF THE BEAM IS CRACKED.(FLAGGED). C-CHECK RO 9/1/2020. REPLACED CLIP ANGLE, PN 601R35050-121, WITH NEW PART PER CRJ 200 SRM & BOMBARDIER DWG. SEE CONTINUE CARD FOR DETAILS.Jul 21, 2020 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020090452204Vane · chafedRT INBOARD FLAP VANE SKIN CHAFED AT THE CENTER OF THE LEADING EDGE. C-CHECK RO 9/1/2020. REMOVED AND REPLACED WITH NEW RT INBOARD FLAP CENTER VANE SKIN, REF CRJ 200 SRM AND BOMBARIDER DWG. COMPLIED WITH SKYWEST TASK CARD.Jul 21, 2020 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090452203Skin · chafedRT AILERON UPPER LEADING EDGE OUTBOARD SKIN IS CHAFFED. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW RT AILERON UPPER LEADING EDGE SKIN, PART # CC670-13052-4 REF CRJ-200-SRM, AND BOMBARDIER DRAWING. SEE CONTINUATION CARD FOR DETAILS.Jul 20, 2020 · N445SW · Cndair CL6002B19 · AileronsSDR SWIA2020090452306Cam · chafedPASSENGER DOOR SURROUND AFT CAM CHAFED THROUGH PROTECTIVE COATING. REPLACED CHAFED AFT DOOR CAM? AND SHIM WITH NEW DOOR CAM AND SHIM P/N 600-31688-18 AND 600-31900-83, REF CRJ 200 SRM.Jul 18, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452305Cam · chafedPASSENGER DOOR SURROUND FORWARD CAM CHAFED THROUGH PROTECTIVE COATING. REPLACED CHAFED FWD DOOR CAM? AND SHIM WITH NEW DOOR CAM AND SHIM P/N 600-31688-17 AND 600-31900-83, REF CRJ 200 SRM.Jul 18, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452304Stop Fitting · chafedLEFT AFT AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE CHAFED. INSTALLED NEW PART LEFT AFT AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE, PER CRJ 200 SRM.Jul 18, 2020 · N445SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020090452303Stop Fitting · chafedRIGHT FORWARD AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE CHAFED. REMOVED DAMAGED FWD RT AVIONICS BAY DOOR STOP FITTING, AND INSTALLED NEW P/N 601R38343-1, PER CRJ 200 SRM AND AMM TASK.Jul 18, 2020 · N445SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020090452302Stop Fitting · chafedLEFT FORWARD AVIONICS BAY DOOR STOP FITTING ON THE FUSELAGE CHAFED. REMOVED DAMAGED FWD LT AVIONICS BAY DOOR STOP FITTING, AND INSTALLED NEW P/N 601R38343-1, PER CRJ 200 SRM 51-41-02 AND AMM TASK.Jul 18, 2020 · N445SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020090452268Vane · crackedCRACK ON OUTBOARD MOVEABLE FLAP VANE AT APPROXIMATELY WS 226.51 TRAILING EGDE. REMOVED AND REPLACED RT OUTBOARD FLAP, REF CRJ200 AMM. ALL ASSOCIATED OPERATIONS CHECKS GOOD.Jul 18, 2020 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020090452202Housing · chafedCARGO DOOR OUTER HANDLE HOUSING CHAFED (MARKED). C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW CARGO DOOR HANDLE HOUSING, REF CRJ 200 SRM AND BOMBARIDER DWG 601R35027 REV-AY. COMPLIED WITH SKYWEST TASK CARD. ALL OPERATIONS CHECKS AND LEAK CHECK GOOD.Jul 18, 2020 · N445SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2020090452267Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE CRACKED NEAR PULLEY BRACKET. REMOVED AND INSTALLED NEW PASSENGER DOOR AFT DRAG ANGLE, REF CRJ 200 SRM.Jul 17, 2020 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2020090452201Pan · corrodedSERVICE DOOR LOWER FORWARD PAN HAS CORROSION (MARKED). C-CHECK RO 9/1/2020. REMOVED SERVICE DOOR CORROSION FROM LOWER FORWARD PAN, REF CRJ-200 AMM. BLENDED AREA FOUND TO BE OUT OF LIMITS, REF CRJ200 SRM. REPAIRED SERVICE DOOR LOWER FORWARD PAN, REF REO. SJul 17, 2020 · N445SW · Cndair CL6002B19 · Galley DoorsSDR SWIA2020090452200Housing · chafedSERVICE DOOR CHAFED 3 PLACES AROUND OUTER HANDLE CUTOUT (MARKED). C-CHECK RO 9/1/2020. BLENDED SERVICE DOOR CHAFES AT 3 PLACES AROUND OUTER HANDLE CUTOUT (MARKED), REF CRJ-200 REO. EVALUATED AND FOUND TO BE OUT OF LIMITS. SUBMITTED TO ENGINEERING. RECIEVEDJul 17, 2020 · N445SW · Cndair CL6002B19 · Galley DoorsSDR SWIA2020090452199Skin · dentedDENT ON THE SERVICE DOOR BETWEEN THE 'C' AND 'T' LETTERING. EVALUATE AND REPAIR OR FILL AND PAINT AS NEEDED. C-CHECK RO 9/1/2020. REPAIRED DENT ON THE SERVICE DOOR BETWEEN THE 'C' AND 'T' LETTERING, REF MHIRJ REO. SEE CONTINUATION CARD FOR DETAILS.Jul 16, 2020 · N445SW · Cndair CL6002B19 · Galley DoorsSDR SWIA2020090452197Bracket · crackedD: EXTERNAL POWER SERVICE PANEL LOWER MOUNTING BRACKET HAS A 2" CRACK IN THE RADIUS OF THE BEND. REPAIR AT NEXT C CHECK C: MCI. C-CHECK RO 9/1/2020. REMOVED AND INSTALLED NEW EXTERNAL POWER SERVICE PANEL, REF CRJ-200 SRM, ENG. DWG. AND MHIRJ REO. SEE CONTJul 16, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2020090452274Bushing · wornREMOVE AND REPLACED BUSHINGS AND HARDWARE ON LT AILERON WING AFT SPAR, REF CRJ 200 AMM 20-26-00-910-804. REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LT AILERON WING AFT SPAR, REF CRJ 200 AMM AND CRJ 200 AMM.Jul 9, 2020 · N445SW · Cndair CL6002B19 · AileronsSDR SWIA2020090452195Bulkhead Web · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD-COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FWD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IAW AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND Jul 9, 2020 · N445SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019071646061Unknown · fireDURING SECOND ENGINE START WE HAD A HOT START. GROUND CREW INDICATED ENGINE FIRE. AFTER MOTORING THE ENGINE, THE GROUND CREW STILL INDICATED ENGINE FIRE. WE ELECTED TO RUN THE EXPEDITED DEPLANING CHECKLIST WHICH INCLUDING ACTIVATING THE FIRE BOTTLES. FIRE CREWJul 16, 2019 · N445SW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA2019012145455Rod · failedPASSENGER DOOR WARNING MESSAGE ON APPROACH. EMERGENCY DESCENT. DEPLOYED PAX O2 MASK. (FLT#3502) CLOSED REMOVED AND REPLACED PAX DOOR ROD. ALSO REPACKED OXYGEN GENERATORS. 6L AND 11R AND LAV FOUND NOT USED IAW AMM. REMOVED AND REPLACED REST OF OXYGEN GENERATORSJan 21, 2019 · N445SW · Cndair CL6002B19 · Door Warning SystemSDR SWIA2018070644862Crossbeam · corrodedCORROSION FOUND ON FLOOR SUPPORT CROSS BEAM UNDER NYLON PAD AT FS 349.0 AT LBL 39.0. (C-CHECK) RO: 07/03/2018 REMOVED AND INSTALLED NEW ANGLE IAW SRM.Jun 7, 2018 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018070644857Floorbeam · crackedFS 280 FLOORBEAM CRACKED AT RBL 9 ON FS 280 FLOORBEAM. (C-CHECK) RO: 07/03/2018 COMPLIED WITH PERMANENT REPAIR FS 280 FLOORBEAM BULKHEAD IAW REO.Jun 2, 2018 · N445SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2018070644856Intercostal · crackedPAX DOOR INTERCOSTAL DD1 (P/N:601R31902-318) CRACKED ON UPPER FLANGE. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL IAW SRM.Jun 1, 2018 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018070644855Intercostal · crackedPAX DOOR INTERCOSTAL DD7 (P/N:601R318825-1) CRACKED ON UPPER FLANGE. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED PAX DOOR INTERCOSTAL IAW SRM.Jun 1, 2018 · N445SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018070644861Door Sill · corrodedAFT CARGO DOOR LOWER SILL HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES FROM FS 574.00 TO FS 621.00. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED AFT CARGO DOOR LOWER SILL IAW REO. LEAK CHECK GOOD AT THIS TIME.May 31, 2018 · N445SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2018070644854Cargo Track · corrodedAFT CARGO SEAT TRACK CAP AT LBL 27.00 HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES BETWEEN FS 559.00+112 TO FS 574.00. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACE CARGO FLOOR BEAM CAP FROM FS559+112 TO 574 IAW REO AND SRM.May 31, 2018 · N445SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2018070644860Angle · corrodedCLIP (ANGLE) ON FWD LWR AREA OF BATT RIB LOCATED AT WS 58.88 IS CORRODED. (C-CHECK) RO: 07/03/2018 REMOVED AND REPLACED WITH NEW CLIP P/N 601R10205-7 IAW SRM.May 30, 2018 · N445SW · Cndair CL6002B19 · Wing Miscellaneous StructureSDR SWIA2018070644859Floor Panel · corrodedLT PRESSURE FLOOR SILL, FLOOR PANEL HAS AREAS OF CORROSION FROM FS 409+128 - FS 559. (C-CHECK) RO: 07/03/2018 REMOVED CORROSION FROM LT PRESSURE FLOOR SILL, FLOOR PANEL IAW REO. PRESSURE CHECK GOOD AT THIS TIME.May 30, 2018 · N445SW · Cndair CL6002B19 · Fuselage Floor Panel
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