N440SW

Service difficulty reports · 245

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 = 'N440SW' 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 SWIA2020030348930Fitting · cracked*CLIP COMMON TO THE STGR15R INTERCOSTAL ON THE AFT SIDE OF THE FS621.00 BULKHEAD AND THE OUTER SKIN IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW CLIP (PART # 601-35012-41) AT THE STGR15R INTERCOSTAL ON THE AFT SIDE OF THE FS621.Jan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348929Fitting · cracked*CLIP COMMON TO THE STGR14R INTERCOSTAL ON THE AFT SIDE OF THE FS621.00 BULKHEAD AND FRAME FS625.30 IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REPLACED WITH NEW CLIP COMMON TO INTERCOSTAL AT FS625, STR14R REF BOMBARDIER DWG SRM.Jan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348928Fitting · cracked*CLIP COMMON TO THE STGR14L INTERCOSTAL ON THE AFT SIDE OF THE FS621.00 BULKHEAD AND FRAME FS625.30 IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED WITH NEW CLIP COMMON TO INTERCOSTAL AT FS625, STR14L REF BOMBARDIER DWG SRM.Jan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348927Channel · cracked*CHANNEL ON THE OUTBOARD END OF INTERCOSTAL AT STGR14L ON THE AFT SIDE OF THE FS621.00 BULKHEAD IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED CHANNEL ON THE OUTBOARD END OF INTERCOSTAL AT STGR14L ON THE AFT SIDE OF THE FS621.00 REF CRJJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348926Fitting · cracked*CLIP AT THE TOP OF THE LBL9 VERTICAL BEAM ON THE AFT SIDE OF THE 621.00 BULKHEAD IS CRACKED.(FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW CLIP (PART # 601-35012-5) AT THE TOP OF THE LBL9.0 VERTICAL BEAM ON THE AFT SIDE OF THE 621.00 BULKHEAJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348925Door Sill · corroded* THE RH CABIN FLOOR SILL HAS CORROSION IN MULTIPLE SPOTS BETWEEN APPROX. FS 349 AND APPROX. FS 364. (C-CHECK) RO 2/28/2020 BLENDED CORROSION, FOUNUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH CABIN FLOOR SILL AT FS 349.0 TO FS 409+20,REF CRJ-200 SJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348924Door Sill · corroded* THE RH CABIN FLOOR SILL HAS CORROSION IN MULTIPLE SPOTS BETWEEN APPROX. FS 295 AND APPROX. FS 319. (C-CHECK) RO 2/28/2020 REMOVED CORROSION ON R/H CABIN FLOOR SILL BETWEEN FS 295 TO FS 319, ORIGINAL PART THICKNESS = .063", MATERIAL REMOVED = .036", MATERJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348923Intercostal · corroded* THE INTERCOSTAL IN THE AVIONICS BAY, FORWARD OF THE DOOR CUTOUT, BETWEEN FS 349 AND FS 364 TO THE RH SIDE OF STRINGER 27, COMMONLY REFERED TO AS STRINGER 27R, HAS CORROSION IN MULTIPLE SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED INTERCOSTALBETWEENJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348922Deck Plate · cracked*CRACK IN THE LEFT TRU BAY DECK BETWEEN THE GAGGE MOUNTING PLTE ANE THE EDGE OF THE TRU BAY. (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED PERMANENT CRACK REPAIR TO LEFT TRU BAY DECK BETWEEN THE GAUGE MOUNTING PLATE AND THE EDGE OF THE TRU BAY. REF BOMBARDIERJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348921Intercostal · corroded* THE INTERCOSTAL IN THE AVIONICS BAY, FORWARD OF THE DOOR CUTOUT, BETWEEN FS 349 AND FS 364 TO THE LH SIDE OF STRINGER 27, COMMONLY REFERED TO AS STRINGER 27L, HAS CORROSION IN MULTIPLE SPOTS. (C-CHECK) RO 2/28/2020 REMOVED CORRODED & INSTALLED NEW INTERCJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030348920Frame · corroded* THE FRAME FORWARD OF THE AVIONCS DOOR, FS 364, HAS CORROSION ON ITS FORWARD FACE'S WEB AND LOWER ANGLE, AND CHAFE MARKS ALONG ITS UPPER ANGLE BETWEEN STRINGERS 25L AND 25R. (C-CHECK) RO 2/28/2020 INSTALLED NEW FS364 FRAME SECTOR, SHEAR CLIP, REINFORCEMENJan 10, 2020 · N440SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020030348919Support Channel · cracked* THE CARGO DOOR FORWARD TRACK'S LOWER AFT SUPPORT/MOUNTING CHANNEL IS CRACKED. ( MARKED WITH ORANGE FLAG TAPE) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW CHANNEL P/N 6001R35050-25 AT CARGO DOOR FORWARD TRACK'S LOWER AFT SUPPORT/MOUNTING REF BOMBARDIJan 10, 2020 · N440SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA2020030348989Plate · chafed* THE RH OUTBD FLAP CENTER HINGE ARM SIDE PLATE IS CHAFFED. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CHAFED AND INSTALLED NEW RH OUTBD FLAP CENTER HINGE ARM SIDE PLATE REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.Jan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348988Plate · chafed* THE RH INBD FLAP INBD HINGE ARM INBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP INBD HINGE ARM ONBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOODJan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348987Plate · chafed* THE RH INBD FLAP OUTBD HINGE ARM OUTBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP OUTBD HINGE ARM OUTBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOOD.Jan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348986Plate · chafed* THE RH INBD FLAP OUTBD HINGE ARM INBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP OUTBD HINGE ARM INBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOODJan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348983Fastener · corroded* THE RH OUTBD FLAP INBD HINGE ARM LOWER FITTING FLAP SIDE HAS CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 REMOVED THE ANTI-ROTATION KEEPER (CORRODED HARDWARE) FROM THE INBD HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. REMOVED THE CORRODED HARDWARE FRJan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348982Fastener · corroded* THE RH OUTBD FLAP INBD HINGE BOX HAS CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED 4EA SCREWS AND 4EA WASHERS LOACTED ON ON RH OUTBOARD FLAP, INBOARD MOST HINGE REF CRJ-200 SRM.Jan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348981Fastener · corroded* THE RH OUTBD FLAP CENTER HINGE ARM HAS CORRODED HARDWARE FOR KEEPER PLATE. (C-CHECK) RO 2/28/2020 REMOVED THE ANTI-ROTATION KEEPER (CORRODED HARDWARE) FROM THE CENTER HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. INSTALLED THE ANTI-ROTATION KEEPER Jan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348980Fastener · corroded* THE RH AILERON OUTBD HIGNE FITTING WING SIDE HAS CORRODED HARDWARE FOR ANTI ROTATION PLATE. (C-CHECK) RO 2/28/2020 ORDERED AND RECIEVED HARDWARE 1(EA) BOLT, 1(EA) WASHER AND 1(EA) FOR ANTI ROTATION PLATE ON RH OTBD HINGE FITTING ANTI-ROATATION PLATE SEEJan 9, 2020 · N440SW · Cndair CL6002B19 · Wing, Control Surface Attach FittingsSDR SWIA2020030348979Fastener · corroded* THE RH AILERON HAS MULTIPLE LOCATIONS OF CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 ORDERED AND RECIEVED NEW FROM STOCK 3 BOLTS, 8EA WASHERS, 2EA NUTS AND 2 EA COTTER FOR CORRODED HARDWARE ON RH AILERON. FOR INSTALLATION DETAILS SEE JOB 2758985, OP 5175 Jan 9, 2020 · N440SW · Cndair CL6002B19 · AileronsSDR SWIA2020030348918Skin · crackedRH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 AT REAR SPAR HAS CRACK. (C-CHECK) RO 2/28/2020 REPAIRED RH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 AT REAR SPAR HAS CRACK.REF CRJ BOMBARDIER REO. SEE CONTINUATION FOR DETAIL.Jan 9, 2020 · N440SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030348917Skin · crackedLH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 HAS CRACK. (C-CHECK) RO 2/28/2020 REPAIRED LH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 AT REAR SPAR HAS CRACK.REF CRJ BOMBARDIER REO. SEE CONTINUATION FOR DETAIL.Jan 9, 2020 · N440SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030348916Angle · corrodedMAIN AVIONICS DOOR AFT ANGLE HAS CORROSION AS MARKED. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED THE MAIN AVIONICS DOOR AFT ANGLE REF CRJ 200 SRM. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.Jan 9, 2020 · N440SW · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR SWIA2020030348915Hinge · corroded* THE RH OUTBD FLAP MIDDLE HINGE BOX HAS CORROSION ON THE AFT SIDE. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM RH OUTBD FLAP MIDDLE HINGE BOX AND FOUND REWORKED AREA ACCEPTABLE AS IS REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**Jan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348914Hinge · corroded* THE RH OUTBD FLAP INBD HINGE BOX HAS CORROSION ON AFT SIDE. (MARKED). (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM RH OUTBD FLAP INBD HINGE BOX AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RJan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348913Hinge Arm · chafed* THE RH OUTBD FLAP CENTER HINGE ARM IS CHAFFED. (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED BLEND OUT REPAIR TO CHAFE ON THE RH OUTBD FLAP CENTER HINGE ARM. REF: BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.Jan 9, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348912Attach Fitting · gougedLEFT WING OUTBOARD FLAP BOX ATTACH FITTINGS #4 AFT INBOARD SIDE HAS A GOUGE AS MARKED. (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND OUT REPAIR TO GOUGE LEFT WING OUTBOARD FLAP BOX ATTACH FITTINGS #4 AFT INBOARD SIDE. REF CRJ 200 & BOMBARDIER REO. SJan 8, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348911Attach Fitting · gougedLEFT WING FLAP BOX ATTACH FITTINGS #1 AFT INBOARD HAS A GOUGE APPROX WS56.03 AS MARKED (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND OUT REPAIR TO GOUGE ON LEFT WING FLAP BOX ATTACH FITTINGS #1 AFT INBOARD APPROX WS56.03. REF. CRJ 200 & BOMBARDIER REJan 8, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348910Skin · chafedLH AILERON UPPER SKIN LEADING EDGE HAS CHAFING DAMAGE AS MARKED (C-CHECK) RO 2/28/2020 BLENDED OUT CHAFE DAMAGE ON LH AILERON UPPER SKIN LEADING EDGE. REF CRJ (TR51-44) SRM.- ORIGINAL MATERIAL THICKNESS OF LH AILERON UPPER SKIN LEADING EDGE IS .090" NON CHJan 8, 2020 · N440SW · Cndair CL6002B19 · AileronsSDR SWIA2020030348978Fastener · corroded* THE RH ELEVATOR INBD FLUTTER DAMPER ATTACHING HARDWARE TO LINK HAS CORROSION. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW HARDWARE FOR THE R/H ELEVATOR INBOARD AND OUTBOARD FLUTTER DAMPER ATTACHING TO LINKS REF CRJ200 AMM. ALL CHECKS GOOD.Jan 7, 2020 · N440SW · Cndair CL6002B19 · Elevator Miscellaneous StructureSDR SWIA2020030348977Fastener · corroded* THE LH ELEVATOR FLUTTER DAMPERS ATTACHING HARDWARE TO LINKS HAS CORROSION. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW HARDWARE FOR THE L/H ELEVATOR INBOARD AND OUTBOARD FLUTTER DAMPER ATTACHING TO LINKS REF CRJ200 AMM. ALL CHECKS GOOD.Jan 7, 2020 · N440SW · Cndair CL6002B19 · Elevator Miscellaneous StructureSDR SWIA2020030348975Splice Plate · corroded*LH ENGINE AFT PYLON UPPER AND LOWER SPLICE PLATES ARE CORRODED AS MARKED (C-CHECK) RO 2/28/2020 REPAIRED LH ENGINE AFT PYLON UPPER AND LOWER SPLICE PLATES THAT ARE CORRODED AS MARKED BY INSTALLING (4EACH) NEW REPLACEMENT BONDING PLATES PER BOMBARDIER RIL.Jan 7, 2020 · N440SW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2020030348993Mount · chafed* RIGHT WING OUTBOARD FLAP VANE MOUNTS ARE CHAFFED / GALLED AT 4 PLACES. MARKED. (C-CHECK) RO 2/28/2020 REMOVED GOUGED OUT OF LIMITS VANE ASSY AND INSTALLED NEW RH OUTBOARD FLAP VANE ASSY. PART # 601R14502-2. REF CRJ200 SRM AND BOMBARDIER DWG. SEE ATTACHEJan 6, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348976Plate · corroded* RIGHT PYLON TRAILING EDGE UPPER BONDING PLATES ARE CORRODED. (C-CHECK) RO 2/28/2020 COMPLIED WITH BOMBARDIER RIL# 1166, REV. C, DATED 17-JUL-2007. REMOVED DAMAGED RH PYLON T/E UPPER BONDING PLATES 2EA, CLEANED AND INSTALLED BONDING PLATES 601-37012-33 (Jan 6, 2020 · N440SW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR SWIA2020030348908Skin · chafed* RIGHT WING INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED AT 3 SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW RH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.Jan 6, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348907Skin · chafed* LEFT WING INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED AT 3 SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW LH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.Jan 6, 2020 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2020030348906Fairing · dentedADM #4953. DENT AT FUSELAGE STATION 559.00 + 112 LH SIDE AFT WING TO FUSELAGE FAIRING (PN 601R35232). DENT DIAMETER IS .750 INCHES BY 1.00 INCHES. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PJan 2, 2020 · N440SW · Cndair CL6002B19 · Aerodynamic FairingsSDR SWIA2019030348992Door Sill · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA - BLENDED AREA ALONG RH FLOOR SILL FS 493. RBL 43 FOUND TO BE OUT OF LIMITS. REPAIRED. REF REO. PERFORM DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, PART NUMBER: - , SERIAL NUMBER: 7589, POSITION: Dec 3, 2019 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019030348991Structure · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA - BLEND ON PREVIOUS REPAIR PART FOUND TO BE OUT OF LIMITS. RH PRESSURE FLOOR FS.442. REPAIRED PREVIOUS REPAIR REF REO. PERFORM DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, PART NUMBER: - , SERIAL NUDec 3, 2019 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019030348990Door Sill · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA - 3EA BLENDED AREAS ALONG LH FLOOR SILL FS.436, FS.442 AND FS.447 FOUND TO BE OUT OF LIMITS. REPAIRED. REF REO. PERFORM DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, PART NUMBER: - , SERIAL NUMBER: 7Dec 3, 2019 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019030348905Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODec 3, 2019 · N440SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201904195769Duct · damagedCABIN ALT WARNING. PERFORMED EMERGENCY DESCENT. MASKS DEPLOYED. (FLT#7410) REMOVED AND REPLACED LT PACK DISCHARGE DUCT IAW AMM. PERFORMED A PRESSURIZATION RUN IAW AMM. PRESSURIZATION RUN GOOD AT THIS TIME. REMOVED AND REPLACED O2 GENERATORS IAW AMM. PERFORMEDApr 17, 2019 · N440SW · Cndair CL6002B19 · Air Distribution SystemSDR SWIA201844154Vane · dentedFLAP VANE IS DENTED. (C-CHECK) RO: 1/15/2018. REMOVED AND REPLACED FLAP REF AMM.Jan 12, 2018 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201744155Door Sill · corrodedCARGO DOOR SILL HAS CORROSION. (C-CHECK) RO: 1/15/2018. REPLACED CARGO DOOR SILL PLATE REF SRM.Dec 18, 2017 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744153Structure · dentedFUSELAGE DENT BELOW PLACARD. (C-CHECK) RO:1/15/2018. REPAIRED FUSELAGE REF REO.Dec 14, 2017 · N440SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201541755Vane · chafedCHAFE OUT OF LIMITS, INBD FLAP VANE, CENTER L/E. REPLACED RT INBD FLAP, CENTER FLAP VANE L/E IAW SRM AND STS EA.Dec 20, 2015 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541754Vane · chafedCHAFE OUT OF LIMITS, LT, INBD FLAP VANE, OTBD L/E. REPLACED LT INBD FLAP, OTBD FLAP VANE L/E IAW SRM AND STS EA.Dec 20, 2015 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541753Vane · chafedCHAFE OUT OF LIMITS, RT, INBD FLAP VANE, OTBD L/E. REPLACED RT INBD FLAP, OTBD FLAP VANE L/E IAW SRM AND STS EA.Dec 20, 2015 · N440SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201541752Pressure Panel · damagedBLEND FOUND OUT OF LIMITS. RT PRESSURE FLOOR FS 531. REPAIRED RT PRESSURE FLOOR AT FS 528-540 IAW REO. PRESSURE CHECK GOOD.Dec 19, 2015 · N440SW · Cndair CL6002B19 · Fuselage Floor Panel
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