N946SW

Service difficulty reports · 218

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 = 'N946SW' 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 SWIA202161708None · corroded* THE RH PRESSURE FLOOR SILL HAS CORROSION, CHAFES AND SCRATCHES BETWEEN FS 499 AND FS 559. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 10/8/2021) CORROSION REMOVED AT 4EA MARKED AREAS OF RH PRESSURE FLOOR SILL BETWEEN FS499 AND FS559 PER BOMBARDIER R.EAug 15, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161707None · corroded* THE LH PRESSURE FLOOR SILL HAS CORROSION, CHAFES AND SCRATCHES BETWEEN FS 409+128 AND FS 559. (MARKED WITH RED GREASE PENCIL) (C-CHECK RO 10/8/2021) THE CORROSION DAMAGE ON THE PRESSURE FLOOR WAS REMOVED AND TREATED AND MEETS ALL SERVICEABILITY REQUIRAug 15, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161706None · cracked* THE PRESSURE FLOOR SUPPORT STRUCTURE'S FS 484 INTERCOSTAL BETWEEN LBL 9 AND LBL 18 HAS A CRACKED INBOARD CLIP THAT ATTACHES TO LBL 9. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK RO 10/8/2021) REMOVED AND REPLACED INBD CLIP FOR PRESSURE FLOOR SUPPORT STRUAug 15, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161705None · cracked* THE PRESSURE FLOOR SUPPORT STRUCTURE'S FS 484 INTERCOSTAL BETWEEN RBL 27 AND RBL 36 HAS A CRACKED INBOARD CLIP THAT ATTACHES TO RBL 27. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK RO 10/8/2021) REMOVED AND REPLACED INBD CLIP ON FS 484 INTERCOSTAL BETWEEN Aug 15, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202161704None · cracked* THE PRESSURE FLOOR SUPPORT STRUCTURE'S FS 484 INTERCOSTAL BETWEEN LBL 27 AND LBL 36 HAS A CRACKED INBOARD CLIP THAT ATTACHES TO LBL 27. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK RO 10/8/2021) REMOVED AND REPLACED INBD CLIP ON FS 484 INTERCOSTAL LBL 27 RAug 15, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202161703None · corrodedLH FRAME 589 HAS SPOTS OF CORROSION FWD AND AFT SIDE STRG 20LH TO 24RH (C-CHECK RO 10/8/2021) REPAIRED L/H FRAME AT FS 589 FWD AND AFT SIDE STRG 20LH TO 24RH REF REO 601R-53-61-7708 REV.:-- DATE: 2021-09-03. PRESSURE CHECKS GOOD AND COMPLIED WITH 5Aug 14, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202161702None · corrodedLH LBL9 SEAT RAIL BEAM FS 559+112-621 HAS CORROSION (C-CHECK RO 10/8/2021) REMOVED CORROSION ON LH LBL9 SEAT RAIL BEAM ONLY AT FS 621. NO OTHER CORROSION FOUND REF. CRJ200 SRM 51-21-06. BLENDED AREA FOUND TO BE OUT OF LIMITS REF. BOMBARDIER REO 601R-Aug 14, 2021 · N946SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202161701None · corrodedRH 559+112-559+80 OUTBOARD SILL AROUND FASTENER HEAD AND NUTPLATE HOLES HAS CORROSION (C-CHECK RO 10/8/2021) REMOVED CORROSION ON RH SILL BETWEEN FS 559+80 TO FS 559+112 REF CRJ200 SRM 51-21-06. BLENDED AREA FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 53Aug 14, 2021 · N946SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202161736None · excess playBOTH CENTER HINGE POINTS AND UPPER HINGE POINT BEARINGS ON THE RUDDER VERTICAL STAB TRAILING EDGE SIDE HAVE EXCESSIVE PLAY, ALL FLAGGED (C-CHECK RO 10/8/2021) REMOVED AND REPLACED WORN BEARINGS ON UPPER AND CENTER HINGE FITTINGS ON RUDDER R VERTICAL STAAug 13, 2021 · N946SW · Cndair CL6002B19 · Vertical Stabilizer, Attach FittingsSDR SWIA202161700None · dented* R/H HORIZONTAL STABILIZER UPPER SKIN HAS A DENT AT APPROX. HSS100, MARKED. (C-CHECK RO 10/8/2021) PERFORMED CUT OF R/H HORIZONTAL STABILIZER UPPER SKIN AT BETWEEN RIB 7 & RIB 6 AND STGR2 & STGR3 REF CRJ200 SRM 55-11-31. COMPLIED WITH 51-900-1003-SKYAug 10, 2021 · N946SW · Cndair CL6002B19 · Horizontal Stabilizer, Tab StructureSDR SWIA202161746None · corroded* L/H FLIGHT SPOILER ALL 4 HINGE FITTINGS HAVE CORRODED HARDWARE. (C-CHECK RO 10/8/2021) REMOVED AND REPLACE DWITH NEW 4EA BOLTS, 8EA SCREWS, 4EA NUTS AND 14EA WASHERS ON L/H FLIGHT SPOILER ALL 4 HINGE FITTINGS REF CRJ 200 AMM 27-64-05-400-801. OPS CHEAug 9, 2021 · N946SW · Cndair CL6002B19 · Wing StructureSDR SWIA202161745None · corrodedRH WING INB GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE AT ATTACH POINTS. (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED NEW RH WING INB GROUND SPOILER ACTUATOR HARDWARE AT ATTACH POINTS REF CRJ200 AMM 27-65-01-400-801. OPS CHECK GOODAug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161744None · corrodedRH WING OUTB GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE AT ATTACH POINTS. (C-CHECK RO 10/8/2021) REMOVED AND REPLACED HARDWARE WITH NEW ON RH OTBD GROUND SPOILER IAW CRJ200 AMM 27-63-01-400-801 STEPS 2.B.(3)&(4) OPS CHECK GOODAug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161743None · corrodedRH WING INB GROUND SPOILER HAS CORRODED HARDWARE AT MIDDLE HINGE CONNECTION TO ACTUATOR. (C-CHECK RO 10/8/2021) .REMOVED AND INSTALLED NEW HARDWARE TO THE RH WING INBOARD GROUND SPOILER HINGE. REF CRJ200 AMM 27-65-01-400-801. OPS CHECK GOODAug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161742None · corrodedRH WING OUTB GROUND SPOILER HAS CORRODED HARDWARE AT MIDDLE HINGE CONNECTION TO ACTUATOR. (C-CHECK RO 10/8/2021) REPLACED CORRODED HARDWARE AT R/H WING O/B GROUND SPOILER MIDDLE HINGE TOPSIDE CONNECTION AREA TO ACTUATOR WITH NEW WASHER (P/N: NAS1149C05Aug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161741None · corrodedLH WING INB GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE AT ATTACH POINTS. (C-CHECK RO 10/8/2021) REMOVED AND INSTALLED NEW LH WING INB GROUND SPOILER ACTUATOR HARDWARE AT ATTACH POINTS. REF CRJ200 AMM 27-65-01-400-801. OPS CHECK GOODAug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161740None · corrodedLH WING OUTB GROUND SPOILER ACTUATOR HAS CORRODED HARDWARE AT ATTACH POINTS. (C-CHECK RO 10/8/2021) INSTALLED NEW BOLT (P/N:NAS6205-12D), 2 WASHERS (P/N:NAS1149D0516K/NAS1149D0563K), 1 NUT (P/N:MS17826-5), 1 COTTER PIN (P/N:MS24665-134) TO REPLACE CORROAug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161739None · corrodedLH WING OUTB GROUND SPOILER HAS CORRODED HARDWARE AT MIDDLE HINGE FITTING CONNECTION TO ACTUATOR. (C-CHECK RO 10/8/2021) INSTALLED NEW WASHER (P/N: NAS1149C0563B), NUT (P/N: MS17826-5) AND COTTER PIN (P/N: MS24665-134) TO REPLACE CORRODED HARDWARE AT L/Aug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161738None · corrodedLH WING, INB FLIGHT SPOILER, INB PCU HAS CORRODED HARDWARE AT LOWER ATTACHMENT POINT. (C-CHECK RO 10/8/2021) REMOVED AND REPLACED L/H WING I/B FLIGHT SPOILER I/B PCU LOWER ATTACHMENT POINT HARDWARE REF CRJ 200 AMM 27-62-01-000-801 STEP 3. D. (4-5) AND RAug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161737None · corrodedLH WING, INB FLIGHT SPOILER, OUTB PCU HAS CORRODED HARDWARE AT LOWER ATTACHMENT POINT. (C-CHECK RO 10/8/2021) REMOVED AND REPLACED L/H WING I/B FLIGHT SPOILER O/B PCU LOWER ATTACHMENT POINT HARDWARE REF CRJ 200 AMM 27-62-01-000-801 STEP 3.D. (4-5) AND CAug 9, 2021 · N946SW · Cndair CL6002B19 · Flight Control SystemSDR SWIA202161699None · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITHJul 21, 2021 · N946SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202157576Stop · chafedTHE LEFT ELEVATOR STOPPER BRACKET FOR HINGE BL24.5 IS CHAFFED/WORN. ( INBOARD SIDE ) (FILED CLOSED) REPLACED LEFT ELEVATOR STOPPER BRACKET FOR HINGE BL24.5 PN 600-24054-121. IN REF TO CRJ 200 AMM 27-34-01. / ALSO SEE CP 22631012 RII 27-900-1004-SKY ITEApr 15, 2021 · N946SW · Cndair CL6002B19 · Elevator StructureSDR SWIA202052198Control Cable · frayedLEFT ELEVATOR DOES NOT MOVE UP DURING FLIGHT CONTROL CHECK. RIGHT ELEVATOR DOES NOT MOVE FULLY DOWN. RESISTANCE ON YOKE IS LIGHT WHEN PULLING AFT OF CENTER, BUT IT IS STRONG WHEN MOVING FORWARD OF CENTER. OUTSIDE OBSERVATION AFTER RETURNING TO GATE SHOWS LESep 2, 2020 · N946SW · Cndair CL6002B19 · Elevator Control SystemSDR SWIA2020090252147Flap System · failedSTAB AND MACH TRIM MASTER CAUTION AT FL320, WOULD NOT REENGAGE. LANDED AT FLAPS 20, BRAKE TEMPS AT 6,6,7,7 RESPECTIVELY. FLIGHT 5900 - FILED CLOSED. PERFORMED VISUAL INSPECTION AND OPERATIONAL CHECK OF THE MAIN LANDING GEAR BRAKES WITH NO DEFECTS NOTED IN RSep 1, 2020 · N946SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA202052081A/C Pack · failedLOST THE LEFT PACK AT CRUISE, FL240. STARTED DESCENT. IAW QRH PRESSED EMERGENCY DEPRESS AT 17000 FEET. PAX O2 MASKS DEPLOYED. FLIGHT 5171.Aug 26, 2020 · N946SW · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA2020050750554Seat Track · corrodedFLOOR SEAT TRACK LBL 9 HAS SEVERAL AREAS OF CORROSION AROUND FASTENER HEADS BETWEEN FS513.00 - FS559.00. (48 MO INSP) RO 5/6/2020 REMOVED AND EVALUATED CORROSION FOR SEAT TRACK FROM FS513.00 - FS559.00 LBL 9. FOUND TO BE OUT OF LIMITS REF SRM. FABRICATED NEW Apr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020050750553Seat Track · corrodedFLOOR SEAT RAIL LBL9 FROM FS364 TO FS409 IS CORRODED AND GOUGED IN MULTIPLE SPOTS. (48 MO INSP) RO 5/4/2020 REMOVED, REPLACED AND WET INSTALLED FABRICATED FLOOR SEAT RAIL FROM FS364.00 TO 409.00 LBL9. REF AMM AND REO.Apr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020050750552Seat Track · corrodedFLOOR SEAT RAIL RBL9 FROM FS364 TO FS409 IS CORRODED AND GOUGED IN MULTIPLE SPOTS. (48 MO INSP) RO 5/4/2020 REMOVED, REPLACED AND WET INSTALLED FLOOR SEAT RAIL FROM FS364.00 TO FS409.00 RBL9. REF REO AND AMM.Apr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020050750551Seat Track · corrodedFLOOR SEAT RAIL LBL9 FROM FS409 TO FS409+128 IS CORRODED AND GOUGED IN MULTIPLE SPOTS. (48 MO INSP) RO 5/4/2020 REMOVED AND EVALUATED CORROSION FOR SEAT TRACK FROM FS409.00 - FS409+128 LBL 9. FOUND TO BE OUT OF LIMITS REF SRM. FABRICATED NEW SEAT RAIL TRACK RApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020050750550Seat Track · corrodedFLOOR SEAT RAIL RBL9 FROM FS409 TO FS409+128 IS CORRODED AND GOUGED IN MULTIPLE SPOTS. (48 MO INSP) RO 5/4/2020 REMOVED, REPLACED AND WET INSTALLED FABRICATED FLOOR SEAT RAIL FROM FS409.00 TO 409+128. REF AMM AND REO.Apr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202005070549Frame · gouged*FS605.00 FRAME IS CORRODED, STGR20L €“ STGR24R. (48 MO INSP) RO 5/6/2020 REMOVE CORROSION ON THE AFFECTED AREA, GOUGE NOTED ON THE FS605.00 FRAME DURING REMOVAL OF CORROSION. GOUGE PUNCTURED THROUGH FRAME. REMOVED AND INSTALLED NEW FROM SLPICE ANGLES ATApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202005070548Frame · cracked*FS574.00 FRAME IS CORRODED, STGR23L €“ STGR20L. (48 MO INSP) RO 5/6/2020 REMOVED CORROSION IN MULTIPLE AREA ON FRMAE AT FS574.00 BETWEEN STGR23L AND STGR20L. AFTER CORROSION REMOVAL, FOUND CRACK ON FLANGE NEAR RIVET HOLE OUTBOARD SIDE OF STGR23L REF CApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202005070547Strap · corroded*FS559.00 FLOOR BEAM STRAP BETWEEN LBL 27 AND PRESSURE FLOOR SILL CORRODED IN SEVERAL AREAS (MARKED) (48 MO INSP) RO 5/6/2020 REMOVED CORRIOSON AND MEASURED REMNAING MATERIAL THICKNESS. FOUND RAMAINING MATERIAL THICKNESS TO BE OUT OF LIMITS REF CRJ 200 Apr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202005070546Angle · corroded*LH PRESSURE FLOOR SILL ANGLE FS424.00 €“ FS559.00 HAS SEVERAL AREAS OF CORROSION (MARKED) (48 MO INSP) RO 5/6/2020 REMOVED CORROSION FROM THE LH PRESSURE FLOOR SILL ANGLE FS424.00 €“ FS559.00. EVALUATED AND FOUND MULTIPLE AREA'S TO BE OUT OF LIMITS.Apr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202005070545Door Sill · corroded*RH PRESSURE FLOOR SILL FS424.00 €“ FS559.00 HAS SEVERAL AREAS OF CORROSION (MARKED) (48 MO INSP) RO 5/6/2020 REPAIRED RH PRESSURE FLOOR SILL BETWEEN FS424.00 €“ FS559.00 REF BOMBARDIER REO, AND BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILSApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20205070544Door Sill · corroded*LH PRESSURE FLOOR SILL FS424.00 €“ FS559.00 HAS SEVERAL AREAS OF CORROSION (MARKED) (48 MO INSP) RO 5/6/2020 REPAIRED LH PRESSURE FLOOR SILL BETWEEN FS424.00 €“ FS559.00 REF BOMBARDIER REO, AND BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILSApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20205070543Beam · corroded* THE FS280 BEAM HAS CORROSION ON 2 SPOTS BETWEEN LBL9 AND RBL9, MARKED IN RED. (48 MO INSP) RO 5/6/2020 BLEND ON FS 280 BEAM BETWEEN LBL 9 AND RBL 9 IS LOCATED ON A REPAIR ANGLE P/N 601R-53-11-2930-6. NO ALLOWABLE DAMAGE LIMITS FOR BLENDS ON REPAIR PAApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20205070542Angle · corroded* PAX DOOR SILL ANGLE IS CORRODED IN MULTIPLE SPOTS, MARKED IN RED. (48 MO INSP) RO 5/6/2020 REMOVED CORROSION FROM THE PAX DOOR SILL ANGLE REFERENCE CRJ200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS.REPLACED PAX DOOR SILL ANGLE WITH NEW PART. REF: BOMApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20205070541Attach Fitting · cracked* FLOOR BEAM ATTACH CLIP AT FS280, LBL9, OUTBOARD, IS CRACKED. (48 MO INSP) RO 5/6/2020 REMOVED PREVIOUSLY REPAIRED OUTB`D ATTACH CLIP ON FS280 FLOOR BEAM AT LBL 9 AND INSTALLED NEW OUTB`D ATTACH CLIP ON FLOOR BEAM AT FS 280 AND LBL 9 REF CRJ200 SRM ANDApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20205070540Attach Fitting · cracked* FLOOR BEAM ATTACH CLIP AT FS280, RBL9, OUTBOARD, IS CRACKED. (48 MO INSP) RO 5/6/2020 REMOVED PREVIOUSLY REPAIRED OUTB`D ATTACH CLIP ON FS280 FLOOR AND INSTALLED NEW OUTB`D ATTACH CLIP ON FLOOR BEAM AT FS 280 AND RBL 9 REF CRJ200 SRM AND BOMBARDIER Apr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20205070539Door Sill · corroded* R/H FLOOR SILL HAS CORROSION BETWEEN FS310 AND FS319, MARKED IN RED. (48 MO INSP) RO 5/6/2020 REMOVED CORROSION ON R/H FLOOR SILL BETWEEN FS310 AND FS319 REF REO BLENDED AREA ON R/H FLOOR SILL WAS FOUND TO BE WITHIN LIMITS REF CRJ200 SRM, BOMBARDIEApr 23, 2020 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020050750555Fastener · chafedFS621 PRESSURE BULKHEAD HAS NUMEROUS INNER SKIN FASTENERS CHAFED. (48 MO INSP) RO 5/4/2020 REPLACED 8EA AFFECTED FASTENERS ON THE FS621 PRESSURE BULKHEAD. REF SRM. PRESSURE CHECKS GOOD, NO DEFECTS FOUND.Apr 21, 2020 · N946SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA20205060538Vane · chafedRIGHT INBD FLAP VANE LEADING EDGE OUTBD HAS CHAFFE (48 MO INSP) RO 5/6/2020 REMOVED AND INSTALLED NEW LEADING EDGE FLAP AT RIGHT INBOARD FLAP OUTBD. REF. CRJ 200 SRM AND BOMBARDIER DWG. COMPLIED WITH AND SEE CONTINUATION CARD FOR DETAILSApr 20, 2020 · N946SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20205060537Vane · chafedRIGHT INBD FLAP VANE LEADING EDGE INBD HAS CHAFFE (48 MO INSP) RO 5/6/2020 REPLACED RH INBD FLAP VANE INBD CAP. REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUE CARD FOR ADDITIONAL DETAILS. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)Apr 20, 2020 · N946SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA20205070536Vane · chafed* LEFT INBD FLAP VANE LEADING EDGE OUTBD HAS CHAFFE (48 MO INSP) RO 5/6/2020 BLENDED THE CHAFE ON LEFT INBD FLAP VANE LEADING EDGE OUTBD CAP REFERENCE CRJ200 SRM. EVALUATED AND FOUND TO BE OUT OF ,LIMITS. REPLACED LH INBD FLAP VANE OUTBOARD CAP. REF CRJApr 20, 2020 · N946SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2019011545453Proximity Switch · out of adjustGEAR DISAGREE LEFT MAIN ON TAKEOFF. DIVERTED. EMERGENCY-DECLARED. GEAR CAME DOWN NORMALLY. (FLT 5137) CLOSED PSEU REPORTS "S20 FAR" INSPECTED LT MLG UPLOCK PROX SWITCH AS REQUIRED, FOUND GAP TO BE .056", ADJUSTED PROX SWITCH TO TARGET GAP TO .037" IAW AMM. FOUJan 15, 2019 · N946SW · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018101545136Overheat Loop · failedLEFT JETPIPE OVERHEAT CAUTION ON TAKEOFF, THEN ON DESCENT LEFT JETPIPE OVERHEAT WARNING CAME ON AND WOULD NOT EXTINGUISH. DIVERTED TO LAX. CREW SHUTDOWN LEFT ENGINE DURING DESCENT. (FLT 5197) FO: 10/15/2018 CLOSED REMOVED AND REPLACED LT PYLON LOOP B ELEMENT IOct 14, 2018 · N946SW · Cndair CL6002B19 · Overheat DetectionSDR SWIA2018092145012Unknown · malfunctionedGEAR DISAGREE ON FINAL. NOSE GEAR DID NOT COME DOWN. WE DID A GO AROUND AND THE NOSE GEAR CAME DOWN ON IT'S OWN. NO FURTHER ISSUES. (FLT 5489) FO: 08/29/2018 CLOSED. CHECKED FOR WEAK ACMPS 3A AND 3B HYD SYSTEMS. BOTH CHECKED GOOD SEPARATELY ON GEAR SWINGS. FOLAug 29, 2018 · N946SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA2018081444989Pump · failedGEAR DISAGREE WARNING MESSAGE. COMPLIED WITH THE QRH. CYCLED THE GEAR HANDLE ONE TIME. GEAR DOWN AND LOCKED. REMOVED AND REPLACED THE NR 3A HYDRAULIC PUMP. PERFORMED GEAR SWINGS IAW AMM. OPS CHECKED GOOD.Aug 13, 2018 · N946SW · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), MainSDR SWIA2018072444897Angle · corrodedSERVICE DOOR SILL ANGLE HAS CORROSION. (C-CHECK) RO: 7/21/2018. R&R THE LOWER SERVICE DOOR SILL ANGLE WITH A NEW ANGLE REF SRM 51-42-06, SRM 51-42-13 AND SRM 51-42-21, OPS TEST GOOD.Jun 29, 2018 · N946SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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