N929SW

Service difficulty reports · 288

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 = 'N929SW' 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 SWIA202164299None · gouged*LH WING OTBD FLAP VANE HAS GOUGE ON LOWER LEADING EDGE INBD OF FLS 296.07 (C CHECK RO 02-12-2022) REMOVED AND REPLACED LH WING OTBD FLAP VANE AT FLS 296.07. REF CRJ 200 CRJ 200 SRM 51-42-13 AND INSTALLATION DWG 601R14502 REV -D. COMPLIED WITH 51-900-1003Dec 17, 2021 · N929SW · Cndair CL6002B19 · Aileron TabsSDR SWIA202164298None · corroded* THE FRAME DOUBLER AT FS473.15 AT THE LH PRESSURE FLOOR SILL BEWEEN STR 17L AND 16L HAS CORROSION. (MARKED) (C CHECK RO 02-12-2022) REPAIRED FRAME DOUBLER AT FS473.15 AT THE LH PRESSURE FLOOR SILL BETWEEN STR 17L AND 16L REF REO 601R-53-41-2999 REV -- DADec 17, 2021 · N929SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164335None · corrodedFLOOR BEAM RBL9 FS424.0 - FS484.0 HAS CORROSION ON FLOOR SILL (MARKED) (C CHECK RO 02-12-2022) REPAIRED FLOOR BEAM INBOARD FLANGE RBL9 BETWEEN FS424.0 - FS499.0. REF REO 601R-53-41-3003 REV. -- DATE 2022-01-11Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164328None · corroded* THE SEAT TRACK AT RBL9 FROM APPROX FS409.00+96 TO FS 409.00+128 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK RO 02-12-2022) INSTALLED NEW SEAT TRACK AT RBL9 FROM APPROX FS. 409+96 - FS. 409+128 USING NEW HARDWARE. REF. CRJ 200 AMM 53-01-11-40Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164327None · corroded* THE SEAT TRACK AT RBL9 FROM APPROX FS364 TO FS409 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK RO 02-12-2022) INSTALLED NEW SEAT TRACK AT RBL9 FROM APPROX FS364 TO FS409 USING NEW HARDWARE. REF. CRJ 200 AMM 53-01-11-400-802 TORQUE TOOL : TUC56Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164326None · corroded* THE SEAT TRACK AT LBL9 FROM APPROX FS364 TO FS409 HAS MULTIPLE LOCATIONS OF CORROSION. (MARKED) (C CHECK RO 02-12-2022) INSTALLED NEW SEAT TRACKS AT LBL9 FROM APPROX FS364 TO FS409 USING NEW HARDWARE. REF. CRJ 200 AMM 53-01-11-400-802 TORQUE TOOL : TUC56Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164325None · damaged2EA FASTENERS DAMAGED ON FLOOR BEAM RBL9 FS559+64 (MARKED) (C CHECK RO 02-12-2022) REMOVED AND REPLACED DAMAGED FASTENERS AT FLOOR BEAM RBL9 FS559+64 REF CRJ 200 SRM 51-42-06Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164324None · corrodedRH SIDEWALL SEAT TRACK AT FS473.00 HAS CORROSION (MARKED) (C CHECK RO 02-12-2022) REPLACED R/H SIDE SEAT TRACK AT FS.448 - FS.501 REF. CRJ200 AMM TASK 53-01-11-400-802 .Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164297None · corroded* THE GALLEY FITTING BETWEEN RBL27 AND RH FLOOR SILL AND FS280 AND FS295 HAS CORROSION. (MARKED) (C CHECK RO 02-12-2022) REMOVED CORROSION AT THE GALLEY FITTING BETWEEN RBL27 AND RH FLOOR SILL AND FS280 AND FS295. REF CRJ-200 SRM 51-21-06. FOUND TO BE IN LDec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164296None · corroded* THE RH PRESSURE FLOOR SILL PANEL HAS CORROSION BETWEEN FS409.00+128 TO FS499 APPROX. (MARKED) (C CHECK RO 02-12-2022) BLENDED AREAS WITHIN LIMITS RH PRESSURE FLOOR SILL PANEL BETWEEN FS409.00+128 TO FS499 / REF BOMBARDIER REO 601R-53-41-666 REV-C, DADec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164295None · corroded* THE LH PRESSURE FLOOR SILL ANGLE HAS CORROSION BETWEEN FS449.85 TO FS461 APPROX. (MARKED) (C CHECK RO 02-12-2022) BLENDED CORROSION ON LH PRESSURE SILL ANGLE BETWEEN FS 449.85 TO FS 461 REF REO 601R-53-41-666 REV -C DATE 2012-11-06 AND BLENDED AREA IS Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164294None · corroded* THE LH PRESSURE FLOOR SILL PANEL HAS CORROSION BETWEEN FS449.85 TO FS461 APPROX. (MARKED) (C CHECK RO 02-12-2022) REPAIRED LH PRESSURE FLOOR SILL PANEL BETWEEN FS449.85 TO FS461 REF REO 601R-53-41-666 REV C DATED 2012-11-06 STEP 1.2 A-F. COMPLIED WITH 5Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164293None · corrodedFRAME AT FS589.00 HAS CORROSION STGR 21L TO 22R IN MULTIPLE AREAS (MARKED) (C CHECK RO 02-12-2022) REMOVED AND REPLACED NEW SECTION FRAME AT FS 589.00 BETWEEN STGR 21L - STGR 22R REF CRJ200 SRM 51-42-06 AND DWG 601R36025 REV -P AND DWG 601R35005 REV AG. Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164292None · corrodedRH FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FROM FS589.00 TO FS559+96 (MARKED) (C CHECK RO 02-12-2022) REPAIRED R/H FLOOR SILL BETWEEN FS 559+112 TO 605 REF REO 601R-53-00-526 REV -- DATED 22-MAY-2013. SEE CAMP 24163913 FOR REPLACEMENT OF RH CARGO FLOODec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164291None · corrodedLH FS461.00 FRAME ON THE FLOOR SILL HAS CORROSION (MARKED) (C CHECK RO 02-12-2022) REMOVED CORROSION @LH FS461.00 FR ON THE FLOOR SILL PER REF CRJ 200 SRM 51-21-06. PART FOUND TO BE WITHIN LIMITS AND REPAIR ACCOMPLISHED IAW REO 601R-53-41-2998 REV-- DATE Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164290None · crackedLBL36 FLOOR BEAM SUPPORT FITTING FS460.0 SUSPECTED CRACK (MARKED) (C CHECK RO 02-12-2022) INSTALLED LBL36 FLOOR BEAM SUPPORT FITTING FS360.0 IAW REO 601R-53-41-2997 REV -- DATE 2021-12-27 . PERFORMED LEAK CHECK REF CRJ 200 AMM 21-32-00-863-801. LEAK CHECKDec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164289None · crackedLBL27 FLOOR BEAM INBD AND OUTBD SUPPORT FITTINGS AT FS460.0 HAVE A SUSPECTED CRACK (MARKED) (C CHECK RO 02-12-2022) INSTALLED NEW LBL27 FLOOR BEAM INBD AND OUTBD SUPPORT FITTINGS AT FS460.0 REF DWG 601R31118 REV.L AND CRJ 200 SRM 51-42-21 COMPLIED WITHDec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202164288None · crackedLBL18 FLOOR BEAM SUPPORT FITTING AT FS460.0 HAS A SUSPECTED CRACK ON THE UPPER AND LOWER CORNERS (MARKED) (C CHECK RO 02-12-2022) REMOVED AND INSTALLED NEW FLOOR BEAM SUPPORT FITTING FS460.0 LBL18 REF DWG 601R31118 REV L AND CRJ 200 SRM 51-42-21. COMPLIED Dec 16, 2021 · N929SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202164342None · worn*RH INBOARD FLAP THE OUTBOARD FLAP VANE ACTUATOR CARRIAGE LOWER ROLLER HAS A FLAT SPOT. (C CHECK RO 02-12-2022) REMOVED AND REPLACE LOWER ROLLER ON THE RH INBOARD FLAP OUTBOARD FLAP VANE ACTUATOR REF CRJ200 CMM 57-52-03Dec 14, 2021 · N929SW · Cndair CL6002B19 · Aileron TabsSDR SWIA202164336None · worn*RH INBOARD FLAP HAS A SEIZED ROLLER ON THE MIDDLE FLAP VANE ACTUATOR. (C CHECK RO 02-12-2022) REPLACED ROLLER ON RH IND FLAP MIDDLE FLAP VANE ACTUATOR REF CRJ200 CMM 57-59-00. OPS TEST GOODDec 14, 2021 · N929SW · Cndair CL6002B19 · AileronsSDR SWIA202164334None · corrodedRH AILERON, OUTB HINGE ASSEMBLY HAS MULTIPLE CORRODED HARDWARE. (FLAGGED) (C CHECK RO 02-12-2022) REMOVED AND INSTALLED NEW HARDWARE FOR R/H AILERON OUTBOARD HINGE REF CRJ200 SRM 51-41-02. BONDING TEST GOOD.Dec 14, 2021 · N929SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164333None · corroded*THE CENTER HINGE ON THE RH WING OB GROUND SPOILER HAS CORRODED/RUSTY HARDWARE(MARKED) (C CHECK RO 02-12-2022) REMOVED AND REPLACED HARDWARE ON CENTER HINGE RH WING OB GROUND SPOILER PER CRJ 200 AMM 27-65-01-000-801 STEP 3.B. PER CRJ 200 AMM 27-65-01-400-Dec 14, 2021 · N929SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164332None · corroded*HARDWARE ON RH WING OB GROUND SPOILER IS RUSTY/CORRODED(MARKED) (C CHECK RO 02-12-2022) REMOVED CORRODED HARDWARE AND REPLACED 3EA WASHERS AND 3EA NUTS ON RH WING OB GROUND SPOILER REF CRJ 200 AMM 27-65-01-400-801. OPS CHECK GOOD.Dec 14, 2021 · N929SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164331None · corroded*RIGHT WING FLIGHT SPOILER IB HARDWARE IS RUSTY/CORRODED (MARKED) (C CHECK RO 02-12-2022) REMOVED AND INSTALLED NEW HARDWARE ON RIGHT WING FLIGHT SPOILER IB HINGE REF CRJ200 AMM 27-64-05-400-801. OPS CHECK GOOD.Dec 13, 2021 · N929SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164330None · corroded*LEFT OB GROUND SPOILER I/B HINGE HARDWARE IS CORRODED/RUSTY (MARKED) (C CHECK RO 02-12-2022) REMOVED CORRODED/RUSTY HARDWARE AND INSTALLED WITH NEW HARDWARE AT LEFT OB GROUND SPOILER I/B HINGE REF AMM 27-65-01-400-801. OPS CHECK GOOD.Dec 13, 2021 · N929SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164323None · chafed*FLIGHT OBSERVERS SEAT LWR SEAT RAIL HAS EXCESSIVE PLAY (MARKED) (C CHECK RO 02-12-2022) REMOVED DISCREPANT AND INSTALLED SERVICABLE REPLACEMENT FLIGHT OBSERVER'S LWR SEAT RAIL ASSY P/N 15981-1 REF. CRJ200 AMM TASK 25-12-01-400-801 FIG. 401 . NO MORE PLAY Dec 11, 2021 · N929SW · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR SWIA202164287None · damagedPILOTS WINDSHEILD, SIDE EXTERNAL POST HAS NUMEROUS SCRATHES (MARKED WITHIN RED GREASE PENCIL) (C CHECK RO 02-12-2022) REMOVED DAMAGED PILOT WINDSHIELD STRAP REF CRJ 200 AMM 56-11-01-000-801 INSTALLED NEW PILOT WINDSHIELD STRAP REF CRJ 200 AMM 56-11-01-400-Dec 10, 2021 · N929SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202164286None · damagedCO-PILOTS WINDSHEILD, SIDE EXTERNAL POST HAS NUMEROUS SCRATHES (MARKED WITHIN RED GREASE PENCIL) (C CHECK RO 02-12-2022) REMOVED AND REPLACED WITH NEW CO-PILOT WINDSHIELD STRAP REF CRJ-200-AMM 56-11-01-000-801 AND CRJ 200 AMM 56-11-01-400-801 . LEAK CHECDec 10, 2021 · N929SW · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA2021021664285Fairing · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA64967-601R-54-62-214 N929SW MXCODEID54119-PR - RH AFT PYLON FAIRING UPPER SURFACE SKIN DAMAGED DUE TO ENGINE EXHAUST FIRE. COMPLIED WITH TEMPORARY REPAIR TO AFT PLYON FAIRING BETWEEN FS.682 & FS.736 RHS PER REO 601R-Nov 18, 2021 · N929SW · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous StructureSDR SWIA202164284None · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA55489-601R-57-31-1334-N929SW MXCODEID50310-PR - THE LHS WINGLET STRUCTURE HAS DISCREPANT FASTENER HOLES. PERFORMED TEMP REPAIR IN REF TO REO 601R-57-31-1334 REV B, DTD 12/25/2019. PERM REPAIR DUE WITHIN 5000 FLT HRSNov 18, 2021 · N929SW · Cndair CL6002B19 · Wing StructureSDR SWIA202164283None · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA18418-601R-57-21-1707 RH 929SW-PR - RH MLG TRUNNION HAS 3 HOLES THAT ARE CRACKED. COMPLIED WITH REO 601R-57-21-1707. THIS IS A SAFE LIFE REPAIR. REPLACEMENT IS DUE 20745 FC FROM INCORPORATION OF REPAIR DUE BY TAC 4207Nov 18, 2021 · N929SW · Cndair CL6002B19 · Landing Gear SystemSDR SWIA202054716Skin · chafedFUSELAGE CHAFE DAMAGE DISCOVERED BETWEEN THE PYLON TRAILING EDGE FAIRING CAUSED BY THE RUB STRIP RIGHT HAND SIDE OUT OF LIMITS IN NUMEROUS AREAS BETWEEN FS 700 AND FS 755 AND STR 9-12. COMPLY WITH REO MAJOR REPAIR. COMPLIED WITH REO FOR FUSELAGE CHAFE DAMAGEDec 6, 2020 · N929SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2019123147508Mount · crackedUPON INSTALLING AFT CARGO DOOR NET MOUNTING BRACKETS ASSY FOUND CRACK ON CLIP AT FS621 LBL35.00 (C-CHECK) RO 12/27/2019 REMOVED AND INSTALLED NEW SERVICEABLE CLIP P/N# 601R35031-209 ON FS621 BULKHEAD AT LBL 35.30 REF CRJ200 SRM AND BOMBARDIER DRAWING. COMPLIDec 11, 2019 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019123147507Vertical Beam · crackedFS 409+128 VERTICAL POST INBD HALF IS CRACKED AT RBL 27, AT THE LOWER FLANGE. (C-CHECK) RO 12/27/2019 REMOVED CRACKED POST AND INSTALLED NEW INB`D HALF POST PN 601R-32208-34 AT RBL 27 AND FS 409+128 REF BOMBARDIER REO, BOMBARDIER, CRJ200 SRM. COMPLIED WITH SDec 6, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019123147506Vertical Beam · crackedSUSPECTED CRACK ON FS409+128 I/B VERTICAL POST @ LBL27 LOWEST RIVET NEAR THE RADIUS. (C-CHECK) RO 12/27/2019 REMOVED CRACKED AND INSTALLED NEW INB`D POST AT LBL 27 AND FS 409+128 REF BOMBARDIER REO, BOMBARDIER DWG, CRJ200 SRM. SEE CONTINUATION CARD FOR DETAIDec 5, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019123147505Rib · crackedBATT RIB INTERCOSTAL AT REAR SPAR W.S58.80 IS CRACKED (C-CHECK) RO 12/27/2019 DISCREPANT AREA MARK WAS NOTED AT W.S58.80, BUT WAS ACTUALLY LOCATED AT LH W.S. 53.60. REPAIRED BATT RIB ASSY AT LH W.S. 53.60 PER REO. COMPLIED WITH SKYWEST TASK CARDNov 26, 2019 · N929SW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2020061851082Hinge Fitting · gougedRT CENTER HINGE FITTING ON HORIZONTAL STAB GOUGED (DURING INSP OF ADDWORK TASK. WORK IN CONJUNCTION WITH JOB 27703105) REPAIRED THE GOUGED RT HORIZONTAL STAB CENTER HINGE FITTING IN ACCORDANCE WITH SRM, REO. COMPLIED WITH TASK CARD. THIS SDR FOR T/STEADY FITTNov 21, 2019 · N929SW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWIA2020061851081Hinge Fitting · gougedLT CENTER HINGE FITTING ON HORIZONTAL STAB GOUGED, FOUND ON INSP OF ADDWORK TASK CARD 55-330-603. ( WORK IN CONJUNCTION WITH JOB 27703105) REPAIRED THE GOUGED LT HORIZONTAL STAB CENTER HINGE FITTING IN ACCORDANCE WITH SRM, REO. COMPLIED WITH TASK CARD. THIS SNov 21, 2019 · N929SW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR SWIA2019123147504Floorbeam · crackedFS 484 OUTBOARD CLIP AT RBL 36 BRACKET IS CRACKED (C-CHECK) RO 12/27/2019 REMOVED CRACKED AND INSTALLED NEW FS 484 OUTBOARD CLIP AT RBL 36 BRACKET REF BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS. LK CK GOOD.Nov 21, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019123147503Channel · crackedLH WING WS 53.60 CHANNEL IS CRACKED UPPER AFT CORNER AS MARKED. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED THE DAMAGED CHANNEL CLIP (P/N 601R10203-25) AT WS 53.60 LHS REF DWG, CRJ200 SRM. COMPLIED WITH SKYWEST TASK CARDNov 20, 2019 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019123147502Door Frame · cracked* FORWARD CABIN - APPROX. FS.330.00 BETWEEN STGR 1 AND 2 LEFT HAND ABOVE PAX DOOR CUT OUT- FRAME HAS SIGNS OF A CRACK AT A TOOLING HOLE (C-CHECK) RO 12/27/2019 REMOVED AND INSTALLED NEW FRAME SECTION AT FS333, BETWEEN STR1L AND STR2L REF CRJ200 SRM AND Nov 20, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019123147501Vertical Beam · cracked* FS 409+128 VERTICAL POST OUTBOARD HALF HAS A SUSPECTED CRACK AT RBL 18, NEAR THE LOWER END'S FASTENER. (C-CHECK) RO 12/27/2019 REMOVED CRACK OUTBD POST AND INSTALLED NEW P/N 601R32208-30 VERTICAL OUTBD POST RBL18 AT FS409+128 REF BOMBARDIER REO AND BOMBARDINov 18, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019123147500Stiffener · crackedF/S 621.0 PRESSURE BULKHEAD L/H AFT SIDE STIFFENER IS CRACK. (C-CHECK) RO 12/27/2019 REMOVED CRACKED AND INSTALLED NEW BULKHEAD STIFFENER IAW CRJ 200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS. LK CK GOOD.Nov 17, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019123147499Angle · cracked* R/H WING JUST OUTBOARD OF SPAR JACK FITTING LOCATION ANGLE HAS SUSPECT CRACKS IN BETWEEN RIVET LOCATIONS. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED WITH NEW, THE RH WING JOINT STRAP NEAR JACK FITTING AREA AT REAR SPAR REF BOMBARDIER DRAWING, SRM. COMPLINov 15, 2019 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019123147498Fitting · cracked* L EFT SIDE JACK FITTING AREA OUTBOARD ANGE AT REAR SPAR IS CRACKED IN BETWEEN RIVET HOLES. (C-CHECK) RO 12/27/2019 REMOVED AND REPLACED WITH NEW, THE LH WING JOINT STRAP NEAR JACK FITTING AREA AT REAR SPAR REF BOMBARDIER DRAWING, CRJ200 SRM. COMPLIED WITH Nov 15, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2019123147530Floor Support · corroded*APPROX. FROM FS563 TO FS621 CARGO FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO 12/27/2019 REMOVED CORRODED AND INSTALLED NEW CARGO BAY FLOOR SILL FROM FS574-FS621. REF BOMBARDIER REO, BOMBARDIER DWG, CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILSNov 14, 2019 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019123147529Floor Support · corroded*APPROX. FROM FS569 TO FS621 CARGO FLOOR BEAM HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK) RO 12/27/2019 REPLACED WITH NEW CARGO FLOOR BEAM APPROX. FROM FS569 TO FS621 REF CRJ-200 SRM, BOMBARDIER COMPLIED WITH SKYCARD.Nov 14, 2019 · N929SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2019123147528Floorbeam · corroded*FS 280 FWD FLOOR SUPPORT HAS CORROSION. (C-CHECK) RO 12/27/2019 ORIGINAL MATERIAL THICKNESS IS 0.040€? REF CRJ200 SRM. REMAINING MATERIAL THICKNESS PER NDT IS 0.030€?. MATERIAL REMOVED WAS 0.010€?. ALLOWED MATERIAL TO BE REMOVED IS 10% (0.004€?) REF CRJ2Nov 14, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2019123147527Skin · corrodedEXTERNAL SKIN UNDER FARING 191BB AND 192BB HAS CORROSION AROUND NUT PLATES (C-CHECK) RO 12/27/2019 REMOVED CORROSION UNDER FAIRINGS PANELS 191BB AND 192BB REF CRJ200 SRM, MATERIAL THICKNESS IS OUT LIMITS REF CRJ200 SRM, COMPLIED WITH ALL STEPS 1-6 REF BOMBNov 14, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2019123147526Frame · corroded* R/H SIDE FUSELAGE ST FS 513 FRAME HAS EVIDENCE OF CORROSION. (C-CHECK) RO 12/27/2019 REMOVED CORROSION AND ROTOPEENED WORKED AREA ON R/H FRAME AT FS513. REF: CRJ200 SRM. AND BOMBARDIER REO. SEE CONTINUE CARD FOR DETAILS.Nov 14, 2019 · N929SW · Cndair CL6002B19 · Fuselage Main, Frame
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