N962SW

Service difficulty reports · 173

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 = 'N962SW'
  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 SWIA2025090900008Thrust Reverser · warning messageLEFT REV UNLOCKED MESSAGE IN FLIGHT. LT REV UNLOCKED IN FLIGHT. RAN QRC AND QRH. IN GRB. IS NOT DEPLOYED. DEFERRED LEFT THRUST REVERSER PER MEL 78-30-1. MX PROCEDURE COMPLIED WITH. PLACARDED AS REQUIRED.Sep 8, 2025 · N962SW · Cndair CL6002B19 · Engine Thrust ReverserSDR SWI2025F00414Stop Fitting · gougedCARGO DOOR SURROUND LOWER AFT STOP FITTING IS GOUGED (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW AFT LOWER STOP FITTING P/N:601R35203-5 & SHIM LAMINATED P/N: 601R35207-9. REF DWG 601R35207 REV -W AND REF CRJ 200 SRM 51-41-02. COMPLIED WITH SKYWEST TASK CAMar 6, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA2025033106Stop Fitting · gougedCARGO DOOR SURROUND LOWER FWD STOP FITTING IS GOUGED (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW CARGO DOOR SURROUND FWD LOWER STOP FITTING P/N:601R35203-5 & SHIM LAMINATED P/N: 601R35207-9 IAW CRJ 200 SRM 51-41-02 AND DWG 601R35203 REV -A. TORQUE WRENCH Mar 6, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA20250331206Skin · chafedS/N 0412RIGHT WING LOWER WING PLANK ACCESS HOLE 640BB HAS CHAFING AND PIN HOLES AROUND IT'S CIRCUMFRANCE. FLAGGED (C-CHECK RO 03/30/2024)REPAIRED RH WING LOWER WING PLANK ACCESS HOLE 640BB IAW REO 601R-57-21-030 REV -L DATED: 2014-02-05 AND REO 601R-57-21-3899Feb 6, 2025 · N962SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWI2025F00413Attach Angle · crackedCRACK NOTED ON CLIP ANGLE ATTACHED TO FRAME 625.30 AT APPROX STRG 14R (MARKED) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW CLIP ANGLE (INTERCOSTAL) P/N 601-35012-52, ON FS 625.30 AT APPROX. STRG 14R, REF. CRJ-200, SRM 51-42-21 AND DWG 601-35012, REV. D. CJan 25, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA20250331025Attach Angle · crackedCRACK NOTED ON CLIP ANGLE ATTACHED TO FRAME 625.30 AT APPROX STRG 14L (MARKED) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED CLIP ANGLE CRACKED FROM FRAME 625.30 AT APPROX. STRG 14L, REF. CRJ-200, SRM 51-42-21 AND DWG 601-35012, REV. D. COMPLIED WITH TASK CARD Jan 25, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA20250331124Floor Support · corrodedLEFT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FS409+128 - FS559.00. (MARKED) (C-CHECK RO 03/30/2024)REMOVED CORROSION ON L/H PRESSURE FLOOR SILL FS409+128 - FS559.00 AT 14 EA LOCATIONS REF CRJ200 SRM 51-21-06. FOUNS TO BE OUT OF LIMITS. RECEIVED ANDJan 24, 2025 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202503310124Floor Support · corrodedRIGHT PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION FS409+128 - FS559.00. (MARKED) (C-CHECK RO 03/30/2024)REMOVED CORROSION ON R/H FLOOR SILL AT 14EA LOCATIONS FROM FS 409+128 TO FS 559 REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMJan 24, 2025 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20250331123Door Sill · corrodedAFT CARGO DOOR SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW AFT CARGO DOOR FLOOR SILL. REF REO 601R-53-61-1574 REV B DATED 2012-04-15 ALL STEPS, DWG 601R35011 REV R & CRJ200 SRM 51-42-06. SRM 51-42-21. COMPLIED WITJan 23, 2025 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2025F00410Mount · crackedRH MLG VOLUMETRIC FUSE MOUNT IS CRACKED INSIDE WHEEL WELL (UNDERSIDE OF PRESSURE FLOOR) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW RH MLH VOLUMETRIC FUSE MOUNTING BRACKET REF CRJ200 SRM 51-41-02, CRJ200 SRM 51-42-06 AND BOMBARDIER DWG: 601R75278 REV -G. Jan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWI2025F00409Floorbeam · crackedFLOOR BEAM RBL9 INBOARD CLIP ON THE FS280.00 BEAM IS CRACKED IN THE RADIUS AT THE TOP OF THE CLIP. (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW FLOOR BEAM RBL9 INBOARD CLIP ON THE FS280.00 BEAM REF: CRJ-200 SRM 51-42-06 , CRJ-200 SRM 51-42-21 AND DWG. 601RJan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2025F00408Mount · corrodedGALLEY 1 FORWARD INBOARD, AFT AND AFT INBOARD MOUNTS ON THE CABIN FLOOR STRUCTURE ARE CORRODED. (MARKED) (C-CHECK RO 03/30/2024)REMOVED AND REPLACED GALLEY 1 AFT INBD FLOOR MOUNT PLATE REF CRJ 200 SRM 51-42-06 AND DWG NO 601R38669 REV -N. BLENDED AND EVAL'D GAJan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage, Equipment Attach FittingsSDR SWI2025F00407Mount · crackedLH MLG VOLUMETRIC FUSE MOUNT IS CRACKED INSIDE WHEEL WELL (UNDERSIDE OF PRESSURE FLOOR) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW LH MLG VOLUMETRIC FUSE MOUNTING BRACKET REF DWG 601R75278 REV G, CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-41-02. COMPLIED WITHJan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2025033100120Mount · damagedLH MLG PRESSURE TRANSDUCER MOUNTING ANGLE INSIDE WHEEL WELL (UNDERSIDE OF PRESSURE FLOOR) (C-CHECK RO 03/30/2024)REMOVED AND INSTALLED NEW LH MLG PRESSURE TRANSDUCER MOUNTING ANGLE P/N 601R75262-159. REF: CRJ-200 SRM 51-42-06 AND DWG. 601R75261 REV -N. COMPLIEJan 20, 2025 · N962SW · Cndair CL6002B19 · Fuselage, Landing Gear Attach FittingsSDR SWI2025F00412Skin · chafedCHAFFE ON AFT CARGO DOOR UPPER SKIN (MIDDLE ABOVE EXISTING DOUBLER) CAMP 29497077. (C-CHECK RO 03/30/2024) REMOVED AND REPLACED CHAFED DOUBLER ON THE AFT CARGO DOOR UPPER SKIN WITH NEW FABRICATED DOUBLER, PER MHIRJ REO 601R-52-31-340 REV -- DATED 2021-02-16. Jan 18, 2025 · N962SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWI2025F00411Fitting · gougedAFT UPPER AND LOWER FITTING GOUGED ON AFT CARGO DOOR CAMP 29497087. (C-CHECK RO 03/30/2024)DISCREPANCY SHOULD READ, AFT LOWER CARGO DOOR STOP FITTING AND CARGO DOOR SURROUND LOWER AFT STOP FITTING IS GOUGED. INSTALLED NEW AFT LOWER STOP FITTING ON CARGO DOOR PJan 18, 2025 · N962SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202503310118Fitting · gougedFWD UPPER AND LOWER FITTING GOUGED ON AFT CARGO DOOR CAMP 29497081. (C-CHECK RO 03/30/2024)DISCREPANCY SHOULD READ, FWD LOWER CARGO DOOR STOP FITTING AND CARGO DOOR SURROUND LOWER FWD STOP FITTING IS GOUGED. INSTALLED NEW FWD LOWER CARGO DOOR STOP FITTING IAW Jan 18, 2025 · N962SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWI2025F00406Handle · no testDURING OPERATIONAL TEST OF THE CREW ESCAPE HATCH (EES), THE OUTER HANDLE DOESN'T OPERATE PROPERLY. (29444062) (C-CHECK RO 03/30/2024)REMOVED AND REPLACED NEW OUTER HANDLE OF THE CREW ESCAPE HATCH REF CRJ200 SRM 51-42-06 AND DWG CC670-38002 REV -E. COMPLIED WITJan 8, 2025 · N962SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA20250331106Skin · gougedADM# N962SW-7829 FS 640.00--FS 654.5 RH STRINGER 4-5. FOUND GOUGE 1.6" AFT OF FS 640.00 AND 1.5" ABOVE RH STRINGER 5. GOUGE IS .0019" DEEP, WIDTH .44", LENGTH .58". PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USIJan 6, 2025 · N962SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI202402270177A/C Pack · pressure lossR PACK HI PRESS CAUTION AT 10000. WHEN IT FAULTED, L PACK HI TEMP CAUTION CAME ON. (FLIGHT 5291 FILED CLOSED)TROUBLESHOT PER CRJ 200 FIM 21-50-00. REMOVED AND REPLACED PRESSURE REGULATING SOV REF CRJ 200 AMM 21-51-43. OPERATIONAL TEST GOOD AT THIS TIME.PLEASE Feb 23, 2024 · N962SW · Cndair CL6002B19 · Cabin Cooling SystemSDR SWIA202402190018Landing Gear · warning message****AIRCRAFT DOWNGARDED FROM CAT 2 *****D:GEAR DISAGREE WARNING MESSAGE FOLLOWED BY NOSE DOOR OPEN WARNING MESSAGE AFTER SELECTING GEAR UP AFTER TAKEOFF. RAN EMERGENCY QRH 13-13 AND RETURNED TO AIRPORT.C:MEL 32-30-1CAT A DUE 02/19/24*** DUE TO ODI REQUIRES SMFeb 18, 2024 · N962SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202266661None · failedNOSE DOOR AND GEAR DISAGREE RED MESSAGES DURING GEAR EXTENSION. FOLLOWED QRH WHICH WORK TO CLEAR THE MESSAGES (FLIGHT 5911 - FILED CLOSED) INTERROGATED PSEU FOR TROUBLESHOOTING OF NOSE DOOR AND GEAR DISAGREE CAUTION MESSAGES AND FOUND FAULT CODE D044 STOOct 25, 2022 · N962SW · Cndair CL6002B19 · Landing Gear Door ActuatorSDR SWIA202156899Angle · crackedCLIP CRACKED AT FS193.00 FRAME WS80.00 AT OUTBOARD FASTENER LOCATION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED CLIP AT FS193.00 FRAME WS 80.00 LH. REF CRJ 200 SRM 51-42-06 AND DWG 600-33101 REV-RFeb 17, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156897Skin · dentedFUSELAGE SKIN DENT W/GOUGE ADJACENT TO FS 295 BETWEEN STGR 24L AND 25L. (C-CHECK) RO 3/10/2021 REPAIRED FUSELAGE SKIN DENT W/GOUGE ADJACENT TO FS 295 BETWEEN STGR 24L AND 25L. REF REO 601R-53-21-3401 REV. -- DATED 2021-03-01. ALL CHECKS GOOD. COMPLIED WFeb 17, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202156919Plate · chafed* LH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED DAMAGE ON LH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE REF CRJ200 SRM 51-12-00 SEE CONTINUATION FOR WORK PERFORMEDFeb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156918Plate · chafed* LH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED DAMAGE ON LH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE REF CRJ200 SRM 51-12-00 SEE CONTINUATION FOR WORK PERFORMEDFeb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156917Plate · chafed* RH INBOARD FLAP INBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED CHAFE ON I/B GUIDE PLATE OF R/H I/B FLAP I/B HINGE ARM REF CRJ 200 SRM 51-12-00. PART WAS OUT OF LIMITS PER REF CRJ 200 SRM 57-40-00 FIG 101. REMOVED AND REPLAFeb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156916Plate · chafed* RH INBOARD FLAP OUTBOARD HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO 3/10/2021 REMOVED CHAFE ON R/H I/B FLAP O/B HINGE ARM I/B GUIDE PLATE REF CRJ 200 SRM 51-12-00. PART WAS OUT OF LIMITS PER REF CRJ 200 SRM 57-40-00 FIG 101. REMOVED AND REPLACEFeb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156898Plate · cracked* LH INBOARD FLAP INBOARD HINGE ARM OUTBOARD GUIDE PLATE CRACKED. (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW 1EA. GUIDE PLATE, 4EA NUTPLATES, 10EA SOLID RIVETS AND 8EA BLIND NUTPLATE RIVETS, REF: CRJ 200, SRM 51-45-00, SRM 51-42-06, SRM 51-42-15Feb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156896Hinge Arm · gouged* RH INBOARD FLAP INBOARD HINGE ARM GOUGED AT ATTACH LUG COMMON TO HINGE BOX. (C-CHECK) RO 3/10/2021 BLENDED GOUGE ON R/H I/B FLAP I/B HINGE ARM ATTACH LUG COMMON TO HINGE BOX REF CRJ 200 SRM 51-12-00. PART IS WITHIN LIMTS PER MHI-RJ REO 601R-57-54-319, RFeb 13, 2021 · N962SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156895Housing · damagedWHILE REMOVING CARGO DOOR HANDLE HOUSING, MISDRILLED ONE FASTNER LOCATION INTO THE SKIN AND INNER DOUBLER. (C-CHECK) RO 3/10/2021 REPLACED CARGO DOOR HANDLE HOUSING DOUBLER AND REPAIRED THE FASTENERS HOLE REF REO 601R-52-31-341 REV -- DATED 2021-03-05, CRFeb 12, 2021 · N962SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202156912Floor Support · corroded* FLOOR SILL FWD OF THE SERVICE DOOR CORRODED AT APROX. F.S.331.00. (C-CHECK) RO 3/10/2021 FLOOR SILL FWD OF SERVICE DOOR REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, 51-42-13, 51-45-00Feb 10, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156915Coaming · chafed* AFT CARGO DOOR COMING CHAFED IN MULTIPLE SPOTS. (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW LOWER CARGO DOOR COAMING, REF: CRJ 200, SRM 51-41-02 / PERFORMED PRESSURE CHECK ON CARGO DOOR SEAL COAMING. REF CRJ200 AMM 21-32-00-863-801. CHECK FAILED DUFeb 9, 2021 · N962SW · Cndair CL6002B19 · Cargo/Baggage DoorsSDR SWIA202156911Seat Track · corroded* FS 559+80 TO FS 621.0 RBL 27 HAS SEAT TRACK CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED FS 559+80 TO FS 621.0 RBL 27 P/N 601R386631-3, P/N 601R386631-9 AND P/N 601R38779-9 AT FS 559+80 TO FS 621.0 TOOL USED: TUC5657 DUE 31-MAR-21. REF. CRFeb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202156910Seat Track · corroded* BETWEEN FS 559+80 AND FS 559+96 RBL 9 AND LBL 9 TWO SMALL SECTIONS OF SEAT TRACK HAVE CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW CARGO TIE DOWN SEAT TRACK SECTION FROM FS 559+80 TO FS617 ON RBL 9 AND LBL 9 PART # 601R386631-3, 601R3866Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202156909Seat Track · corroded* LBL 27 FS 559+80 TO FS 617.0 SEAT TRACK HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED CORRODED SEAT TRACKS, AND INSTALLED NEW SEAT TRACKS (P/N'S: 601R386631-3, 601R386631-9, AND 601R38779-9) WITH NEW HARDWARE ON LBL27 FROM FS559 +80 TO FS617.00 REF CRJ20Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202156908Bolt · corroded* R/H SPOILERON ALL ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED R/H SPOILERON ALL ATTACHING HARDWARE REF CRJ 200 AMM 27-64-01-400-801 OPS CHECK GOODFeb 9, 2021 · N962SW · Cndair CL6002B19 · SpoilersSDR SWIA202156907Bolt · corroded* R/H FLIGHT SPOILER ALL ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW R/H FLIGHT SPOILER ALL ATTACHING HARDWARE REF CRJ 200 AMM 27-64-05-400-801. OPS CHECK GOODFeb 9, 2021 · N962SW · Cndair CL6002B19 · SpoilersSDR SWIA202156906Bolt · corroded* L/H FLIGHT SPOILER ALL ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW L/H FLIGHT SPOILER ATTACHING HARDWAR. REF CRJ 200 AMM 27-64-05-400-801. OPS CHECK GOOD SEE CONTINUE CARD FOR DETAILSFeb 9, 2021 · N962SW · Cndair CL6002B19 · SpoilersSDR SWIA202156905Bolt · corroded* L/H SPOILERON ATTACHING HARDWARE HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND REPLACED WITH NEW L/H SPOILERON ATTACHING HARDWARE REF CRJ 200 AMM 27-64-01-400-801. OPS CHECK GOODFeb 9, 2021 · N962SW · Cndair CL6002B19 · SpoilersSDR SWIA202156894Pressure Deck · corroded* LH PRESSURE FLOOR SILL PANEL FROM F.S. 409+128 TO F.S.559.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED).BLENDED OUT 11 SPOT OF CORROSION ON LH PRESS FLOOR SILL PANEL BETWEEN FS409-128 AND FS559 PER REF CRJ 200 SRM 51-21-06. FOUND 4 OF THEM OUT OF LIMITS DUE TOFeb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202156893Pressure Deck · corroded* RH PRESSURE FLOOR SILL PANEL FROM F.S. 409+128 TO F.S.559.00 HAS MULTIPLE SPOTS OF CORROSION (MARKED). (C-CHECK) RO 3/10/2021 REMOVED CORROSION FROM RH PRESSURE FLOOR SILL PANEL FROM F.S. 409+128 TO F.S.559.00. REF REO 601R-53-41-666 REV. -C DATED 2012-Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202156892Floorbeam · corroded* FS 559+80 RBL 9 TO RBL 27 TOP CAP HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW CAP PN 601R32215-43. REF. CRJ200 SRM 51-42-06 AND DWG 601R32215 REV. M. COMPLIED WITH 51-900-1003-SKY.Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202156891Support · damaged* LH SILL AT FS 559.0+16 TO FS 559.0+32 HAS A MISDRILLED HOLE (C-CHECK) RO 3/10/2021 REPAIRED LH SILL AT FS 559.0+16 TO FS 559.0+32. REF REO 601R-53-51-560 REV. -- DATED 2021-02-12. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILSFeb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156890Strap · corroded* LH TOP STRAP @ FS 559.0 RBL 27 TO SILL HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED CORROSION ON L/H STOP STAP AT FS559 LBL27 TO FLOOR SILL REF CRJ 200 SRM 51-21-06, PART WAS OUT OF LIMITS PER 53-00-00, REMOVED AND REPLACED STRAP REF CRJ 200 SRM 51-42-0Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156889Strap · corroded* RH TOP STRAP @ FS 559.0 RBL 27 TO SILL HAS CORROSION (C-CHECK) RO 3/10/2021 REMOVED CORROSION ON R/H STOP STAP AT FS559 RBL27 TO FLOOR SILL REF CRJ 200 SRM 51-21-06, REMOVED AND REPLACED STRAP REF CRJ 200 SRM 51-42-06, & BOMBARDIER DWG # 601R31025, REV Feb 9, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202156888Lintel · cracked* PAX DOOR UPPER LINTEL CRACKED AT F.S.379.00 STR.3L. (C-CHECK) RO 3/10/2021 REPAIRED PAX DOOR UPPER LINTEL AT F.S.379.00 STR.3L. REF DRAWING 601R31016 REV D AND CRJ200 SRM 53-00-03. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILSFeb 9, 2021 · N962SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202156904Bolt · corroded* LH ELEVATOR HINGES ATTACH AND BONDING HARDWARE HAS CORROSION ( ALL THREE HINGES) (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED NEW BONDING JUMPER HARDWARE 33EA NUTS, 8EA SCREWS, 19 WASHERS/LOCKWASHERS REF. CRJ-200 AMM 51-80-00-400-803. / PERFORMED BONDINFeb 8, 2021 · N962SW · Cndair CL6002B19 · Elevator StructureSDR SWIA202156903Bolt · corroded* RH ELEVATOR HINGES ATTACH AND BONDING HARDWARE HAS CORROSION ( ALL THREE HINGES) (C-CHECK) RO 3/10/2021 ORDERED AND RECEIVED 10EA NUTS, 8EA WASHERS 4EA SCREWS 4EA LOCK WASHERS FOR RH ELEVATOR HINGES SEE TRANS# 22107719 JOB 2785990 OP 517 FOR INSTALLATIOFeb 8, 2021 · N962SW · Cndair CL6002B19 · Elevator StructureSDR SWIA202156887Angle · cracked* RH FS 625.0 UPPER CLIP CRACKED (C-CHECK) RO 3/10/2021 REMOVED AND INSTALLED FS 625.0 UPPER CLIP AT STR 14 REF CRJ-200-SRM 51-42-21 .AND REO 601R-53-61-422 REV NC DATED 2001-08-23. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILSFeb 8, 2021 · N962SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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