N945SW

Service difficulty reports · 305

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 = 'N945SW' 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 SWIA2021080560084Rib · corrodedLEFT AILERON ASSEMBLY @ RIB ASSY WS 364, OUTBOARD AND INBOARD BRACKET BOLT RETAINERS HAVE CORRODED HARDWARE. (C-CHECK RO 8/1/2021) REPLACED LEFT AILERON ASSEMBLY RIB ASSY WS 364 OUTBOARD AND INBOARD BRACKET BOLT RETAINERS PER CRJ 200 SRM 51-41-04 / USEMay 23, 2021 · N945SW · Cndair CL6002B19 · AileronsSDR SWIA2021080560057Vane · chafed* THE RH INBOARD FLAP VANE IS CHAFED ON ITS MID OUTBOARD VANE CAP. (C-CHECK RO 8/1/2021) REPAIRED R/H INBOARD FLAP VANE MIDDLE OUTBOARD VANE CAP REF REO 601R-57-52-004 REV -D, DATED 2012-12-19. SEE CONTINUATION CARD FOR DETAILSMay 23, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021080560055Vane · chafed* THE LH INBOARD FLAP VANE IS CHAFED ON ITS INBOARD VANE CAP. (C-CHECK RO 8/1/2021) FOUND TO BE OUT OF LIMITS PER REO 601R-57-52-004 REV -D DATED 2012-12-19. ORDERED AND RECEIVED NEW FLAP VANE ASSEMBLY P/N 601R14302-1 ON CAMP#22866305. SEE CAMP# 2287903May 23, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021080560024Skin · damaged* THE LH OUTBOARD FLAP HAS APPROX. 40 SMOKING RIVETS ON ITS UPPER SKIN. (ALL RIVETS MARKED WITH RED GREASE PENCIL) (C-CHECK RO 8/1/2021) REMOVED AND INSTALLED 40(EA) NEW RIVETS ON L/H OUTBOARD FLAP UPPER SKIN REF. REO 601R-57-53-1223 REV -- DATED 2021-May 23, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021080560023Skin · dented* THE RH INBOARD FLAP'S LOWER SKIN HAS 1 DENT LOCATED JUST INBOARD OF THE OUTBOARD HINGE ARM, 28 INCHES FROM THE OUTBOARD EDGE AND 7 INCHES FWD OF THE TRAILING EDGE. (DENT IS CIRCLED WITH RED GREASE PENCIL) (C-CHECK RO 8/1/2021) REPAIRED THE RH INBOARD May 23, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021080560022Skin · dented* THE LH INBOARD FLAP'S LOWER SKIN HAS 2 DENTS. THE FIRST DENT IS LOCATED AT THE LOWER INBOARD CORNER BEHIND THE INBOARD TIRE, THE SECOND DENT IS LOCATED ON THE TRAILING EDGE 23 INCHES FROM THE INBOARD END. (BOTH DENTS CIRCLED WITH RED GREASE PENCIL) (C-CHMay 23, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021080560021Vane · chafed* THE RH INBOARD FLAP VANE IS CHAFED ON ITS OUTBOARD VANE CAP. (C-CHECK RO 8/1/2021) REMOVED AND REPLACED WITH NEW. LOCATED AND DRILLED REF CRJ200 SRM 51-42-13 DWG 601R14302 REV E . COMPLIED WITH 51-900-1003-SKYMay 23, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202160020Vane · chafed* THE RH INBOARD FLAP VANE IS CHAFED ON ITS INBOARD VANE CAP. (C-CHECK RO 8/1/2021) INSTALLED NEW INBOARD FLAP VAINE CAP AT R/H INBOARD FLAP. REF. CRJ 200 SRM 51-42-13, DWG 601R14302 REV. E COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DEMay 23, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021080560098Drag Angle · cracked*PASSENGER DOOR AFT DRAG ANGLE HAS A POSSIBLE CRACK NEAR PULLEY BRACKET. (C-CHECK RO 8/1/2021) REMOVED AN REPLACED WITH NEW DRAG ANGLE REF CRJ200 SRM 51-42-10May 21, 2021 · N945SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202160019Skin · dented*DENT FORWARD LH FUSELAGE APPROXIMATELY 6.5€? FORWARD OF FS250 BETWEEN STR21L AN STR22L. (C-CHECK RO 8/1/2021) REPAIRED FORWARD LH FUSELAGE APPROXIMATELY 6.5€? FORWARD OF FS250 BETWEEN STR21L AN STR22L. REF MHIRJ REO 601R-53-11-3707 REV -- DATED 2021May 21, 2021 · N945SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202160018Skin · dentedDENT BETWEEN FS672.20 TO FS 700.0 BETWEEN STRINGERS 18L AND 19L MEASURES 18" LONG BY 0.500" WIDE AND 0.013" DEEP IS WITHIN LIMITS AND YELLOW DOTTED. (C-CHECK RO 8/1/2021) REPAIRED FUSELAGE SKIN BETWEEN FS672.20 TO FS 700.0 BETWEEN STRINGERS 18L AND 19L May 15, 2021 · N945SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA2021080560095Structure · gougedREMOVE AND INSTALL LH ELEVATOR. COMPLY WITH TASK CARD 27-900-1004-SKY (C-CHECK RO 8/1/2021) REMOVED AND REINSTALLED LH ELEVATOR REF CRJ-200 AMM 27-34-01-400-801. COMPLIED WITH TASK CARD 27-900-1004-SKY. BOND CHECK GOOD. / SEE JOB 27770101 OP 436 MX TRANMay 10, 2021 · N945SW · Cndair CL6002B19 · Elevator StructureSDR SWIA2021080560086Hinge Arm · corrodedREMOVE AND INSTALL RH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00, AND WS264.00 (C-CHECK RO 8/1/2021) REMOVED AND INSTALLED RH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00 AND WS264.00 IAW CRJ-200 AMM 57-53-02-400-801, 57-53-02-400-803 AND 57-5May 10, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202160017Vane · dentedD: FOUND SMALL DENT ON L/E OF LH OUTBOARD FLAP VANE, JUST INBOARD OF #3 HINGE ARM. INSPECTED DENT ON L/E OF LH OUTBOARD FLAP VANE IN REFERENCE TO SRM 57-53-00. DENT MEASURED 0.5" L X 0.25" W X 0.0175" D. DENT FOUND TO BE WITHIN ACCEPTABLE LIMITS AT THIS TIME.May 8, 2021 · N945SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202156979Angle · crackedLH INTERCOSTAL CLIP, AFT OF REAR PRESSURE BULKHEAD AT STGR 14L, CRACKED. FILED CLOSED COMPLIED WITH TEMPORARY DISPOSITION OF CRACKED LH INTERCOSTAL CLIP AT AFT PRESSURE BULKHEAD STGR 14L (CLIP PN 601-35012-51) IN REF TO GREO 601R53-61-1550 REV -B DATED Mar 24, 2021 · N945SW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2021080560085Bushing · corrodedREMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 8/1/2021) ORDERED AND REIVED 4EA NEW BUSHINGS P/N#S1512-52 FOR LH AILERON WING TRAILING EDGE CENTER HINGE FITTING LUGS @ WS319.604 AND WS32Mar 8, 2021 · N945SW · Cndair CL6002B19 · AileronsSDR SWIA2021080560016Bulkhead Web · 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 WITHMar 8, 2021 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549038Floor Support · corrodedF.S. 615 ON LBL 27 FLOOR SUPPORT BEAM O/B FLANGE HAS CORROSION AROUND NUT PLATE HOLE (C CHECK) RO 3/2/2020 INSTALLED REPAIR ON FLOOR SUPPORT BEAM O/B FLANGE AROUND NUT PLATE HOLE AT FS 615, LBL 27 IAW REO.Feb 28, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030549090Nut Plate · damagedFLOOR SILL RH SIDE FS 564-FS 621 HAS DAMAGED NUT PLATES (C CHECK) RO 3/2/2020 REMOVED AND REPLACED NUTPLATES AND RIVETS ON R/H SIDE FLOOR SILL AT FS 564 TO FS 621. RESTORED PROTECTIVE FINISH PER SRM.Feb 17, 2020 · N945SW · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA2020030549037Skin · damagedWING FUEL TANK PANEL 640BB WING PLANK LANDING HAS AREAS OF PITTING (C CHECK) RO 3/2/2020 C/W REPAIR OF RH WING PLANK FUEL ACCESS LANDING LOWER (640BB) IAW REO. BLEND WAS FOUND OUTSIDE OF CRITICAL AREA. ORIGINAL .186, REMOVED .002, REMAINING .184 NO FURTHERFeb 17, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549036Skin · damagedWING FUEL TANK PANEL 540BB WING PLANK LANDING HAS AREAS OF PITTING (C CHECK) RO 3/2/2020 C/W REPAIR OF LH WING PLANK FUEL ACCESS LANDING LOWER (504BB) IAW REO. BLENDOUT WAS OUTSIDE OF THE CRITICAL AREA WITH A REMAINING THICKNESS OF .188. FOUND TO BE WITHIFeb 17, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549086Angle · corrodedDURING INSPECTION CORROSION FOUND ON SERVICE DOOR ENTRY WAY AT FS 319 RBL 43 (C CHECK) RO 3/2/2020 FOUND CORROSION ON SERVICE DOOR ENTRY WAY TO BE OUT OF LIMITS. NOMINAL 0.050, REMOVED 0.020, REMAINING 0.030. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED PFeb 11, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030549092Support Bracket · corrodedDURING INSPECTION CORROSION WAS FOUND ON SUPPORT BRAKET AT FS 621 LBL 45 WL 75 (C-CHECK) RO 3/2/2020 REMOVED AND REPLACED BRACKET PER CRJ 200 SRM.Feb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030549091Support Bracket · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SUPPORT BRACKET AT FS 621 RBL 40 (C CHECK) RO 3/2/2020 UPON EVALUATION, FOUND CORROSION ON NUTPLATES ON FLOOR SUPPORT BRACKET AT FS 621 RBL 40. SURROUNDING AREA WAS ONLY BARE METAL. REMOVED AND REPLACED AFFECTFeb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030549078Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SUPPORT ANGLE AT FS 621 RBL 45 (C CHECK) RO 3/2/2020 UPON EVALUATION, FOUND CORROSION ON NUTPLATE UNDER FLOOR SUPPORT ANGLE AT FS 621 RBL 45. SURROUNDING AREA WAS ONLY BARE METAL. REMOVED AND REPLACED AFFECTEDFeb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030549072Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON SEAT TRACK RAILS FLOOR AT FS 559-559+80 RBL 9 (C CHECK) RO 3/2/2020 REMOVED AND REPLACED SEAT TRACK AT FS 559 TO FS 559+80 RBL 9 PER SRM. SEE WC 1057 FOR SEAT TRACK FABRICATION. (REF: CRJ-200 SRM 53-01-11) TORQUE WRFeb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030549068Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SEAT TRACK RAIL AT FS 364-394 LBL 9 (C CHECK) RO 3/2/2020 REMOVED AND REPLACED SEAT TRACK AT FS 364-394 LBL 9 PER CRJ-200 SRM AND AMM. (TORQUE WRENCH: AV8584 DD: JUNE 2020)Feb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030549066Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SEAT TRACKS AT FS 409+128-559+40 LBL 9 (C CHECK) RO 3/2/2020 AFTER EVALUATION. SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH SERVICABLE SEAT TRACK THAT WAS FABRICATED ON W/C 1057. CRJ 2Feb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030549065Seat Track · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SEAT TRACK AT FS 409+128-559+40 RBL 9 (C CHECK) RO 3/2/2020 AFTER EVALUATION, SEAT TRACK WAS FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED WITH SERVICEABLE SEAT TRACK THAT WAS FABRICATED ON W/C 1057. / CRJ20Feb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020030549034Frame · corrodedDURING INSPECTION CORROSION WAS FOUND ON FRAME AT FS 605 STRG L20 STRG R 19 (C CHECK) RO 3/2/2020 REMOVE CORROSION AND EVALUATE; CORROSION WAS FOUND BEYOND ALLOWABLE LIMITS.REMOVE FRAME AT FS 605, STRG L20 R 19. MATCH DRILLED REJECTED FRAME TO NEW FRAME Feb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2020030549032Floor Support · corrodedDURING INSPECTION CORROSION FOUND ON FLOOR SUPPORT STRUCTURE NUT PLATE HOLE AT FS 615 RBL 29 (C CHECK) RO 3/2/2020 REMOVED CORROSION IAW REO. DAMAGE WAS OUT OF LIMITS WITH AN ORIGINAL MATERIAL THICKNESS OF .080", A LOSS OF .055" AND A REMAINING MATERIAL THFeb 10, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030549029Skin · damagedDURING INSPECTION OF LH WING LOWER PLANK ACCESS HOLE FRETTING FOUND (510AB) (C CHECK) RO 3/2/2020 ACCOMPLISHED REPAIR OF LH LOWER WING PLANK ACCESS PANEL LANDING 510AB IAW REO. BLEND WAS FOUND OUTSIDE OF CRITICAL AREA. ORIGINAL .182, REMOVED .005, REMAININFeb 10, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549028Skin · damagedDURING INSPECTION OF LH WING LOWER PLANK ACCESS HOLE PITTING WAS FOUND (540FB) (C CHECK) RO 3/2/2020 ACCOMPLISHED REPAR OF LH LOWER WING PLANK ACCESS PANEL LANDING 540FB IAW REO. BLEND WAS FOUND OUTSIDE OF CRITICAL AREA. ORIGINAL .182, REMOVED .002, REMAINFeb 10, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549026Skin · damagedDURING INSPECTION OF LH WING LOWR PLANK ACCES HOLE PITTING WAS FOUND (550BB) (C CHECK) RO 3/2/2020 ACCOMPLISHED REPAIR OF LH WING LOWER PLANK ACCESS PANEL LANDING 550BB IAW REO REV. BLEND FOUND INSIDE OF CRITICAL AREA. ORIGINAL .182, REMOVED .002, REMAININFeb 10, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549025Skin · gougedDURING INSPECTION OF LH WING LOWER PLANK ACCESS HOLES A SMALL GOUGE WAS FOUND (550EB) (C CHECK) RO 3/2/2020 ACCOMPLISHED REPAIR OF LH WING LOWER PLANK ACCESS PANEL LANDING IAW REO REV L DATED MAY 2014. BLEND WAS FOUND OUTSIDE OF CRITICAL AREA. ORIGINAL .18Feb 10, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549021Skin · damagedDURING INSPECTION OF LH WING LOWER PLANK ACCESS HOLE PITTING WAS FOUND (550FB) (C CHECK) RO 3/2/2020 ACCOMPLISH REPAIR OF LH WING LOWER PLANK ACCESS PANEL LANDING 550FB BLEND WAS FOUND OUTSIDE OF CRITICAL AREA. ORIGINAL .182, REMOVED .003, REMAINING .179 NFeb 10, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549016Skin · damagedDURING INSPECTION PITTING FOUND ON LH WING LOWER PLANK ACCESS HOLE (550HB) (C CHECK) RO 3/2/2020 ACCOMPLISHED REPAIR OF LH LOWER WING ACCES PANEL LANDING 550HB IAW REO BLEND TO BE FOUND OUTSIDE OF CRITICAL AREA. ORIGINAL .182, REMOVED .002, REMAINING .180 Feb 10, 2020 · N945SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA2020030549051Bulkhead · crackedREAT PRESSURE BULKHEAD U/T CRACK INDICATION RBL 36.20 49"-55" ABOVE FLOOR (6EA FASTNERS) (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO .215 ON REAR PRESSURE BULKHEAD 49"-54" ABOVE FLOOR AND INSTALLED FASTENERS PER CRJ200 SFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549049Bulkhead · crackedULTRA SOUND REAR PRESSURE BULKHEAD CRACK INDICATION AT FASTNER RBL 27.50 31" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENER AND REAMED FASTENER HOLE FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 50" AND 52" ABOVE FLOOR INSTALLED FASTENER PER Feb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549047Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION. FASTNER HOLE RBL 27.50 41" AND 44" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 41" AND 44" ABOVE FLOOR INSTALLED Feb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549046Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION RBL 18.00 32" AND 33" ABOVE FLOOR EMITTING FROM FASTNER HOLES (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 32" AND 33" ABOVE FFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549045Bulkhead · crackedREAR PRESUURE BULKHEAD ULTRA SOUND CRACK INDICATION EMITTING FROM FASTNER HOLES RBL 18.00 50 AND 52" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD RBL 18.00 50" AND 52" ABOVE FLOFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549044Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION EMITTING FROM FASTNER HOLES LBL 9.5 13" AND 35" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD LBL 9.50 13" AND 35" ABOVE FLOORFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549043Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION EMITTING FROM FASTNER HOLES AT LBL 18.00 26" AND 27" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD LBL 18.00 26" AND 27" ABOVEFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549042Bulkhead · crackedREAR PRESSURE BULKHEAD ULTRA SOUND CRACK INDICATION LBL 36.20 13" ABOVE FLOOR (C CHECK) RO 3/2/2020 REMOVED FASTENER AND REAMED FASTENER HOLE FROM 5/32" TO 3/16" ON REAR PRESSURE BULKHEAD LBL 36.20 13" ABOVE FLOOR INSTALLED FASTENER PER CRJ200 SRM. ACCOMPLFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549041Bulkhead · crackedREAR PRESSURE BULKHEAD CRACK INDICATIONS (2 EA) FASTNERS IN UPPER CHORD. LBL 5.00 (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO #5 ON REAR PRESSURE BULKHEAD UPPER CHORD (2EA) HOLES AT LBL 5.00 INSTALLED FASTENERS PER CRJ20Feb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549040Bulkhead · crackedREAR PRESSURE BULKHEAD UPPER CHORD CRACK INDICATIONS EMITTING FROM FASTER (2EA) HOLES AT LBL 11.0 (C CHECK) RO 3/2/2020 REMOVED FASTENERS AND REAMED FASTENER HOLES FROM 5/32" TO #5 ON REAR PRESSURE BULKHEAD UPPER CHORD (2EA) HOLES AT LBL 11.0 INSTALLED FASFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549039Bulkhead · crackedREAR PRESSURE BULKHEAD CRACK INDICATION EMITTING FROM FASTNER HOLE IN UPPER CHORD LBL 19.00 (C CHECK) RO 3/2/2020 REMOVED FASTENER AND REAMED FASTER HOLE FROM 5/32" TO #5 ON REAR PRESSURE BULKHEAD UPPER CHORD LBL 19.00 INSTALLED FASTENER PER CRJ200 SRM. ACFeb 8, 2020 · N945SW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2020030549059Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SUPPORT AT FS 313 LBL 40 (C CHECK) RO 3/2/2020 BLENDED CORROSION IAW SKYWEST CRJ200 SRM. DAMAGE WAS FOUND TO BE OUT OF LIMITS IAW SKYWEST CRJ200 SRM WITH AN ORIGINAL MATERIAL THICKNESS OF .063", A LOSS OF .016Feb 7, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2020030549057Floor Support · corrodedDURING INSPECTION CORROSION WAS FOUND ON FLOOR SUPPORT AT FS 346 LBL 40 (C CHECK) RO 3/2/2020 BLENDED CORROSION IAW SKYWEST CRJ200 SRM. DAMAGE WAS FOUND TO BE OUT OF LIMITS IAW SKYWEST CRJ200 SRM WITH AN ORIGINAL MATERIAL THICKNESS OF .063", A LOSS OF .054Feb 7, 2020 · N945SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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