JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 jasc_code = '5300' 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.
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 jasc_code = '5300' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA2022010801Stanchion · corrodedSTANCHION CORRODED BEYOND LIMITSSDR SWIA202264766None · corroded*CORROSION ON PLATE ATTACHED TO TOP FLANGE ON FRAME FS 501.00 APPROX STGR 25L (C CHECK RO 02/25/2022) REMOVED AND REPLACED WITH NEW PLATE FOR NUTPLATE P/N SH670-34081-11 ON FS501 AT STR 25L REF CRJ 700 SRM 51-42-06-001-001-A01.SDR SWIA202264696None · corroded*CORROSION ON FWD CARGO MACHINED BRACKET (LBL 2.6) (C CHECK RO 02/25/2022) REMOVED AND REPLACED MACHINE BRACKET FWD CARGO LBL2.6. REF CRJ 700 SRM 51-42-21-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, DWG: SH670-33600 REV AD, COMPLIED WITH SKY CARD 51-900SDR SWIA202264695None · corroded*CORROSION ON FWD CARGO DOOR SILL. AREAS MARKED. (C CHECK RO 02/25/2022) COMPLIED PER REO # 670-53-31-766, REV€”DATED 2022-01-17 STEPS 1 TO 5. WORKED CONDITIONS ARE STRUCTURALLY ACCEPTABLE FOR MULTIPLE BLENDED CORROSION DAMAGED TO FORWARD BAGGAGE BAY DOOSDR JJBA20220107013Not Reported · not reportedREAR FUSELAGE SKIN HAS CORROSION UNDER RAR #2 ANTENNA BASE. CUT OUT DAMAGE AT RAR #2 FR68-69 STR 21L-21R AND INSTALLED REPAIR DOUBLER AND FILLERSDR A6WA202101118064Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.50+15" AND S26L TO S27. DENT DIMENSIONS ARE: (P1) .400"L X .350"W X .020"D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVISDR A6WA202101118062Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.00 AND S21R+3. DENT DIMENSIONS ARE: (P1) 1.00L X .800W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SERVICE**********SDR GTIA2022011036210None · dentedDENT CAUSED BY BIRD STRIKE ON FUSELAGE BELOW F.O.S SLIDING WINDOW BETWEEN FRAM 5&6 ,ZONE 1, CODE C. RAF 01 CREATED-REPAIRED DENTED FUSELAGE SKIN BELOW FO'S SLIDING WINDOW FR 5-6 IAW A320 SRM 53-11-11-300-011, REPAIR REQUIRES RE INSP AT 60,000/120,000 FH SUBSIQSDR A6WA202101108052Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 654.00 TO FS 672.00 AND S25R-26R. DENT DIMENSIONS ARE: (P1) .600L X .300W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROM SESDR A6WA202101108053Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 736+15 AND S20R+2. S21R HAS EDGE DAMAGE AT SAME AREA ON SKIN INTERIOR MEASURING: .450"L X .050"W X .050"D. DENT DIMENSIONS ARE: (P1) .600L X .300W X .008D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IASDR A6WA202101108055Skin · dentedAIRCRAFT L/H SKIN EXTERIOR HAS 1 EACH DENT AT FS 605.00 TO FS 621.00 AND S17L-19L. DENT DIMENSIONS ARE: (P1) 3.500"L X .800"W X .017"D. EVALUATED DENT AND FOUND NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV. 38. ****************AIRCRAFT REMOVED FROSDR CALA2022011000080None · crackedL/H FR 16 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A AFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPEC " REFF VT MAE NRC 0020933 FOR WORK PERFORMED. 2A OF LATESSDR CALA2022011000079None · crackedR/H FR 16 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #3 D AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A OF ACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS VT MAE NRC 0020971 FOR WORK PERFORMED. LATEST REVISION OF EC/RASDR CALA2022011000077None · crackedL/H FR 20 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B REACHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION FF VT MAE NRC 0020973 FOR WORK PERFORMED. OF LATEST REVISSDR CALA2022011000076Fitting · crackedWHILE AT VT AREOSOACE BFM DURING C-1 CHECK REF NR0021094 ROTO PROBE OF RH FR66 #5 DOOR STOP FITTING HOLE D1 FOUND CRACK INDICA TION. PLUG & WASHER IAW SRM 53-73-12-001. RE-INSTALLED DOORSTOP FITTIN EMBODIMENT 33000FC (FH NOT RELAVENT) SUBSEQUENT INSP AT INTERVSDR CALA2022011000075Intercostal · corrodedL/H FR 20 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #3 AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L CHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONSSDR CALA2022011000073None · none(AD 2018-03-12) L/H FR66 DOOR STOP #7 TOP AND BOTTOM O/B HOLES H AVE OVALITY. DOOR STOP #3 BOTTOM I/B HOLE HAS A REJECTABLE DAMAG E INDICATION. DOOR STOP #1 TOP O/B HOLE HAS A CRACK INDICATION,B OTTOM O/B HOLE HAS OVALITY REPAIRED L/H FR66 DOOR STOPS IAW EC/RASDR CALA2022011000068None · cracked(AD 2018-03-12) R/H SIDE FR66 DOOR STOP #7 TOP I/B HOLE HAS A CR ACK INDICATION. DOOR STOP #3 BOT I/B HOLE HAS REJECTABLE DAMAGE INDICATION.() REPAIRED R/H FR66 DOOR STOP #7 IAW EC/RA 5341-01293 EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBSDR 2A6D2022010710401Deck Plate · dentedSHARP DENTS ON THE R/H SIDE IN AN AREA .35” LONG BY 1.1” WIDE WITH A MAX DEPTH OF .033” DEEP. THE DAMAGE IS LOCATED AT APPROXIMATELY STA 4370, WL 1759, AND BL 350R.SDR IXXA2022010704Shear Tie · corrodedSHEAR TIE CORRODED OUT OF LIMITSSDR IXXA2022010703Shear Tie · corrodedSHEAR TIE CORRODED BEYOND LIMITSSDR SWIA202264878None · corrodedLH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED THE LH OVERWING EXIT INTERCOSTAL IAW CRJ-200 SRM 51-42-06. LEAK CHECK IS GOOD AT THIS TIME. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED. NO CHSDR SWIA202264876None · corrodedRH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IS CORRODED (C CHECK RO 3/11/2022) REPLACED RH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06 REV 38B DATED 11/25/2020, COMPLIED WITH 51-900-1003-SKY, NO CHANGE TO WEIGHT AND BALANCE. RESDR SWIA202264872None · gougedPASSENGER DOOR OUTER SKIN GOUGED ON LOWER FWD EDGE. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR FWD SEAL RETAINER IAW CRJ-200 SRM 51-42-13 AND 51-42-06. COMPLETED FORM M-337 AND TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REF ATTACSDR SWAA2022022159185Bracket · crackedCRACK BRACKET LOCATED BS540 PLUS 34 INCH AND RBL44.10 AT AIR CONDITIONING BAY 2022-15677 / [01] REPLACED BRACKET ASSY LOCATED BS540 PLUS 34 INCH AND RBL.44.10 AT AIR CONDITIONING BAY AND FASTENERS IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG # 111A5000 RSDR A6WA202202218114Web · noneREAR SKIN PANEL OF AFT PRESSURE BULKHEAD IS MISSING ALL REINFORCEMENT ANGLES (7 EA) -59, -61, -62, -65, -66, -69, & -70 REF BOMBARDIER REO 601R-53-61-1240 REV D DTD 2016-10- 13 ***AIRCRAFT REMOVED FROM SERVICE*** GENERAL AND DETAILED INSPECTION C/W, WITH NSDR A6WA202202158102Doubler · dentedAFT PRESSURE BULKHEAD HAS A DENT LOCATED AT FS621.00 AND RBL6.0, WL80.0. ***AIRCRAFT REMOVED FROM SERVICE*** CUT AWAY EXISTING UPPER DOUBLERS P/N 601R-53-61-1240-3 AND -4 AND EXISTING LOWER DOUBLERS P/N 601R-53-61-1240-1 AND -2. REMOVED DENT DAMAGE. FABSDR SWIA202264189None · corrodedCORROSION FOUND ON STIFFENER BETWEEN FS985.00 AND FS1000.00, BETWEEN STGR25L AND STGR26L COMMON TO FUEL-SYSTEM AFT DRAIN MAST (C CHECK RO 02-03-22) REPLACED STIFFENER BETWEEN FS985 - FS1000 STR 25L - 26L. REF CRJ700 SRM 51-40-11-001-001-A01 AND REF CRJ700 SDR SWIA202264077None · crackedCRACKED RIVET AND EVIDENCE OF CRACKED AERODYNAMIC FLANGE AT FRAME 54, ABOVE OVER-WING PNL. (MARKED) (C CHECK RO 01/28/2022) REMOVED AND REPLACED AERODYNAMIC FLANGE AT FRAME 54 REF EMB SRM 51-40-08SDR JJBA20220106016Not Reported · not reportedCORROSION FOUND ON RH OMEGA BEAM AT FR 23 IN CF I FLOOR STRUCTURE AREA. RH OMEGA BEAM AT FR 23 IN CFI FLOOR STRUCTURE BLENDED OUT OF LIMITS FOR CORROSION REMOVAL. PERFORMED CUTOUT AND DOUBLER REPAIR ON RH OMEGA BEAM AT FR23.SDR JJBA20220106008Not Reported · not reportedCF II, EXTERNAL FUSELAGE, LIGHTING STRIKE 1.000 INCH FWD FRAME 27 BTW STR 8R-9R. CFII, EXTERNAL FUSE SKIN, 1 FWD OF FRAME 27 BTW STR 8R-9R, PAINT STRIPPED FOR INVESTIGATION. DOUBLER REPAIR FABRICATED. CFII EXTERNAL SKIN, LIGHTNING STRIKE 1 IN FWD OF FR 27 BTW SDR JJBA20220106007Not Reported · not reportedCORROSION FOUND UNDER DATA PLATE ON AFT RF2 EXTERNAL SKIN BTW FR 78-79 AND STR 21L-21R. CORROSION BLENDED OUT OF LIMIT. REAR FUSELAGE II LOWER SKIN BTW FR 80-81 AND BTW STR 21L-21R REPAIRED WITH CUT OUT AND DOUBLER.SDR IXXA2022010602Skin · corrodedFUSELAGE SKIN CORRODED STA. 676 S36LSDR SWIA202265079None · cracked*ANGLE INSIDE RH AFT EQUIPMENT BAY HAS A POSSIBLE CRACK. FS 625.30.STGR 15R. FLAGGED AND MARKED (C-CHECK RO 3/14/2022) REMOVED AND REPLACED ANGLE BRACKET IN R/H AFT EQUIPMENT BAY AT FS625.30 STGR 15R WITH NEW P/N 601-35012-54 REF CRJ 200 SRM 51-42-06 ANSDR SWIA202264779None · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA47357-ETD2019-170-043590-N108SY-PR - DENT AND SCRATCH DAMAGE TO THE FWD FUSE SKIN BTWN FR10-FR11 AND STR14L-15L. PERFORMED TEMP ACTIONS IN REF TO ETD2019-170-043590, REV :/, DTD 03/29/2019. PERFORM PERM REPAIR PER SRM SDR SWIA202264747None · corroded*LH WING REAR SPAR AFT SIDE €“ CORRODED ANGLE ATTACHED TO REAR SPAR BETWEEN APPROXIMATELY WS48 AND WS58 (MARKED). (C CHECK RO 02/25/2022) REPLACED ANGLE PN CC670-10338-1 REF CRJ 700 SRM 51-42-21-001-001-A01. SEE CONTINUE CARD FOR DETAILS.SDR SWIA202264641None · crackedLH WINDSHIELD POST HAS EXCESSIVE SEALANT CONCEALING POST STRUCTURE FROM INSPECTION, COULD NOT DETERMINE IF UPPER / BARREL NUT HOLE IS CRACKED. (C CHECK RO 02/22/2022) REMOVED AND REPLACED WITH NEW LH WINDSHIELD POST REF CRJ 700 SRM 51-42-21-001-001-A01. SDR SWIA202264320None · corrodedWHILE REMOVAL OF RH APRON SKIN FOR REPALCEMENT ,FOUND A BOTTOM SUPPORT CHANEL CORRODED. (C CHECK RO 02-12-2022) INSTALLED NEW R/H BOTTOM SUPPORT CHANEL REF DWG 601R31058 REV.R AND CRJ 200 SRM 51-42-06 REV.38 DATED JUL 10/19 . COMPLIED WITH 51-900-1003SDR JJBA20220105005Not Reported · not reportedLAV UNDER FLOOR SUPPORT AT FR 59-61 BUT LINE O CORROSION. REMOVED AND REPLACED LAV FLOOR SUPPORT CENTER GUSSET AT FR 59-61SDR IXXA2022010505Door Sill · corrodedCORROSION ON AFT LOWER CARGO DOOR LOWER SILLSDR IXXA202201050004Intercostal · corrodedCORROSION ALC STATION 1241 INTERCOASTAL FWD. END O/B SIDE OF STRING 32RSDR IXXA2022010503Intercostal · bentINTERCOSTAL IS BENTSDR IXXA2022010502Seat Track · corrodedUPPER CABIN SEAT TRACK CORRODEDSDR HNAA2022010500045None · noneE893076 - CENTER CABIN FLOOR BEAM SEAT TRACK #3 IS CORRODED ... REMOVED CORRODED SEAT TRACK AND INSTALLED SERVICEABLE CENTER SEAT TRACK #3 IAW EMB 145 AMM 53-01-06SDR IXXA2022010501Longeron · corrodedSTRINGER CLIP CORRODEDSDR 2022FA0000322Magneto · faultyENGINE FAILED TO START WHEN HOT! NEW MAGNETO FAILED TO START MULTIPLE TIMES AND STRAINED PILOT! INSTALLED ANOTHER NEW MAGNETO AND ENGINE STARTED NORMALLY AND NO FURTHER PROBLEMS NOTED.SDR SWIA202265011None · chafedANGLE ON THE VERTICAL FRONT SPAR TO FUSELAGE SPLICE STRAP IS CHAFFED (MARKED) (C-CHECK RO 3/14/2022) REPLACED ANGLE ON THE VERTICAL FRONT SPAR TO FUSELAGE SPLICE STRAP REF DWG 600-21108 REV. C, CRJ200 SRM 51-42-21, CRJ200 SRM 51-41-02. COMPLIED WITH 51-9SDR SWIA202264640None · crackedRH WINDSHIELD POST APPEARS CRACKED RADIATING FORWARD FROM UPPER BARREL NUT HOLE. (C CHECK RO 02/22/2022) C/W NDT INSP REF CRJ-700 NDTM PT1 51-20-006-250-A01. CRACK NOTED TUC9452 CAL DUE 31 AUG 2022. SEE ATTACHED NDT -9 REPORT. / REMOVED AND REPLACED BEAM SDR SWIA202264637None · damagedFUSELAGE SKIN DAMAGED AT FS977 TO FS985 AND STGR27. (C CHECK RO 02/22/2022) REMOVED DAMAGE REF CRJ700 SRM 51-12-00-001-001-A01. BLEND IS OUT OF LIMITS REF CRJ700 SRM 53-61-01-101-003-A01. COMPLIED WITH REO 670-53-00-290 REV -F DATED 2019/04/26. COMPLIED SDR A6WA202202218111Seat Track · corrodedLH SIDEWALL SEAT TRACK FROM FS409.00 TO FS559.00 +112 HAS SURFACE CORROSION. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED AND REPLACED LH SIDEWALL SEAT TRACK PN 20276-144-0-0 FROM FS409.00 TO FS559.00 +112. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS
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