JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, Plate/Skin, 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 = '5330' 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 = '5330' 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 DALA2022021701071None · noneSHIP 174 THE FUS EXTERNAL SKIN SCRATCH AT BS1417 TO 1395 AND S -36L TO 38L. CORRECTIVE ACTION: REPAIRED AND DOCUMENTED AS PER DAL ER/ A476909-14. (2120408)SDR DALA2022021500991None · noneEVALUATE AFT EXTERIOR SKIN DAMAGE. DURING SV IN BHM PERFORMED WORK ON NRC #5 COMPLIED WITH PRI 596293-14 REV O-6 (767121) QC 5209 PRI 596293-14 REV O-6 MATCHES ERA 596293-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596293-14 REV O (767121) QC 5209. (LP# 212066SDR DALA2022021500990None · noneSKIN DAMAGED BELOW C3 CARGO DOOR. DURING SV IN BHM PERFORMED WORK ON NRC # 31 COMPLIED WITH PRI 596659-14 REV O-2 (767121) QC 5209 PRI 596659-14 REV O-2 MATCHES ERA 596659-14 REV O (767121) QC 5209 COMPLIED WITH ERA 596659-14 REV O (767121) QC 5209. (LP# 21206SDR DALA2022021500986None · noneREF: N/R 138 - RIGHT SIDE REAR FUSELAGE EXTERNAL SKIN SCRATCHED AT FR52 + 3 INCHES , AT STR 40R. COMPLIED WITH ALL STEPS ON PRI 597290-14 REV. "O" DATED 11 FEB. 2022 23:30E INSURED ALL PRI REVISION STEPS MATCHED WITH FINALE ERA INSTRUCTIONS 597290-14 REV. ORIGSDR SCNA20220217001None · noneTASK: TEMPORARY SKIN REPAIR INSTALLED STA 420 STR 20R. RESOLUTION: REMOVED TEMPORARY SKIN REPAIR AT BS 420 STR 20 AND INSTALLED 1 DOUBLER 2024-T3 .063", -2 TRIPLER 2020-T3 .063" AND -3 FILLER 2024-T3 .090" IAW SUN COUNTRY ENGINEERING TASK CARD ENG-53SCA-1091SDR DALA2022021500951None · noneFUSELAGE CROWN LIGHTNING STRIKE DAMAGE AT PREVIOUS BLEND OUT. NO REPAIR TAG PRESENT. -M-. SUMMARY SEE NRC 001-0249:5300-2018/003 00365: REPAIRED LIGHTNING STRIKE DAMAGE ON CROWN PER ER/A 597099-14 PRI REV. 0 THROUGH REV 1. AND ER/A 597099-14AD REV. ORIGINAL. (SDR DALA2022021500949None · noneCORROSION AROUND EXTERIOR SIDE OF VACUUM BLOWER FOR LAV TANK EXHAUST VENT -M-. SUMMARY SEE NRC 001-0247:2550-2003/001 00405: REPAIRED AREA AROUND VENT PER ER/A 597013-14 PRI REV 0 THROUGH REV 3 AND ER/A 597013-14 REV ORIGINAL. (LP #2118994)SDR SWAA2022032171578Gusset · crackedFWD CARGO COMPT GUSSET CRACKED AT BS 500D S19L / [01] REMOVED GUSSET AT FWD CARGO STA 500D; STG 19L AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW GUSSET AT FWD CARGO; STA 500D; STG 19LAS PER B737-700 SRM 51-40-05-0G-0;[03] VERIFIED 1-2. OK TO SDR SWAA2022032171577Gusset · crackedFWD CARGO COMPT GUSSET CRACKED AT BS 500D S19R / [01] REMOVED DAMAGE GUSSET AT FWD CARGO R/H SIDE STA 550D S-19R REF B 737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW GUSSET AT FWD CARGO R/H SIDE STA 550D S-19R REF B 737-700 SRM 51-40-05-0G-0 AND DWG# SDR SWAA2022030871127Baffle · crackedFWD CARGO BAY BAFFLE IS CRACKED AT BS 500B LBL25 / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02-OG-0 STEP 9.;[02] REMOVED BAFFLE DAMAGED AT FWD CARGO BAY BS500B LBL25;IAW SRM 51-40-02-OG-0.;[03SDR AALA202202117574Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE CUT OUT DOUBLER FOR PANEL 312AR. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS. REPAIRED DOUBLER PER EA 333617.SDR N6WA2022021102Support Angle · corrodedL/H SIDE (TIRE BURST PANEL AREA) FWD TIRE BURST PANEL SUPPORT ANGLE CORRODED.R&R L/H SIDE FWD TIRE BURST PANEL SUPPORT ANGLE IAW CRJ SRM 51-42-20SDR DALA2022022401221None · none***DTE*** A321 / FUSELAGE / DENT AND GOUGES/ PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. LOG-PAGE UPDATED @ 09FEB22 1502 UTC 02 DFRD BY GRAY 00495354 BHM 09FEB22 RII: N ENTR 00495354 W REPAIR APPROVAL IS LIMITED TO 6 MOSDR DALA2022022401220None · none***DTE*** A321 / FUSELAGE / FR61-FR62 / STR 40R -STR 41R / DENT / PERMANENT REPAIR. REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM REPAIR ACCOMPLISHMENT. LOG-PAGE UPDATED @ 09FEB22 1425 UTC 02 DFRD BY GRAY 00495354 BHM 09FEB22 RII: N ENTR 00495354 W REPAIR APPROVSDR SWAA2022021470445Skin · corrodedLOWER EXTERNAL SKIN AROUND TOILET SERVICE DOOR CORRODED. STRIPPED PAINT ON EXTERNAL SKIN AREA IAW AMM 51-21-11-150-801 & BEGAN REMOVING PAN ASSY IAW SRM 51-40-02-0G-0 PARA 4.E AND 7.D. STARTED FABRICATING REPAIR PARTS IAW EA 22-153-00433-WIP1. FINISHED FABRSDR SWAA2022030370081Support · missingFORWARD CARGO BAY AFT BULKHEAD SUPPORT CLIP BS 500D STRINGER 24 R/H IS MISSING / [01] LOCATED AND DRILLED NEW SUPPORT CLIP AT BS 500D STR 24R PER SRM 51-40-05-0G-0 AND DWG 143A7902. OK TO INSTALL;[02] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED OK TO INSTALL.;SDR VNAA2022020899923Seat Track · corrodedCORROSION AT SEAT RAIL OF LBL9 BETWEEN FS 581 TO FS 693.0+8SDR VNAA2022020899922Seat Track · corrodedCORROSION AT SEAT RAIL OF LBL9 BETWEEN FS 501 TO FS 581SDR VNAA2022020899921Seat Track · corrodedCORROSION AT SEAT RAIL OF LBL9 BETWEEN FS 377.0 TO FS 501.SDR VNAA2022020899919Stringer · corrodedCORROSION ON STRINGER 27 IN STA.FS 280 TO FS 295 AT MAIN AVIONICS COMPARTMENTSDR SWAA2022022869909Skin · crackedCRACK WAS FOUND ON LEFT HAND FUSELAGE BETWEEN STA. 925+5' S20L AND S21 / [01] PERFORMED HFEC ON CRACK IAW NDTM PART 6;51-00-00 PROCEDURE 23. CRACK LENGTH : 0.433';[18] REPAIR IS BEING ACCOMPLISHED UNDER TASK CARD EA NO:22-153-00509;[19] LOCATED AND DRILLED FUSSDR N6WA2022020906Nut Plate · corrodedRH MLG BURST PANEL 642AZ IS CORRODED. R&R PANEL 642AZ NUT PLATE IAW CRJ 700 SRM 51-42-13 INSRALLED RH MLG BURST PANEL 642AZ IAW CRJ 700 AMM 57-52-32SDR N6WA2022020903Nut Plate · corrodedLH MLG BURST PANEL 542AZ IS CORRODED, R&R ALL NUT PLATED IAW CRJ 700 SRM 51-42-13 INSTALLED LH MLG BLAST PLATE 542AZ IAW CRJ700 AMM 57-52-32.SDR SWAA2022030869697Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25. / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02-OG-0 STEP #9.;[02] REMOVED CRACKED ANGLE AT FWD CARGO BAY BS500C FWD SIDSDR N6WA2022022501Skin Panel · damagedMOVE TEAM STRUCK LEFT SIDE OF AC AFT OF PAX DOOR WHILE TOWING AC. REPAIRED LH SKINDAMAGE BETWEEN FS 279 AND FS 409 STR 16L TO STR 20L IAW GOJET EO C550/700-53MR-059-OM MHIJ REO 670-53-21-2233 AND MHIRJ REO 67-51-00-085 MAJOR REPAIRSDR DALA2022020700775None · noneSHIP 3247 DENT EXTERNAL SKIN LOC. AT FRAME 73 BTW STR 23L AND 24L AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER PRI 596722-14 REV 0 AND ER/A 596722-14 REV ORIGINAL. (2112934)SDR DALA2022020700768None · noneSHIP 3247 DENTS ON EXTERNAL SKIN LOC. AT FRAME 71 R/H BTW STR 14R AND STR 16R ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER PRI 596721-14 REV.0 AND ERA 596721-14 REV. ORIGINAL. (2112907)SDR DALA2022020700767None · noneSHIP 3247 DENT EXTERNAL SKIN LOCATED FR4 AT LEVEL -Y675 ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER ERA 596749-14 REV, ORIGINAL. (2112891)SDR DALA2022020700766None · noneSHIP 3247 DENT EXTERNAL SKIN LOC.AT FRAME 74 BTW STR 19 AND STR 20 ON UPPER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER PRI 596720-14REV.0 AND ERA 596720-14 REV. ORIGINAL. (2112888)SDR DALA2022020700751None · none(LOG 2112317) DURING INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN ATTACH FASTENER 3 INCHES FWD STA 500I AT STR 25L. COMPLIED WITH ENGINEERING REPAIR INSTRUCTIONS 597141-14. INSTALLED REPAIR PARTS -1, -2 AND -3 IAW B737-900ER SRM 53-00-01-2R PROCEDURE 1 SSDR DALA2022020800838None · noneSHIP 3407 SUSTAINED IMPACT DAMAGE UNDER THE 2L DOOR WHILE ON THE LINE IN CDG. THE FUSELAGE SKIN IS DENTED AND GOUGED JUST FWD OF FR37 AND BELOW STR 27L. THE DAMAGED SKIN AREA IS APPROX. 3.5" LONG AND 1.5" HIGH. THE MAXIMUM DEPTH OF DAMAGE IS 0.078". STR 27L ISSDR REXA2022031000374Floorbeam · corrodedLBL27 FLOOR BEAM IS CORRODED BETWEEN F.S. 985 TO F.S. 1000. - COMPLIED WITH REPAIR OF LBL27 FLOOR BEAM IAW CRJ900 SRM 53-00-41-201-001-A03 PERFORMED EDDY CURRENT ON FLOOR BEAM IAW CRJ900 SRM 53-00-41-201-001 A03 STEP 5B3 REMOVED AND INSTALLED SEAT TRACK IAW CSDR IPXA2022022479357None · noneINSPECTION TYPE:CAFT CARGO COMPT FLOOR PNL 152LG DAMAGE BROKENREPAIR IAW SREO A300-5320-42722-FSDR IPXA2022022079193Floor Panel · noneINSPECTION TYPE:SEGFWD CARGO COMPT. FLOOR PANEL 132SG DAMAGE/BROKENREPAIR IAW SREO A300-5320-42722-FSDR DALA2022021500945None · noneWHILE PERFORMING INSPECTION OF APU ENCLOSURE FWD SKIN ASSY. STA 1064 FOUND -2 REPAIR DOUBLER TO BE MISSING UPPER RH FASTENER PER ERA 540237-14 REV. O FIG. 2. SUMMARY SEE NRC 007-0001:21-0553-8- 7617/001 00320: REPAIRED PER ERA 540237-14 AND UPDATED LOG 2167684SDR DALA2022020700752None · none(LOG 2112864) DURING INSPECTION FOUND LH FWD FUSELAGE BETWEEN STA 360 AND STA 380 AND BETWEEN S-17L AND S-18L FUSELAGE DENTED. MAINTNENACE REPAIRED DENT PER ERA 597051-14.SDR MASA20220204107None · noneSERVICE BULLETIN 670-BA-53-057 WAS BEING CARRIED OUT WHEN DRAIN HOLES WERE INCORRECTLY DRILLED AFT OF THE CORRECT LOCATION PER THE SERVICE BULLETIN (SEE FIGURE 1 SHEET). PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) . 53-21-01-001-002-A01,SDR SWAA2022031067071Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN BST 380 TO BST 400 APPROX LBL 1.0 AT PASSENGER CABIN 2022-55725 / [01] TOOLS USED: TEMPERATURE CONTROLLERS P/N P3015GOES00000 S/N 112031023 DUE DATE 01 FEB 23; P/N P3015GOES00000 S/N 112820025 DUE DATE 01 FEB 23.;[02SDR SWAA2022031067070Angle · crackedCRACK ANGLE FLOOR STRUCTURE BETWEEN BST 380 TO BST 400 APPROX RBL 9.0 AT PASSENGER CABIN 2022-55726 / [01] TOOLS USED: TEMPERATURE CONTROLLERS P/N P3015GOES00000 S/N 112031023 DUE DATE 01 FEB 23; P/N P3015GOES00000 S/N 112820025 DUE DATE 01 FEB 23;[02] REPLACESDR SWAA2022031067072Angle · crackedCRACK ANGLE FLOOR STRUCTURE BETWEEN BST 380 TO ST 400 APPROX RBL 40 AT PASSENGER CABIN 2022-55727 / [01] TOOLS USED: TEMPERATURE CONTROLLERS P/N P3015GOES00000 S/N 112031023 DUE DATE 01 FEB 22; P/N P3015GOES00000 S/N 112820025 DUE DATE 01 FEB 22;[02] REPLACED SDR SWAA2022022367099Skin · corrodedCORROSION ON FUSELAGE EXTERNAL SKIN AT BS 1088 AND S-24L / [01] REMOVED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA TO FOM PER AMM 51-21-11ICKNESS 0.080' [REF SRM 53-80-01-0I-1 FIG 9;12] REMAINING 0.076'. DAMAGE OUT OF LIMITS DUE TO MATERIAL REMOVAL IS NOT PSDR SWAA2022022367097Skin · corrodedCORROSION ON EXTERNAL SKIN AT BS 1085 AND S-26R FWD SIDE OF JACK POINT C. REMOVED CORROSION ON SKIN. L=3.5' X W=3.2' PER SRM 53-00-01-1A-1 PARARGRAPH 2.E. ACCOMPLISHED HFEC INSPECTION OF EXISTING HOLES AND COUNTERSINKS NO CRACK NOTED IAW 737 NDTM PART 6; 51SDR SWAA2022022367098Skin · corrodedCORROSION ON FUSELAGE EXTERNAL SKIN FWD EDGE BUTT JOINT BS1016 AND STR 21L / [01] REMOVED DECORATIVE EXTERIOR PAINT AT DISCREPANCY AREA TO FOM PER AMM 51-21-11;[10] EVALUATED DAMAGE ON FUSELAGE SKIN L=5.7'; W=2.0'; D=0.011'. ORIGINAL THICKNESS 0.071' [REF SRM SDR MASA20220204106None · noneTHE LOWER FUSELAGE SKIN PANEL (P/N: MM690-35146-005)WAS DISCOVERED WITH (2) ELONGATED HOLES NEAR FS1088.20 BETWEEN STGR21 R-STGR22R. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) BOMBARDIER REPAIR ENGINEERING ORDER (REO) 690-53-61-877 (SDR MASA20220204105None · dentedLOWER FUSELAGE SKIN PANELS WERE DISCOVERED WITH SEVERAL DENTS, PREVIOUS BLEND OUTS, AND ELONGATED HOLES BETWEEN FS1088.20-55.63% REAR SPAR DATUM AND STGR21L-STGR22L, STGR21R-STGR22R. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) MESA AISDR DALA2022020400714None · noneSHIP 3261 CROWN OF FUSELAGE BETWEEN FR 44-45 AND BETWEEN STRINGER 1L & R EXTERNAL SURFACE REQUIRES CLEANING AND NDT CHECK FOR POSSIBLE CORROSION OF SCREW HOLES FOR ADF-1 ANTENNA MOUNT. CORRECTIVE ACTION: CLEANED CORROSION PER ERA. OK FOR SERVICE. (2109227)SDR HNAA2022022300110Not Reported · not reportedE901499 - LH #2 OUTBOARD FLOOR SILL CORRODED .... REMOVED AND REPLACED LH #2 OUTBOARD FLOOR SILL IAW EMB145 SRM 51-40-02. SEE TURNOVER FOR DETAILS.SDR IPXA2022022379339None · noneINSPECTION TYPE:CLOWER AFT CARGO PIT BELLY SKIN AT FS 1459 STINGER 30 BL 0 WAS CORRODED 1.5" FROM EDGE REMOVED CORROSION REMAINING MATERIAL .067" FOUND TO BE OUT OF LIMITS PER SRM 53-00-03-1A-1REPAIR PER SRM 53-00-03-2R-1 PROCEDURE 1SDR WX0A2022021674001None · noneNRC 2000-0011: 32779-02 ON EXTERNAL FUSELAGE SKIN AT FR 14 AND STGR 13 RH AREA, SUSPECTED CRACK. / EXTERNAL FUSELAGE SKIN AT FR14 AND BETWEEN Z+780 (STR14R AREA) AND Z+950 (STR15R) REPAIRED AS PER AIRBUS TD/81022810/015/2022#A AND APPROVED BY AIRBUS RDSDR DALA2022020300711None · noneSHIP 3402 LIGHTNING STRIKE ON FASTENER AT FR. 7, 7" L OF E&E DOOR OPENING. CORRECTIVE ACTION: REMOVED FASTENER. PERFORMED ET OPEN HOLE INSPECTION. NO CRACKS NOTED. INSTALLED REPLACEMENT FASTENER IAW A330 SRM 53-11-11 AND RESTORED FINISH. THIS REPAIR IS PERMANE
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