JASC 5730
Service difficulty reports · 27,262
Reports filed under 5730 · Wing, 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 = '5730' 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 = '5730' 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 AALA202204197731Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING UPPER SKIN PANEL #2 TRAILING EDGE AT WS 5512 AFT OF STRINGER 17. REPAIRED SKIN PANEL PER EA 334281 AND SRM 51-42-00.SDR AALA202204132031Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE SKIN LOWER SURFACE AT WS 8268 AFT OF STRINGER 17. REPAIRED SKIN PER EA 334281.SDR AALA202204134146Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE SKIN LOWER SURFACE AT WS 8744 AFT OF STRINGER 17. REPAIRED SKIN PER EA 334281SDR AALA202204139914Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING UPPER SKIN AT WS 7792 AND AFT OF STRINGER 17. REPAIRED SKIN PER EA 334281.SDR SWAA2022040882682Access Panel · delaminatedR/W T/E ACCESS PANEL 661BB INNER SURFACE CRACKED / [01] CLEANED DAMAGE AREA FOR REPAIR ON ACCESS PANEL #661BB LOWER SKIN AS PER B737 SRM 51-70-05-2R-3;[02] PERFORMED DRY OUT ON DAMAGE AREA ON R/W T/E ACCESS PANEL 661BB ;FOUND NO WATER AS PER B737 SRM 51-70-05-SDR DALA2022031501705None · noneSHIP 6819 AWR: AD, A.A: LOOSE FASTENERS NBR 1,2,3,4,6,7,8,9, AND 10 OF RH DRAG FITTING. CORRECTIVE ACTION: SUMMARY OF NRC 00205: HOLES WERE REPAIRED PER ER/A 592314-14AD REV. A. SECTION V: PERMANENT REPAIR, PRI 592314-14 REV. 1 AND ETI-57-22-017 REV 1.PER ER/ASDR FDEA202203091293Skin · damagedREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX XORS 799, SLAT TRACK #14 CUT OUT HAS EXISTING REPAIR DOUBLER DOT. 54 0000356511 : LOGAN, DAVID D - 24-MAY-2022 17:58 EXISTING MAJOR REPAIR WAS PREVIOUSLY INSTALLED PER SRM 57-40-02 REPAIR 7, FIG. 201. REF. E.SDR SIMA20220309004Spar · crackedRIGHT WINGLET IS CRACKED ON THE FWD SPAR RADIUS.-C/A-COMPLETE:INSTALLED SERVICEABLE RH WINLET IAW AMM 57-30-00. REF NRTC:E910621SDR SIMA20220309003Spar · crackedLEFT WINGLET IS CRACKED ON THE FWD SPAR RADIUS.-C/A-COMPLETE:REF BOW360562 FOR REPAIR OF LH WINGLET FWD SPAR. INSTALLED SERVICEABLE LH WINLET IAW AMM 57-30-00. REF NRTC:E910621 FOR AERODYNAMIC SEALANT.SDR FDEA202203081388Doubler · unknownREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 599 HAS EXISTING BEADED DOUBLER DOT 14. REMOVED EXISTING DOUBLER AND INSTALLED NEW REPAIR DOUBLER REF. MD-11 SRM 57-40-02-2R FIG. 203 REPAIR 15.SDR FDEA202203081139Skin · crackedREPAIR ASSESSMENT: L/H FIXED WING LOWER SKIN ACCESS DOOR CUTOUT STA APROX XORS 683 - 714 HAS MULTIPLE BUSHING REPAIR DOT 24. REPAIRED PER SRM 57-20-02 FIG. 201 REP. 5SDR FDEA202203081138Skin · crackedREPAIR ASSESSMENT: R/H FIXED WING LOWER SKIN ACCESS DOOR CUTOUT STA APROX XORS 683 - 714 HAS MULTIPLE BUSHING REPAIR DOT 22. REPAIRED PER SRM 57-20-02 FIG. 201 REPAIR 5SDR FDEA202203081051Doubler · unknownREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 645 HAS EXISTING BEADED DOUBLER . EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203081042Doubler · unknownREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 568 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203081041Doubler · unknownREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 562 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR RPEVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203081040Doubler · unknownREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 562 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED P ER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203081008Doubler · unknownREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 550 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT 1 - 4.SDR FDEA202203081005Doubler · unknownREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 524 HAS EXISTING BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PERSRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203081004Skin · noneREPAIR ASSESSMENT: L/H WING FIXED L/E STA APROX. XORS 372 HAS EXISTING RAP AROUND DOUBLER ON THE CUTOUT OF TELESCOPIC DUCT. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-01-2R REPAIR 10 FIG. 201, SHT. 1 - 5.SDR FDEA202203080999Skin · unknownREPAIR ASSESSMENT: R/H WING SLAT #3 STA APROX XOS 456 HAS EXISTING REPAIR DOUBLER ON THE OUTTER LOWER SKIN. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-01-2R REPAIR 8, FIG. 201, SHT. 1 - 3 AND PREVIOUS OPERATOR LUFTHANSA TECHNIK ENGINEERINGSDR FDEA202203080997Doubler · unknownREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 603 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203080994Doubler · unknownREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 582 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57- 40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203080993Doubler · unknownREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 576 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203080952Doubler · unknownREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 570 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203080951Doubler · inoperativeREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 562 HAS EXISTIN BEADED DOUBLER. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPAIR 15, FIG. 203, SHT. 1 - 4.SDR FDEA202203080950Doubler · inoperativeREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 511 HAS EXISTING BEADED DOUBLE. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-02-2R REPIAR 15, FIG. 203, SHT. 1-4.SDR FDEA202203080946Skin · noneREPAIR ASSESSMENT: R/H WING FIXED L/E STA APROX. XORS 372 HAS EXISTING RAP AROUND DOUBLER ON THE CUTOUT OF TELESCOPIC DUCT. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 57-40-01-2R REPAIR 10, FIG. 201, SHT. 1-5.SDR DALA2022031001599None · noneSHIP 691 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 589429-14AD REV.A. CORRECTIVE ACTION: REF ERA 589429-14AD REV A. (2147851)SDR DALA2022030901535None · noneSHIP 697 A.A / A.D. CRACK WAS FOUND ON LH ENG DRAG FTG CLAMP -UP HOLE #2, ON FITTING AT 5 HRS POS. IN REF CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00169: HOLE WAS REPAIRED PER ERA 584933-14AD REV. C. SECTION V: PERMANENT REPAIR AND ETI-57-22-043 REV.7. (2145182SDR DALA2022030901534None · noneSHIP 697 [AD.AA]RH ENGINE DRAG FITTING CLAMP UP HOLES WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #12 CORROSION ON FITTING BTW 9 TO 11 CLOCK POS ; HOLE #13 CORROSION ON FITTING AT 5, 11 AND 12 CLOCK POS , GOUGE ON FITTING UPPER EDGE BTW 2 AND 3 CLOCKSDR DALA2022030901533None · noneSHIP 697 [AD.AA] RH ENGINE DRAG FITTING CLAMP UP HOLES WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #3 CORROSION ON FITTING AT 4 OCLOCK POS, HOLE #4 CORROSION ON SKIN AT 7 OCLOCK POS AND HOLE #5 CORROSION ON SKIN AT 6 OCLOCK POS. IN REF. TASK CARD. COSDR DALA2022030901532None · noneSHIP 697 A.A / A.D. CRACKS WERE FOUND ON LH ENG DRAG FTG CLAMP -UP HOLE #12, ON SKIN AT 9 HRS POS. & FITTING AT 6 HRS POS. IN REF CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00170: THE HOLES OF THE FASTENERS AT LOCATIONS HOLE #12, ON SKIN AT 9 HRS POS. AND FITTINGSDR DALA2023010500072Skin · damagedELONGATED HOLE CUT-OUT STRUCTURE BWT RIB 14 AND RIB 15 FUEL TANK ON LH WING. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-21-11-300-002. (2142880)SDR FDEA202203020395Doubler · crackedLEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 703 - 709 BEADED DOUBLER FOUND CRACK . DOUBLER AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202203020394Doubler · crackedLEFT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 752 - 758 BEADED DOUBLER FOUND CRACK . DOUBLER AREA REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202203020392Doubler · damagedLEFT WING - TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 398 FOUND DETACHED . FORWARD EDGE FINGER DOUBLER AT XW 398 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203. REPAIR CLASSIFIED AS MAJORSDR FDEA202203020391Doubler · damagedRIGHT WING - TRAILING EDGE INBOARD ISLAND UPPER FIXED PANEL LOWER SURFACE FORWARD EDGE FINGER DOUBLER AT XW 400 FOUND DETACHED . FORWARD EDGE FINGER DOUBLER AT XW 400 REPAIR CARRIED OUT AS PER SRM 57-50-01-2R REPAIR 6 FIGURE 203. REPAIR CLASSIFIED AS MAJOSDR FDEA202203020390Former · crackedRIGHT WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XOS 1026 01 EACH FORMER FOUND CRACK. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB2920 REVISION BB. REPAIR CLASSIFIED AS MAJOR PER GSDR AALA202204050676Skin Panel · damagedFOUND DAMAGE PENETRATION UNDER WING AT LOWER WINGBOX AT INTERSECTION OF RIB CENTER-LINE 2 AND RIB CENTER-LINE 5 ON LEFT WING. **SUPPLEMENTAL REPORT FOR AALA202203020676: ACCOMPLISHED PERMANENT REPAIR PER EA 334496.** (CLOSED)SDR AALA202203020676None · noneFOUND DAMAGE PENETRATION UNDER WING AT LOWER WINGBOX AT INTERSECTION OF RIB CENTER-LINE 2 AND RIB CENTER-LINE 5 ON LEFT WING. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)SDR SWAA2022030978503Skin · elongatedRIGHT WING TRAILING EDGE PANEL 651GB INBOARD FASTENER HOLES ELONGATED IN COMPOSITE SKIN. DOT 234/12. / [01] WORK ACCOMPLISHED ON NON-ROUTINE TTG8Q00B1K45 (43253/6000/0023)SDR AALA202203161133Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING UPPER SKIN TRAILING EDGE FORWARD OF THE AILERON, AT RIB 25. **SUPPLEMENTAL REPORT FOR AALA202203011133: REPAIRED SKIN PANEL PER EA 34491A** (CLOSED)SDR AALA202203011133None · noneAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING UPPER SKIN TRAILING EDGE FORWARD OF THE AILERON, AT RIB 25. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)SDR SIMA20220221007Spar · crackedRH WING TIP SPAR 1 IS CRACKED. (INSIDE 651AB)-C/A-COMPLETE:SEE NRTC E904836** ONETIME REPLACEMENT - EO-EJ-5700-004 OPS PTB DUE FOR REPLACEMENT OF RH WING TIP SPAR 1SDR SCNA20220321005None · noneDEFECT: R/H WING. L/E UPPER SKIN, I/B OF NACELLE HAS 12X SMOKING RIVETS (MARKED). RESOLUTION: REPAIRED R/H WING FIXED L/E SKIN, JUST IB OF NO.2 ENGINE PER ATSER 22-01295 REV1R AND SCA EA-57-0072 REV 00.SDR SCNA20220321004None · noneDEFECT: L/H WING, L/E UPPER SKIN, I/B OF NACELLE HAS 12X SMOKING RIVETS (MARKED). RESOLUTION: REPAIRED L/H WING, L/E UPPER SKIN, I/B OF NACELLE IAW ER 22-01301 REV 1R. COMPLIED WITH SLA EA 57-0073 REV 00.SDR DALA2022022201160None · noneSHIP 5801 AFTER RH ENG DRAG FTG CLAMP-UP HOLES INSPECTION, FOLLOWING DAMAGES WERE FOUND: HOLE #12 NICK ON SKIN AT 2 CLOCK POS. HOLE #13 CORROSION ON SKIN AND FITTING BTW 3 - 4 CLOCK POS. IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00138: HOLE #13 AND HSDR SWAA2022040475371Panel · corrodedRT WING FUELING STATION P-15 PANEL HAS CORROSION AROUND CTR & I/B GAUGES. 124-007. REMOVED P-15 REFUEL PANEL. REF AMM TASK 28-41-61-000-801. VERIFIED STEP 1. REPLACED P-15 REFUEL PANEL BRACKET ASSEMBLY. REF. BSWPM 20-83-11 & 20-84-20. VERIFIED STEP 3<BR>SDR DALA2022022201158None · none'SUPPLEMENTAL INFORMATION' SHIP 5801 AFTER LH ENG DRAG FTG CLAMP-UP HOLES INSPECTION, FOLLOWING DAMAGES WERE FOUND: HOLE #1 SCRATCH ON SKIN AT 5 CLOCK POS.; HOLE #2 SCRATCH ON SKIN AT 1 CLOCK POS; HOLE #6 NICK ON FITTING AT 6 CLOCK POS; HOLE #7 SCRATCHES ON SKSDR DALA2022022201159None · noneSHIP 5801 RH ENG DRAG FTG CLAMP-UP HOLES WERE INSPECTED AND FOLLOWING DAMAGES WERE FOUND: HOLE #2 CORROSION ON SKIN AND FITTING BTW 2 - 4 CLOCK POS. HOLE #5 SCRATCH ON SKIN AND FITTING AT 5 CLOCK POS, ALSO GOUGE ON FITTING AT 5 CLOCK POS. IN REF TASK-CARD. COR
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