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 KO0R201611150083Skin · crackedCRACK INDICATIONS FOUND ON OUTER WING LOWER SKIN INBD ACCESS PANEL CUTOUT RIGHT WING (636AB) XORS 696.730 STRINGER 36SDR SCNA20161114300Skin · damagedDURING WALK AROUND, FOUND TWO FASTENERS PULLED THRU LEADING EDGE SKIN ON RIGHT WING 7 FT OTBD OF WING ROOT. ACCOMPLISHED REPAIR.SDR DALA2016111508810Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL COUNTERSINK ON THE RT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.SDR DALA2016111508809Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL ON COUNTERSINK 520DT ON LT WING. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.SDR DALA2016111508808Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL ON SETTLEMENT AREA AND COUNTERSINK 520 CT AT RT WING. THE ACCESS PANEL REPLACED IAW SRM 57-10-01.SDR FDEA201611134009Skin · crackedLEFT WING FIXED LEADING EDGE UPPER INTERIOR SKIN CRACKED. REPAIRED IAW SRM 57-10-00 FIG 71 PAGE 222 VOL1.SDR FDEA201611134008Skin · crackedLEFT WING FIXED LEADING EDGE INT UPPER SKIN CRACKED. SEVERAL CRACKS BEYOND PREVIOUS STOP DRILLS. REPAIRED IAW SRM 57-10-00 FIG.71 PAGE 222 VOL 1.SDR REXA2016111202309Access Panel · chafedACCESS PANEL 584EB IS CHAFED ALONG THE L/E AT THE CUTOUT. LOCATED HOLES IN NEW ACCESS PANEL IAW SRM 51-40-11-001-001-A01.SDR DALA2016111308749Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF SECOND ACCESS NR 1303C AND 1307C AT LT WING. CORROSION ON SETTLEMENT AREA OF SECONDARY ACCESS NR 1307C WAS REPAIRED PER ER/A 551683-14AD REV. ORIGINAL AND CORROSION ON SETTLEMENT AREA OF SECONDARY ACCESS NR 1303C WAS REPAIRED PESDR FDEA201611113959Doubler · crackedRIGHT WING LEADING EDGE BEADED DOUBLER CRACKED AT XOS 589. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611113958Doubler · crackedRIGHT WING LEADING EDGE BEADED DOUBLER CRACKED XOS 734. REPAIRED IAW SRM 57-40- 02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR SWAA2016111409684Skin · damagedLT WING FIXED LEADING EDGE SKIN DAMAGED BETWEEN NR 2 AND NR 3 RIB AT APPROXIMATELY STA 180. REPAIRED SKIN IAW EA.SDR JRAA2017081100446Skin · corrodedDURING A C1 CHECK, FOUND THE LEFT WING UPPER SURFACE WAS CORRODED ON REAR SPAR BETWEEN WS 150 - 205. CORROSION WAS BLENDED OUT BEYOND SRM LIMIT. REPAIRED IAW DOCUMENT ROO3 REV 01.SDR FDEA201611103946Skin · corrodedRT WING UPPER SKIN AT STRINGER 13, XORS 264, SHOWS CORROSION. REMOVED CORROSION IAW EA 8-5730-T0329998.SDR FDEA201611103943Skin · corrodedRT WING UPPER SURFACE, AT STRINGER 16, XORS 264, 2 FASTENERS SHOW CORROSION. CORROSION REMOVED IAW EA 8-5730-T032-9998.SDR FDEA201611103942Skin · corrodedRIGHT WING UPPER SURFACE, STRINGER 17, XORS 264, PREVIOUS REPAIR HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 57-10-00 FIG 59 VOL 1.SDR FDEA201611093917Doubler · crackedLEFT WING LEADING EDGE CAVITY WITH BEADED DOUBLER CRACKED AT XOS 734. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611093916Doubler · crackedLEFT WING LEADING EDGE CAVITY BEADED DOUBLER CRACKED AT XOS 636. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR DALA2016111008429Skin · corrodedCORROSION ON RT LOWER ACCESS PANEL CUT OUT WING LWR SKIN BETWEEN XRS =189.0 TO 214.0 . REPAIRED IAW ERA NO.551715-14AD REV. ORIGINAL AND ETI-88-16-419 REV. 2.SDR REXA2016110802236Skin · chafedSKIN PANEL 684GB IS CHAFED. INSTALLED A NEW PANEL IAW SRM 51-40-11-001-001-A01.SDR REXA2016110802232Skin Panel · chafedSKIN PANEL 684EB IS CHAFED. LOCATED & DRILLED IAW SRM 51-40-11-001-001-A01.
"SDR DALA2016110908365Access Panel · crackedRIGHT WING FUEL ACCESS PANEL 620MB FOUND CRACKED. THE ACCESS PANEL WAS REPLACED, NO LEAK WAS FOUND.SDR DALA2016110708301Access Panel · corrodedCORROSION ON SETTLEMENT AREA ON FWD FUEL BOOST PUMP SECONDARY ACCESS COVER NR 1410 AT RT WING. DUE TO EXCESSIVE CORROSION DAMAGE ACCESS COVER NR 1410 WAS REPLACED IN ACCORDING ERA 530866-14MA REV ORIGINAL.SDR DALA2016110508304Access Panel · corrodedCORROSION ON CENTER TANK FUEL ACCESS PANEL 141AL. THE CORROSION WAS REMOVED AND FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.SDR DALA2016110508303Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 620AT RT WING. THE CORROSION WAS REMOVED. FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-10-01.SDR DALA2016110508286Skin · corrodedCORROSION ON INTERNAL FASTENER HOLES (9) LWR ACCESS DOOR CUTOUT BTW XRS=189 TO 214, STR 12 AND 15 AT LT WING. THE REPAIR WAS PERFORMED PER ER/A 550361-14AD REV ORIG AND ETI- 88-16-389 REV 1.SDR DALA2016110508284Skin · corrodedCORROSION ON INTERNAL HOLES (8) LWR ACCESS DOOR CUTOUT BTW XRS=189 TO 214, STRINGER 12 AND 15 AT RT WING. REPAIR WAS PERFORMED PER ER/A 550361-14AD REV ORIG.SDR DXTR2016110401Skin · dentedLT WING LOWER LEADING EDGE SKIN HAS A 5" LONG DENT CENTERED AT APPROXIMATELY WS 139.07. ACCOMPLISHED REPAIR IAW REPORT S-560-0685/04RD.SDR DALA2016110408255Skin · corrodedCORROSION ON LT LOWER ACCESS DOOR CUT OUT WING LOWER SKIN BETWEEN XRS =189.0 TO 214.0 . REPAIRED IAW ERA NO.551715-14AD REV. ORIGINAL AND ETI-88-16-419 REV. 2.SDR SWAA2016111409621Skin Panel · crackedRT WING FIXED TRAILING EDGE SKIN PANEL CRACKED ON RSS 270. R&R PLATE IAW SRM AND DWG.SDR FDEA201611013780Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT CORNER NR 13 SLAT TRACK. NR 10 CUTOUT, AFT INBOARD CORNER FOUND CRACKED APPROXIMATELY 1/4 INCH LENGTH AT XOS 659. REPAIRED IAW SRM 57-10-00 FIGURE 68 (SHESDR DALA2016110208133Access Door · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NBR 1307C. ACCESS DOOR 1307C WAS REPLACED PER SRM 51-22-2A PAR 6 TABLE 1.SDR FDEA201610303755Skin · crackedFOUND CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION ON RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201610303754Skin · crackedFOUND CRACK INDICATION DURING HFEC INSPECTION ON LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS 683.4 AND XORS 713.6.6. REPAIRED IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR DALA2016103108070Access Panel · corrodedCORROSION ON FUEL TANK ACCESS NR 1454C, 1409C AND 1311C AT LT/RT WING. FUEL TANK ACCESS NR 1409C, 1454C AND 1311C AT LT/RT WING WAS REPLACED PER SRM 51-22-2A.SDR DALA2016103108004Panel · looseDURING INSPECTION FOUND UPPER FIXED T/E PANEL IS LOOSE AFT OF NR 2 PYLON. MAINTENANCE REPAIRED PER ERA 534870-14MA.SDR ASAA2016102918676Skin · chafedLT WING I/B EXHAUST GATE O/B UPPER CORNER SKIN IS CHAFED. GROUNDED - YES. REMOVED DAMAGE FROM UPPER SKIN REMAINING MAT. FOUND TO BE .0605, RESTORED FINISH IAW SRM 57-53-01-0G-0. REQUIRES A DETAILED VISUAL INSPECTION OF AREA AT EVERY 3000 FLT CYCLES OR EVERY 12SDR SWIA201642821Panel · chafedCHAFE ON PANEL 584EB. REPLACED THE PANEL IAW SRM.SDR SWAA2016111609752Skin · crackedRT WING FLAP TRACK FAIRING 644BB INTERNAL AREA SKIN CRACKED. REPAIRED SKIN IAW EA.SDR FDEA201610283734Doubler · crackedLT WING LEADING EDGE CAVITY AT XOS 621 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201610283733Doubler · crackedRT WING FIXED LEADING EDGE CAVITY AT XOS 778 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201610283732Doubler · crackedRT WING FIXED LEADING EDGE CAVITY AT STA XOS 651 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS A MAJOR IAW GMM 6-2-100.SDR FDEA201610283731Doubler · crackedRT WING FIXED LEADING EDGE CAVITY AT XOS 699 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS A MAJOR IAW GMM 6-2-100.SDR FDEA201610283730Doubler · crackedLT WING FIXED LEADING EDGE CAVITY AT XOS 654 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. CLASSIFIED AS A MAJOR IAW GMM 6-2-100.SDR SWAA2016110309358Skin · delaminatedRT WING LEADING EDGE FRONT SPAR UPPER SKIN DELAMINATED AT STA 522. REPAIRED SKIN PER SRM.SDR 2016FA0000541Skin · crackedAT PHASE INSPECTION , FOUND ONE 2.5 INCH CRACK, 8 INCHES FROM AFT LOWER INBOARD EDGE AND ONE 1.5 INCH CRACK IN LOWER FORWARD AREA OF THE LEFT OUTER WING LEADING EDGE SKIN,1 INCH CRACK IN 000-110133-21 STIFFENER RIB, AND 000-110133-9 CLIP LOOSE AT THREADED MOUNSDR 2016FA0000540Skin · crackedAT PHASE INSPECTION , FOUND FOUR INCH CRACK IN LOWER FORWARD AREA OF THE LEFT OUTER WING LEADING EDGE SKIN,1 INCH CRACK.SDR DALA2016102507622Access Panel · damagedLEFT WING L/E ACCESS PANEL 511FB FOUND PUNCHED. REPAIRED IAW ERA 551280-14 AND SRM 51-70-17.SDR DALA2016102507540Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE NBR 1367C. ACCESS PANEL WAS REPLACED PER IPC 57-30-00 AND MAGNETIC DRIPLESS FUEL MEASURING STICK WAS INSTALLED PER AMM 28-40-02.SDR DALA2016102507539Access Door · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS PLATE NR 1303C. FUEL ACCESS DOOR 1303C WAS REPLACED.
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