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 GTIA2016090801589Skin · corrodedDURING INSPECTION, FOUND CORROSION ON THE LEFT WING TOP SKIN PANEL RIBS 7-8. REPAIRED IAW EO 5721-1646.SDR DALA2016090806465Access Panel · bentBENT RIGHT WING ACCESS PANEL 1476C. THE ACCESS PANEL WAS REPLACED.SDR DALA2016090906489Panel · bulgedWING PANEL FORWARD OF INBD SPOILER ON RT WING BULGING IN FLIGHT. REMOVED PANEL. INSTALLED NEW PANEL IAW DWG 5936824-508.SDR FDEA201609063202Skin · chafedLEFT WING, JUST FWD. OF INBD FLAP HINGE FITTING, LOWER WING SKIN SURFACE HAS EVIDENCE OF HEAVY CHAFING. DEPTH MEASURED 128 DEEP BEFORE REWORK USING DIAL DEPTH GAUGE MA1548. WORK COMPLETED IAW EA T-8-5730-T0328126 PT.1SDR FDEA201609063200Doubler · wornLEFT DROOPED LEADING EDGE ASSY HAS A DOUBLER WORN BEYOND LIMITS ON THE OTBD LEADING EDGE. REMOVED AND REPLACED FILLER ON PREVIOUS REPAIR AT LEADING EDGE REF SRM 51-31-01 VOL II.SDR DALA2016090706401Access Panel · damagedELONGATED HOLE ON FUEL ACCESS PLATE 520LB, SN 575. HOLE WAS REWORKED IAW SRM 57-10-01, PAR 5, CONDITION II, 3. HOLE AND COUNTERSINK WERE MEASURED WITH ID 0.3435" AND COUNTERSINK 0.613" THEREFORE WITHIN LIMITS OF REPAIR IAW SRM 57-10-01, PAR 5 CONDITION II. SDR DALA2016090606419Access Door · corrodedCORROSION ON FUEL ACCESS PLATE NR 1303C. FUEL ACCESS DOOR 1303C WAS REPLACED IAW SRM 51-22-2A CONDITION 3, PAR B AND IPC 57-30-00.SDR DALA2016090606418Access Door · corrodedCORROSION ON FUEL ACCESS PLATE NR 1409C. FUEL ACCESS DOOR 1409C WAS REPLACED IAW SRM 51-22-2A CONDITION 3, PAR B AND IPC:5730-00.SDR IPXA2016091608327Fastener · looseINSPECTION TYPE:1C, RIGHT WING UPPER SURFACE, PANELS FORWARD OF INBD SPOILER FASTENERS LOOSE. ACCOMPLISHED REPAIR IAW REO-G20257, REV IR AS REQUIRED.SDR SCNA20160904139Skin · wornWING PANEL 651EB HAS WEAR MARKS. REPAIRED THE PANEL.SDR DALA2016090406411Access Panel · corrodedAWR: CORROSION ON COUNTERSINKS AND SETTLEMENT AREA AT FUEL TANK ACCESS NR 1414C AND NR 1462C. ACCESS PLATE 1414C AND 1462C WERE CLEANED, BOTH ACCESS PLATES HAD 3 COUNTERSINKS ADJACENT OUT OF LIMITS, THEREFORE WERE REPLACED IAW SRM 51-22-2A, PAR 6, CONDITION ISDR DALA2016090506380Tip Cap · damagedL/E RT WING OTBD OF NR 5 SLAT AT WING TIP HAS SLAT, WING TIP, AND WING L/E CHAFING. CHECK LIMITS. L/E R/W OTBD NR 5 SLAT REMOVED IAW SRM 51-41-02 DUE TO GOUGE AND WAS OUT OF LIMITS .025. REMOVED ORIGINAL THICKNESS WAS .063, TAG 2721 IAW SRM 57-00-00, FIG 103SDR SWIA201642573Access Panel · chafedLEFT WING ACCESS PANEL 599BB IS CHAFED. REPLACED LT WING ACCESS PANEL 599BB IAW SRM.SDR DALA2016090206360Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA AT FUEL TANK ACCESS NR 1335C AND NR 1365C. FUEL TANK ACCESS PLATES NR 1335C AND NR 1365C WERE CLEANED, WERE FOUND OUT OF LIMITS AND WERE REPLACED.SDR DALA2016090206357Door · crackedINITIAL: CRACKED LT WING OTBD FLAP INBD BUTE DOOR MID SECTION INNER AREA. LEFT WING OTBD FLAP INBD BUTE DOOR WAS REPAIRED IAW ER/A466345-14MA, REV B.SDR IPXA2016091008086Panel · chafedINSPECTION TYPE: 1C, LEFT WING T/E PANEL 575CB INNER MATTING SURFACE CHAFED. REMOVED DAMAGE, NDT INSPECTED, AND DVI INSPECTED AREA AND APPLIED PROTECTIVE FINISHES IAW REO-G20241, REV. A.SDR FXGA201609121625Skin · crackedCRACKED WING SKIN AND FILLER WITH STA 235.5 AND WING STR 20 TO REPAIR A CRACK IN THE WING SKIN AND FILLER BETWEEN WING SKIN AND LANDING DOUBLER. PERFORM CUTOUT OF THE CRACKED SKIN AND FILLER. INSTALL EXTERNAL DOUBLER MADE FROM 7075-T6 0.125" IAW THE ACCOMPLISDR DALA2016102607674Access Panel · corrodedCORROSION ON SEATING AREA AND COUNTERSINK OF FUEL PANEL ACCESS PLATE 620DT. REPLACED PANEL.SDR DALA2016083106303Skin · corrodedCORROSION ON INTERNAL HOLES LOWER ACCESS DOOR CUTOUT STA XRS=189 TO 214 BETWEEN STR 12 AND STR 15 AT LT WING. CORROSION ON HOLES WERE REPAIRED IAW ER/A 549272-14AD, REV ORIGINAL. THIS DOCUMENT IS READY TO ENTRY AND MONITOR WILL BE WORK IAW ER /A 549272-14AD,SDR DALA2016083106302Skin · corrodedCORROSION ON INTERNAL HOLES LOWER ACCESS DOOR CUTOUT STA XRS=-189 TO 214 BETWEEN STR 12 AND STR 15 AT RT WING. CORROSION ON HOLES WAS REPAIRED IAW ER/A 549272-14AD, REV ORIGINAL. THIS DOCUMENT IS READY TO ENTRY AND MONITOR WILL BE WORKED IAW ER/ A 549272-14 SDR DALA2016083106299Access Door · corrodedINITIAL PART RACK. CORROSION ON SETTLEMENT AREA OF FUEL ACCESS DOORS 1409C AND 1303C. ACCESS PLATE NR 1409C AND 1303C: BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR, PN 3912757 DUE TO REDUCED AREA OF THE CONDUCTIVE INTERFACE. THEREFORE THSDR IPXA2016092208547Skin · chafedINSPECTION TYPE: 3C, RIGHT WING FIXED L/E SKIN IS CHAFED AT XIS. 717.66 TO 178. REPAIRED THE RT WING L/E SKIN IAW EA 011-5730-01-A6429. (MAJOR)SDR DXTA2016082906295Skin · scratchedSCRATCHES ON LEADING EDGE AND UNDERSIDE AT OUTER PORTION OF RT WING. VENT IN SAME AREA SLIGHTLY DENTED. NO EFFECT ON AIRWORTHINESS NOTED. REPAIRED SCRATCHES ON L/E AND VENT, ALL WORK ACCOMPLISHED IAW SRM.SDR IPXA2016090808012Doubler · crackedINSPECTION TYPE: 3C, LT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 629 - 633. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. MAJOR REPAIR.SDR FXGA201608291623Access Panel · crackedCRACKED ACCESS PANEL ATTACH FLANGES AT WING STA 49 AT PANEL 136 LT AND RT, AND 133 RT. TO REPAIR 5 CRACKS IN THE ATTACH FLANGES OF ACCESS PANELS. THE CRACKS IN THE ATTACH FLANGES ARE AT WING STA 41 LT AND RT AT PANELS 136 FORWARD AND AFT FLANGES AND PANEL 133SDR DALA2016083006290Skin · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BETWEEN XRS 163 - 168 ON RT WING. REPAIRED IAW ER/A 549286-14AD REV.ORIGINAL.SDR DALA2016083006289Skin · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR BETWEEN XRS 163 - 168 ON THE LT WING. REPAIRED IAW ER/A 549286-14AD REV. ORIGINAL.SDR R61A201609140535Skin · crackedRT WING LOWER SURFACE SKIN IS CRACKED AT RIB 17 AND THE END OF STRINGER 19 SEEN INTERNALLY PERFORMED TEMPORARY REPAIR OF RT WING SKIN BY CUTOUT AND DOUBLER/TRIPPLER INSTALL AT RIB 17 REF ETD2016-170-07876.SDR J7SA20160827001Screw · missingLEFT WING LEADING EDGE HAS SCREWS MISSING ON LOWER SIDE MID WING. INSTALLED 16 ATTACH SCREWS IN LT LEADING EDGE.SDR DALA2016102607673Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL PANEL 620AT. REPLACED PANEL.SDR DALA2016102607672Access Panel · corrodedCORROSION ON SEATING AREA AND COUNTERSINK OF FUEL PANEL 520 FT. FOUND OUT OF LIMITS. REPLACED PANEL.SDR IPXA2016090908047Doubler · crackedINSPECTION TYPE: 3C, RIGHT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 610 - 616. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. (MAJOR)SDR IPXA2016090908042Doubler · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 542 - 547. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. MAJOR REPAIR.SDR IPXA2016090808023Doubler · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 551 - 555. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203. MAJOR REPAIR.SDR IXXA20161117138Skin Panel · corrodedFOUND CORROSION UNDER TRAILING EDGE SKIN PANEL AT WS 432 ON TOP OF WING. REMOVED CORROSION, REPAIRED AREA IAW REA 47224REA07. AIRCRAFT GROUNDED.SDR IPXA2016082507466Skin · chafedINSPECTION TYPE: 1C, LT WING FIXED L/E SKIN CHAFED AT XDLE 330.2745. REPAIRED IAW EA O11-5710-01-A6398-IR AND EO MD11-5740-61670-A.SDR ASMF201611004Fastener · damagedDURING TRANSIT CHECK, A LIGHTNING STRIKE WAS DETECTED ON LEFT WINGLET TRAILING EDGE. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING DAMAGES IN THREE FASTENERS AND IN THE LEFT WINGLET TRAILING EDGE SKIN OF 2.2 INCHES LENSDR ASMF201610013Skin · damagedDURING TRANSIT CHECK, A LIGHTNING STRIKE WAS DETECTED ON LEFT WINGLET TRAILING EDGE. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW MM 05-51-19 DETECTING DAMAGES IN THREE FASTENERS AND IN THE LEFT WINGLET TRAILING EDGE SKIN OF 2.2” LENGTH, 0SDR DALA2016082406228Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL 620CT. REPLACED THE ACCESS PANEL. (LP# 2647779)SDR DALA2016082306169Access Panel · corrodedCORROSION ON SEATING AREA AND COUNTERSINK OF FUEL ACCESS PANEL, 620FT. REPLACED THE ACCESS PANEL.SDR DALA2016082306167Access Panel · corrodedCORROSION ON SEATING AREA AND COUNTERSINK OF FUEL ACCESS PLATE 520DT. REPLACED THE ACCESS PANEL.SDR DALA2016082306156Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE COUNTERSINKS NR 1409C, 1410C AND 1464C AT RT WING. OUT OF LIMITS DUE TO CORROSION DAMAGE EXCEEDS IAW SRM 51-22-2A, CONDITION II. THEREFORE WERE REPLACED IAW SRM 51-22-2A, CONDITION III.SDR TIMA20160822014Skin · corrodedTHE LEFT WING LEADING EDGE CENTER SECTION WAS FOUND TO HAVE CORROSION ON SKIN BETWEEN BONDED LAYERS DURING MAINTENANCE.SDR UHLA201608210436Skin · damagedMAJOR REPAIR, DURING REMOVAL OF FASTENERS FOR SB 170-57-0042 R0, THERE IS SOME TOOLING DAMAGE TO STR 24 ON SURFACE ON RT WING BETWEEN RIB 8A AND RIB 9. C/W ETD2016-170-078206.SDR FDEA201608202943Skin · cracked05 EA FASTENER HOLES, NR 6, 10, 12, 33, 34, FOUND CRACK INDICATION DURING HFEC OPEN-HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=683.4 AND STA XORS =713.6. REPAIR CARRIED OUT IAW SRM 57-20-02-2R, FIG 201, REPAIR 5. REPAIR CLASSIFSDR FDEA201608192938Doubler · crackedLT WING FIXED L/E LOWER SURFACE AT STA XOS 906 DOUBLER CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-03-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201608192937Doubler · crackedRT WING FIXED L/E LOWER SURFACE AT STA XOS 906 DOUBLER CRACKED. CARRIED OUT REPAIR IAW SRM 57-40-03-2R, FIG 201, REPAIR 1. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201608192936Doubler · crackedRT WING FIXED L/E LOWER SURFACE AT STA XOS 605 DOUBLER CRACKED. DOUBLER R & R IAW SRM 51-31-01-0G. THE NEW DOUBLER FABRICATED IAW DWG ARB2933, REV AJ. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201608192935Doubler · crackedRT WING FIXED L/E LOWER SURFACE AT STA XOS 546 DOUBLER CRACKED. CRACKED DOUBLER R & R IAW SRM 51-31-01-0G. THE NEW DOUBLER FABRICATED IAW DWG ARB2933, REV AJ. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201608182925Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 669 BEADED DOUBLER CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, FIG 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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