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 DALA2015102006257Access Panel · corrodedCORROSION ON SEATING AREA AND COUNTERSINK AT LT WING ACCESS PLATE NR 1363C. CORROSION ON SEATING AREA AND COUNTERSINK WAS REMOVED AND COUNTERSINK HOLES WERE MEASURED. MAX DIAMETER ALLOWABLE IS 0.532 AND MAX DIAMETER MEASURED IS 0.564, 3 ADJACENT HOLES. THEREFSDR DALA2015102006256Access Panel · corrodedCORROSION ON COUNTERSINK AT RT WING FUEL ACCESS, NR 1456C, RW, AYP, CARD 109, ZONE 00. CORROSION ON COUNTERSINK WAS REMOVED. COUNTERSINK HOLES WERE MEASURED. MAX DIAMETER ALLOWABLE IS .532" AND MAX DIAMETER MEASURED IS ".538" IN 3 ADJACENT HOLES. THEREFORE, SDR DALA2015102006253Access Panel · corrodedCORROSION ON SEATING AREA AND COUNTERSINK AT LT WING ACCESS PLATE NR 1377C, AYP, CARD 118, ZONE 00. CORROSION ON COUNTER SINK WAS REMOVED AND COUNTERSINK HOLES WERE MEASURED, MAXIMUM DIAMETER AVALIBLE IS "0.532" AND MAXIMUM DIAMETER MEASURED IS "0.544" IN, 7 SDR WVER201510190004Skin · nickedWHILE PERFORMING SB 670BA-57-020 NOTICED, 1EA HOLE AT .453" WITH A NICK AT LOWER EDGE OF HOLE ON INNER DIAMETER LOCATED AFT OF RT WING STRAP AS MARKED.SDR WVER2015101800012Skin · nickedWHILE PERFORMING SB 670BA-57-020, SHOP FLOOR FINDS 1 FASTENER HOLE ON RT WING PLANK MEASURING .453" WITH A NICK AT LOWER EDGE OF HOLE INNER DIAMETER. REPAIRED DAMAGE FASTENER HOLE IAW REO 690-57-21-204, REV.SDR DALA2015101906248Access Panel · corrodedCORROSION AT SETTLEMENT AND COUTER SKIN AREAS OF THE ACCESS PANEL 2301C, FOUND TO BE OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED.SDR SCNA20151018148Skin · damagedRT WING FIXED L/E JUST INBD OF THE NR 2 PYLON HAS MULTIPLE LOOSE AND SMOKING FASTENERS. R & R FASTENERS ON RT WING L/E INBD OF NR 2 PYLON.SDR SCNA20151018147Skin · damagedLEFT WING FIXED L/E JUST INBD OF THE NR 1 PYLON HAS MULTIPLE LOOSE AND SMOKING FASTENERS. R & R FASTENERS.SDR DALA2015111006856Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520 CT AND 620CT LT WING. FOUND OUT OF LIMITS. REPLACED PANEL.SDR DALA2015111006855Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 520FT RT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.SDR DALA2015111006854Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL 620FT. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.SDR DALA2015101606353Skin · crackedDURING C-CK, REWORK OF LOWER WING SKIN. GROUP A FASTENER HOLES. STG L 9.5/NDT, STEP 3C. HFEC. FOUND CRACK INDICATION OF HOLES 1 AND 2. REPAIRED IAW AMDS 5724-01010-03B, JOB 006-001, STEP 3D, NO FURTHER CRACK INDICATION.SDR 33AY2016FA0000072Skin · corrodedINSPECTION FOUND LT WING LOWER T/E SKIN CORRODED BETWEEN WBL 254 TO WBL 279.25 . THE CORRODED SKIN AREA WAS BLENDED AND REPAIRED IAW REPAIR PLAN 121083-R039, REV 02.SDR 7C7A20151215100Panel · damagedLADDER PLATE FOR 624CT AFT INBD SCREW HOLE IS ELONGATED AT STATION YW335, RD 8-57-7149.SDR DALA2015111006853Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREAS OF FUEL ACCESS PLANTE 620CB RT WING. FOUND OUT OF LIMITS. REPLACED FUEL ACCESS PANEL.SDR DALA2015111006852Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 520CB LT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PANEL.SDR ERKR2015122100014Skin · corrodedLEFT WING UPPER TE SKIN PANEL AT XW=670 CORRODED.SDR SWAA2015112346344Skin · crackedLEFT WING CRACKED NOTED COMMON TO WING SKIN AT TE ROW, BETWEEN RSS 213 - 295. REPAIRED SKIN IAW EA.SDR AALA20151014003Skin · corrodedLEFT WING LOWER SKIN IS CORRODED UNDER THE 540 FRAME ANGLE. REPAIRED WING SKIN IAW EA 255087.SDR FDEA201510133182Skin Panel · corrodedLEFT WING, AFTER FILL PORT REMOVAL, UPPER SKIN UPPER SURFACE FOUND CORROSION AT OVERWING FILL PORT ADAPTER MATING AREA. LT WING OVERWING FILL PORT CORROSION REPAIRED IAW EA F-5730-T0320974 P 1. REPAIR CLASSIFIED AS MINOR.SDR DALA2015111006851Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620DT RT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PLATE.SDR DALA2015111006850Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE NR 620 RT WING. FOUND OUT OF LIMITS. REPLACED ACCESS PLATE.SDR DALA2015111006849Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 520DT AT LT WING. FOUND OUT OF LIMITS. REPLACED PANEL ON AMDS 5730-0433.SDR AALA20151012011Skin · corrodedRIGHT WING OVERWING FUELING CAP CORRODED AROUND CAP FITTING AREA. REPAIRED IAW EA 254884.SDR DALA2015101306078Access Panel · damagedELONGATED HOLES ON RT WING ACCESS PANEL 1414C CUT OUT, BELOW RUBSTRIP. THE ACCESS PANEL WAS REPAIRED IAW SRM 51-22-2A, 51-30-2, AND 51-10-3 PAR 21 AND 14.SDR DALA2015101306087Access Panel · corrodedACFT HAS TOOL MARK AND CORROSION ON COUNTERSINK AT LT FUEL ACCESS NR 1355C. FUEL ACCESS NR 1355C WAS REPLACED IAW SRM 51-22-2A AND WILL BE INSTALLED UNDER CARD 2800-0120, JOB 001-0396.SDR DALA2015101206056Access Panel · corrodedCORROSION FOUND ON THE COUNTERSINK OF LT WING FUEL ACCESS PANEL 1361C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.SDR CA151014005Strap · cracked(CAN) CRACK INDICATION ON LOWER WING ASSY AREA BETWEEN REAR SPAR AND AUXILIARY SPAR WS65.75 LOCATED BETWEEN THE MLG DOOR HINGES. THE CRACK APPEARS TO BE APPROXIMATELY 1.5" LONG AS DETERMINED ON THE X-RAY.SDR SWAA2015111846182Skin · crackedLEFT WING UPPER TE SKIN RSS 240, MOST AFT OPENED FASTENER HOLE IN SKIN CRACKED. REPAIRED SKIN IAW EA.SDR SWAA2015111846181Skin · crackedLEFT WING UPPER TE SKIN RSS. 266, MOST AFT OPENED FASTENER HOLE IN SKIN CRACKED. REPAIRED SKIN IAW EA.SDR DALA2015101206060Door · crackedA CRACKED WAS FOUND ON THE SLAT TRACK DOOR NR 7R. THE SLAT TRACK DOOR WAS REPLACED IAW ERA: 512356-14 MA, REV: ORIG, LP2172495.SDR DALA2015101006040Access Panel · corrodedAICORROSION ON REPAIR BUSHINGS, COUNTERSINK AND SETTLEMENT AREA AT RT WING FUEL ACCESS NR 1410C. ACCESS DOOR 1410C WAS REPLACED.SDR DALA2015101006039Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF RT WING ACCESS PANEL 1436C. THE ACCESS PANEL WAS REPLACED.SDR SWAA2015112346305Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR, CHORD CRACKED AT RSS 164. REPAIRED SKIN IAW EA.SDR SWAA2015112346316Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 265. REPAIRED SKIN IAW EA.SDR SWAA2015112346315Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 263. REPAIRED SKIN IAW EA.SDR SWAA2015112346314Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 262. REPAIRED SKIN IAW EA.SDR SWAA2015112346313Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 255. REPAIRED SKIN IAW EA.SDR SWAA2015112346312Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 254. REPAIRED SKIN IAW EA.SDR SWAA2015112346311Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 225. REPAIRED SKIN IAW EA.SDR SWAA2015112346310Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 224.5. REPAIRED SKIN IAW EA.SDR SWAA2015112346309Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 224. REPAIRED SKIN IAW EA.SDR SWAA2015112346308Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 223. REPAIRED SKIN IAW EA.SDR SWAA2015112346307Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 221. REPAIRED SKIN IAW EA.SDR SWAA2015112346306Skin · crackedRIGHT WING UPPER SKIN AT AFT SPAR CHORD, CRACKED AT RSS 220. REPAIRED SKIN IAW EA.SDR DXTR2015110901Skin · dentedBIRD STRIKE DENT ON RT WING L/E AT WS 183. REPAIRED RT WING L/E PANEL IAW AQRD ENGINEERING REPAIR ORDER ERO-798861 AND SRM 51-00-03 AND NDI MANUAL. NO DEFECTS NOTED.SDR FDEA201510073101Skin · crackedDURING HFEC OPEN HOLE INSPECTION CARRIED OUT ON RT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUT OUT, FOUND FOUR EACH, NR 6, 9, 10 & 35 HOLES WITH CRACK INDICATION. NEW REPAIR BUSHINGS FABRICATED & INSTALLED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. REPAISDR FDEA201510073100Skin · crackedDURING HFEC OPEN HOLE INSPECTION CARRIED OUT ON LT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUT OUT, FOUND ONE NR 35 HOLE WITH CRACK INDICATION. REPAIR BUSHING FABRICATED & INSTALLED IAW SRM 57-20-02-2R FIG 201 REPAIR 5. REPAIR CLASSIFIED AS MAJOR IASDR CA151008001Skin · cracked(CAN) DURING PRE-FLIGHT THE PILOTS MOVED THE FLIGHT CONTROLS THROUGH THE FULL RANGE OF MOTIONS AND FOUND THE LH ROLL SPOILER BINDING. MAINTENANCE FOUND A CRACKED EDGING IN THE LT OUTBOARD SPOILER FLAP WELL AT WING STATION 3400 (MM). THE CRACK ON THE EDGING CAUSDR SWAA2015111846160Skin · crackedLEFT WING UPPER SKIN, 3RD FROM AFT FASTENER ROW HOLE AT APPROX RSS 168 CRACKED. REPAIRED SKIN IAW SRM & EA.
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