JASC 5730
Service difficulty reports · 27,269
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 UPS04443319Plate · crackedINSPECTION TYPE:C, RIGHT BS 1241 WL 180 UPPER WING SPLICE PLATE NR 5 FASTENER HOLE CORROSION CRACK REVEALED AT WING UPPER SKIN LAYER. RIGHT BS 1241 UPPER WING SPLICE PLATE NR 5 FASTENER HOLE AT UPPER SKIN LAYER REWORKED AS PER EO B747-5740-17032.SDR CA040930002Skin · cracked(CAN) DURING INSPECTION, CRACKS WERE DISCOVERED AT THE IB END OF THE LT AND RT UPPER OB WING SKINS WHERE THEY UNDERLAP THE FUEL TANK BAY COVERS. THE CRACKS ARE LOCATED IN THE RADIUS OF CUTOUT AREAS IN THE SKINS WHERE THE STINGERS JOIN AT WING STATION 150.0. TSDR GTIA040838Skin · chafedLT WING L/E CHAFED ON EXTERNAL SURFACE AT STA XRS 240, XRS 164, XRS 137. BLENDED OUT CHAFED AREAS IAW SRM 57-01, FIG 1, MATERIAL LOSS AT XRS 137 AND 240 OUT OF LIMITS, FABRICATED 2EA REPAIR DOUBLERS FROM 7075-T6-.063, LOCATED DRILLED REPAIR DOUBLERS, TREATED,SDR DHL2004801551Skin · damagedCRT L/E HAS INTERIM REPAIR AT XFS 347.750 RT (LWR PART). PERFORMED MAJOR REPAIR IAW DWG W51-R09, FAA FORM 8110-3 DATED 09-28-2004. REMOVED INTERIM REPAIR IAW DWG W51-R09. CUT OUT DAMAGED SECTION IAW DWG W51-R09. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-1SDR ASAA0480525Skin · chafedOKC - C-CHECK, LT WING L/E UPPER SURFACE CHAFED 25 INCHES OB OF L/E SLAT NR 0, OB TRACK REMOVED DAMAGE. HFEC, NO CRACKS NOTED, TREATED AND PRIMED IAW EA 5740-01411 AND EA 10592.SDR ARWA20040906Skin · crackedDURING A "C" CHECK INSPECTION, THE FOLLOWING WAS FOUND, RT WING INBOARD L/E LOWER SECTION STA XCW 69 OUTER PLATING AND INNER DOUBLER WITH 3 INCH CRACK.SDR CALA0400652Skin · debondedINSPECTION FOUND LT WING UPPER SURFACE FIXED L/E FAIRING SKIN DEBONDED AT WS 400 (JUST AFT OF NR 4 SLAT). REPAIRED IAW EA 5731-01010, REV D.SDR COMA0460544Skin · crackedCRACK FOUND ON LEFT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130.SDR COMA0460543Skin · crackedCRACK FOUND ON RIGHT WING PLANK. REPAIRED IAW CRJ REO 601R-57-21-130.SDR 04FDEA02835Panel · damagedPANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1.SDR 04FDEA02834Panel · damagedPANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998.SDR 04FDEA02833Panel · damagedPANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998SDR 04FDEA02819Panel · delaminatedPANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL BY FABRICATING AND BONDING NEW INNER SKIN, OUTERSKIN, DOUBLER AND CORE IAW DC10 DRAWING ARC0264 AND EA8-5710-77620.SDR CALA0400647Skin · crackedINSPECTION FOUND A 6 INCH CRACK IN LT WING LEADING EDGE SKIN. THE SKIN WAS REPAIRED IAW EA 5731-01010.SDR 04FDEA02823Panel · delaminatedPANEL 641CR HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77617. REFERENCE NON ROUTINE N00169.SDR 04FDEA02829Panel · delaminatedPANEL 541CR HAS MANY AREA OF DELAMINATION. REPAIRED PANEL 541CR BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2906 AND FEDEX EA 8-5710-77618. REFERENCE NON-ROUTINE N00163.SDR 04FDEA02826Panel · delaminatedRIGHT WING TRAILING EDGE PANEL 641BB DELAMINATED. REPAIRED PANEL IAW FEDEX EA 8-5710-77621, REFERENCE NON ROUTINE N00419.SDR 04FDEA02825Panel · delaminatedPANEL 636HL HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77614. REFERENCE NON ROUTINE N00323.SDR 04FDEA02824Panel · delaminatedPANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77620, REFERENCE NON ROUTINE N00125.SDR ASAA0480507Skin · gougedOKC - C-CHECK, RT WING LOWER IB T/E SKIN GOUGED. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-10-4, 57-22-3.SDR EIA2004110Fairing · corrodedLT WING LEADING EDGE WING ROOT ALUMINUM NOSE CAP (D-FAIRING) AT LALDG LIGHT LWR AREA FOUND CORROSION. CORROSION REMOVED, HFEC INSP TO INSURE CORROSION CRACK FREE. APPLIED FINISH PER BOEING MESSAGE NR I-OYSCJ, I-OW4AE, TEC-XMN-04-01388C. EN EA-57-0428, REPETSDR DHL2004801540Access Door · damagedLT WING ACCESS DOOR NR 583F HOLES ELONGATED. REMOVED ACCESS DOOR NR 583F IAW DC8 SRM 51-1-21 PG 1. FABRICATED NEW ACCESS DOOR (7075T6 0.080) IAW DC8 SRM 57-2-0 PG 1. CLEANED, TREATED AND PRIMED INNER SIDE OF ACCESS DOOR IAW DC8 SRM 51-1-8B. INSTALLED NEW ASDR MWEA040172Doubler · dentedLT WING FIXED VANE HAS MANY SMALL DENTS ON LOWER SURFACE IN A 6 IN X 6 IN AREA. FABRICATED AND INSTALLED DOUBLER.SDR 2004FA0000734Panel · missingDURING A LT TURN IN A PLEASURE FLIGHT; THE TOP LT IB PANEL FLEW OFF AND THERE WAS LOSS OF LIFT IN LT WING. IN TRYING TO LAND, HAD TO MAINTAIN HIGH AIRSPEED, MADE A HARD LANDING. NOSE WHEEL BROKE OFF, PROPELLER WAS DAMAGED. MISSING PANEL IS JUST OB OF THE FUSSDR UIEA200400173Skin · corrodedDURING SCHEDULED MAINTENANCE, FOUND CORROSION ON LEFT WING TOP SKIN UPPER SURFACE AT APPROXIMATELY WBL 143, JUST FORWARD OF STRINGER 30. THE CORROSION WAS REMOVED BY BLENDING. HFEC INSPECTED THE SKIN SURFACE TO ENSURE DAMAGE AND DEFECT FREE. FLAP PEEN THE BSDR DHL2004801549Doubler · crackedLT WING TOP PANEL PLATING INNER DOUBLER 505F ACCESS DOOR CRACKED 1.500 BETWEEN XRS 8.000 AND XRS 22.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW MESSAGE BOEING NUMBER 1-NRSB2, ROD SKETCH 04-08-25-001, FAA FORM 8110-3 DATED 09-01-04. REMOVED FASTENERS FROM SDR USAA040617Panel · crackedPIT - FOUND WING PANEL CRACKED 3 INCHES, LEFT ENGINE PYLON, WING UPPER SURFACE FIXED PANEL AFT INBOARD EDGE. INSTALLED DOUBLER AND SEALED PER TYP REPAIR 54-50-14A. (M)SDR USAA040614Skin · crackedPIT - FOUND PYLON CUT OUT CRACKED APPROX 1 INCH, NR 2 ENGINE PYLON ACCESS PANEL NR 5827R AFT INBOARD CORNER. INSTALLED DOUBLER PER TYP REPAIR 54-30-07. (M)SDR UIA9316Skin · corrodedDURING C06 CHECK OF DATUM, A/C FOUND SEVERAL CORROSION ON UPPER SKIN (P/N:59305002-150) OF RT WING AT STA XRS=282.SDR IXXA060419SPanel · delaminatedDURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE DIHEDRAL PANEL DELAMINATED. REPLACED PANEL PER ALL APPLICABLE DATA.SDR USAA040601Access Panel · missingMISSING PANEL AND ADJACENT STRUCTURE DAMAGED. RT WING IB LOWER SURFACE BETWEEN T/E FLAP AND UNDERCARRIAGE BODY. FABRICATED AND INSTALLED PANEL. REPAIRED STRUCTURE.SDR COMA0460520Skin · crackedRT WING PLANK AT VS 148 IS CRACKED. IAW EO 57-020.SDR DHL2004363533Skin · crackedDURING C-CHECK, RT WING L/E UPPER SKIN 1.5 INCH CRACK JUST RIGHT UP I/B SIDE JACK SCREW NR 3. CUT OUT DAMAGE SECTION OF L/E SKIN AT RT WING. PERFORMED HFEC OF CUTOUT AREA, NO DISCREPANCIES NOTED. INSTALLED DOUBLER AND FILLERS AS REQUIRED TO RT WING L/E UPPESDR UPS04243173Access Panel · delaminatedINSPECTION TYPE:C, RIGHT WING ACCESS PANEL NR 8640 DELAM ALONG EDGE AND SUSPECT CRACK ON LWR SURFACE. DAMAGED AREA CUT OUT AND REPAIRED IAW SRM 51-40-20.SDR UPS04243172Panel · delaminatedINSPECTION TYPE:C, RIGHT WING UPPER SURFACE T/E PANEL DELAM ON UPPER SURFACE AT I/B AFT CORNER. PANEL REPLACED IAW MM 20-80-01.SDR P5CA0401200Skin · corrodedLEFT WING UPPER SKIN 24 INCHES FWD OF SPAN WISE BEAM NR 2 HAS CORROSION. REMOVED CORROSION, TREATED & PRIMED.SDR P5CA0401196Skin · corrodedRIGHT UPPER WING SKIN HAS CORROSION ALONG FWD OF MID SPAR. BLENDED OUT CORROSION, TREATED & PRIMED.SDR GAIA04139Skin · crackedDURING C-CHECK INSPECTION FOUND LT WING L/E CAVITY WS110-130 FWD. SKIN BUCKLED AND CRACKED. REF FASI NR 86706, STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 12.SDR GAIA04141Skin · crackedDURING C-CHECK INSPECTION FOUND LT WING UPPER L/E SKIN NR 3 SLAT HOOK CUT OUT CRACKED. REF FASI N/R ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-30-4.SDR GAIA04140Skin · crackedDURING C-CHECK INSPECTION, FOUND LT WING L/E SKIN WS549 CRACKED. REF FASI NR 86708 STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-30-4.SDR UPS04243218Skin · corrodedINSPECTION TYPE: C, AREA OF LITE SURFACE CORROSION AROUND FASTENER HEADS ON HORIZ FLANGE OF RT WING UPPER SPLICE PLATE AT BS 850. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-02. HFEC CARRIED OUT IN ABOVE AREA IAW B727 NDTM 51-00-00 PTSDR COOSDR040039Panel · corrodedLT WING, INNER WING T/E UPPER PANEL WITH HEAVY CORROSION.SDR UPS04243213Stringer · corrodedINSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN AT STR 10C RBL 65 BS 810. CLEANED CORROSION IAW SRM 51-10-01. HFEC CARRIED OUT IAW B727-NDTM -5 1-00-00 PT6 FIG 4, NO DEFECTS FOUND. FLAP PEENING CARRIED OUT IAW SOP M 20-10-03. AREAS REPROTECSDR UPS04243212Skin · corrodedINSPECTION TYPE: C, CORROSION ON WING CENTER SECTION UPPER SKIN BETWEEN STR 12-13C RBL 65 BS 795 IN THE AREA INTERFACING WITH Y FLANGE FITTING. CORROSION REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT ON BLENDED AREA IAW B727 NDTM 51-00-00PT6 FIG 4, NO DEFECTS FSDR UPS04243206Panel · delaminatedINSPECTION TYPE:C DELAM ON RT WING T/E PANEL LOWER SURFACE OF WING BELOW NR 13 SPOILER. REPAIRED DELAM ON PANEL IAW SRM 51-40-20.SDR MWEA040158Panel · corrodedLEFT WING UPPER SURFACE PANEL 1325C HAS INTERGRANUALAR CORROSION AROUND SEVERAL FASTENERS. FABRICATED AND INSTALLED PANEL.SDR MWEA040157Panel · corrodedRIGHT WING TOP PANEL NR 1428 HAS INTERGRANULAR CORROSION AROUND ONE FASTENER. FABRICATED AND INSTALLED PANEL.SDR DHL2004801530Skin · delaminatedRT WING T/E PANEL INTERNAL SKIN DELAMINATED, XW 97.000 TO XRS 162.000 (LWR). REMOVED DELAMINATED RT WING T/E LWR PANEL (XW 97.000 - XRS 162.000) IAW DC8 SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED NEW RT WING T/E LWR PANSDR DHL2004801525Panel · delaminatedLT WING T/E LOWER PANEL INTERNAL SKIN DELAMINATED (STA. XW 5.000 - 97.000). REMOVED DELAMINATED LT WING T/E LOWER PANEL (XW 5.000 - 97.000) IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW LT WING T/E LOWER PANEL IAW SRM 51-SDR P5CA0401193Skin · corrodedRIGHT WING UPPER SKIN HAS SURFACE CORROSION. REMOVED LITE CORROSION, TREATED & PRIMED.
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