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 2008FA0000501Skin · damagedAIRCRAFT WAS BROUGHT IN FOR INSPECTION OF DOUBLE ROW OF RIVETS AT WING STA 209.016. RIVETS WERE FOUND SMOKING AND PAINT WAS POPPED ON THE RIVET HEADS. USED BOROSCOPE TO INSPECT RIVET BUCKTAILS. FOUND ALL OF THE RIVETS IN THE DOUBLE ROW OF THE SKIN LAP AT WSSDR 08FDEA02902Skin · dentedRIGHT WING TIP, LOWER SURFACE HAS 2 DENTS, CENTER AREA. CHECKED WING TIP LOWER SURFACE, NOTED CREASES. FOUND TO BE OUT OF LIMITS IAW DC/MD-10 SRM 51-80-01, PARA 2-C, VOL II. CUT OUT DAMAGED AREA. MATERIAL ID FOR THE DOUBLER IS 2024-T3, 0.063, PO 614988.3. SDR 08FDEA02881Skin · damagedFOUND TOOLMARK ON CENTER TANK TOP SKIN C 46, TRACK 1-2 LT REPAIR PERFROMED BY SMOOTH BLEND OUT AND NDT FOR CRACK FREE CONDITION IAW. RAS 70507169/2008 ISS.A , APPROVED BY EA 6-5710-120053SDR 08FDEA02877Skin · corrodedFOUND CORROSION ON LT TOP SKIN AT FRONT SPAR AREA BETWEEN RIB 24-28 REPAIR PERFORMD BY CORROSION REWORK , NDT FOR CRACK FREE CONDITION AND INSTALLING FIRST OVERSIZED FASTENER IAW. RAS/BAE/1007273/2008 ISS.A, APPROVED BY EA 6-5720-120110.SDR 08FDEA02863Skin · crackedLEFT WING FIXED L/E IS CRACKED AT THE INBD OF SLAT DRIVE MECHANISM ACCESS PANEL. CUT OUT CRACKED AREA AND FABRICATED A DOUBLER AND FILLER IAW SRM 57-10-00; FIG 68; VOL I. ALODINED AND PRIMED THE DOUBLER AND FILLER IAW SRM 51-21-01; VOL II; PGS 21-24. INSTALSDR 08FDEA02852Skin · crackedLEFT HAND WING NR 14 SLAT TRACK LOWER CUT OUT FOUND CRACKED. SKIN REPAIRED AS PER SRM 57-10-00, FIG 21 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA02831Skin · crackedLEFT WING TIP T/E AREA EXTERNAL SKIN IS CRACKED. REMOVED DAMAGED AREA PER DC/MD-10 SRM 57-00-01;VOL I. FABRICATED A DOUBLER REPAIR PER DC/MD-10 SRM 57-00-01; VOL I. ALODINED AND PRIMED DOUBLER REPAIR PER DC/MD-10 SRM 51-21-01; VOL II. INSTALLED DOUBLER RESDR IXX2008F00064Skin · damagedDURING ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND RSDR IXX2008F00062Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR RT WING OUTBOARD SLOT VANE LEADING EDGE AT STATION XOLDI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CSDR 08FDEA02765Skin · crackedLEFT WING FIXED L/E INTERNAL STA XFS 664 AT THE RIB, TOP STRAP IS CRACKED. REMOVED RIB TO FOM, REMOVED DOUBLER SPLICE. MATERIAL ID FOR A DOUBLER SPLICE 7075-0, 0.071, PO 620987.4 IAW DAC DWG ARB 1249; REV AA. FABRICATED A NEW DOUBLER SPLICE IAW DAC DWG 1249SDR EHA2008F00002Skin · crackedDURING A ROUTINE INSP, FOUND AND DOCUMENTED CRACKS IN THE UPPER WING SKINS AT APPROX STA 6700 TO 7100 ON BOTH THE LT AND RT WINGS. (K)SDR 08FDEA02769Skin · cracked05 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT.SDR 08FDEA02768Skin · damaged11 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT.SDR 08FDEA02736Skin · corrodedFOUND CORROSION ON UPPER SURFACE OF BOTTOM SKIN RIB 6A-7A, AFT OF REAR SPAR, LT WING. REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECT THE AREA IAW RAS/BAE/1007293/2008 ISS A, APPROVED BY EA 6-5751-120113.SDR 08FDEA02732Skin · damagedFOUND OLD DOUBLER REPAIR ON LT WING TOP SKIN, TRAILING EDGE, RIB 18-19 WITHOUT ANY OLD DOCUMENTATION. DOUBLER REPAIR RENEWED IAW RAS/BAE/1007270/2008 ISS A, APPROVED BY EA 6-5751-120109 .SDR WRL2008F00002Skin · crackedDURING 1C + 12A CHECK FOUND RT WING L/E SPLICE DOUBLER HAD CRACK AT STATION XORS 683. REPLACED DAMAGE DOUBLER IAW MD 11SRM 51-35-01 VOL LL, REV 40 COND CHECK NORMAL AND JOB COMPLETED. (K)SDR 08FDEA02695Skin Panel · corrodedFOUND CORROSION ON LT WING TOP SKIN, REAR SPAR AREA RIB 25-29 REPAIR PERFORMED BY BLEND OUT CORROSION, NDT FOR CRACK FREE IAW RAS/BAE/1007272/2008 ISS A, APPROVED BY EA 6-5720-120108.SDR 08FDEA02632Skin · crackedLT WING L/E CHORD FIXED PANEL FOUND CRACK. REPAIRED WING LOWER L/E STRINGER DOUBLER IAW SRM 57-10-00 FIG 49 VOL I.SDR 2008FA0000377Skin · crackedDURING A PREFLIGHT INSPECTION, MAINTENANCE TECH NOTED A 3.75 INCH LONG CRACK IN THE RT WING LOWER WING SKIN JUST FWD OF THE IB SECTION OF THE OB FLAP. ADDITIONALLY A SUPPORT/ ANCHOR TAB THAT ATTACHES THE LOWER WING SKIN TO THE IB MOST FLAP WELL RIB OF THE OB WSDR 08FDEA02566Skin · corrodedMAIN DECK CARGO COMPARTMENT, CORROSION FOUND ON UPPER SURFACE OF PRESSURE BOUNDARY OVERWING AT STA Y=1228, XCW= 63.5-64.5 RT. UPPER SURFACE CORROSION ON MAIN DECK CARGO COMPARTMENT AT STA Y=1228 XCW=63.5-64.5. REMOVED AS PER SRM 51-21-01 VOL II AND FOUND WSDR 08FDEA02565Skin · corrodedMAIN DECK CARGO COMPARTMENT, CORROSION FOUND ON PRESSURE BOUNDARY OVERWING UPPER SURFACE AT STA Y= 1227 TO 1228, XCW= 96-97 RT UPPER SURFACE CORROSION ON MAIN DECK CARGO COMPARTMENT AT STA Y=1227 TO STA 1228 XCW 96- 97. REMOVED AS PER SRM 51-21-01 VOL II ANDSDR 08FDEA02564Skin · corrodedMAIN DECK CARGO COMPARTMENT, CORROSION FOUND ON UPPER SURFACE OF PRESSURE BOUNDARY OVER WING AT STA 1227, XCW= 72.5 RT FASTENER AREA APPROXIMATELY 1 INCH DIAMETER. UPPER SURFACE CORROSION ON MAIN DECK CARGO COMPARTMENT AT STA 1227 XCW=72.5 FASTENER AREA. REMSDR UPS08852601Panel · corrodedLT WING PANEL CORROSION. REMOVED DAMAGED SKIN. ACCOMPLISHED STEPS 1-6 OF EO DC8-5720-29785 APPENDIX A. ACCOMPLISHED REPAIR STEPS 1-9 OF EO DC8-5720-29785-A.SDR 08FDEA02509Skin · misrepairedPREVIOUS EXTERNAL BONDED REPAIR DOUBLER LOCATED ON RT WING O/B FLAP TRAILING EDGE LOWER SKIN BETWEEN RIBS 3 AND 4 MEASURING 5.7 INCH BY 5.7 INCH REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT EXTERNAL BONDED REPAIR DOUBLER LSDR SWAA083525Skin · wornDURING SCHEDULED 6Y CHECK, FOUND RT WING LOWER SKIN WORN OUTBOARD OF PYLON AFT END. REPAIRED SKIN PER SWA EA.SDR 08FDEA02454Panel · crackedRT LOWER SIDE T/E PANEL FOWARD OF I/B AILERON HAS CRACK IN O/B EDGE SUPPORT ANGLE 1 3/4 INCH FORWARD FROM AFT EDGE. REMOVED DAMAGED PART PER REF SRM 51-30-2 PG 1-3. FABRICATED NEW PART PER DWG 65-19281-107. TREATED AND PRIMED NEW PART PER REF SRM 51-10-02. SDR UPS08B52894Skin · damagedINSPECTION TYPE-C2, DRILL START IN LOWER SKIN OF RT WING OB, L/E, NEXT TO A RIVET, FWD AND IB OF 3RD. PANEL FROM OB END CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 5 1-1-21, 51-2-0 FIG.7,SDR UPS08852895Skin · damagedINSPECTION TYPE-C2, DRILL START IN LOWER SKIN OF R/W OB, L/E, FWD OF 3RD. PANEL FROM OB END. REMOVED DAMAGE, FAB AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 57-2- 0 FIG.7 51-1-21.SDR UIE2008F00005Fairing · damagedLT IB FLAP NR 3, MOVEABLE FLAP TRACK FAIRING HAS A HOLE AT WBL 353.0 HOLE SIZE
IS 4.0 INCHES X 7.0 INCHES. PERMANENT REPAIR ACCOMPLISHED IAW B747200, SRM 51-40-09, FIG 6 SHEET 1 THRU 3, 250 DEGREES F CURE IAW SRM 51-40-12. ALSO, REFERENCE EO 4757A449. (K)SDR KCSA081291Skin · corrodedCORROSION ON RT. WING LOWER SKIN AT BOOST PUMP CUTOUT WS 538 (B)SDR 08FDEA02348Panel · crackedRIGHT WING L/E PANEL 613 AB CUTOUT FWD OUTBD FASTENER HOLE IS CRACKED. MATERIAL ID FOR THE REPAIR IS 2024-T3, 0.056, PO 609852.1 IAW A300-600 SRM 53-52-00; FIG 703. FABRICATED THE REPAIR IAW A300-600 SRM 53-52-00; FIG N703. ALODINED IAW A300-600 SRM 51-21-1SDR 08FDEA02337Skin · cracked03 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122497 PART 1. THIS REPAIR CLASSIFIED AS MISDR 08FDEA02336Skin · cracked02 EACH FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STATION XORS = 690 AND STATION XORS = 700. CARRIED OUT REPAIR AS PER EA 1-5710-122496 PART 1. THIS REPAIR CLASSIFIED AS MINSDR 08FDEA02317Skin · failedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RIGHT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN FLAP TRACK NR 5 TO RIB 11 AND 1.4 INCH FWD OF REAR SPAR MEASURING 13.6" BY 4.3". REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED ANSDR 08FDEA02316Skin · failedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 2 AND FLAP TRACK NR 3 MEASURING 6 INCH BY 5 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED AN APPROVED REPAIR ON LEFT WINSDR 08FDEA02315Skin · damagedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP BETWEEN RIB 3 AND FLAP TRACK NR 3 MEASURING 4" BY 6". REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED APPROVED REPAIR ON LEFT WING O/B FLAP SDR 08FDEA02314Skin · damagedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING O/B FLAP UPPER MAIN SKIN UNDER RUB STRIP AT FLAP TRACK NR 4 MEASURING 4 INCH BY 5.7 INCH. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT REPAIR ON LEFT WING O/B FLAP UPPESDR IXX2008F00065Skin · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND LT WING CRACKED ON LEADING EDGE UPPER SKIN AT STATION XCW 69.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION, FABRICATED DOUBLER, FILLER PLUSDR IXX2008F00029Skin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND LT WING CRACKED ON LEADING EDGE UPPER SKIN AT STATION XCW 69.500. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION, FABRICATED DOUBLER, FILLER PLUSDR 08FDEA02287Skin · misrepairedLT WING LOWER SURFACE FOUND EXISTING REPAIR ON BEAVER TAIL NOT IN COMPLIANCE WITH SRM 57-00-01 VOL I FIG 8. ACCOMPLISHED EA 8-5710-120488.SDR 08FDEA02280Doubler · corrodedRT WING MODERATE EXFOLIATION CORROSION ON LOWER BEAVER TAIL. ACCOMPLISHED EA NR 8-5710-120489.SDR IXX2008F00052Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING CENTER LEADING EDGE UPPER SKIN HAS IMPROPER REPAIR AT STATION 285.250. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO COSDR UALA2008111303354Skin · wornRT WING FIXED LEADING EDGE SKIN IS WORN. PER UA-EVA-71666 DAMAGED AREA BLENDED OUT PER SRM 57-41-01. PERMANENT REPAIR TO BE ACCOMPLISHED WITHIN 200 FLT HOURS.SDR GUUA94357061208ASkin · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING, UPPER SKIN, T/E HAD CORROSION AND DEBOND BETWEEN WS 121 THROUGH 194.85. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED AND EXTERNAL REPAIR DOUBLERSDR IXX2008F00086Skin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT STATION XW 736.000-761.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLSDR IXX2008F00039Skin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING LEADING EDGE LOWER SKIN CORRODED AT STATION XW 736.000-761.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLSDR GLB2008F00006Panel · looseENROUTE, THE PILOTS REPORTED THAT A LARGE FUEL LEAK WAS OBSERVED IN FLIGHT FROM THE LT FUEL TANK. 300 POUNDS OF FUEL LOST IN ONE HOUR OF FLIGHT. MAINTENANCE RETORQUED SCREW ON AFFECTED WING PANELS IAW MM 28-10-00. LEAK CHECK WAS GOOD. (K)SDR KCSA081279Skin · corrodedRT WING UPPER SKIN CORRODED AT WBL 148, 6" FWD OF REAR SPAR (B)SDR KCSA081277Skin · corrodedLT WING UPPER SKIN CORRODED AT AFT RABBET AREA W.S.522 (B)SDR IXX2008F00079Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LT WING INBOARD SLOT VANE LEADING EDGE AT STATION XILD 7095.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND R
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