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.

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 WSJul 15, 2008 · N613BA · Beech 300BEECHSDR 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. Jul 15, 2008 · N372FE · Doug MD1010FSDR 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 6-5710-120053Jul 15, 2008 · N742FD · Airbus A300B4622RSDR 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.Jul 15, 2008 · N742FD · Airbus A300F4622RSDR 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. INSTALJul 14, 2008 · N372FE · Doug MD1010FSDR 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.Jul 14, 2008 · N597FE · Doug MD11FSDR 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 REJul 11, 2008 · N383FE · Doug MD1010FSDR 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 RJul 9, 2008 · N721CX · Doug DC872FSDR 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 CJul 9, 2008 · N721CX · Doug DC872FSDR 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 1249Jul 8, 2008 · N372FE · Doug MD1010FSDR 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)Jul 8, 2008 · N423CA · Casa C212CCSDR 08FDEA02769Skin · cracked05 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT.Jul 8, 2008 · N601FE · Doug MD11FSDR 08FDEA02768Skin · damaged11 FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT.Jul 8, 2008 · N601FE · Doug MD11FSDR 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.Jul 8, 2008 · N742FD · Airbus A300B4622RSDR 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 .Jul 8, 2008 · N742FD · Airbus A300B4622RSDR 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)Jul 5, 2008 · N274WA · Doug MD11FSDR 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.Jul 4, 2008 · N742FD · Airbus A300B4622RSDR 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.Jul 2, 2008 · N40061 · Doug DC1010SDR 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 WJul 1, 2008 · N7232R · Beech B200CSDR 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 WJun 30, 2008 · N609FE · Doug MD11FSDR 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 ANDJun 30, 2008 · N609FE · Doug MD11FSDR 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. REMJun 30, 2008 · N609FE · Doug MD11FSDR 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.Jun 27, 2008 · N880UP · Doug DC873FSDR 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 LJun 27, 2008 · N423FE · Airbus A310203SDR SWAA083525Skin · wornDURING SCHEDULED 6Y CHECK, FOUND RT WING LOWER SKIN WORN OUTBOARD OF PYLON AFT END. REPAIRED SKIN PER SWA EA.Jun 25, 2008 · N406WN · Boeing 7377H4SDR 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. Jun 25, 2008 · N467FE · Boeing 727225SDR 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,Jun 24, 2008 · N572UP · Boeing 747400SDR 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.Jun 24, 2008 · N752UP · Doug DC871FSDR 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)Jun 21, 2008 · N524MC · Boeing 7472D7BSDR KCSA081291Skin · corrodedCORROSION ON RT. WING LOWER SKIN AT BOOST PUMP CUTOUT WS 538 (B)Jun 19, 2008 · N703CK · Boeing 747212BSDR 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 51-21-1Jun 19, 2008 · N665FE · Airbus A300F4605RSDR 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 MIJun 19, 2008 · N586FE · Doug MD11FSDR 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 MINJun 19, 2008 · N586FE · Doug MD11FSDR 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 ANJun 18, 2008 · N443FE · Airbus A310203SDR 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 WINJun 18, 2008 · N443FE · Airbus A310203SDR 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 Jun 18, 2008 · N443FE · Airbus A310203SDR 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 UPPEJun 18, 2008 · N443FE · Airbus A310203SDR 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 PLUJun 17, 2008 · N721CX · Doug DC872FSDR 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 PLUJun 17, 2008 · N721CX · Doug DC872FSDR 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.Jun 17, 2008 · N40061 · Doug DC1010SDR 08FDEA02280Doubler · corrodedRT WING MODERATE EXFOLIATION CORROSION ON LOWER BEAVER TAIL. ACCOMPLISHED EA NR 8-5710-120489.Jun 16, 2008 · N40061 · Doug DC1010SDR 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 COJun 16, 2008 · N721CX · Doug DC872FSDR 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.Jun 12, 2008 · N334UA · Boeing 737322SDR 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 DOUBLERJun 12, 2008 · N49543 · Beech 1900DSDR 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. INSTALLJun 12, 2008 · N721CX · Doug DC872FSDR 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. INSTALLJun 12, 2008 · N721CX · Doug DC872FSDR 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)Jun 11, 2008 · N71GL · Emb EMB120ERSDR KCSA081279Skin · corrodedRT WING UPPER SKIN CORRODED AT WBL 148, 6" FWD OF REAR SPAR (B)Jun 11, 2008 · N712CK · Boeing 747122SDR KCSA081277Skin · corrodedLT WING UPPER SKIN CORRODED AT AFT RABBET AREA W.S.522 (B)Jun 11, 2008 · N712CK · Boeing 747122SDR 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 RJun 10, 2008 · N721CX · Doug DC872F
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