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 FDEA201104251604Skin · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND 05 EACH HOLES WITH CRACK INDICATION AT RT OUTER WING LOWER ACCESS DOOR CUT-OUT AT STA XORS 696.730. REPAIR CARRIED OUT PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REVISION 112.Apr 25, 2011 · N604FE · Doug MD11FSDR VNAA2011042900021Winglet · damagedCREW REPORTED LIGHTNING STRIKE DURING DESCENT INTO DAY. CREW LANDED IN DAY WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DAMAGE TO RIGHT WINGLET, REMOVED AND REPLACED STATIC DISCHARGERS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AApr 25, 2011 · N242JS · Cndair CL6002B19SDR A6WA201140528Skin · corrodedFUEL PANEL WING PLANK ACCESS HOLE AT 540BB HAS FRETTING CORROSION. REPAIRED IAW AWACS E06/021 REV A & REO 601R-57-21-030, REV H OUTSIDE OF CRITICAL AREA.Apr 21, 2011 · N409AW · Cndair CL6002B19SDR FDEA201104211542Skin · crackedLT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 0.375 INCH AND 0.3125 INCH CRACK. STOP DRILLED IAW SRM 57-40-01, REV 46, REPAIR 5 FIG 201. REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND SRM 51-35-01, REV 46. REPAApr 21, 2011 · N644FE · Doug MD11FSDR FDEA201104211541Skin · crackedRT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 1.75 INCH CRACKED. STOP DRILLED IAW SRM 57-40-01 REV 46, REPAIR 5, FIG 201. REPAIR DOUBLER FABRICATED IAW SRM 57-40-01, REV 46, REPAIR 5, FIG 201 AND INSTALLED IAW SRM 51-33-01, REV 46. REPAIR AREA REPROTEApr 21, 2011 · N644FE · Doug MD11FSDR IPXA1M66409Doubler · crackedINSPECTION TYPE:3C, CRACKS RUNNING SPAN WISE FROM 2EA ADJACENT FASTENERS ON RT WING L/E BEADED DOUBLER APPROX XOS STA 703. REPAIRED RT WING INNER BEADED DOUBLER BEWTEEN STA XOS697-703, REF SRM 57-40-02, REPAIR 9, FIG 203.Apr 20, 2011 · N289UP · Doug MD11FSDR IPXA1M66397Doubler · crackedINSPECTION TYPE:3C LT WING L/E COMPT AT APPROX STA XOS737 CEILING DOUBLER CRACKED AT 2EA. FASTENER REPAIRED LT WING INNER BEADED DOUBLER BETWEEN STA XOS 728-740, SRM 57-40-02, REPAIR 9, FIG 203.Apr 20, 2011 · N289UP · Doug MD11FSDR IPXA1M66396Doubler · crackedINSPECTION TYPE:3C, LT WING L/E COMPT AT XOS756 APPROX CEILING DOUBLER IS CRACKED AT 3 FASTENERS. REPAIRED LT WING L/E INNER BEADED DOUBLER BETWEEN XOS 752-758 REF SRM 57-40-02, REPAIR 9, FIG 203.Apr 20, 2011 · N289UP · Doug MD11FSDR IPXA1M66395Doubler · crackedINSPECTION TYPE:3C, CRACK RUNNING FROM FASTENER TO FASTENER OF RT WING L/E BEADED DOUBLER APPROX XOS STA 553. REPAIRED RT WING INNER BEADED DOUBLER BETWEEN STA XOS551-555, REF SRM 57-40-02, REPAIR 9, FIG 203.Apr 20, 2011 · N289UP · Doug MD11FSDR ANZY20110503Skin · corrodedWING CTR SECTION, UPPER SKIN PANEL, U-17C AND LBL 92 UPPER WING SKIN AND SPLICE: SKIN CORRODED BEYOND SRM LIMITS. DURING FINAL CLOSE UP OF AIR RETURN GRILLS IN THE OVER WING AREA, A FOD INSP WAS CARRIED OUT WITH MIRROR, PRIOR TO INSTALLING THE PANEL. HEAVY CApr 20, 2011 · N598HA · Boeing 767332SDR FDEA201104201540Skin · crackedRT WING BOTTOM SKIN, BOTTOM SURFACE AT T/E 13.5IN INBD OF RIB 9 HAS A CRACK. ABOUT 1.25 IN LONG. REPAIRED CRACKED SKIN IS ACCOMPLISHED ON E6-5710-7-5013, REV 01, PT6.Apr 20, 2011 · N650FE · Airbus A300F4605RSDR DALA1134856313Skin · damagedRIVETS (4 EA) WERE LOOSE ON L/E SURFACE OF RT WING WS 320, PER SRM 57-41-01 R5 REPAIRED THE SKIN PER NR-57-021, HT-AC-040, NR-57-019, HT-AC-022. HEAT TREATMENT THE REPAIR PARTS.Apr 19, 2011 · N673US · Boeing 747451SDR QXEA2011042500293Skin · damagedBIRD STRIKE DAMAGE BETWEEN STA YW 510.229 AND YW 494.019. RT WING FWD SPAR, UPPER FLANGE HAS 32 DEGREE DOWNWARD DEFLECTION (APPROX .040") MAX DEFLECTION IS APPROX 3.0" OTBD FROM YW 494.019 DECREASING OTBD APROX 10.0" UPPER SKIN HAS IMPACT DAMAGE TO PAINT IN TApr 19, 2011 · N437QX · Bombdr DHC8402SDR UALA2011041901901Panel · damagedUPPER INBOARD WING LEADING EDGE BULLNOSE HAS DAMAGE. IN REFERENCE TO SMC002, NEED TO REMOVE THE LT WING FIXED L/E PANEL UNDER NR 6 SLAT THAT HAS 7 CRACKS AND A COUPLE OF DELAM AREAS AND REMOVED AND REPLACED TO SHOP. 90% OF FASTENERS ARE REMOVED, NEED TO CONTIApr 18, 2011 · N539UA · Boeing 757222SDR DALA1134846313Skin · crackedLT WING FIXED L/E SKIN HAS TWO CRACKS. ILES 330. LMAX: 1.5 INCH PER SRM 57-41-01 R5. REPAIRED THE SKIN, PER NR-57-022, HT-AC-037, NR-57-018, HT-AC-021, NR-57-020, HT-AC-039. HEAT TREATMENT THE REPAIR PARTS.Apr 17, 2011 · N673US · Boeing 747451SDR UALA2011041801865Fastener · looseLT WING, INBOARD MOST, LOWER, FUEL TANK ACCESS PANEL LEAKING FUEL. RETORQUED FASTENERS. REFUELED CTR FUEL TANK, LEAK CHECKED FOR AN EXTENDED TIME. LEAK CHECKED OKAY. REBALANCED FUEL LOAD.Apr 16, 2011 · N593UA · Boeing 757222SDR FDEA201104161506Skin · wornLT WING RIB 5 FITTING HAS 2 EA TAPERLOKS INSTALLED AT HOLES 47/54 REWORKED SPOTFACE AND INSTALLED NEW TAPERLOKS AT HOLES 47/54 IAW EA 6-5710-136750 TITLE WINGS- AD2010-23-26-EO6-5710-7-3325-SB A300-57-6110-MLG RIB 5 SPOTFACE ON THE BOTTOM FLANGE.Apr 16, 2011 · N668FE · Airbus A300F4605RSDR BQVA2011041900009Winglet · corrodedDURING COMPLIANCE OF CMP CODES 576511 & 576516 WINGLET ATTACH HARDWARE (LEFT & RIGHT) - INSPECTION (144 MONTH), SOME CORROSION WAS FOUND IN THE WINGLET ATTACH BORES ONCE THE BUSHINGS WERE REMOVED.Apr 15, 2011 · N58AJ · Gulstm G1159ASDR REXA201100219Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLE NR 1 AT WS 54.897 HAS CORROSION AT INBOARD END, NOT IN CRITICAL REGION. CORROSION REMOVED IAW BOMBARDIER REO 601R-57-21-030 REV H.Apr 14, 2011 · N8869A · Cndair CL6002B19SDR A6WA201140377Panel · corrodedFUEL PANEL CUT OUT 510AB HAS FRETTING CORROSION. REPAIRED FUEL PANEL CUT OUT 510AB IAW REO 601R-57-21-030.Apr 13, 2011 · N459AW · Cndair CL6002B19SDR GLBA20110413FSkin · delaminatedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND EROSION DAMAGE TO THE TOP OF L/E TIP OF THE RT WINGLET, DELAMENATION ON THE INBD SIDE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-003. MATERIALS UTILIZEDApr 13, 2011 · N257GL · Beech 1900DSDR IPXA1B66702Skin · misrepairedINSP TYPE:D, REPAIR DOES NOT CORRELATE TO A SRM. REPAIRED IAW HX RS NR R-57-44-37048, REV A & EO NR B747-5750-42645-A, ORG MAT'S IS CLAD 2024T42-0.040" DENT AREA IS 0.022" DEPTH X 0.075" WIDTH & 1.25" LENGTH. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Apr 12, 2011 · N582UP · Boeing 7474R7FSDR FDEA201104121445Skin · corrodedRIGHT WING UPPER SURFACE FOUND CORROSION POSITION AT O /B GROUND POINT ABOUT RIB 27-28 PERFORMED WINGS, SKIN AND PLATES: PERMANENT REPAIR REF. TO EA 6-5730-150286. PER GMM 6-2-100 CLASSIFIED MAJOR.Apr 12, 2011 · N426FE · Airbus A310203SDR FDEA201104121460Skin · corrodedSURFACE CORROSION AROUND WING FUEL LEVEL INDICATOR 1A-1 ON LT WING LOWER SURFACE. REPAIR CARRIED OUT IAW EA6-5730-150102. AREA BLENDED AND SHOT PEENED, NDT CARRIED OUT IAW NTM 57-20-10 WITH NO CORROSION EVIDENT.Apr 12, 2011 · N727FD · Airbus A300B4622RSDR FDEA201104121444Skin · corrodedLT WING FOR SKIN GOT CORROSION AT STA 845 SURROUND GROUNDING STUD (RIB 13-14, STR7-8).Apr 12, 2011 · N426FE · Airbus A310203SDR GR4D20110412001Skin · corrodedRT WINGLET CORRODED.Apr 12, 2011 · N472QS · Gulstm GIVXSDR LR7A2011041900188Skin · crackedDURING SCHEDULED C-9 CHECK, FOUND RT UPPER CTR WING NR 2 STRINGER WING PLANK LAYER HOLE CRACK AT CWS212. REPAIR ACCOMPLISHED IAW MEA 382-57-11-005.Apr 11, 2011 · N405LC · Lkheed 382GSDR VNAA2011041400009Winglet · damagedAT MLB, CREW REPORTED BIRD STRIKE TO RIGHT WINGLET. AIRCRAFT FERRIED FOR REPAIR OF DAMAGE. MAINTENANCE INSPECTED, REMOVED AND REPLACED SEVERAL DAMAGED FAIRINGS ON RIGHT WINGLET, REPAIRED WINGLET SKIN AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. Apr 11, 2011 · N703PS · Cndair CL6002C10SDR QXEA2011041200272Skin · corrodedWING SKIN MATING SURFACE FOR ACCESS 524AT HAS POSSIBLE CORROSION ON OTBD SIDE. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-445.Apr 11, 2011 · N417QX · Bombdr DHC8402SDR QXEA2011041200271Skin · corrodedWING SKIN MATING SURFACE FOR ACCESS 524ET HAS CORROSION ON INBD SIDE. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-445.Apr 11, 2011 · N417QX · Bombdr DHC8402SDR IPXA1666340Panel · debondedINSPECTION TYPE:C, RT WING T/E OTBD FORE FLAP, OTBD UPPER PANEL FOUND DISBONDED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR 2, FIG 203, REV 59.Apr 10, 2011 · N582UP · Boeing 7474R7FSDR IPXA11M66556Skin · corrodedINSPECTION TYPE:4C, CTR CABIN UNDER FLOOR CTR WING UPPER SKIN PANEL APB7441-1 SPLICE AT STRINGER 15 HAS CORROSION ON UPPER SURFACE AT RBL28.5, 53.2, 42, 50, 52.5, 53.5, 74, 79, 95, 98. REPAIRED NOTED CORROSION REF EO MD11-5730-42603-A AND STASA EA 011-5730-0Apr 9, 2011 · N251UP · Doug MD11FSDR IPXA11M66555Skin · corrodedINSPECTION TYPE:4C, CTR CABIN SUBFLOOR CTR WING UPPER PANEL APB7441-1 HAS CORROSION ON UPPER SURFACE BETWEEN STRINGER 17 & 18 AND BETWEEN X-102 AND X-106 4 AREAS. REPAIRED CORROSION ON MAIN CABIN CTR WING BOX UPPER SKIN S17-S18 REF EO MD11-5730-42604-A AND STApr 9, 2011 · N251UP · Doug MD11FSDR A6WA201140378Skin · chafedRT AILERON UPPER AND LOWER L/E SKIN FIXED AND REMOVEABLE PANELS ARE CHAFED. REPAIRED PANELS IAW REO 601R-57-60-020. REPLACED PANEL 699AB IAW SRM 51-40-11.Apr 8, 2011 · N459AW · Cndair CL6002B19SDR UALA2011040801698Skin · damagedRIGHT WING, FIXED LEADING EDGE PANEL, AFT EDGE DIRECTLY ABOVE NUMBER THREE ENGINE, HAS 2 RIVETS SHEARED AND PROTRUDING. RIVETS ARE NEXT TO EACH OTHER. INSTALLED 2 EA BLIND RIVETS REF MM. REQUIRES RE-CHECK EVERY AK AND PERMANENT REPAIR AT CK MF6728 OPENED TOApr 8, 2011 · N118UA · Boeing 747422SDR UALA2011040801697Skin · damagedLEFT L/E PANEL, ILES 414.50 PANEL INBD AFT CORNER HAS 1 EA RIVET SHEARED. INSTALLED 1 EA ALUMINUM BLIND FASTENER,THIRD FASTENER FORWARD FROM FRONT SPAR L/E, PANEL 6 AT ILES 414.50 IAW AMM. REPLACED THE BLIND RIVET WITH A SOLID RIVET PER AMM.Apr 8, 2011 · N118UA · Boeing 747422SDR QXEA2011041200277Panel · corrodedPANEL 524AT HAS ONE SMALL AREA OF POSSIBLE CORROSION ON L/E OF PANEL. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-442.Apr 8, 2011 · N417QX · Bombdr DHC8402SDR QXEA2011041200276Panel · corrodedPANEL 524BT HAS AREA OF POSSIBLE CORROSION ON OTBD END OF PANEL. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-442.Apr 8, 2011 · N417QX · Bombdr DHC8402SDR QXEA2011041200275Panel · corrodedPANEL 524ET HAS TOOLING MARKS AND POSSIBLE CORROSION ON OTBD END. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-442.Apr 8, 2011 · N417QX · Bombdr DHC8402SDR QXEA2011041200274Panel · corrodedPANEL 624AT HAS POSSIBLE CORROSION ON OTBD ENDS. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-442.Apr 8, 2011 · N417QX · Bombdr DHC8402SDR QXEA2011041200273Panel · corrodedPANEL 624CT HAS POSSIBLE CORROSION ON BOTH INBD AND OTBD ENDS. BLENDED OUT CORROSION AND COMPLETED REPAIR IAW RD 8/4-57-442.Apr 8, 2011 · N417QX · Bombdr DHC8402SDR CA110413014Panel · missing(CAN) DURING MAINTENANCE WALK-AROUND, IT WAS DISCOVERED THAT A RIVETED PANEL, FWD OF INBD FLAP ON RT WING WAS MISSING IAW SRM 57-51-39.Apr 7, 2011 · Airbus A330243SDR A6WA201140341Skin · chafedBUTTE DOOR 694PB INNER SKIN CHAFED. R & R BUTTE DOOR 694PB SKIN IAW SRM 51-42-06.Apr 6, 2011 · N417AW · Cndair CL6002B19SDR A6WA201140280Skin · chafedWS 45.00 AT FS 511 ON LOWER CENTER PLANK HAS CHAFING BLENDED W/S LBL 45.00 AT FS 511. FOUND TO BE WITHIN LIMITS IAW REO 601R-57-21-880, REV B COMPLIED WITH REO 601R-57-21-880, REV B, SHEETS 1-5.Apr 6, 2011 · N459AW · Cndair CL6002B19SDR FDEA201104061343Skin · crackedLT WING - 15 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. CARRIED OUT REPAIR AS PER BOEING DRAWING : SG11570004 REVISION B. QUANTITY 01 EACH CRACKEDApr 6, 2011 · N616FE · Doug MD11FSDR FDEA201104061344Skin · crackedRT WING - 13 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 TO STA XORS 713.6. CARRIED OUT REPAIR AS PER DRAWING : SG11570004 REVISION B. REPAIR CLASSIFIED AS MINOR AS PER Apr 6, 2011 · N616FE · Doug MD11FSDR FDEA201104061336Skin · crackedLT WING L/E NOSE SKIN AT NACELLE AT ISS 280 FOUND WITH 1.5" CRACK. LT WING L/E NOSE SKIN AT NACELLE AT ISS 280 REPLACED BY FABRICATION IAW DWG 114N1802, SHT 1, REV G. ALTERNATE FINISHING PROCESS CARRIED OUT IAW EA F-5730- 142535 PART 1, STEP 1, WINGS - PLAApr 6, 2011 · N948FD · Boeing 757236SDR FDEA201104061334Skin · crackedRT WING L/E NOSE SKIN AT NACELLE AT ISS 280 FOUND WITH 1.5" CRACK. EVALUATE AND RECTIFY. RT WING L/E NOSE SKIN AT NACELLE AT ISS 280. REPLACED BY FABRICATION IAW DWG 114N1802, SHT 1 REV G. ALTERNATE FINISHING PROCESS CARRIED OUT IAW EA F-5730- 142535, WINApr 6, 2011 · N948FD · Boeing 757236SDR DALA13009473169Panel · wornRT WING L/E PANEL LANDING BETWEEN SLAT TRACK NR 5 THROUGH NR 6 INBD SIDE WORN. REMOVED DISCREPANT PANEL LANDING. INSTALLED NEW LAND IAW TRM 57-27-13. COMPLIED WITH PERMANENT REPAIR IAW TRM 57-27-13.Apr 5, 2011 · N369NB · Airbus A319114SDR IPXA1M66278Skin · corrodedINSPECTION TYPE:4C, RT WING UPPER SKIN HAS CORROSION AROUND FASTENERS BETWEEN XORS402-433 AT STRINGER 9. REPAIRED CORROSION REF EO MD11-5730-42373-A AND STASA EA 011-5730- 01-A3045 REV IR ON RT WING UPPER SURFACE STA XORS402-433 ALONG STR 9.Apr 5, 2011 · N251UP · Doug MD11F
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