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 2010FA0000739Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 640 QB. NO CORROSION REMOVAL LIMITS FOUND IN SRM. PANEL IS LISTED AS A PRIMARY STRUCTURAL ELEMENT. REPLACED PANEL WITH NEW PANEL.SDR FDEA201007182579Skin · unknownEXISTING REPAIR AT RT WING TIP LWR SKIN XW931, 38" FROM AFT T/E. REMOVED AND REPLACED WITH NEW REPAIR AS PER EA 8-5710-140406 REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA201007162557Skin · misrepairedRT WING NR1 SLAT INNER SKIN AT STA XIS 237 FOUND EXISTING REPAIR. EXISTING REPAIR AT RT WING NR1 SLAT INNER SKIN STA XIS 237 EVALUATED AND FOUND NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR REMOVED IAW SRM 51-31-01 VOLUME II REV 96 AND NEW REPAIR CARRIED OUSDR FDEA201007162570Skin · corrodedRT WING UPPER SKIN SURFACE 8 INCH AFT OF REAR SPAR AND RIB 4 HAS 4 SQ INCH OF CORROSION COMMON TO FASTNER HEAD. REPAIR ACCOMPLISHED IAW EA 6-5730-135225 IAW APPROVED DATA REF 6, RAS/BAE/1013408/2010, ISSUE A. THE REPAIR IS IAW THE A/B REPAIR RECOMMENDATIOSDR IPXA10B61592Panel · noneINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE UPPER SURFACE EXISTING REPAIR (REDO) REF SURVEY SEQ NO 581-W3-09 (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61590Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) SURVEY SEQ NR 581-W3-04. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61589Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) NO REPAIR RECORD. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 57.SDR FDEA201007152552Skin · misrepairedRT L/E LOWER ACCESS FWD CUTOUT AREA FOUND 01 EA EXISTING REPAIR INBD OF ACCESS PANEL 626FB. EXISTING REPAIR AT RT L/E LOWER ACCESS FWD CUTOUT AREA INBD OF ACCESS PANEL 626FB FOUND NOT CONFORM TO SRM. EXISTING REPAIR REMOVED AND NEW REPAIR ACCOMPLISHED IAW SRMSDR USAA2010071691438Panel · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING FUEL PANEL 640EB. REPLACED RIGHT WING FUEL PANEL 640EB.SDR UALA2010071502533Panel · crackedRT WING OTBD T/E PANEL AT WS 905, FASTENERS ARE TORN THROUGH PANEL, PANEL IS CRACKED ABOUT 12' LONG. REMOVED T/E PANEL AND REPAIRED AT SHOP. REINSTALLED PANEL IAW MM. WORK WAS ACP ON NR 2176N00126.SDR UALA2010071402527Panel · damagedVIBRATION NOISE ENCOUNTERED IN FLIGHT. ACP VIBRATION CK AND FOUND PANEL 191DT HAS EROSION DAMAGE ON L/E OF PANEL. ACP QUICK DISPATCH SPEED TAPE REPAIR. A PERMANENT REPAIR MUST BE ACCOMPLISHED WITHIN 300 FLT HOURS. FLT 225-25 CREW REPORTS NO VIB-NOISE FELT ISDR IPXA10B61585Panel · noneINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE LWR SURFACE EXISTING REPAIR. (NO REPAIR RECORD) FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV.57.SDR TRBACPCP2010047Skin · corrodedTHIS IS A FINAL REPAIR OF CORROSION PREVIOUSLY FOUND DURING SCHEDULED MX PHASE CHECK, THE AREAS OF CORROSION WERE FOUND AT LT WING LOWER SURFACE AT T/E BETWEEN RIBS 9-10. COMPLIED WITH TDMI 570424 CORROSION FOUND ON LT AFT WING AREA BTW RIB 9-10 FINAL REPAIR, SDR FDEA201007122478Skin · unknownEXISTING REPAIR AT RT WING NR5 SLAT L/E LOWER SKIN XORS 738. EXISTING REPAIR AT RT WING NR5 SLAT L/E LOWER SKIN XORS 738. R & R WITH NEW REPAIR IAW SRM 57-10-00, FIG 31, VOL I, REV 96, EO 8-5100-7-5001, A7 PT2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, RESDR A6WA201040539Panel · chafedLT OTBD FLAP, BUTTE DOOR PANEL NR 594PB HAS MINOR CHAFING. R & R BUTTE DOOR PANEL NR 594PB WITH SERVICEABLE PART PN 601R102279 IAW SRM 51-42-06.SDR ASMF201007004Access Panel · brokenDURING FUELING, TECH DETECTED A FUEL LEAK IN RT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 632FB; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT.SDR GUUA93957071110ASkin · debondedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED FUEL PANELS 542DB, 542CB AND 532FB HAD SEVERE DEBONDING OF DOUBLER RING ACCESS HOLES AT WING SKIN. FABRICATED AND INSTALLED REPAIR DOUBLERS FOR FUEL PANEL ACCESS HOLES.SDR IPXA0B61956Skin · dentedINSPECTION TYPE:C, RT WING INBD AFT FLAP LWR SKIN FOUND DENTS. SKIN METAL HOT BOND INTERIM REPAIRED IAW HX RS NR R57-51-36778, REV A AND EO B747-5750-39125-A. THIS IS A MAJOR REPAIR WITH ALUMINUM SHEET : 2024T3-0020IN. REPAIR PATCH SIZE: 51.5" X 19". FINAL CUSDR FDEA201007092438Skin · crackedRT WING FIXED L/E STA XOS 774 SLAT TRACK NR 12 CUT OUT LOWER OTBD CORNER FOUND CRACKED. TRIMMED OUT AND REPAIRED IAW SRM 57-10-00, FIG 68, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.SDR FDEA201007092437Skin · crackedLT WING FIXED L/E STA XOS 774 SLAT TRACK NR 12 CUT OUT LOWER OTBD CORNER FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIG 68, VOLUME I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.SDR COER2010FA0000711Skin · corrodedREMOVED CORROSION IAW ATR 72 SRM 57-14-12 PB400 REV 77. FINAL DIMENSION OF .732" - .738" WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FOIL + SPACERS ON 521DT ACCESS PNL FOR REWORKED DOOR CUTOUT AS PER SRI DO/TS-3754/10-13808. NOTE: APPLICATION OF SRI DO/TSDR UIEA2010070800112Skin · corrodedDURING THE D-03 CHECK, CORROSION FOUND ON RT WING T/E, LOWER SKIN 112U4502-2 WHICH MATING WITH FIXED PANEL 112U4710-38 AT WBL 1144. LEVEL 1 CORROSION. (CORROSION WAS COMPLETELY REMOVED AND THE BLENDED SKIN AREA AND FASTENER HOLES ARE DET/HFEC INSPECTED TO CONSDR FDEA201007082428Access Door · crackedRT WING - WING TIP LOWER SURFACE AFT OF STROBE LIGHT ACCESS DOOR FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR8-5720-138577, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR FDEA201007082427Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. REPAIR CARRIED OUT IAW EA NR8-5710-140426, REPAIR IS CLASSIFIED MAJOR IAW GMM 6-2-100, REV 110.SDR 2010F00152Skin · corrodedREMOVABLE PANEL CUTOUT FOR PANEL 622CT IS CORRODED BEYOND SRM LIMITS. (LEVEL II) REMOVED CORROSION IAW ATR 72 SRM 57-14-12, PB 400 REV 77. FINAL DIMENSIONS AT .713 - .717 WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FOIL + SPACERS ON ACCESS PNL 622CT FOR RESDR 2010F00151Skin Panel · corrodedREMOVABLE PANEL CUTOUT FOR PANEL 522CT IS CORRODED BEYOND SRM LIMITS. REMOVED CORROSION IAW SRM 57-14-12, PB 400, REV 77. FINAL DIMENSIONS OF .691"- .696" WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW FOIL & SPACERS ON PANEL 522CT FOR REWORKED DOOR CUTOUT IAW SDR 2010FA0000711Skin Panel · corrodedREMOVABLE PANEL CUTOUT FOR PANEL 521CT IS CORRODED BEYOND SRM LIMITS. (LEVEL II)SDR FDEA201007082408Skin · dentedLT WING TIP UPPER SURFACE AT FWD SIDE FOUND DENTED. REPAIR CARRIED OUT IAW SRM 57-00-01, FIG 4, VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.SDR IPXA10M61224Skin · chafedINSPECTION TYPE:3C, LT ANTI-ICE TELESCOPIC DUCT L/E CUT OUT EXTERNAL DOUBLER CHAFED. REMOVED DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLER IAW STA SA EA 011-5730-01-A2545 EO MD11-5730-38820-A.SDR IPXA10M61223Skin · chafedINSPECTION TYPE:3C, LT WING FIXED L/E HAS CHAFED WEAR LOWER SURFACE APPROX XDLE 309. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW STA SA EA 011-5750-01-A2547 I/R AND EO MD11-5730-38832-A.SDR IPXA10M61197Skin · chafedINSPECTION TYPE:3C, LT WING FIXED L/E APPROX W/S 267 FOUND CHAFE WEAR 10" LONG. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND SHIM IAW SRM 57-40-02, REPAIR 5, FIG. 201.SDR IPXA10M61176Doubler · crackedINSPECTION TYPE:3C, RT WING OTBD L/E COMPARTMENT CEILING HAS MULTIPLE CRACKS AT STA XOS 698. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MM-57-40-02, REPAIR 9, FIG. 203SDR IPXA10M61175Skin · crackedINSPECTION TYPE:3C, LT WING DROOP L/C UPPER SURFACE HAS 2 CRACKS. STOP DRILLED CRACKS, FABRICATED AND INSTALLED REPAIR DOUBLER AND RUB STRIP IAW SRM 57-40-01, REPAIR 5, FIG 201.SDR ASMF201007003Access Door · damagedDURING TRANSIT CHECK A BIRD STRIKE WAS DETECTED BETWEEN SLAT NR 9 AND 10. MX PERFORMED A BIRD STRIKE INSP IAW 05-51-18 DETECTING DAMAGES IN ANTI ICE RELEASE ACCESS DOORS SLAT. THE RT WING SLAT LEADING EDGE NR 9 WAS REPLACED IAW DWG NR 114W4565 AND INSTALLED FASDR USAA2010071591426Access Door · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON RIGHT WING LOWER SKIN ACCESS DOOR 640KB. REPLACED SKIN ACCESS DOOR 640KB IAW A319 SRM 57-27-11.SDR USAA2010071591424Access Panel · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON RIGHT WING LOWER SURFACE SKIN ACCESS PANEL 640FB. REPLACED SKIN ACCESS PANEL 640FB IAW A319 SRM 57-27-11.SDR USAA2010071591423Access Panel · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 INTERGRANULAR CORROSION ON NUMEROUS FASTENER HOLE COUNTERSINKS AT RIGHT WING LOWER SURFACE SKIN ACCESS PANEL 640JB. REPLACED SKIN ACCESS PANEL 640JB IAW A319 SRM 57-27-11.SDR FDEA201007062371Skin · corrodedCORROSION - UPPER SKIN, EXTERIOR SURFACE OF WING CTR SECTION FUEL TANK. APPROX BS 825, RBL 12. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-10-6 AND 57-30-1 FIG 4. REPAIRED AREA IAW EA 7-5730-142035.SDR FDEA201007062351Skin · corrodedCABIN RT STATION 1195 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV. 96. FOUND EXCEED LIMIT IAW SRM 57-20-00 FIG 8A, VOL I, REV 96.ORIGINAL THICKNESS: 0.143", REMAINING THICKNESS: 0.106", MATERIAL SDR FDEA201007062350Skin · corrodedCABIN RT STA 1189 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.139", REMAINING THICKNESS = 0.107", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A SDR GUUA93357070510ASkin · dentedDURING INSPECTION FOUND SKIN DENTS ON SEVERAL AREAS OF RIGHT WING UPPER SKIN BETWEEN WS 236.62 AND WS 249.75. CUT OUT DAMAGED AREAS AND INSTALLED AN INSERTION PATCH AND REPAIR DOUBLERS.SDR UIEA2010070400089Skin · corrodedNRC 0740 (RA4174), "MAIN DECK" FOUND CORROSION ON THE WING CTR SECTION BOX UPPER SURFACE SKIN AT STA 1241, RBL 75 TO 80, WL 149 (THE WORK ACCOMPLISHED IAW REA: MF0068720008 AND RF7A: 00687-0008).SDR SIMA201018702Skin · damagedDURING MAINTENANCE BASE VISIT FOUND DAMAGE TO LEFT WING LOWER SKIN AND ANGLE DUE TO TIRE STRIKE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED REPAIR OF DAMAGE TO LEFT WING LOWER SKIN AND ANGLE IAW EO-EM-57MR0488R3. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR FDEA201007022314Skin · crackedRT WING ANTI ICE TELESCOPIC DUCT DOOR CUT OUT SKIN FOUND CRACKED. RT WING ANTI ICE TELESCOPIC DUCT DOOR CUT OUT SKIN REPAIRED IAW EA NR 8-5710-132442, TITLE: WINGS - RT WING ANTI-ICING TELESCOPIC DUCT DOOR CUTOUT - REPAIR. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-SDR USAA2010070791357Skin Panel · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON RIGHT LOWER WING PANEL 640DB 360 DEGREES AT INNER MATING AREA. REPLACED RIGHT LOWER WING PANEL 640DB IAW A319 SRM 57-27-11.SDR USAA2010070791356Skin Panel · corrodedPIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON RIGHT LOWER WING PANEL 640EB 360 DEGREES AT INNER MATING AREA. REPLACED RIGHT LOWER WING PANEL 640EB IAW A319 SRM 57-27-11.SDR DHLA201000085Skin · crackedRT WING TOP AFT PANEL PLATING CRACKED 4" STA XCW 69.500 PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 20, SHEET 1. REMOVED FASTENERS IAW SRM 51-3-0, SRM 51-1-20D. CUT OUT DAMAGED AREA + FABRICATED (-5) DOUBLER (7075"0" 0.160") + (-7) TRIPLER (7075"0" 0.125") + FISDR IPXA10M60858Skin · puncturedINSPECTION TYPE:1C, PANEL ARC0583 ON LT WING T/E UPPER SURFACE HAS HOLE ACCOMPLISHED REPAIR ON LT WING T/E UPPER SURFACE SKIN PANEL ARC0583 IAW SRM 57-00-01, FIG 201, SHEETS 1&2.SDR FDEA201006302231Panel · corrodedRT OVERWING FILL PORT ADAPTER CUT OUT FOUND WITH LIGHT CORROSION. AFTER CLEANING, RT OVERWING FILL PORT ADAPTER CUT OUT CORROSION REPAIRED IAW EA NR F-5730-135853, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR TRBACPCP2010040SUSkin · corrodedC/W LT WING LOWER SKIN CORROSION BLENDED OUT PERMENANT REPAIR AT FUEL DRAIN BTW RIBS 4-5 IAW EO E2-57MR-400. NDT REPORT ACCOMPLISHED IN REF TO AMS 100603-42. COMPLIED WITH SRAS REF DO/TS-2060/10-5710 ISSUE B. SRI DO/TS-2060-13328. OPEN TDMI DVI TO BE PERFOR
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