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 ABXR200910030029Skin · corrodedDURING A HEAVY MX INSP, THE LWR WING PLATE WAS FOUND EXFOLIATED ABOVE THE LT PRIMARY HEAT EXCHANGER. DAMAGED AREA APPROX 6" X 5", REMOVED ALL CORROSION, BEYOND MFG LIMITS. MACHINED PAD-UPS TO ACCOMMODATE EXTERNAL DOUBLER. SPOT FACED SANDWICHED FASTENER HEADS SDR ABXR200910020024Skin · corrodedDURING A HEAVY MX INSP EVENT, LWR WING PLATE HAS 2 AREAS OF CORROSION. CORROSION WAS REMOVED, AREAS WERE WITHIN LIMITS. RETURNED TO SERVICE.SDR IPXA09M57766Skin · misrepairedINSPECTION TYPE:1/C REPAIR SURVEY SEQ. 283-W3-05 AT LT WING FIXED L/E EXISTING REPAIR AP PROX. BETWEEN XOS STA. 610 AND 621 DOES NOT CORRELATE TO SRM 57-1 0-00, FIG. 14, AND PAGE 40, VOL. 1, REV. 38 REPAIRED AS PER UPS EO MD11-5730-35339-A AND SAA EA 011-5SDR AALA20091104TUL06Skin · crackedCRACK ON RIGHT WING INBOARD LEADING EDGE BULLNOSE SKIN. INSTALLED EXTERNAL DOUBLER REPAIR UNDER ESO 90309 AND SRM 57-41-01-2R.SDR CALA2009100100580Skin · wornRT WING FUEL TANK TUBING FOR WATER SCAVENGE JET PUMP LOCATED INSIDE TANK O/B OF WING RIB 5 HAS MADE RUB MARK IN LOWER WING SKIN (INSIDE TANK) ABOUT 10 INCHES O/B OF RIB 5 AND 2 INCHES FROM REAR SPAR. ACCESS THROUGH LOWER WING PANEL 632A B, BLENDED OUT SMOOTH SDR IPXA09M57705Doubler · crackedINSPECTION TYPE:1/C LT WING FIXED L/E INSIDE FUEL PANEL APPROX STA X0S631, BEADED DOUBLER HAS NUMEROUS CRACKS. REPAIRED AS PER MD11 SRM 57-40-02, REPAIR 9, FIG 203, SHEETS 1-4 REF IPXA RCD NR 358082.SDR IPXA09M57671Skin · misrepairedINSPECTION TYPE:1/C RT WING FIXED LEADING EDGE REPAIR SURVEY SEQ NR 283-W4-06 DOES NOT CORRELATE WITH SRM. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW IPXA EO NR MD11-5730-35 228-A AND SAA EA NR 011-5730-01-A2064 ISSUE "A", REF IPXA RCD NR 358007.SDR FDEA200909293425Skin · corrodedRT WING (TOP) HAS EXFOLIATION CORROSION AT BS 922, 20 INCHES FROM FRONT WING SPAR. REPAIR CARRIED OUT IAW EA F-5710-132616.SDR AALA20091104TUL08Skin · crackedCRACK FOUND IN RIGHT WING BULLNOSE SKIN OVER PYLON INBOARD BEND. REPLACED UNDER AARD 51-41-01-01 PG 1 AND SRM 57-41-01-01 PG 1, FIG 1.SDR AALA20091104TUL07Skin · crackedCRACK AT LEFT WING IN BULLNOSE SKIN OVER PYLON INBOARD BEND. REPLACED UNDER ESO 90309 AND AARD 51-00-00-1.SDR IPXA09M57625Skin · crackedINSPECTION TYPE:C1 RT WING L/E BEADED SKIN CRACKED IN 3 AREAS, JUST OTBD OF NR 10 SLAT TRACK (BOTH SIDES OF RIB). REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER MD-11 SRM 57-40-02 FIG 203 REPAIR 9.SDR IPXA09M57624Skin · crackedINSPECTION TYPE:C1 RT WING L/E UPPER SKIN IS CRACKED, JUST OTBD OF NR 12 SLAT TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED 1 DOUBLER, 1 FILLER AND 2 REPAIR ANGLES PER MD-11 SRM 57-40-02 REPAIR 9 FIG 203.SDR FDEA200909283417Skin · corrodedLT WING (TOP) HAS EXFOLIATION CORROSION AT BS 1019.5 BELOW SUPPORT ASSY. CORROSION ON WING TOP AT BS1019.5 REPAIRED IAW EA NR F-5710-132618. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200909283416Skin · corrodedRT WING (TOP) HAS EXFOLIATION CORROSION AT BS 922, TWENTY INCHES FROM FRONT WING SPAR. CORROSION ON RT WING REPAIRED IAW EA F-5710-132616. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200909283415Skin · corrodedRT WING (TOP) HAS EXFOLIATION CORROSION AT BS 1020, 7 INCHES FROM FUSELAGE SKIN SURFACE. REPAIR CARRIED OUT IAW EA F-5710-132617. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRTIERIA.SDR UALA2009092503026Access Panel · leakingDURING PREFLT FOUND FUEL LEAKING FROM RT WING 2ND ACCESS DOOR. REPLACED ACCESS PANEL 631BB AND SEAL. ALSO REPLACED SEAL ON ACCESS PANEL 631AB. LEAK CHECKS OKAY.SDR A6WA200940630Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640DB. REPAIR PERFORMED ON FUEL ACCESS DOOR DUT-OUT 640DB IAW REO 601R-57-21-030, REV "G" AND AWAC E06/021/457, REV "A". (K)SDR GUUA94057092409ASkin · corrodedDURING SCHEDULED ROUTINE INSP DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 123.988 THROUGH 196.06. REMOVED DAMAGED SKIN AND INSTALLED AN EXTERNAL REPAIR DOUBLER.SDR IPXA09557546Skin Panel · crackedINSPECTION TYPE:C1 RT WING FIXED L/E SKIN CRACKED AT FSS 433.5. REPAIRED PER STANDARD EO B757-5740-11855-D.SDR ASOA200901039Skin · crackedLT WING PLANK IS CRACKED AT THE AFT SPAR ON WS 148.019. REPAIRED LT WING PLANK AT THE AFT SPAR IAW EC/TC 600-57-134 C/W LK CK GOOD IAW CRJ 200 AMM 28-11-00.SDR IPXA09M57764Skin · gougedINSPECTION TYPE:4C REPAIR SURVEY SEQ NR 278-W4-02 RT WING LE HAS GOUGE ON LE DOUBLER INBD OF ANTI-ICE TELESCOPIC DUCT STA XOS 454-XOS 481. REMOVED EXISTING REPAIR AT RT WING LE SKIN AT STA XOS454- XOS 481. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MSDR WRLA20090922227Skin · damagedLEFT WING FIXED LEADING EDGE NOSE OUTER SKIN AT ILES 330.00, THERE ARE 11 FASTENERS WORN AND 4 FASTENER HOLES ENLARGED. REPAIRED LEFT WING FIXED LEADING EDGE NOSE OUTER SKIN ILES 330, PER 747-400 SRM 57-41-01 REPAIR 5 DETAIL I REV 73. REMOVED AND REINSTALLEDSDR WRLA20090921226Skin · wornDURING C-CHECK, MAINTENANCE DISCOVERED 11 FASTENERS WORN AND 4 FASTENER HOLES ENLARGED ON THE RIGHT WING FIXED LEADING EDGE NOSE OUTER SKIN AT ILES 330.00. CORRECTIVE ACTION WAS TO REPAIR THE SKIN PER B747-400 SRM 57-41-01 REPAIR 5, DETAIL I, REV 73. REQUIRESDR EE4Y090279Skin · corrodedFOUND THE LT WING LOWER SKIN INNER SURFACE CORRODED, AT XRS 69.500 NEAR TO REAR SPAR.SDR EE4Y090274Skin · corrodedCOO REPORTED, IN LT WING, THE LEADING EDGE UPPER SKIN, WITH CORROSION FROM XFS 228.5 TO XFS 250.5SDR IPXA09M57669Skin · crackedINSPECTION TYPE:4C RT WING LE CEILING SKIN ABOVE THE INBD FUELING RECEPTACLE HAVE 2 PLACES OF CRACK ACROSS THE FASTENER XORS 50. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW MD-11 SRM 57-40-02 REPAIR 9, FIGURE 203 SHT 1-4.SDR IPXA09557526Skin Panel · crackedINSPECTION TYPE:C2 RT WING FSS 440 FIXED LOADING EDGE 6 INCHES CRACK IN FIBER. ACCOMPLISHED WORK EO B757 5740-11855-D APPENDIX B.SDR A6WA200940595Skin · corrodedCORROSION ON INTERNAL SURFACE OF LT WING L/E 520ML. CORROSION REMOVED IAW SRM 51-21-06 ON L/E 520ML. (K)SDR FDEA200909183325Skin · corrodedCORROSION - RT UPPER WING SURFACE AT XORS197. REPAIRED IAW EA 1-5710-132215.SDR A6WA200940612Skin · gougedLT WING LWR SKIN GOUGED AFT OF FUEL PANEL 540EB. LT WING LWR SKIN GOUGE BLENDED IAW SRM 51-12-00. NDT C/OUT - NO CRACK FOUND. (K)SDR HALA200909150412Skin · corrodedWING LOWER SKIN TE EXTENSION AT WS 1055 CORROSION, FWD OF FUEL SURGE TANK VENT. REWORK PER SRM 57-20-01/101 TABLE II, & HAL M105 FILE 596112. 35687SDR A6WA200940623Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650CB CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 650CB IAW REO 601R-57-21-030, REV G. (K)SDR A6WA200940614Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650BB. CORRODION ON FUEL ACCESS DOOR CUT-OUT 650BB REPAIRED IAW REO 601R-57-21-030, REV G AND EO E06/012/457 REV "A". (K)SDR A6WA200940615Skin · corrodedCORRODION FOUND ON FUEL TANK ACCESS DOOR CUT-OUT 510AB. ON FUEL TANK ACCESS DOOR CUT-OUT 510AB CORROSION REPAIRED IAW REO 601R-57-21-030 REV G AND EO E06/021/457, REV "A". (K)SDR A6WA200940624Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 650DB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 650DB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A".SDR A6WA200940625Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640BB ON FUEL TANK ACCESS DOOR CUT-OUT 640BB CORROSION REPAIRED IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)SDR A6WA200940616Skin · corrodedLT WING CORROSION FOUND ON FUEL ACCESS DOOR CUT OUT 540EB. ON LT WING, ON FUEL TANK ACCESS DOOR CUT-OUT 540EB CORROSION REPAIRED IAW REO 601R57-21-030, REV G. (K)SDR A6WA200940617Skin · corrodedLT WING CORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550GB. ON LT WING, ON FUEL TANK ACCESS DOOR CUT-OUT 550GB CORROSION REPAIRED IAW REO 601R-57-21-030, REV G. (K)SDR A6WA200940613Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 640AB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 640AB IAW REO 601R-57-21-030, REV G. EO. E06/021/457, REV A. (K)SDR FDEA200909163310Panel · debondedLT WING UPPER INBD FIXED PANEL EXT- SKIN AT RSTA 177.5, PANEL MOUNTING HOLES ELONGATED SKIN BULGING / DISBONDED. ACCOMPLISHED EA F- 5730-131110, THIS REPAIR HAS RECEIVED FIRST STAGE APPROVAL, THE DTA WILL BE TRACKED VIA ENMDS, 24 MONTHS FROM FAA FORM 8100-9SDR A6WA200940628Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550CB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 550CB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)SDR A6WA200940629Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 550DB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 550DB IAW REO 601R-57-21-060, REV G. (K)SDR A6WA200940626Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 540DB. CORROSION ON FUEL ACCESS DOOR CUT-OUT 540DB REMOVED IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV A. (K)SDR A6WA200940627Skin · corrodedCORROSION FOUND ON FUEL ACCESS DOOR CUT-OUT 510BB. CORROSION REMOVED ON FUEL ACCESS DOOR CUT-OUT 510BB IAW REO 601R-57-21-030, REV "G" AND EO E06/021/457, REV "A". (K)SDR HALA200909150409Skin · debondedRIGHT OUTER WING, L/E PANEL P/N 114T2800-300 (ADJACENT L/E SLAT NR 9: DISBOND DAMAGE. REPAIRED PER TECHNICAL INSTRUCTION 190126750-0001 AND HAL105 596119.SDR FDEA200909153300Access Panel · crackedRT WING NR 3 SLAT AREA, STA XOS 464 L/E UPPER ACCESS CUT OUT FOR WING ANTI ICE TELESCOPIC DUCT CRACKED AT 02 CORNERS. REPAIR IAW SRM 57-40-01, FIG 201 REV 41.SDR UIEA200900056Panel · delaminatedRT WING FIXED UPPER L/E PANEL AT ILES 700.72 AND 30.0 INCHES FROM FRONT OF PANEL HAS AN AREA OF A PREVIOUS REPAIR 22.00 BY 15.0 INCHES OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09 SHEET 2 AND 5, PREPREG 250 DEGREES F CURE IAW SRM 51-40-12.SDR USAA2009100592698Panel · delaminatedSAL - C8 - MAJOR REPAIR - DELAMINATION ON RIGHT WING PANEL 640CZ BETWEEN WING RIBS 5 & 6. REPLACED RIGHT WING PANEL 640CZ BETWEEN WING RIBS 5 & 6 IAW A320 AMM 57-27-11.SDR USAA2009100592697Panel · delaminatedSAL - C8 - MAJOR REPAIR - DELAMINATION ON LEFT WING PANEL 540DZ BETWEEN WING RIBS 6 & 6B. REPLACED LEFT WING PANEL 540DZ BETWEEN WING RIBS 6 & 6B IAW A320 AMM 57-27-11.SDR USAA2009100592696Panel · delaminatedSAL - C8 - MAJOR REPAIR - DELAMINATION ON LEFT WING PANEL 540CZ BETWEEN WING RIBS 5 & 6. REPLACED LEFT WING PANEL 540CZ BETWEEN WING RIBS 5 & 6 IAW A320 AMM 57-27-11.
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