JASC 5730
Service difficulty reports · 27,262
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 DALA14033540969Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE NBR 1409C COUNTERSINK AND SETTLEMENT AREA AT RT WING SUMMARY: BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR, PN 3912757, DUE TO THE REDUCED AREA OF THE CONDUCTIVE INTERFACE THEREFORE ACCESS PLATE NR 1409C WAS RSDR FDEA201406021271Skin · crackedPOSSIBLE CRACK LT WING T DUCT CUT OUT UPPER INBD CORNER. PERFORMED HFEC TO VERIFY SUSPECTED CRACK. FOUND POSITIVE INDICATION IAW NTM 23-30-00 PART 6. INSTALLED DOUBLER AND FILLER AND EDGE SEALED IAW EA 8-5710-T0308710 P1 AND SRM 57-40-01 REPAIR 10 FIG.201 SDR FDEA201406021266Skin · crackedFUEL PANEL DOOR CUT OUT HAS A CRACK INDICATION BETWEEN TWO FASTENERS. A .75 INCH BLACK SMOKE LINE & PAINT CHIPPING AWAY IN A STRAIGHT LINE FROM SKIN EDGE. WIPED AWAY, STILL HAS A SLIGHT APPEARANCE OF A CRACK. PERFORMED HFEC INSPECTION IAW NTSPM 06-10-01.SDR FDEA201406021274Skin · crackedLEFT WING REFUELING DOOR OTBD DOOR LAND CRACKED. PERFORMED HFEC TO VERIFY SUSPECTED CRACK. FOUND POSITIVE INDICATION IAW NTM 23-30-00 PART 6. FABRICATED NEW LOWER SECTION OF INNER RIB PER DRAWING ARB 1187. INSTALLED REPAIR PARTS IAW EA 8-5710-T0308715 PASDR FDEA201406021273Skin · wornDISCOVERED WORN AREAS ON FIXED LE SKIN INBD & OTBD OF LT NR 15 SLAT TRACK. BLENDED WORN AREASIAW SRM 57-10-00 FIG 37.SDR FDEA201406021272Skin · crackedLEFT WING POSSIBLE SKIN CRACKED NR 10 TRACK CUT OUT LWR SURFACE. PERFORMED HFEC TO VERIFY SUSPECTED CRACK. FOUND POSITIVE INDICATION IAW NTM 23-30-00 PART 6. INSTALLED REPAIR DOUBLER AND FILLER IAW EA 8-5710-T0308676.SDR FDEA201406021270Skin · crackedPOSSIBLE CRACK ON LT WING FIRE BOTTLE DOOR INBD. CRACK VERIFIED IN LT WING LE FIRE BOTTLE ACCESS DOOR IAW NDT SPM PT 6. INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-10-00 VOL 1 FIG 68 AND EA 8-5730-T0308636.SDR FDEA201406021269Skin · crackedPOSSIBLE CRACK ON LT WING INBD SLAT CUT OUT, BOTH CORNERS. PERFORMED HFEC OF AREA IAW NTM 51-10-08 BLOCK 601, TWO CRACK INDICATIONS. REPAIRED AREAS, INSTALLED FILLERS AND DOUBLER IAW EA 6-5730-T0308606.SDR FDEA201406021268Skin · crackedPOSSIBLE CRACK RT WING SLAT CUT OUT SEVEN INCHES FROM WING TIP. VERIFIED CRACK IN RT WING SLAT CUT OUT WITH HFEC IAW NDT SPM PT 6, CRACK APPROX 3/4 INCH LENGTH. CUT OUT CRACK IAW SRM 57-10-00. PERFORMED HFEC INSPECTION TO CUT OUT IAW NDT SPM PT 6, NO DEFESDR FDEA201406021265Skin · crackedCRACK IN RT WING SKIN BETWEEN SLAT 5 & 6 AT SLAT TRACK 12. PERFORMED HFEC INSPECTION. HFEC SHOWS POSITIVE INDICATION IAW 20-30-00 PART 6. INSTALLED DOUBLER AND FILLER IAW SRM 57-10-00 FIG 68.SDR AALA20140602003Skin · corrodedCORROSION FOUND ON FUEL TANK SKIN. ACCOMPLISHED REPAIR IAW EA B737-57-034887.SDR AALA20140602001Skin · corrodedCORROSION FOUND ON RT CTR FUEL TANK SKIN AROUND DRAG BRACE. ACCOMPLISHED REPAIR IAW EA B737-57-034887.SDR DALA14033530969Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE NRS 1454C AND 1436C AT LT WING, MRB 5732-083, SM. CORROSION ON COUNTERSINKS AT FUEL ACCESS PLATE NR 1454C WAS REMOVED AND MAXIMUM DIAMETER ALLOWABLE IS 0.532" ND WERE FOUND 4 COUNTERSINKS ADJACENTS OUT OF LIMITS, MEASURED 0.55SDR FDEA201406021264Skin · crackedRIGHT WING LE IS CRACKED BETWEEN NR 4 & NR 5 LE SLATS. REMOVED ACCESS PNL AFT OF CRACK. PNL IN COURIER AREA. REMOVED EXISTING FASTENERS & CUT OUT DAMAGE AREA IAW SRM 57-10-00 FIG 68 SHEET 1. COMPLIED WITH HFEC OF CUT OUT AREA IAW NDT SPM PART 6 20-30-00, NOSDR DALA2014062503751Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL NR 1414C. CORROSION REMOVED IAW SRM 51-22-2A. FOUND OUT OF LIMITS IAW SRM 51-22-2A. ACCESS PANEL REPLACED.SDR DALA2014062503750Access Panel · corrodedCORROSION ON ACCESS PANEL NR 1456C. CORROSION REMOVED IAW SRM 51-22-2A AND FOUND OUT OF LIMITS IAW SRM. ACCESS PANEL REPLACED.SDR SWAA2014060428703Fairing · crackedLEFT WING NR 3 CANOE FAIRING CRACKED ON INSIDE 12 INCHES FWD OF HORSE SHOE FITTING. REPAIRED FAIRING IAW EA.SDR DALA14033470963Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE NR 1355C AT SETTLEMENT AREA AND COUNTERSINK HOLES IN REF CARD 42, ZONE 00. CORROSION ON COUNTERSINK HOLES ON SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A COUNTERSINK HOLES WERE MEASURED MAX DIAMETER IS .532" NAD MAX DIAMETER MESDR DALA14033460963Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE NR 1470 AT COUNTERSINK HOLES AND SETTLEMENT AREA, AYP, IN REF CARD 41, ZONE 00, MRB 57-083-02, H1L1-AYP, CARD 82, ZONE 00. CORROSION ON FUEL ACCESS PLATE NBI 1470 ON COUNTERSINK HOLES AND SETTLEMENT AREA WERE REMOVED IAW SRM 51-SDR DALA14033450963Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE NR 1307C AT COUNTERSINK HOLES SETTLEMENT AREA (AYP) IN REF CARD 42, ZONE 00, MBR 57-083-02, H1L1-AYP, CARD78, ZONE 00. CORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A. COUNTERSONK HOLES WERE MEASSDR FDEA201406011247Skin · crackedLEFT WING NR 12 SLAT TRACK CUT OUT HAS EVIDENCE OF CRACK. LT WING NR 12 SLAT CUT OUT NEEDS NDT VERIFICATION. VERIFIED & MARKED THE END OF THE CRACK WITH HFEC IAW NDT SPM PART 6, 06-00-06. REMOVED FASTENERS FROM NR 12 SLAT TRACK CUT OUT AREA, TO FACILITATE ISDR FDEA201406011246Skin · crackedAPPEARS TO BE A CRACK IN RADIUS ON LT INBD FUELING PNL. PERFORMED HFEC INSP ON NEW CUT OUT IAW NTM PT 6, NO CRACK INDICATION FOUND. FABRICATED REPAIR DOUBLER & FILLERS FROM PREVIOUSLY VERIFIED MATERIAL IAW SRM 57-10-00. MX REQUEST OK TO INSTALL REPAIR PARTSSDR FDEA201406011245Skin · crackedON PRE-FLIGHT INSP SUSPECT CRACK RT WING LE PANEL INBD RADIUS OF SLAT DRIVE MECHANISM DOOR CUT OUT. VERIFIED AREA TO BE CRACKED IAW NDT SPM PART 6. CRACK IS MARKED WITH PERMANENT MARKER. CUT OUT DAMAGE IAW SRM 57-40-02. NEED NDT TO INSPECT FOR DAMAGE REMSDR FDEA201406011244Skin · crackedNUMBER 7 SLAT CUT OUT HAS CRACK INDICATION HAD A 1 INCH BLACK SMOKE LINE. WIPED AWAY, STILL HAS A SLIGHT APPEARANCE OF A CRACK. REMOVED DAMAGED SKIN USING .5" RADIUS IAW SRM 57-10-00 VOLUME 1 FIGURE 68. PERFORMED HFEC OF THE CUT OUT AREA IAW NDT SPM PART 6,SDR FDEA201405302090Skin · crackedRIGHT WING XOS -464 CORNER OF ANTI-ICE TUBE CUT OUT UPPER INBD HAS A .5 INCH CRACK TRAVELS FROM CORNER TO SCREW, VERIFIED END OF CRACK. REPAIRED ANTI-ICE TUBE CUT OUT ON LE OF RT WING IAW SRM 57-40-01. REFER TO EA 8-5720-T0308578 PART 1.SDR FDEA201405301230Skin · crackedON WALK AROUND FOUND POSSIBLE CRACK ON LT WING AT FWD INBD CORNER OF FUEL PNL. CONFIRMED CRACK AT FWD INBD CORNER OF FUEL PNL BY HFEC INSPECTION IAW NDTSPM PT 6. CRACK TERMINATES AT RIVET. STARTED REMOVING DOOR TO ASSIST SHEET METAL. FINISHED REMOVING LT WSDR 7AHR201405307372Skin · corrodedRT WING UPPER SKIN AT FRONT SPAR BETWEEN WS475 & WS531 HAS CORROSION. REPAIRED IAW DWG 57-13172-1.SDR 7AHR201405307369Skin · corrodedRIGHT WING UPPER SKIN HAS CORRROSION BETWEEN WS479 & WS505 AT S-11. REPAIRED IAW DWG 57-13169-1.SDR 7AHR201405307374Skin · corrodedRIGHT WING UPPER SKIN AT REAR SPAR AREA HAS CORROSION BETWEEN WS315 & WS370. REPAIRED IAW DWG 57-13174-1.SDR 7AHR201405307373Skin · corrodedRIGHT WING UPPER SKIN HAS CORROSION AT FRONT SPAR BETWEEN WS315 & WS375. REPAIRED IAW DWG 57-13173-1.SDR 7AHR201405307392Skin · damagedRT WING UPPER SKIN BLENDOUTS BETWEEN WS270 & WS583.SDR ASOA2014070110793Skin · damagedLOWER WING SKIN BURNED WS 21.4. REPAIRED IAW EC/TC REO 670-57-00-053. MAJOR REPAIR.SDR FDEA201405271199Skin · crackedDURING INSPECTION, THE RT WING FIXED LE FOUND A 1/2 INCH CRACK AT THE NR 2 SLAT TELESCOPING ANTI-ICE DUCT CUT OUT, UPPER OTBD RADIUS. PERFORMED HFEC ON RT WING, AT SUSPECTED CRACK LOCATION TO VERIFY CRACK IAW NTM PT 6. IAW SHEET METAL REQUEST, REMOVED RT WINSDR FDEA201405271203Skin · crackedFOUND CRACK ON RT WING AT OTBD SLAT TRACK CUT OUT FOR NR 6 SLAT. VERIFIED BY NDT. REMOVED LWR RT WING PANEL 626EB & PLACED IN COURIER COMPARTMENT. REMOVED DAMAGED SKIN IAW SRM 57-40-02 REPAIR 7 FIGURE 201. PERFORMED HFEC OF CUT OUT AREA IAW NTM PT 6. NO SDR FDEA201405271202Skin · crackedFOUND POSSIBLE CRACK ON LT WING AT INBD SIDE OF PRESS REFUEL DOOR, NDT NOTIFIED. LT WING LE LWR CRACK AREA, HFEC INSPECTION OF SUSPECT CRACK AREA, COMPLIED WITH & CONFIRMED CRACK IAW NTM 06-00-06. CUT OUT CRACK IAW 57-40-02. PERFORMED HFEC OF CUT OUT AREA IASDR FDEA201405271200Skin · crackedON WALK AROUND FOUND A CRACK AT LT WING FUELING DOOR INBD SIDE. LT WING LWR LE CRACK VERIFICATION, PERFORMED HFEC OF SUSPECT CRACK AREA, CONFIRMED CRACK. CRACK ENDS AT RIVET HOLE. LT WING REFUEL & DEFUEL PANEL HAS BEEN REMOVED IAW SMP & PLACED IN THE COUSDR FDEA201405271198Skin · crackedPOSSIBLE CRACK FOUND ON LT WING AFT BOTTOM SIDE SKIN BY NR 1 SLAT CTR TRACK PANEL. SLATS EXTENDED FOR SHEET METAL REPAIR ACCESS, CB FOR AUX PUMPS ON BACK WALL PULLED & COLLARED. PERFORMED HFEC TO VERIFY CRACK IAW NTM PT 6. REMOVED THE NR 1 SLAT IAW MM 27-8SDR DALA14032240963Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE NR 1466C AT SETTLEMENT AREA AND COUNTERSINK HOLES IN REF CARD 41, ZONE 00, MRB 57-083-02, CORROSION ON COUNTERSINK HOLES ON SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A. CONTERSINK HOLES WERE MEASURED AND, MAX DIAMETER ALLOWABLESDR DALA14032230963Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE NR 1436C AT SETTLEMENT AREA AND COUNTERSINK HOLES IN REF CARD 41, ZONE 00, MRB 57-083-02, H1L1 -AYP. CORROSION ON COUNTERSINK HOLES ON SETTLEMENT AREA WERE REMOVED IAW SRM 51-22-2A. CONTERSINK HOLES WERE MEASURED AND MAX DIAMETESDR FDEA201405261197Skin · crackedDURING SERVICE CHECK FOUND POSSIBLE CRACK AT SLAT DRIVE MECH DOOR FWD INBD CORNER RT WING. PERFORMED HFEC, ON RT WING AT SLAT DRIVE MECH DOOR FWD INBD CORNER, TO VERIFY CRACK IAW NTM PT 6. TWO EACH CRACKS VERIFIED IN AREA. CUT OUT CRACK IAW SRM 57-10-00 CRSDR FDEA201405261193Skin · crackedON WALK AROUND FOUND SUSPECTED CRACK ON RIGHT WING INBD CORNER OF FUEL PANEL ON LOWER WING. COMPLIED WITH HFEC INSPECTION OF ABOVE NOTED AREA IAW SPM 06-10-01.001 CRACK NOTED. RUNNING FROM CORNER OUT PAST FIRST RIVET TO SECOND RIVET APPROXIMATELY 2 1/2 INCHESDR FDEA201405261191Skin · crackedON WALK AROUND FOUND POSSIBLE CRACK ON LT WING AT FUELING PANEL FWD INBD CORNER. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6. TRIMED OUT CRACK AREA IAW SRM 57-40-02 REPAIR 7 FIG 202. PERFORMED HFEC OF DAMAGE CUT OUT IAW NTSPM 06-10-01.001. INSTALLEDSDR SWAA2014052728358Skin · crackedRIGHT WING LE CRACKED AT NR 5 SLAT OTBD AUXILIARY TRACK CUT OUT CRACKED. REPAIRED CUT OUT IAW SRM.SDR COEA2014061709917Skin · corrodedRIGHT WING LANDING PANEL 622CT HAS LEVEL 1 FRETTING CORROSION. REPAIR IAW SRAS SO & TS-4504 08 888 6/17/2014.SDR COEA2014061708917Skin · corrodedLEFT WING PANEL LANDING 521DT HAS LEVEL 1 FRETTING CORROSION. REPAIR IAW SRAS SO & TS-4504 08 4888 6/17/2014.SDR COEA2014061707917Skin · corrodedLEFT WING PANEL LANDING FOR 522CT HAS LEVEL 1 FRETTING CORROSION. IAW SRAS DO TS-4504 08 4888 6/17/2014.SDR REXA2014052700097Skin · corrodedRIGHT WING FUEL PANEL ACCESS LANDING AT WS 12.245 CORRODED 0.015 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.SDR SWAA2014060628758Panel · delaminatedRIGHT WING PANEL 621MB CORNER DELAMINATED. REPAIRED PANEL IAW SRM.SDR 7AHR201405292260Skin · corrodedLEFT WING UPPER T/E PANEL HAS CORROSION AT APPROXIMATELY WS 434 & 450. CORROSION REMOVAL EXCEEDED THE LIMITS AND WITH FURTHER INSPECTION FOUND UPPER SKIN ON PANEL WAS ALSO DELAMINATED. REMOVED DELAMINATED SKIN IAW SRM 51-70-02 WHICH WAS ALSO OUT OF LIMITS. SDR FDEA201405231147Skin · crackedPOSSIBLE CRACK ON RT WING LOWER SLAT TRACK PANEL BETWEEN NR 5 & 6 SLAT, MARKED WITH TAPE. INSPECTION WILL VERIFY IF IT IS CRACKED. INSTALLED DOUBLER & FILLER IAW SRM 57-40-02.
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