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 CA061101002Clamp · burned(CAN) ELECTRICAL ARC BURN MARKS FOUND ON THE REAR FACE OF NUTPLATES (QTY 17) FOR THE WING FUEL TANK ACCESS DOORS. AS PER THE TECHNICAL RECORDS THERE WERE TWO REPORTED LIGHTNING STRIKES ON THIS AIRCRAFT SINCE NOVEMBER 09/2005. THE BURN MARKS ARE A LIKELY INDICSDR 06FDEA03807Skin · damagedRT WING I/B FLAP L/E SKIN EXISTING REPAIR. REPAIR CARRIED OUT AT RT WING I/B FLAP L/E SKIN AS PER FEDEX EA NR 1- 5750-104818,TITLE: "WINGS, FLIGHT CONTROLS, I/B RT TRAILING EDGE FLAP. PERMANENT REPAIR, EA 1-5750-102907". REPAIR CLASSIFIED AS MINOR AS PER GMSDR ASMF200610013Panel · leakingDURING TRANSIT CHECK, CAPTAIN REPORTED A FUEL LEAK ON THE RT WING. DURING MAINTENANCE CHECK, A LEAK WAS DETECTED IN THE RT WING UPPER PANEL. TWO NUTS WERE REPLACED IAW SRM 51-30-2 AND PANEL WAS SEALED AGAIN, TESTED CORRECT.SDR QXEA200602911Skin · corrodedC3 YYC - RIGHT WING FUEL TANK BOTTOM SKIN ACCESS PANEL REBATE HAS FRETTING CORROSION AT INBOARD AND OUTBOARD END OF ACCESS OPENING AT WS 70 AND WS 88. REPAIRED IAW REO670-57-00-025.SDR QXEA200602909Skin · corrodedC3 YYC - RIGHT WING FUEL TANK BOTTOM SKIN ACCESS HOLE REBATE AT WS 96 HAS LIGHT FRETTING CORROSION ON MATING SURFACE OF PANEL. REPAIRED IAW REO670-57-00-025.SDR QXEA200602908Skin · corrodedC3 YYC - RIGHT WING FUEL TANK BOTTOM SKIN ACCESS HOLE REBATE AT WS 45 HAS LIGHT FRETTING CORROSION ON MATING SURFACE OF PANEL. REPAIRED IAW REO670-57-00-025.SDR QXEA200602907Skin · corrodedC3 YYC - RIGHT WING FUEL TANK BOTTOM SKIN ACCESS HOLE REBATE AT WS 24 HAS LIGHT FRETTING CORROSION ON MATING SURFACE OF PANEL. REPAIRED IAW REO670-57-00-025.SDR QXEA200602906Access Panel · corrodedC3 YYC - RIGHT FUEL TANK ACCESS PANEL 641 BB HAS FRETTING CORROSION ON MATING SURFACE OF PANEL. REPAIRED IAW REO670-57-12-003.SDR SWAA064144Skin · corrodedDURING SCHEDULED SPV CHECK, FOUND LT WING UPPER SKIN CORRODED AT WING STA 75, STR 7. REPAIRED SKIN PER ER.SDR MWEA060282Skin · corrodedFOUND CORROSION ON CENTER FUEL TANK UPPER SURFACE AT FRAME STATION 835 X+58, Z-8.SDR 06FDEA03780Skin · misrepairedRT WING L/E SKIN AT NR 13 CUT OUT SLAT TRACK LOWER AREA, EXISTING DOUBLER REPAIR XOS 832. RT WING L/E SKIN AT NR 13 LOWER SLAT TRACK AT XOS 832 REMOVED NON CONFORMING REPAIR AND REPLACED WITH DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1. FAB PART IAW DETAIL PART TRSDR 2006UALA02051Skin · damagedLT WING LOWER SKIN FUEL PLATE 540HB FASTENER HOLE DAMAGED. PERMANENT REPAIR ACCOMPLISHED PER EVA 60643.SDR 2006UALA02050Skin · damagedRT WING LOWER SKIN FUEL PLATE 640PB CUT OUT FASTENER DAMAGED. PERMANENT REPAIR ACCOMPLISHED PER EVA 60643. MAJOR REPAIR REPORTED BECAUSE A REPAIR WAS ACCOMPLISHED ON A PRINCIPLE STRUCTURAL ELEMENT.SDR 06FDEA03762Skin · crackedRT WING CUTOUT SKIN AT SLAT TRACK STA XOS 550 LOWER AREA, EXISTING DOUBLER REPAIR. EXISTING DOUBLER REPAIR REMOVED, AREA ASSESSED. CRACK TRIMMED OUT AND FILLER MANUFACTURED. NEW DOUBLER FABRICATED AND FITTED IAW SRM 57-10-00 FIG 68 VOL 1 PAGE 215. EDGES OFSDR QXEA200602902Rivet · looseC3 YYC - THERE ARE TWO SMOKING RIVETS ON THE LEFT WING TOP SKIN AT STATION 165 JUST INBOARD OF THE SPOILER. REPAIRED IAW SRM 51-42-06.SDR QXEA200602901Skin · scratchedC3 YYC - LEFT WING LOWER SKIN HAS A SMALL SCRATCH JUST FORWARD OF THE OUTBOARD END OF THE OUTBOARD FLAP. REPAIRED IAW SRM 51-12-00.SDR 06FDEA03726Skin · crackedLT WING TELESCOPIC DUCT CUTOUT UPPER O/B CORNER FOUND CRACKED AS MARKED. LT WING TELESCOPIC DUCT CUTOUT UPPER O/B CORNER CRACK REPAIRED AS PER EA 1-5740- 104739, WING- LEADING EDGE AND LEADING EDGE DEVICES- LEFT- HEAD FIX LEADING EDGE SKIN REPAIR XORS= SDR 06FDEA03725Skin · crackedLT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER FOUND CRACKED AS MARKED. LT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER CRACK REPAIRED AS PER EA# 1-5740- 104739, WING- LEADING EDGE AND LEADING EDGE DEVICES- LEFT- HEAD FIX LEADING EDGE SKIN REPAIR XORS= SDR 06FDEA03723Skin · crackedRT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER FOUND CRACKED AS MARKED. RT WING TELESCOPIC DUCT CUTOUT UPPER I/B CORNER CRACK REPAIRED AS PER EA 1-5740- 104740, LEADING EDGE AND LEADING EDGE DEVICES- RIGHT HAND FIX LEADING EDGE SKIN REPAIR XORS=464.00 THRSDR 06FDEA03722Access Panel · crackedRT WING LOWER L/E ACCESS PANEL NR 626FB I/B FLANGE FOUND CRACKED BETWEEN NR 14 AND NR 15 SLAT TRACK. REPAIRED AS PER SRM 57-10-00 FIG 18 VOL I. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03721Access Panel · crackedLT WING LOWER L/E ACCESS PANEL NR 526FB I/B FLANGE FOUND CRACKED BETWEEN NR 14 AND NR 15 SLAT TRACK. LT WING LOWER L/E CRACK AT ACCESS PANEL 526 FB I/B FLANGE BETWEEN NR 14 AND 15 SLAT TRACK REPAIRED AS PER SRM 57-10-00 FIG 18 VOL I. THIS REPAIR CLASSIFIED SDR 06FDEA03712Skin · crackedLT WING ON L/E DROP FOUND 1 CRACK .050" LONG ON SKIN UPPER SURFACE AT STA XW 320 AFTER REMOVE PLATE ( REMOVED PART AND SEE NRC N00169 ). SKIN REPAIRED WITH DOUBLER IAW SRM 57-10-00 FIG 55 SHT 1 AND 2 VOL 1. SEE DETAILED PARTS TRAVELER N01887/ F171887.SDR 06FDEA03651Skin · unknownRT WING DROOP L/E UPPER SURFACE O/B TOP CORNER FOUND WITH EXISTING DOUBLER REPAIR. RT WING DROOP L/E UPPER O/B TOP CORNER EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 VOL II AND AREA REPAIRED AS PER SRM 57-10-00 FIG 26 VOL I. THIS REPAIR CLASSIFIED ASSDR QXEA200602896Skin Panel · gougedC3 YYC - RIGHT WING WS 128 LEADING EDGE SKIN PANEL HAS A GOUGE AT LEADING EDGE NEXT TO EDGE OF SKIN. REPAIRED IAW SRM 57-40-01, 51-25-01.SDR QXEA200602894Skin · gougedC3 YYC - LEFT WING LEADING EDGE, WS 108, LEADING EDGE SKIN PANEL HAS A GOUGE AT EDGE OF CUTOUT FOR NR 1-2 SLAT TRACK. REPAIRED IAW SRM 57-41-01, 51-25-01.SDR QXEA200602893Skin · gougedC3 YYC - LEFT WING LEADING EDGE, WS 180, LEADING EDGE SKIN HAS GOUGES ON UPPER LEADING EDGE SURFACE. REPAIRED IAW SRM 51-12-00, 51-25-06, AND 51-25-16.SDR UPS06848399Skin · crackedINSPECTION TYPE:C2 PANEL LANDING FOR ACCESS PNL 505F IS CRACKED. REPAIRED PNL LANDING FOR ACCESS PNL 505F IAW SAA EA NR 008-5710-01- A0505, UPS RAA NR DC8-57-20194, BAC MSG NR 1-237786953, AND FAA FORM 8100-9SDR UPS06848349Access Panel · crackedCRACK FOUND ON ACCESS PANEL LANDING L/CENTER TANK ACCESS HOLE 516 REPAIRED DAMAGED AT LT CENTER TANK ACCESS HOLE 516 IAW SAA EA NR 008-5730-01-A0493, UPS EO DC8-5730-25433-A, BAC MSG NR 1-237497515-1, BAC MSG 1-237497515-2, AND FAA FORM 8100-9SDR 06FDEA03642Skin · chafedCHAFE MARK FOUND AT LT WING FIXED LE BOTTOM CORNER NEXT TO DROOP LE INBD EDGE (P/N ARB2434-1). NEW SKIN INSTALLED AS PER SRM 51-35-01 VOL2 AND SRM 51-33-01 VOL2 (MAJOR REPAIR).SDR UPS06448674Skin · corrodedINSPECTION TYPE:C RIGHT WING L/E CAVITY LWR EXTENSION SKIN FOUND CORRODED AT WS 1540 JUST BEHIND NR 26 VC FLAP. CORROSION BLEND OUT 0.053" X 1" X 2" EXCEED SRM LIMIT. RIGHT WING L/E CAVITY LWR EXTENSION SKIN AT WS 1512 AREA REPAIR PER RS R57-26-25675 AND UPSSDR UPS06448624Skin · corrodedINSPECTION TYPE:C RIGHT WING L/E CAVITY LOWER EXTENSION SKIN FOUND CORROSION AT WS 1400 JUST BELOW NR 1 L/E FLAP PDU. CORROSION BLEND OUT 0.103" X 7/8" X 1.5" EXCEED SRM LIMIT. RIGHT WING L/E LOWER EXTENSION SKIN AT WS 1400 REPAIRED AS PER SRM 57-30-03 FIG 4SDR 06FDEA03625Skin · damagedLEFT WING LOWER SURFACE PANEL 550NB PANEL LAND HAS ONE EA DRILL START NEXT TO HOLE COMPLIED WITH EA 6-5730-104975, OPENED HOLE TO 0.402, COLD WORKED AND FINAL REAMED TO 0.418. FABBED AND INSTALLED BUSHING AND DRILLED NEW HOLE IAW TD/J1/S1/03541/2006.SDR CA061013004Skin · damaged(CAN) A MAINTENANCE FACILITY RECEIVED THESE RE-LIFED WINGS FROM RW MARTIN. INCOMING INSPECTION REVEALED A LT/RT BUCKLED TOP SKIN AND DAMAGED SHROUD SKINS. THE DAMAGE DOES NOT APPEAR TO BE SHIPPING RELATED. RW MARTIN WERE NOT ABLE TO SEND AN NDT REPORT FOR DELASDR CA061013003Skin · damaged(CAN) A MAINTENANCE FACILITY RECEIVED THESE RE-LIFED WINGS FROM RW MARTIN. INCOMING INSPECTION REVEALED A LT/RT BUCKLED TOP SKIN AND DAMAGED SHROUD SKINS. THE DAMAGE DOES NOT APPEAR TO BE SHIPPING RELATED. RW MARTIN WERE NOT ABLE TO SEND AN NDT REPORT FOR DELSDR QXEA200602699Access Panel · chafedLT UPPER WING ACCESS PANEL CUTOUT, TOP SURFACE OF LADDER PLATE HAS CHAFE DAMAGES. REPAIRED IAW RD8-57-3486.SDR QXEA200602701Panel · fodC4 YYC - RIGHT WING UPPER TANK PANEL 622AT BOTTOM EDGE OF PANEL DAMAGED BY FOREIGN OBJECT AT YN52 AND REBATE ON WING ALSO DAMAGE AT SAME LOCATION. REPAIRED IAW RD8-57-3485.SDR 06FDEA03583Access Panel · crackedLEFT WING 519CB LT LEADING ACCESS PANEL FWD INBD CUTOUT FOUND CRACK. REPAIR CARRIED OUT AT LEFT WING 519CB LT LEADING ACCESS PANEL FWD INBD CUTOUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 06FDEA03579Doubler · chafedRT WING O/B OF NR 3 ENGINE L/E DOUBLER IS CHAFED. REMOVED CHAFED DOUBLER IAW DC/MD10 SRM 51-35-01 VOL II MAT. ID FOR NEW DOUBLER 7075-T6 - .050 PO 543347.6 AND FABRICATED IAW DC/MD10 SRM 57-10-00 FIG 40 VOL 1. ALODINED AND PRIMED IAW DC/MD10 SRM 51-21-01 PG SDR 06FDEA03551Skin · crackedRIGHT WING, FIXED LEADING EDGE SKIN AT NR 14 TRACK CUTOUT FOUND CRACKED. CUTOUT TRIMMED OUT AS PER SRM 57-10-00 FIGURE 21 VOLUME I. REPAIR DOUBLER AND FILLER FABRICATED AS PER SRM 57- 10-00 FIGURE 21 VOLUME I AND INSTALLED AS PER SRM 51-33-01 VOLUME II. RESDR QXEA200602700Access Panel · chafedLT WING UPPER ACCESS PANEL 523AT HAS CHAFE DAMAGE ON MATING SURFACE. REPAIRED IAW RD8-57-684.SDR HALA0600784Panel · missingFOUND LUBE PANEL 521 AAB LT WING L/E MISSING. REPLACED LE LUBE PANEL NR 521 AAB LT WING SECURITY CHECK OK.SDR 06FDEA03546Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 765 FOUND CRACKED. CRACKED BEADED DOUBLER ON RIGHT HAND WING FIXED LEADING EDGE AT XOS 698 REPAIRED AS PER FEDEX E.A. 1-5730-104794, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03545Doubler · crackedRIGHT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 730 FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104794.SDR 06FDEA03544Skin · crackedRIGHT WING, FIXED LEADING EDGE AT TELESCOPIC DUCT CUTOUT SKIN CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104793.SDR 06FDEA03527Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT STA XOS 623 TO 627 FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104791.SDR 06FDEA03526Doubler · crackedLEFT WING LEADING EDGE BEADED DOUBLER AT STA XOS 630 TO 634 FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104791.SDR SIMA200629201Skin · damagedAIRCRAFT LIGHTNING STRIKE. ACCOMPLISHED LIGHTNING STRIKE INSPECTION IAW AMERICAN EAGLE WORK CARD 05-200-00. REPAIRED RIGHT TRAILING EDGE OF WING TIP IAW 51-21-07 WORK CARD 05-200-00. REPAIRED RIGHT TRAILING EDGE OF WING TIP IAW 51-21-07. RETURNED AIRCRAFT SDR QXEA200602678Skin · damagedC4 YYC - LEFT WING UPPER SKIN STATION YW 261.0 OUTBOARD END OF BARE ALUMINUM LIGHTNING STRIP HAS ONE SMOKING RIVET. REPAIRED IAW SRM 51-40-11.SDR CA070131006Skin · cracked(CAN) 2 CRACKS WERE DETECTED ON THE WING SKIN JUST UNDER THE LEADING EDGE ON BOTH WINGS. THE WING ATTACHMENT FITTINGS OF THE AIRCRAFT WERE INSPECTED AND NO FURTHER CRACKS WERE DISCOVERED. THE WINGS WERE REMOVED TO CONDUCT A MORE DETAILED EXAMINATION AND THE ASDR 06FDEA03471Skin · crackedLEFT WING ANTI-ICING TELESCOPIC DUCT DOOR CUT OUT BOTH CORNER FOUND CRACKED. REPAIRED AS PER FEDEX E.A. 1-5730-104789.
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