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 SWAA2015040238067Skin Panel · crackedRIGHT WING UPPER SURFACE FIXED TE PANEL JUST INBD OF NR 7 SPOILER MIDDLE ATTACH RIB FWD LOWER FASTENER HOLE CRACKED. R & R PANEL IAW DWG & SRM.SDR SWAA2015032637894Skin · delaminatedLEFT WING NR 4 CANOE FAIRING SKIN DELAMINATED ON FWD LE SIDE. REPAIRED SKIN IAW SRM.SDR MASA2015032412973Skin · dentedDENT FOUND ON LT SIDE WING FIXED L/E SS57.16. REPAIRED.SDR FXGA201503151512Skin · chafedCHAFED WING SKIN AT WS 297R, STRINGER 26R. TO REPAIR CHAFING, CAUSED BY A FAIRING, BEAVER TAIL, RUBBING AGAINST THE LOWER WING SKIN AT WS 297R, STRINGER 26R. CUT OUT DAMAGED AREA & INSTALLED AN EXTERNAL REPAIR DOUBLER IAW SRM AN 01-40NL-3 FIGURE 2-62.SDR COEA2015032306805Skin · corrodedHEAVY CHECK MAJOR REPAIR. LT UPPER WING PANEL LANDING 522CT HAS FRETTING. REPAIR IAW SRAS DO TS 1529 05 3169 ISSUE E DATED 4 17 15.SDR COEA2015032305805Skin · corrodedHEAVY CHECK MAJOR REPAIR. RT UPPER WING PANEL LANDING 622CT HAS FRETTING & TOOLING DAMAGE. REPAIR IAW SRAS DO TS 1529 05 3169 ISSUE E DATED 4 17 15.SDR FDEA201503231064Doubler · crackedRIGHT WING LE CAVITY AT STATION XOS 789 DOUBLER CRACKED. DOUBLER FABRICATED IAW DWG ARB3954 REVISION K. CRACKED EXISTING DOUBLER R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201503231063Doubler · crackedRIGHT WING LE CAVITY AT STATION XOS 667 DOUBLER CRACKED. FABRICATED IAW DWG ARB3954 REVISION K. R & R WITH NEW FABRICATED DOUBLER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR SWAA2015033037938Panel · crackedLEFT WING OTBD FIXED TE PANEL, CTR RIB, FWD FLANGE CRACKED. R & R PANEL IAW SRM.SDR DALA2015032402325Access Panel · corrodedCORROSION ON HOLE COUNTERSINKS AND FAYING SURFACE AT LT FUEL TANK ACCESS PANEL 1307C. CORROSION FOUND TO BE OUT OF LIMITS. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.SDR DALA2015032202313Skin · crackedWHILE PERFORMING BHEC, FOUND FASTENER HOLE NR 1 STILL CRACKED AT .282 OF GROUP "A" FASTENER HOLES, LT WING LOWER SKIN AT L 9.5. C/W 5724-01010-05.SDR DALA2016102807838Access Panel · corrodedCORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520QB. REPLACED THE ACCESS PANEL.SDR DALA2016041402903Skin · damagedREMOVED RT WINGTIP ASSY IAW AMM 57-20. REPLACED RT WING TIP ASSY IAW AMM 57-20-02. OPS CHECKED GOOD. COMPLIED WITH ER/A 534223-14, REV ORIGINAL.SDR DALA2015032102312Skin · crackedWHILE PERFORMING BHEC, FOUND FASTENER HOLE NR 1 STILL CRACKED AT .282 OF GROUP "A" FASTENER HOLES, RT WING LOWER SKIN AT L 9.5. C/W AMDS CARD 5724-01010-06.SDR DALA2016102807839Access Panel · corrodedCORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620AT. REPLACED THE ACCESS PANEL.SDR ASOA2015041012591Skin · crackedRIGHT SIDE WING, AT 148.019 IS CRACKED ON AFT PLANK, PROXIMITY .102. COMPLIED WITH ECTC REO 601R-57-21-130-01 AND REO 601R-57-21-130-01, REV K DATED 11/27/2013 AS WRITTEN. INSTALLED RT WING -9 REPAIR STRAP AT WS148.019, REF SRM 51-42-21 AND REO 601R-57-21-13SDR IPXA2015032487363Skin · crackedINSPECTION TYPE:3C, RT WING FIXED L/E EXTERIOR SKIN CRACKED NEAR SLAT TRACK 12 CUTOUT, XOS 774. REPAIRED RT WING L/E SKIN BETWEEN X0S 768-783 IAW SRM 57-40-02, REPAIR 7, FIG 201.SDR IPXA2015032487358Doubler · crackedINSPECTION TYPE:3C, RT WING FIXED L/E PANEL LANDING DOUBLER CRACKED NEAR REFUELING PANEL. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PANEL LANDING DOUBLER IAW DWG ARB2933, SRM 51-31-01, 51-33-01.SDR CALA2015032093443Panel · damagedRIGHT WING FUEL PANEL 640MB LANDING HAS AN ELONGATED SCREW HOLE AFT SIDE 1ST HOLE OTBD OF CTR LINE. REPAIRED SCREW HOLE IAW REO-L18752 REV IR & UAL ECRA 5720 636. THIS REPAIR HAS BEEN APPROVED AS CAT B PERMANENT REPAIR & TO ACP INITIAL INSPECTION IAW PART 2 OSDR DALA2016102807844Access Panel · corrodedCORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520GB. REPLACED THE ACCESS PANEL.SDR DALA2016102807843Access Panel · corrodedCORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520DB. REPLACED THE ACCESS PANEL.SDR DALA2016102807842Access Panel · corrodedCORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620DT. REPLACED THE ACCESS PANEL.SDR DALA2016102807841Access Panel · corrodedCORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 620CB. REPLACED THE ACCESS PANEL.SDR DALA2016102807840Access Panel · corrodedCORROSION ON COUNTERSINK OF THE FUEL ACCESS PANEL 520DT. REPLACED THE ACCESS PANEL.SDR SWAA2015042939106Skin · crackedLEFT WING FIXED LE SKIN CRACKED AT STATION 208. REPAIRED SKIN IAW EA.SDR JJBA20150317015Skin Panel · damagedPERMANENT REPAIR FOR DENT & GOUGE DAMAGE ON LT LOWER OTBD WING SKIN PANEL ASSEMBLY, PN 5710016 BETWEEN STATIONS Y440.00 - YW457.00 & BETWEEN STRINGERS 14A - 1S.SDR HYIA20150320001Skin · corrodedDURING INSPECTION A LOWER WING FUEL LEAK WAS DISCOVERED. THE REPAIR TO THE LOWER WING CONSTITUTES A MAJOR REPAIR. REPAIRED THE LOWER WING ASSEMBLY, OEM PN 5122011-21, AT WING STATION 137.2 CTR IAW MEB95-11R1 & AMM D2527-10-13 AS REVISED CHAPTER 51, STRUCTURASDR IXXA20150330071Skin Panel · corrodedAIRCRAFT ON GND FOR HEAVY MX, FAILSAFE INSPECTION. UPPER WING SURFACE AT STATION 187 REAR SPAR AREA PANEL IS BULGED UP. POSSIBLE SIGNS OF CORROSION UNDER PANEL. REMOVED CORROSION IAW SRM 57-20-1 FIG 101. REMOVED & INSTALLED FASTENERS IAW AM 28-11-00. LEAKSDR DALA2015031502173Skin · damagedFASTENER NR 1 EXCEEDS .5775 AFTER REWORK. IAW AMDS 5724-01010-04B. REF NRC 211. REPAIRED PER ERA 533881-14AD. REV ORIG.SDR DALA2015031502172Skin · crackedWING SKIN LOWER SURFACE CRACKED AT IB END OF LONGERON L9.5. REPAIRED PER ERA 533859-14.SDR ASOA2015040212530Skin · crackedRT WING LOWER WING PLANK IS CRACKED AT WS 148.019 RHS. REO 601R-58-21-2311, REV HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.SDR ASOA2015040212529Skin · crackedLOWER WING RT BOOST PUMP CUTOUT FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON VERTICAL SURFACE GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSP. NOTED PITTING AT RT LOWER WING BOOST PUMP CUTOUT. BLENDED PITT CORROSION AT RT LOWER SDR DALA2015031402171Skin · crackedGROUP OF FASTNER HOLES 1, 3 AND 5 SHOW CRACK INCICATIONS AT .282. REPAIRED IAW AMDS CARD 5724-01010-05 AND PRI533894-14AD IAW ERA 533894-14AD REV ORIG REF NR 101.SDR DALA2015031402170Skin · crackedHFEC OPEN HOLE INSPECTION IAW 5724-01010-05 STEP 23. H. REVEALS CRACK INDICATION AT MOST INBOARD FASTENER HOLE.SDR DALA2015031402169Skin · damagedWING SKIN DAMAGED. REPAIRED WING SKIN IAW AMDS 5724-01010-05.SDR DJFA20150313001Skin · corrodedWHILE COMPLYING WITH INSPECTION, FOUND AREAS OF CORROSION AT WING SKIN BEYOND ALLOWABLE LIMITS IAW THE MANUFACTURER. ACCOMPLISHED REPAIR DEFINITION S-750-0073 09RD REPAIR OF LOWER WING SKIN CORROSION. LEAK & OPERATION CHECKS WERE GOOD & THE ACFT RETURNED TO SDR IPXA2015031386956Skin · crackedINSPECTION TYPE:CRT, WING SLAT NR 9 INBD TRACK ON THE INBD COVE SKIN PANEL HAVE CRACKS. REMOVED AND INSTALLED NEW FABRICATED SKIN, COVE PANEL IAW DWG 114N4003-18, MATERIAL 7075-T6, .050.SDR IPXA2015031386955Skin · crackedINSPECTION TYPE:CRT, WING SLAT NR 9 INBD TRACK ON THE INBD COVE SKIN PANEL HAVE CRACKS. REMOVED AND INSTALLED NEW FABRICATED SKIN, COVE, PANEL IAW DWG 114N4003-18, MATERIAL 7075-T6, .050.SDR ASMF201503025Winglet · damagedCAPTAIN INFORMED THAT DURING FLIGHT ACFT RECEIVED A LIGHTNING STRIKE. ACFT WAS SENT TO THE HANGAR & LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW MM05-51-19. DETECTED DAMAGED OUT OF LIMITS ON RT WINGLET. NON-ROUTINE CARD A022497 WAS GENERATED FOR REPLACING SDR DALA2015031202237Skin · corrodedCORROSION ON SETTLEMENT ARE OF FUEL ACCESS DOOR CUTOUTS. COMPLIED WITH WORK ON NRC 61, ZONE 500.SDR KO0R201503110023Skin · corrodedRIGHT WING UPPER SURFACE AT APPROX. WING STATION 827 HAS POSSIBLE CORROSION AROUND FASTENER HEAD.SDR KO0R201503110012Skin · corrodedLEFT WING TRAILING EDGE PANEL RETAINER STRIP BETWEEN APPROX. XORS 317 AND XORS 370 HAS EVIDENCE OF CORROSION.SDR KO0R201503110011Skin · corrodedLEFT WING TOP SIDE FORWARD EDGE APPROXIMATELY XORS 282, HAS EVIDENCE OF CORROSION.SDR KO0R201503110010Skin · corrodedLEFT WING TOP SIDE CENTER SECTION APPROX. XORS 184 HAS EVIDENCE OF CORROSION.SDR KO0R201503110009Skin · corrodedLEFT WING TOP SIDE CENTER SECTION APPROX. XORS 157 HAS EVIDENCE OF CORROSION.SDR UHLA2015031000210Skin · crackedLEFT WING LOWER SKIN INBD OF RIB 17 HAS CRACK. REPAIRED CRACK DAMAGE TO LT WING LOWER SKIN INBD OF RIB 17 BY ROUTE OUT AND DOUBLER/TRIPPLER INSTALL IAW ETD2014-170-022096, REV B.SDR DALA2015031102098Skin · crackedRT WING LOWER SKIN CRACKS. C/W AMDS CARD 5724-01010-06.SDR QXEA2015031600135Access Panel · damagedRIGHT WING FUEL PANEL 622CT HAS SPINNING NUT PLATE. REMOVED GANG CHANNEL IAW SRM 51-42-05-02-01 STEP 4 E. INSTALLED GANG CHANNEL IAW SRM 51-42-05-02-01 STEP 4D (2)-(10). REMOVED DOME NUT IAW SRM 51-42-05-02-01 STEP 4E. INSTALLED DOME NUT IAW SRM 51-42-05-02-01SDR DALA2015031002110Skin · corrodedPREVIOUS BLEND OUT ON RT WING UPPER SKIN, STA 988 - 953, X=61, 67 AND 70. REMOVED CORROSION. FLAP PENNING IAW 95900-4. AREA TREATED AND PAINTED. FASTENER INSTALLED IAW SRM 51-30-03.SDR JJBA20150309010Skin · damagedDAMAGE TO LT WING UNDERSIDE SKIN DURING MX. LOCATED BETWEEN YW 444.00 & YW 457.00. EXACT DAMAGE, THE 45" IS FROM OTBD EDGE OF LOWER SKIN TO DENT. THE 8" IS FROM AFT EDGE OF LOWER SKIN TO DENT. THE 13" IS FROM FWD EDGE OF LOWER SKIN TO DENT. THE DENT HAS A
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