JASC 5710
Service difficulty reports · 4,462
Reports filed under 5710 · Wing Main, Frame Structure, 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 = '5710' 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 = '5710' 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 2010F00127Diffuser · cracked((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOCSDR 2010F00125Diffuser · cracked((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOCSDR GUUA95757061510AStructure · damagedPILOT REPORTED CHECK FOR BIRD STRIKE ON RT OTBD WING. FOUND BIRD STRIKE ON RT OTBD WING L/E REPAIRED DAMAGED SECTION OF WING.SDR 2010FA0000820Structure · wornDURING ANNUAL INSP, DISCOVERED EXCESSIVE FORE AND AFT PLAY IN RT WING, PN 22-5708-00-00-WIP. MX RECORD REVIEW INDICATED THAT THE RT WING WAS REPLACED ON 4/25/09. DISCOVERED SPAR, MAIN BOLT, BUSHING, PN 20-2700-01-20 WAS TON INSTALLED WITH NEW WING. THE ACFTSDR FDEA201006071855Plate · crackedLT WING L/E CAVITY UPPER JOINT PLATE IS CRACKED AT XFS 669. R & R JOINT PLATE AT LT WING L/E STA XFS 669 IAW SRM 51-33-01, VOL II AND SRM 51-35-01, VOL II.SDR A6WA201040398Structure · damagedACFT RT WING TIP STRUCK WING OF PARKED ACFT DURING TAXI. R & R RT WINGLET AFT/FWD SPAR CHANNEL REF DWG NR 600-15108, SRM 51-42-2, 51-42-26, 51-40-11 AND DWG NR 600-15102.SDR 2010FA0000630Structure · damaged((Z4AR)) ACFT WAS BROUGHT IN FOR INSP IAW SAID CE10-20 AND ANNUAL INSP. ACFT IS EQUIPED WITH EXTENDED RANGE FUEL STC AND WING TIP STC. ACFT IS ALSO EQUIPED WITH STALL FENCES STC AND BOOM TO VERTICAL FAIRINGS. AN INSP IS IAW SAIB WAS PERFORMED. COMPRESSION SDR GTIA1000016Structure · corrodedCORROSION FOUND AROUND HEAD ON RT UPPER WING SURFACE APPROX 4 INCHES FWD OF INBD SPOILER HINGE POINT.SDR GUUA93657051310AStructure · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED CORROSION ON TOP LT WING T/E BY NR (1) FLAP. REMOVED CORRODED SECTION OF SKIN AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR IPXA10659875Stiffener · crackedINSPECTION TYPE:C, RT WING FRONT SPAR STIFFENER UPPER AREA FOUND CRACKED JUST AT OFSS532. RT WING FRONT SPAR STIFFENER JUST AT OFSS532 AREA FABRICATED WITH MATL AND10133-2403 7075T6511 EXTRUSION, REPLACED AND INSTALLED IAW RS R57-21-36728 & EO B767-5710-37790SDR IPXA10M59819Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT UPPER SKIN WEB IS CRACKED AS MARKED BEHIND WHEEL CABLE XOS 652 TO STA XOS657 THRU ACCESS PANEL 619DB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203SDR IPXA10M59821Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED LE COMPT UPPER SKIN WEB IS CRACKED AS MARKED BET STA XOS 643 TO STA XOS 647 THRU ACCESS PANEL 619DB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW MD-11 57-40-02 REPAIR 9, FIG. 203SDR IPXA10M59820Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT UPPER SKIN WEB IS CRACKED AS MARKED BET STA XOS 550 TO STA XOS 587 THRU ACCESS PANEL 618GB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG. 203SDR TRBACPCP2010030SPStructure · damagedREPAIRED RT WING ELECTRO FUEL PUMP SURROUNDING AREA IAW EO E2 57-MR-385 REF AMS NDT REPORT 8/30 3H100505-70.SDR TRBACPCP2010030Structure · corrodedDISCREP: REF AML 434552/4 - RT WING ELECTRO FUEL PUMP SURROUNDING AREA HAS CORROSION. AWAITING COMPLETION OF EO E2-57MR-385 AND AML PAGE.SDR DALA1011570661Support Fitting · mismanufacturedWHILE ACCOMPLISHING EA 06-070332-03 AD, FOUND 2 EA INCOMING PILOT HOLES MARKED 2 & 5 ON SUPPORT FITTING PN 012N8888-4 NOT CLEANED UP & DO NOT ALIGN W/ RT WING FRONT SPAR LWR CHORD AND SKIN. ACCOMPLISHED ER/A 482133-14AD REF ORIG AT ST AEROSPACE SAT REF NON ROSDR FDEA201004231316Structure · crackedLT WING - NR 1 SLAT LOWER SIDE BETWEEN NR 1 AND NR 2 TRACK FOUND EXTRUSION WITH CRACK. REPAIR CARRIED OUT IAW EA 8-5750-137977: REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.SDR FDEA201004221280Bolt · shearedLT WING / SIDE LOAD FITTING AFT INBD BOLT FOUND SHEARED AT THE SPAR INSIDE THE TANK. (FOUND WHILE CLEANING TANK FOR CLOSE). REMOVED BOLT IAW 51-40-21 PARA 5. PERFORMED BHEC INSP OF THE BOLT HOLE IAW NTM 51-10-01. NO CRACKS NOTED. INSTALLED NEW BOLT PART SDR IPXA10659410Stiffener · crackedINSPECTION TYPE:C, WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94" WING CTR SECTION FRONT SPAR VERT STIFFENER REPAIRED IAW RS R57-00-36703, EO B767-5710-37458 JUST AT STA785.9 RBL10.94" ORG MATL IS BAC1518-749-2024T3511SDR TRBACPCP2010020Structure · corrodedCORROSION FOUND ON LT WING FUEL PUMP SURROUNDING AREA. COMPLIED WITH LT WING, LOWER SKIN CORROSION BLEND OUT TEMPORARY REPAIR AT FUEL PUMP CUT-OUT AREA IAW EO NR E2-57MR-376.SDR FDEA201004071089Angle · corrodedRT WING FIXED L/E,THROUGH ACCESS HOLES, BEHIND NR 10 SLAT, CORROSION ON INNER SURFACE. REMOVED CORROSION RT WING FIXED L/E AT ANGLE IAW SRM 51-10-02, BLENDED AREA L=5.0", W=1.0", D=0.050", MAT ORIG. .050", OUT OF LIMITS IAW SRM 57-41-13, FIG 101 DET II. RSDR 2010FA0000311Structure · cracked(SPUY) DURING ROUTINE C-CHECK INSPECTION, LT OTBD WING L/E INNER SECTION. LOWER PLATING CRACKED AT STA XFS 597.500.SDR FDEA201003090682Structure · crackedRT WING - UPPER PYLON BOX OTBD LOWER EDGE FOUND CRACKED.SDR FDEA201003010550Support · crackedLT WING LOWER L/E PANEL SUPPORT STRUCTURE IS CRACKED AT SLAT TRACK NR 8. R & R WITH NEW PN ARB 1162-9 IAW SRM 51-33-01, VOL II.SDR FDEA201003010549Former · crackedLT WING L/E LOWER SKIN PANEL INTERNAL SUPPORT IS CRACKED AT THE PRESSURE REFUEL DOOR CUTOUT. CUT OUT DAMAGED AREA IAW SRM 57-00-01, VOL I. FABRICATED REPAIR FILLER AND DOUBLER IAW SRM 57-00-01, VOL I. ALODINED AND PRIMED REPAIR PARTS IAW SRM 51-21-01, VOL ISDR TRBACPCP2010015Structure · corrodedCORROSION AROUND LT WING LWR SURFACE BOOST PUMP BETWEEN RIBS 4-5. CORROSION REPAIRED IAW ATR SRI DO/TS-1229/10-13115, REF NDT REPORT AMS 100226-20 FOR HEFC AND UT RESULTS, COMPLIED WITH ANA/E/3684/2004/E-002 3038 ISSUE B. ACCOMPLISHED EO E2-57MR-370, SUPPLEMSDR FDEA201002150427Shim · migratedSTRUT NR 1 INBD WING FITTING HAS A SHIM MIGRATION ON OTBD SIDE ABOUT .5". COMPLIED WITH EA F-5740-131555 WINGS LT INBD SIDE LOAD FITTING EXPOSED SHIM PART 1. TRACKING IS REQUIRED IAW PART 2, AND PART 3 OF EA. A/C FLIGHT CYCLES (21,726), AND FLIGHT HOURS (52,SDR FDEA201002070356Skin · crackedLT WING ANTI-ICE TELESCOPIC DUCT DOOR CUTOUT FOUND INBD AND OTBD CORNER CRACKED. CARRIED OUT REPAIR AT LT WING ANTI-ICE TELESCOPIC DUCT DOOR CUTOUT IAW SRM 57-40-01, FIGURE 101, REVISION 42. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 109.SDR FDEA201002050339Angle · crackedCRACKED CHORD ANGLE, RT WING FALSE SPAR AT NR 8 SPOILER ACTUATOR ATTACH FITTING. REMOVED DAMAGE BY CUTTING OUT WEB AND CHORD IAW FED EX B727 DRAWING NUMBER SR27-57-038 REV C. FABRICATED 2 REPAIR ANGLES, LOWER CHORD, DOUBLER , STRAP, WEB, & 2 RADIUS FILLERSSDR 2010FA0000084Bolt · misinstalledPROBLEM WITH ELECTRICAL CONDUCTIVITY OF RT TOP WING SKIN WAS TRACED TO IMPROPERLY TORQUED WING TO FUSELAGE JUNCTION. 20 OUT OF 28 WING ASSY BOLTS WERE UNDER OR IMPROPERLY TORQUED; OF THESE 12 OUT OF 14 WERE ON THE RT SIDE CAUSING THE CONDUCTIVITY PROBLEM. 8 OFSDR DL757100396Fitting · damagedRT WING SIDE LOAD FITTING AT WS 297 HAS 1 EA HOLE OVERSIZED. HOLE IS MARKED 68 REF EA06-070332-03AD OPN NBR 0214. C/W ERA 479536-14AD REV ORIG.SDR 2010FA0000069Structure · corrodedCORROSION FOUND AROUND FASTENERS ON RT WING L/E WING STATION 277.SDR CA100812015Structure · damagedLT WING LOCKER OPENED IN FLIGHT. ACFT RETURNED SAFELY, CONSULTED WITH ENGINEER AND MX INSP CARRIED OUT FOR DAMAGE.SDR ASOA201000067Skin · corrodedINDICATIONS OF CORROSION NOTED AT WS 55.38 (540BB) ON THE FLAT LANDING SURFACE APRPOX 70 PERCENT FULL SCREEN HEIGHT. AREAS MARKED ON ACFT LOWER WING PLANK. C/W EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FWDED ALL REQUIRED FORMS TO STRUCTURES ENSDR N93A01132010Bolt · corrodedMOST CADMIUM PLATED HARDWARE INSTALLED IN WING INTERGRAL FUEL TANKS HAVE DEVELOPED CORROSION. HARDWARE REQUIRES REPLACEMENT. MULTIPLE PART NUMBERS AFFECTED.SDR N93A01112010Bolt · corrodedMOST CADMIUM PLATED HARDWARE INSTALLED IN WING INTERGRAL FUEL TANKS HAVE DEVELOPED CORROSION. HARDWARE REQUIRES REPLACEMENT. MULTIPLE PART NUMBERS AFFECTED.SDR TRBACPCP20090023Structure · corrodedCORROSION FOUND AROUND RT WING ELECTRICAL FUEL PUMP. BLEND OUT PERFORMED IAW EO NR E2-57MR-358.SDR EE4Y090358Door · corrodedRT WING INBD BUTTE DOOR CORRODED.SDR DXTA2009110203838Structure · dentedBIRD STRIKE ON THE RIGHT SIDE JUST ABOVE THE ROSEMOUNT, IT CONTINUE TO THE RIGHT WING AT THE STALL STRIP DENTING THE WING AND IT HIT THE RT ENGINE JUST BELOW THE BOTTOM. REMOVED DENTED RT WING INBD HEATED L/E, INSTALLED NEW L/E IAW SRM 51-40-03, OPS CHECKED GSDR TRBACPCP20090022Structure · corrodedCORROSION FOUND ON LT WING T/E AREA BETWEEN RIBS 9 AND 10. PERFORMED BLEND-OUT IAW SRM 51-21-58 AND EO E2-57MR-350.SDR IPXA09657878Fairing · delaminatedINSPECTION TYPE:C LT WING O/B FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.SDR FDEA200910193606Doubler · crackedCTR LANDING GEAR WW, WWL LT FWD SIDE DOUBLER CRACKED. REMOVED IAW SRM 51-31-01 REV. 41. DOUBLER FABRICATED IAW DWG AEA0526 REV. NC. NEW DOUBLER INSTALLED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.SDR GUUA94057093009DStructure · corrodedDURING SCHEDULED LEFT WING X-RAY INSPECTION DISCOVERED SMALL AREA OF CORROSION AREA 1 FWD BONDED STRINGER. CLEANED SURFACE CORROSION AT AREA 1 FOUND TO BE WITHIN ALLOWABLE LIMITS.SDR WRLA20090926234Beam · crackedDURING 2C CHECK, EGAT MECHANIC FOUND CRACK ON THE LT WING FIXED INNER T/E LOWER BEAM, STA XW200,L=14 . JOB COMPLETED IAW EI NR W2009A57B-1122 REV00 AND REV01.SDR QXEA2009092900720Vane · chafedRT L/E CHAFING BETWEEN 684FT AND 684GT PANELS ON INBD FLAP VANE. BLENDED CHAFED AREA. REMOVED MATERIAL IS .006" AND WITHIN LIMITS. TREATED PRIMED AND PAINTED AREA.SDR FDEA200908313164Former · crackedLT WING L/E INTERIOR COMPARTMENT XOS 1020 FORMER FOUND CRACKED. LT WING L/E INTERIOR FORMER REMOVED AND FABRICATED IAW DWG ARB2920, REV BB. LT WING L/E INTERIOR FORMER AT (XOS 1020) INSTALLED IAW SRM 51-35-01, REV 41 AND SRM 51-33-01 REV 41. REPAIR CLASSIFISDR SWIA200922472Frame · crackedRIGHT WING FRAMES, SUPPORTS CRACKED. (C CHECK) REPLACED PER SRM.SDR CA090819007Rivet · corrodedACFT IS HANGARED. ACFT WAS NOTED TO HAVE MISSING RIVET (HEAD) AT LT WS 24-54. LWR SPAR CAP AREA. TCAC WAS CONTACTED AND WE WERE ADVISED TO REPLACE RIVETS AND INSPECT THE AREA IAW TCAC SB 208A. ULTRASONIC INSP WAS COMPLETED BETWEEN WS 24 - WS 52. AVERAGE FLSDR MZZA2009071500092Structure · corrodedLEFT HAND WING KRUEGER FLAP CAVITY SIGN OF CORROSION ON FRONT SPAR LOWER STRAP WS 190. REPAIR CARRIED OUT IAW EC/RA 5730-02564. REFER TO L/P 0976298 FOR NDT INSPECTION.SDR DHLA2009873598Former · crackedRIGHT WING CTR L/E UPPER FORMER CRACKED 1/2" STA XFS 291.500. REMOVED FASTENERS IAW SRM 51-1-21, SRM 51-1-20D. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER IAW SRM 57-3-3 PG 15, SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SR
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