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 DALA2019030804805Shim · migratedSHIP 689 WHILE IN ATL FOR ACCOMPLISHMENT OF WORK CARD 5720-01100-0101A, MAINTENANCE FOUND THE SHIM BETWEEN THE INBOARD DRAG FITTING AND SKIN PANEL ON THE LH WING MIGRATED. EXCEEDS THE ALLOWABLE MIGRATION LIMITS PER WORK CARD. CORRECTIVE ACTION: REF ERA 575709-SDR R61A20190404349Winglet · crackedMAINTENANCE REPORTED A CRACK ON THE LH WING TIP FORWARD SPAR ATTACHMENT. MAINTENANCE REMOVED AND REPLACED THE LH WING TIP IAW EMB AMM 57-30-00.SDR IPXA2019022439349Fitting · crackedINSPECTION TYPE:5YRWHILE ACCOMPLISHING EO A300-5710-68606-B APPX B ON LH WING CRACK DETECTED AT HOLE C 12 OCLOCK POSITION DEPTH GREATER THAN .039 REF FIG1 SHEET 2ACCOMPLISHED REPAIR ON LH FR 47 LOWER JUNCTION HOLE PER VT SAA EA# A300-5710-01-7612 I/R AND UPS ESDR IPXA2019022549348Fitting · crackedINSPECTION TYPE:5YRWHILE ACCOMPLISHING EO-A300-5710-68606-B APP C RH WING CRACK DETECTED AT HOLE C AT 11 AND 6 OCLOCK POSITION DEPTH GREATER THAN .039 REF FIG 1 SHEET 2ACCOMPLISHED REPAIR ON RH FR 47 LOWER JUNCTION HOLE PER VT SAA EA #300-5710-01-7612 AND UPS SDR FDEA201902210466Former · crackedRIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT FORMER AT APPROXIMATELY STATION XIS 237 FOUND CRACK. FORMER ON RIGHT HAND WING INBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY STATION XIS 237. REMOVED AND REPLACED AS PER AMM 20-50-02. FORMER FABRICATED AS PESDR VNAA2019022099909Trunnion · corrodedDISCREPANCY: WHILE PERFORMING SB 601R-57-046 FOUND A CRACK IN R/H WING ASSY (TRUNION FITTING, WING PLANK AND STEEL STRAP) AT WS 65.75 BETWEEN REAR SPAR AND AUX SPAR . CA REPAIRED CRACKED AREA BY OVERSIZING THE HOLE UNTIL CRACK FREE AND INSTALLING AN OVERSIZED SDR SWAA2022030338303Barrier · crackedR/H WHEEL WELL VAPOR BARRIER HAS A CRACK EXTENDING O/B + DOWN FROM RBL 45.64 3.5 INCHES LONG + 7.5 INCHES FROM BOTTOM / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10-1A-2SDR SWAA2022030338304Barrier · crackedR/H WHEEL WELL VAPOR BARRIER HAS A CRACK EXTENDING I/B + UP FROM RBL 45.64 1.0 INCH LONG + 16.0 INCHES FROM BOTTOM / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10-1A-2SDR ABXR2019020800284Beam · corrodedLT WING T/E UPPER AFT BEAM CHORD CORRODED.SDR DALA2019020540755Door · missingLEFT WING #7 LEADING EDGE SLAT TRACK CUTOUT DOOR MISSING. DEFERRED AS PER MD90 CDL 57-30-01 CDL/PLACARD INSTALLED DISPATCH APPROVED. (LP# 3788178)SDR SWAA2022030262214None · crackedCUSTOMER REQUEST. CRACKED LOWER CORD COMMON TO FUEL __ TANK STA 663 ;LBL9; WL165 / REPAIRED CRACKED LOWER CHORD COMMON TO FUEL TANK BS 663 LBL 8 WL 165 PER ER 19-01358 REV IR AND EA 1-757-1587 REV IRSDR UIEA2018122862920Structure · corrodedRIGHT WING UPPER FILL PORT HAS CORROSION AROUND FLANGE.(<P>COMPLIED WITH FEA 18207 RIR.</P>)SDR UIEA2018122862921Structure · corrodedLEFT WING UPPER FILL PORT HAS CORROSION AROUND FLANGE.(<P>COMPLIED WITH FEA 18210 IR.</P>)SDR IPXA2019011537887Beam · corrodedINSPECTION TYPE:3C RT WING O/B T/E O/B STATIC WICK BASE IS LOOSE. REMOVED STATIC WICK BASE AND FOUND RT WING TIP UPPER BEAM CORRODED. REPAIRED RT WING TIP UPPER BEAM CORROSION IAW SRM 57-30-11 PAR. 4.J. FIG. 214 SHEET 4. (MINOR)SDR UIEA2018121982871Plate · corrodedCORROSION-PLATE,R/H WING INBD T/E CAVITY REAR SPAR NO.3 TANK JETTISON PUMP BONDING END AREA, WS 425(<P>1.REPAIR DAMAGE AREA I.A.W. EI NO:T2018A57M-7278,REV.0.</P><P>2.JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR CALA2018120702537Support Beam · crackedRT WING APPROX WS 480 SPOILER SUPPORT BEAM TO BACKUP RIB SUPPORT ASSY FOUND CRACKED. PERFORMED INTERIM REPAIR PER ECRA 5751-01314. PLACING ON DIP TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE NOVEMBER 29, 2020. PL ANNING TO CONTACT ENGINEERING AFTER SEPTEMBER SDR CALA2018120702490Bulkhead Web · crackedRT CENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB CRACKED BETWE EN WL 200.6 AND 192.0 RBL 40.00 TO RBL-45.64 REMOVED DAMAGE FROM WL 200.6-192.0 OF RT CENTER WING BOX REAR SPAR PRESSURE WEB. HFEC VERIFIED NO FURTHER DMG EXISTS.REPAIRED WEB REF SRM 57-10-10 REPSDR JGVR20181114001Drag Angle · corrodedRH AND LH WING @ WING STATION 37 (FWD, MIDDLE, AFT) OVERWING DRAG ANGLES HAVE NUMEROUS AREAS OF CORROSION.SDR UIEA2018110902552Support Beam · corrodedUPPER FACE OF THE LT WING OTBD L/E LOWER FIXED PANEL FWD SUPPORT BEAM, WAS CORRODED. REMOVED CORROSION IAW 51-10-02, REV 41.SDR UIEA2018110902551Support Beam · corrodedRT WING SUPPORT BEAM LWR FLANGE UPPER SURFACE NEAR OLES 1592. REMOVED CORROSION ARE RIVETS AND REPAIRED DAMAGED AREA IAW SRM 51-40-02 REV.41 AND T2018A57M-6134 REV. 2. CONDITION CHECKS NORMAL. </P>)SDR CALA2018110902333Ring · crackedLH BS 1035 UNDERWING LONGERON RING CHORD ARTEA 1 EACH FASTENER HOLE FOUND CRACK AT RING CHORD. REPAIRED THE LH BS 1035 UNDERWING LONGERON RING CHORD 1 EACH FASTENER HOLE PER ECRA 5710-02691 PART 1 INTERIM REPAIR. DIP INITATED TO ACCOMPLISH INITIAL INSPECTIONS SDR IPXA2018111656007Fairing · crackedINSPECTION TYPE: 4C, RT WING PERFORMANCE FAIRING WAS CRACKED COMMON TO THE ALIGNMENT HOLE AT XIS 150.74. REPAIRED THE FAIRING IAW EA 011-5754-01-A7536, REV I/R, AND EO MD11-5720-70620-A. MINOR.SDR HALA2018102900550Structure · damagedLINE SVC REPORTS DAMAGE ON RH WINGLET. // RH WINGLET REPAIRED AND INSTALLED IAW AMM 57-31-22-400-801A. OK FOR SERVICE.SDR ABXA201811213106Strut · corrodedCORROSION ON LOWER STRUT ON AIRLOAD RIB ON RIGHT WING. THE STRUT WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR FDEA201810132862Former · crackedRIGHT WING FIXED LEADING EDGE LOWER FORMER AT XOS 993 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB1164 REV M. INSTALLED NEW FORMER AT RIGHT HAND WING FIXED LEADING EDGE LOWER AT XOS 993 AS PER SRM 51SDR FDEA201810132861Former · crackedRIGHT WING FIXED LEADING EDGE LOWER FORMER AT XOS 963 FOUND CRACK. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED NEW FORMER PER DRAWING ARB1164 REV M. INSTALLED NEW FORMER AT RIGHT HAND WING FIXED LEADING EDGE LOWER AT XOS 963 AS PER SRM 51-33-0SDR IPXA2018102935443Hinge · crackedRIGHT OUTER WING T/E LOWER DOOR HINGE WAS CRACKED AT XORS 653.5. REPAIRED HINGE AT XORS 653.5 IAW EA 011-5720-01-A7514REV. I/R AND UPS EO MD11-5720-70329-A. (MINOR)SDR IPXA2018102935442Hinge · crackedRT OUTER WING T/E, LOWER HINGE WAS CRACKED AT XORS 745.3. REPAIRED THE HINGE IAW EA 011-5720-01-A7513, REV I/R, AND EO MD11-5720-70328-A. MINOR.SDR IPXA2018102235236Former · crackedRIGHT WING L/E FORMER WAS CRACKED AT XOS. 995. REMOVED, FABRICATED, AND REPLACED THE FORMER IAW DWG ARB1164, AND SRM 51-31-01. MINOR.SDR IPXA2018102235235Former · crackedLEFT WING L/E FORMER WAS CRACKED AT XOS. 920. REMOVED, FABRICATED, AND REPLACED THE FORMER IAW DWG ARB2920, SRM 51-33-01, & 51-35-01. MINOR.SDR COEA2018111623803Landing · corrodedWO 188611 NR 500008 HEAVY CHECK COE/MAJOR REPAIR: FRETTING DAMAGE TO 522CT PANEL LANDING, LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-4828...6020 ISSUE D, DATED 10/18/2018.SDR FDEA2018092092585Former · crackedLEFT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG AND 51-33-01-OG. FORMER PART NUMBER ARB2920-13 FABRICATED AS PER DRAWING ARB2920 REVISION BB. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-1SDR FDEA2018091432518Former · crackedRIGHT HAND WING LEADING EDGE CAVITY FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT RIGHT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PSDR FDEA2018091432512Former · crackedLEFT HAND WING LEADING EDGE FORMER AT STA XOS 1025 FOUND CRACKED. CRACKED FORMER REMOVED PER SRM 51-31-01-0G AND FABRICATED NEW FORMER AS PER DRAWING ARB2920 REVISION BB. INSTALLED NEW FORMER AT LEFT HAND WING LEADING EDGE CAVITY AT STA XOS 1025 AS PER SRM 51SDR DALA2018082805309Structure · damagedDURING A WALK AROUND, FOUND THE GAUGE ON THE LT WING L/E UNDER SLAT NR 1, XFS 136. COMPLIED WITH A DETAILED VISUAL INSPECTION OF THE DAMAGED AREA. FABRICATED A REPAIR DOUBLER IAW SRM 57-06B, FIG 13. COMPLETED INSTALLATION OF REPAIR IAW SRM 57-06B, FIG 31SDR DALA2018082005148Channel · crackedCRACKED CHANNEL IN THE RT MLG WHEEL WELL, FWD DOOR FRAME. THE CHANNEL WAS REPLACED IAW SRM 51-30-02, VOL II, AND SRM 51-30-05, VOL II.SDR FOTR201808209003Spar · crackedRT WING REAR SPAR RSS 218 CRACKED AT INBD SIDE OF MLG SUPPORT FITTING.SDR ABXA2018082017092Beam · corrodedCORROSION ON THE RIGHT WING REAR SPAR TO TRAILING EDGE UPPER PANEL ATTACH BEAM AT WING STATION 280. THE UPPER PART OF THE ATTACH BEAM WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA2018082017090Beam · corrodedCORROSION ON THE LEFT WING REAR SPAR TO TRAILING EDGE, UPPER PANEL ATTACH BEAM AT LWS 285. THE ATTACH BEAM AND UPPER PANEL WERE REPLACED. THE AIRPLANE WAS GROUNDED.SDR SRXR201808160017Landing · corrodedLEFT WING T/E ACCESS PANEL LANDING HAD CORROSION AT XORS 402. ACCOMPLISHED A BLEND OUT REPAIR IAW EA 011-5750-52-A7390, I/R.SDR SRXR201808160014Beam · corrodedLEFT WING T/E BEAM ASSY, UPPER CAP HAD CORROSION AT XW 265. ACCOMPLISHED A REPAIR IAW EA 011-5710-52-A7320 I/R.SDR SWAA2018090424777Former · crackedRT WING FIXED LEADING EDGE INBOARD FAIRING SUPPORT FORMER CRACKED ON UPPER END. R&R FORMER IAW SRM AND DWG.SDR COEA2018012063807Panel · corrodedWO 187945 NR 500032 HEAVY CHECK COE/MINOR REPAIR: LEVEL 2 CORROSION ON LH OVERWING FUEL PANEL 523GT. CORRECTIVE ACTION: REPLACED WITH OEM PART.SDR SCNA201808098100Rib · corrodedLEFT WINGLET RIB WAS CORRODED ON THE OUTBOARD SIDE. REMOVED AND INSTALLED LEFT WINGLET. CHECKED GOOD AND SEALED.SDR SWAA2022022234857Bracket · crackedR/H WING FWD ATTACH POINT FOR PNL 651EB (WIGGLE) PLATE IS CRACKED AND NOT SECURE / R&R FWD ATTACH BRACKET PLATE ASSY FOR PNL 651EB PER SRM 51-40-02SDR ABXA201807132076Beam · chafedCHAFING AT BODY STATION 900, LBL 57 ON THE LOWER WING SKIN PANEL (P/N: 111T4015-4) AND LOWER CENTER WING BEAM WEB (P/N: 111T5077-2), DOUBLER (P/N: 111T5012-21), & LOWER CHORD (P/N: 111T5012-17). THE SKIN PANEL, WEB, DOUBLER, AND CHORD WERE REPAIRED. THE AIRPLASDR IPXA2018073032165Former · crackedINSPECTION TYPE:3C, LT WING L/E FORMER IS CRACKED AT STA XOS 917. REMOVED, FABRICATED AND REPLACED LT WING L/E FORMER IAW DWG ARB2920 AND SRM 51-33-01. (MINOR)SDR FDEA201806261519Former · crackedLT WING FIXED LE COMPARTMENT STA XOS 698 FORMER SUSPECT CRACK. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DWG ARB2930 REV F. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201806181518Former · crackedRIGHT WING FIXED LEADING EDGE FORMER AT XOS 584 FOUND CRACK. FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DWG ARB 2931 REV H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201806181515Former · crackedLT WING FIXED L/E COMPARTMENT STA XOS 584 FORMER CRACKED. FORMER ON LT WING FIXED L/E COMPARTMENT AT STA XOS 584 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. FORMER FABRICATED AS PER DWG ARB2931 REV H. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.
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