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 FDEA202006231310Former · crackedLEFT HAND WING LEADING EDGE CAVITY FORMER AT STATION XOS = 733 FOUND CRACK. CRACKED FORMER REMOVED IAW SRM 51-31-01-0G, AND FABRICATED A NEW FORMER IAW DRAWING ARB2923, REVISION D. INSTALLED THE NEW FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR ISDR FDEA202006191281Doubler · corrodedLEFT WING UPPER INBOARD SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER CORRODED NEAR INBOARD EDGE. CORROSION REMOVED AND FOUND EXCEEDED LIMITS. CORROSION REMOVAL 0.100 INCHES MAXIMUN IAW SRM 57-20-01-1A, FIGURE 101, ALLOWABLE DAMAGE 1. REPAIRED IAW EA 1-5SDR FDEA202006191280Doubler · corrodedRIGHT WING UPPER INBD SURFACE, MAIN LANDING GEAR SUPPORT DOUBLER CORRODED NEAR TWO INBD AFT FASTENERS. CORROSION REMOVED AND FOUND EXCEED LIMITS. CORROSION REMOVAL 0.100 INCHES MAXIMUN IAW SRM 57-20-01-1A, FIGURE 101, ALLOWABLE DAMAGE 1 . REPAIRED IAW EA 1-SDR SWIA2020072151344Doubler · crackedRIGHT WING AUX SPAR LOWER FLANG DOUBLER WAS CRACKED AT RWS 148. REPAIRED THE RIGHT WING AUX SPAR LOWER FLANG DOUBLER IAW REO. LEAK CHECKED GOOD.SDR FDEA2020071031215Former · crackedLEFT WING LEADING EDGE REFUELING PANEL COMPARTMENT CUTOUT EDGE FOUND CRACKED AT OUTBOARD AFT CORNER AREA XOS 643. REMOVED AND FABRICATED A FORMER IAW DRAWING ARB 2917, REVISION L . FABRICATED FORMER INSTALLED IAW SRM 51-31-01-OG. REPAIR CLASSIFIED AS MAJOSDR ABXA20200721132Beam · corrodedWS 897, REPLACED CORRODED NOSE BEAM-LH WING LE BEHIND #2 SLAT. AIRCRAFT WAS GROUNDED.SDR IPXA2020062957109Cap · corrodedINSPECTION TYPE:2CL/H WING T/E LOWER CAP HAS CORROSION BETWEEN STA. XW= 276.029 TO XW= 328.00.REPAIRED CORRODED L/H WING T/E LOWER CAP BETWEEN STA XW= 276.029 TO XW= 328.00 IAW SRM 57-50-02 REPAIR 9 FIG. 201. (MAJOR)SDR IPXA2020062967021Beam · crackedINSPECTION TYPE:2C, RT WING O/B FLAP I/B FWD HINGE FAIRING BEAM IS CRACKED.REMOVED AND REPLACED CRACKED RT WING O/B FLAP I/B FWD HINGE FAIRING BEAM IAW MD-11 SRM 51-33-01. (MINOR)SDR SWAA2021052681881Gusset · crackedLEFT WING TRAILING EDGE ; ABOVE THE FIXED PANEL (BETWEEN SPOILERS #5 AND #6) GUSSET CRACKED AT LWR FASTENER HOLE / REMOVED AND REPLACED GUSSET AT L/W T/E BETWEEN SPOILER #5 AND #6 AS PER SRM 51-40-02-0G-0 AND DRAWING 115A2982SDR IPXA2020072097946Tee Fitting · chafedINSPECTION TYPE:3C, RIGHT WING FIXED L/E LWR T CHORD AND UPPER ANGLE ARE CHAFED FROM THE TELESCOPIC DUCT PANEL ON I/B SIDE.REMOVED CHAFED T-CHORD, FABRICATED AND INSTALLED ON RH WING FIXED L/E XOS-464 IAW DWG ARB2926.SDR IPXA2020072097945Cap · chafedINSPECTION TYPE:3C, RT WING FIXED L/E LOWER T-CHORD AND UPPER ANGLE CHAFED FROM TELESCOPIC DUCT PANEL ON I/B SIDE.REMOVED CHAFED T-CAP, FABRICATED AND INSTALLED ON RH WING FIXED L/E XOS=464 IAW DWG 1284.SDR IPXA2020072097944Splice Angle · chafedINSPECTION TYPE:3C, RT WING FIXED L/E LWR T CHORD AND UPPER ANGLE CHAFED FROM THE TELESCOPIC DUCT PANEL ON I/B SIDE. REMOVED CHAFED SPLICE ANGLE, FABRICATED AND INSTALLED ON THE RT WING FIXED L/E XOS=464 IAW DWG 1284.SDR IPXA2020052255632Fitting · crackedINSPECTION TYPE:SEG3UPPER SKIN FITTING RH PYLON #3 HOLE HAD REJECTABLE CRACK INDICATIONS AT BOTTOM OF HOLEREAMED HOLE TO REMOVED INDICATION PER E.O. B757-5720-76605-A.SDR SWAA2021082777198Retainer · crackedLEFT WING I/B UPPER FIXED TE PANEL FWD. SEAL RETAINER BRACKET CRACKED / REMOVED AND REPLACED LEFT WING I/B UPPER FIXED TE PANEL FWD. SEAL RETAINER BRACKET PER SRM 51-40-02.SDR SWAA2021070789124Plate · crackedON THE RIGHT WING TRAILING EDGE LOWER SURFACE AT APPROXIMATELY ORSS 256; THE WAFFLE PLATE IS CRACKED AT INBD END AND NOT SECURED PROPERLY. / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02 RESTORED FINISH PER AMM 51-21-99SDR SWAA2021082745022Bracket · crackedRH WING; LWR INBOARD FIXED TRAILING EDGE PANEL 651FB FWD SEAL RETAINER HAS CRACKED ANGLE BRACKET / REMOVED AND REPLACED ANGLE BRACKET P/N 287A9152-24; ON FWD SEAL RETAINER OF RH WING PANEL 651FB IAW SRM 51-40-02-0G-0 AND BOEING DWG. 115A2710 REV. -. A-TAG # DFSDR SWAA2020041336244Attach Angle · crackedSUPPLEMENTAL INFORMATION: (SKYLINE DTIP) PREVIOUS REPAIR LH LWR COMPOSITE BULKHEAD (VAPOR BARRIER); STA 663; UPPER ATTACH ANGLE CRACK REPAIRED / NO FURTHER EVALUATION IS NECESSARY PER EA 1-751-1142SDR SWAA2020041336232Vapor Barrier · deterioratedSUPPLEMENTAL INFORMATION: (SKYLINE DTIP) FOUND PREVIOUS REPAIR AREA; AT LH VAPOR BARRIER; STA 663; LBL 35 DETERIORATED WITH VAPOR BARRIER CRACKS / FABRICATED SEALANT PATCH 3EA WITH FIBERGLASS CLOTH BMS 9-3 TYH2 ST 1581 LOT # 1419982-3; IMPREGNATED WITH BMS 5-9SDR SWAA2020032734763Vapor Barrier · crackedSUPPLEMENTAL INFORMATION: L.H W/W VAPOR BARRIER HAS A CRACK 6' IN LENGTH. C/W REPAIR PER SRM 57-10-10-1A-2 REPETITIVE ACTION REQUIRED DO A VISUAL INSPECTION OF THE REPAIR AREA AT 1200 FLIGHT CYCLE INTERVALS OR MORE FREQUENTLY. MAKE SURE THAT CRACK HAS NOT GROWSDR SWAA2021082781465Retainer · chafedL/H WING TRAILING EDGE PANEL 551GB BULB SEAL RETAINING BRACKET CHAFFED AND WORN. / REMOVED AND REPLACED L/H WING T/E PANEL 551GB BULB SEAL RETAINING BRACKET REF SOPM 20-50-01.SDR SWAA2021041532797Barrier · crackedRT MAIN GEAR WHEEL WELL STA. 663.75; RBL 31.83 VAPOR BARRIER HAS A 4.5 INCH CRACK / RT MAIN GEAR WHEEL WELL STA. 663.75; RBL 31.83 VAPOR BARRIER HAS A 4.5 INCH CRACK. COMPLIED E.A. 1-A57-13410; THIS IS A TIME LIMITED REPAIR. REINSPECT EVERY 100 CYCLES. REMOVE SDR DALA2021081804804Shim · migratedSHIP 689 MAINTENANCE FOUND THE SHIM BETWEEN THE INBOARD DRAG FITTING AND FRONT SPAR ON THE RH WING MIGRATED,WHICH EXCEEDS THE ALLOWABLE MIGRATION LIMITS. CORRECTIVE ACTION: ERA 575624-14 HAS BEEN UPDATED TO REVISION B. (1518743)SDR FDEA2020031290445Former · crackedLEFT WING - FIXED LEADING EDGE LOWER SUPPORT FORMER AT XOS 1027 FOUND CRACK. LEFT WING - FIXED LEADING EDGE LOWER SUPPORT CRACKED FORMER AT XOS 1027 REMOVED AND REPLACED AS PER SRM 51-31-01-0G.FORMER FABRICATED AS PER DOUGLAS DRAWING : ARB 2920 REVISION BBSDR FDEA202002280439Former · crackedRIGHT WING - FIXED LEADING EDGE LOWER SUPPORT FORMER AT XOS 1025.289 FOUND CRACK RIGHT WING - FIXED LEADING EDGE LOWER SUPPORT CRACKED FORMER AT XOS 1025.289 REMOVED AND REPLACED AS PER SRM 51-31-01-0G.FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2920 RESDR FDEA202002270433Skin · crackedL/H WING TIP AFT - LOWER SURFACE BETWEEN ACCESS PANEL#528CB AND AFT POSITION LIGHT - 2 CRACKS EMINATING FROM FASTENER HOLE, CRACKS CONFIRMED AND ENDS. PERFORMED A PERMANENT REPAIR IN ACCORDANCE TO SRM VOLUME I CHAPETER 57-00-01 FIGURE 4 (SHEET 2).SDR SWAA2021082782056Retainer · chafedRIGHT WING TRAILING EDGE PANEL 651GB SEAL RETAINER CHAFED. MARKED 29-87 / REMOVED AND REPLACED SEAL RETAINER AT RIGHT WING TRAILING EDGE PANEL # 651GB IN REF B737-700 SRM 51-40-02-0G-0.SDR SWAA2021082718808Retainer · crackedR\H WING FIXED T\E; AFT OF SAIL TAIL; AFT LOWER SEAL RETAINER BRACKET CRACKED. / REMOVED AND REPLACED R/H WING FIXED T/E; AFT OF SAIL TAIL AFT LOWER SEAL RETAINER BRACKET IAW B-737 SRM 51-40-02 AND B-737 AIPC 57-50-00-25SDR IPXA2020022655469Panel · crackedINSPECTION TYPE:SEGRIGHT WING KRUGER FLAP COVE PANEL HAS A CRACK IN O/B CORNERREPAIRED IAW SRM 51-70-10SDR FDEA202002240376Former · crackedRIGHT HAND WING LEADING EDGE CAVITY FORMER AT XOS 993 FOUND CRACKED. CRACKED FORMER REMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DOUGLAS DRAWING ARB1164 REVISION M. INSTALLED FABRICATED FORMER AT RIGHT HAND WING LEADING EDGE CAVITY AT XOS 993 ASDR ABXR2020022104009Splice Plate · corrodedCORROSION AROUND GROUNDING JACK ON FRONT SPAR UPPER CHORD AFT OF NUMBER 3 SLAT OUTBOARD DRIVE ROD ACTUATOR.COMPLETED REPAIR IAW REA: 47396REA05 AND 47396REA06 SEE BACK AND PARTIAL WS 27 PGS 1 AND 2 FOR PARTIAL WORK ACCOMPLISHED. COMPLETED HOLE SCAN ON SPLICE PSDR SWAA2021082719218Retainer · crackedRIGHT WING FIXED T/E PANEL VERTICAL BULB SEAL RETAINER IS CRACKED 9' I/B OF DEFLECTION RIB. MARKED / REMOVED AND REPLACED RIGHT WING FIXED T/E PANEL VERTICAL BULB SEAL RETAINER P/N 115A2953-2 AT 9' I/B OF DEFLECTION RIB. IAW SRM 51-40-02 AND AIPC 57-50-00-25 8SDR SWAA2021082719221Retainer · crackedLEFT WING T/E UPPER SEAL RETAINER IS CRACKED 3' BELOW FIXED T/E PANEL 10' I/B OF DEFLECTION RIB ORSS269. / REMOVED AND REPLACED LEFT WING T/E UPPER SEAL RETAINER AT 3' BELOW FIXED T/E PANEL 10' I/B OF DEFLECTION RIB ORSS 269 P/N 115A2982-9. IAW. SRM 51-40-02. SDR SWAA2021081919956Support Beam · brokenLOWER T/E PANEL SUPPORT BEAM AT ORSS 292 AND 11'AFT OF THE REAR SPAR IS BROKEN (P/N 115A3758-10) RIGHT WING / REMOVED AND REPLACED LOWER T/E PANEL SUPPORT BEAM P/N 115A3758-10 IAW. SRM 51-40-02 AND AIPC 57-50-00-18 8920U 18FEB20 ON RT WING.SDR IPXA2020030452755Beam · corrodedINSPECTION TYPE:CLH WING TIP UPON REMOVAL OF UPPER SURFACE O/B STATIC WICK BASE FOUND EXFOLIATED CORROSIONREMOVED UPPER BEAM LH WING TIP IAW A300-600 SRM 51-40-21 RECEIVED NEW BEAM P/N A5726021320600 INSTALLED UPPER BEAM AT LH WING TIP IAW A300-600 SRM 51-40-2SDR IPXA2020030452752Beam · corrodedINSPECTION TYPE:CLH WING TIP UPON REMOVAL OF O/B STATIC W/C BASE FOUND EXFOLIATED CORROSION UNDER BUBBLE FAUNT ON LWR SURFACE SKINREMOVED LWR BEAM ON LH WING TIP IAW A300-600 SRM 51-40-21 RECEIVED NEW PART A5726021420600 INSTALL NEW LWR BEAM AT LH WING TIP IAWSDR DALA2020021181091Fitting · damagedSHIP 697 LT WING DRAG BRACE FITTING - #8 BOLT HOLE HAS TOOLING DAMAGE. CORRECTIVE ACTION: SUMMARY SEE NR 033-0001:5720-01100-0101A/010 00333 COMPLIED WITH ERA 584933-14AD REV. O. (1480534)SDR DALA2020021181090Structure · crackedSHIP 697 STEP 26 FASTENER HOLE #7 CRACK INDICATION. SEE NR FOR ADDITIONAL INFORMATION 033-0001:5720-01100-0101A/008 00331 COMPLIED WITH ERA 584933-14AD REV. O. (1480530)SDR DALA2020021181085Structure · cracked(AIRCRAFT 697, L/P 1480531) STEP 27 FASTENER HOLE #13 CRACK INDICATION. CORRECTIVE ACTION: COMPLIED WITH ERA 584933-14AD REV. O. VERIFIED PRI 584933-14AD, REV. 0-2 AND ERA 584933-14AD REV. O MATCH.SDR DALA2020021181084Structure · cracked(AIRCRAFT 697, L/P 1480529) STEP 26 FASTENER HOLE #3 CRACK INDICATION. CORRECTIVE ACTION: COMPLIED WITH ERA 584933-14AD REV. O. VERIFIED PRI 584933-14AD, REV. 0-2 AND ERA 584933-14AD REV. O MATCH.SDR DALA2020021181083Structure · cracked(AIRCRAFT 697, L/P 1480529) STEP 26 FASTENER HOLE #3 CRACK INDICATION. CORRECTIVE ACTION: COMPLIED WITH ERA 584933-14AD REV. O. VERIFIED PRI 584933-14AD, REV. 0-2 AND ERA 584933-14AD REV. O MATCH.SDR EE4Y2020020710627Structure · corrodedWING CENTER SECTION REAR SPAR BS 663 LEVEL, WL 209, RBL 61 UPPER CHORD WITH CORROSION. NOTE: THE WING REAR UPPER CHORD WAS REPAIRED AS PER BOEING SERVICE REQUEST NO: 3-4565173757 INSTRUCTIONS. (REF: JOB: A1H267 ITEM 1-76 COOPESA ENGINEERING ORDER NO: COO-EO-20SDR DALA2020020530901Fastener · loose(AIRCRAFT 5655, L/P 1472712) LOOSE FASTENER #14 AT LH WING DRAG FTG UPPER SURFACE. CORRECTIVE ACTION: REPLACED WITH NRC 00654 UNDER LOG NUMBER 1471528 PER ER/A 584900-14AD REV: ORIGINAL SECTION I PERMANENT REPAIR AND ETI-57-20-006 REV. 10.SDR DALA2020020530900Fastener · loose(AIRCRAFT 5655, L/P 1472581) LOOSE FASTENERS # 1, #3, #5 AND #8 AT LH WING DRAG FTG UPPER SURFACE. CORRECTIVE ACTION: REPLACED WITH NRC 00654 UNDER LOG NUMBER 1471528 PER ER/A 584900-14AD REV: ORIGINAL SECTION I PERMANENT REPAIR AND ETI-57-20-006 REV. 10.SDR DALA2020020530902Fastener · loose(AIRCRAFT 5655, L/P 1471156) LOOSE FASTENERS #2, #3, #4 AND #9 AT RH WING DRAG FTG UPPER SURFACE. CORRECTIVE ACTION: REPLACED WITH NRC 00581 UNDER NUMBER LOG: 1467364 PER ER/A 584920-14AD REV. ORIGINAL, SECTION 1: PERMANENT REPAIR AND ETI-57-20-008 REV. 5.SDR DALA2020013190738Shim · migratedMIGRATED SHIM ON DRAG FITTING, FRONT SPAR OUTBOARD 0.300, LH ENG DRAG FTG CLAMP-UP & DIAG BRACE. REPLACED IAW ETI-57-19-213 REV 11, AND ER/A 584851-14AD REV. ORIGINAL.SDR IPXA202002051822Rib · damagedINSPECTION TYPE:A300LMLG RIB 5 FWD BORE FOUND TO HAVE DAMAGE/ FITTING COURSEREPAIRED PER DWG R57240425SDR C77A2020012314057Structure · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART II, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT RH WING TIP SPAR 1 (P/N 171-16231-002 OR 171-16231-004) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-171-22480-40SDR C77A2020012314056Structure · crackedTHIS EO PROVIDES INSTRUCTIONS TO COMPLY WITH SB 170-57-0072 PART I, WHICH ACCOMPLISHES A STRUCTURAL MODIFICATION THAT CONSISTS OF REPLACING THE CURRENT LH WING TIP SPAR 1 (P/N 171-16231-001 OR 171-16231-003) WITH A NEW, REDESIGNED SPAR 1 (P/N 171-22480-401), WSDR J7SA202002062001Screw · looseRIGHT LEADING EDGE HAS LOOSE SCREW ON MIDDLE LEADING EDGE PANEL. REMOVED AND REPLACED LOOSE SCREW PER BD100 AMM 57-41-09 P/N NAS8703-3.SDR SWAA2021041522883Barrier · dislodged*CUSTOMER REQUEST*REPAIR BS 663 LOWER VAPOR BARRIER L/H (EXISTING REPAIR AT LBL 12 WL 150 IS DISBANDED.) / REPAIRED DAMAGE A LBL 12 AND WL 150 ON BS 663.75 LOWER VAPOR L/H IAW 737 SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-10 AND SRM 51-70-04-2R-0
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