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 FDEA202010172539Former · crackedLEFT HAND WING FIXED LEADING EDGE CAVITY AT STATION XOS=584 FORMER FOUND CRACK. CRACKED FORMER REMOVED, AS PER SRM 51-31-01-OG AND FABRICATED FORMER, AS PER DOUGLAS DRAWING ARB 2931 REVISION H. INSTALLED FABRICATED FORMER AT LEFT HAND WING LEADING EDGE CAVSDR SWAA2021051323466Plate · crackedR/W T/E SPAR LWR SURFACE WIGGLE PLATE CRACKED I/B OF #8 CANOE FAIRING. / REMOVED AND REPLACED WIGGLE PLATE AT R/W T/E SPAR LWR SURFACE I/B OF #8 CANOE FAIRING IAW B737-700 SRM 51-40-02-0G-0SDR FDEA202010152520Former · crackedRIGHT WING, NR 8 SLAT, OUTBOARD ROTARY ACTUATOR ARM CUTOUT, FORMER IS CRACKED. REMOVED AND REPLACED NOSE FORMER, IAW BOEING DWG 114T2161 REV E AND FEDEX EA H-5720-T0357395 P1. TITLED: WINGS-SECONDARY WING STRCT-RT WING, LEADING EDGE, ANGLE, OSS 499, ALTERNATSDR SWAA2021081622992Support Rod · brokenLEFT WING TRAILING EDGE PANEL 551GB; THE INBOARD MOST FORWARD SUPPORT ROD IS BROKE AT THE THREADED ROD END. / REMOVED AND REPLACED SUPPORT ROD IAW AMM 57-50-02.SDR SWAA2021011122931Fastener · looseLEFT WING TRAILING EDGE TWO LOOSE FASTENERS ARE CHAFING ON DEFLECTION RIB UPPER ATTACH TAB ORSS279. TRIMMED OUT THE DAMAGE PART OF THE DEFLECTION CONTROL RIB UPPER TAB AND INSTALLED REPAIR PARTS, IAW SRM 57-51-02-2R-4 88920U 30OCT20.SDR SWAA2021051323353Plate · crackedLEFT WING AFT LOWER I/B FIXED TRAILING EDGE PANEL #551GB FWD WIGGLE PLATE CRACKED (102-001) / REPLACE FWD WIGGLE PLATE @ LEFT WING AFT LOWER I/B FIXED TRAILING EDGE FWD OF PANEL 551GB AS PER B737-700 SRM 51-40-02-0G-0SDR AALA202010129006Vapor Barrier · crackedAIRCRAFT WAS NOT GROUNED. LEFT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER CRACKED AT LBL 32, JUST FORWARD OF THE A HYDRAULIC SYSTEM RETURN FILTER ASSEMBLY. REPAIRED VAPOR BARRIER, PER AARD 57-10-10-9.SDR SIMA20201010001Fairing · chafedLT FIXED LEADING EDGE FAIRING IS CHAFED ON LEADING EDGE. FOUND ON OPEN UP. C/A: COMPLETED INSTALLING REPAIR DOUBLER ON LT FIXED LEADING EDGE FAIRING ON LEADING EDGE, IAW EMB 175 SRM 57-49-01 FIGURE 201.SDR FDEA202010092581Former · crackedLEFT WING LEADING EDGE FORMER CRACKED AT NR 5 SLAT AUX TRACK. REMOVED AND REPLACED LEFT WING LEADING EDGE FORMER AND ANGLE, IAW BAC DWG 114T2241, REV. AND EA H AND EA: H-5720-T0357387, P1, RELEASE DATE: OCT 14, 2020, REV DATE: WINGS-SECONDARY WING STRCT SECOSDR REXA2020101200696Fitting · obstructedWHILE INCORPORATING SB670BA-57-020, FOUND THE REAR SPAR MOD PREVIOUSLY ACCOMPLISHED, THE FITTING INTERFERES WITH WIRING PLANK FASTENER INSTALLS.
REPAIRED REINFORCING FITTINGS INSTALLED, PER SB 670BA-57-015 DUE TO INTERFERENCE WITH COLLAR INSTALLED PER SB 67SDR AALA202010109016Vapor Barrier · crackedAIRCRAFT WAS NOT GROUNDED. RIGHT HAND MAIN LANDING GEAR WHEEL WELL VAPOR BARRIER PREVIOUSLY INSTALLED REPAIR FAILED, WHICH WAS LOCATED ON THE FORWARD BULKHEAD BEHIND THE B HYDRAULIC SYSTEM RETURN FILTER ASSEMBLY. REPAIRED VAPOR BARRIER, PER AARD 57-10-10-9.SDR GTIA2020100835379Structure · corrodedCORROSION FOUND ON RT WING STATION 9239 RIB 17-18 RAF 01 2433110-02. OPENED REPAIR PERFORMED ON LTPR NRI 5001016214-0011, IAW EO 5720-2020 REV 00. THIS IS A CAT A NO FURTHER ACTION REQUIRED.SDR SWAA2021051321292Plate · brokenLEFT WING T/E WIGGLE PLATE AT ORSS 375 HAS BROKEN PHENOLIC / REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE AT ORSS 375 P/N.115A3760-49 IAW.SRM 51-40-02 AND DWG 115A3700 88920U 10OCT20SDR SWAA2021051321291Plate · crackedLEFT WING WIGGLE PLATE AT ORSS 404.0 IS BENT AND PHENOLIC IS CRACKED / REMOVED AND REPLACED LEFT WING WIGGLE PLATE AT ORSS 404.0 P/N 115A3760-13 IAW SRM 51-40-02 AND DWG 115A3700 AND DWG 115A3711 88920U 13OCT20SDR IPXA2020102861765Former · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE FORMER IS CRACKED JUST INBOARD OF NR 9 SLAT TRACK. REMOVED, FABRICATED, AND REPLACED FORMER IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)SDR IPXA2020102761717Former · crackedINSPECTION TYPE: 2C LT WING FIXED LEADING EDGE COMP RIB/FORMER IS CRACKED AT STA XOS 685. REMOVED, FABRICATED, AND REPLACED FORMER, IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)SDR FDEA202010042410Doubler · corrodedLEFT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION. CORROSION REMOVED AND FOUND EXCEED LIMIT AS 0.100" MAXIMUM MATERIAL REMOVAL. REMOVAL FOR GENERAL CORROSION REMOVAL, PER SRM 57-20-01-1A FIGURE 101 ALLOWABLE DAMAGE 1 SDR FDEA202010042408Doubler · corrodedRIGHT HAND WING, UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER FOUND CORROSION. FOUND CORROSION YW 467 RIGHT HAND WING UPPER WING SURFACE MAIN LANDING GEAR SUPPORT UPPER DOUBLER YW 467. CORROSION REMOVED AND FOUND EXCEED LIMIT AS 0.100" MAXIMUM SDR FDEA202010022396Former · crackedLEFT HAND WING, FIXED LEADING EDGE FORMER AT APPROXIMATELY XORS 480-500, BEHIND SLAT NR 4 MID SECTION, FOUND CRACKED. LEFT HAND WING, FIXED LEADING EDGE CRACKED FORMER AT APPROXIMATELY XORS 480-500, BEHIND SLAT NR 4 MID SECTION, REMOVED AND REPLACED WITH FABRSDR SWAA2021051320885Plate · crackedFOUND R/H WIGGLE PLATE AT ORSS261 LWR FLANGE TO BE CRACKED / REMVOED AND REPLACED R/H WIGGLE PLATE AT ORSS261 LWR FRAMES P/N 115A2781-14 IAW. SRM 51-40-02 AND AIPC 57-50-00-30. 88920U 10OCT20.SDR SWAA2021051320883Plate · crackedLEFT WING T/E WIGGLE PLATE IS CRACKED ORSS261. / REMOVED AND REPLACED LEFT WING T/E WIGGLE PLATE @ ORSS 261 COMMON TO T/E ACCESS PANEL 551GB IAW SRM 51-40-02-0G-0 CHEMICAL CONVERSION COATING APPLIED TO BARE METAL AREAS IAW AMM 51-21-41-370-802 PRIMER & DECORATSDR IPXA2020101761376Former · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE FORMER IS CRACKED JUST OUTBOARD OF NR 9 SLAT TRACK. REMOVED AND REPLACED CRACKED RT WING FIXED LEADING EDGE FORMER JUST OUTBOARD OF NR 9 SLAT TRACK, IAW MD-11 SRM 51-33-01. (MINOR)SDR IPXA2020101261222Landing · crackedINSPECTION TYPE: 2C RT UNDERWING ACCESS PANEL (636AB) LANDING HAS 2 FASTENER HOLES WITH CRACKS.REPAIRED CRACKED RT UNDERWING ACCESS PANEL (636AB) LANDING, IAW SRM 57-20-02 REPAIR 5 FIG 202 (MINOR).SDR 2020F00424Splice Plate · damagedNON-ROUTINE 3018.0330 DISCREPANCY: LEFT WING LEADING EDGE LOWER STRUCTURE AT WS 416 BENT AND CRACKED. CORRECTIVE ACTION: REPAIRED LEFT WING LEADING EDGE LOWER STRUCTURE AT WS 416 IAW EO NR 20449-1 WITHOUT ANY DEVIATIONS.SDR SWAA2021060920229Former · crackedCRACKED FAIRING FORMER ON RIGHT WING FIXED LEADING EDGE AT INBOARD END. / REMOVED CRACKED FAIRING FORMER AT R/H WING FIXED L/E I/B END PER SRM 51-40-02 AND LOCATED AND DRILLED REPLACEMENT FAIRING FORMER PER SRM 51-40-05 AND DWG. 116A3118. OK TO INSTALL. LEAD 1SDR IPXA2020102361591Former · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE RIB/FORMER IS CRACKED AT STA XOS 643.590. REPAIRED CRACKED RT WING FIXED LEADING EDGE FORMER, IAW VT-SAA EA 011-5740-01-A8620 REV I/R AND UPS EO MD11-5740-78271-A. (MAJOR)SDR IPXA2020102361590Former · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE RIB/FORMER IS CRACKED AT STA 584.891. REPAIRED CRACKED RT WING FIXED LEADING EDGE FORMER AT STA XOS 584.891, IAW VT-SAA EA 011-5740-01-A8601 REV I/R AND UPS EO MD11-5740-78269-A. (MAJOR)SDR SWAA2020123139041Panel · looseRT WING TRAILING EDGE DEFLECTION CONTROL RIB UPPER FIXED PANEL ATTACHED FASTENERS LOOSE, SERRATE PLATE SIGN OF WEAR. ACCOMPLISHED RT WING TRAILING EDGE DEFLECTOR CONTROL RIB FIXED UPPER PANEL REPAIR, REF B737-7 SRM 57-51-02-2R-4 FIG 202 DETAIL 4-A.SDR SWAA2021042720157Bonding Strap · corroded***CORROSION*** RH WING FWD BOOST PUMP AT UPPER BONDING STRAP APPROX LE STA 124 IFSS 120.00 WBL 94.24 / REPAIRED RH WING FWD BOOST PUMP AT UPPER BONDING STRAP APPROX LE STA 124 IFSS 120.00 WBL 94.24 IAW SWA EA 20-157-02051 REV IR AND ATS ER 20-03390 REV IRSDR SWAA2021051323764Plate · crackedRIGHT WING; WAFFLE PLATE IS CRACKED. O/B OF HYD ACCESS PANEL 651DB / REMOVED AND REPLACED RIGHT WING; WAFFLE PLATE IS LOCATED O/B OF HYD ACCESS PANEL 651DB PER SRM 51-40-02.SDR IPXA2020101061142Former · crackedINSPECTION TYPE: 2C RT WING FIXED LE COMPARTMENT FORMER STRUCTURE CRACKED AT APPROXIMATELY STA XOR 559. REMOVED CRACKED FORMER, FABRICATED, AND INSTALLED IN RT WING FIXED LEADING EDGE COMPARTMENT AT STA XOR 559, IAW SRM 51-33-01 (MINOR).SDR IPXA2020101061141Strap · crackedINSPECTION TYPE: 2C RT WING FIXED LEADING EDGE COMPARTMENT SPLICE STRAP AT APPROXIMATELY XOR 780, IS CRACKED. REMOVED CRACKED SPLICE STRAP, FABRICATED AND INSTALLED IN RT WING FIXED LEADING EDGE AT XOR 789, IAW SRM 51-33-01 (MINOR).SDR JGVR20200922001Drag Angle · corrodedLEFT WING AFT DRAG ANGLE HAS 2 AREAS OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 8 AREAS OF VERIFIED CORROSION ON MIDDLE DRAG ANGLE OUTBOARD EDGE. RIGHT UPPER WING AFT DRAG ANGLE HAS 1 AREA OF VERIFIED CORROSION ALONG OUTBOARD EDGE AND 7 AREAS OF VERIFIED CSDR FDEA202009162224Former · crackedLEFT HAND WING - LEADING EDGE FORMER AT APPROXIMATELY XORS 980 , BEHIND #8 SLAT CENTER AREA , FOUND CRACKED AS MARKED. LEFT HAND WING LEADING EDGE FORMER AT APPROXIMATELY XORS 980 , BEHIND #8 SLAT CENTER AREA REMOVED AND REPLACED WITH FABRICATED FORMER AS SDR FDEA202009162223Former · crackedRIGHT HAND WING, FIXED LEADING EDGE FORMER BETWEEN XOS 1010-1030, BEHIND NR 8 SLAT INBOARD SIDE, FOUND CRACKED AS MARKED. RIGHT HAND WING FIXED LEADING EDGE CRACKED FORMER BETWEEN XOS 1010-1030, BEHIND NR 8 SLAT INBOARD SIDE. REMOVED AND REPLACED WITH FABRICSDR SWAA2020093015953Panel · looseLEFT WING DEFLECTION CONTROL RIB ATTACH FASTENERS TO THE UPPER FIXED TRAILING EDGE PANEL LOOSE AND CAUSING WEAR DAMAGE. ACCOMPLISHED REPAIR ON LT WING DEFLECTOR CONTROL RIB UPPER TAB AND BEAM, IAW SRM 57-51-02-2R-1 AND 4.SDR IPXA2020091416123Skin · crackedINSPECTION TYPE: 2C LT INBOARD WING T/E BLISTER FAIRING CRACKED AFT OF LT MLG. REPAIRED LT INBOARD WING T/E CRACKED BLISTER FAIRING, IAW SRM 51-31-01 AND 51-35-01 (MINOR).SDR SWIA2020091152462Cap · out of limitsWHILE COMPLYING WITH DETAILED INSPECTION OF WINGLET AND HORIZONTAL END CAP STATIC WICKS, FOUND THE RIGHT WINGLET TOP; THE RIGHT HORIZONTAL END CAP OUTBOARD AND INBOARD; THE LEFT HORIZONTAL END CAP INBOARD AND LEFT WINGLET TOP; MIDDLE AND BOTTOM STATIC WICKS OUSDR JGVR20200909001Clamp · out of positionFOUND VACUUM WASTE TUBE CLAMP TO BE CONTACTING UPPER WING PLANK DURING COMPLIANCE WITH CUSTOMER BULLETIN 206. REMOVED PRIMER IN CHAFED AREA AND PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. APPLIED ALODINE AND PRIMER TO REPAIR AREA PER GULFSTREAM W/O INSDR FDEA2020090982147Former · crackedRT WING LEADING EDGE INTERNAL FORMER CRACKED ON OUTBOARD SIDE OF SLAT NR 8 OUTBOARD ACTUATOR. REMOVED AND REPLACED RT WING RIB FORMER AT W/S 480, PER FEDEX B767 SRM 51-40-02 & BAC DWG 114T2511. LOCATED AND DRILLED PER FEDEX B767-SRM 51-40-05.SDR FDEA2020090972139Bracket · crackedLT WING, LEADING EDGE CAVITY FWD FORMER BRACKET CRACKED, LEADING EDGE STA 430. REMOVED CRACKED FORMER BRACKET IAW B767 SRM 51-40-02, MATERIAL ID 2024T3 .040" IAW BAC DWG 114T2170. FABRICATED RIB FORMER BRACKET, IAW BOEING DWG 114T2170 REV ALODINED, IAW BOEINSDR FDEA2020090972138Splice Plate · crackedRT WING LEADING EDGE INTERNAL SPLICE PLATE CRACKED APPROX 1' OUTBOARD OF SLAT #8 OUTBOARD ACTUATOR. REMOVED AND REPLACED SPLICE P/N 114T2800-165, PER BAC DWG 114T2800 REV G.SDR FDEA2020090922082Former · crackedLT WING LEADING EDGE CAVITY FWD FORMER STRAP CRACKED LEADING EDGE STA 505. REMOVED AND REPLACED LT WING LEADING EDGE CAVITY FWD FORMER STRAP LES 505 PN 114T2800-165 SEAL STRIP PO NR 979532.1, IAW BAC DWG 114T2800 REV G, B767 SRM 51-40-02.SDR QXEA2020090200271Stiffener · crackedWHILE CLEANING GREASE ON LT WING, A SUSPECTED CRACK WAS FOUND AT WS #226, EXTENDING FROM THE AFT EDGE 4 INCHES FORWARD ON BOTTOM SKIN. C/W W/O 287639. STOP DRILLED CRACK AT WS #226 AND APPLIED TAPE. PERFORMED HFEC INSP TO BONDED STIFFENER STRAP AT LT WING O.BSDR P5CA2020090410298Fill Port · corrodedLT OVERWING FUEL PORT HAS CORROSION ON MATING SURFACE FOR FUEL CAP HOUSING. REPAIRED LT OVERWING FUEL PORT, IAW FAS EA 20021 REV. IR.SDR FXGA202009012010Doubler · crackedLANDING DOUBLER REPLACEMENT BETWEEN W/STA 167R AND 242R PER SB 799. TO REPLACE A CRACKED LANDING DOUBLER PER SB 799. REMOVE AND REPLACE CRACKED LANDING DOUBLER PER INSTRUCTIONS IN DOUGLAS SB 799.SDR FDEA202008302447Former · crackedLT WING LEADING EDGE, PER WIP EA NR 8-5710-T0356192 P1 STEP NR 2, FOUND CRACK INDICATION WITH HFEC APPROXIMATELY .25" IN LENGTH OF FORMER AT XOS 643, EMANATING FROM RADIUS TO FASTENER HOLE AREA ACCESSIBLE AFTER TRIMOUT OF CRACKED INBOARD FLANGE. REPAIRED LEFTSDR FDEA202008302445Former · crackedLT WING LEADING EDGE, PER WIP EA NR 8-5710-T0356192 P1 STEP NR 2, FOUND CRACK INDICATION WITH HFEC, APPROX .25" IN LENGTH OF FORMER AT XOS 643, EMANATING FROM RADIUS TO FASTENER HOLE, AREA ACCESSIBLE AFTER TRIMOUT OF CRACKED INBOARD FLANGE. THIS SDR ENTERED ISDR A6WA202009227292Shroud · crackedTWO CRACKS FOUND ON RT LEADING EDGE PANEL 630KL AT AROUND W/S 314.50. THE FIRST CRACK WAS 8.44" FROM THE INBOARD EDGE THAT MEASURED .7" AND THE SECOND CRACK WAS 6.75" FROM THE OUTBOARD EDGE THAT MEASURED 1.3". AIRCRAFT REMOVED FROM SERVICE. REMOVED SHROUD (SDR SWAA2021051313979Plate · crackedLT WING WAFFLE PLATE CRACKED I/B OF #3 FLAP TRACK / REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-40-02
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