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 CHQA20130924353Torque Box · crackedDURING INSPECTION, THE LT WING LOWER SURFACE INBD TORQUE BOX, AROUND SIX FASTENER HOLES WERE FOUND CRACKED. TORQUE BOX REPAIRED IAW ETD 2013-145-042825.SDR USAA2013091000013Shroud · chafed2S CHECK - CHAFING ON RT WING SHROUD BOX LOWER SKIN PANEL BETWEEN RIB WX531 TO WX666 BETWEEN 14" TO 32" FROM INBD END ON SHROUD BOX T/E. REPAIRED RT WING SHROUD BOX LOWER SKIN PANEL IAW EA 505531.SDR FDEA201309082163Structure · gougedGOUGE DAMAGE TO RT WING TIP FWD OF WINGLET. REPAIR CARRIED OUT IAW EA 6-5700-T0207148.SDR USAA2013090900021Shroud · chafed2S CHECK, CHAFING ON LT WING SHROUD BOX LOWER SKIN PANEL BETWEEN RIB WX531 TO WX666. REPAIRED LT WING SHROUD BOX LOWER SKIN PANEL IAW EA 505530.SDR UHLA2013090700422Structure · crackedLEVEL 2 CORROSION ON RT WING CRACK-LIKE INDICATIONS IN A2 HOLE. REAMED RT WING A2 HOLE TO .622 REMOVING CRACK INDICATIONS. INSTALLED BUSHING IN A2 HOLE.SDR R61A201309020853Rib · crackedWHILE IN HEAVY CHECK, CRACK FWD LT WHEEL WELL PANEL. MX R & R LT RIB, PN 170-08669-005. ACFT REMAINS AT FOR COMPLETION OF HEAVY CHECK.SDR ASOA20130901218VBushing · migratedDURING C-CHECK, LT AILERON OTBD PCA ATTACHMENT FITTING OTBD LUG, OTBD HAT BUSHING MIGRATED. MX R & R THE LT AILERON OTBD PCA ATTACHMENT FITTING IAW EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR BQVD20130823002Fitting · corrodedINSPECTION OF WING STRUT ATTACH FITTINGS WAS COMPLIED WITH. LT WING STRUT LOWER ATTACH FITTING WAS FOUND CORRODED.SDR ABXA20130820507Structure · corrodedUPPER PANEL ATTACH CAP ON RIB FROM REAR SPAR TO T/E AT WS 433 HAS CORROSION UNDER NUTPLATE. FABRICATED NEW CAP IAW DWG 113T1510, HEAT TREATED TO T6 IAW BAC 5602, TABLE 1, PAGE 12 AND 17 NOTE C, INSTALLED NEW CAP IAW SRM 51-40-02 AND AMM 20-11-00D.SDR CALA2013081990529Seal · out of alignmentA RUBBER SEAL BETWEEN RT AILERON AND WING APPEARS TO BE LOOSE. REPLACED MISSING FASTENER AND REALIGNED SEAL.SDR W9FA2013FA0000467Structure · corrodedWHILE PERFORMING AN INSPECTION, DISCOVERED CORROSION OF HARDWARE AND PITTING IN THE BORE OF THE ATTACH POINT ON THE RT WINGLET. BEYOND THE MFG LIMITS. CORROSION WAS DUE MOISTURE INTRUSION THROUGH THE SEALANT COVERING THE ATTACH POINTS.SDR A6WA2013082741167Structure · crackedRT WING L/E UPPER EDGING IS CRACKED ON OTBD SIDE. REMOVED UNSERVICEABLE EDGING & FABRICATED AND INSTALLED NEW SERVICEABLE EDGING.SDR 2013FA0000463Strut · corrodedLT WING STRUT UPPER ATTACH FITTING AND RT WING STRUT LOWER ATTACH FITTING WERE FOUND CORRODED. REPLACED.SDR 2013FA0000462Strut · corrodedWING STRUT LOWER ATTACH FITTINGS WERE FOUND CORRODED. REPLACED.SDR DU4R2013004Angle · damagedDURING SCHEDULED INSPECTION, FOUND ELONGATED HOLE IN LOWER RT WING ANGLE FITTING AT XRS 69 BETWEEN S15-16R.SDR ASOA2013082108888Link · crackedRT AFT WING LINK UPPER AND LOWER BEARINGS ARE CRACKED AND TOUCHING ATTACH FITTING. REPAIRED IAW SB 670BA-57-016, REV B. REPAIR CLASSIFIED AS MAJOR.SDR ASOA2013082108887Bearing · crackedLEFT AFT WING LINK UPPER AND LOWER BEARINGS ARE CRACKED AND TOUCHING ATTACH FITTING. REPAIRED IAW REO 670-57-27-398-01 AND SB 670BA-57-016, REV B, DEC 07/2012. REPAIR CLASSIFIED AS MAJOR.SDR REXA2013072401105Structure · crackedA FASTENER HOLE WAS FOUND CRACKED AROUND THE RT FUEL BOOST PUMP MEASURING 0.05" LONG. REPAIRED IAW REO 601R-57-21-169.SDR UHLA2013072200334Structure · damagedRIGHT WING AFT SPUR DAMAGED AT HYD SYS NR 1 PRESSURE PASS THROUGH. REMOVED DAMAGE, FABRICATED BUSHING, INSTALLED. MAJOR REPAIR.SDR ABXA20130717488Structure · corrodedCORROSION UNDER NUTPLATE ON WING L/E AFT OF NR 8 SLAT LES 466. R & R OUT OF LIMIT DAMAGE. IAW SRM 51-70-11, DETAIL II. ACFT WAS GROUNDED.SDR ABXA20130715486Beam · corrodedCORROSION AROUND NUTPLATE ON WING L/E AT L/E S682 AFT OF INBD END OF NR 10 SLAT. REPAIRED AREA IAW SRM 51-70-11, REPAIRED AREA IAW SRM 51-70-11, ACFT WAS GROUNDED.SDR ABXA20130711485Beam · corrodedCORROSION ON WING L/E WEB AT LES 695 AFT OF NR 10 SLAT. REPLACED NOSE BEAM IAW SRM 51-40-02, ACFT WAS GROUNDED.SDR UALA2013071204885Seal · missingON EXTENSION OF FLAPS FOUND RT WING INNER FLAPERON OTBD SEAL MISSING. REPLACED MISSING SEAL.SDR DU4R20130711001Structure · looseDURING SCHEDULED INSPECTION, FOUND RT WING TIP (LOWER SIDE, AFT, INBD) HAS LOOSE/SMOKING RIVETS.SDR ASOA2013082108882Link · damagedDURING INSPECTION OF RT WING, LINK WAS FOUND TO BE TOUCHING ON UPPER AND LOWER FITTING. COMPLIED WITH EC/TC SB670BA-57-016 IAW PART A SB 670BA-27-016, REV B, DEC 07/2012. REPAIR CLASSIFIED AS MAJOR.SDR USAA2013080500017Strut · corrodedDURING 2S CHECK - CORROSION WAS FOUND ON RT INTERCONNECTING STRUT AT WS 4862, RIB 9. REPLACED RT INTERCONNECTING STRUT IAW CMM 57-52-17.SDR USAA2013080500016Strut · corrodedDURING 2S CHECK, CORROSION FOUND ON LT INTERCONNECTING STRUT AT WS 4862, RIB 9. REPLACED LT INTERCONNECTING STRUT IAW CMM 57-27-17.SDR CA130705003Collar · missing(CAN) DURING A 16000 HR WING INSPECTION OF THE WING CRITICAL FASTENER, THE PRC WAS REMOVED TO EXPOSE THE STEM OF THE HY-LOK FASTENER. UPON INSPECTION IT WAS NOTED THAT NO COLLAR WAS ON THE HY-LOK. THIS IS THE FIRST INSPECTION OF THIS PART SINCE MFG AND THE FSDR CHQA20130705269Fastener · misinstalledDURING HEAVY MX 1 FASTENER ON THE THE LT WING AT THE TORQUE BOX EXCEEDS CLASS 3 FIT TOLERANCE. THE FASTENER WAS REPAIRED IAW ETD 2013-145-014014.SDR REXA2013070301403Panel · chafedPANEL 584EB IS CHAFED. LOCATED & DRILLED NEW PANEL IAW SRM 51-40-11.SDR 2013FA0000382Bracket · crackedTHE AILERON HINGE REINFORCING BRACKET FOUND SEVERELY CORRODED AND CRACKED.SDR SIMA20130702003Bushing · corrodedDURING MX BASE VISIT INSPECTION FOUND THE LT AILERON OTBD HINGE FITITNG BOTH HAT BUSHINGS PITTED. ACFT REMOVED FROM SERVICE. R & R LT AILERON OTBD HINGE FITTING IAW EO EM-27MR-112. RETURNED TO SERVICE.SDR ASAA2013070195609Structure · dentedLEFT AFT WING TIP DAMAGED AT STATIC WICK. ACFT GROUNDED. R & R MID AND AFT WING TIPS IAW AMM 57-21-11-404-013, SEAM C.SDR ASAA2013070195422Structure · dentedLEFT AFT WING TIP DAMAGED AT STATIC WICK. ACFT GROUNDED. R & R MID AND AFT WING TIPS IAW AMM 57-21-11-404-013.SDR REXA2013062801305Panel · chafedPANEL 684EB IS CHAFED. REPAIRED IAW REO 690-57-52-146.SDR REXA2013062801304Panel · chafedPANEL 584GB IS CHAFED. BLENDED CHAFED AREA IAW SRM 57-52-01, OPS CHECKED IAW AMM 27-52-00 CHECKED GOOD.SDR CALA2013062600455Pressure Panel · crackedRIGHT WHEEL WELL , REAR SPAR PRESSURE WEB HAS A 2 INCH CRACK BETWEEN RBL 40 AND 64 AND WL 200.6 AND 192.0. REPAIRED IAW SRM 57-10-10, REPAIR 3.SDR FDEA201306201356Angle · crackedRIGHT WING KREUGER FLAP CAVITY AT FIXED L/E HAS A SUSPECTED CRACK AT RIB, 8 AT OTBD OF KREUGER ACTUATOR. REPAIRED IAW SRM 51-72-10 REF DWG A57241993.SDR FDEA201306201358Web · crackedNDT INSPECTION OF CENTER WING BOX, CENTER SPAR AT CUTOUT DOUBLER RUNOUT L/H AT FR. 44, CRACK FOUND AT R/H LOWER HOLE 4 , INDICATION 25 PERCENT FSH 10MM FROM AFT FACE AT APPROXIMATE VERTICAL POSITION. REPAIRED OUT IAW EA 6-5710-167465.SDR ASAA2013061695428Beam · chafedRT MLG BEAM CHAFED ON LOWER SIDE. ACFT GROUNDED. C/W BLEND REPAIR OF RT MLG BEAM IAW EA 400-57EA-10584, REV NEW DATE ISSUED 6-26-13.SDR DALA1502273254Structure · noneREFUEL APERTURE/WING ELEC BOND, INSPECT, IDENTIFIED AS MAJOR IAW AA 5724-01007.SDR UALA2013061103993Structure · damagedRT WING TANK LANDING HAS TWO MISDRILLED HOLES.SDR CA130831001Hinge Bracket · corroded(CAN) ON ACCOMPLISHING ANNUAL INSPECTION, FOUND DIS-COLOURED SPOT ON BOTTOM OF HINGE BRACKET PIVOT. ON APPLYING "MAULE TESTER" FOR STRENGTH TEST. TUBE COLLAPSED. INSPECTION FOUND THE SUPPORT TUBE WAS NOT DRILLED FOR DRAINAGE. THE NEW REPLACEMENT BRACKET WASSDR UALA2013060703971Seal · damagedSEAL STRIP BETWEEN INBD SIDE RT AILERON AND OTBD SIDE OF /FLAP TORN AND WEDGED BENEATH AILERON. REPLACED DAMAGED SEAL.SDR ABXA20130605439Skin · corrodedCORROSION ON UPPER WING SURFACE ALONG SKIN T/E ABOVE REAR SPAR FROM INBD EDGE OF OTBD AILERON TO APPROX WS 990.5. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I. WS LOCATION FROM 912 TO 1008; ACFT WAS GROUNDED.SDR UALA2013060603949Seal · damagedNR 1 RT MOVABLE FAIRING - AFT INBD OF FAIRING MISSING 5" OF SEAL. REPAIRED.SDR ASOA2013061903841Fitting · crackedJACK PAD FITTING INBD FASTENER HOLE HAD CRACK INDICATION PRIOR TO FINAL SIZE OF HOLE. REPAIRED IAW REO 601R-57-21-1948, REV P1 DATED 2JUN2013 AND REO 601R-57-21-130, REV J.SDR U2RA201306010002Structure · crackedLEFT WING L/E CAVITY LOWER FIXED PANEL AT WS 850 FOUND STRUCTURE CRACKED. CRACK IS 1.5" IN LENGTH.SDR U2RA201306010001Support · crackedLEFT WING LEADING EDGE CAVITY AT WING STATION 780 FOUND SUPPORT ROD FRACTURED, REF NRC MOL0217 GENERATED FROM TASK 57-804-01-01.SDR DALA13026310126Fairing · delaminatedLEFT WING INBD MAIN FLAP L/E OTBD END FAIRING DELAMINATED. LT WING INBD MAIN FLAP L/E OTBD END FAIRING COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01, REPAIR 1, SRM 51-70-05.
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