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 DALA2016080105704Splice · crackedCRACKED SPLICE ON FIXED LEADING EDGE STRUCTURE XFS=194.850 ON RT WING. THE DOUBLER WAS REPLACED IAW ER/A 379404-14MA REV.A.SDR UIEA2016072100614Splice · corrodedCORROSION ON SPLICE LT WING OUTBD LE LWR FIXED PANEL BUTTJOINT. REPLACED THE SPLICE IAW SRM 51-40-02-0G-0 REV.77 AND DWG 65B11862 SHEET 2 REV.F.SDR IXXA20160821056Splice Plate · corrodedLEFT WING LEADING EDGE LOWER CHORD SPLIT ON EDGE WHERE NUMBER 5 SLAT INBOARD DRIVE ROD DOOR CONTACTS. REMOVED DAMAGE SPLICE PLATE AT LEFT WING STATION 330.475. INSTALLED NEW SECTION OF SPLICE PLATE IN ACCORDANCE WITH 472222REA01 AND SRM 51-40-02. AIRCRAFT GROSDR IPXA2016080106544Former · crackedINSPECTION TYPE: 1C, LEFT OTBD WING L/E COMP. AT XOS 585 FORMER IS CRACKED. REMOVED, FABRICATED AND REPLACED THE FORMER IAW DWG ARB 2931 AND SRM 51-33-01.SDR COEA2016071103917Brace · corrodedRIGHT WING RIB 8 FLAP SUPPORT BEAM SIDE BRACE HAD CORROSION. REPLACED SIDE BRACE.SDR SWAA2016072754281Support Fitting · crackedRIGHT WING AFT SUPPORT FITTING ON REAR UPPER CHORD CRACKED AT RSS 222.22. R & R IAW SRM AND DWG.SDR SWIA201642391Panel · chafedPANEL 684ET CHAFED. INSTALLED NEW PANEL 684ET IAW SRM.SDR SWAA2016070653557Plate · crackedLEFT WING LOWER TRAILING EDGE WAFFLE PLATE JUST INBOARD OF NR 1 PYLON, AFT TIP CRACKED. R & R WAFFLE PLATE IAW EA.SDR SWAA2016070253736Plate · crackedRIGHT WING LOWER TRAILING EDGE WAFFLE PLATE CRACKED JUST INBOARD OF NR 2 PYLON AFT TIP. R & R WAFFLE PLATE IAW SRM.SDR IPXA2016070705524Stringer · crackedINSPECTION TYPE: 3C, LEFT WING FIXED L/E COMPARTMENT STRINGER AT XOS.789-795 IS CRACKED. REPAIRED CRACKED STRINGER IAW SRM 57-40-03 REPAIR 2 FIG. 201. (MAJOR)SDR IPXA2016070705508Angle · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E SPLICE ANGLE IS CRACKED AT XOS. 584. REMOVED, FABRICATED AND REPLACED THE ANGLE IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)SDR IPXA2016070105274Doubler · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 789-795. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15, FIG 203.(MAJOR)SDR IPXA2016063005258Doubler · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS 906-911.5. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG.203.(MAJOR)SDR IPXA2016063005257Doubler · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED BETWEEN XOS.789-795. REPAIRED THE DOUBLER IAW SRM 57-40-02 REPAIR 15 FIG. 203 (MAJOR)SDR SWAA2016071453803Arm · crackedRIGHT WING TRANSVERSE WEB CRACKED INBOARD OF MAIN FLAP ROLLER SUPPORT ARM. R & R THE SUPPORT ARM IAW SRM.SDR SWAA2016080254409Bulkhead · crackedRIGHT WING INBOARD FLAP INBOARD TRACK FAIRING ASSEMBLY BULKHEAD CRACKED. REPAIRED THE BULKHEAD IAW EA.SDR DALA2016060204339Structure · corrodedRT WINGLET INTERFACE BS 0 HAS PITTING ABOVE BOLT HOLE NR 6. ACCOMPLISHED PERMANENT REPAIR ON RT WINGLET INTERFACE ABOVE BOLT HOLE NR 6 IAW ER/A 547302-14, REV ORIG.SDR REXA2016060100962Panel · gougedPANEL 592BB HAS A GOUGE IN IT, NEEDS FURTHER INVESTIGATION. REMOVED GOUGED PLATE GUIDE FROM PANEL 592BB & INSTALLED NEW SERVICEABLE PLATE GUIDE IAW SRM 51-40-06, 51-40-11 & 51-42-06.SDR SWAA2016070553465Gusset · crackedLEFT WING UPPER TRAILING EDGE PANEL SUPPORT GUSSET CRACKED ABOVE THE NR 1 PYLON AFT TIP AT TRANSVERSE WEB ATTACH POINT. R & R THE GUSSET IAW SRM.SDR IPXA2016061004444Doubler · chafedINSPECTION TYPE: 1C, RT WING FIXED LEADING EDGE EXTERNAL DOUBLER HAS CHAFE DAMAGE BS XOS 442-467 ACCOMPLISHED BLEND REPAIR ON RT WING FIXED L/E EXTERNAL DOUBLER IAW EA 011-5700-01-A6289, REV I/R AND EO MD11-5700-60939-A.SDR IPXA2016052803988Beam · crackedINSPECTION TYPE:3C, VERTICAL SUPPORT BEAM CRACKED IN RT WING T/E ADJACENT TO INBD AILERON AREA. REMOVED FABRICATED AND INSTALLED REPLACEMENT BEAM IAW DWG ARC0472 AND SRM 51-31-01.SDR IPXA2016052603883Support · crackedINSPECTION TYPE: 3C, LEFT WING T/E INDISE PANEL 541JB, OTBD VERTICAL TEE ANGLE IS CRACKED AT LOWER END. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IN SIDE PANEL 541JB.SDR KC8A20160510002Casting · crackedDURING ROUTINE INSPECTION THE LT TIP TANK AFT CASTING, INTERNAL, WAS FOUND CRACKED. CRACK TO BE REPAIRED IAW FAA FORM 8110-3, DWG NR 12235-027, REV F, DATED 2/21/2000.SDR SWAA2016062853302Beam · crackedRIGHT WING LOWER T/E BEAM CRACKED AT RSS 287. R & R BEAM IAW SRM.SDR DALA2016050603704Bushing · corrodedCORROSION FOUND ON BUSHINGS AT RT OVERWING HEATER BLANKET REAR SPAR. BUSHINGS 1, 2, 6, 7, 8, 9 AND 10 WERE REPLACED IAW SRM 51-30-10 AND BUSHINGS 3, 4 AND 5 WERE REPLACED IAW ER/A 545121-14AD, REV A, ETI-88-16-165, R8.SDR SWAA2016050951610Angle · crackedRIGHT WING OTBD ANGLE CRACKED FOR FIXED UPPER TE PANEL AT NR 6 CANOE. R & R ANGLE IAW SRM.SDR R61A201605010330Bolt · corrodedDURING HEAVY CHECK , LT WING NR 5 MFS PCV TOP BOLT ATTACHING HARDWARE IS CORRODED. MX R & R LT WING NR 5 MFS PCV TOP BOLT ATTACHING HARDWARE IAW AMM 27-65-01, NAS6212-31D, BOLT.SDR DALA2016050403728Structure · damagedDURING REMOVAL OF FUEL TANK SUMP DRAIN VALVE BUSHING THE HOLE WAS FOUND TO BE ELONGATED BEYOND DWG 112N4101 LIMITS AND DOES NOT ALLOW THE CORRECT INSTALLATION OF NEW SUMP DRAIN VALVE BUSHING.SDR IPXA2016041502147Deflector · crackedINSPECTION TYPE:5Y, PANEL 672LB, DEFLECTOR ASSY, CRACKED. R & R DEFLECTOR ASSY PANEL 672LB IAW AMM 27-54-41.SDR DALA2016033002636Structure · crackedRIGHT WING LOWER L/E CRACKED AT OTBD FWD CORNER OF FUELING BAY. REPAIRED IAW SRM 57-20-01.SDR ABXA20160317057Beam · crackedBEAM BELOW HYD BAY ACCESS DOOR 447BR CHAFED & CRACKED AT FWD END. REMOVED OLD BEAM & INSTALLED NEW BEAM IAW 51-40-02. CRACKED 1", PN 313T1380-209, SN NSN, PART NAME BEAM, EXACT FS & BS LOCATION ON ACFT, ENG BS O.OO - 10.0, EXACT STRINGER & WS LOCATION ON ACFSDR DALA2016031502168Ballscrew · corrodedNR 6 BALLSCREW CORRODED. INSTALLED ON AMDS CARD.SDR DALA2016030701710Structure · crackedCRACK ON RT WING L/E BS XOS=286. REPAIRED IAW ER/A 397957-14MA, REV ORIGINAL.SDR 2016FA0000114Structure · corrodedCORROSION IN LT AND RT MLG WHEEL WELLS. INCLUDING ON AFT SPAR.SDR IPXA2016031600814Former · crackedINSPECTION TYPE:3C, RT WING FIXED L/E FORMER CRACKED XOS 996. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB 2920, SRM 57-00-00, 51-35-01, 51-33-01.SDR IPXA2016031500763Former · crackedINSPECTION TYPE: 3C, RT WING FIXED L/E FORMER CRACKED XOS 996. REMOVED FABRICATED AND INSTALLED REPLACEMENT FORMER IAW DWG ARB2920, SRM 57-00-00, 51-33-01, 51-35-01.SDR ABXA20160302039Failsafe · crackedRIGHT WING FAILSAFE BOTTOM HOLE CRACKED. ACCOMPLISHED TRIM OUT & REWORK OF FAILSAFE STRAP IAW DOCUMENT 470080RD04 STEPS 1 - 9. SEE 470080RD04 FOR ALL OTHER REWORK & ASSEMBLY STEPS. CRACKED LENGTH .500, PN 145T2524-20, PART NAME, FAILSAFE STRAP, SN NSN, FS &SDR R61A201602040137Doubler · crackedDURING HEAVY CHECK, PREVIOUS REPAIR BELOW LT AILERON TOWER REPAIR IS CRACKED. MAINTENANCE R & R PREVIOUS REPAIR BELOW LT AILERON TOWER REPAIR IAW SRM 51-41-01, PN RAH53061 DOUBLER.SDR ABXA2016020223Beam · corrodedNUMBER 8 SUPPORT 123 BEAM, C FASTENER ONE EACH SHOWS CRACK INDICATION & CORROSION IN BOTTOM. REQUEST TECHNICAL ENGINEERING ASSISTANCE, REPAIRED HOLE ON THE NR 8 FLAP SUPPORT 1 - 3 BEAM IAW REA CO57-61926-MR. CORRODED LEVEL 2, PN 113T1313-8, PART NAME 1-3 BESDR ABXA20160202022Beam · gougedNUMBER 2 FLAP SUPPORT 1-3, BEAM HAS A GOUGE AROUND FASTENER HOLE. REPAIRED HOLE ON THE NR 2, 1 - 3 BEAM FOR THE NR 2 FLAP SUPPORT IAW REA CO57-61933-MR. PN 113T1314-15, PART NAME 1 - 3 BEAM. SN ABXV654, WS LOCATION, 616.2 - 616.2. ACFT WAS GNDED.SDR IPXA2016031100619Fairing · crackedINSPECTION TYPE:3C, RT WING L/E CRUISE PERFORMANCE FAIRING INBD WEB CRACKED. REPAIRED CRACKED WEB IAW EA 011-5754-01-A6100, REV. IR AND EO MD11-5720-60162-A.SDR IPXA2016030300298Doubler · crackedINSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 667-673. REPAIRED RT WING BEADED DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG. 203.SDR IPXA2016022900149Doubler · crackedINSPECTION TYPE:3C, RT WING L/E BEADED DOUBLER REPAIR, XOS 610-616, REQUIRES REPLACEMENT DUE TO TIME LIMITED ACCOMPLISHED BEADED DOUBLER TEMP REPAIR ON RT WING L/E BS XOS 610-616 IAW SRM 57-40-02, REPAIR 15, FIGURE 206.SDR IPXA2016030100216Doubler · crackedINSPECTION TYPE:3C, REF D-511308 AND D-511309. LT WING L/E EDGE BEADED DOUBLER REPAIR AT BS 584-589, REQUIRES PERMANENT REPAIR. REMOVED EXISTING BEADED DOUBLER REPAIR LT WS XOS 584-589. ADDITIONAL CRACKS FOUND. ACCOMPLISHED PERMANENT REPAIR IAW SRM 57-40-02,SDR IPXA2016030200251Doubler · crackedINSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED XOS 698 -703. REPAIRED RT BEADED DOUBLER XOS 698-703 IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA2016022499871Doubler · crackedINSPECTION TYPE:3C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS789. REPAIRED BEADED DOUBLER BETWEEN BS 789-795 IAW SRM 57-40-02, REPAIR 15, FIG. 203.SDR IPXA2016021899586Structure · crackedINSPECTION TYPE:3C, LEFT WING L/E PANEL LANDING CHORD CRACKED AT BS XORS 506. R & R LT WING PANEL LANDING CHORD DOUBLER IAW SRM 51-35-01, SRM 51-33-01 AND DWG ARB2933.SDR IPXA2016021899584Structure · crackedINSPECTION TYPE:3C, LEFT WING L/E PANEL LANDING CHORD CRACKED AT BS XORS506. R & R LT WING CHORD IAW SRM 51-35-01, SRM 51-33-01, AND DAC DWG ARB2933.SDR FDEA201601310404Former · crackedRIGHT WING LE CAVITY XOS 794, FORMER FOUND CRACKED. REPAIRED IAW DWG ARB3954 REV K, AND SRM 51-33-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR KPVA20160128Angle · corrodedLT WING LOWER SKIN ANGLE AT WING RIB 23 FOUND CORRODED INTERGRANULAR CORROSION WHILE AT 2YE CHECK. REPLACED IAW SRM 51-25-04.
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