JASC 5713
Service difficulty reports · 2,091
Reports filed under 5713 · Wing, Longeron/Stringer, 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 = '5713' 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 = '5713' 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 SWAA2023090584764Stringer · crackedCRACK FUEL TANK LOC. BTW RIB 21 AND RIB 22 STRINGER 9 INTERNAL AREA UPPER AFT POSITION AT RT WING 2023-470128<[01] REPAIRED STRINGER 9 INTERNAL AREA UPPER AFT POSITION BTW WSTA 617.0 TO WSTA 643.5 AND SKIN ATTACHMENT FLANGE AT RT WING I.A.W. EA 23-157-02451 ANSDR IPXA2023081793948Stringer · crackedINSPECTION TYPE:3C*** MAJOR REPAIR *** R/H WING FUEL TANK AT THE UPPER STRINGER #6 HAS A CRACKED BETWEEN STA XORS=981, XORS=1013 .REPAIRED CRACKED UPPER STRINGER #6 AT THE R/H WING FUEL TANK AT STA XORS=981, XORS=1013 IAW VTSAA EA 011-5710-01-B0051 I/R, UPS EOSDR IPXA2023080193769Stringer · crackedINSPECTION TYPE:4CR/H WING L/E LWR STRINGER HAS A CRACKED ON EXISTING DOUBLER JUST O/B OF SLAT TRACK #14 AT STA XOS=906.5607.REPAIRED EXISTING CRACKED DOUBLER AT THE R/H WING L/E LWR STRINGER JUST O/B OF SLAT TRACK #14 STA XOS=906.5607 IAW SRM 57-40-03 FIG.201SDR IPXA2023063093555Stringer · crackedINSPECTION TYPE:3C*MAJOR REPAIR* R/H WING #3 TANK UPPER STRINGER 1 IS CRACKED BETWEEN STA XORS=1012.55 AND 1042.350.REPAIRED CRACKED STRINGER 1 AT THE R/H WING #3 TANK UPPER SIDE BETWEEN STA XORS=1012.55 AND XORS=1042.350 IAW VTSAA EA 011-5710-01-A9977 I/R ANDSDR 2023FA0000271Stringer · crackedRH WING RIB 12, 6EA STRINGERS (STRINGER 26, 28, 29, 30, 31, 32) CRACKED. REFER ATTACHED AMAC OCCURRENCE REPORT NO. 760 REV. A AND BOEING SERVICE REQUEST NO. 4-5828495000.SDR SWI2023F00088Unknown · cracked*CRACK NOTED AT R/H WING REAR SPAR WEB ASSY AT WS53.60 COMMON TO CANNON PLUGS J410 AND J412 (MARKED) (C-CHECK RO 6/20/2023) REPAIRED R/H WING REAR SPAR WEB ASSY AT WS53.60 COMMON TO CANNON PLUGS J410 AND J412 REF MHIRJ REO 601R-57-51-1012 REV -- DATED 2SDR IPXA2023051993268Stringer · crackedINSPECTION TYPE:3C*MAJOR REPAIR* UPPER CENTER AUXILIARY TANK HAS CRACKED EXISTING REPAIR BETWEEN STA XCW =-46 AND XCW =-17 ON STRINGER 47.REPAIRED CRACKED STRINGER 47 AT THE UPPER CENTER AUXILIARY TANK BETWEEN STA XCW=-46 AND XCW=-17 IAW VTSAA EA 011-5710-01-SDR FDEA202304190691Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW -17 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR FDEA202304190690Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 17 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR FDEA202304190689Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 46.5 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6- 2-100.SDR FDEA202304190688Stringer · crackedUPPER AUXILIARY TANK - STRINGER 46 AT STATION XCW -17 FOUND CRACK. REPAIR CARRIED OUT AS PER EA# 1-5710-T0374206 PART 1. TITLE: WINGS - BASIC WING STRUCTURE - CENTER WING LOWER PANEL CRACK FOUND ON STRINGER S-46 BETWEEN XCW 17.000 AND XCW -17.000. REPASDR FDEA202304190687Stringer · crackedUPPER AUXILIARY TANK - STRINGER 46 AT STATION XCW 17 FOUND CRACK. REPAIR CARRIED OUT AS PER EA# 1-5710-T0374206 PART 1 TITLE: WINGS - BASIC WING STRUCTURE - CENTER WING LOWER PANEL CRACK FOUND ON STRINGER S-46 BETWEEN XCW 17.000 AND XCW -17.000. REPAIRSDR FDEA202304190686Stringer · crackedUPPER AUXILIARY TANK - STRINGER 42 AT STATION XCW 46.5 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA202304190683Stringer · crackedUPPER AUXILIARY TANK - STINGER 51 AT STATION XCW 46.5 FOUND CRACK. REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR SWIA2023041000206Unknown · crackedFOUND CRACKING AT RIGHT HAND WING LOWER WING PLANK AT APPROX WS 148.019, FWD OF REAR SPAR (C-CHECK RO 4/5/2023) COMPLIED WITH PARAGRAPH (B) OF AD 2002-03-14 BY REPAIRING CRACK ON THE RIGHT SIDE LOWER WING PLANK BEFORE FURTHER FLIGHT PER A METHOD APPROVESDR SWAA2023020898858Stringer · crackedFOR TRACKING PURPOSES ONLY. BOEING AOG REPAIR. CRACK ON LH WING UPPER NO. 8 STRINGER (PN 112A3208-5) AT WSTA 574; WL 231<[01] AS PER EA 23-157-00135; EDGE TRIM REPAIR DOCUMENTED ON BOEING FRR-03.?;[02] UPDATED MEASUREMENTS;[03] C/W;[04] C/W<BR>AUDIT C/WSDR 2023FA0000077Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN, FORWARD STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR DALA2023012400560Stringer · damaged(LOG 6985198) DURING INSPECTION FOUND STRINGER DAMAGED ON RT WING. INSTALLED A NEW STRINGER IAW DRAWING 116A4008 AND SRM 51-40-02.SDR 2023FA0000076Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN, FORWARD STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR 2023FA0000075Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN, AFT STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR SWAA2023020889637Stringer · crackedCRACK ON UPPER STRINGER U-9 INTERNAL CAVITY BETWEEN RIB 21 TO RIB 22 AT RT WING 2022-707430<[01] REPAIRED UPPER STRINGER U-9 INTERNAL CAVITY BETWEEN RIB 21 TO RIB 22 AT RT WING IAW EA 23-157-00142 AND EA 23-157-00142-WIP1 SEE INDIVIDUALS SIGN OFF BELOW;[02] RESDR 2023FA0000074Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN, FORWARD STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR 2023FA0000073Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN, AFT STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR 2023FA0000072Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN, AFT STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR 2023FA0000071Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN, FORWARD STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR 2023FA0000070Stiffener · crackedRIGHT WING BOTTOM INBOARD FORWARD SKIN STIFFENER FOUND CRACKED. REPLACED STIFFENER WITH NEW.SDR AALA202302078194Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING BOTTOM SKIN PANEL #1, LOWER FLANGE OF STINGER 2 BETWEEN RIB 5 AND 6. MAINTENANCE REPAIRED STRINGER PER EA 340803.SDR SWAA2023011062557Stringer · crackedLT WING (#1 TANK) AFT VENT STRINGER IS CRACKED AT STRINGER U-11 JUST I/B OF RIB #6 WSTA 228.25 AND EXTENDING O/B BEYOND RIB #6. JACKED AIRCRAFT IAW AMM 07-11-01-580-815. SHORING REQUIRES AN OK TO CONTACT AT FUSELAGE STATIONS 360; 662; & 1016. LH WING STATISDR IPXA2022102287362Stringer · crackedINSPECTION TYPE:SV, CRACK FASTENER HOLE ON L/H WING LOWER SURFACE WHEN PERFORM APB SB AP767-57-013 BETWEEN WSTA 962.2 AND WSTA 1018.2. REPAIR IAW BOEING SR:4-5635772766, EO B767-5710-84921 AND EO B767-5710-85030-A.SDR SWAA2022101272277None · crackedLEFT WING STRINGER U-8 CRACKED AT WSTA 564.50+10' / [01] PERFORMED HFEC INSP TO DETERMINE CRACK LENGTH WHICH IS 0.0250'. SEE ATTACHED PHOTO. CRACK PROPAGATES FROM FASTENER HOLE TO END OF STRINGER.;[02] INSTALLED EWIS PROTECCION AROUND OF REPAIR AREA AS PER AMMSDR KCSA202208301103Stringer · crackedSUPPLEMENTAL INFORMATION: 7.(C) CRACK LENGTH SHOULD BE .375 AND 7.(D) NUMBER OF CRACKS SHOULD BE 1SDR 2022FA0000481Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR 2022FA0000480Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR SWAA2022082943937Stringer · crackedWHILE REMOVING LH WING INBD LEADING EDGE FOUND STRINGER AT KRAS 206.32 TO KRAS 218 AT STRINGER ROW 2 CRACKED (116A4531-1) / [01] LOCATED AND DRILLED NEW STRINGER IAW SRM 51-40-05-0G-0 AND BOEING DWG# 116A4008 ID:0015 REV:F.;[02] LOCATED AND DRILLED NEW STRINGESDR 2022FA0000479Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR 2022FA0000478Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR FDEA202208111963Former · crackedL/E FORMER CRACKED AT STA 565 UNDER #4 L/E SLAT L/H WING MARKED WITH TAPE REPLACED L/E FORMER AT STA. 565. REF. E.A. H-5720-T-3670034 P1SDR FDEA202208081917Stringer · crackedLEFT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 666 STRINGER CRACKED. STRINGER REPAIR CARRIED OUT AT STRINGER AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 202 . REPAIR CLASSIFED AS MAJOR PER GMM 6-2-100.SDR FDEA202208081916Stringer · crackedLEFT WING - OUTBOARD LEADING EDGE COMPARTMENT STATION XOS 791 STRINGER CRACKED. STRINGER REPAIR CARRIED OUT AT STRINGER AS PER SRM 57-40-03-2R REPAIR 2 FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR SWAA2022082539251Stringer · crackedL/H FIXED LEADING EDGE STRINGER 15 INCHES FWD OF WING LEADING EDGE SPAR NEXT TO SEAL RIB IN ZONE 1A JUST INBOARD OF PYLON THE SECOND STRINGER IS CRACKED AT OUTBOARD END. / [01] REMOVED THE EXISTING CRACKED STRINGER PER SRM 51-40-02 AND DRILLED THE NEW STRINGERSDR 2022FA0000477Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR 2022FA0000476Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR SWAA2022080233814Stringer · crackedRIGHT WING UPPER SKIN AFT STRINGER END IS CRACKED BETWEEN RIB 19 AND 20. TRIMMED OUT CRACKED PORTION OF STRINGER END IAW SRM 51-10-02-0G. HFEC IAW NDT PART 6; 51-00-00 PROC 23 & 16; 53-30-00 PROC 5. NO DEFECTS NOTED. INSTALLED 3 EA. FASTNERS COMMON TO STRINGSDR SWAA2022080233815Stringer · crackedRIGHT WING UPPER SKIN AFT STRINGER END IS CRACKED BETWEEN RIB 21 AND 22. / [01] REMOVED 4 FASTENERS TO GAIN ACCESS I.A.W SRM 51-40-02-0G-0;[02] CUT OUT CRACKED AREA I.A.W SRM 51-10-02-0G-0;[03] VERIFIED ITEMS 1 AND 2;[04] HFEC IAW B737 NDT PART 6; 51-00-00 PROSDR 2022FA0000475Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR 2022FA0000474Stiffener · crackedRIGHT WING, INBOARD, BOTTOM, FORWARD SKIN, FORWARD AND AFT STIFFENERS CRACKED.SDR CALA2022070401633Structure · crackedAD 2019-11-02 EA 5310-06900 REV D OP 012 - 1EA HOLE FOUND CRACK AT WEB OF RH BS 1035 UNDERWING LONGERON LOWER CHORD AREA TRANSFER REF. NON-ROUTINE HX NRC WO.851401 AND ORIGINATED BY EMP NO. V893003 EA 5310-06900 REV D OP 011 LH UNDERWING LONGERON BS 1035 PART SDR CALA2022070401632Structure · crackedAD 2019-11-02, EA5310-06900 REV D OP 011, 1EA HOLE FOUND CRACK AT LH CENTER TANK FRONT SPAR LOWER CHORD TRANSFER REF. NON-ROUTINE HX NRC WO.851417 AND ORIGINATED BY EMP NO. V917699 EA 5310-06900 REV D OP 011 LH BS1035 UNDERWING LONERON AREA ITEM 2 AND ITEM 3,SDR FDEA202206281610Former · crackedRH WING O/B SLAT I/B FORMER CRACKED-MWT- REPAIRED IN REF. TO B767 SRM 51-40-02-0G AND B767 SRM 51-40-03-0GSDR LR7A2022062403162Longeron · crackedDURING SCHEDULED C-14 WHILE PERFORMING OTHER MAINTENANCE, FOUND THE CENTER DRY BAY CWS20R LONGERON WITH CRACKED HOLES AT FS517, WL269. / REPAIRED IAW LAC MEA 382-57-22-020. NR# 1000699797.
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