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 SWAA2022042691455Vapor Barrier · crackedRH VAPOR BARRIER CRACKED / [01] PERFORMED VISUAL INSPECTION AND TAP TEST INSPECTION AT LOWER RIGHT WEB (VAPOR BARRIER) FOUND CRACK RBL 54'' AND 10'' OF LENGTH. DRILLED STOP HOLES 0.25'' AT THE CRACK ENDS. REF B737-700 NDT PART 1 51-05-01 PARAGRAPH 5 AND SRM 57SDR YENA2022040600342Rib · crackedDURING HEAVY MAINTENANCE, ADDITIONAL WORK REQUEST OUT OF SCOPE IN REF. TO R.C. 57-40-012-1316 : CRACK ON RIB #22 AT LH FIXED LEADING EDGE; REPLACE PER EMB 190 SRM 51-41-01 AND 51-43-01 , SRM 51-43-04 REF QRO NR # 73 WO # N193JB/1880 /E190 / BRIDGE CHECK ACC SDR FDEA202204050865Former · looseLH WING LE AT STA 565 RIVETS ARE LOOSE. REPAIRED REF. E.A. TH-5720-T0367852P1.SDR FDEA202204050863Former · looseLH WING LE AT STA OSS499 RIVETS ARE LOOSE. REPAIRED IAW EATH-5720-T0367852P1SDR SWAA2022051090804Web · crackedCRACK INTERNAL CAVITY TRAILING EDGE WEB LOCATED ORRS 271 APPROX AT LT WING 2022-168778 / [01] REPLACED WEB AND FASTENERS LOCATED ORRS 271 APPROX AT LT WING IAW B737-700 SRM 51-40-02 DWG:115A2512 REV:-<BR><BR>SEE INDIVIDUAL SIGNOFFS BELLOW .;[02] REPLACED WEB ASDR FDEA202204010811Former · damagedSECONDARY WING STRCT - FIELD SERVICE EVALUATION LH SIDE OSS 441.596 REPL COMPLY WITH E..A. H-5720-T0367775 REV NO. POS. P1 INFO 31MAR22 19:01 REPAIRED DAMAGED FORMER REF EA H-5720-T0367775 P1 REPLACED BOEING FORMER 114T2120-5 WITH PN B67-57-002-01 USSDR COEA2022052711901None · chafedWO 235601 NR 600009 HEAVY CHECK COE/MAJOR REPAIR: R/H WING FWD SPAR LOWER CHORD BOTTOM SURFACE IS CHAFED AT R/H RIB 5. CORRECTIVE ACTION: BLEND REPAIR AT R/H WING RIB 5 PER SRAS ES_0158366_01...18915 ISSUE A, DATED 5/9/2022.SDR COEA2022052709901None · chafedWO 235601 NR 500012 HEAVY CHECK COE/MAJOR REPAIR: L/H WING FWD SPAR LOWER CHORD BOTTOM SURFACE IS CHAFED AT L/H RIB 5. CORRECTIVE ACTION: BLEND REPAIR AT RIB 5 STRIP SLAT PER SRAS ES_0158366_01...18914 ISSUE A, DATED 5/9/2022.SDR 2022FA0000178None · crackedWHILE PERFORMING A FUSELAGE SKIN REPAIR. THE RH WING WAS REMOVED. AN EDDY CURRENT INSPECTION WAS PERFORMED ON THE WING SPAR ATTACH FITTINGS, UPPER AND LOWER. FOUND A CRACK APPROX. 3 INCHES LONG ON THE UPPER SPAR FACE, ORIGINATING FROM THE OUTBOARD, FORWARD, SESDR SWAA2022041189154Angle · crackedCRACK FOUND IN A/C BAY ON UPPER ATTACH ANGLE AT 663 LBL 8 / [01] REMOVED ALL FASTENERS AND TRIMMED OUT DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5;14] INSTALLED REPAIR PARTS WITH PERMANENT FASTENERS IAW B737 SRM 57-10-10-2R-5;[15] VERIFIED ITEM 14; OSDR SWAA2022041189372Angle · crackedCRACK FOUND IN A/C BAY ON UPPER ATTACH ANGLE AT STA 663 RBL 8 / [01] REMOVED ALL FASTENERS AND TRIMMED OUT DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5;[02] PERFORMED DETAILED VISUAL INSPECTION OF REPAIR AREA; NO DEFECTS NOTED IAW SRM 57-10-10-2R-5;[0SDR FDEA202202290739Bracket · crackedRIGHT WING LEADING EDGE TORQUE TUBE SUPPORT BRACKET IS CRACKED AFT OF # 7 SLAT OUTBOARD SIDE AT LES 283.82 REMOVED & REPLACED TORQUE TUBE GUIDE BRACKET IAW BAC DWG 114T1240 REVISION ESDR FDEA202203280705None · crackedLH WING INTERNAL STRUCTURE FRONT SPAR LWR FLANGE FOUND 1EA CRACK JUST I/B OF RIB9 COMPLIED WITH FEDEX EA: 6-5710-T0367806 P1 REPAIRED LH WING INTERNAL STRUCTURE FRONT SPAR LWR FLANGE JUST I/B OF RIB9. THIS IS A CAT B REPAIR. THE FOLLOW UP INSPECTION REQSDR SWAA2022042588891Barrier · crackedCRACK IN LEFT HAND VAPOR BARRIER AT B.S. 663; L.B.L. 8; W.L. 150. / [38] INSTALLED L/H VAPOR BARRIER BS 663 IAW SRM 51-40-02-0G-0 AND DWG 111A1000 REV-B AND 111A1001 REV-B AND 111A7000 REV-A. REQ OK TO INSTALL STEPS 4; 12 AND 13;[39] OK TO INSTALL EXHAUST PNL SDR SWAA2022041188914Angle · crackedFOUND CRACK ON LOWER ATTACH ANGLE AT STA 663 OUTBOARD SIDE OF LBL 45 / [01] VERIFY -1 REPLACEMENT ANGLE AND -2 SPLICE RECEIVED FROM BACKSHOP FABRICATED ON W/O 43508-5000-0002 AND 43508-5000-0001 IAW 22-157-00935-WIP1.;[02] VERIFIED STEP 1;[03] LOCATED AND DRILSDR DALA2022032802070Fitting · corrodedSHIP 179 RH WING CENTER SECTION REAR SPAR WEB BULKHEAD FITTING (PICKLE FORK) SUSPECT CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 14-597468. (2173827)SDR IPXA2022040680896Stiffener · crackedINSPECTION TYPE:C14CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV .82.01, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-A.SDR IPXA2022040680895Stiffener · crackedINSPECTION TYPE:C14CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2008-12) ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.82.01 , UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-A.SDR IPXA2022040680894Stiffener · crackedINSPECTION TYPE:C14CRACK ON CENTER WING TANK STIFFENER (P/N: 111T2005-8) ON STA 785.9, RBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV .82.01, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-ASDR SIMA20220326009Spar · crackedRT WING TIP HAS A CRACK ON LOWER CORNER OF SPAR 1-C/A-COMPLETE:C/W REPLACEMENT OF WING TIP INBOARD SPAR L WITH REINFORCED SPAR SECTION IAW EO EJ-5700-004 PT B.SDR IXXA2022032507Door · cracked# 10 SLAT ROD DOOR COVER IS CRACKEDSDR IXXA2022032506Door · cracked#4 SLAT OB ROD COVER DOOR CRACKEDSDR IXXA2022032505Door · damaged#3 SLAT OB CLOSE OUT DOOR DAMAGED.SDR FDEA202203240675Doubler · damagedEXISTING REPAIR FOUND AT LEFT HAND WING TANK STRINGER END 14 (UPPER) BETWEEN XORS 506 TO XORS 538 . EXISTING REPAIR AT LEFT HAND WING TANK STRINGER END 14 BETWEEN XORS 506 AND XORS 538 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R REPSDR FDEA202203240673Doubler · damagedEXISTING REPAIR FOUND AT RIGHT HAND WING TANK STRINGER END 14 ( UPPER) BETWEEN XORS 506 TO XORS 538. EXISTING REPAIR AT RIGHT HAND WING TANK STRINGER END 14 BETWEEN XORS 506 TO XORS 538 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R RESDR FDEA202203240672Doubler · damagedEXISTING REPAIR FOUND AT RIGHT HAND WING TANK STRINGER END 13 (UPPER) BETWEEN XORS 562 TO XORS 592. EXISTING REPAIR AT RIGHT HAND WING TANK STRINGER END 13 BETWEEN XORS 562 TO XORS 592 EVALUATED AND FOUND NOT REPAIRED IN ACCORDANCE WITH SRM 57-00-03-2R RESDR SIMA20220322003Spar · crackedRIGHT WING SPAR 1 CRACKED AT OTBD END (MAJOR REPAIR)-C/A-REMOVED AND REPLACED RH WING SPAR 1 FITTING IAW EMB 175 SRM 51-40-08, 51-41-02, 51-43-03, AND 51-43-04.SDR SIMA20220322004Spar · crackedLH WING SPAR 1 CRACKED AT OTBD END (MAJOR REPAIR) -C/A-REMOVED AND REPLACED LH WING SPAR 1 IAW EMB 175 SRM 51-40-08, 51-43-04, AND 51-43-03SDR FDEA202203200605Stiffener · crackedLEFT HAND WING LOWER STIFFENER AT APPROXIMATELY XOS 542 FOUND CRACK. LEFT HAND WING LOWER AT APPROXIMATELY XOS 542 CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRICATED AS PER DOUGLAS DRAWING ARB 2918 REVISION G. REPAIR CLASSSDR FDEA202203200604Former · crackedLEFT HAND WING UPPER FORMER AT APPROXIMATELY XOS 912 FOUND CRACKED. LEFT HAND WING UPPER COMPARTMENT FIXED LEADING EDGE APPROXIMATELY XOS 912 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2921 REVSDR FDEA202203200603Stiffener · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 STIFFENER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 542 CRACKED STIFFENER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. STIFFENER FABRISDR FDEA202203200602Doubler · crackedRIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER FOUND CRACKED. RIGHT HAND WING OUTBOARD LEADING EDGE COMPARTMENT AT APPROXIMATELY XOS 789 RIB DOUBLER REMOVED AND REPLACED AS PER SRM 51-31-0-OG. RIB DOUBLER FABRICATEDSDR FDEA202203200601Former · crackedLEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 FORMER FOUND CRACKED. LEFT HAND WING FIXED LEADING EDGE AT APPROXIMATELY XOS = 789 CRACKED FORMER REMOVED AND REPLACED AS PER SRM 51-31-01-OG. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2930SDR SWAA2022042086119Web · corrodedCORROSION FUEL STATION PANEL WEB LOCATED OFSS 385 AT RT WING 2022-148009 / [01] REPLACED FUEL STATION PANEL WEB LOCATED OFSS 385 AT RT WING IAW B737-700 AMM 28-41-61-401-NG TEST IS OK. TOOL USED: P/N: T477W; S/N: 2073; DUE DATE: 17-NOV-22.;[02] CORRECTED STEP SDR FDEA202203190593Cap · corrodedLEFT HAND WING REAR SPAR LOWER CAP AFT FLANGE XORS = 1051 FOUND CORROSION LEFT HAND WING REAR SPAR LOWER CAP AFT FLANGE XORS = 1051 CORROSION REMOVED AND FOUND EXCEED LIMIT AS PER SRM 57-00-10-1A FIGURE 101 ALLOWABLE DAMAGE 1. LEFT HAND WING REAR SPAR LOWESDR FDEA202203180577None · noneDURING PERFORMING EA: T G-5710-T0366591 P1, STEP10.D.(4), AT STA1035 LBL70, QTY 01 HOLE REQUEST TO INSTALL BACB30WR5K()LX IN HOLE DIA.0.3232"-0.3252", AND NOW OVERSIZED TO 0.371". THE NEXT OVERSIZE FASTENER INSTALLED AT THE DISCREPANT FASTENER HOLE LOCATISDR SWAA2022041185072Ballast · corrodedRH WING OUTBOARD LEADING EDGE AFT OUTBOARD BALLAST WEIGHT HAS CORROSION. / [01] REMOVED RH AFT OUTBOARD BALLAST WEIGHT; COMPLIED WITH ATTACHED EA; AND REINSTALLED PER APB SMM 57-44-02.;[02] C/W INSPECTIONSDR SWAA2022032285286Tab · crackedR/H WING; FLAP ROLLER DEFLECTOR RIB ; UPPER TAB IS CRACKED / [01] ACCOMPLISHED REPAIR TO INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB R/H WING PER SRM 57-51-02-2R-3 REPAIR 3. THIS IS A PERMANENT REPAIR NO FURTHER ACTION REQUIRED.SDR FDEA202203180579Doubler · damagedDURING PERFORMING EA T G-5710-T0366591 P2 STEP 11.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y406, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE SDR FDEA202203180578Doubler · damagedDURING PERFORMING EA T G-5710-T0366591 P1 STEP 11.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED STEP OF DOUBLER P/N 143W2314Y405, AND WILL RESULT IN KNIFE EDGE WITH MACHINED STEP ON AFT EDGE SDR REXA2022040600570Fitting · corrodedR/H WING, AILERON CENTER HINGE FITTINGS GOUGED IN SEVERAL AREAS (MARKED) - REMOVED RH WING AILERON CENTER HINGE FITTING IAW MHIRJ REO 690-57-51-255 REV-- DATED 2022-03-02SDR IPXA2022031780233Fitting · brokenINSPECTION TYPE:SEGLH WING KRUEGER FLAP MIDDLE ZONE HAS METAL PLATE BROKENFABRICATED AND REPLACED PLATE PER SRM 57-41-12 FIG 3 SECTION B-BSDR SWAA2022042084686Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8; W.L. 163. / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT);08] FABRICATED; LOCATED AND DRILLED REPLACEMSDR SWAA2022040784590Angle · crackedRIGHT WHEEL WELL FWD BULKHEAD RBL 5' VAPOR BARRIER HORIZONTAL ANGLE SECOND HOLE FROM I/B CRACKED / [01] PERFORMED HFEC IAW NDTM PART 6;51-00-00 PROCEDURE 23.<BR>CRACK CONFIRMED. CRACK LENGTH: 0.875';[02] FABRICATED NEW REPLACEMENT ANGLE FOR REPAIR ON RIGHT WHESDR SWAA2022042084186Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8; W.L. 163. / [01] VERIFIED APPLICABILITY OF SRM 57-10-10-2R-5 (REPAIR 5 - WING CENTER SECTION REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR - PERMANENT);07] FABRICATED; LOCATED AND DRILLED REPLACEMSDR FDEA202203150515Strip · crackedLEFT WING L/E CAVITY SKIN JOINT PLATE CRACKED @ OFSS 504 REMOVED & REPLACED LH WING FIXED L/E CAVITY STRAP IAW B767 SRM 51-40-02 & BAC DWG 114T2800 REV CSDR IPXA2022040580878None · damagedINSPECTION TYPE:A300R/H WING #5 TRACK I/B RIB NOSE REQIURES REPLACEMENTREMOVED,FABRICATED AND INSTALLED IAW SRM 51-40-21SDR SWAA2022032983906Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE IN A/C BAY AT STA 663 LBL 8 / [01] REMOVED ALL FASTENERS IN REPAIR AREA AND TRIMMED OUT DAMAGED SECTION OF UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5[10] INSTALLED REPAIR ANGLES AT STATION 663 CAP SEALED OUTER FASTENERS IAW B737SDR IPXA2022032680513Stringer · corrodedINSPECTION TYPE:C3CORROSION DAMAGE WAS FOUND ON STRINGER (P/N : 65B10857-9) ON R/H WING NO.18 V.C FLAPREPLACE PART I.A.W. 747-400SF SRM 51-40-02-0G , REV.53.00 AND BOEING DWG 65B15170 SH 2 , REV H.SDR SWAA2022032482787Vapor Barrier · crackedWHILE ACCOMPLISHING CHORD REPAIR AT STA 663 RBL 39; FOUND VAPOR BARRIER BULKHEAD CRACKED / [01] EVALUATED RBL VAPOR BARRIER AND FOUND A CRACK OF 16' AT RBL 39. AND A CRACK OF 3' AT RBL 20. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 57-10-10-2R-2 PAR 1A & NOTE. C
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