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 CALA2019111101948Fitting · crackedSHEAR FITTING AT STA LBL 32.40 IS CRACKED, SUPPORT TASK, L/P 586 5640 REMOVED AND REPLACED SHEAR FITTING IAW 737-700 SRM 51-40-02 AND DWG NO. 111A2000 REV ORIGINAL DATA WAS TRANSCRIBED FROM NR 58656 40 ACCOMPLISHED BY INSPECTED BY SSFR REPORT FORM 46-0024 ENTESDR CALA2019111101942Fitting · crackedSHEAR FITTING AT STA LBL 40.87 IS CRACKED. SUPPORT TASK, L/P 582 5492 REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND SB 737-57-1309 REV 1 RECEIVED ECRA 5714-01037 REV ORIGINAL TO R EPLACE THE SHEAR FITTING DATA WAS TRANSCRIBED FROM NR 5825492SDR CALA2019111101941Fitting · crackedSHEAR FITTING AT STA RBL 32.40 IS CRACKED, SUPPORT TASK, L/P 586 5636 REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND SB 737-57-1309 REV 1 RECEIVED ECRA 5714-01040 REV ORIGINAL TO R EPLACE THE SHEAR FITTING DATA WAS TRANSCRIBED FROM NR 5865636SDR CALA2019111101947Fitting · crackedSHEAR FITTING AT STA RBL 6.14 IS CRACKED LP 5865638 SPT REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND DWG NO. 111A2000 REV ORIGINAL DATA TRANSCRIBED FROM NR 5865638 ACCOMPLISHED BY MECHANIC INSPECTED BY SSFR REPOR T FORM 46-0024 ENTERED BY USDR CALA2019111101946Fitting · crackedSHEAR FITTING AT STA RBL 54.60 IS CRACKED, SUPPORT TASK, L/P 582 5491 REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND SB 737-57-1309 REV 1 RECEIVED ECRA 5714-01041 REV ORIGINAL TO R EPLACE THE SHEAR FITTING DATA TRANSCRIBED FROM NR 5825491 ACCSDR CALA2019111101945Fitting · crackedSHEAR FITTING AT STA RBL 15.04 IS CRACKED, SUPPORT TASK, L/P 586 5637 REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND SB 737-57-1309 REV 1 RECEIVED ECRA 5714-01039 REV ORIGINAL TO R EPLACE THE SHEAR FITTING DATA WAS TRANSCRIBED FROM NR 5865637SDR CALA2019111101944Fitting · crackedSHEAR FITTING AT STA LBL 6.14 IS CRACKED, SUPPORT TASK, L/P 5865 639 REMOVED AND REPLACED SHEAR FITTING IAW B737-700 SRM 51-40-02 AND SB 737-57-1309 REV 1 RECEIVED ECRA 5714-01038 REV ORIGINAL TO R EPLACE THE SHEAR FITTING DATA WAS TRANSCRIBED FROM NR 5865639 SDR IPXA2019111879074Former · crackedINSPECTION TYPE:2CR/H WING FIXED L/E FORMER IS CRACKED AT STA. XOS.558.REMOVED, FABRICATED AND REPLACED FORMER AT STA. XOS=558 IAW DWG ARB1162 AND SRM 51-33-01. (MINOR)SDR IPXA2019111148807Landing · crackedINSPECTION TYPE:12YRL/H WING FIXED T/E UPPER PNL. INTERCOSTAL/SUPPORT IS CRACKED ABOVE CENTER FLAP O/B FLAP TRACK.REMOVED AND REPLACED INTERCOSTAL/SUPPORT IAW SRM 51-40-21.(MINOR)SDR SWAA2019103038390Plate · crackedL/H WING INBOARD WIGGLE PLATE FOR WING TRAILING EDGE PANEL 551EB CRACKED. / R&R WIGGLE PLATE IAW SRM.SDR SCNA20191025217Panel · delaminatedPANEL 621JB LOWER LEADING EDGE DELAMINATION. REPAIRED DELAMINATED EROSION STRIP ON PANEL 621 JB IN REF. TO B737-800 SRM 57-41-01.SDR SCNA20191025216Panel · delaminatedPANEL 621DB LOWER LEADING EDGE DELAMINATION. REPAIRED DELAMINATED EROSION STRIP ON PANEL 621DB IN REF TO B737-800 SRM 57-41-01.SDR SCNA20191025215Panel · delaminatedPANEL 521PB LOWER LEADING EDGE DAMAGED. REPAIRED DELAMINATED EROSION STRIP ON PANEL 521 PB IN REF TO B737-800 SRM 57-4-01.SDR SCNA20191025213Support · damagedPANEL 643AB FLAP SUPPORT #7 FWD ASSY. ACCESS PANEL DAMAGED. REPAIRED PANEL 613AB FLAP SUPPORT #7 FWD ASSY ACCESS PANEL IN REF. TO B737-800 SRM 57-53-70.SDR SCNA20191025212Support · damagedPANEL 644AB FLAP SUPPORT #8 FWD ASSY. ACCESS PANEL DAMAGED. REPAIRED PANEL 644AB FLAP SUPPORT #8 FWD ASSY IN REF TO B737-800 SRM 57-53-70.SDR IPXA2019102868317Fitting · gougedINSPECTION TYPE:2CRT WING REFUEL ADAPTER FITTING IS GOUGED ON INSIDE.REPAIRED GOUGED RT WING REFUEL ADAPTER FITTING IAW VT-SAA EA 011-5720-01-A7931 REV. IR AND UPS EO MD11-5700-74425-A. (MINOR)SDR FDEA2019101092530Retainer · corrodedRIGHT WING UPPER FIXED TE AREA OUTBOARD OF AILERON ACTUATORS, FIXED TE SEAL RETAINER CORRODED. THE SEAL RETAINER WAS REPLACED IAW DRAWING 113N1640 AND GMM 7-0-1001.SDR IPXA2019103098432Landing · corrodedINSPECTION TYPE:2CR/H WING T/E AT PANEL # 641FB, THE PANEL LANDING IS CORRODED.REMOVED, FABRICATED AND REPLACED LANGING/TEE IAW DWG. ARC0307 AND SRM 51-33-01. (MINOR)SDR HKGA20191008019Rib · crackedRH NACELLE FLAP INTERNAL TRAINING EDGE STUB RIB AFT OF LOWER SKIN ACCESS HOLE IS CRACKED & HAS ENLARGED FASTENER HOLES. MATCHDRILLED NEW STUB RIB (REF EMB120 SRM 51-25-00 REV 58). INSTALLED NEW STUB RIB (REF EMB120 SRM 51-40-02 REV 58).SDR FDEA201910072506Rib · crackedMDIS 750 57-10 0606 08OCT19 MEM OPEN U RH OUTBOARD SIDE OF RIB 5, EVIDENCE OF CRACK. COMPLIED WITH E.A. 6-5710-T0350686 PART 1 REV A, PART 2 AND PART 3 TEMPORARY REPAIR OF R/H WING RIB SDR SIMA20191007003None · noneL/H WINGTIP FWD SPAR ATTACHMENT CRACKED.-C/A-COMPLETE:REMOVED AND REPLACED LH WINGTIP IAW EMB 175 AMM 57-30-00. SEE WIPS AND TASKS FOR DETAILSSDR SIMA20191007002None · noneR/H WINGTIP FWD SPAR ATTACHMENT CRACKED.-C/A-COMPLETE:REMOVED AND REPLACED RH WINGTIP IAW EMB 175 AMM 57-30-00. SEE WIPS AND TASKS FOR DETAILSSDR R61A2019102561135Winglet · crackedUPPER AND LOWER PORTION OF R/H WING TIP SPAR CRACKED. CRACK IS 1.375 INCHES LONG REMOVED
AND REPLACED WING TIP IAW 57-30-00SDR R61A2019102561133Winglet · crackedUPPER AND LOWER PORTION OF R/H WING TIP SPAR CRACKED. CRACK IS 1.375 INCHES LONG REMOVED
AND REPLACED WING TIP IAW 57-30-00SDR DALA2019100705765Rub Strip · corrodedCORROSION AT CUTOUTS (RUBSTRIPS) #620CT, 620DT, 620FT, AND 141AR RH WING. ORIGINAL THICKNESS ARE .020" AND REMAINING THICKNESS ARE .011" THEREFORE ARE OUT OF LIMITS IN REF NRC 00565. NRC 0627: CORROSION LEVEL 2, FUEL ACCESS (RUBSTRIPS) #620CT, 620DT, 620FT, ANSDR SWAA2019101767962Plate · crackedR/H WING PANEL 651EB FORWARD INBOARD SUPPORT WIGGLE PLATE CRACKED. / R&R WIGGLE PLATE PER SRM.SDR SWAA2022040584989Seal Ring · crackedBS 663 VAPOR BARRIER UPPER SEAL RETAINER IS CRACKED RBL 20 WL 140 / REMOVED AND INSTALLED NEW VAPOR BARRIER SEAL RETAINER AT BS 663 RBL 20 WL 140 PER SRM 51-40-02 AND AIPC 57-11-00-02SDR R61A2019102561130Winglet · crackedUPPER AND LOWER PORTION OF L/H WING TIP SPAR CRACKED. CRACK IS 1.25 INCHES LONG REMOVED AND REPLACED WING TIP IAW 57-30-00SDR SWAA2022032920012Web · crackedL/W TRAILING EDGE CURVED BULB SEAL RETAINER AFT OF TRANSVERSE WEB CRACKED / REMOVED AND REPLACED SEAL RETAINER L/W TRAILING EGDE AFT OF TRANSVERSE WEB IAW SRM 51-40-02-0G-01 FASTENERS IAW AIPC 57-50-00-25 898134 10-12-19SDR TSAA20191003056Structure · crackedREPAIRED CRACKED FASTENER HOLE ON RH WING T/E WBL 136 IAW BOEING SR# 4-4546890303 DATED SEP 23, 2019.SDR DALA2019100305667Shim · migratedMIGRATION ON SHIM ID #1A WAS NOTED ON MEASUREMENT ID# 2A, AT INBOARD DRAG FITTING PERCARD 5720-01100-0101A, STEP 17. CORRECTIVE ACTION: MIGRATION SHIMS WERE REPAIRED PER ER/A 581720-14AD REV ORIGSECTION 1 AS PERMANENT REPAIR AND ETI-57-19-102 REV 15.SDR SIMA2019100198009Spar · crackedR/H ENHANCED WINGTIP SPAR 1 ATTACHMENT FITTING CRACKED. FOUND ON OPEN UP. REMOVED, REPAIRED, AND REINSTALLED RH WING TIP IAW ERJ-175 AMM 57-30-00, AND ERS-EJ-57MR-1151 PART B; OPS CHECKS OF LIGHTS GOOD, ALL BONDING CHECKS GOOD, NO DISCREPANCIES NOTED.SDR SWAA2019101657805Support Beam · crackedL/H WING TRAILING EDGE STRUCTURE BETWEEN SPOILERS #5 AND #6 OUTBOARD SUPPORT BEAM CRACKED. R&R SUPPORT BEAM IAW SRM AND DWG.SDR IPXA201910147805Angle · crackedINSPECTION TYPE:4C, LT WING FIXED L/E INTERNAL SUB-SPAR WEB BOTTOM ANGLE IS CRACKED IN 2 PLACES ALONG LOWER RADIUS INSIDE ACCESS PANEL 524GB.REPAIRED CRACKED LT WING FIXED L/E INTERNAL SUB-SPAR BOTTOM ANGLE INSIDE ACCESS PANEL 542GB IAW VT-SAA EA 300-5710-01-ASDR SCNA2019100192179Fastener · looseLEFT WING, UPPER L/E 16 LOOSE FASTNERS FROM THE PYLON INBD. ALONG THE AFT SIDE OF PANEL. REMOVED 16 EA LOOSE FASTENERS ON L/H WING UPPER SKIN JUST INBD OF # 1 PYLON. REAMED HOLES TO 1ST OVER 3/16. .199" OPEN HOLE AND COUNTER SINK HFEC ACCOMPLISHED BY NDI. NO CSDR SWIA2019101846528Rib · crackedR/H MLG BATT RIB AT W.S. 53.60 IS CRACKED. (C-CHECK) RO: 10/16/2019 REPAIRED RH MLG BATT RIB AT WS 53.6 IAW REO.SDR SWAA2022032972959Web · crackedRIGHT WING ANGLED WEB SUPPORT COMMON TO INBOARD SIDE OF DEFLECTION CONTROL RIB CRACKED / REMOVED AND REPLACED RIGHT WING ANGLED WEB SUPPORT COMMON TO INBOARD SIDE OF DEFLECTION CONTROL RIB PER SRM 51-40-02SDR SWAA2022032928571Vapor Barrier · crackedREINFORCEMENT DOUBLER ON THE FWD SIDE OF THE L/H BS663 LOWER VAPOR BARRIER IS CRACKED LBL20 WL154 / FORMED CHEMICAL CONVERSION COATED AND PRIMERED NEW REINFORCEMENT DOUBLER L/H BS. 663 LOWER VAPOR BARRIER LBL20 WL154 IAW DWG 111A1511; MM 51-21-72-370-804; MM 5SDR FDEA201909102194Former · crackedLEFT HAND WING LEADING EDGE CAVITY FORMER PART NUMBER ARB1164-5 FOUND CRACKED AT XOS 993. CRACKED FORMER RMOVED AS PER SRM 51-31-01-0G AND FABRICATED FORMER PER DRAWING ARB 1164 REV: M. INSTALLED FABRICATED FORMER AT LEFT HAND WING LEADING EDGE CAVITY AT XOS 9SDR SWAA2022032986042Attach Angle · crackedWING CENTER SECTION REAR SPAR LOWER CHORD CRACKED AT STA 663.75 LBL 24.92 AND WL 167.48. VIEWED THRU LEFT A/C BAY / ACCOMPLISHED PERMANENT REPAIR AT VAPOR BARRIER ATTACH ANGLE CRACK AT BS 663; LBL 24.92 AS PER SOUTHWEST EA # 1-757-16549 REV IRSDR FDEA2019082171918Fitting · crackedR/H FR47 FASTENER 11RH AND BUSHINGS REQUIRE REMOVAL FOR NDT ROTOTEST INSP. COMPLIED WITH EA 6-5710-T0348474-P1SDR FDEA2019082171917Fitting · crackedINDICATIONS DURING ROTOPROBE INSPECTION OF HOLE "166" DUE TO VISIBLE DAMAGE INSIDE OF HOLE. RH WING COMPLIED WITH EA 6-5710-T0348474-P1SDR FDEA2019082171916Fitting · crackedR/H WING INSPECTION OF FASTENER HOLE (C)FAILED ROTO PROBE INSPECTION DUE TO MULTIPLE CRACK INDICATIONS AT APOX. DEPTH OF .9" TO 1.4" INSPECTION FROM THE BOTTOM SKIN UPWARDS. POSSIBLE SHIM LOCATED IN AREA OF INDICATIONS. COMPLIED WITH EA 6-5710-TO348474-P1SDR JGVR20190814004Drag Angle · corrodedRIGHT WING UPPER DRAG ANGLES HAS CORROSION ALONG SEAMS APX TOTAL LENGTH OF 28 INCHES ALONG DRAG ANGLE OUTBD SEAMS ON WS 37.00.SDR FDEA201908302039Rib · crackedLEFT NR 1 SLAT CRUISE PERFORMANCE FAIRING ARB7105-3 CRACKED AT UPPER ATTACHMENT STUD. REPAIRED THE RIB IAW SRM 57-40-71 FIG 201 SH. 1 MAJOR REPAIR.SDR UIEA2019081435051Structure · corrodedFOUND THAT OVERWING FILL PORT ON BOTH WINGS HAS CORROSION AROUND THE STRUCTURE.(<P>REPAIRED CORROSION AREA IAW EI NO T2019A57M-2788 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR SIMA20190810003None · noneINSPECT LH WINGLET TO WING SPAR 1 ATTACH FITTING FOR CRACKING.-C/A-COMPLIED WITH GVI OF LH WINGLET TO WING SPAR 1 ATTACH FITTING AND EDDY CURRENT INSPECTION IAW ENVOY NDT MANUAL TASK ET 0400-1 AND FOUND TO BE CRACKED. SEE ITEM 2 OF THIS NRWC.SDR RAIA2019081700002Wedge · crackedR/H WING STUB AFT WED IS CRACKED IN 2 PLACES.... REMOVED AND REPLACED R/H WING STUB AFT WEB.SDR COEA20191023919Bracket · corrodedWO 198966 NR 500034 HEAVY CHECK COE/MINOR REPAIR: L/H WING OUTBOARD UPPER TRAILING EDGE PANEL HAS LEVEL 2 CORROSION ON 2 STRUT BRACKETS AT INBOARD END. CORRECTIVE ACTION: REPLACED 2EA BRACKETS WITH OEM PARTS.SDR SWAA2019081335775Plate · crackedWAFFLE PLATE ON R/H WING TRAILING EDGE AT STATION ORSS. 217 CRACKED. R&R WAFFLE PLATE PER SRM AND DWG 115A2001
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