JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous 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 = '5720' 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 = '5720' 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 SWAA2022072735031Fitting · missingRIGHT IB FLAP MISSING ZERT FITTING AT AFT FLAP IB TRACK OB AFT ROLLER. MISSING LUBRICATION AT AFT FLAP TRACK ROLLERS; TRACK END BEARINGS AND AT IB AND OB END ROLLERS ON AFT FLAP. / [01] INSTALLED ZERT FITTING IN RIGHT AND LEFT IB FLAP ; LUBRICATED (RIGHT AND LSDR SWAA2022072825539Fitting · crackedDURING REMOVAL OF FWD LT SIDE AIR SUPPLY ELBOW DUCT I/B OF KRUEGER FLAP FWD WTB SUPPORT STRUCTURE CRACKED. / [01] REMOVED IB FWD ANGLE AND IB FITTING OF FRONT SPAR TO GAIN ACCESS AS PER B737-700 SRM 51-40-02-0G-0;[02] REMOVED CRACKED FWD WTB FITTING LH WING IBSDR SWAA2022080425439Support Angle · crackedCRACK SUPPORT ANGLE FIXED TRAILING EDGE LOCATED ORSS 278 AT LT WING 2022-354557 / [01] REPLACED SUPPORT ANGLE FIXED TRAILING EDGE LOCATED ORSS 278 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A6200 SHEET 10 REV- <BR>SEE INDIVIDUAL SISDR SWAA2022080425440Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET LOCATED ON ORSS 273 AT LT WING 2022-354555 / [01] REPLACED TRAILING EDGE SUPPORT BRACKET LOCATED ON ORSS 273 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED TRAILINSDR SWAA2022080225261Angle · crackedCRACK REAR SPAR TRAILING EDGE SUPPORT ANGLE LOCATED ORSS280 AT RT WING 2022-372778 / [01] REPLACED SUPPOR ANGLE AND FASTENERS LOCATED ORSS280 AT RT WING I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPOR SDR SWAA2022080225268Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE REAR SPAR LOCATED IRSS270 AT LT WING 2022-372790 / [01] TOOL USED: CALIPER; PN: 500-197-30; SN: B16144224; DUE DATE: 10-DEC-22.;[02] REPLACED SUPPORT BRACKET TRAILING EDGE REAR SPAR LOCATED IRSS270 AT LT WING I.A.W B737-700 SDR SWAA2022080225265Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE REAR SPAR LOCATED IRSS270 RT WING 2022-372776 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE REAR SPAR LOCATED IRSS270 RT WING IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 DUE TO ALLOWABLE DAMAGE NO FOUND IN SRM B7SDR SWAA2022071223315Attach Angle · crackedATTACH ANGLE CRACKED AT O/B END OF R/W TRAILING EDGE TRANSVERSE WEB ABOVE #2 PYLON AFT TIP / [01] REMOVED AND REPLACED ATTACH ANGLE (CLIP) AT O/B END OF R/W T/E TRANSVERSE WEB ABOVE #2 PYLON AFT TIP IAW SRM 51-40-02-0G-0.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2022071223316Attach Angle · crackedATTACH ANGLE CRACKED AT O/B END OF L/W TRAILING EDGE TRANSVERSE WEB ABOVE #1 PYLON AFT TIP / [01] REMOVED AND REPLACED THE ATTACH ANGLE AT THE O/B END OF THE L/W TRAILING EDGE TRANSVERSE WEB ABOVE THE #1 PYLON AFT TIP IAW SRM 51-40-02-0G-0; STEP 7 AND IPC 57-4SDR SWAA2022071123125Bracket · crackedRH WING OUTBD OF R2 PYLON FITTING HYDRAULIC TUBING BRACKET CRACKED IN HALF. DOT# A177-001 / [01] REMOVED BROKEN SUPPORT ANGLE I.A.W SRM 51-40-02-0G-0;[02] DRILLED NEW SUPPORT BRACKET I.A.W SRM 51-40-05-0G-0 AND BOEING DWG 112A4001REV:-<BR> ATAG# FOR NEW BRACKESDR FDEA202206251563Former · crackedBROKEN FORMERS, LH WING #5 SLAT REPLACED FORMERS114T2170-5 AND 114T2511-13 PER E.A. H-5720-T0369185 P1SDR FDEA202206251562Former · crackedTWO EACH BROKEN FORMERS ON RH WING LEADING EDGE UNDER #8 SLAT. MWT. 0000553921 : M - 25-JUN-2022 23:01 REMOVED AND REPLACED 2EA FORMERS REF EA H-5720-T0369185 P1 FORMER PART#S 114T2170-6 / 114T2511-14SDR SWAA2022071122471Panel · cracked(AEROMAN REQUEST) CRACK ON FAIRING PANEL 543EB LH WING 2022-268372 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE: 28-SEP-22;[02] TOOL USED: HOT BONDER P/N: HCS9000B S/N: 18175469 DUE DATE: 05-AUG-22.;[03] TOOL USED: SCALE: P/N: SCA-301 S/N: AE-41SDR SWAA2022072222178Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 273 RT WING 2022-353017 / [01] REPLACED SUPPORT BRACKET AND FASTENERS LOC TRAILING EDGE LOCATED ORSS 273 RT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED SUPPORT BRACKET AND FASTESDR SWAA2022071122024Attach Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE (WL 196) AT STA 663 OUTBOARD SIDE OF RBL45 / [01] STA 663 UPPER ATTACH ANGLE AT RBL 45 AND WL 196 WAS REPAIRED PER EA 22-157-01860;[02] JOB COMPLETE; AUDIT C/WSDR U2RA2022062000023Skin Panel · damagedFOUND A 47.5" CRACK TO RH WING UPPER SURFACE L/E PANEL P/N 65B14962-4. ACCOMPLISHED INTERIM MAJOR REPAIR IAW FLIGHT VEHICLES CONSULTING INC E.O. CONTROL # 22098-2 REV IR DATED 06/21/2022.SDR U2RA2022062000022Skin Panel · damagedFOUND A 47.5" CRACK TO LH WING UPPER SURFACE L/E PANEL P/N 65B14962-5. ACCOMPLISHED INTERIM MAJOR REPAIR IAW FLIGHT VEHICLES CONSULTING INC E.O. CONTROL # 22098-1 REV IR DATED 06/21/2022.SDR FDEA202206221507Former · crackedL/H WING L/E NOSE FORMER IS CRACKED AT APPROX OSS 437 (JUST INBD OF THE #5 SLAT INBD AUX TRACK) REPLACEDFORMER IAW EA # H-5720-T0368847-P1.SDR FDEA202206221505Former · crackedRW FIXED L/E NOSE FORMER CRACKED AT THE #8 SLAT INBD AUX TRACK REPLACED FORMER IAW EA # H-5720-T0368847-P.SDR FDEA202206221504Former · crackedL/H WING LE SUBSTRUCTURE NOSE FORMER IS CRACKED JUST INBD OF THE #4 SLAT INBD ROTARY ACUTATOR OSS 565 REPLACED FORMER IAW EA # H-5720-T0368847-P1.SDR FDEA202206221503Former · crackedL/H WING LE SUBSTRUCTURE NOSE FORMER IS CRACKED JUST OTBD OF THE #5 SLAY OTBD ROTARY ACTUATOR AT OSS 499 REPLACED FORMER IAW FEDEX EA # H-5720-T0368847-P1, RELEASED JUN 07, 2022, TITLED, " WING - SECONDARY WING STRCT - FIELD SERVICE EVALUATION, LH WING OSSSDR FDEA202206211495Former · crackedRIGHT-HAND WING LEADING EDGE AT STA OSS-499 FORMER P/N 114T2511-14 IS CRACKED REPAIRED IN REF TO SRM B767-300 51-40-02-06, SRM B767-300 51-40-03-06. REF. EA H-5720-T0369070SDR FDEA202206211494Former · crackedRIGHT-HAND WING LEADING EDGE FORMER AT STA OSS-441 P/N 114T2170-6 IS CRACKED REPAIRED IN REF TO SRM B767-300 51-40-02-06, SRM B767-300 51-40-03-06. REF. EA H-5720-T0369070SDR FDEA202206211493Former · crackedLEFT-HAND WING LEADING EDGE AT STA OSS441 FORMER P/N 114T2170-5 IS CRACKED. REPAIRED IN REF TO SRM B767-300 51-40-02-06, SRM B767-300 51-40-03-06. REF. EA H-5720-T0369070SDR AALA202206309587Strut · brokenAIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAPSDR AALA202206302580Strut · brokenAIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAPSDR AALA202206309409Strut · brokenAIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAPSDR AALA202206308669Strut · brokenAIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAPSDR AALA202206308288Strut · brokenAIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAPSDR AALA202206305270Strut · brokenAIRCRAFT WAS GROUNDED: FLAP DRIVE EICAS MESSAGE ON APPROACH TO LIS. EMERGENCY DECLARED; FLIGHT LANDED SAFELY. #4 GEARED ROTARY ACTUATOR REPLACED PER AMM 27-51-00A-720A-A (AALA202206305038). REPLACED 6 BROKEN STRUT ASSEMBLIES ON LEFT INBOARD WING ABOVE #12 FLAPSDR FDEA202206171459Web · crackedL/H WING L/E AREA BULLNOSE WEB IS CRACKED IN THE LOWER RADIUS AT APPROX OFSS 675 UNDER THE LE FUEL SVC ACCESS DOOR 521QB REPAIRED LEFT WING LEADING EDGE NOSE BEAM WEB @ OSS 679 IAW B767 SRM 57-41-13-2R, REPAIR 3. FUELING STATION DOOR 521QB REMOVED & REINSTSDR SWAA2022071519004Winglet · crackedR/H WINGLET CRACKED AT LWR AFT SCIMITAR CONNECTION POINT (MARKED) / [01] REMOVED AND REPLACED WINGLET. WINGLET INSTALLED ON TTG8R008EC09.SDR FDEA202206111421Slat · delaminated#5 SLAT DAMAGED DUE TO LOOSE FASTENER HEADS REPAIRED SLAT IN REF. TO B767 SRM 51-70-10-2R AND B767 SRM 57-43-02-2R.SDR YENA2022060900576Rib · crackedDURING HEAVY MAINTENANCE, WINGS / LH WING / FIXED LEADING EDGE RIB 17 / CRACK - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR IPXA2022061483126Tie Clip · crackedINSPECTION TYPE:CIH KRUGER FLAP WELL FWD O/B CORNER HAS A CRACKED CLIPREMOVED FABRICATED AND INSTALLED IAW A300 SRM 51-40-21SDR SWAA2022060814950Retainer Seal · crackedRH WING TE CAVITY UNDER SPOILER N8 LOCATION LOWER PANEL INB SEAL RETAINER CRACKED 2022-284074 / [01] REPLACED SEAL RETAINER AND FASTENERS LOCATED RH WING TE CAVITY UNDER SPOILER N8 LOWER PANEL INB SEAL IAW SRM 51-40-02 AND SRM 51-10-02.;[02] COMPLETE TASK CERTSDR YENA2022060200544Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TRAILING EDGE LOCATED TOP SKIN, LOWER SURFACE, OVERHANG AREA AT LEVEL RIB 8 ON LH WING (CPCP RELATED REFER TO MPDTASK 572178-01); ACCOMPLISHED REPAIR OF THE CORROSION IN AN EXISTING REPAIR AREA ON THE LH WING TOP SKIN PANEL SDR YENA2022060200542Skin Panel · corrodedDURING HEAVY MAINTENACE, WINGS / LH WING / TOP SKIN PANEL 2 / TRAILING EDGE OVERHANG / LOWER SURFACE / RIB 7A / CORROSION AT PREVIOUS REPAIRED AREA – TIME-LIMITED REPAIR. (CONSIDERED A MAJOR REPAIR)SDR SWAA2022060713856Support Beam · brokenLEFT WING TRAILING EDGE PANEL 561AB MOUNT SUPPORT ANGLE IS BROKEN AT INBOARD END / [01] REMOVED AND REPLACED L/W TRAILING EDGE PANEL 561AB MOUNT SUPPORT BEAM PER REF B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.SDR SWAA2022061713334Angle · elongatedELONGATED HOLE FRONT SPAR BOOST PUMP ANGLE AT RT WING 2022-291520 / [01] REPLACED ANGLE LOCATED FRONT SPAR BOOST PUMP AT RT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 112A2004 REV- SEE INDIVIDUAL STEP SIGN OFF BELOW;[02] JOB COMPLETED;[03] RII JOB COMPLESDR U2RA2022060600011None · noneCORROSION DAMAGE FOUND AT LEFT WING L/E PANEL SUPPORT BEAM @ OLES 1510 APPROXIMATE. REMOVED DAMAGED SECTION AND SPLICED IN REPLACEMENT BEAM AS REQUIRED PER B747-400 SRM 57-41-13 REPAIR 3, BAC SR #4-5471089571, AND FORM 8100-9 ISSUED BY BOEING; DATED 05/29/202SDR FDEA202205281320Angle · crackedRH WING OUTBD FIXED LEADING EDGE FORMER ATTACH ANGLE IS CRACKED AT RIB #5 REMOVED AND REPLACED THE RH WING O/B FIXED L/E FORMER ATTACH ANGLE AT STA OSS 437 IAW FEDEX EA H-5720-T0368613-P1, TITLE: WING - SECONDARY WING STRCT - FIELD SERVICE EVALUATION, RH WSDR FDEA202205271313Former · crackedRH WING OUTBD FIXED LEADING EDGE FORMER IS CRACKED AT RIB #6 REMOVED AND REPLACED RH WING OB LE FORMER AT RIB #6, REF. FEDEX EA H-5720-T0368613- P1, TITLE: WING-SECONDARY WING STRCT-FIELD SERVICE EVALUATION, RH WING OSS 437 AND LH & RH 441 & 499, LEADING EDSDR IPXA2022060682863Angle · damagedINSPECTION TYPE:1CL/H WING REAR SPAR VERTICAL STIFFNER IS DAMAGED AT STA., XORS. 420.0.REMOVED, FABRICATED AND REPLACED STIFNER ANGLE IAW DWG. ARC7014 AND SRM 51-35-01. (MINOR)SDR FDEA202205251292Bracket · crackedRIGHT WING IB LEADING EDGE TORQUE TUBE GAURD BRACKET IS CRACKED AT FASTENER HOLE REMOVED & REPLACED RH WING IB LEADING EDGE TORQUE TUBE GAURD BRACKET IAW BOEING DWG 114T1240 REV-, B767 SRM 51-40-02-0G, AND B767 SRM 51-40-05-0GSDR SWAA2022061411125Support Angle · crackedRIGHT WING T/E SHELF PANEL AT FLAP DEFLECTION RIB HAS SUPPORT ANGLE CRACKED ON OUTBOARD END. (MARKED) / [01] REMOVED RIGHT T/E SHELF PANEL SUPPORT ANGLE IN IAW SRM 51-40-02.;[02] INSTALLED RIGHT T/E SHELF PANEL IAW SRM 51-40-02.;[03] CWSDR SWAA2022060111139Web · crackedRIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SUPPORT WEB CRACKED AT OUTBOARD ATTACH FASTENER HOLE. REMOVED DAMAGE WEB ANGLE AT R/H WING TRAILING EDGE DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART WED ANGLE SDR SWAA2022060111136Support Angle · crackedRIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL SEAL SUPPORT ANGLE CRACKED AT WEB ATTACH POINT. REMOVED DAMAGE SEAL SUPPORT ANGLE AT R/H WING TRAILING EDGE DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW PART WEB ANGLSDR SWAA2022060111137Support Angle · crackedLEFT WING DEFLECTION CONTROL RIB PANEL VERTICAL SEAL SUPPORT ANGLE CRACKED AT THE FORWARD SIDE OF WEB. / [01] REMOVED AND REPLACED SEAL SUPPORT ANGLE AT FWD SIDE OF WEB ON L/W DEFLECTION CONTROL PANEL PER REF B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1.SDR SWAA2022070110066Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED ON ORSS 275 AT RT WING 2022-265839 / [01] REPLACED ANGLE LOCATED ON TRAILING EDGE AT ORSS 275 AT RT WING. IAW B737-700 SRM 51-40-02 AND DWG #115A2930; SHEET 8 AND REV -. <BR>SIZE CRACK IS: 2.150?. TOOL USED IS CALIPER P/N: 700
Back to JASC 5720