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 SWAA2022032271917Spar Web · corrodedCORROSION TRAILING EDGE REAR SPAR WEB LOCATED IRSS 146 APROX. BOOST PUMP LOWER AREA AT LT WING 2022-79981 / [01] ET TOOL USED PN: MIZ-21C; SN: 769680. DUE DATE: 26-FEB-22;[02] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG; S/N: 130066701; DUE DATE: 22-APR-22;SDR R61A2022030800176Doubler · crackedCRACK AT LOWER RH WING RIB 4A FASTENER TO FASTENER. PERFORMED LOWER RH WING DOUBLER REPAIR AT RIB 4A REF ETD2022-170-006182SDR SWAA2022031571069Attach Angle · crackedLEFT WING; TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT / [01] REMOVED AND REPLACED LEFT WING; TRANSVERSE WEB O/B ATTACH ANGLE AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT P/N 115A6260-1 IAW SRM 51-40-02 SDR SWAA2022031571063Plate · crackedLEFT WING; WAFFLE PLATE CRACKED JUST I/B OF #1 PYLON AFT TIP / [01] REMOVED AND REPLACED L/H WING WAFFLE PLATE I/B #1 PYLON IAW SRM 51-40-02.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.SDR SWAA2022030171284Angle · crackedLH WING TRAILING EDGE ANGLE JUST INBOARD OF DEFLECTION CONTROL RIB IS CRACKED. PART # 115A2156U7 / [01] REMOVED AND REPLACED TRAILING EDGE ANGLE PER SRM 51-40-02.SDR SWAA2022021470816Retainer · crackedLEFT WING FIXED TRAILING EDGE PANEL AT DEFLECTION RIB; COVE SEAL RETAINER CRACKED. ; / [01] REMOVED AND REPLACED COVE SEAL RETAINER BRACKET AT LEFT WING DEFLECTION RIB IN REF TO SRM 51-40-02; [02] INSPECTED WORK PERFORMEDSDR FDEA202202100270Angle · crackedLEFT WING FIXED LEADING EDGE NOSE FORMER ATTACH ANGLE IS CRACKED @ OSS 441 REMOVED & REPLACED NOSE FORMER ATTACH ANGLE IAW BAC DWG 114T2241, REV - & FEDEX EA H-5720-TO366786SDR FDEA202202100269Former · crackedLEFT WING, FIXED LEADING EDGE FORMER IS CRACKED @ OSS 441 REMOVED & REPLACED FORMER IAW BAC DWG 114T2241, REV -SDR FDEA202202100268Angle · crackedLEFT WING FIXED LEADING ECGE FORMER ATTACH ANGLE IS CRACKED @ OSS 437.4 REMOVED & REPLACED ATTACH ANGLE IAW BAC DWG 114T2240, REV - & FEDEX EA H-5720- T0366762-P1SDR AALA202304186233Vapor Barrier · crackedAIRCRAFT WAS GROUNDED: CRACKED VAPOR BARRIER IN RH WHEEL WELL, ACCOMPLISHED TEMPORARY SPEED TAPE REPAIR IAW AARD 57-10-10-9 WITH 600 FC REPETITIVE INSPECTION. **SUPPLEMENTAL REPORT FOR AALA202202106233: REMOVED REPAIR AND INSTALLED PERMANENT REPAIR PATCH PER ASDR SWAA2022031470827Angle · crackedCRACK FRONT SPAR SUPPORT ANGLE LOCATED FUEL BOOST PUMP IFSS 120 APROX. AND WBL 94.24 AT RT WING 2022-68053 / [01] CALIPER PN: 500-197-30; SN: B20189362; DUE DATE: 03-DEC-22.;[02] TOOL USED: POWER PACK P/N FMK0007096 S/N PE0414/70786 DUE DATE: 23-FEB-22. MULTIMSDR SWAA2022030870887Panel · corrodedWING FUELING; GAGE SUPPORT ANGLE IS CORRODED / [01] REMOVED WING FUELING GAGE PANEL IAW AMM 28-41-61-000-801;[02] MOUNTED REFUEL PANEL TOGGLE SWITCHES ONTO REPLACEMENT REFUEL PANEL ASSEMBLY PER SWPM 20-83-11.<BR>TERMINATED HARNESS GROUND WIRES INTO GROUND BLOCSDR SWAA2022021470456Retainer · crackedRIGHT WING AFT FIXED UPPER PANEL ABOVE NACELLE STRUT FAIRING SEAL RETAINER CRACKED ; / [01] REMOVED AND REPLACED RIGHT WING AFT FIXED UPPER PANEL ABOVE NACELLE STRUT FAIRING SEAL RETAINER PER AMM 57-50-01; [02] INSPECTION C/W REMOVED AND REPLACED RIGHT WING AFSDR AALA202202106233None · noneAIRCRAFT WAS GROUNDED: CRACKED VAPOR BARRIER IN RH WHEEL WELL, ACCOMPLISHED TEMPORARY SPEED TAPE REPAIR IAW AARD 57-10-10-9 WITH 600 FC REPETITIVE INSPECTION. **SUPPLEMENTAL REPORT WILL BE SUBMITTED.** (OPEN)SDR FDEA202202090253Angle · crackedR/W FIXED L/E, NOSE FORMER ATTACH ANGLE AT O.S.S. 441.6 REMOVED AND REPLACED THE R/W FIXED L/E NOSE FORMER ATTACH ANGLE AT O.S.S. 441.6 IAW BAC DWG 114T2241, REV. - AND FEDEX EA H-5720-T0366759, TITLE: WINGS - SECONDARY WING STRCT - RH WING, LEADING EDGE, SDR FDEA202202090252Angle · crackedR/W FIXED L/E, NOSE FORMER ATTACH ANGLE AT O.S.S. 437.4 IS CRACKED REMOVED AND REPLACED THE R/W FIXED L/E NOSE FORMER ATTACH ANGLE AT O.S.S. 437.4 IAW BAC DWG# 114T2240, REV. - AND FEDEX EA H-5720-T0366760, TITLE: WINGS - SECONDARY WING STRCT - RH WING, LESDR FDEA202202090251Former · crackedRW #8 SLAT INBD AUX TRACK OTBD NOSE FORMER IS CRACKED REMOVED AND REPLACED THE NOSE FORMER AT STA O.S.S. 441.6, R/W FIXED L/E AT THE #8 SLAT AUX TRACK O/B SIDE IAW BAC DWG# 114T2241, REV. - AND B767 SRM 51-40-02-0G.SDR ABXA2023050271Skin · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE DISCOVERED CORROSION ON THE LOWER SURFACE OF THE RIGHT-HAND WING BOTTOM SKIN PANEL #1 (P/N 112T4701-4) AT W.S 930 AND THE REAR SPAR OVERHANG. THE CORROSION WAS REMOVED BY BLENDING PER B767-300 SRM SDR SWAA2022021670370None · crackedDOT A-24-10. PANEL 551FB AFT SUPPORT CLIP CRACKED OFF ABOUT 2 FEET O/B OF I/B END. / [01] REMOVED AND REPLACED PNL 551 FB AFT SUPPORT CLIP CRACKED WITH A NEW SUPPORT CLIP P/N 287A9152-23; A TAG# WN7755. IAW SRM 51-40-02-OG-0; IPC # 57-50-00-38.;[02] VERIFIED ISDR SWAA2022032170285Panel · delaminatedPANEL 551BT HAVE ONE CORNER DELAMINATED. / [01] PREPARED AREA FOR REPAIR AT PANEL 551 BT AS PER B737-700 SRM 51-70-06-2R-1;[02] PREPARED AREA FOR REPAIR AT PANEL 551 BT AS PER B737-700 SRM 51-70-06-2R-6.;[03] VERIFIED STEP 2.;[04] REPAIRED AT PANEL 551BT AS PESDR SWAA2022031470179Bracket · crackedAT THE RIGHT WING TRAILING EDGE; INBD AND ABOVE THE TANK 2 AFT BOOST PUMP; THERE IS A CRACKED ATTACH BRACKET. PICTURE ATTACHED / [01] REMOVED AND REPLACED CRACKED ATTACH BRACKET AT RIGHT WING TRAILING EDGE; INBOARD AND ABOVE TANK 2 AFT BOOST PUMP WITH NEW BRACSDR SWAA2022030170161Angle · crackedRH WING TRAILING EDGE ANGLE JUST INBOARD OF DEFLECTION CONTROL RIB IS CRACKED. (MPN IS 115A2156-8) / [01] REMOVED CRACKED TRAILING EDGE ANGLE AND ATTACHED SEAL RETAINER FOR REPLACEMENT.;[02] LOCATED AND DRILLED UP NEW TRAILING EDGE ANGLE MPN 115A2156-8 PER SRMSDR FDEA202202080247Former · crackedLH WING OUTBD FIXED LEADING EDGE FORMER IS CRACKED AT APPROX. OFSS 490 REMOVED AND REPLACED THE L/W FIXED O/B L/E NOSE FORMER AT STA O.S.S. 499.6 IAW BAC DWG# 114T2161, REV. - AND FEDEX EA H-5720-T0366757, TITLE: WINGS - SECONDARY WING STRCT - LH WING, LEASDR FDEA202202080246Former · crackedRW FIXED L/E AT #8 SLAT OTBD ROTARY ACTUATOR SLAT CURTAIN, THE OTBD NOSE FORMER IS CRACKED REMOVED AND REPLACED THE R/W FIXED L/E NOSE FORMER AT STA O.S.S. 499.6 IAW BAC DWG# 114T2161, REV. - AND FEDEX EA H-5720-T0366756, TITLE: WINGS - SECONDARY WING STRCT SDR FDEA202202080244Former · crackedR/H WING LEADING EDGE #9 SLAT INBD TRACK AREA HAS CRACKED FORMER ON INBD SIDE OF CURTAIN REMOVED AND REPLACED THE R/H WING FIXED L/E NOSE FORMER AT O.S.S. 565.9 IAW BAC DWG #114T2162, REV. - AND FEDEX EA H-5720-T0366755, TITLE: WINGS - SECONDARY WING STRCT -SDR FDEA202202080243Bracket · crackedLH WING OUTBD FIXED LEADING EDGE FORMER ATTACH ANGLE IS CRACKED ON THE INBD SIDE AT APPROX. OFSS 475 REMOVED AND REPLACED BRACKET 114T2171-4 ON THE L/W O/B FIXED L/E AT O.S.S. 484 IAW FEDEX EA H- 5720-T0366792, TITLE: WINGS - SECONDARY STRCT - LH WING, LEADSDR SWAA2022032169896Support · crackedRIGHT WING T/E STRUCTURE - DEFLECTION CONTROL RIB ANGLE SUPPORT RIB HAS CRACK .. DOT EV13 / [01] REMOVED DEFLECTION CONTROL RIB ANGLE SUPPORT CRACKED IN REF BB737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED DEFLECTION CONTROL RIB ANGLE SUPPORT IN REF B737-7SDR SWAA2022030869926Panel · pulledPANEL 561CB HAS SEVERAL PULLED FASTENER HOLES (MARKED) / FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). <BR><BR>DAMAGE WILL BE REPAIRED ACCORDING TO SRM 51-70-04-2R-9; AS REQUIRED BY SRM 57-51-01-2R-1; PARA. 4.B.(2); TABLE 202SDR SWAA2022030870145Panel · pulledPANEL 661BB HAS SEVERAL PULLED FASTENER HOLES / FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). <BR><BR>DAMAGE WILL BE REPAIRED ACCORDING TO SRM 51-70-04-2R-9; AS REQUIRED BY SRM 57-51-01-2R-1; PARA. 4.B.(2); TABLE 202SANDED RESDR SWAA2022030870146Panel · pulledPANEL 661AB HAS SEVERAL PULLED FASTENER HOLES / FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-51-01-1A-1; PARA. 4.B.(5). FILLED FASTENER HOLES IN REPAIR AREA WITH A MIXTURE OF BMS 8-301; CL1 RESIN (LOT# JH1GAA7833) AND MILLED GLASS FIBERS; THEN CURED RSDR SWAA2022031469540Fairing · crackedCRACK ACCESS PANEL 542BB FLAP SUPPORT FAIRING 3 RETAINER SEAL LT WING 2022-68006 / [01] REPLACED RETAINER SEAL ACCESS PANEL 524BB FLAP SUPPORT FAIRING 3 AT IAW B737-700 SRM 51-40-02-0G-0;[02] CORRECTED STEP 1<BR>REPLACED RETAINER SEAL ACCESS PANEL 542BB FLAP SSDR UIEA2022020200084None · noneCORROSION ON THE UPPER SURFACE OF U-17 STRINGER OF RH WING SKIN PANEL 1 & 2 AND RIB 1 AND RIB 3(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>AFFECTED U-17 STRINGER SEGMENT WAS TRIMMED TO REMOVE ALL CORROSION.</SPAN></P> / <P STYLE="MARGIN: 0IN 0IN 0.0SDR UIEA2022020200086None · noneCUT OUT ON UPPER CHORD, RIB #2 BETWEEN U-16 STRINGER TO U-18 STRINGER. THIS WAS REQUIRED TO GET ACCESS DURING U-17 STRINGER REMOVAL(<P ><SPAN>UPPER CHORD, RIB #2 BETWEEN U-16 STRINGER TO U-18 STRINGER WAS REPAIRED PER 767 SRM 57-20-09 REPAIR 1</SPAN></P> / <P>SDR SWAA2022022874579Panel · elongatedLH WING PANEL 521ZB HAS TWO HOLE SCREWS ELONGED. / [01] PREPARED PANEL #521ZB FOR REPAIR AS PER B737 SRM 51-70-06-2R-9;[02] VERIFIED PREPARED AREA;[03] REPAIRED PANEL #521ZB AS PER B737 SRM 51-70-2R-6 AND SRM 51-70-06-2R-0. MATERIALS USED RESIN P/O#1753536 FABSDR SWAA2022032167645Angle · crackedCRACKED ATTACH ANGLE AT MID PASSENGER CABIN ABOVE PRESSURE DECK BS691 RBL1 WL206. / [01] RECEIVED HEAT TREATED BACKET FROM OSS JOB # 541207 LOCATED AND DRILLED ; TRIMMED TO SIZE AND DEBURRED PER SRM 51-40-05 AND DWWG # 273A9112 REV-;[02] PRIOR TO STEP 1. REMOVSDR SWAA2022031766254Web · crackedRT WING TE ANGLE AT IB END OF TRANSVERSE WEB IS CRACKED WHERE IT ATTACHES TO DEFLECTION CONTROL RIB RT WING TE ANGLE AT O/B END OF TRANSVERSE WEB (CLIP) IS CRACKED WHERE IT ATTACHES TO DEFLECTION CONTROL RIB / [01] CORRECTION TO WRITE UP NAME; RT WING TE ANGLESDR SWAA2022031574070Angle · crackedRT WING TE BULB SEAL SUPPORT ANGLE AT ORSS 273 (WBL 201.9) ABOVE PYLON STRUT FAIRING TIP / [01] REMOVED R/H WING T/E BULB SEAL SUPPORT ANGLE AT ORSS 273 IAW SRM 51-40-02-0G-0.;[02] REPLACED R/H WING T/E BULB SEAL SUPPORT ANGLE AT ORSS 273 IAW SRM 51-40-02-0G-0SDR SWAA2022031066534Bracket · crackedCRACK TRAILING EDGE SUPPORT BRACKET AT LEVEL OF WBL 191 AT LT WING (1 EA) 2022-55624 / [01] REPLACED TRAILING EDGE SUPPORT BRACKET AT LEVEL OF WBL 191 AT LT WING (1 EA) IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG #115A2930 REV - SEE INDIVIDUAL SIGN OFFS BELOW.;SDR SWAA2022031066361Bracket · crackedCRACK BODY STATION 540 SUPPORT BRACKET OF BLEED DUCT ON LH SIDE AT LOWER FUSELAGE (1 EA) 2022-55506 / [01] REPLACED SUPPORT BRACKET OF BLEED DUCT ON LH SIDE AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 DWG 212A1116 REV -;[02] CERTIFIED WORK PERFORMED.SDR SWAA2022031066150Web · elongatedELONGATED HOLE ON WEB INTERNAL CAVITY OF ACCESS PANEL 611AT AT RT WING 2022-55484 / [01] REPLACED WEB LOCATED ON CAVITY OF ACCESS PANEL 611AT AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 212A1901 SHEET:1 REV:A.<BR>SEE INDIVIDUAL SIGN OFFSDR SWAA2022031465316Access Panel · crackedCRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES RT WING 2022-67653 / [01] TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18185733 DUE DATE: 16-JAN-23.;[02] TOOL USED: SCALE P/N: CL5000; S/N: AE-408751; DUE DATE: 19-MAR-22;[03] TOOL USED MULTIMETER P/N: FLUKE 15SDR SWAA2022031065383Panel · corrodedCORROSION LEADING EDGE FUEL SERVICE PANEL; LOC INTERNAL AREA OF ACCESS PANEL 621GB AT RT WING 2022-55450 / [01] REPLACED REFUELING SERVICE PANEL LOC. AT INTERNAL AREA LEADING EDGE RT WING IAW B737-700 SRM 51-40-02-0G-0; REMOVAL/INSTALLATION AND OPERATIONAL TESSDR SWAA2022031065366Bracket · crackedCRACK TRAILING EDGE BRACKET LOCATED BS. 663.75; IRSS 139.0 MLG AREA; AT RT WING 2022-55366 / [01] REPLACED TRAILING EDGE BRACKET LOCATED BS. 663.75; IRSS 139.0 MLG AREA; AT RT WING IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 <BR>SEE INDIVIDUAL SIGN OFFSDR SWAA2022020165018Fairing · crackedL/H WING # 3 CANUE FWD FAIRING IS CRACKED ; LH WING # 3 CANE FWD FAIRING IS CRACKED / [01] REMOVED AND REPLACED L/H WING # 3 FLAP SUPPORT FAIRING IAW AMM 27-51-18SDR SWAA2022020464758Support Bracket · corrodedLEFT WING BOOST PUMP TANK # 1 LOWER BONDING STRAP AND SUPPORT BRACKET CORRODED ; / [01] REMOVED SUPPORT BRACKET AT LT WING BOOST PUMP TANK # 1 LOWER BONDING AS PER B737-700 SRM 51-40-02-0G-0.; [02] BONDING TESTER USED BC 168698 EXP APR 2022; [03] CLEANED CORROSDR SWAA2022022164489Bracket · crackedLT WING ATTACH BRACKET CRACKED BELOW FWD INBD END OF PANEL 551AT [MARKED]. / [01] REMOVED AND REPLACED BRACKET PER SRM 51-10-02.;[02] REMOVED AND REPLACED BRACKET PER SRM 51-10-02.SDR SWAA2022020464059Skin · delaminatedR/W REAR SPAR UPPER PANEL ABOVE RMLG STRUT LOWER SKIN AREA DELAMINATED FWD OF SPEED BRAKE CABLE SAFETY LOOP MKD DOT ; / [01] PREPARED FOR REPAIR AT R/W SPAR UPPER PANEL ABOVE RMLG STRUT LOWER SKIN AS PER B737-700 SRM 51-70-04-2R-1; [02] VERIFIED STEP #1.; [03]SDR SWAA2022020463590Fitting · crackedR/W REAR SPAR FIXED T/E DEFLECTION CONTROL RIB PANEL VERTICAL BULB SEAL FITTING CRACKED I/B SIDE MKD ; / [01] REMOVED SEAL FITTING AT R/W REAR SPAR T/E REF B-737-700 SRM 52-40-02-0G-0; [02] LOCATED AND DRILLED SEAL FITTING AT R/W REAR SPAR T/E REF B-737-700 SRSDR SWAA2022012763883Fairing · cracked#3 CANOE FAIRING CENTER HAS CRACK ON THE INSIDE OF FAIRING (CENTER AFT ) ; / [01] REMOVED DAMAGE TO #3 CANOE IAW SRM 51-70-05-2R-0. DAMAGE LIMITED TO INNER PLIES. NO HONEYCOMB DAMAGE NOTED. APPLIED REPAIR AS PER SRM 51-70-05-2R-0; SEALED PER SRM 51-70-08.SDR SWAA2022021663455Web · crackedRIGHT WING DEFLECTION CONTROL RIB WEB CRACKED / [01] REMOVED DAMAGED WEB; LOCATED; DRILLED NEW WEB PER SRM 51-40-02. OK TO INSTALL;[02] REMOVED AND REPLACED PER SRM 51-40-02.
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