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 SWAA2022042687027Bracket · crackedCRACK INBOARD TRAILING EDGE BRACKET LOCATED ON IRSS 140 AT RT WING 2022-158252 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500 D; S/N: N500X12101V022235; DUE DATE: 03-JUN-22.;[02] REPLACED BRACKET LOC ON INBOARD TRAILING EDGE ON IRSS 140 AT RT WING ISDR SWAA2022041886086Panel Support · corrodedRT WING L/E PANEL SUPPORT AT SS 75.0 HAS CORROSION ON VERTICAL FLANGE / [01] NO ALLOWABLE DAMAGE ENTRY FOUND IN SRM; PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9 C.;[02] REMOVED AND REPLACED RT WING L/E PANEL SUPPORT PN 116A5301U38 AT SS 75.0 IAW SDR SWAA2022041287052Bracket · elongatedELONGATED HOLE BRACKET ON ACCESS PANEL 651GB AT RT WING 2022-131837 / [01] REPLACED BRACKET ON ACCESS PANEL 651GB AT RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-40-02;[02] REPLACED BRACKET ON ACCESS PANEL 651GB AT RT WING IAW B737-700 SRM 51-10-02 AND SRM 51-SDR IXXA20220509201Angle · crackedRH WING LE STA 522 ANGLE CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00280SDR SWAA2022042686101Access Panel · crackedCRACK ACCESS PANEL 544BB AT LT WING 2022-158116 / [01] TOOL USED: CALIPER P/N:500-464 S/N:15331926 DUE DATE:28-SEP-22.;[02] TOOL USED:SCALE P/N:CL5000 S/N:AE-39087 DUE DATE:07-JUL-22.;[03] REPAIRED ACCESS PANEL 544BB IAW B737-700 SRM 57-53-70-2R-5 REPAIR 5 TOOSDR SWAA2022042686103Bracket · crackedCRACK BODY STATION 540 ON ANGLE AT AIR CONDITIONING BAY (L/H SIDE ) 2022-158146 / [01] REMOVED AND REPLACED BRACKET ASSY AT PNEUMATIC DUCT BODY STATION 540 LT AIR CONDITIONING BAY IAW SRM 51-40-02-0G-0 SEE INDIVIDUALS SING-OFFS BELOW.;[02] TASK COMPLETED<BR><BSDR IXXA2022050703Web · crackedR WING WS 522 LE, UPON REMOVAL OF CRACKED ANGLE FOUND THE ATTACHING WEB IS CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00256SDR IXXA2022050702Angle · crackedR/W STA 664 L/E LOWER RIB SUPPORT ANGLE IS CRACKED. FAS WO N431AZ-01-01 NON ROUTINE 00253SDR IXXA2022050605Angle · corrodedRH WING LE RIB AT WS 656 HAS CRACKED LOWER ANGLE. FAS WO N431AZ-01-01 NON ROUTINE 00111SDR SWAA2022042085229Bracket · crackedLOWER BULB SEAL BRACKET AT ORSS 261+13 IS CRACKED. (MARKED) / [01] REMOVED AND REPLACED LOWER BULB SEAL BRACKET AT ORSS 261+13 IAW SRM 51-40-01-0G-0 PARA. 4.;[02] INSPECTION COMPLETESDR SWAA2022041284649Support · crackedWING TO BODY FAIRING SUPPORT AT BS 500I APROXIMATLY S19RH CETER SPLICE CRACKED AT UPPER OTBDHI LOC A225-013 / [01] REMOVED FAIRING SUPPORT IAW B737 SRM 51-40-02-0G-0. NEW PART VERIFIED AS P\N 116A3118U10 IAW BOEING DWG # 116A3110 REV B. STARTED LOCATING AND DRSDR ABXA2022031647Skin · corrodedDURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE LH WING SKIN PANEL NO. 1(112T4102-1) AT THE REAR SPAR AND WS 440-450. THE CORROSION IS LOCATED ON THE UPPER SURFACE OF THE BOTTOM SKIN AND TRAVELS BETWEEN THE SKIN AND REAR SPAR, ANDSDR IPXA2022033080667Former · crackedINSPECTION TYPE:C1L/H O/B WING L/E HAS A FORMER THAT IS CRACK JUST I/B OF THE #9 SLAT TRACK.REMOVED, FAB, REPLACED CRACK FORMER IAW DWG ARB2931 AND SRM 51-33-01. (MINOR)SDR FDEA202203150514Former · crackedLEFT WING L/E CAVITY CURTAIN BRACKET CRACKED AT OFSS 437 REMOVED AND REPLACED NOSE FORMER ON THE L/W L/E AT STA OSS441 (APPROX STA OFSS 437) IAW BAC DWG 114T2241, REV.- AND FEDEX E.A. H-5720-T0367288-P1, RELEASE DATE: MARCH 03, 2022, TITLE: WINGS - SECONDASDR IXXA202206088001Torque Tube · wornLW INBD #4 SUPPORT TORQUE TUBE WORN AND PITTEDSDR SWAA2022041283810Access Panel · delaminatedDELAMINATED ACCESS PANEL 521DB AT LT WING 2022-131697 / [01] TOOL USED: CALIPER P/N 500-464 S/N 15331926 DUE DATE 28-SEP-22.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18196119 DUE DATE 24 FEB 23;[03] TOOL USED SCALE P/N:CL5000 S/N:AE-408758 DUE DATE 09-FEBSDR FDEA202203140505Former · crackedR/W FIXED L/E, NOSE FORMER CRACKED AT STA. O.S.S. 437 (RIB 5) REMOVED AND REPLACED R/W FIXED L/E NOSE FORMER AND ATTACH ANGLE AT OSS 437 IAW BAC DWG 114T2240, REV.- AND FEDEX EA H-5720-T0367286-P1, RELEASE DATE: MARCH 03, 2022, TITLE: WINGS - SECONDARY WINSDR FDEA202203140501Former · crackedLEFT WING L/E EXTERNAL UPPER SKIN 3(EACH) FASTENERS NOT FLUSH AT OFSS 490 REMOVED FORMER AND REPLACED WITH NEW FORMER IAW B767 SRM 51-40-02-0G AND BAC DWG 114T2161, REV.- AND FEDEX EA H-5720-T0367285-P1, RELEASE DATE: MARCH 03, 2022, TITLE: WINGS - SECONDASDR SWAA2022041283306Access Panel · elongatedDOT # A-111-001 PANEL # 521QB LEFT WING LOWER L/E ONE HOLE ELONGATED / [01] EVALUATED PANEL 521QB AND FOUND DAMAGE AROUND UPPER SURFACE OF MARKED FASTENER HOLE. FOUND TO BE REPAIRABLE. IAW B737-800 SRM 57-41-01-2R-1 PAR 1A & 2.B.(2) REV74. CLEAN AND PREP AREA SDR SWAA2022040583428Panel · crackedCRACK ACCESS PANEL 621PB AT RT WING 2022-144761 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29-SEP-22.;[02] TOOL USED HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23.;[03] TOOL USED SCALE CL5000 S/N: AE-408758 DUE DATE: 09-FEB-2SDR SWAA2022041283130Access Panel · crackedCRACK ACCESS PANEL 621FB AT RT WING 2022-131656 / [01] TOOL USED P/N 500-464 S/N 15331926 DUE DATE 28-SEP-22.;[02] TOOL USED SCALE P/N:CL5000 S/N:AE-408758 DUE DATE 09-FEB-23;[03] TOOL USED: HOT BONDER: P/N: HCS9200B; S/N: 1622983; DUE DATE: 16-JAN-23.;[04] TOSDR FDEA202203120489Former · crackedRW LE NOSE FORMER CRACKED L/E 436.0 REMOVED AND INSTALLED NEW FORMER P/N 114T2170-6 IAW BOEING DWG# 114T2241 REV.- AND FEDEX EA H5720-T0367291-P1, DATED MAR 03, 2022, TITLE: WINGS - SECONDARY WING STRCT - RH WING, LEADING EDGE, ANGLE, OSS 441, ALTERNATE FASDR SWAA2022041982723Angle · crackedCRACK ANGLE TRAILING EDGE AREA DEFLECTION CONTROL RIB ON ORSS 273 AFT SIDE AT LT WING 2022-122223 / [01] REPLACED ANGLE TRAILING EDGE AREA DEFLECTION CONTROL RIB ON ORSS 273 AFT SIDE AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND DWG-115A2930 REV:- SEE INDIVISDR FDEA202203110472Former · crackedRW LE SKIN HAS A BROKEN FASTENER, L/E STA 488.0 UPON FURTHER INVESTIGATION FOUND FORMER CRACKED AT FASTENERS. REMOVED AND INSTALLED NEW FORMER IAW BOEING DWG# 114T2161, REV.- AND E.A.# H-5720-T0367292-P1, DATE: 03 MARCH 2022, TITLE:WINGS - SECONDARY WING SSDR SWAA2022041982452Access Panel · crackedCRACK ACCESS PANEL 661CB ON OPEN HOLE AT RT WING 2022-122142 / [01] TOOL USED: CALIPER P/N 500-196-30 S/N A21033416 DUE DATE 07-OCT-22.;[02] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 15102320 DUE DATE: 16-JAN-23.;[03] TOOL USED: SCALE PN:CL5000 SN:AE-37099 DUESDR SWAA2022031480987Fitting · crackedLEFT WING - MID SPAN BULKHEAD SEAL RETAINER FITTING IS CRACKED. / [01] REMOVED AND REPLACED SEAL RETAINER FITTING ON LEFT WING MID SPAN BULKHEAD IN REF TO SRM 51-40-02SDR SWAA2022031880920Panel · elongatedPANEL 651FB O/B AFT EDGE HOLE ENLONGATED / [01] REMOVED SEAL RETAINER TO GAIN ACCESS FOR COMPOSITE REPAIR IAW SRM 51-40-02-0G-0. REPAIRED ENLONGATED HOLE AT AFT EDGE ON PANEL 651FB IAW SRM 51-70-04-2R-9.SDR DALA2022030801513None · noneSHIP 3318 DURING DEICE. DEICE TRUCK BOOM MADE CONTACT WITH RIGHT WINGTIP. WINGLET AFT SIDE ONLY. CORRECTIVE ACTION: FWD TO CDL 57-00-02. REMOVED RT WINGLET PER A330 AMM 57-31. C/W INSPECTION OF IMPACT ON WINGTIP & SURROUNDING AREAS. NO DAMAGE FOUND. ONLY DAMAGSDR SWAA2022030980629Bracket · crackedR/H WING PANEL SUPPORT FORWARD Z ANGLE IS CRACKED / [01] REMOVED AND REPLACED R/H WING PANEL SUPPORT FORWARD Z ANGLE BRACKET IAW SRM 51-40-02SDR REXA2022040100499Angle · corrodedPANEL 642AZ SUPPORT ANGLE ON AUX SPAR IS CORRODED. REMOVED AND REPLACED SUPPORT ANGLE IAW CRJ 900 SRM 51-42-21-001-001-A01.SDR SWAA2022032979227Panel · corrodedA-061 DOT 013 R/H WING FUEL QTY PNL UNDER PNL 621GB CORRODED AT CUTOUT FOR TANK #1 FUEL QTY GAUGE / [01] REMOVED CORROSION FROM FUEL QTY PANEL ON R/H WING IAW SRM 51-10-02-0G-0 SECTION 15. VERIFIED WITH 10X MAGNIFICATION.;[02] VERIFIED STEP 1;[03] MEASURED FORSDR SWAA2022032880495Plate · crackedA-061 DOT 018 R/H WING T/E WIGGLE PLATE INBD 0F #7 FLAP TRACK LOOSE / [01] REMOVED WIGGLE PLATE I.A.W SRM 51-40-02-0G-0;[02] VERIFIED NEW PLATE AS PART #115A3760-42 I.A.W BOEING DWG 115A3700 REV:- ATAG#A117635;[03] DRILLED NEW WIGGLE PLATE I.A.W SRM 51-40-05-0SDR YENA2022031600233None · noneDURING HEAVY MAINTENANCE, (EA A22-132-01) WINGS / RH WING / TOP SKIN PANEL 2 / TE OVERHANG LOWER SURFACE
AT RIBS 10-11 / CORROSION - PERMANENT REPAIR (CLASSIFIED AS A MAJOR REPAIR)SDR FDEA202203010442Fitting · corrodedSMIS 597 57-20 5046 05MAR22 MEM FACT U MOD TYPE T MOD NO. 1-5720-T0367318 REV NO. A PS P1 WING - SECONDARY WING STRCT - R/H MLG TRUNNION UPPER / LOWER PAD WHERE A-FRAME COMPLY WITH E..A. 1-5720-T0367318 REV NO. A POS P11 INFO 06MAR22 00:27 SDR SWAA2022030779023Bracket · crackedLH WING T/E CAVITY TO I/B FLAP SEAL SUPPORT BRACKET IS CRACKED BEHIND #1 PYLON / [01] REMOVED AND REPLACED LH WING T/E CAVITY TO I/B FLAP SEAL SUPPORT BRACKET PER SRM 51-40-02 AND AMM 20-50-11SDR SWAA2022040178855Panel · pulledLT WING PANEL 543EB HAS SEVERAL PULLED THROUGH FASTENERS. / [01] REMOVED OLD TAIL CONE AND PICKED UP HOLES IN NEW TAIL CONE 543EB PER SRM 51-40-02-0G-0.;[02] VERIFIED;[03] INSTALLED AFT TAIL CONE FAIRING ONTO CANOE PER AMM 27-51-28-400-802.;[04] C/W INSPECTIONSDR SWAA2022040178431Balance Weight · corrodedON THE LEFT WING LEADING EDGE OTBD END; THE BALLAST WEIGHTS HAVE EVIDENCE OF CORROSION. / [01] COMPLIED WITH EA M-22-157-00365.;[02] C/W EA M -22-157-00365SDR SWAA2022040178427None · crackedRT WING FLAP DEFLECTION RIB PLATE CRACKED (MARKED) / [01] REMOVED DAMAGED DEFLECTION RIB TAB PER SRM 57-51-02-2R-3 REPAIR 3;[02] ACCOMPLISHED NDT ON DAMAGE REMOVAL. NO DEFECTS NOTED PER NDT MANUAL PART 6 CH51-00-00 PROCEDURE 23.;[03] TOOL UPDATE.;[04] ROTO PEESDR SWAA2022032978889Attach Angle · crackedA-061 DOT 003 L/H WING ATTACH ANGLE FOR UPPER FIXED TRAILING EDGE PNL BETWEEN #5 AND #6 FWD ATTACH ANGLE CRACKED / [01] REMOVED DAMAGE ATTACH ANGLE IAW SRM 51-40-02-0G-0;[02] VERIFIED NEW ATTACH ANGLE P/N 115A2156-7 TAG # A117676 IAW DWG 115A2512;[03] VERIFIEDSDR SWAA2022032978890Attach Angle · crackedA-061 DOT 002 L/H WING ATTACH ANGLE FOR UPPER FIXED TRAILING EDGE PANEL BETWEEN #5 AND #6 SPOILERS CRACKED / [01] REMOVED DAMAGE ATTACH CLIP IAW SRM 51-40-02-0G-0;[02] VERIFIED NEW ATTACH CLIP P/N 115A6260-1 TAG#A117854 IAW DWG 115A6200;[03] VERIFIED STEPS 1 ASDR REXA2022040100511Panel · chafedRH WING PANEL 699AB HAS CHAFE DAMGE. DRILLED, COUNTERSINK AND PAINTED NEW PANEL IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-25-01-001-001-A01.SDR SWAA2022040178410Panel · crackedLEFT WING PANEL 561AB HAS CRACKS AROUND NUMEROUS FASTENER HOLES. / [01] REPAIRED PER SRM 51-70-04 REPAIR #9.;[02] INSPECTED WORK PERFORMED IN CORRECTIVE ACTION #1. NICHOLAS DEBUS (TECHNICIAN); 11-MAR-2022 20:41 UTC REPAIRED PER SRM 51-70-04 REPAIR #9.;[03] REPSDR SWAA2022040178413Panel · crackedLEFT WING PANEL 561CB HAS CRACKS AROUND NUMEROUS FASTENER HOLES. / [01] REPAIRED PER SRM 51-70-04 REPAIR #9.;[02] INSPECTED WORK PERFORMED IN CORRECTIVE ACTION #1. NICHOLAS (TECHNICIAN); 11-MAR-2022 20:36 UTC REPAIRED PER SRM 51-70-04 REPAIR #9.;[03] INSPECTEDSDR SWAA2022030978125Shield · crackedNO.2 PYLON STRUT FAIRING INTERNAL SUPPORT RIB NO. 5 (CASTING)PN 313A2752-2 CRACKED AT FASTENER HOLES. DOT 234/05. / [01] DISPLACED INBD AND OUTBD BLADE SEALS FOR F.O.M IAW ARM 51-40-02-0G-0;[02] REMOVED AFT FITTING MOUNT FOR F.O.M IAW ARM 51-40-02-0G-0;[03] RESDR SWAA2022030978504Fitting · elongatedRIGHT WING TRAILING EDGE PANEL 651GB FORWARD ADJUSTMENT ROD UPPER CLEVIS ATTACH POINT TEE FITTING HOLE ELONGATED. DOT 234/11 / [01] REMOVED AND REPLACED ELONGATED TEE FITTING WITH PN 115A2350-1 ATAG# A117187 IAW BOEING DWG 115A5300 SHT 6 REV- AND SRM 51-40-02-SDR ASAA2022022439662Skin · corrodedCORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 3" I/B OF RIB 18 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 3" I/B OF RIB 18 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022SDR ASAA2022022439656Skin · corrodedCORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 2" I/B OF RIB 13 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN UPPER SURFACE 2" I/B OF RIB 13 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022SDR ASAA2022022439655Skin · corrodedCORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 6" I/B OF RIB 14 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 6" I/B OF RIB 14 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022SDR ASAA2022022439654Skin · corrodedCORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12" O/B OF RIB 21 GROUNDED - YES. CORROSION ON RIGHT WING UPPER TRAILING EDGE SKIN LOWER SURFACE 12" O/B OF RIB 21 REPAIRED PER EA A320-57EA-01458 REV 00 DATED 8/22/2022SDR SWAA2022032876642Panel · delaminatedRT WING L/E PANEL 621HB HAS DELAMINATED AREAS ALONG L/E / FOUND DAMAGE TO GLASS FIBER PLIES TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARA 4. A. (5) (A)-(B) REMOVED DAMAGED PLIES IN (1 EA) LOCATION. TAPER SANDED AND CLEANED REPAIR WITH NO CONTAMINATI
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