JASC 5710
Service difficulty reports · 4,458
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 SWAA2024071690668Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 305 AT RT WING 2024-345622<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 305 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9; B737-700 SRM 51-40-02 AND DWG # 115A3700 REV-;[02] COMPLETED TASK CERTIFIEDSDR SWAA2024070990661Retainer · crackedLEFT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL LOWER T/EHORIZONTAL BULB SEAL RETAINER O/B ATTACHED CLIP CRACKED @ FASTENER HEAD MKD DOT<[01] REMOVED AND REPLACED LT WING FIXED T/E REAR SPAR DEFLECTOR CONTROL RIB PANEL LOWER O/B CLIP REF B737-700 SRSDR SWAA2024070990655Retainer · crackedRIGHT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL LOWER VERTICAL SEAL RETAINER CRACKED @ FASTENER HEAD MKD DOT<[01] REMOVED AND REPLACED SEAL RETAIN AT RIGHT WING FIXED T/E REAR SPAR DEFLECTION CONTROL RIB PANEL PER REF B 737 SRM 51-40-02-0G-0.;[02] SDR SWAA2024071690379Panel · corrodedCORROSION ON REFUELING PANEL ON LEADING EDGE AT RT WING 2024-345588<[01] ON STEP 4. TOOL USED: THICKNESS GAGE. P/N: 45MG. S/N: 221859911. DUE DATE: 17-NOV-24. <BR><BR>ON STEP 5. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 60009161631. DUE DATE: 11-MAR-25.SDR SWAA2024071690030Support Beam · crackedCRACK ON SUPPORT BEAN ON DEFLECTION CONTROL RIB TRAILING EDGE AT LT WING 2024-345553<[01] TOOL USED STEP 8: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21 JUL 24.;[02] PERFORMED PERMANENT REPAIR ON DEFLECTION CONTROL RIB AREA LH WING IASDR UIEA2024052400441Fitting · corrodedLH WING FWD LOAD PITCH FITTING, CORROSION DAMAGE ON INB FITTING.(<P>CORROSION ON INBD FITTING WAS REWORKED IAW TRE6757246, REV 1, MAY 20, 2024. LEVEL CORROSION 2. NO FURTHER DEFECTS NOTED.</P>)SDR FDEA202405240725Former · crackedWING FIXED LEADING EDGE NOSE FORMER ANGLE CRACKED AT OSS 499.6 ON THE LEFT WING. REMOVED THE DAMAGED NOSE FORMER ANGLE FROM THE LEFT WING FIXED LEADING EDGE AT OSS 499.6. INSTALLED A NEW NOSE FORMER ANGLE. FEDEX DRAWING SR67-57-002 REV. A.SDR FDEA202405240724Former · crackedFIXED LEADING EDGE NOSE FORMER ANGLE CRACKED AT OSS 441 ON THE LEFT WING. REMOVED THE DAMAGED NOSE FORMER ANGLE FROM THE LEFT WING FIXED LEADING EDGE. INSTALLED A NEW FORMER ANGLE, B67-57-002-01. FEDEX DRAWING SR67-57-002 REV. A.SDR SWAA2024061489383Bracket · crackedCRACK BRACKET ANGLE ACCESS PANEL 651FB AT RT WING 2024-340178<[01] REPLACED BRACKET LOC. ON ACCESS PANEL 651FB AT RT WING I.A.W B737-800 SRM 51-40-02-0G-0 AND DWG 115A2710 SHEET 9 REV A AND MEASURES OF CRACK ARE: L:1.356? TOOL USED CALIPER P/N: 500-196-30; S/NSDR AALA202406253915Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND 3. REPAIRED LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FITTSDR AALA202406253291Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FITTING BETWEEN WS 70 AND WS 141, BETWEEN RIBS 2 AND 3. REPAIRED RIGHT WING MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT BRACKET / JACK FISDR IPXA2024052977830Former · cracked- CRACK - FORMER, LH WING OUTBD FXD LE OSS 441.6 NOSE SKIN (REPLACE).REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 114T2241 SH. 4 REV. JOB COMPLETED. REVIEW COMPLETEDSDR JR2R20240524405Heat Shield · damagedLH AFT PYLON FAIRING FWRWARD LOWER HEAT SHIELD HAS ELONGATED SCREW HOLES. REPAIREDSDR IPXA2024052277830Former · crackedCRACK - FORMER, LH WING OUTBD FXD LE OSS 441.6 NOSE SKIN (REPLACE) OKAY TO WORK OPENSDR SWAA2024071187644Vapor Barrier · cracked(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 RH SIDE AT WING CENTER SECTION 2024-345335<[01] TOOL USED: CALIPER: P/N:500-197-30 SN: B20189521; DUE DATE: 26-JAN-25.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185781 DUE DATE: 15-FEB-25.;[0SDR SWAA2024061090725Panel · damagedRIGHT WING PANEL 621KB INNER SURFACE FOIL TORN<[01] ACCOMPLISHED REPAIR TO FOIL PER SRM 51-70-14-2R-3.;[02] VERIFIED 1. RYAN ROGERS (TECHNICIAN); 28-MAY-2024 20:23 UTC<BR>ACCOMPLISHED REPAIR TO FOIL PER SRM 51-70-14-2R-3. C/WSDR DALA2024051505239Isolator · wornWORN ISOLATOR ITEM #11 WORN TO LIMITS ON LH WING RIB 6. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 100-0001:2820-01281-05A/009 00244 REMOVED AND REPLACED ISOLATOR PER AMDS 2820-01281-05A-LH. (LP# 0343015)SDR VNAA20240724002Canister · crackedSETTLEMENT FITTING AT FS310 LBL37 WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-43-101-001-A03 AND WAS REPLACED PER CRJ900 SRM 51-42-21-001-001-A01. CANISTER OF SLAT TRACK 1-3 AT RH FUEL TANK WAS REPAIRED PER REO 670-57-42-577. REV. - -SDR NACA2024051400001Winglet · ground damageLEFT WINGLET DAMAGED, STRUCK AIRCRAFT ON THE GROUND. REMOVED LH WINGLET PER NAC EA 767-57-000046. INSTALLED LEFT HAND WINGLET IAW B767 AMM 57-31-03SDR SWAA2024060384930Fuel Panel · corrodedFUELING STATION PANEL AT 621GB HAS SURFACE CORROSION.<[01] REMOVED AND REPLACED FUELING PANEL PER SOPM 20-50-01 AND MM 28-41-61;[02] VERIFIED. REMOVED AND REPLACED FUELING PANEL PER SOPM 20-50-01 AND MM 28-41-61;[03] WING REFUELING PANEL INDICATORS AND LIGHTS SDR SWIA20240507Guide Fitting · gougedRH INTERNAL OUTBOARD WING TRAILING EDGE (EWIS) OUTBOARD FLAP AFT ROLLER GUIDE FITTING GOUGED (C-CHECK RO 7/17/2024) PERFORMED REPAIR TO RH OUTBD FLAP AFT ROLLER GUIDE FITTING. PER REO 670-57-53-366 REV -- DATED 2024-06-08. COMPLIED WITH TASK CARD 51-900SDR FDEA202405240561Former · crackedLEFT WING - FIXED LEADING EDGE FORMER AT STATION XOS 584 FOUND CRACK ABOUT 2 INCHES. LEFT WING FIXED LEADIING EDGE CRACKED FORMER AT STATION XOS 584 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISISDR FDEA202405030566Former · crackedRIGHT WING - FIXED LEADING EDGE UPPER FORMER AT STATION XOS 584 FOUND CRACK ABOUT 1 INCH. RIGHT WING FIXED LEADING EDGE CRACKED UPPER FORMER AT STATION XOS 584 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARSDR FDEA202405030561Former · crackedLEFT WING - FIXED LEADING EDGE FORMER AT STATION XOS 584 FOUND CRACK ABOUT 2 INCHES. LEFT WING FIXED LEADIING EDGE CRACKED FORMER AT STATION XOS 584 REMOVED AND REPLACED AS PER MD-11 SRM 51-31-01-0G. FORMER FABRICATED AS PER DOUGLAS DRAWING ARB 2931 REVISISDR VNAA20240531026Canister · crackedREF. TO: DURING INSPECTION OF THE TASK CARD TRFKE000WL78: 600-08E2-JIC IT WAS DETECTED CRACK IN CANISTER WELDED NO.3 STA. WS148 OF INTERNAL LH MAIN FUEL TANK. CANISTER WELDED NO.3 STA. WS148 OF INTERNAL LH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577. RESDR SWAA2024060580600Fuel Panel · corrodedCORROSION LEADING EDGE FUEL QUANTITY INDICATOR CASE AT RT WING 2024-293815<[01] REPLACED REFUEL PANEL (P15) TEST OK IAW B737-700 AMM 28-21-00-400-801<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED REFUEL PANEL (P15) TEST OK IAW B737-700 AMM 28-21-00-401<BR>SEESDR AALA202405027816Beam · brokenAIRCRAFT IN BASE MAINTENANCE: LEFT HAND WING T/E PANEL LANDING BROKEN JUST BELOW NUMBER 3 SPOILER. REMOVED AND INSTALLED NEW LOWER CHORD (AALA202405021209), AND NEW BEAM ASSEMBLY (AALA202405027816). PER B777-200 SRM 51-40-02-0G PARA 7 AND 9.SDR SWAA2024052280130Plate · crackedLH WING REAR SPAR WAFFLE PLATE CRACKED JUST OUTBD OF ACCESS 551DB<[01] REPLACED PLATE ASSY PER SRM 51-40-02.SDR UIEA2024042600317Beam · corrodedCORROSION ON RH WING TRAILING EDGE STRUCTURE SPOILER BEAM UPPER CHORDS BETWEEN WBL 154.54 / 294.02(<P>CORROSION DAMAGES ON RH WING TRAILING EDGE STRUCTURE SPOILER BEAM UPPER CHORDS WERE BLEND OUT, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS PER SRM 57-51-02-1ASDR DALA2024042804740Drag Fitting · damagedAIRCRAFT 6809, DURING H CHECK MAINTENANCE VISIT AT MX (QRO), WHILE ACCOMPLISHING INSPECTIONS ON THE LH WING, FORWARD DRAG FITTINGS PER EM 5720-01100-04A & EM 5720-01100-05A DAMAGE INDICATION WAS FOUND ON WING SKIN AND FITTING LAYER ON HOLES #2-#5, #7-#9, #12, SDR JR2R20240425818Panel · damagedPANEL 522DB HAS DAMAGED/ELONGATED HOLE. REPAIREDSDR SWAA2024060778429Winglet · corrodedCORROSION AT RIGHT WINGLET UPPER TIP AFT EDGE.<[01] CUT OUT DAMAGED AREA WITH CORROSSION AT RIGHT WINGLET UPPER TIP AFT EDGE AS-PER SRM 57-30-01 REPAIR 6 FIG 201 DETAIL 2.TREATED PRIMED AND TOP COATED WORKED AREAS AT RIGHT WINGLET UPPER TIP AFT EDGE. AS-PER SOSDR UIEA2024041900286Nut · unknownREFER JOB CARD SEQ 1.725 #1 CANOE AFT FRAME MOD FIG 6 INSTALLATION AFTER ROW HAS 5EA FASTENER HOLE LOCATION CAN NOT USE BACC30AC6 DUE HOLES TOO CLOSE TO ART INTERFERENCE COLLAR(<P>NUTS REPLACED AS PER RI-57-50-16856 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024042200303Beam · crackedRHW L/E ILES 560 D BEAM WEB CRACKED(<P>RHW L/E ILES 560 D BEAM WEB REPAIRED AS PER RI-57-41-16827 REV A. NO FURTHER DEFECTS NOTED</P>)SDR SWAA2024053177680Nut Plate · crackedCRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS576 AT LT WING 2024-270036<[01] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS576 AT LT WING. IAW B737-700 SRM 51-40-02; DWG: 112A4402 SHEET: 14 REV:- AND IAW B737-700 SRM 51-10-SDR SWAA2024053177678Nut Plate · crackedCRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS574 AT RT WING 2024-270033<[01] REPLACED INTERNAL CAVITY LEADING EDGE RAIL NUTPLATE LOCATED OFSS 574 AT RT WING .IAW B737-700 SRM 51-40-02; DWG:112A4402 SHEET:14 REV:-AND IAW B737-700 SRM 51-10-02SDR SWAA2024053177679Nut Plate · crackedCRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT RT WING 2024-270034<[01] REPLACED INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 112A4402 SHEETS 13 REV-.;[02] COMPLETED JOBSDR SWAA2024053177682Nut Plate · crackedCRACK INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT LT WING 2024-270035<[01] REPLACED INTERNAL CAVITY LEADING EDGE ON RAIL NUTPLATE LOCATED OFSS449 AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 112A4402 SHEETS 13 REV-.;[02] COMPLETED JOBSDR SWAA2024052383782Deflector · damagedCHECK L/H WING DEFLECTOR RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATES FOR CONDITION AND ELONGATED HOLES.<[01] VISUAL INSPECTION ACCOMPLISHED AT LT WING TE DEFLECTION RIB TO DEFLECTOR PANEL ATTACH SERRATED PLATES REF. SRM 51-10-04-0G-0 AND AMM 57-50-01-820-801SDR HNAA20240522466Torque Box · cracked57-2275 3 HOLES FOUND WITH NDT INDICATION ON RH WING TQ BOX AT RIB 1. REPAIRED IAW EO1-57-24-0297SDR HNAA2024052200465Torque Box · cracked57-2274 2 HOLES WITH NDT INDICATIONS ON LH WING TQ BOX AT RIB 1 WITH 1 BUSHING DAMGED. REPAIRED IAW EO1-57-24-0297SDR SWAA2024050676904Support Bracket · crackedBLEED AIR DUCT SUPPORT BRACKET IS CRACKED AT LEFT HAND A/C BAY BS 663;LBL 8 . BLEED AIR DUCT SUPPORT BRACKET IS CRACKED AT LEFT HAND A/C BAY BS 540LBL 8 .<[01] REMOVED AND REPLACED BLEED AIR DUCT SUPPORT BRACKET BS 540 LBL 8 P/N 212A1116-1 PER SRM 51-40-02-0G-SDR AALA202405035918Pressure Deck · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING SECTION REAP SPAR, RIGHT HAND WHEEL WELL, VERTICAL PRESSURE DECK WEB AT STA 663, BETWEEN RBL 40.00 AND RBL 45.64. REPAIRED WEB PER SRM 57-10-10-2R REPAIR 3 ALTERNATIVE 2.SDR IPXA2024041849724Landing · crackedWHILE ACCOMPLISHING TASK CARD MXP-7633-JIC FOUND 2 EA CRACKED HOLES ON FUEL LANDING AS MARKED ON PART WITH TAPE. ATA. 57-20. INSTALLED 2 EA BUSHING REPAIR AT L/H WING FUEL ACCESS PANEL 536AB REF. MD-11 SRM 57-20-02-2R-5 REPAIR 5.SDR DALA2024041504407Structure · handler errorSHIP 3244 DISC: LT WINGTIP ASSEMBLY DAMAGED FROM IMPACT. C/A: REMOVED LT WINGTIP ASSY PER A320 AMM 57-31-21(WIP 511629). REPLACED LT WINGTIP/ FENCE PER A320 AMM 57-31. OK FOR SERVICE. (LP: 0292122)SDR 2024FA0000458Spar · corrodedFOUND MAJOR INTERGRANULAR CORROSION ON BOTH REAR WING ATTACH POINTS . BLOCK BEARING P/N 0512122. WINGS WERE REMOVED FOR RESTORATION. FURTHER FLIGHT WOULD HAVE LED TO TOTAL WING FAILURE AND WING SEPARATING FROM FUSELAGE. SIMILAR DAMAGE FOUND ON ANOTHER AIRCRAFSDR SWAA2024061073696Panel · corrodedREFUEL PANEL (P15) FACE PLATE HAS SIGN OF CORROSION AROUND FUEL QTY GAUGES.<[01] REMOVED REFUEL PANEL (P15) AS PER B737 AMM TASK 28-21-00-000-801. REMOVED REFUEL QUANTITY INDICATOR AS PER B737 AMM TASK 28-41-61-000-801<BR>REINSTALLED REFUEL QUANTITY INDICATOR SDR HNAA2024050900336Rivet · corroded00119 CORROSION FOUND ON FWD RIB AND RIVET LINE IN RH WHEEL WELL. REMOVED AND REPLACED FWD RIB P/N 145-72022-002 AT RH WHEEL WELL IAW EMB 145 SRM 51-40-02SDR DALA2024041204366Drag Fitting · damagedSHIP 6814 FASTENER #11 FOUND OVERSIZE WHILE WORKING WC 5720-01100-02B RH DRAG FITTING INSP. CORRECTIVE ACTION: BHEC INSPECTED #11 HOLE PER MTC REQUEST REF B757 NDTM 51-00- 16PART 6. NO ITEMS NOTED. CW PRI 616845-14 REV 0. C/W PRI 616845-14 REV 1. CW PRI 616845SDR SWAA2024051472487Winglet · corrodedCORROSION ON WINGLET TIP AT RT WING. PERFORMED PERMANENT REPAIR ON WINGLET TIP AT RT WING IAW SRM 51-10-02-0G-0 AND SRM 57-30-01 REPAIR 6. SCIMITAR TIP CAP REPAIR.
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