JASC 5710
Service difficulty reports · 4,456
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 AALA202503126362Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON #2 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.SDR GTIA2025030638786Skin Panel · corrodedCORROSION AROUND FASTENERS AT INNER REAR TOP SKIN, GEAR RIB ATACHMENT AND REAR FALSE SPAR ON RH WING. RAF-01 3577668-01 GENERATED.-PERFORMED PERMANENT REPAIR LOC ON RH WING TOP SKIN PANEL 2 - GEAR RIB - 5 TO RIB 4 REAR SPAR AND AFT OF FALSE REAR SPAR IAW EA 5SDR IPXA2025032821491Fitting · corrodedCORROSION - FITTING, L/H WING L/E CAVITY FRONT SPAR FITTING OLES 1493.45 (REPAIR). EMOVE DAMAGE FITTING I.A.W. SRM 51-40-02-0G REV.62. PERFORM UPS EO-93174-REQ1 REV.1. INSTALL NEW FITTING I.A.W. SRM 51-40-02-0G REV.62 AND BOEING DWG NO.112U2001 SH 30 REV.D .SDR IPXA2025032610358Cover · crackedRH WING, FAIRING 632BB, CIRCLE PANELS ARE CRACKED (3EA) DOT 103-44. REMOVED AND REPLACED PANELS COVER 632AL 632FL AT R/H WING FAIRING 632BB IAW AMM 27-50-21.SDR IXXA20250426001Fuel Panel · corrodedRIGHT WING LOWER PANEL 631AB IS WORN AND CORRODED. HAECO W.O. 320011 AND NR 34518SDR IPXA2025040806386Seal · damagedRH WING, FAIRING 636AB HASO/B SIDE BULB SEAL DAMAGED. DOT 103-10. INSTALLED NEW I/B SIDE BULB SEAL ON R/H WING FAIRING 636AB IAW A300-600 SRM 51-40-23. P/N A5786412800200 BATCH#0004340329, CR3212-4-03, BATCH#0004217010.SDR IPXA2025032606193Cover · cracked**SDR FILED OPEN**FAULT - Z600, APG, RH WING, FAIRING 635BB HAS CIRCLE PANEL CRACKED AT SCREW HOLE (2EA). DOT 103-08 APPROVEDSDR IPXA2025032593531Support Beam · corrodedCORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1530 ~ OLES 1535 (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93163-REQ1 REV.1.SDR IPXA2025032593591Support Beam · corrodedCORROSION - BEAM, L/H WING L/E LOWER PNL FWD SUPPORT BEAM INNER FACE, OLES 1535 ~ OLES 1540 (REPAIR). REPAIR DAMAGE AREA I.A.W. UPS EO-93161-REQ1 REV.1. ALL PAPERWORK REVIEWED AND C/WSDR IPXA2025031093354Splice Plate · corrodedCORROSION - PLATE, UPPER FACE OF L/H WING L/E LOWER PNL, OLES 1545 (REPLACE). FABRICATE P/N:65B11862-36 PER BOEING DWG NO:65B11862 SH 2 REV. "F";PL REV."N";PSDL REV."-", AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX CH 9.08 REV 10.1 REQUIREMENT . INSTALL FABSDR IXXA20250428003Former · crackedRIGHT WING LEADING EDGE FORMER IS CRACKED AT APPROX OSS 560SDR DALA2025030301626Seal · damagedSHIP 5049 - DIV - TO PHX DUE TO AIRFRAME VIBRATIONS IN MID CABIN. CORRECTIVE ACTION: FOUND DAMAGED SEAL AT UPPER WING PANEL 193AT. RESEALED ALL BELLY FAIRING PANELS. FOUND LH AILERON SERVOS FAILED FREE PLAY CHECKS. MAINTENANCE IN PROGRESS. (7163274)SDR DALA2025030301606Shear Tie · damagedAIRCRAFT 3744, LH WING, SHEAR TIES AT RIBS 14 AND 18 - TRIM, RII; SECTION 02A. INCORRECT INSTALLATION AND DAMAGED FASTENERS ON STRAPS AND SPLICE BTW RIB.15-RIB.18 STA.458.50-STA. 537.5 LH WING. STEP #22. CORRECTIVE ACTION: FASTENERS ON STRAPS AND SPLICE BTW RISDR SWAA2025040299338Vapor Barrier · crackedLEFT HAND BS 663 COMPOSITE VAPOR BARRIER HAS MULTIPLE CRACKS AT LBL 28; WL 164. <[01] L/H VAPOR BARRIER BS663 MULTIPLE CRACKS AT LBL 28 WL 164 WERE REPAIRED IAW SRM 51-70-04-2R-10.SDR SWAA2025040299570Web · crackedCRACK VAPOR BARRIER WEB LOCATED BS663.75 AND LBL 40 AT MAIN WHEEL WELL COMPARTMENT 2025-167480 <[01]. TOOL USED CALIPER P/N 500-197-30 S/N A18135086 DUE DATE 21 JUN 25; [02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 22 FEB 26; [03] ON STEP 12SDR CALA2025022802528Access Panel · missingPDA 2 LEFT WING #5 SLAT, ANTI-ICE DUCT ACCESS PANEL MISSING ON SERVICE CHECK WALKAROUND. UPDATE TO INCLUDE PANEL SIZE AND PHOTOS. PANEL IS APPROX 5X12.5 INCHES, FALLING INTO CATEGORY 2 PDA PER GMM 02-30-95.SDR FDEA202502250277Skin · crackedRIGHT WING LEADING EDGE, SLAT ASSEMBLY NUMBER 5 UNDERSIDE COVE PANEL INBOARD EDGE FOUND WITH CRACKLINE FROM RIVETED HOLE, AT STATION XOS 660.537. RIGHT WING LEADING EDGE, SLAT ASSEMBLY NUMBER 5 UNDERSIDE COVE PANEL INBOARD EDGE AT STATION XOS 660.537 REPAISDR CALA2025021800376Strap · corrodedREMOVED AND INSTALLED NEW R/W FRONT SPAR LOWER STRAP INBD OF PYLON AT IFSS 155 AS PER SRM 51-40-02-0G-0,DWG 112A4401.REF AAR N/R9935224.WORK ACCOMPLISHED BY V945157.SDR AALA202503267971Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING #1 AILERON HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED SUPPORT FRAME PER AMM 57-51-31.SDR SWAA2025032095952Panel · crackedPANEL 621YB CRACKED ON O/B FWD. END <[01] PANEL 621YB WITH CRACK ON O/B FWD END WAS REPAIRED PER SRM 51-70-05-2R-6.SDR DXTA2025021702363Wing · damagedLH WINGTIP HAS SUSTAINED DAMAGE FROM CONTACT WITH A SCISSOR LIFT DURING A REPO INTO THE HANGAR. THE LINE PERSONNEL TOWED THE AIRCRAFT INTO THE HANGAR FOR MX. THE AIRCRAFT ROLLED BACKWARDS AFTER BOTH MAINS BEING CHOCKED BEFORE THE TUG WAS DISCONNECTED. THE HANGSDR KCSA202502121010Beam · crackedLW FIXED TRAILING EDGE BEAM LWR CHORD DAMAGED INBD OF #4 FLAP TRACK FAIRING AT APPROX WBL 255SDR DALA2025021201089Fitting · damagedPERFORM COLDWORK ON INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING. SUMMARY OF NRC 00924: INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING WAS REPAIRED PER PRI 621176-14 REV 10 AND ERA 621176-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. ALSO FAIRING WAS RESDR VNAA202502110028Canister · crackedIN REFERENCE TO JOB CARD TRFKE000WKWW WAS DETECTED CRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV - -SDR VNAA202502110029Canister · crackedCRACK IN CANISTER WELDED NO.3 IN, STA. WS148 OF INTERNAL LH MAIN FUEL TANK. REPAIRED PER REO 670-57-42-577 REV - -SDR SWAA2025031093738Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 422 AT LT WING 2025-110659<[01] REPLACED CORRUGATED PLATE LOCATED ORSS 422 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 115A3700 REV -<BR>SEEE INDISDR IPXA2025021411890Landing · damagedFAULT: Z500-STR-L/WING UNDER KRUEGER L/E PANEL AFT AREA HAS SEVERAL NICKS (9EA MARKED IN RED). DOT 34-022. REMOVED FLANGE (LANDING) FROM LH WING KRUEGER WITH SEVERAL NICKS 9(EA) AND REPLACED WITH A NEW ONE P/N A5724200920000, BATCH 0004365682 USING FASTENERS PSDR SWAA2025031093555Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS451 AT RT WING 2025-110633<[01] REPLACED CORRUGATED PLATE AND FASTENERS TRAILING EDGE LOCATED ORSS451 AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 115A3700; SHEET 48; REV-; SRM 51-10-02 ITEM 9.;[02] REPLACED CORSDR SWAA2025021092660Plate · crackedCRACK CORRUGATED PLATE AT OFS 353 BTW SPOILER 3 AND 4 LT WING 2024-780547<[01] REPLACED CURRUGATED PLATE LOC OFS 353 BTW SPOILER 3 AND 4 LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 STEP 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED<BR><BR>SEE INDSDR SWAA2025030592189Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT LT WING 2025-94291<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT LT WING AND FASTENER IAW B737-700 #DWG:115A2781 SHEET: 2 REV: B AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[SDR SWAA2025030592190Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT RT WING 2025-94294<[01] REPLACED CORRUGATED PLATE TRAILING EDGE AT LEVEL IRSS 215 AT RT WING AND FASTENER IAW B737-700 #DWG:115A2781 SHEET: 2 REV: B AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[SDR AALA202502032683Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SLAT TRACK 5 FWD BOLT ON RH WING, CORROSION MEASURES L:0.493IN, W:0.189IN, D:0.007IN. MAINTENANCE REPLACED SLAT TRACK 5 FWD BOLT ON RH WING IAW AMM 27-84-64-400-002-A,SDR CALA2025013000239Structure · damagedRII INSPECTION REQUIRED RIGHT WING LOWER CHORD DAMAGED AT STRIKER PLATE LOCATION STA 540 RBL 40.875 OUT OF LIMITS . VERIFIED REPAIR MATERIAL REF SRM 57-10-13-2R-3 TABLE 201. OK TO REF: SRM 57-10-13-2R-3 STEP 4 F - ACCOMPLISHED HFEC 737 NDT PART VERIFIED FLAP PSDR SWAA2025022690483Winglet · corrodedDOT#26 A-043 LH WINGLET CORRODED ON AFT OTBD EDGE 10' FROM TOP EDGE<[01] AUDIT C/WSDR DALA2025012900696Pressure Panel · cracked(LOG 0780115) CRACK ON REAR SPAR VERTICAL PRESSURE DECK RH PERFORM PERMANENT REPAIR. PERMANENT REPAIR ON REAR SPAR VERTICAL PRESSURE DECK RH WAS PERFORMED PER B737-800 SRM 57-10-10-2R, PROCEDURE 3, REPAIR 3.SDR DXTA2025012802101Winglet · ground damageUPON WALK-AROUND AND GETTING READY TO LEAVE. MAIN GEAR WERE ALREADY UNCHOCKED. FUELER HAD FINISH FUELING. I PROCEEDED TO UNCHOCK THE NOSE GEAR. ALL WAS FINE UNTIL I LOOKED BACK AND NOTICED THE PLANE ROLLING FORWARD. I ATTEMPTED TO HOP ON THE AIRPLANE TO STOP ISDR SWIA202503260121Landing · corrodedLH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 540EB HAS AN AREA OF MINOR CORROSION ON THE AFT EDGE MID POINT OF LANDING, APPROX 8" IN TOTAL. (C-CHECK RO 03/25/2024) (FILED CLOSED) BLENDED CORRODED AREA OF LH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 54SDR IPXA2025021652064Retainer · corrodedCORROSION - RETAINER , R/H WING LOWER T/E FIX PANEL INTERNAL SURFACE INBD FWD CORNER , WBL 128 (AGING A/C INSPECTION) (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.102 AND BOEING DWG NO.65B11631 SH2 REV.J. ALL PAPERWORK REVIEWED AND C/WSDR AALA202503122830Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #2 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.SDR AALA202503126787Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #3 HINGE SUPPORT FRAME HAS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.SDR AALA202503067883Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #5 HINGE SUPPORT FRAME AS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.SDR AALA202503064557Support Frame · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT WING AILERON #4 HINGE SUPPORT FRAME AS EXCESSIVE PLAY. REPLACED HINGE SUPPORT FRAME PER AMM 57-51-31.SDR IPXA2025021289146Flange · damagedDAMAGE FOUND ON LH FR47 HORIZONTAL JUNCTION (HOLES F AND S). ACCOMPLISH THE REPAIR PER EA 300-5710-27-A3766 REV. -.SDR IPXA2025012689498Web · crackedWEB O/B OF LH KRUEGER FLAP P/N A5724199320200 CRACKED. DOT# 110-136 JP-110. INSTALLED WEB/ANGEL USING FASTNERS P/N MS20470AD5-5 BATCH #004237215 AND CR2313-5-05 BATCH # 0004287420 IAW SRM 57-41-11 AND SRM 51-40-21.SDR SWAA2025022085662Winglet · corrodedDOT#42 A-043 RH WINGLET HAS CORROSION ON LOWER OTBD T/E 18' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 57-30-01-1A-2-APB-AP37.1-0632-A01611 (PERMANENT (NON-DENT DAMAGE TYPES)-WINGLETS)];[02] VERIFIED STEP 1<BR>AUDIT CWSDR SWAA2025022085661Winglet · corrodedDOT#43 A-043 RH WINGLET HAS CORROSION ON UPPER INBD T/E 42' FROM BOTTOM EDGE<[01] 04 - REPAIRED PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)] AND IAW APB 57-30-01 FIGURE 102 (D);[02] 04 - REPAIRED PER [SRM 5SDR IPXA2025020957045Bracket · brokenLH WING, CENTER FLAP, O/B EDGE HAS BRACKET BROKEN. DOT 103-62. REMOVERD AND REPLACE BRACKET AT L/H WING CENTER FLAP. FABRICATED BRACKET:P/N 2024-T3 0.32B BATCH 0004247650 P/N C3213-5-08 BATCH: 00044268033 IAW A300-600 SRM 51-40-21.SDR IPXA2025011351200Panel · crackedRT WING #8 SLAT OUTBD TRACK GAP PANEL IS CRACKED. DOT 8-010. RH SLAT#8 P/N 114N4004-172SP SERIAL:A2-0388 , INSTALLED IAW AMM TASK 27-81-02-424-021.SDR CALA2025011000074Winglet · crackedLH WINGLET CRACK . REMOVED LEFT WINGLET LOWER BLADE PER AMM TASK 57-31-21-000-80. INSTALLED 4 COUNTERSUNK RIVETS IN NEW SCIMATAR WINGLET IAW SRM 51-40-02. INSTALLED NEW LH WINGLET PER AMM TASK 57-31-21-400-802. PLANE RESTORED TO ORIGINAL CONFIGURATION.SDR DALA2025010600078Plate · corrodedSHIP 3136 CORROSION TRAILING EDGE PLATE LOCATED ON WING TIP BRAKE BTW RIB 15 TO RIB 16 ON LH WING. CORRECTIVE ACTION: REPLACED PLATE (TEE PIECE) LOC. WING TIP BRAKE AREA ON LH WING AS PER A319 SRM 51-42-11. (0747361)
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