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 SWAA2025111026076Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE ORSS 261 AT LT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 115A2001 SHEET: 29 REV-.SDR SWAA2025110725800Plate · crackedCRACK RT WING TE CORRUGATED PLATE TRAILING EDGE IRSS 215. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 115A2001, SHEET 30, REV A. . CRACK LENGTH WAS 0.867 INCH.SDR SWAA2025110726075Plate · crackedCRACKED LT WING T/E CORRUGATED PLATE, IRSS 215. REPLACED THE CORRUGATED PLATE IAW SRM 51-10-02, ITEM 9, AND DWG 115A2001, SHEET 29, REV -.SDR IPXA2025111846321Support Beam · corrodedLEFT WING OTBD FLAP INBD HINGE STRUCTURE FAIRING 535 DL AREA UPPER SUPPORT BEAM HAS EVIDENCE OF CORROSION, INSTALLED FAIRING SUPPORT BEAM AND 3EA ANGLES IN LH WING OUTBOARD FLAP I/B HINGE REF EA# 011-5700-01-B0623 REV P1 STEP 9, MD-11 SRM 51-33-01-0G-0 AND SSDR SWAA2025112025725Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT RT WING. IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0. MEASUREMENT OF CRACK IS: 0.215 INCHES.SDR SWAA2025112025727Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-40-02 SRM 51-10-02, ITEM 9 AND DWG 115A2001 SHEET 30 REV A.SDR IPXA2025110149647Plate · crackedLEFT WING CENTER FLAP, METALIC PLATE ON TOP SURFACE LE SIDE HAS GOUGING AND SHOWS EVIDENCE OF A CRACK. REMOVED AND REMPLACED METALIC PLATE ON TOP SURFACE LE SIDE IAW SRM 51-40-21.SDR CALA2025102110339Winglet · ground damageON TAXI IN RIGHT WING HIT ANOTHER AIRCRAFT BEGAN REMOVAL OF RIGHT WINGLET REF AMM 57-21-21-000-801. UP TO STEP 2. H(3) ADD EMP:U425084 CONTINUED FROM STEP 2. H (4) AND REMOVED RH WINGTIP REF AMM 57-21-21-000-801 ADD EMP:U397485,438241 SDR INFO UPDATE ADD EMP:SDR VNAA20251014018Landing · corrodedTHE LANDING FOR PANEL 642CT IS CORRODED. REPAIRED LANDING IAW MHIRJ REO 670-57-21-1032 REV-- DATED 2025-1-13SDR VNAA20251014016Landing · corrodedTHE LANDINGS FOR PANEL 542ET, 542DT, AND 542CT ARE CORRODED. REPAIRED LANDINGS IAW MHIRJ REO 670-57-21-1030 REVSDR ABXA20251014268Beam · corrodedTHIS AIRCRAFT IS CURRENTLY UNDERGOING AN A-CHK IN CVG, AND MAINTENANCE FOUND THE RIGHT WING FIXED L/E NOSE BEAM AT OSS 500 TO BE BADLY CORRODED. THE CORROSION WAS REMOVED BY BLENDING, AND THE BLEND WAS BEYOND THE ALLOWABLE LIMIT GIVEN IN REF /A/. THERE IS NO RSDR SWI2025F01524Rib · crackedLEFT BATTERU RIB CAP ANGLE CRACKED AT W/S 48.30 (FILED CLOSED)REMOVE AND REPLACED LH BATT RIB CAP ANGLE AT W/S 48.30 REF DWG600-10389 REV E AND CRJ200 SRM 51-42-21.COMPLIED WITH 51-900-1003-SKYSDR IPXA2025110188289Deflector · crackedFAULT - STR, Z500, PANEL RACK, LH WING, DEFLECTOR PANEL 572LB HAS GOUGE W/CRACK. DOT 103-1524. PROFILE WAS INSTALLED IAW A300/600 SRM 51-40-21 REVIEWEDSDR SWAA2025100922969Fastener · looseNUMBER 6 TRAILING EDGE AFT FLAP FAIRING HAS 3 LOOSE AND/OR PULLED THRU FASTENERS FWD OF PREVIOUS REPAIR. REPAIRED NR 6 INBD TE FLAP FAIRING ATTACH FASTENER HOLES IAW SRM 57-53-70-2R-2, ALTERNATIVE 1.SDR IPXA2025102838770Fitting · crackedCRACK FOUND AT OPEN HOLE OF LT WING FR 40 LOWER RADIUS, CRACK NOTED AT FIRST LAYER FWD LAYER, 6 O'CLOCK POSITION, CRACK DEPTH FROM FWD TO AFT AT 5MM. INSTALLED REINFORCING SKIN AND STIFFENER UNDER IAW SRM 51-40-21 .SDR VNAA202510020003Helicoil · missingRH WING JACK POINT MISSING HELI-COIL AND NYLON PLUG. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 670-57-22-155, REV -- DATED 2025-09-22 - TEMPORARY DISPOSITION FOR REMAINING THREADS AFTER REAMING RH WING JACKING FITTING BORE (DEVIATION TO GENERIC REO 670-57-22-SDR EE4Y2025092723237Reinforcement · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-ZL-471-01-4-001, LH WING BOTTOM SKIN LOWER SURFACE AFT SECTION AREA SKIN AT RIB 8 WITH CORROSION WAS FOUND. AIRBUS WAS CONTACTED FOR REPAIR INSTRUCTIONS. THE REPAIR INSTRUCTIONS WERE RECEIVED AND PERFORMED PERMASDR VNAA202511270003Canister · crackedCRACK IN CANISTER WELDED NO.3, ON WS148.019 OF INTERNAL RH MAIN FUEL TANK. CANISTER WELDED NO.3, ON WS148.019 OF INTERNAL RH MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV. --SDR SWAA2025103118371Beam · crackedCRACKED BEAM ORSS 297 TRAILING EDGE AT LT WING. REPLACED THE BEAM ORSS 297 TRAILING EDGE AT LT WING IAW SRM 51-10-01 ITEM 9; SRM 51-40-02 AND DWG: 115A3700, SHEET 30, REV - .MEASUREMENT OF CRACK: 0.9390 IN.SDR UATA2025100605301Fairing · crackedFOUND CRACK IN RH WING TO FUSELAGE FAIRING AT FRAME F5. (SEE AOT-C212-53-0001 FOR DETAILS). REPAIRED CRACK DAMAGE AND REINFORCED F5 RH BY INSTALLATION OF SB KIT SB212530055K01. SEE 337 DATED 09/25/2025. FOR FURTHER DETAILS.SDR DALA2025092607006Bonding Plate · corrodedCORRODED STATIC DISCHARGER PLATE-BONDING FLAP TRACK FAIRING 532CB ON LT WING. COMPLIED WITH ER/A 622998-14TR. (1217688).SDR DALA2025092607005Bonding Plate · corrodedCORRODED BONDING PLATE FLAP TRACK FAIRING 631CB ON RT WING. COMPLIED WITH ER/A 622998-14TR. (1217597).SDR DALA2025092607004Bonding Plate · corrodedCORRODED FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. COMPLIED WITH ER/A 622998-14TR. (1217586).SDR VNAA202510300002Fitting · damagedREPAIR DAMAGED JACKING PAD HELICOIL INSERT LEFT, JACK FITTING LT WING WAS REPLACED PER SRM 51-42-21-001-001-A01.SDR REXA2026052600622Fitting · wornWEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING). WEAR ON FLAP FITTING AND PLATE SUPPORT OF FLAP STUB FAIRING 171DL AND 172DR AT RH/LH WING TRAILING EDGE (ROOT WING) WERE FOUND OUT LIMITS THERSDR SWAA2025092416652Winglet · corrodedLEFT UPPER WINGLET ASSEMBLY MISSING PAINT IS SHOWING SIGNS OF CORROSION APPROXIMATELY 0.5 INCHES WIDE BY 2.0 INCHES IN LENGTH. EVALUATED IAW SRM 57-31-00 AP37.1-0632. REMOVED CORROSION IAW SRM 51-10-02. DAMAGE DIMENSIONS ARE AS FOLLOWS; LENGTH: 2.60 INCHESDR SWIA2025091875385Hinge Fitting · gougedLEFT WING #5 FLAP HINGE BOX AFT IB ATTACHMENT FITTING LUG IS GOUGED. BLENDED GOUGE ON LT WING NR 5 FLAP HINGE BOX AFT IB ATTACHMENT FITTING LUG IN REFERENCE TO SRM 51-12-00. PERFORMED EDDY CURRENT IN REFERENCE TO NDTM 51-20-006 AND FOUND REWORKED AREA TO BE CSDR UIEA2025091001175Strut · brokenRHE ILES 440 APPROX L/E CAVITY DIAGONAL STRUT & UPPER ATTACH FITTING FOUND BROKEN. RHE ILES 440 APPROX L/E CAVITY DIAGONAL STRUT & UPPER ATTACH FITTING REPAIRED IAW SRM 57-41-09-2R-2 REPAIR 2, FIG 203 REV 46. . NO FURTHER DEFECTS NOTED.SDR KCSA202509171161Stiffener · crackedAILERON CAVITY I/B STRUCTURE 20 IN. FWD OF HINGE POINT VERTICAL STIFFENER CRACKED AT LOWER EDGESDR CALA2025091709004Wing · damagedLEFT WING TIP STRUCK VEHICLE GROUND CREW AND AUTOMATIC PARK CLEA RED PICS INCLUDED. PIC. REMOVED LEFT WINGLET WING TIP IAW 57-31-21-000-801, REMOVED WINGLET LOWER BLADE IN REF TO AMM 57-31-21-000-802 INSTALLED NEW LOWER BLADE TO ORIGINAL UPPER BLADE REF AMM 57SDR FDEA202509161709Former · crackedRIGHT WING - LEADING EDGE COMPARTMENT LOWER FORMER AT STATION XOS 559 FOUND CRACK ABOUT 0.4 INCHES. RIGHT WING LEADING EDGE COMPARTMENT LOWER CRACKED FORMER AT STATION XOS 559 REMOVED AS PER MD-11 SRM 51-35-01-0G AND 51-33-01-0G. FABRICATED FORMER AS PER SDR KCSA202509161159Beam · corrodedLH WING TE FIXED TRAILING EDGE BEAM UPPER CHORD @ APPROX WBL 340 CORRODEDSDR DALA2025091506793Shim · migratedRIGHT WING L/E INBD DRAG FITTING HAS SHIM MIGRATION AT LOCATION (1, A) FIGURE 4, AT AFT I/B SIDE OF FITTING PER AD CARD #5720-01100-02B. REPLACED RIGHT WING LE INBD DRAG FITTING SHIM IAW ERA 628611-14AD. (LP 1198810)SDR SWAA2025102114316Strap · corrodedCORROSION ON STRAP LOCATED OFSS405 LEADING EDGE AT RT WING . PERFORMED REPAIR ON BETWEEN OSS 163.95 TO OSS 227.95 AT RT WING IAW EA 25-157-02564-WIP1 ; EA 25-157-02564-WIP2 ; EA 25-157-02564-WIP3 ;EA 25-157-02564 B737-800 SRM 51-40-02; DWG 112A4402 SHEET 40; SDR HNAA2025102100709Structure · corrodedF069855 RH MLG BAY LOWER SKIN FWD OF MAIN SIDE BRACE AT SPAR II HAS CORROSION, BLENDED AREA ON RH MLG BAY. DAMAGE ACCEPTED AS IS IAW ETD2025-145-928499 AND PIEDMONT EO1-05-25-0363.SDR HNAA2025102100708Structure · corrodedF069854 LH MLG BAY LOWER SKIN FWD OF MAIN SIDE BRACE AT SPAR II INTERNAL HAS CORRODED AREA. RAR LH MLG BAY LOWER SKIN FWD OF MAIN SIDE BRACE AT SPAR II IAW EMB 145 SRM 51-40-02.SDR JJBA20251111046Strap · corrodedLEFT WING LOWER SPAR STRAP CORRODED FROM RIB 19 TO RIB 25. REMOVED CORROSION ON LH WING LOWER SPAR STRAP FROM RIB 19 TO RIB 25 BY BLENDINGSDR JJBA20251111045Strap · corrodedLH WING UPPER SPAR STRAP CORRODED FROM RIB 19 TO RIB 25. REMOVED CORROSION ON LH WING UPPER SPAR STRAP FROM RIB 19 TO RIB 25 BY BLENDINGSDR SWAA2025100613337Plate · crackedLEFT WING OTBD OF ACCESS PANEL 551DB HAS CRACKED WIGGLE PLATE. REMOVED AND REPLACED WIGGLE PLATE OTBD OF PANEL 551DB IAW SRM 51-40-02-0G-0 AND DWG.115A2001, REV-.SDR SWAA2025100613339Plate · crackedRIGHT WING OTBD OF ACCESS PANEL 651DB HAS CRACKED WIGGLE PLATE. REMOVED AND REPLACED WIGGLE PLATE OTBD OF PANEL 651DB IAW SRM 51-40-02-0G-0 AND DWG 115A2001, REV-.SDR ASAA2025090961323Angle · crackedCENTER WING REAR SPAR VAPOR WEB, LH PACK BAY AFT VAPOR BARRIER SKATE ANGLE CRACKED BS 663.75 LBL +9. GROUNDED - YES. REPAIRED REAR VAPOR WEB SUPPORT ANGLE IAW B737-900 SRM 57-10-10-2R-5 REPAIR 5 REV 56-10 JUL 2025. CAP SEALED IAW B737-900 SRM 57-10-10-2R-5. ELSDR SWAA2025100213026Fairing · crackedCRACKED FAIRING 644BB AT RT WING. PERFORMED PERMANENT REPAIR ON FAIRING PANEL 644BB AT RT WING IAW EA 25-157-02530-WIP1 AND STEPS ARE DOCUMENTED ON FAULT TTG8Q0157YT6.SDR CALA2025091108773Support Beam · wornPERFORM PERMANENT REPAIR AT LT WING FIXED TE SUPPORT BEAM IAW SRM 57-51-02-2R-1. REPAIRED LT WING DEFLECTION CONTROL RIB & SUPPORT BEAM IAW SRM 57-51-02-2R-1 OF LT WING FIXED T/E, NDT INSP PERFORMED IAW NDT PART 6 51-00-00 PROCEDURE 16 & PROCEDURE 23 AT LT WSDR SWIA2025091000009Winglet · ground damageLT WINGLET RAMP DAMAGE - THE T/E CLOSING RIB HAS MISSING EDGE MATERIAL, DENT AND CRACK DAMAGE NEAR 1-OFF NUTPLATE LOCATION NEAR WS 398.00 T/E (FLIGHT 3898 - FILED OPEN)SDR IXXA2025091801Former · crackedRH WING LE 3 NOSE FORMERS FOUND CRACKED AT OSS446, OSS499 AND OSS550. P/N 114T2512U14, 114T2511U14, AND 114T2202-22.SDR SWAA2025100311315Rail · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 449 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED OFSS 449 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B373-800 SRM 51-40-02 AND 51-10-02 APPLIED PROTECTIVE TREATMENT ON NEW FASDR SWAA2025100311316Rail · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 332 INTERNAL CAVITY LEADING EDGE AT LT WING . REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED OFSS 332 INTERNAL CAVITY LEADING EDGE AT LT WING IAW B373-800 SRM 51-40-02 AND 51-10-02 ITEM 9. APPLIED PROTECTIVE TREATMENT OSDR SWAA2025100311322Rail · crackedCRACK ON RAIL NUT-PLATE LOCATED OFSS 604 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED ON OFSS 604 AT INTERNAL CAVITY OF LEADING EDGE OF LT WING IAW B737-800 SRM 51-40-02-0G-0 AND DRAWING 112A4402; SHEET: 41; REV: A.SDR SWAA2025100311331Rail · corrodedCORROSION ON RAIL NUT-PLATE LOCATED OFSS 308 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE AND FASTENERS LOCATED OFSS 308 INTERNAL CAVITY LEADING EDGE AT LT WING IAW SRM 51-40-02 AND DWG 112A4402 SHEET 40 REV A.SDR SWAA2025092611531Beam · elongatedELONGATED HOLE ON BEAM LOCATED ORSS281 TRAILING EDGE AT LT WING 2025-549032<[01] REAMED HOLE ON BEAM LOCATED ORSS281 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-05-0G-0 FIGURE 4 SHEET 3 TABLE B.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] CERTIFIED ACTION 1; CO
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