JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 FDEA201003100733Skin · corrodedCORROSION - LT WING STA XORS279 AT UPPER SURFACE DOUBLER AREA. REPAIRED IAW EA NR 1-5730-137933, THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109.SDR DALA1011880661Skin · damagedWHILE PERFORMING THE TRIM OUT OF THE UPPER SKIN PANEL AT WS 711.50 ON LT AND RT WING FOUND THAT THE TRIM LINE NEEDS TO DEVIATE FROM THE ORIGINAL STRAIGHT TRIM LINE IAW APB DWG 757-3500 TO ALLOW EDGE DISTANCE ON EXISTING FASTERNERS BE MAINTAINED COMMON TO THE FSDR TRBACPCP2010017Skin · corrodedAREA OF CORROSION WAS FOUND AT RT WING LOWER SKIN AROUND JACK POINT AT RIB 10. CORROSION WAS BLENDED OUT IAW SRM 51-21-42 AND NDT ASSURING THERE IS NOT MORE CORROSION. CORROSION DOES NOT REACH ANY FASTENER SEATING, FASTENERS WERE NOT REMOVED. REF SRI NR DO/SDR FDEA201003090787Access Panel · corrodedLT WING FUEL TANK PANEL NR 543BB LOWER SURFACE SKIN HAS CORROSION. FUEL TANK PANEL NR 543BB LOWER SKIN REPAIRED IAW EA F-2810-135836 (FUEL TANK ACCESS COVER CORROSION DAMAGE REWORK). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201003080678Panel · damagedLT WING LOWER T/E HINGE PANEL AFT OF THE NR 2 TANK SUMP DRAIN IS DENTED. (WING ROOT) ROOT) REMOVED PANEL IAW SRM 51-31-01, VOL II. EVALUATE 2 EA OUTER SKIN DENTS. THE FWD DENT MEASURES 0.033" DEEP , THE AFT DENT IS 0.043" DEEP. THE DENTS ARE LESS THAN 0.0SDR FDEA201003080677Panel · dentedLT WING LOWER T/E PANEL AT THE NR 2 TANK SUMP DRAIN IS DENTED. (WING ROOT) EVALUATED OUTER SKIN DENT AT THE MARKED LOCATION AND FOUND TO MEASURE 0.043" DEEP WITH NO DELAMINATION NOTED AT THIS TIME USING TIMCO DIGITAL DEPTH GAUGE T8563A AND IS WITHIN ALLOWABLSDR DALA105145649Skin · delaminatedDURING "L" CHECK FOUND LT WING FIXED LEADING EDGE UPPER SURFACE SKIN IS DELAMINATED AT OSS 312. REPAIRED PER ERA 480019-14.SDR UALA2010030800808Panel · leakingRUNNING FUEL LEAK FROM FLAME ARRESTER AT RIGHT WING INBOARD OF PYLON NR 2 ENGINE. PANEL 632AB CENTRE TANK DRY BAY ACCESS PANEL AT RIGHT WING REMOVED FOR ACCESS TO LEAK IN DRY BAY. PANEL IS LOCATED INBOARD OF NO 2 ENGINE PYLON. EALED DRY BAY BULKHEAD FITTING.SDR FDEA201003070664Skin · misrepairedEXISTING REPAIR - RT WING L/E AT SLAT TRACK NR 6 UPPER SKIN REPAIR PATCH FOUND. EXISTING REPAIR AT RT WING L/E SLAT TRACK NR 6 UPPER SKIN EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTING PATCH REPAIR REMOVED IAW SRM 51-35-01,SDR FDEA201003070656Skin · misrepairedEXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 226 LOWER SEGMENT AREA. EXISTING REPAIR AT LT WING INBD FLAP UPPER SKIN AT XIFH 226 LOWER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISDR FDEA201003070655Skin · misrepairedEXISTING REPAIR - LT WING INBD FLAP REPAIR PATCH FOUND AT UPPER SKIN AT XIFH 149 UPPER SEGMENT AREA. EXISTING REPAIR AT LT WING INBD FLAP UPPER SKIN AT XIFH 149 UPPER SEGMENT AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. EXISTINGSDR FDEA201003070654Skin · misrepairedEXISTING REPAIR - LT WING NR3 SLAT REPAIR PATCH (2 EACH) FOUND ON INBD OUTER SKIN AREA. EXISTING REPAIR (2 EACH) AT LT WING NR 3 SLAT ON INBD OUTER SKIN AREA EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW ANY SRM REPAIR SCHEME. EXISTING REPAIR PATCH (2SDR FDEA201003070670Skin · crackedCRACK FOUND ON NR 34 FASTERNER HOLE ON RIGHT HAND SIDE OUTER WING LOWER SKIN PANEL ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND XORS 713.6. REPAIR CARRIED OUT AS PER E.A. 1-5710-137915, REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REVISION 109.SDR IXXA10SMN033SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND LT WING INBD FLAP AFT UPPER SURFACE SKIN HAS SCRATCHES AND DENTS AT STA XW 2.000 - 91.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARSDR IXXA10SMN032SSkin · dentedDURING ROUTINE C-CHECK INSP FOUND RT WING INBD FLAP FWD UPPER SURFACE SKIN HAS DENTS AT STA XW 104.000 - 122.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLESDR IXXA10SMN031SSkin · misrepairedDURING C-CHECK INSP, FOUND RT WING OTBD FLAP AFT LOWER HAS IMPROPER REPAIR AT STA XF 375.000 - 415.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH SDR UALA2010030800806Panel · leakingFUEL LEAK UNDER RT INBD WING. 12 FOOT SEEP AT SEAM WITH WIDE AREA OF DRIPS. LOCATED LEAK EXTERNALLY AND INTERNALLY. REMOVED SEALANT EXTERNALLY, CLEANED AND RESEALED WITH A1-2 AND B1-2 AT 1400 HRS. NEEDS TO RESEAL INTERNALLY. RESEALED INTERNALLY WITH A1-2 AND SDR DALA1012010661Skin · chafedRT WING LOWER SURFACE WS 303 AREA HAS CHAFE WEAR (JUST FWD OF AFT SKATE ANGLE) COMPLIED WITH ER/A 482150-14 REV ORIGINAL, REF NON ROUTINE CARD 159393. (DL757101371)SDR IPXA10M58899Skin · chafedINSPECTION TYPE:2C, LT WING FIXED L/E STA XOS 464 TELESCOPING DUCT CUT OUT REPAIR DOUBLER CHAFED DEEP BOTH SIDES. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED FILLER AND DOUBER IAW EA 011-5730-A2220 AND EO MD11-5750-31916-C.SDR UALA2010030500773Seal · leakingLEFT WING OTBD OF NR 1 ENG, PANEL LEAKING FUEL. REMOVED FLAP TRACK FAIRING FOR ACCESS TO REPLACE FUEL PLATE AND SEAL. HAVE ALL NEEDED PARTS. REPLACING PLATE NOW. REPLACED FUEL ACCESS PANEL.SDR FDEA201003040629Skin · noneEXISTING REPAIR - REPAIR DOUBLER FOUND ON LT WING L/E UPPER SKIN AT XIS 247. EXISTING REPAIR - AT LT WING L/E UPPER SKIN STA XIS 247 EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-40-02 FIGURE 201, REPAIR 8 REV 42. CHAFED DOUBLER REMOVED IAW SRM 51-31SDR CALA2010030800069Skin · damagedDAMAGE TO RT WING I/B LEADING EDGE ABOVE STALL STRIP RE-INSPECTED AND FOUND TO BE OUT OF LIMITS AT 4.0LX1.5WX0.215D PER SRM 57-41-01 FIG 107 SHEET 3. DMG L/P 4230587. REWORK ON DENT COMPLIED WITH REF ECRA 5731-01362. 8418FOR.SDR GUUA93357030210BAccess Panel · debondedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED RIGHT WING FUEL ACCESS PANEL 632 AT INNER RING DEBONDED. FABRICATED AND INSTALLED RING DOUBLER REPAIR AT ACCESS PANEL 632AT.SDR GUUA93357030210AAccess Panel · debondedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT WING FUEL ACCESS PANEL 531DB INTERNAL RING DEBONDED. FABRICATED AND INSTALLED RING DOUBLERS AT WING FUEL ACCESS PANEL 531DB.SDR IPXA10M58847Skin · crackedINSPECTION TYPE:2C, RT WING FUEL DOOR ACCESS CUT OUT CRACKED AT XOS 611.293 REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-40-02 REPAIR 7 FIG. 201.SDR IPXA10M58811Doubler · crackedINSPECTION TYPE:2C, RT L/E BEADED DOUBLER XOS 672 CRACKED IN 4 SPOTS REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS, DOUBLER, AND ANGLES IAW SRM 57-40-02 REPAIR 9, FIG. 203.SDR IPXA10M58810Doubler · crackedINSPECTION TYPE:2C, RT L/E BEADED DOUBLER CRACKED XOS 793. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES SRM 57-40-02 REPAIR 9, FIG 209.SDR HALA2010030100082Skin · damagedFOUND DAMAGE TO RT WING OTBD AILERON PANEL NR 661NB (3) CORNER SCREWS PULLED THRU DUE TO HAMMER FOUND INSIDE PANEL AREA (DAILY INSP REQ). OK TO CONTINUE IAW M105 NR 589041. CORNER SCREWS PULLED THRU DUE TO HAMMER FOUND INSIDE PNL AREA (DAILY INSP REQ). PICKSDR FDEA201003010565Panel · crackedLT WING UPPER L/E PANEL 525 AT INNER BEADED DOUBLER IS CRACKED OUT. PANEL 525 AT REQUIRES A CRACKED SKIN REPAIR ON THE INTERIOR SKIN OF THE PANEL. REMOVED DAMAGE IAW SRM 57-00-01; FIG 1-A; VOL I. DISCREPANT AREA REQUIRES SRM REPAIR. ALODINED & PRIMED EDGSDR FDEA201003010548Skin · crackedLT WING FIXED L/E SKIN IS CRACKED AT THE NR 4 SLAT INBD TRACK CUTOUT. REMOVED DAMAGED SKIN BY CUTOUT IAW SRM 57-10-00, FIG 68, VOL I. FABRICATED REPAIR FILLER AND DOUBLER IAW SRM 57-10-00, FIG 68, VOL I. ALODINED AND PRIMED IAW SRM 51-21-01, VOL II. INSTSDR 2010FA0000191Access Panel · corrodedTHE CTR WING FUEL CELL ACCESS WAS FOUND TO HAVE CORROSION ON THE FLANGE. THIS FLANGE IS HIDDEN BY THE FUEL CELL COVER AND THE DAMAGE IS NOT READILY VISIBLE DURING NORMAL MX. THIS AREA HAS A HISTORY OF WATER/ CONDENSATION INGRESS AND SHOULD BE THOROUGHLY INSPSDR MASA2010022700163Winglet · damagedLEFT WINGLET DAMAGED DUE TO AC STRIKE. AC WILL BE FERRIED TO PHX FOR COMPLETE REPAIR. WINGLET WAS REPAIRED AND AC RELEASED FOR SERVICE ON 3/1/2010.SDR 2010FA0000373Skin · damaged(KADY) REPLACED TIME LIMITED REPAIR WITH PERMANENT REPAIR - LT WING L/E SKIN.SDR 2010FA0000365Skin · damaged(KADY) REPLACE TIME LIMITED REPAIR WITH PERMANENT REPAIR - LT WING L/E SKIN.SDR TRBACPCP2010013Skin · corrodedAN AREA OF CORROSION WAS FOUND AT RT WING LOWER SKIN DRAIN VALVE BETWEEN RIB 12-13. CORROSION TEMP BLEND-OUT REPAIR PERMANENT REPAIR AT THIS AREA ON THE NEXT 3000 CYCLES OR AT NEXT C-CK INSP. C/W SRI DO/TS - 0958/08-9928 REF NDT REPORT AMS 100226-14 FOR HFECSDR TRBACPCP2010003Skin · corrodedLT FUEL ELECTRIC PUMP SURROUNDING SKIN CORRODED. BLENDED CORROSION AND TREATED IAW EO E2-57MR-366.SDR FDEA201002230493Skin · corrodedRT WING, UPPER WING SURFACE AT XORS258 FOUND CORROSION. RT WING, UPPER WING SURFACE AT XORS258 REPAIRED IAW EA NR 1-5710-132362. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.SDR ASAA1047484Skin · delaminatedRIGHT WING NR 5 O/B EDGE UPPER SURFACE HAS DELAMINATED AREA. REMOVED DAMAGED AREA, FABRICATED REPAIR DOUBLERS AND BONDED REPAIR.SDR FDEA201002220481Skin · crackedCRACK INDICATION DURING HFEC OPEN HOLE INSP AT ONE HOLE (XORS696.730, STR36) ON LT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUT OUT. REPAIRED IAW EA NR 1-5710-132354. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109.SDR DL76L100673Skin · crackedRT WING INBD F/S PITCH LOAD FITTING, 1 FASTENER HOLE FOUND CRACKED AT SKIN ROW MOST AFT HOLE LWR SURFACE APPROX .1250"IN LENGTH, RUNNING AFT OTBD. REPAIRED IAW ERA 479974-14AD.SDR FDEA201002190473Skin · misrepairedEXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 255. EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 255, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT SDR FDEA201002190472Skin · misrepairedEXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 243. EXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT LOWER SKIN APPROX STA XIFH 243, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OUT SDR FDEA201002190471Skin · misrepairedEXISTING REPAIR AT LT WING INBD FLAP OTBD SEGMENT UPPER SKIN APPROX STA XIFH 256. EXISTING REPAIR AT LT WING INBD FLAP, OTBD SEGMENT UPPER SKIN APPROX STA XIFH 256, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. NEW REPAIR CARRIED OSDR FDEA201002190470Skin · noneEXISTING REPAIR AT LT WING INBD FLAP INBD SEGMENT UPPER SKIN APPROX STA XIFH 243. EXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT, UPPER SKIN APPROX STA XIFH 243, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-01 FIGURE 201, REPAIR 1 REVISIONSDR FDEA201002190469Skin · noneEXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT, UPPER SKIN APPROX STA XIFH 193. EXISTING REPAIR AT LT WING INBD FLAP, INBD SEGMENT UPPER SKIN APPROX STA XIFH 193, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-00 FIGURE 201, REPAIR 1, REVSDR FDEA201002190468Skin · noneEXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT LOWER SKIN APPROX STA XIFH 217. EXISTING REPAIR AT RT WING INBD FLAP INBD SEGMENT LOWER SKIN APPROX STA XIFH 217, EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED IAW SRM 57-00-00 FIGURE 205, REPAIR GENERAL REVISDR FDEA201002190467Skin · misrepairedEXISTING REPAIR AT LT WING FIXED L/E STA XORS 433 (BEHIND NR 3 SLAT). EXISTING REPAIR AT L/E WING FIXED L/E STA XORS 433 (BEHIND NR3 SLAT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NR SDR FDEA201002190466Skin · misrepairedEXISTING REPAIR AT LT WING FIXED L/E STA XORS 402 (BEHIND NR 3 SLAT). EXISTING REPAIR AT LT WING FIXED L/E STA XORS 402 (BEHIND NR 3 SLAT), EVALUATED AND FOUND PREVIOUSLY ACCOMPLISHED NOT IAW SRM REPAIR SCHEME. REPAIR CARRIED OUT ON EXISTING REPAIR IAW EA NRSDR ASAA1047418Skin · crackedLEFT WING FIXED LEADING EDGE CRACKED ABOVE NR 3 SLAT O/B CRACK CUTOUT. REPAIRED BY TAPER SANDING AREA AND PERFORMING PLY REPLACEMENT VACUUM BAGGING AND CURED.SDR QXEA2010022200098Panel · chafedC-CHECK - CHAFING ON BOTTOM RT WING BOX WHERE TOP OF PANEL 264AR INTERSECT. BLENDED CHAFE ON BOTTOM RT WING BOX TO REMOVE ALL DAMAGE IAW SRM 57-11-30 (1-6)(B)(1-10). HFEC INSP BLEND FOR CRACKS IAW NDTM PART 6 51-00-01-250-801, NO CRACKS NOTED. UT THICKNESS
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