JASC 5730
Service difficulty reports · 27,262
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 FDEA202109212578Skin · crackedR/H LOWER WING, LOWER RE-FUEL DOOR, FWD INBD CORNER HAS A CRACK. (MKD WITH DOT #1) REPAIRED PER SRM 57-40-01,REPAIR 18, FIG 201. (MAJOR REPAIR)SDR IPXA2021101374919Seal · wornINSPECTION TYPE:A300RT WING FLAP TRACK FAIRING 633AB I/B BULB SEAL WORN/TORN.REMOVED AND REPLACED IAW SRM 51-40-21.SDR IPXA2021101474944Skin · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN BETWEEN XCW -103.84 TO XCW -118.2 AT STRINGERS 19 & 20 IS CORRODED.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN XCW -103.84 TO XCW -118.2 AT STRINGERS 19 & 20 IAW VT-SAA EA 011-5730-01-A9381 REV. IR AND UPSDR CALA2021092001615Rivet · damagedPDA 3 RIGHT WING INBOARD FIXED LEADING EDGE HAS ONE RIVET HEAD BROKEN OFF/MISSING AT OUTBD END NEAR PYLON -- SEE PHOTO PHOTO ADDED REMOVED BAD RIVET AND INSTALLED NEW RIVET REF. SRM 51-40-02SDR IPXA2021101574974None · corrodedINSPECTION TYPE:3CRT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN STA. XORS=782 AND XORS=826.5.REPAIRED CORRODED RT WING UPPER CAP IAW VT-SAA EA 011-5700-01-A9378 REV I/R AND UPS EO MD11-5710-81838-A (MINOR).SDR IPXA2021101274888None · noneINSPECTION TYPE:3CLT WING REAR SPAR UPPER CAP HAS CORROSION BETWEEN STA. XORS=784-826.REPAIRED CORRODED LT WING UPPER CAP IAW VT-SAA EA 011-5710-01-A9384 REV I/R AND UPS EO MD11-5710-81777-A (MINOR).SDR IPXA2021101274858Skin · crackedINSPECTION TYPE:3CLT WING FIXED L/E SKIN IS CRACKED AT XOS 611.REPAIRED CRACKED LT WING FIXED L/E SKIN AT XOS 611 IAW SRM 57-40-01, REPAIR 18, FIGURE 201. (MAJOR)SDR IPXA2021100674664None · noneINSPECTION TYPE:3CR/H WING UPPER SURFACE SKIN HAS CORROSION BETWEEN STA XORS 853 AND XORS 856 AND AT STRINGER 7.REMOVED,REPAIRED CORRODED SKIN SURFACE IAW VT-SAA EA 011-5700-01-A9380 I/R AND UPS EO MD11-5730-81779-A. (MINOR)SDR IPXA2021100474563Skin · corrodedINSPECTION TYPE:3CRT UPPER WING SURFACE SKIN HAS CORROSION BETWEEN STA. XORS 575 AND XORS 619.REPAIRED CORRODED RT WING UPPER SURFACE SKIN BETWEEN STA. XORS 575 AND XORS 619 IAW VT-SAA EA 011-5710-01-A9374 REV I/R AND UPS EO MD11-5730-81772-A (MINOR).SDR FDEA202109182338Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER CRACKED AT STATION XOS 623 AS MARKED. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT STATION XOS 623 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED SDR UIEA2021091302014Skin · crackedCRACK NOTED ON RH WING LOWER SURFACE STR L-6.5 MOST I/B FASTENER AT 6 O'CLOCK POSITION LOOKING UP/FWD. APPROX 1/4" LONG.(<P>REPAIRED CRACK AT RH WING LOWER SURFACE STR L-6.5 MOST I/B FASTENER HOLE BTW WSTA 990.2 AND 1046.2 IAW B767 FAS EA 21069-P1 REV:IR, SRM SDR UIEA2021091302015Skin · crackedWHILE PERFORMING HFEC INSP ON PART 1-2 OF ORIGINATING TASK CARD. VISUALLY NOTED A CRACK AND CONFIRMED WITH HFEC ON THE RH WING LOWER SURFACE STR L-9.5, 22ND FASTENER FROM MOST O/B FASTENER ON STR AT 12 O'CLOCK POSITION LOOKING UP/FWD, APPROX 1/8" LONG.(<P>REPASDR CALA2021091701602Access Panel · missingPDA 3 ACCESS PANEL 621 ADB MISSING DURING WALK AROUND. REPLACED ACCESS PANEL 621 ADB AS REQUIRED A/C OK TO CONTINUE.SDR DALA2021091605527Skin · corrodedSHIP 3265 CORROSION UPPER SURFACE UPPER SKIN LOCATED AT LEVEL RIB13 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: EVALUATED REWORKED UPPER SKIN AND FOUND WITHIN LIMITS AS PER A320 SRM 57-21-11. (1949800)SDR CALA2021091501575Fastener · missingPDA 3 14 FASTENERS MISSING ON UPPER WING PANEL ABOVE LT MLG. PANEL 551BT REPLACED 14 SCREWS ON PANEL 551BT. REF AMM 32-32-11-400-801 AND 20-50-11-910-801. PANEL SECURE.SDR IPXA2021092574272Skin · corrodedINSPECTION TYPE:3CCENTER WING UPPER SKIN AT STRINGER 20 BETWEEN XCW -76.5 TO XCW -82.5 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SKIN AT STRINGER 20 BETWEEN XCW -76.5 TO XCW -82.5 IAW VT-SAA EA 011-5730-01-A9363 REV. IR AND UPS EO MD11-5730-81706-A. (MINSDR IPXA2021092574271Skin · corrodedINSPECTION TYPE:3CCENTER WING UPPER SKIN AT STRINGER 17 BETWEEN XCW -79.7 TO XCW -100 IS CORRODED.REPAIRED CORRODED CENTER WING UPPER SKIN AT STRINGER 17 BETWEEN XCW -79.7 TO XCW -100 IAW VT-SAA EA 011-5710-01-A9352 REV. IR AND UPS EO MD11-5730-81698-A. (MINORSDR IPXA2021092574270Skin · corrodedINSPECTION TYPE:3CUPPER OVER WING TANK WEB BETWEEN X= -47.5 TO X= -75.25 AT Y= 1352.3 IS CORRODED.REPAIRED CORRODED UPPER OVER WING TANK WEB BETWEEN X= -47.5 TO X= -75.25 AT Y= 1352.3 IAW VT-SAA EA 011-5730-01-A9368 REV. IR AND UPS EO MD11-5730-81708-A. (MINORSDR IPXA2021092474225Skin · corrodedINSPECTION TYPE:3CCENTER WING TANK UPPER SKIN BETWEEN XCW -50 TO XCW -86 AT STRINGERS 14 & 15 IS CORRODED.REPAIRED CORRODED CENTER WING TANK UPPER SKIN BETWEEN XCW -50 TO XCW -86 AT STRINGERS 14 & 15 IAW VT-SAA EA 011-5730-01-A9354 REV. IR AND UPS EO MD11-5730SDR 2021F00291Panel · damagedENGINEERING MEMO DQ31487M1 RIGHT WING CUFF PANEL DAMAGE (IMPACT) DATED 9/14/2021.SDR MASA20210914421Access Panel · corrodedLH WING LEADING EDGE ACCESS PANEL (522CB) BETWEEN SS 99.68 & SS 111.922 WAS FOUND WITH WEAR DAMAGE. PERFORMED PERMANENT REPAIR IAW CRJ 700/900 SRM 57-42-32, 57-42-32-991-801, ITEM 9D, EA 72-2021-069. DEFECT LOCATION: LH W1NG LEADING EDGE/ SS 99.68 & SS 111.922SDR FDEA202109132489None · noneREPAIR ASSESSMENT: AT THE TIME OF AGING AIRCRAFT RECORDS REVIEW, A MAJOR REPAIR ON L/H WING FIXED LEADING EDGE AT SLAT TRACK #10 CUTOUT, W.O 75165 N00604, JPF ITEMS REQUIRING RII ARE MARKED (N/A). REPAIR REQUIRES REWORK. MAJOR REPAIR: REMOVED ORIGINAL REPASDR 2021F00240Skin · dentedDENT ON LH WING FIXED LEADING EDGE UPPER SKIN, DURING TRANSIT CHECK, IT WAS DETECTED A DENT ON LH WING FIXED LEADING EDGE UPPER SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT ON LH WING FIXED LEADING EDGE UPPER SKIN STA 150.75; HFEC INSPECTSDR IPXA2021100874736Bracket · gougedINSPECTION TYPE:3CL/H WING INBD FLAP OUTBD FWD HINGE BRACKET ASSY IS GOUGED AT THE INBD BRACKET HALF SURFACE.REPAIRED GOUGED BRACKET ASSY ON THE L/H WING INBD FLAP OUTBD FWD HINGE IAW VT-SAA EA 011-5740-01-A9373 REV I/R AND UPS EO MD11-5740-81818-A AND REF FAASDR DALA2021091405466Skin · corrodedSHIP 3264 CORROSION UPPER SURFACE EXTERNAL SKIN REAR SPAR LOCATED AT RIB17 ON LH WING. CORRECTIVE ACTION: EVALUATED REWORKED AREA LOC. ON UPPER SURFACE EXTERNAL SKIN AT RIB17 ON LH WING AND FOUND WITHIN LIMITS PER A320 SRM 57-21-11. (1947022)SDR DALA2021091405465Skin · corrodedSHIP 3264 CORROSION UPPER SURFACE EXTERNAL SKIN REAR SPAR LOCATED AT RIB 13 ON LH WING. CORRECTIVE ACTION: EVALUATED REWORKED AREA LOC. ON UPPER SURFACE EXTERNAL SKIN AT RIB 13 ON LH WING AND FOUND WITHIN LIMITS AS PER A320 SRM 57-21-11. (1947002)SDR DALA2021091405457Skin · gougedSHIP 3264 GOUGE LOWER SKIN IB FIXED LEADING EDGE INBOARD POSITION ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 593853-14 REV.ORIGINAL. (1946960)SDR FDEA202109132297Skin · crackedLEFT WING FIXED L/E CRACKED AT #3 SLAT INBD TRACK. REPAIRED ALL NOTED AREAS ON L/W FIXED LE BEHIND #3 SLAT IAW B757 SRM 57-41-01-2R FIG 201 SHEET 8 AND SRM 51-70-07-OG AND FIG 10.SDR IPXA2021092474224Doubler · crackedINSPECTION TYPE:3CRT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 584.89 TO XOS 589.89 IS CRACKED.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 584.89 TO XOS 589.89 IAW SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)SDR IPXA2021092474235Doubler · crackedINSPECTION TYPE:3CLT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 661.71 TO XOS 667.67 IS CRACKED.REPAIRED CRACKED LT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 661.71 TO XOS 667.67 IAW SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)SDR IPXA2021092474234Doubler · crackedINSPECTION TYPE:3CRT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 648.29 TO XOS 653 IS CRACKED.REPAIRED CRACKED RT WING FIXED L/E BEADED DOUBLER BETWEEN XOS 648.29 TO XOS 653 IAW SRM 57-40-02, REPAIR 15, FIGURE 205. (MAJOR)SDR IPXA2021092274162Doubler · crackedINSPECTION TYPE:3CLT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 789.645 IS CRACKED.REMOVED AND REPLACED CRACKED LT WING FIXED L/E SKIN SPLICE DOUBLER AT XOS 789.645 IAW SRM 51-33-01 AND SRM 51-35-01. (MINOR)SDR YENA2021091700611Skin · corrodedDURING HMV, CORROSION AROUND FASTENER ROW TOP RIGHT WING SURFACE STR 11 BETWEEN RIB 2/3 DOT 88-017 ; REMOVED CORROSION FROM AREA IAW A320 SRM 51-74-00 PERFORMED NDT INSPECTION ON AREA WITH ORIGINAL MATERIAL .210 MATERIAL LOSS OF .040 AND FOUND OUT OF LIMITS IASDR YENA2021091700610Skin · corrodedDURING HMV, CORROSION AROUND FASTENER ROW TOP RIGHT WING SURFACE STR 11 BETWEEN RIB 3/4 ; REMOVED CORROSION IAW A320 SRM 51-74-00 PERFORMED NDT INSPECTION ON AREA WITH ORIGINAL THICKNESS .210 MATERIAL REMAIN .173 WITH A LOSS OF .037 AND FOUND OUT OF LIMITS IAWSDR YENA2021091700609Skin · corrodedDURING HMV, CORROSION AROUND FASTENER TOP RIGHT-WING SURFACE STR 11 HEAR SLAT #3 DOT 88-023 ; REMOVED CORROSION FROM AREA IAW A320 SRM 57-21-11 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL THICKNESS .166 MATERIAL REMAIN .155 WITH A LOSS OF .011AND FOUND OUT OF LISDR YENA2021091700608Skin · corrodedDURING HMV, L/H WING UPPER SURFACE HAS AREAS OF CORROSION AT STA 1957 RIB 4 AND UPPER SKIN BUTT SPLICE11 DOT 008 ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .213 MATERIAL REMAIN .185 WITH A LOSS OF .028 SDR YENA2021091700607Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREA OF CORROSION AT RIB 1 3"FWD OF UPPER SKIN BUTT SPLICE 11.7 INCHES O/B OF FUSELAGE ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .210 MATERIAL REMAIN .168 WITH LOSSDR YENA2021091700606Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION AT WING WALK AREA STA 700/RIB2 32" AFT OF FRONT SPAR ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .200 MATERIAL REMAIN .155 WITH LOSS OF .045 AND FSDR YENA2021091700605Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION ABOVE FRONT SPAR AT STA 1957/RIB4 ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .260 MATERIAL REMAIN .152 WITH LOSS OF .108AND FOUND TO BE OUT OF LISDR YENA2021091700604Skin · corrodedDURING HMV, LH WING UPPER SURFACE HAS AREAS OF CORROSION AT RIB 8 ABOVE REAR SPAR ; REMOVED CORROSION IN AREA IAW A320 SRM 51-74-00 ACCOMPLISHED NDT INSPECTION WITH ORIGINAL MATERIAL .311 MATERIAL REMAIN .240 WITH A LOSS OF .071 AND TO BE OUT OF LIMITS IAW A32SDR FDEA202109122291Skin · crackedRIGHT WING FIXED L/E CRACKED AT #8 SLAT APROX 2 FT FROM OTBD END REPAIRED RIGHT WING FIXED L/E AT #8 SLAT 2FT FROM O/B END IAW B757 SRM 57-41-01, 57-41-01- 2R FIG 201 SHEET 8 AND 51-70-07-OG.SDR HALA2021091300132Panel · damagedSHIP 361 621GB PANEL (F57450561009) WITH AN AREA OF DAMAGE THAT EXCEEDS THE REPAIRABLE DAMAGE LIMITS. CORRECTIVE ACTION: REPAIR PANEL REF PRI 593971-14 AND ERA 593971-14. (1945680)SDR DALA2021091305406Skin · corrodedSHIP 3265 CORROSION UPPER SURFACE UPPER SKIN LOCATED AT LEVEL RIB24 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: EVALUATED REWORK LOC UPPER SURFACE UPPER SKIN LOCATED AT LEVEL RIB 24 TRAILING EDGE AREA ON RH WING AND FOUND WITHIN LIMITS AS PER SRM A320 57SDR DALA2021091305405Skin · corrodedSHIP 3265 CORROSION UPPER SURFACE UPPER SKIN LOCATED AT LEVEL RIB 27 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: EVALUATED REWORK LOC UPPER SURFACE UPPER SKIN LOCATED AT LEVEL RIB 27 TRAILING EDGE AREA ON RH WING AND FOUND WITHIN LIMITS AS PER SRM A320 5SDR AALA202109228882Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FOUND IN 17 COUNTER SINK HOLES ON FUEL PLATE ACCESS PANEL 640LB LOCATED ON THE RIGHT WING LOWER SURFACE, STR 8-11 AND RIB 16 - 17. REPLACED FUEL PLATE ACCESS PANEL 640LB PER WORK CARD 26C64057007.SDR SWAA2021101115447Panel · crackedCRACKED ACCESS PANEL 661BB RT WING. FOUND WITHIN LIMITS IAW SRM 57-41-01-2R-1, REPAIR 1, PARA 2.B ITEM 2 AND SRM 51-70-04-2R-9 REPAIR 9. REMOVED DAMAGE AND PREPARED IAW SRM 51-70-04-2R-9, REPAIR 9, PARA 4.A - C AND SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2021101115448Access Panel · delaminatedDELAMINATED ACCESS PANEL 621FB, RT WING EVALUATED AND FOUND WITHIN LIMITS IAW SRM 57-41-01-2R-1, REPAIR 1, TABLE 202, PARA 4.D. REMOVED DAMAGE, PREPARED AND DRIED REPAIR AREA AND REMOVED STRIP IAW SRM 51-70-04-2R-6 PAR.4 A TO D AND SRM 57-41-01-2R-6 REPAIRSDR YENA2021091700592Skin · crackedDURING HEAVY MAINTENANCE, CRACK DISCOVERED. FIXED LEADING EDGE SKIN BTW RIB19 & 20 OF THE SLAT TRACK CUTOUT #5 RH WING; (REF TOMX NR 00094) ACCOMPLISHED REPAIR IAW SRM 57-49-01/REPAIR 51P PAR 4.D.SDR AALA202109090951Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE UPPER SKIN PANEL LOWER SURFACE BETWEEN WS 9704 AND WS 10204, BETWEEN RIB 18 AND RIB 19. REPAIRED SKIN PANEL PER SRM 57-21-11-283-012 AND 51-29-11-911-003.SDR REXA2021091400733Skin · crackedDURING COMPLIANCE OF JOB CARD 57-610-601(NDTM PART 6 57-21-112) A SIGNIFICANT AMPLITUDE INDICATION WAS NOTED ON THE 3RD RIVET GOING IB ON THE FIRST ROW OF RIVETS FWD OF STG8. WS 65.75, RH WING. INSTALLED PERMANENT REPAIR TO RH LOWER WING PLANK AT WS 65.75, ST
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