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.

SDR IPXA12M73575Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED JUST INBD OF NR 11 SLAT TRACK XOS 692-698. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-D.Apr 17, 2012 · N289UP · Doug MD11FSDR IPXA12M73515Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED JUST OTBD OF NR 10 SLAT. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS661-667 IAW SRM 57-40-02. REPAIR 9, FIG.203 AND EO MD11-5730-42916-D.Apr 17, 2012 · N289UP · Doug MD11FSDR IPXA2M73333Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED JUST INBD OF FUEL PANEL. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS610-616 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-D.Apr 17, 2012 · N289UP · Doug MD11FSDR IPXA2M73331Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED ABOVE NR 8 SLAT TRACK. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS537-547 IAW SRM 57-40-02, REPAIR 9, FIG 203 & EO MD11-5730-42916-D.Apr 17, 2012 · N289UP · Doug MD11FSDR 2012F00077Skin · dentedDURING POST FLIGHT WALK-AROUND BY FLIGHT CREW NOTICED A POSSIBLE BIRD STRIKE AND DENT ON LT OTBD L/E.Apr 17, 2012 · N477WG · Gulstm G1159ASDR MTNA0417120001Skin · corrodedLEFT AND RIGHT WING HAS CORROSION BETWEEN RIBS 4/5 AND STIFFENERS 8/9. REMOVED CORROSION IAW ATR STRUCTURAL REPAIR INSTRUCTION REF DT/S-2320/12-17325.Apr 17, 2012 · N820FX · Aerosp ATR72212SDR DALA1223150930Skin · corrodedDURING HMV CORROSION WAS FOUND ON RIGHT MAIN FUEL ACCESS DOOR CUTOUT. DOOR CUTOUT REPAIRED IAW ERA 502172-14 REV ORIG.Apr 15, 2012 · N930DL · Doug MD88SDR DALA1223080930Skin · corrodedDURING HMV CORROSION WAS FOUND ON LEFT MAIN FUEL TANK ACCESS DOOR CUTOUT DOOR CUTOUT WERE CLEANED AND NO CORROSION FOUND. REPAIRED IAW ERA 502171-14 REV ORIG AND ERA 502172-14 REV ORIG.Apr 15, 2012 · N930DL · Doug MD88SDR DALA1223070930Skin · damagedDURING HMV TOOLING MARKS WERE FOUND ON LEFT MAIN FUEL TANK ACCESS DOOR CUT OUT NBR 1365C. DOOR CUT OUT REPAIR WILL BE ATTENDED WITH AN ERA. DAMAGE RIVET HOLES WERE STEP UP AND BUSHING INSTALLED IAW ERA 502171-14 REV ORIG.Apr 15, 2012 · N930DL · Doug MD88SDR USAA2012041800017Plate · corrodedS2 CHECK - LEVEL 2 FRETTING CORROSION ON LEFT WING LOWER FUEL TANK PLATE 540JB AT WS 268. REPLACED LEFT WING LOWER FUEL TANK PLATE 540JB IAW A320 AMM 57-27-11-400-002-A.Apr 14, 2012 · N661AW · Airbus A320232SDR CA120416007Skin · corroded(CAN) RIGHT WING DE-ICE BOOT REQUIRED REPLACEMENT. UPON REMOVAL OF DE-ICE BOOT, CORROSION WAS NOTED THROUGHOUT THE LEADING EDGE SKIN, OTBD WING CENTER SECTION FROM WS 147.735-WS 223.485, CORROSION WAS NOTED TO BE ALMOST THROUGH THE SKIN IN SEVERAL AREAS. THIS Apr 13, 2012 · Beech 1900DSDR 7AHR201204132155Skin · corrodedCORROSION RT WING UPPER SURFACE UNDER WING WALKWAY PAINT AT WING STA 765.9 AT WBL 92.5. BLENDED CORROSION, AFTER CORROSION REMOVAL IT WAS DETERMIND THE MATERIAL LOSS WAS OUT OF LIMITS. AFTER REVIEWING THE CURRENT SRM IT WAS DETERMIND THERE WAS NOT REPAIR IN Apr 13, 2012 · N840AL · Boeing 7372X6CSDR UALA2012041202209Seal · leakingMAINT REPORTS FUEL LEAK FROM RT WING ACCESS PANEL INBOARD NR 5 DRIP STICK. PANEL 641KB MOLDED RUBBER SEAL DAMAGED. MOLDED RUBBER SEAL REPLACED PER AMM. FUEL LEAK CHECK PERFORMED. FOUND NO LEAK.Apr 12, 2012 · N663UA · Boeing 767322SDR UALA2012041302241Skin · damagedLEFT WING ACCESS HOLE FOR FUEL PANEL 540HB HAS 1 EA ELONGATED HOLE IN WING LOWER SKIN. HOLE IN LANDING LOCATED BETWEEN RIBS 13 AND 14. EVALUATED HOLE FOR OVERSIZING, GENERATED AN RFTS TO EG. REAMED HOLE TO FINAL SIZE OF .578 ", ACCMP'D BHEC PER NDT 6-51-10Apr 12, 2012 · N454UA · Airbus A320232SDR TRBA20120412002Skin · corrodedDURING MX INSPECTION, FOUND CORROSION AT LT WING LOWER SKIN T/E BETWEEN RIB 7 & 8. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED CORROSION TREATMENT IAW EO E2-5700-482. THE ACFT WAS RETURNED TO SERVICE.Apr 12, 2012 · N447AM · Aerosp ATR72SDR QXEA2012041200276Skin · corrodedPANEL 621BT HAS CORROSION ON THE LOWER SIDE. BLENDED OUT CORROSION IAW RD 8/4-57-425. REMAINING THICKNESS WITHIN LIMITS RD 8/4-57-425. CONFIRMED CRACK FREE AREA REF NTM 51-00-06-910-801. TREATED AND PRIMED IAW SRM 51-21-10 AND 51-25-40. COMPLETED REPAIR IApr 12, 2012 · N417QX · Bombdr DHC8402SDR TRBA20120411002Skin · corrodedDURING INSP, FOUND CORROSION AT LT WING LOWER SKIN T/E BETWEEN RIB 7 AND 8. THE ACFT WAS REMOVED FROM SERVICE. PERFORMED LT WING CORROSION TREATMENT ON RIB 7 STIFFENER 10 IAW EO E2-5700-482. THE ACFT WAS RETURNED TO SERVICE.Apr 11, 2012 · N447AM · Aerosp ATR72SDR QXEA2012041000278Skin · corrodedPANEL 624AT HAS MINOR FRETTING. BLENDED OUT FRETTING IAW RD 8/4-57-442. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-442. CONFIRMED AREA TO BE CRACK FREE REF NTM 51-00-06-910-801 PT 1. TREATED AND PRIMED IAW SRM 51-21-10 AND 51-25-40. COMPLETED REPAIR Apr 10, 2012 · N417QX · Bombdr DHC8402SDR QXEA2012041000277Skin · corrodedPANEL 623AT HAS CORROSION ON THE LOWER SIDE. BLENDED OUT CORROSION IAW RD 8/4-57-425. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-425. CONFIRMED AREA TO BE CRACK FREE REF NTM 51-00-06-910-801 PT 1. TREATED AND PRIMED IAW SRM 51-21-10 AND 51-25-40. COMApr 10, 2012 · N417QX · Bombdr DHC8402SDR QXEA2012041000274Skin · corrodedPANEL 521AT HAS CORROSION ON THE LOWER SIDE. REMOVED CORROSION IAW RD 8/4-57-425. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-425. CONFIRMED CRACK FREE AREA REF NTM 51-00-06-910-801. TREATED PRIMED IAW SRM 51-21-10 AND 51-25-40. COMPLETED REPAIR REF RApr 10, 2012 · N417QX · Bombdr DHC8402SDR QXEA2012041000272Skin · corrodedSKIN PANEL 521BT HAS CORROSION ON THE LOWER SURFACE. REMOVED CORROSION IAW RD 8/4-57-425. REMAINING THICKNESS FOUND WITHIN LIMITS IAW RD 8/4-57-425. CONFIRMED CRACK FREE AREA REF NTM 51-00-06-910-801. TREATED, PRIMED IAW 51-21-10 AND 51-25-40. COMPLETED REApr 10, 2012 · N417QX · Bombdr DHC8402SDR KCSA2012041010049Skin · corrodedLEFT WING T/E WBL 158 UPPER SURFACE WHERE T/E PANEL MEETS SPAR HAS POPPED RIVETS AND EVIDENCE OF CORROSION.Apr 10, 2012 · N748CK · Boeing 747221FSDR QXEA2012040900275Skin · corrodedWING LANDING FOR PANEL 624AT HAS FRETTING. BLENDED OUT FRETTING IAW RD 8/4-57-445. CONFIRMED CRACK FREE AREA REF NTM 51-00-01-250-801 PT 6. REMAINING THICKNESS WITHIN LIMITS IAW RD 8/4-57-445. APPLIED ALODINE AND PRIMER IAW RD 8/4-57-445.Apr 9, 2012 · N417QX · Bombdr DHC8402SDR QXEA2012040900273Skin · corrodedWING LANDING FOR PANEL 524ET HAS MINOR FRETTING AND MISSING SURFACE PROTECTION. BLENDED OUT FRETTING IAW RD 8/4-57-445. CONFIRMED CRACK FREE AREA REF NTM 51-00-01-250-801 PT 6. REMAINING THICKNESS FOUND WITHIN LIMITS RD 8/4-57-445. APPLIED ALODINE AND PRIMApr 9, 2012 · N417QX · Bombdr DHC8402SDR 7AHR201204092258Access Panel · corrodedCORROSION AT LT WING FWD LOWER SPAR AT ACCESS PANEL MATING SURFACE FROM WBL 227.0 TO WBL 522.0. REMOVE ALL CORROSION FROM PANEL MATING SURFACE. MATERIAL LOSS FOUND TO OUT OF LIMITS AT WBL 291.82 AND WBL 314.76. DAMAGE FOUND TO BE OUTSIDE OF THE PARAMETER OUTApr 9, 2012 · N840AL · Boeing 7372X6CSDR 7AHR201204092154Skin · corrodedCORROSION ON TOP OF LT WING UNDER WALKWAY PAINT. BLENDED CORROSION, AFTER CORROSION REMOVAL FROM WING SKIN, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REPAIR REQUIREMENTS FOUND TO BE OUTSIDE OF STANDARD SRM REPAIR. FABRICATED REPAIR PARTS AND INSTALLED ALL RApr 9, 2012 · N840AL · Boeing 7372X6CSDR DALA1221200930Access Panel · damagedDAMAGE ON RT WING FUEL TANK ACCESS PLATES RUB STRIP SETTLEMENT AREA CUTOUT NUMBER 1436C. REPAIRED PER AMR 09570436.Apr 8, 2012 · N930DL · Doug MD88SDR DALA1221190930Access Panel · corrodedCORROSION AND DRILL MARKS ON RT WING FUEL TANK ACCESS PLATE RUB STRIP SETTLEMENT AREA CUTOUT NUMBER 1414C. REPAIRED PER AMR 09570436.Apr 8, 2012 · N930DL · Doug MD88SDR DALA1221180930Access Panel · damagedELONGATED RIVET HOLES AND DRILL MARKS ON RT WING FUEL TANK ACCESS PLATE RUB STRIP SETTLEMENT AREA CUTOUT. REPAIRED PER AMR 09570436.Apr 8, 2012 · N930DL · Doug MD88SDR DALA1221170930Skin · damagedDAMAGE ON LEFT MAIN FUEL TANK ACCESS DOOR CUTOUT. REPAIRED PER AMR 09570436.Apr 8, 2012 · N930DL · Doug MD88SDR FDEA201204071285Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON LT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 536AB CUTOUT AND FOUND CRACK INDICATION ON 04 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157169 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11Apr 7, 2012 · N577FE · Doug MD11FSDR FDEA201204071284Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON RT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 636AB CUTOUT AND FOUND CRACK INDICATION ON 06 EACH FASTENER HOLES. REPAIR CARRIED OUT IAW EA 1-5710-157168 PART 1. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVISION 11Apr 7, 2012 · N577FE · Doug MD11FSDR USAA2012042000009Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER RIGHT WING FUEL ACCESS PANEL NR 640MB BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 TO RIB 18. REPLACED LOWER RIGHT WING FUEL ACCESS PANEL NR 640MB IAW A319 AMM 57-27-11-400-002 & JOB CARD 26T60057033.Apr 7, 2012 · N817AW · Airbus A319132SDR USAA2012042000008Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LOWER RIGHT WING FUEL ACCESS PANEL NR 640NB BETWEEN WS 9704 TO WS 10204 & BETWEEN RIB 18 TO RIB 19. REPLACED LOWER RIGHT WING FUEL ACCESS PANEL NR 640NB IAW A319 AMM 57-27-11-400-002 & JOB CARD 26T60057033.Apr 7, 2012 · N817AW · Airbus A319132SDR FDEA201204061275Skin · crackedRIGHT WING LOWER FIXED L/E AT REFUELING PANEL CUTOUT INBD FORWARD CORNER AREA FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02. REPAIR 7 FIG 201 REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REVISION 114.Apr 6, 2012 · N577FE · Doug MD11FSDR FDEA201204051266Skin · misrepairedLT WING DROOP L/E UPPER SURFACE FOUND MISREPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201. REPAIRED IAW EA 1-5730-159836, CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 5, 2012 · N577FE · Doug MD11FSDR FDEA201204051264Skin · crackedNINE FASTENER HOLES FOUND CRACKED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= -683.4 AND STATION XORS= -713.6.Apr 5, 2012 · N593FE · Doug MD11FSDR FDEA201204051262Skin · crackedSEVEN FASTENER HOLES FOUND CRACKED DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. REPAIRED IAW EA 1-5710-159826 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-Apr 5, 2012 · N593FE · Doug MD11FSDR SWIA201230356Skin · damagedLEFT INBOARD WING LEADING EDGE DAMAGED IN THE FORM OF A DENT. REPAIRED DAMAGED AREAS OF LEFT WING LEADING EDGE SKIN IN REFERENCE TO REO.Apr 5, 2012 · N506CA · Cndair CL6002B19SDR FDEA201204051270Skin · crackedRT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT IAW SRM 57-40-02. REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REApr 5, 2012 · N577FE · Doug MD11FSDR 7AHR201204052466Skin · corrodedCORROSION ON INTERNAL SKIN AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, MATERIAL LOSS WITHIN LIMITS. ALODINED AND PRIMED STRUCTURE IAW CURRENT SRM.Apr 5, 2012 · N840AL · Boeing 7372X6CSDR 7AHR201204052467Skin · corrodedCORROSION ON LEFT WING INTERNAL SURFACE AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, ALODINE AND PRIMED IAW CURRENT SRM.Apr 5, 2012 · N840AL · Boeing 7372X6CSDR 2012F00072Skin · corrodedCORROSION ON INTERNAL SKIN AND LONGERON BETWEEN WING STA 557.0 AND WBL 583.0. REMOVED CORROSION, ALODINE, AND PRIMED STRUCTURE IAW CURRENT SRM.Apr 5, 2012 · N840AL · Boeing 7372X6CSDR FDEA201204051269Skin · crackedLEFT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED AS MAJOR GMM 6-2-100, REV 114.Apr 5, 2012 · N577FE · Doug MD11FSDR FDEA201204051260Finger Doubler · crackedLEFT WING L/E REFUELING ACCESS PANEL COMPARTMENT AT STA XORS 525 FOUND UPPER FINGER DOUBLER CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02, REPAIR 9, FIG 203, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 5, 2012 · N577FE · Doug MD11FSDR IPXA2M73426Skin · gougedINSPECTION TYPE: 4C, RT WING FIXED L/E SKIN UPPER SURFACE AT CUTOUT FOR SLAT TRACK NR 17 AND ACCESS DOOR BETWEEN XOS 1065.6955 AND XOS 1057.188 IS GOUGED. REPAIRED IAW EA 011-5730-01-A3871-IR AND EO MD11-5730-47114-A.Apr 4, 2012 · N260UP · Doug MD11FSDR IPXA2M73407Skin · dentedINSPECTION TYPE: 4C, RT WING FIXED L/E SKIN AT XOS 1187 IS DENTED. REPAIRED IAW EA 011-5730-01-A3806-IR AND EO MD11-5730-47059.Apr 4, 2012 · N260UP · Doug MD11FSDR TRBA20120404002Skin · corrodedDURING MX INSPECTION, FOUND GALVANIC SURFACE CORROSION AT PANEL 1 NR 522CT. THE ACFT WAS REMOVED FROM SERVICE. REMOVED CORROSION BLENDED AND THREATED. THE ACFT WAS RETURNED TO SERVICE.Apr 4, 2012 · N355AT · Aerosp ATR72212SDR TRBA20120404003Skin · corrodedDURING MX INSPECTION, FOUND GALVANIC SURFACE CORROSION AT PANEL 1 NR 622CT. THE ACFT WAS REMOVED FROM SERVICE. REMOVED CORROSION BLENDED AND THREATED. THE ACFT WAS RETURNED TO SERVICE.Apr 4, 2012 · N355AT · Aerosp ATR72212SDR IPXA2M73093Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER, 3 CRACKS BETWEEN XFS663 AND XFS669. REPAIRED RT WING FIXED L/E BEADED DOUBLER REF EO MD11-5730-42916-C.Apr 4, 2012 · N260UP · Doug MD11F
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