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 REXA201000239Skin · dentedBIRD STRIKE DAMAGE (DENT· 3.0"L X 2.0"W X 0.250" DEEP) TO RT WING FIXED L/E SKIN BETWEEN WS 163.00 AND FS 178.00. FERRY FLY FROM LGE TO MEM IAW BOMBADRIER REO 601R-57-41-719 WHERE L/E SKIN WAS REPLACED IAW CRJ200 AMM 57-41-01.Nov 2, 2010 · N8659B · Cndair CL6002B19SDR CALA2015071394091Skin Panel · corrodedCORROSION WAS FOUND ON THE LT WING TOP NR 2 PANEL BETWEEN RIB 19 & 20, AT THE MANUAL REFUELING PORT CUT OUT, FROM DF DATED 11 01 2010. BLEND REPAIR WAS ACCOMPLISHED IAW 80263 & EA 319-5721-13-A2032.Nov 1, 2010 · N824UA · Airbus A319131SDR FDEA201011014202Skin · cracked10 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA XORS 713.6. REPAIR CARRIED OUT AT R/H WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN STATION XORS= Nov 1, 2010 · N618FE · Doug MD11FSDR FDEA201011014201Skin · cracked08 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA 713.6.Nov 1, 2010 · N618FE · Doug MD11FSDR UALA2010110304075Skin · corrodedCORROSION WAS FOUND ON THE LT WING TOP NR 2 PANEL BETWEEN RIB 19 AND RIB 20, AT MANUAL REFUELING PORT CUTOUT. BLEND REPAIR WAS ACP IAW UA EVA 80263 AND EA 319-5721-13-A2032, ON N-R C6017Q. REPAIR MUST BE INSPECTED AT THRESHOLD OF 200,300 FLIGHT HOURS, OR 124Nov 1, 2010 · N824UA · Airbus A319131SDR CA101102008Skin · dented(CAN) DURING OVERNIGHT AT MAINTENANCE BASE, NOTICE DAMAGE TO RT WING LEADING EDGE AT WS380 CAUSED BY BIRD STRIKE. SUSPECT THAT HAPPEN ON LAST FLIGHT OF THE DAY. AFTER FURTHER INSPECTION FOUND DENTED BEYOND LIMITS, DEFECT 947790 RAISED. TEMPORARY REPAIR C/OUOct 31, 2010 · Cndair CL6002B19SDR MASA2010110301216Panel · damagedCONTINUOUS AIRFRAME SHIMMY OR VIB IN FLIGHT. MX REPAIRED AND INSTALLED LEFT OVERWING PANEL.Oct 31, 2010 · N513MJ · Cndair CL6002C10SDR ASMF201011001Access Panel · crackedDURING TRANSIT CHECK, TECH PERSONNEL DETECTED A FUEL LEAK IN RT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 632EB; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT.Oct 30, 2010 · N908AM · Boeing 737705SDR A6WA201040800Panel · corrodedFUEL C/O FOR PNL 550CB REQUIRE AWAC E06/021/457 CURRENT REV TO BE C/W INDICATION FOUND ON AFT OTBD SIDE. REPAIRED FUEL PANEL C/O PNL 550CB IAW REO 601R-57-21-030 REV H, AT APT OTBD SIDE DETAIL III.Oct 28, 2010 · N448AW · Cndair CL6002B19SDR WX0A070641Panel · damagedRIGHT WING LEADING EDGE PANEL 1263C HAS TOOL MARKS. ACCOMPLISHED RT WING LEADING EDGE PANEL NR 1263C REPAIR IAW EA 14186 REV I/R DATED 10/27/2010.Oct 27, 2010 · N414NV · Doug MD88SDR FDEA201010214137Skin · crackedRT WING-CRACK FOUND AT THE TRAILING END OF LOWER WING SKIN,APPROX.WING STATION XORS 419. CRACKED SILL IS ACCEPTABLE FOR STRENGTH AND WILL REMAIN IN SERVICE REF.E.A.8-5710-142474.Oct 21, 2010 · N318FE · Doug MD1030FSDR FDEA201010214128Skin · damagedFOUND AT ZONE 600 RT WING TIP STATIC DISCHARGER NEAR THE POSITION LIGHT IS LOOSEN. RT WING TIP SKIN PANEL REPAIRED IAW EA F-5720-142321 WING SECONDARY STRUCTURE MISDRILLED HOLES C/T RT WING TIP - MID SEC SKIN PANEL FOR DISCHARGER BASE INSTALLATION. REPOct 21, 2010 · N935FD · Boeing 7572T7SDR USAA2010111092588Access Door · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL ACCESS DOOR 540HB AT WS 7792 BETWEEN RIBS 13 TO RIB 14. REPLACED LEFT WING LOWER FUEL ACCESS DOOR 540HB AT WS 7792 BETWEEN RIBS 13 TO RIB 14 IAW A320 AMM 57-27-11.Oct 19, 2010 · N631AW · Airbus A320231SDR USAA2010111092587Access Door · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL ACCESS DOOR 640HB AT WS 7792 BETWEEN RIBS 13 TO RIB 14. REPLACED RIGHT WING LOWER FUEL ACCESS DOOR 640HB AT WS 7792 BETWEEN RIBS 13 TO RIB 14 IAW A320 AMM 57-27-11.Oct 19, 2010 · N631AW · Airbus A320231SDR USAA2010110892551Access Panel · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING LOWER FUEL ACCESS PANEL NR 540JB AT WS 8268 & BETWEEN RIBS 14 TO RIBS 15. REPLACED LEFT WING LOWER FUEL ACCESS PANEL 540JB AT WS 8268 & BETWEEN RIBS 14 TO RIBS 15 IAW A320 AMM 57-27-11.Oct 19, 2010 · N631AW · Airbus A320231SDR USAA2010110892550Access Panel · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL ACCESS DOOR NR 640 RB BETWEEN WS 11198 TO WS 11664 & BETWEEN RIBS 21 TO RIBS 22. REPLACED RIGHT WING LOWER FUEL ACCESS DOOR 640 RB BETWEEN WS 11198 TO WS 11664 & BETWEEN RIBS 21 TOOct 19, 2010 · N631AW · Airbus A320231SDR USAA2010102992446Panel · corrodedSAL - S5 - MAJOR REPAIR - NR 6278799 - CORROSION IN COUNTERSINK HOLES OF LEFT WING LOWER FUEL PANEL 540KB BETWEEN WING RIBS 15 TO RIB 16. REPLACED LEFT WING LOWER FUEL PANEL 540KB BETWEEN WING RIBS 15 TO RIB 16 IAW A320 AMM 57-27-11.Oct 19, 2010 · N631AW · Airbus A320231SDR USAA2010102892440Panel · corrodedSAL - S5 - MAJOR REPAIR - NR 6284608 - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING LOWER FUEL PANEL 640NB BETWEEN WING RIBS 18 TO RIB 19. REPLACED RIGHT WING LOWER FUEL PANEL 640NB BETWEEN WING RIBS 18 TO RIB 19 IAW A320 AMM 57-27-11.Oct 19, 2010 · N631AW · Airbus A320231SDR USAA2010102892435Panel · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF LEFT WING LOWER FUEL PANEL 540PB BETWEEN WING RIBS 19 TO RIB 20. REPLACED LEFT WING LOWER FUEL PANEL 540PB BETWEEN WING RIBS 19 TO RIB 20 IAW A320 AMM 57-27-11.Oct 19, 2010 · N631AW · Airbus A320231SDR USAA2010110892552Access Panel · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL ACCESS PANEL 640LB BETWEEN WS 8744 TO WS 9235 & BETWEEN RIBS 21 TO RIB 22. REPLACED RIGHT WING LOWER FUEL ACCESS PANEL 640LB BETWEEN WS 8744 TO WS 9235 & BETWEEN RIBS 21 TO RIB 22 IOct 18, 2010 · N631AW · Airbus A320231SDR USAA2010102892439Panel · corrodedSAL - S5 - MAJOR REPAIR - NR 6278775 - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING LOWER FUEL PANEL 640JB BETWEEN WING RIBS 14 TO RIB 15. REPLACED RIGHT WING LOWER FUEL PANEL 640JB BETWEEN WING RIBS NR 14 TO RIB NR 15 IAW A320 AMM 57-27-11Oct 18, 2010 · N631AW · Airbus A320231SDR USAA2010102892438Panel · corrodedSAL - S5 - MAJOR REPAIR - NR 6278773 - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING LOWER FUEL PANEL 640KB BETWEEN WING RIBS 15 TO RIB 16. REPLACED RIGHT WING LOWER FUEL PANEL 640KB BETWEEN WING RIBS 15 TO RIB 16 IAW A320 AMM 57-27-11.Oct 18, 2010 · N631AW · Airbus A320231SDR USAA2010102892437Panel · corrodedSAL - S5 - MAJOR REPAIR - NR 6278772 - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING LOWER FUEL PANEL 640PB BETWEEN WING RIBS 19 TO RIB 20. REPLACED RIGHT WING LOWER FUEL PANEL 640PB BETWEEN WING RIBS 19 TO RIB 20 IAW A320 AMM 57-27-11.Oct 18, 2010 · N631AW · Airbus A320231SDR USAA2010102892436Panel · corrodedSAL - S5 - MAJOR REPAIR - NR 6278771 - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLES OF RIGHT WING LOWER FUEL PANEL 640MB BETWEEN WING RIBS 17 TO RIB 18. REPLACED RIGHT WING LOWER FUEL PANEL 640MB BETWEEN WING RIBS 17 TO RIB 18 IAW A320 AMM 57-27-11.Oct 18, 2010 · N631AW · Airbus A320231SDR 5APR577Y45Skin · dented(5APR) RT WING AND DE-ICE BOOT DAMAGE FROM BIRDSTRIKE NOTICED AFTER POST FLIGHT INSPECTION.Oct 18, 2010 · N708AF · Pilats PC1247SDR IPXA10M63484Skin · crackedINSPECTION TYPE:2C, LT WING L/E SKIN AT TELESCOPIC DUCT CUTOUT CRACKED ON INBD AND OTBD UPPER CORNERS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLR IAW SRM 57-40-01, REPAIR 10, FIG 201.Oct 17, 2010 · N271UP · Doug MD11FSDR USAA2010111992624Access Door · corrodedSAL - S5 - MAJOR REPAIR - GALVANIC CORROSION ON COUNTER SINK HOLES OF RIGHT WING LOWER FUEL ACCESS DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIBS 14 TO RIB 15. REPLACED RIGHT WING LOWER FUEL ACCESS DOOR 640JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIBS 14Oct 16, 2010 · N103US · Airbus A320214SDR USAA2010110592525Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640CB BETWEEN WS 4067 TO WS 4862 & BETWEEN RIBS 8 TO RIB 9. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640CB BETWEEN WS 4067 TO WS 4862 & BETWEEN RIBSOct 16, 2010 · N103US · Airbus A320214SDR USAA2010110592524Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540AB BETWEEN WS 700 TO WS 1406 & BETWEEN RIBS 2 TO RIB 3. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540AB BETWEEN WS 4862 TO WS 5512 & BETWEEN WS 700 TOct 16, 2010 · N103US · Airbus A320214SDR USAA2010110392491Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 4862 TO WS 5512 & BETWEEN RIBS 9 TO RIB 10. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 4862 TO WS 5512 & BETWEEN RIBSOct 16, 2010 · N103US · Airbus A320214SDR USAA2010110392490Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640GB BETWEEN WS 6699 TO WS 7316 & BETWEEN RIBS 12 TO RIB 13. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640GB BETWEEN WS 6699 TO WS 7316 & BETWEEN RIBOct 16, 2010 · N103US · Airbus A320214SDR USAA2010110392489Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIOct 16, 2010 · N103US · Airbus A320214SDR USAA2010110392488Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12. REPLACED RIGHT WING CLAMP RING FOR FUEL ACCESS DOOR 640FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIOct 16, 2010 · N103US · Airbus A320214SDR USAA2010110392487Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540BB BETWEEN WS 3758 TO WS 2508 & BETWEEN RIBS 6 TO RIB 7. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540BB BETWEEN WS 3758 TO WS 2508 & BETWEEN RIBS 6 Oct 16, 2010 · N103US · Airbus A320214SDR USAA2010110392486Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS 11 TO RIB 12. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540FB BETWEEN WS 6132 TO WS 6699 & BETWEEN RIBS Oct 16, 2010 · N103US · Airbus A320214SDR USAA2010110392485Ring · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS 10 TO RIB 11. REPLACED LEFT WING CLAMP RING FOR FUEL ACCESS DOOR 540EB BETWEEN WS 5512 TO WS 6132 & BETWEEN RIBS Oct 16, 2010 · N103US · Airbus A320214SDR DALA1027345811Skin Panel · crackedDURING L-CHECK FOUND CRACK ON LEFT WING UPPER SURFACE FIXED LEADING EDGE PANEL OSS 438. REPAIRED PER ERA 483182-14.Oct 15, 2010 · N591NW · Boeing 757351SDR CA101015006Skin · corrodedDURING INTERNAL DVI OF THE LT WING TANK IT WAS NOTED THAT THERE WAS CORROSION UNDER THE LT BOOST PUMP IN THE INTERNAL FUEL TANK OF THE LT WING. UPON FURTHER INVESTIGATION AND SUBSIQUENT BLEND OUT OF THE CORROSION. THE CORROSION HAD SPREAD TO A WIDTH OF 2.5 INOct 14, 2010 · Bag JETSTM3112SDR IPXA10M63429Doubler · crackedINSP TYPE:2C, LT WING L/E COMPT CEILING DOUBLER IS CRACKED AT 2EA FASTENERS DIRECTLY ABOVE ANTI-ICE TELESCOPIC DUCT. REMOVED DAMAGED BEADED DOUBLER SECTION FROM LT WING L/E COMPT BETWEEN XOS464 AND XOS470 ABOVE TELESCOPIC DUCT. FABRICATED AND INSTALLED REPAIROct 14, 2010 · N271UP · Doug MD11FSDR IPXA10M63427Doubler · crackedINSP TYPE:2C, LT WING L/E COMPT BETWEEN XOS625 AND XOS633 CEILING DOUBLER IS CRACKED AT 4EA FASTENERS. CUT OUT DAMAGE ON LT WING L/E COMPT FROM XOS625 TO XOS633. FABRICATED AND INSTALLED 1 REPAIR DOUBLER, 1 REPAIR FILLER AND 10 REPAIR ANGLES REF SRM 57-40-02Oct 14, 2010 · N271UP · Doug MD11FSDR DJFA2010032Skin · corrodedRT WING DWG WT6792502-2, WT6792510 ZONE B2, LOWER SKIN WS 359.595 AT REAR SPAR CORROSION FOUND ON LOWER SKIN, REMOVED .016 OF MATERIAL MORE CORROSION STILL REMAINS. LOWER WING SKIN WAS REPLACED IAW REPAIR DEFINITION REPORT S-750-0145/08RD.Oct 14, 2010 · N709LX · Cessna 750SDR DALA1026695811Skin Panel · damagedDURING L-CHECK FOUND RIGHT WING FIXED LEADING EDGE SKIN PANEL BULGING AND CRACKED AT OSS 436. REPAIRED PER ERA 486181-14.Oct 14, 2010 · N591NW · Boeing 757351SDR ZZDA2010510Panel · wornRT WING UPPER T/E PANEL AFT OF PYLON HAS O/B AFT ATTACH POINT WORN AND BOTH BOLTS LOOSE. REMOVED TWO BOLTS FOR ACCESS TO REPAIR PER SRM 57-51-02, TRIMMED WORN AREA I/B OF RT WING UPPER T/E PANEL PER REF SRM 57-51-02 REPAIR 1, PERFORMED HFEC AROUND EDGES OF TROct 13, 2010 · N173AT · Boeing 73776NSDR ZZDA2010509Panel · wornLEFT WING UPPER T/E PANEL AFT OF PYLON HAS BOTH O/B AFT ATTACH BOLTS LOOSE AND HOLES AREAS WORN. REMOVE BOLTS AT T/E PANEL UPPER SUPPORT BEAM, TRIMMED DAMAGE AREA SRM 57-51-02 FIG 203 REPAIR 1, NDT NO CRACKS NOTED 51-00-00-FIG 23, FABRICATED SHIM 7075T6 .025 Oct 13, 2010 · N173AT · Boeing 73776NSDR FDEA201010134059Skin · corrodedRT WING UPPER SKIN NEAR WING STA 397 ABOVE FRONT SPAR WITH CORROSION. CORROSION ON RT WING UPPER SKIN NEAR WS 397 REPAIRED IAW EA F-5730-142317. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2010 · N935FD · Boeing 7572T7SDR FDEA201010134058Skin · corrodedRT WING UPPER SKIN NEAR WING STA 481.5 ABOVE FRONT SPAR WITH CORROSION. CORROSION ON RT WING UPPER SKIN NEAR WS 481.5 REPAIRED IAW EA F-5730-142317. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2010 · N935FD · Boeing 7572T7SDR FDEA201010134057Skin · corrodedRT WING UPPER SKIN JUST OTBD OF WING STA 231.5 BETWEEN UPPER STRINGER U13R AND U14R WITH CORROSION. CORROSION ON RT WING UPPER SKIN OTBD OF WS 231.5. REPAIRED IAW EA F-5730-142317. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2010 · N935FD · Boeing 7572T7SDR FDEA201010134056Skin · corrodedRT WING UPPER SKIN BETWEEN WS 623.5 AND WS 652.5 ABOVE REAR SPAR WITH CORROSION. CORROSION ON RT WING UPPER SKIN BETWEEN WS 623.5 AND 652.5 REPAIRED IAW EA 5730-142317. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2010 · N935FD · Boeing 7572T7SDR FDEA201010134055Skin · corrodedRT WING UPPER SKIN NEAR WS 630 ABOVE FRONT SPAR WITH CORROSION. CORROSION ON RT WING UPPER SKIN NEAR WS 630 REPAIRED IAW EA F-5530-142317. (RT WING UPPER SKIN CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2010 · N935FD · Boeing 7572T7SDR FDEA201010134053Skin · corrodedRT WING UPPER SKIN BETWEEN WS 313.5 AND WS 341.5 ABOVE FRONT SPAR WITH CORROSION. CORROSION ON RT WING UPPER SKIN BETWEEN WS 313.5 AND WS 341.5 REPAIRED IAW EA F-5730-142317. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 13, 2010 · N935FD · Boeing 7572T7
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