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 COEA2017060102804Skin · corrodedRT WING LOWER SKIN EXTERNAL LEVEL 2 CORROSION AT TRAILING EDGE BETWEEN RIBS 13-14 AND BETWEEN RIBS 15-16 ON MID & AFT OUTER PIANO FITTINGS BTW STRINGERS 5-9. TEMPORARY REPAIR IAW SRAS CETS-2322/17...11488 DATED 6/8/2017. PN S57214358200, S57214397201, S5721439SDR DALA2017060204454Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF FUEL ACCESS 620CT AND 520CT. BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR DUE TO THE REDUCED AREA OF THE CONDUCTIVE INTERFACE THEREFORE FUEL ACCESS PLATES WERE REPLACED PER SRM 57-10-01 AND PART NUMBER WAS VERSDR SWAA2017062014521Skin · crackedRIGHT WING NR 8 LEADING EDGE SLAT NOSE SKIN LOWER SURFACE CRACKED AT ACTUATOR RIB. REPAIRED THE SKIN IAW SRM.SDR SWAA2017062014520Skin · crackedRIGHT WING NR 7 LEADING EDGE SLAT NOSE SKIN LOWER SURFACE CRACKED AT ACTUATOR RIB. REPAIRED THE SKIN IAW SRM.SDR AALA201706059063Skin · crackedRIGHT WING LOWER SKIN DRAIN HOLE AT RIB 10 CRACKED. REPAIRED IAW EA 506657A.SDR DALA2017053004442Rub Strip · corrodedCORROSION ON RUB STRIPS ON ACCESS DOOR CUTOUT 520CB, 520DB, 520EB, 520GB, 520JB, 520LB, 520MB, AND 520QB. REPLACED RUB STRIPS.SDR COEA2017052829923Landing · corrodedHEAVY CHECK COE/MAJOR REPAIR: FUEL PANEL 522CT LANDING HAS FRETTING DAMAGE, LEVEL 2. REPAIRED PER SRAS DO/TS-3988/07...4261 DATED 7/4/2017.SDR AALA201706019041Skin · corrodedCORROSION ON LEFT WING TOP SKIN BETWEEN RIBS 19 AND 20. REPAIRED THE WING SKIN IAW SRM 57-21-11-300-006.SDR AALA201706019040Skin · corrodedCORROSION ON RIGHT WING TOP SKIN AT GRAVITY FILL HOLE CUTOUT, BETWEEN RIBS 19 AND 20. REPAIRED THE SKIN IAW SRM 57-21-11-300-006.SDR DALA2017060404447Skin · crackedCRACKED SKIN JUST FORWARD AND OUTBOARD OF FUELING DOOR PANEL. COMPLIED WITH REPAIR.SDR DALA2017052704306Skin · crackedCRACK INDICATION WAS FOUND AT OPEN HOLE, RT LOWER ACCESS DOOR CUTOUT AT XRS 202, FWD STRINGER 15. REPAIRED IAW ETI-88-17-157, REV 1, & ER/A 558111-14AD, REV ORIGINAL.SDR SWAA2017061914426Skin · crackedLT WING FAIRING 542BB INNER SKIN FORWARD OF A DRAIN HOLE CRACKED. REPAIRED SKIN PER EA.SDR FDEA201705251516Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT XOS 654 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR YENA201705250416Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT WING T/E OVER HANG AREA 1,2 AND 3. REPAIRED IAW EO-A32F-57-3701-00 AND EC A17-470-01.SDR YENA201705250415Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT T/E WING SKIN OVERHANG AREA 3 BETWEEN RIBS 15-16 UNDER SMALL FITTING. REPAIRED.SDR YENA201705250414Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT T/E WING SKIN OVERHANG AREA 2 BETWEEN RIBS 14-15, OTBD SPOILER FITING NR 3. REPAIRED.SDR YENA201705250413Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT T/E WING SKIN OVERHANG AREA 1, BETWEEN RIBS 13-14, INBD SPOILER FITTING NR. 3. REPAIRED.SDR YENA201705250412Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT T/E WING SKIN OVERHANG AREA 5, BETWEEN RIBS 16-17. INBD SPOILER FITTING NR 4. REPAIRED IAW EO A32F-57-3698-00 AND EC A17-469-01.SDR YENA201705250411Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT T/E WING SKIN OVERHANG AREA 4 BETWEEN RIB 16-17. CORROSION WAS REPAIRED IAW EO-A32F-57-3698-00, AND EC A17-469-01.SDR YENA201705250410Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE RT T/E WING SKIN OVERHANG AREA 6 BETWEEN RIBS 17-18, OTBD SPOILER FITTING NR 4. CORROSION WAS REPAIRED IAW EO-A32F-57-3698-00, AND EC A17-469-01.SDR JGVR20170526001Skin · corrodedCENTER WING BOND ASSEMBLY HAS CORROSION ON IT'S LAND FOR FUEL PANEL 510BB. FOUND DURING C INSPECTION. REMOVED CORROSION, PERFORMED EDDY CURRENT CHECK OF WING FUEL LAND WITH NO CRACK OR CORROSION INDICATIONS. REPAIRED IN ACCORDANCE WITH CESSNA ENGINEERING MEMO SDR AALA201706169042Access Panel · elongatedELONGATED HOLE ON RIGHT WING ACCESS PANEL 640JB DOOR ASSEMBLY (TYPE 25) BETWEEN STRINGER 8R AND 11R, BETWEEN RIB 14 AND 15. REPLACED ACCESS PANEL IAW AMM 57-27-11-400-002-A AND SRM 57-27-11.SDR IPXA2017060517888Doubler · chafedINSPECTION TYPE: 2C, RT WING FIXED L/E SKIN REPAIR DOUBLER IS CHAFED BETWEEN XOS 1007.12 AND XOS 1038.04. REPAIRED CHAFED RT WING L/E SKIN REPAIR DOUBLER IAW EA 011-5730-01-A6818, AND EO MD11-5730-64438-A.SDR IPXA2017060417867Skin · corrodedINSPECTION TYPE: 2C, LT WING UPPER FWD SKIN HAS CORROSION IN TWO PLACES XORS 197.2 AND XORS 231, BETWEEN STRINGERS 15-17. REPAIRED IAW EA 011-5730-01-A6814, REV I/R, AND EO MD11-5730-64421-A.SDR IPXA2017060117766Doubler · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E BEADED DOUBLER IS CRACKED AT XOS 785. REPAIRED THE DOUBLER IAW SRM 57-40-02, REPAIR 15, FIG 205. MAJOR.SDR DALA2017052004058Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL TANK ACCESS NR 1409C, 1454C, 1456C AND 1466C. ACCESS PANELS WERE REPLACED PER PAR 6 SRM 51-22-2A CONDITION 2.SDR SWIA201743369Panel · chafedCHAFE ON PANEL 684ET. INSTALLED A NEW PANEL IAW SRM.SDR MK1Y20170604003Skin · crackedCRACK FOUND ON THE LT WING SKIN AT AFT PITCH LOAD FITTING, REPAIRED IAW DRAWING 112T7001.SDR GTIA2017051701914Skin · corrodedLEFT WING SKIN AREA RIB 14-1 FOUND CORRODED. 65MM L X 2.22MM. PERFORMED A BLEND OUT REPAIR IAW EO 5721-1716.SDR SCNA20170518062Lock Fastener · pulledRIGHT WING, LEADING EDGE SKIN, JUST INBOARD OF THE PYLON, HAS TWO LOCK FASTENERS PULLING THROUGH THE SKIN. REMOVED AND REPLACED THE LOCK FASTENERS.SDR SCNA20170518061Lock Fastener · pulledLEFT WING, LEADING EDGE SKIN, JUST INBOARD OF THE UPPER PYLON, HAS TWO LOCK FASTENERS PULLING THROUGH THE SKIN. REMOVED AND REPLACED THE LOCK FASTENERS.SDR DALA2017051904027Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PANEL. FOUND TO BE OUT OF LIMITS AND REPLACED IAW SRM 57-00-04.SDR IPXA2017053117738Skin · corrodedINSPECTION TYPE: 1C, LT WING UPPER SURFACE HAS CORROSION AT XORS 280 BETWEEN REAR SPAR AND AUX SPAR. REPAIRED SKIN IAW EA 011-5730-01-A6809 REV I/R, AND EO MD11-5730-64409-A.SDR IPXA2017052717594Skin · crackedINSPECTION TYPE: 1C, LT DROOPED L/E FORWARD OTBD SKIN CHAFED AND CRACKED. REPAIRED THE SKIN IAW SRM 57-40-01, REPAIR 15, FIG 202. MAJOR.SDR DALA2017051804002Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 520CB. REPLACED THE ACCESS PANEL.SDR DALA2017051803996Access Panel · corrodedCORROSION ON SETTLEMENT AREA ON THE FUEL TANK ACCESS PANEL 1379C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A, PAR 6.SDR DALA2017051803994Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL TANK ACCESS PANEL 1361C. THE ACCESS PANEL WAS REPLACED IAW PAR 6, SRM 51-22-2A, CONDITION II.SDR SWIA201743368Panel · chafedPANEL CHAFED. INSTALLED A NEW 584EB PANEL IAW SRM.SDR UIEA2017042600651Skin · delaminatedLEFT WING LE UPPER SKIN ILES 630-662 HAS EDGE DELAMINATION AND CORNER CRACKED. AREA PREPPED AND CLEANED FOR REPAIR IAW SRM 51-70-06-OG-0. CLEANED THE SURFACE IAW AMM 51-21-02. APPLIED TOP COAT IAW AMM 51-24-11.SDR UIEA2017042600652Skin · delaminatedLEFT WING LE UPPER SKIN ILES 693-704 HAS EDGE DELAMINATION AND DAMAGED FASTENER HOLE. AREA PREPPED AND CLEANED FOR REPAIR IAW SRM 51-70-06-0G-0. CLEANED THE SURFACE IAW AMM 51-21-02. APPLIED TOP COAT IAW AMM 51-24-11.SDR UIEA2017042600653Skin · delaminatedRIGHT WING FIXED LE UPPER SKIN HAS EDGE DELAMINATION AND DAMAGED FASTENER HOLES. AREA PREPPED AND CLEANED FOR REPAIR IAW SRM 51-70-06. CLEANED THE SURFACE IAW AMM 51-21-02. APPLIED TOP COAT IAW AMM 51-24-11.SDR UIEA2017042600656Skin · delaminatedRIGHT WING LE UPPER SKIN ILES 630-662 HAS EDGE DELAMINATION AND RIGHT CORNER CRACK. PREPPED AND CLEANED THE AREA AND APPLIED A REPAIR IAW SRM 51-70-06 AND APPLIED TOPCOAT IAW AMM 51-24-22-370-80L.SDR UIEA2017042600659Panel · crackedLEFT WING UPPER SURFACE WS 863, FIXED LEADING EDGE PANEL HAS CRACK GOING FWD TO AFT OF PANEL. REPAIRED THE L/E PANEL IAW SRM 51-70-17-0G-0.SDR IPXA2017053117744Doubler · crackedINSPECTION TYPE: 1C, LEFT WING FIXED L/E INNER BEADED DOUBLER IS CRACKED BETWEEN XORS. 673.3 AND 703.5. REPAIRED THE DOUBLER IAW EA 011-5740-01-A6805 REV I/R, AND EO MD11-5720-64411-A. MAJOR.SDR AALA201705169057Skin · crackedTWO CRACKS ON THE RIGHT WING LOWER SKIN PANEL DRAIN HOLE. REPAIRED THE SKIN PANEL IAW EA 257882A.SDR FDEA201705141411Skin · crackedONE CRACK FOUND APPRROXIMATELY .500 INCH IN LENGTH ON THE LT WING FIXED LEADING EDGE SLAT ACTUATOR ACCESS DOOR FORWARD INBD CORNER AT XOS 490. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 17. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201705141410Skin · crackedONE CRACK FOUND APPRROXIMATELY .250 INCH IN LENGTH ON THE RT WING FIXED LEADING EDGE, FUEL ACCESSS DOOR FORWARD INBD CORNER AT XOS 610. REPAIRED IAW SRM 57-40-01-2R FIGURE 201 REPAIR 18. CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201705141418Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 625 - 627 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15 .THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201705141417Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY BEADED DOUBLER AT XOS 633 - 636 FOUND CRACKED. REPAIRED THE DOUBLER IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR SWAA2022012405257Retainer · crackedLH WING ; FIXED TRAILING EDGE PANEL I/B OF DEFLECTOR RIB TRIANGLE SEAL ATTACH BRACKET CRACKED. MARKED. / REMOVED WEB SEAL BRACKET FROM LEFT WING FIXED TRAILING EDGE INBOARD OF DEFLECTOR RIB IAW SRM 51-40-02-0G-0. ATTACHED SEAL ASSY TO NEW BRACKET AND INSTALLED
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