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 FDEA201708092155Former · crackedLEFT WING FIXED LEADING EDGE RIB DOUBLER FORMER AT XOS 584 FOUND CRACKED. THE FORMER WAS FABRICATED IAW DRAWING ARB2931, REVISION J. REMOVED AND REPLACED THE FORMER IAW SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR DALA2017081006104Skin · crackedCRACK ON LWR SKIN FROM STA XRS=170 TO XRS=137 AT TRAILING EGDE RT WING (AD). CRACK ON LWR SKIN FROM STA XRS=170 TO XRS=137 AT TRAILING EGDE RT WING WAS REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 5912144 REV AN.SDR SWAA2022012886277Retainer · crackedRIGHT WING; UPPER SHELF PANEL ABOVE PYLON; SEAL RETAINER IS CRACKED ON FORWARD SIDE. / R/R RIGHT WING; UPPER SHELF PANEL ABOVE PYLON; SEAL RETAINER PER SRM 51-40-02SDR DALA2017080906061Access Panel · corrodedCORROSION ON COUNTERSINK AND ELONGATE HOLES ON FUEL TANK ACCES PLATE 141AR. ACCES PLATE WAS REPAIRED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.SDR DALA2017080906060Access Panel · corrodedCORROSION ON COUNTERSINK AND ELONGATE HOLES ON FUEL TANK ACCES PLATE 520PB AND 141AL. ACCESS PLATES 520PB AND 141AL WERE REPAIRED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.SDR DALA2017080906056Skin · crackedCRACK ON LT WING LOWER TRAILING EDGE AT STA XRS=126 APPROX. CRACK ON LT WING LOWER TRAILING EDGE AT STA XRS=126 APPROX WAS REPAIRED PER SRM 57-00-00-2R-1.SDR JGVR20170808001Skin · corrodedFOUND CORROSION ON EXTERNAL AREA OF THE UPPER SKIN NEAR LWS 121 AND AFT SPAR OF THE LEFT WING. REPAIRED BY BLENDING, EDDY CURRENT AND ULTRASOUND INSPECTIONS, AND INSTALLING AN EXTERNAL REPAIR DOUBLER IAW REPAIR DEFINITION S-560-0792/04RD.SDR DALA2017080806035Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA ON FUEL TANK ACCESS PLATE 520DB, 530FT, AND 520CT. ACCESS PLATE 520CT WAS REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION III AND DUE TO EXCESSIVE DAMAGE BY CORROSION ON COUNTERSINK AREAS, ACCESS PLATES 520DB ANDSDR FDEA201708072137Skin · crackedDURING HFEC INSPECTION ON RT WING CORNER 5 OF FIXED L/E SKIN AT FWD I/B CORNER OF SLAT ACTUATOR ACCESS DOOR, CRACK FOUND APPROX 1/2 INCH LENGTH AS MARKED. CARRIED OUT REPAIR AS PER SRM 57-40-01-2R FIGURE 201 REPAIR 17. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-10SDR SWAA2022012733105Plate · crackedLOWER SHELF ATTACH WIGGLE PLATE JUST O/B OF T/E PNL 651DB IS CRACKED. / REMOVED AND REPLACED LOWER SHELF ATTACH WIGGLE PLATE JUST O/B OF T/E PNL 651DB PER SRM 51-40-02.SDR EE4Y2017082204081Skin · crackedDURING INSPECTION, OF THE LT REAR SPAR UPPER CHORD, THERE WERE FOUND THREE CRACKS AT UPPER SKIN T/E AREA, THE AFFECTED LT WING UPPER SKIN AREA WAS REPAIRED.SDR DALA2017080506006Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PANEL : BUSHINGS FABRICATED IAW SRM 57-10-01-2R-2, CONDITION II AND INSTALLED IAW SRM 57-10-01-2R PROCEDURE 2 STEP 5 (B) 3.SDR 2017FA0000341Rivet · looseTHE INBOARD LEADING EDGE RIVETS, LH AND RH, LOOSEN AND WEAR. SOME STEMS AND COLLARS FALL OUT. REPLACED APPROXIMATELY 150 RIVETS, ON EACH WING. THIS ACFT HAS A TOTAL TIME OF 4518 HOURS AND 4149 LANDINGS.SDR SWAA2022012719307None · crackedSUPPLEMENTAL INFORMATION: RT WING SEAL RETAINER ABOVE #2 STRUT AFT POINT CRACKED AT UPPER END / REMOVED RT WING SEAL RETAINER WEB ABOVE #2 STRUT IAW SOPM 20-50-01. 55831C 07AUG17. REMOVED AND REPLACED RT WING SEAL RETAINER ON WEB AND REINSTALLED WEB ABOVE #2 SSDR SWAA2022012719306None · crackedSUPPLEMENTAL INFORMATION: RT WING WIGGLE STRIP LOOSE AND CRACKED AT ORSS 261 / REMOVED AND REPLACED RT WING WIGGLE STRIP AT ORSS261 IAW SRM 51-40-02-0G-0 STEP 4. 56600U 09AUG17SDR IPXA2017082921102Skin · crackedINSPECTION TYPE: 3C, LT WING FIXED L/E SKIN IS CRACKED AT XOS 661.7174. REPAIRED THE SKIN IAW EA 011-5754-01-A6927, REV I/R, AND EO MD11-5750-65438-A. MAJOR.SDR FQAR20170802070Skin · crackedDURING A ROUTINE INSPECTION, THE RIGHT WING SKIN AROUND FUEL TANK VENT PANEL WAS FOUND CRACKED. CRACK WAS APPROX 1.5 INCHES AND EXTENDED FWD OF THE PANEL. THE PANEL AND DOUBLER WERE NOT DAMAGED. THIS AREA HAS A HISTORY OF SEMI-FREQUENT CRACKING ON THIS AIRCRASDR DALA2017080306021Skin · corrodedRIGHT WING UPPER SURFACE, BETWEEN WS 453.5 & 481.5 OVERWING FUEL PORT CUTOUT, DEEP PITTING CORROSION. REMOVED THE CORROSION AND FOUND .160" REMAINING MATERIAL. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, ALLOWABLE DAMAGE 3. REPAIRED IAW ER/A PRI 559862-14, RESDR DALA2017080305882Skin · crackedCRACKS ON 7 HOLES ON LT WING LWR ACCESS DOOR CUTOUT XRS = 189.0 TO 214.0. CRACKS ON 7 HOLES ON LT WING LWR ACCESS DOOR CUTOUT XRS = 189.0 TO 214.0 WERE REPAIRED PER ETI-88-17-199 REV 1 AND ER/A 559533-14AD REV ORIGINAL WITH LOG 0144928.SDR SWAA2022012719294None · crackedSUPPLEMENTAL INFORMATION: LEFT WING UPPER TRAILING EDGE PANEL BETWEEN #5 AND #6 SPOILER PANELS CENTER AFT SEAL RETAINER BRACKET IS CRACKED / REMOVED L/W UPPER T/E PANEL BETWEEN #5 AND #6 SPOILER PANELS CENTER AFT SEAL RETAINER BRACKET THAT WAS CRACKED AND REPLSDR SWAA2022012731048Web · crackedVERTICAL WEB IS CRACKED THAT IS UNDER UPPER T/E PANEL BETWEEN #7 AND #8 SPOILERS. / REMOVED AND REPLACED WEB PER SRM 51-40-02.SDR SWAA2022012785580Bracket · crackedO/B ATTACH BRACKET CRACKED FOR UPPER L/H WING T/E PANEL AT APPROX. RSS STA 280 (MARKED) / REMOVED CRACKED O/B ATTACH BRACKET FOR L/H WING UPPER TE PANEL AT APPROX. RSS STA 280 IAW SOPM 20-50-01. TRANSFERED HOLES TO NEW BRACKET IAW SRM 51-40-05-G-0. REMOVED SEASDR SWAA2022012709301Panel · delaminatedRH WING; LWR LE PNL 621CB IS DELAMINATED AT CORNER. / REPAIRED 621CB EDGE EROSION BE PERMANENTLY SEALING THE ALLOWABLE DAMAGE IAW B737 SRM 57-41-01-1A-1 AND 51-70-08-0G-0 REV 62SDR SWAA2022012709303Panel · delaminatedRH WING; LWR LE PNL 621VB IS DELAMINATED AT CORNER OF PNL. / REPAIRED R/H WING LOWER PANEL 621VB AT CORNER I/A/W SRM 57-41-01-2R-6 PAR 4F-M REV 62.SDR SWAA2022012709305Panel · delaminatedLEFT WING LOWER LEADING EDGE PANEL 521WB HAS DELAM ON FWD OUTBOARD CORNER / PREPPED; CLEANED AND REPAIRED EROSION AT FWD O/B CORNER FLOOR BOARD 521WB IAW B737 SRM 51-70-08 PAR 3 (A-G) REV 62SDR DALA2017092507067Panel · crackedDURING A TURBULENCE INSPECTION OF THE LEFT WING UPPER SURFACE, FOUND A THREE INCH CRACK ON FIXED PANEL AFT OF THE NR 7 SLAT. 12 INCHES INBD OF OTBD EDGE ON AFT EDGE OF PANEL. NO DEFORMATION AROUND CRACKED AREA. REMOVED AND REPAIRED THE PANEL IAW SRM 51-70-0SDR SWIA201743689Skin · dentedRIGHT FORWARD SIDE OF CENTER WING PLANK HAS 9 SMALL DENTS IN AN AREA APROXIMATELY 6" X 8". ALL STEPS COMPLETED OF PERMANENT REPAIR IAW REO AND SRM.SDR DALA2017080205955Ring · corrodedLEFT OVERWING FUELING PORT CUTOUT ADAPTER RING, CORRODED. REPAIRED THE OVERWING FILL PORT CUTOUT IAW SRM 57-20-01, REPAIR 6. REPLACED OVERWING FILL PORT ADAPTER IAW AMM 28-11-04. BOND CHECKED GOOD. LEAK CHECKED GOOD.SDR DALA2017080205861Access Panel · crackedCRACKS ON THE RT WING LOWER ACCESS DOOR CUTOUT XRS 189 TO 214. REPAIRED IAW ETI-88-17-199, REV 1, AND ER/A 559533-14AD, REV ORIGINAL.SDR DALA2017080205860Access Panel · crackedCRACKS ON THE LT WING LOWER ACCESS DOOR CUTOUT XRS 189 TO 214. REPAIRED IAW ETI-88-17-199, REV 1, AND ER/A 559533-14AD, REV ORIGINAL.SDR COEA2017072904816Skin · corrodedHEAVY CHECK COE/MAJOR REPAIR: PANEL 522CT LANDING HAS LEVEL 2 FRETTING CORROSION. REPAIR PER SRAS DO/TS-3018/09. 5261 DATED 8/16/2017.SDR DALA2017081706278Skin · crackedCRACK ON OUTBOARD UPPER CORNER NEXT TO FUEL PANEL. PERMANENT REPAIR IAW SRM 57-20-01.SDR SWIA201743658Skin Panel · chafedRT WING SKIN PANEL 684HT CHAFED. INSTALLED A NEW SKIN PANEL IAW SRM.SDR FDEA201707282066Doubler · crackedLT WING LEADING EDGE CAVITY BEADED DOUBLER AT STA XOS 653 - XOS 659 FOUND CRACKED. BEADED DOUBLER REPAIRED AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201707282065Doubler · crackedLEFT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 698 - 703 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707282064Doubler · crackedRIGHT WING LEADING EDGE CAVITY BEADED DOUBLER AT XOS 626 FOUND CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707282063Skin · crackedDURING HFEC OPEN HOLE INSPECTION OF THE RT WING CORNER NR 2 OF SLAT ANTI -ICE TELESCOPING DUCT CUTOUT, UPPER OTBD CORNER, A CRACK WAS FOUND APPROX. 1/2 INCH IN LENGTH, AT XOS 470. REPAIRED IAW SRM 57-40-01-2R, FIGURE 202, REPAIR 10. REPAIR CLASSIFIED MAJOR SDR FDEA201707282062Skin · crackedDURING HFEC OPEN HOLE INSPECTION ON THE RT WING CORNER NR 5 OF SLAT ACTUATOR ACCESS DOOR, THE FORWARD INBD CORNER WAS FOUND CRACKED APPROX. 1/2 INCH IN LENGTH, AT XOS 490. REPAIRED IAW SRM 57-40-01-2R, FIGURE 201, REPAIR 17. REPAIR CLASSIFIED AS MAJOR IAWSDR FDEA201707282077Skin · damagedRIGHT WING LOWER WING ACCESS PANEL CUTOUT AT XORS 683 HAS ONE DAMAGED HOLE AT THE 6 O'CLOCK POSITION AFT. REPAIRED IAW EA 8-5730-T0334612.SDR MK1Y20170727005Skin · corrodedCORROSION AROUND THE WING UPPER SURFACE FUEL FILL PORT AT WS 785, BETWEEN STRINGERS 15 AND 16.SDR MK1Y20170727004Skin · corrodedCORROSION ON THE FILL PORT SURFACE AT LT WING, WS 798.2, S15-S16.SDR AWKA2017080201Skin · damagedAFTER THE AIRCRAFT TAXIED INTO THE FBO, A FUEL LEAK UNDER THE RIGHT WING WAS NOTED. A SMALL HOLE WAS SEEN UNDER THE WING, INBOARD SECTION. MAINTENANCE WAS CONTRACTED TO INSPECT THE AIRPLANE. ONCE DEFUELED AND FUEL CELL OPENED FOR INSPECTION, CORROSION WAS FOUNSDR DALA2017072805724Access Panel · corrodedCORRODED COUNTERSINKS ON FUEL ACCESS PANEL. THE ACCESS PANEL ARE OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A PAR. 6.SDR DALA2017072805723Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL TANK ACCESS PANEL 1436C. THE ACCESS PANEL FOUND OUT OF LIMITS AND REPLACED IAW SRM 51-22-2A PAR 6.SDR DALA2017072805722Access Panel · corrodedCORROSION ON UPPER SURFACE ON FUEL TANK ACCES PANEL 1307C. THE ACCESS PANEL IS OUT OF LIMITS AND WAS REPLACED IAW SRM 51-22-2A PAR. 6.SDR DALA2017072805730Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENNT AREA AT FUEL ACCESS PLATE 1414C. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A COND. II.SDR FDEA201707252028Access Panel · crackedRIGHT WING LOWER OUTER FUEL ACCESS DOOR ATTACH HOLES HAD CRACK INDICATIONS. REPAIRED IAW SRM 57-20-02-2R, PG 29.SDR FDEA201707252036Doubler · crackedLEFT WING XOS 906 DOUBLER FOUND CRACKED. REPAIRED IAW SRM 57-40-03-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707252035Doubler · crackedRIGHT WING FIXED LEADING EDGE DOUBLER AT XOS 906 FOUND CRACKED. REPAIRED IAW SRM 57-40-03-2R, FIG 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201707252034Doubler · crackedRH WING-FIXED LEADING EDGE DOUBLER AT XOS 545 FOUND CRACKED. REMOVED AND REPLACED IAW SRM 57-31-01-0G. DOUBLER FABRICATED IAW DWG ARB2933, REV AJ. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
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