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 FDEA201612134402Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 768 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR DALA2016121409839Access Panel · corrodedCORROSION ON FUEL ACCESS PLATE 620DT. CORROSION WAS REMOVED ON COUNTERSINK AREA AND SETTLEMENT SURFACE ON ACCESS PLATE 620DT PER SRM 51-10-04 PAR 26, COUNTERSINK AREA WAS MEASURED MAXIMUM COUNTERSINK DIAMETER ALLOWABLE IS 0.660", MAX DIAMETER MEASURED IS 0.705SDR DALA2016121309805Access Panel · corrodedCORROSION ON FUEL ACCESS PANEL 620CT SETTLEMENT AREA AND COUNTERSINK. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01 STEP 5 C(1) CONDITION III.SDR FDEA201612114568Skin · crackedRIGHT WING NR 7 SLAT TRACK CUTOUT O/B CORNER CRACKED. REPAIRED IAW SRM 57-10-00, FIG.104 A , VOL. ISDR SWIA201642970Panel · chafedRIGHT WING PANEL 684EB IS CHAFED. REMOVED AND REPLACED THE PANEL IAW SRM.SDR DALA2016121209787Skin · not reportedDURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT LT WING. ATTENDED WITH ER/A NR 552817-14AD REV ORIGINAL.SDR DALA2016121209786Skin · not reportedDURING NDT INSPECTION, A DISCREPANT AREA WAS FOUND (SEVEN DIFFERENT FASTENERS OF PSE) ON LOWER SKIN REAR SPAR BTW XRS=163 TO 168 AT RT WING. ATTENDED WITH ER/A NR 552817-14AD REV ORIGINAL.SDR SWIA201642969Skin · chafedRIGHT WING PANEL 699BB HAS CHAFED. REPAIRED IAW REO.SDR SWIA201642968Skin · chafedRIGHT WING PANEL 699AB HAS CHAFED. REPAIRED IAW REO.SDR DALA2016120909710Access Door · corrodedCORROSION ON COUNTERSINKS AND SETTLING SURFACE OF FUEL ACCESS PLATES 1335C AND 1311C. FUEL ACCESS DOORS WAS REPLACED PER SRM 51-22-2A PAR 6.SDR DALA2016120709815Skin · damagedLT WING SKIN AT AFT PITCH LOAD FITTING O/B DAMAGED HOLE REPAIRED PER ERA 551291-14.SDR FDEA201612074342Skin · crackedLEFT WING BOTTOM SKIN FOUND CRACKED AT 581AB CUTOUT. REPAIRED IAW EA 6-5730-T0330205 P1 AND DWG R57249152. MAJOR REPAIR IAW GMM 6-2-100.SDR IXXA20170210102Skin · corrodedCORROSION FOUND AT LEFT WING LOWER SKIN INBOARD OF THE OUTBOARD SKATE ANGLE. BLENDED AND REMOVED CORROSION IAW ENGINEERING DOCUMENT 47224REA39.SDR DALA2016120709673Skin · delaminatedRIGHT WING HAD A DELAMINATED OTBD TE PANEL XA=429-434. REPAIRED IAW ERA 551768-14 REV ORIGINAL.SDR FDEA201612064331Skin Splice · crackedRT WING FIXED L/E SKIN SPLICE ANGLE IS CRACKED AT XOS 584. REMOVED AND REPLACED RT WING FIXED L/E SKIN SPLICE ANGLE AT XOS 584 IAW SRM 51-33-01-0G, 51-35-01-0G , 51-31-01-OG.SDR FDEA201612064329Skin Splice · crackedRT WING FIXED L/E SKIN SPLICE ANGLE IS CRACKED AT XOS 584. REMOVED AND REPLACED RT WING FIXED L/E SKIN SPLICE ANGLE AT XOS 584 IAW SRM 51-33-01-0G, 51-35-01-0G, 51-31-01-OG.SDR UIEA2016112200898Seal · wornLT WING FUEL ACCESS PANEL SEAL WORN. REMOVED AND REPLACED THE SEAL IAW AMM 28-11-10-908-001 THROUGH STEP 1.SDR UIEA2016112200899Seal · wornRIGHT WING FUEL ACCESS PANEL WORN. REMOVED AND REPLACED THE ACCESS PANEL SEALS IAW AMM 28-11-10-900-001 THROUGH STEP 1.SDR RAIA2018091250002Skin · crackedRT WING LE NR 3 HAS VERTICAL CRACKS ABOVE THE O/B 2 VORTILONS, ALSO AT BOTTOM OUTBOARD EDGE. REMOVED AND REPLACED RT NR 3 LE A/C STORAGE. A/C REPAIR 8-18-18 A/C NOT YET RELEASED.SDR FDEA201612044323Skin · gougedRT WING LWR SURFACE SKIN AT FR47 FASTENER HOLE "A" GOUGED. REPAIRED HOLE "A" OF FR47 PER EA 6-5710-T0330142 P1.SDR DALA2016120509633Access Panel · corrodedCORROSION ON ACCESS PANEL 640JB ON RT WING. REPLACED ACCESS PANEL 640JB ON RT WINGSDR DALA2016120509632Access Panel · corrodedCORROSION ON ACCESS PANEL 540PB FUEL TANK ON LT WING. REPLACED ACCESS PANEL 540PB ON LT WING.SDR FDEA201612034313Access Panel · puncturedLEFT WING, BOTTOM ACCESS PANEL 541EB HAS A DAMAGED CORNER AND A PUNCTURE. PREPPED AND BONDED THE ACCESS PANEL IAW SRM 57-71-00 VOL 2 PAGE 64 PARA .16 A2.SDR DALA2016120209475Skin · corrodedLEFT HAND WING TRAILING EDGE SPAR UPPER SKIN, BETWEEN STA XRS 383 - XRS 240 CORRODED. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. PERMANENT REPAIR IAW SRM 57-30-01 IAW ERA 551872-14.SDR FDEA201612014303Skin · crackedRIGHT WING UPPER SKIN HAS CRACKS. INSTALLED A REPAIR DOUBLER IAW SRM 57-10-00 FIG 55SDR FDEA201611294285Skin · corrodedRIGHT WING LOWER SKIN HAS CORROSION. REPAIRED IAW EA F-5730-T0329901.SDR DALA2016112609274Skin · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR XRS=163 TO 168 AT LT WING. REPAIRED IAW ER/A NO. 551774-14AD REV. ORIGINAL .SDR DALA2016112609273Skin · damagedDURING NDT INSPECTION A DISCREPANT AREA WAS FOUND ON LOWER SKIN REAR SPAR XRS=163 TO 168 AT RT WING. REPAIRED IAW ER/A NO. 551774-14AD REV. ORIGINAL .SDR DALA2016112509269Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANELS 1303C AND 1409C. THE ACCESS PANELS 1409C AND 1303C WERE REPLACED IAW SRM:51-22-2A.SDR A6WA2016113044604Skin · chafedWING SKIN UNDER THE AFT L OTBD EDGE OF PANEL 193AB IS CHAFEDSDR DALA2016112409261Skin · crackedCRACKED INBD BUTTE DOOR INBD SKIN AT RT WING. REPAIRED IAW ETI-17-16-171 REV. 1 AND ER/A 551772-14 REV. ORIG.SDR FDEA201611214144Skin · crackedDURING HFEC INSPECTION ON RT WING FIXED LEADING EDGE SLAT TRACK NR 10 CUTOUT, AFT INBD CORNER NR 13, FOUND ONE CRACK APPROXIMATELY 0.25IN LONG. REPAIRED IAW SRM 57-40-02 FIGURE 201 REPAIR 7. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR REXA2016111902323Access Panel · chafedACCESS PANEL 684GB IS CHAFED ON THE LEADING EDGE. THE DAMAGE OUT OF LIMITS IAW 57-52-01-101-001-001-A01. A NEW ACCESS PANEL WAS LOCATED AND DRILLED IAW SRM 51-40-11-001-001-A01.SDR DALA2016112008948Access Panel · crackedCRACK ON FUEL ACCESS PLATE 620MB. ACCESS PLATE 620MB WAS REPLACED PER AMM 28-00-00 AND IPC 57-23-01-01.SDR FDEA201611184091Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 664 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611184090Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 767 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174058Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 683 BEADED DOUBLER CRACKED. REPAIRED SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174057Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 669 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174056Doubler · crackedRH WING FIXED LEADING EDGE CAVITY AT STA XOS 638 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174055Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 628 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174054Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 613 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174053Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 563 BEADED DOUBLER CRACKED. REPAIR IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174052Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 553 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174051Doubler · crackedLEFT WING FIXED LEADING EDGE CAVITY AT XOS 620 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201611174050Doubler · crackedRIGHT WING FIXED LEADING EDGE CAVITY AT XOS 738 BEADED DOUBLER CRACKED. REPAIRED IAW SRM 57-40-02-2R, FIGURE 203, REPAIR 15. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR DALA2016111808921Access Panel · delaminatedLEFT WING DELAMINATED FWD BOOST PUMP SECONDARY ACCESS COVER. REPAIRED IAW ER/A 530866-14AD MA REV.ORIGINAL.SDR DALA2016111808917Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL COUNTERSINKS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A COND II.SDR REXA2016111602322Access Panel · chafedACCESS PANEL 684ET IS CHAFED ON THE TOP. REPLACED IAW SRM 51-12-00-001-001-A01, 51-40-11-001-001-A01 AND 51-25-16-001-001-A01.
"SDR REXA2016111502319Access Panel · chafedACCESS PANEL 584GB IS CHAFED. LOCATED, DRILLED AND COUNTERSUNK IAW SRM 51-40-11-001-001-A01.
"SDR KO0R201611150084Skin · crackedCRACK INDICATIONS FOUND ON OUTER WING LOWER SKIN I/B ACCESS PANEL CUTOUT LEFT WING (536AB) IN 16 FASTENER HOLES AT APPROXIMATELY STATION XORS 697.730 STRINGER 36.
Back to JASC 5730