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 WX0A2024061932081Skin · corroded(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0022: (1042-001A) RH WING TOP SKIN LOWER SURFACE AT OVERHANG TRAILING EDGE, CORROSION FOUND BETWEEN RIB 15 AND RIB16. / RH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA BSDR WX0A2024061932080Skin · corroded(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0035: LH WING TRAILING EDGE OVERHANG, CORROSION FOUND AT UPPER SKIN LOWER SURFACE BETWEEN INBD OF RIB 14 AND RIB 16. / LH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH AREA BTSDR SBOY2024060200417Fastener · crackedAIRCRAFT IS CURRENTLY IN HANGAR FOR A10 CHECK. DURING THE ACCOMPLISHMENT OF ALERT SI: IB777570085(LEFT WING -INSPECTION OF UPPER WING SKIN COMMON TO FASTENERS 0 TO 6 AT WING FIXED TRAILING EDGE), FOUND CRACK ON LH UPPER WING SKIN #5 FASTENER.SDR R61A2024062100290Skin · crackedRH WING FIXED LEADING EDGE SKIN TOP SIDE BET L/E RIB 14-15 FOUND CRACKED. MX REPLACED DOUBLER WITH MANUFACTURED PART IAW ETD2024-0157061 CRACK .500. MAJORSDR VNAA202407100006Panel · wornINITIAL INSPECTION: WEAR ON LEADING EDGE PANEL 622AR, 622BR AND 631AR AND 531AL AT RH/LH WING. WEAR ON LEADING EDGE PANEL 622AR, 622BR AND 631AR AND 531AL AT RH/LH WING WERE REPAIRED PER REO 690-57-41-432 REV- -AND REO 690-57-41-431 REV- -SDR VNAA202407090008Skin · damagedIN REF. TRFKE00C9ELU:REO 690-57-21-456. 560FH PERM REPAIR - TEMPORARY DISPOSITION FOR BLENDED LIGTHNING STRIKE DAMAGE TO LH WING LOWER PLANK BETWEEN WS264.00-WS274.00 AND STR22-STR23 WITHIN 560FH, PERFORM A PERM REPAIR IAW APPROVED PROCEDURES. NOTE: ROTO/SHOT SDR WX0A2024061932084Skin · corroded(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 6000-0005: 33284-001 RH WING TOP SKIN LOWER SURFACE AT OVERHANG TRAILING EDGE, CORROSION FOUND BETWEEN RIB16 AND RIB17 (WMRX 5855.60). / RH WING TOP SKIN PANEL #2 LOWER SURFACESDR WX0A2024061932082Skin · corroded(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0023: 1711-15 LH WING TRAILING EDGE OVERHANG, CORROSION FOUND ON UPPER SKIN LOWER SURFACE BTW RIB 16 TO OUTBD OF RIB 17. / LH WING TOP SKIN PANEL #2 LOWER SURFACE TEOH ARESDR IPXA2024062384287Skin · crackedRT WING, UPPER SURFACE, APPROX RIB 18, HAVE A CRACK ON SKIN. DOT 103-199 INSTALLED REPAIR AS REQUIRED IAW SRM 57-51-12 PARA G FIG 207 RIVETS INSTALLED.SDR A6WA202405288755Winglet · damagedREPAIR TO RIGHT WINGLET TIP STRUCTURE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE FOLLOWING ITEMS REF CRJ200 SRM 51-42-13, 51-40-11, 51-41-00, 51-42-06, 51-42-20, 51-42-13 REV.39. TIP FAIRING PN 600-15110-4; LEADING EDGE PN 600-15111-4; AFT FSDR VNAA202407020002Skin · wornWEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRING 683AB, 686AB, 692AB, 695AB AND 697AB AT RH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-476 REV.SDR VNAA202407020001Skin · wornWEAR ON SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER REO 690-57-21-475 REV.--SDR CALA2024052901604Skin · corrodedLEFT WING TOP AFT PLATE AT RIB 11 FWD OF LH SPOILER #2 HAS EXFOLIATION CORROSION. WING TOP SKIN PANEL 2 COVERED BY THE REPAIR PLATE AND AROUND THE R PART 2A OF THE LATEST REVISION OF ECRA 5721-01495 ON OR BEFORE 447 TOTAL AIRCRAFT FLT HOURS. REPAIR PLATE & ASDR SWAA2024061490020Access Panel · crackedCRACK ACCESS PANEL 642BB PLATE AT RT WING 2024-340198<[01] REPLACED PLATE ON ACCESS PANEL 642BB AT RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02.;[02] REPLACED PLATE ON ACCESS PANEL 642BB AT RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02.SDR AWKA202405290002Skin Panel · corrodedRESUBMIT FROM 27-MAY-24: CORROSION DAMAGE ON THE LH WING LOWER SKIN (P/N 6722172-1) AT ACCESS PANEL LAND 551EB. ***ACCOMPLISHED AEROSPACE QUALITY RESEARCH & DEVELOPMENT (AQRD) ENGINEERING REPAIR ORDER ERO-979707 REV. IR DATED 16-APR-24 "N716XJ LH WING ACCESS PSDR AWKA202405290001Skin Panel · corrodedRESUBMIT FROM 27-MAY-24: CORROSION WAS FOUND ON THE LH WING LOWER FORWARD SKIN (P/N 6722166-1) AT ACCESS PANEL 531AB AND RH WING LOWER FORWARD SKIN (P/N 6722166-2) AT ACCESS PANEL 621BB. ***ACCOMPLISHED FIELD REPAIR FR-750-0016-13486 REV. - DATED 02-APR-24 "FISDR AWKA202405277161Skin · corrodedACCOMPLISHED FR-750-0016-13486 BY REMOVAL OF THE CORRODED FUEL LANDS AT PANEL LOCATIONS 531 AB AND 621 BB. ACCOMPLISHED EDDY CURRENT PER NDTM 6-20-00-02 AND ULTRA SONIC INSPECTION PER NDTM 4-20-10-01, NO REMAINING DEFECTS. LOCATED EXTERNAL DOUBLERS: 531AB LOCASDR SWAA2024061489457Panel · crackedRT WING L/E PANEL 621YB CORNER IS CRACKED (MARKED)<[01] CRACKED CORNER ON RT WING L/E PANEL 621YB WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.SDR DALA2024052405485Skin · damagedSHIP 6700 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 617505-14AD. CORRECTIVE ACTION: REF ERA 617505-14AD. (0357490)SDR FDEA202405230993Skin · corrodedRH WING UPPER SKIN LOWER SURFACE FOUND CORRODED BEHIND REAR SPAR BETWEEN RIB27 AND RIB28 ACCESS FROM 690BB ACCOMPLISHED THE REINFORCING DOUBLER REPAIR AT RH WING UPPER SKIN PANEL NO.3, REAR SPAR, RIB25~29 I.A.W FEDEX EA NO:T6-5730-T0379408 P1, SEQ NO:1260,SDR SWAA2024070190876Skin · wornLEFT WING I/B DEFLECTION CONTROL RIB UPPER TAB IS WORN/HAS LOOSE HARDWARE AT BEAM ATTACH PT. REMOVED DAMAGE TO WITHIN LIMITS FROM UPPER TAB OF DEFLECTION RIB PER SRM 57-51-02-1-1A-1. MAX MATERIAL REMOVED .027. NO DEFECTS NOTED. REMOVED DAMAGE FROM PANEL SDR SWAA2024062589199Bracket · damagedRIGHT WING TRAILING EDGE ACCESS PANEL 651GB I/B AFT BRACKET HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ACTION STEP 1<BR><BR>AUDIT C/W RSDR SWAA2024062401200Access Panel · damagedRIGHT WING TRAILING EDGE ACCESS PANEL 651GB SECOND BRACKET FROM I/B ROD HOLE ELONGATED<[01] REMOVED AND INSTALLED NEW BRACKET AT PANEL # 651GB RIGHT WING TRAILING EDGE AS PER SRM 51-40-02-0G-0 AND AIPC 57-15-00-09.;[02] VERIFIED CORRECTIVE ACTION STEP 1<BR><BRSDR IPXA2024052977775Skin · punctured- PUNCTURE - SKIN, LH WING OUTBD LE LWR FXD PNL 521RB (REPAIR). REMOVE THE DAMAGE MATERIALS AND CLEAN. MEASURE THE DAMAGE AREA (DIAMETER:2", DEPTH:3" PLIES", 9.5" FROM LEADING EDGE, 6" FROM RIGHT HAND). BONDED FIBERGLASS PREPREG REPAIR PLIES WITH FILM ADHESIVESDR IPXA2024052277775Skin · punctured*** SDR FILED OPEN *** FAULT - PUNCTURE - SKIN, LH WING OUTBD LE LWR FXD PNL 521RB (REPAIR) OKAY TO WORKSDR JR2R202405212442Skin · chafedRH WING FIXED LEADING EDGE CHAFED AT #2 PYLONSDR JR2R202405212441Skin · chafedLH WING FIXED LEADING EDGE CHAFED AT #1 PYLONSDR JR2R2024052121037Skin · chafedLH WING FIXED LEADING EDGE CHAFFED AT #1 PYLONSDR SWAA2024060688823Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL 634AB INTERNAL SURFACE HAS CORROSION AROUND 5EA. NUTPLATES.<[01] 01 - REMOVED AND REPLACED PER [AMM 51-00-53-201-NG-01 (CORROSION REMOVAL - MAINTENANCE PRACTICES - AIRFRAME - PERMANENT)];[02] COMPLETE<BR>AUDIT C/WSDR JR2R20240518605Skin · dentedRH WING TIP LOWER SKIN DENT-GOUGE-SCRATCH. REPAIRED.SDR IPXA2024061321868Skin · crackedFIXED LEADING EDGE BETWEEN SLAT #2 AND #3 IS CRACKED. INSTALLED WING LEADING EDGE IAW SRM 51-40-01 WS 565.0 TO WS 681.5SDR IXXA2024060502Skin · gougedR/H WING L/E SKIN JUST OTBD OF THE PYLON HAS 4EA HEAVILY GOUGED AREAS ON THE UPPER SUFACE IN LINE WITH #8 SLAT INBD ROTARY ACTUATOR TIEROD AND 1EA FASTENER MISSING THROUGH SKIN JUST INBD OF THE TELESCOPING TAI DUCT AND 9 DAMAGED FASTENER HOLES. BOTH INBOARD ASDR YENA2024052100767Skin · dentedDURING HEAVY MAINTENANCE: DENT UPPER SURFACE LEADING EDGE BTW RIB 22 AND RIB 23 ON RH WING; REPLACED EXTERNAL SKIN, LOC. LEADING EDGE TO RIB 21 AT RIB 23 RH WING I.A.W A321 SRM 51-42-11, A321 SRM 51-72-11 AND DRAWING D57459076. PERFORMED VISUAL INSPECTION ANDSDR JR2R20240517410Skin · corrodedRH WING FIXED LEADING EDGE CHAFFED AT #2 PYLON. REPAIREDSDR JR2R20240517409Skin · corrodedLH WING FIXED LEADING EDGE CHAFFED AT #1 PYLON. REPAIREDSDR IXXA2024061101Skin · damagedLW UPPER LEADING EDGE SKIN HAS 6 FASTENERS PULLED THRU THE SKIN JUST O/B OF O/B SLAT ROTARY ACTUATORSDR IXXA2024060501Skin · gougedLW LEADING EDGE SKIN IS GOUGED AT OB SIDE AFT OF #6 SLAT, 1.25 INCHES FROM THE INBOARD EDGE, 23 INCHES FROM THE AFT EDGE AND 1 INCH IN WIDTHSDR IXXA2024060505Skin · damagedDURING ROUTINE MAINTENANCE IN GSO, MAINTENANCE DISCOVERED STATIC DISCHARGE DAMAGE TO THE MID TRAILING EDGE OF THE LEFT-HAND WINGLET. THE DAMAGE WAS REMOVED WITH A 0.130-INCH EDGE BLEND PER REF /C/ AND FOUND TO BE BEYOND PUBLISHED LIMITS. THE TRAILING EDGE IS SDR FDEA202405130654Doubler · crackedLEFT WING - LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWARD EDGE DOUBLER AT STATION XOS 547 FOUND CRACK ABOUT 1". LEFT WING LEADING EDGE LOWER ACCESS PANEL CUTOUT FORWARD EDGE AT STATION XOS 547 CRACKED DOUBLER REMOVED AND REPLACED AS PER MD -11 SRM 51-31-0SDR 21GA20240513013Skin · corrodedCORROSION FOUND ON LH WING UPPER SKIN BETWEEN STR U-2 AND U-4 AND SPLICE AND BODY STATION 97.42.SDR 21GA20240513012Skin · corrodedCORROSION BEYOND LIMITS FOUND ON RH WING LOWER SKIN BETWEEN WS 1045.0 & WS 1070.59 AND THE REAR SPAR.SDR IPXA2024062923528Access Panel · crackedL/H WING ACCESS PANEL 577DT HAS A COMPOSITE CRACK ON THE INNER SIDE. DOT 110/01. REPAIRED CRACKED AREA IAW AMM A300 53-15-63/801 PARA C.2.A-F. 08-010 (EA 934) BATCH 4271892.SDR R61A2024051500212Skin · crackedRH WING LOWER SKIN CRACKEDAFT OF FWD SPAR BETWEEN RIBS 16 AND 17, LENGTH 66MM.REPAIRED SKIN IAW ETD2024-170-013274,INSTALLED FILLER,DOUBLER AND TRIPLER. ALSO REF VP-019530-2024 N/R #1 FOR WORK ACCOMPLISHED.SDR DALA2024051405198Access Panel · worn(LOG 0337391) LEFT WING TANK PLATE OPENING 532AB HAS SLIGHT PITTING/WEAR. REPAIRED CORROSION DAMAGE REF B737 SRM 57-20-01-2R PROCEDURE 1.SDR DALA2024051405197Access Panel · worn(LOG 0337385) LEFT WING TANK PLATE OPENING 531AB HAS SLIGHT PITTING/WEAR. REPAIRED CORROSION DAMAGE REF B737 SRM 57-20-01-2R PROCEDURE 1.SDR DALA2024051405196Access Panel · worn(LOG 0337388) LEFT WING TANK PLATE OPENING 531BB HAS SLIGHT PITTING/WEAR. REPAIRED CORROSION DAMAGE REF B737 SRM 57-20-01-2R PROCEDURE 1.SDR SWAA2024061284056Access Panel · crackedCRACK ON FLOAT ACCESS PANEL 632NB AT RT WING 2024-294769<[01] REPLACED FLOAT ON ACCESS PANEL 632NB FUEL TANK RT WING IAW SAFRAN CMM 28-40-11 REV 3 TASK 28-11-000-801-A01 STEP 3.A.(3)(A) AND TASK 28-40-11-400-801-A01 STEP 3.A(3)(E);[02] CORRECTED STEP 1:<BR>REPSDR SWAA2024061284057Access Panel · crackedCRACK ON FLOAT ACCESS PANEL 532NB AT LT WING 2024-294768<[01] REPLACED FLOAT ON ACCESS PANEL 532NB FUEL TANK LT WING IAW SAFRAN CMM 28-40-11 REV 3 TASK 28-11-000-801-A01 STEP 3.A.(3)(A) AND TASK 28-40-11-400-801-A01 STEP 3.A(3)(E);[02] CORRECTED STEP 1:<BR>REPSDR JR2R20240509408Skin · corrodedRH WING FIXED LEADING EDGE AT #2 PYLON CHAFED. REPAIRED.SDR SWAA2024061483908Panel · delaminatedLT WING L/E PANEL 521AAB HAS CORNER THAT IS DELAMINATED (MARKED)<[01] LEFT WING LEADING-EDGE PANEL 521AAB; WITH DELAMINATED CORNER; WAS REPAIRED IAW SRM 51-70-05-2R-6.;[02] VERIFIED CORRECTIVE ACTION #1
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