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 FDEA202301040022Doubler · crackedLEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 745, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 745 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202301040021Doubler · crackedLEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 654, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 654 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202301040020Doubler · crackedLEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 619, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 619 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202301040019Doubler · crackedLEFT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 466, BEADED DOUBLER CRACKED. LEFT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 466 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. SDR FDEA202301040018Doubler · crackedRIGHT WING OTBD FIXED LEADING EDGE COMPARTMENT STATION XOS 695, BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 695 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. RSDR FDEA202301040017Doubler · crackedRIGHT WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 683 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 683 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203.SDR FDEA202301040016Skin · crackedRIGHT WING DROOP LEADING EDGE ASSEMBLEY UPPER SURFACE STATION XDLE 314 CRACKED. RIGHT HAND WING DROOP LEADING EDGE ASSEMBLEY UPPER SURFACE STATION XDLE 314 CRACKED AREA REPAIR CARRIED OUT IAW SRM 57-40-01-2R REPAIR 5 FIGURE 201. REPAIR CLASSIFIED AS MAJOSDR FDEA202301020003Doubler · crackedRIGHT WING, OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 749 BEADED DOUBLER CRACKED. RIGHT HAND WING OUTBOARD FIXED LEADING EDGE COMPARTMENT STATION XOS 749 CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 20SDR FDEA202301020001Skin · crackedLEFT WING, NR 16 SLAT TRACK CUTOUT STATION XOS 1008 CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02-2R, REPAIR 7, FIGURE 201. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR CALA2023010200014Access Panel · missingPDA 3, ON ARRIVAL FOUND ONE LEADING EDGE SLAT LUBRICATION ACCESS PANEL MISSING AT R/H SLAT NO. 8. COMPLIED WITH CDL 57F. INSTALLED LEADING EDGE SLAT LUBRICATION ACCESS PANEL 621VB AT R/H SLAT NO.8.SDR IPXA2023011789997Doubler · crackedINSPECTION TYPE: C3, MAJOR REPAIR. RT WING FIXED L/E BEADED DOUBLER CRACKED AT APPX. STA XOS-635. REMOVED, FABRICATED, REPAIRED THE CRACKED BEADED DOUBLER AT STA XOS-635 IAW SRM 57-40-02 REPAIR 15 FIG 205, REV 69.01. (MAJOR)SDR SWAA2023012686053Panel · crackedLT WING L/E PANEL 521FB I/B FWD CORNER HAS CRACK<[01] IDENTIFIED PANEL 521FB IAW SRM 57-41-01-0I-4 FIGURE 5 ITEM [1] DAMAGE TO THE PANEL IS BEYOND ALLOWABLE LIMITS IAW SRM 57-41-01-1A-1 PARAGRAPH 4.A.(2).(A) AND WILL BE REPAIRED IAW SRM 51-70-05-2R-6 PER SRM 5SDR SIMA20221227001Spar · crackedLH WINGLET CRACKED AT FWD SPAR 1 ATTACH POINT.-C/A-COMPLETE:LH WINGLET REPLACED ON NRTC E949108SDR DALA2022122908475Access Panel · corrodedDURING INSPECTION FOUND CORROSION ON FUEL TANK ACCESS HOLES 531AB, 531BB, 532AB, 532DB, 532EB, 532GB, 532HB, 532KB, 532PB, AND 532QB (CUT-OUT ) AT LH WING LOWER AREA. REPAIRED CORROSION PER B737-900ER SRM 57-20-01-2R.SDR DALA2022122308315Skin · corrodedLEFT WING UPPER SURFACE: PAINT BUBBLING WITH EVIDENCE OF POSSIBLE CORROSION AT TWO LOCATIONS JUST AFT OF #3 SLAT. REMOVED CORROSION AT XRS 317 STR 2 LH WING AND REPAIRED PER ERA 604553-14 REV O, SRM 57-10-01-1A PROCEDURE 1.SDR DALA2022122308314Skin · corrodedLEFT WING, CORROSION FOUND AROUND FUELING CAP. REMOVED CORROSION AT XRS 425 STR 2 LT WING AND REPAIRED IAW ERA 604553-14 REV O. ASSOCIATED ER/A 14-604553.SDR 2023F00016Skin · corrodedCORROSION AT LWR LT WING SKIN SURFACE INSPAR WS 583.SDR DALA2022122708381Skin · crackedCRACKED LWR WING SKIN WS 300 AT LH WING. AREA WAS REPAIRED IAW ER/A 603592-14, REV ORIGINAL, SECTION I.SDR SWAA2023010983277Skin · crackedSKIN IS CRACKED AT PANEL 667AT O/B VORTEX GENERATOR ATTACHED RIVET<[01] LOCATED AND DRILLED NEW PANEL 667AT PER REF SRM 51-40-05-0G-0;[02] VERIFIED STEP 1. OK TO TREAT AND PRIME HOLES.;[03] TREATED AND PRIMED HOLES PER REF AMM 51-21-41-370-802 AND AMM 51-21-72SDR EE4Y2022121916836Skin · corrodedDURING THE STRUCTURAL INSPECTION PER WORK ZL-575-01-1-001 CORROSION ON LH WING TOP SKI PANEL 2 LOWER SURFACE BETWEEN RIB 10 AND RIB 12 WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSDR EE4Y2022121916835Skin · corrodedDURING THE STRUCTURAL INSPECTION PER WORK ZL-575-01-1-001 CORROSION ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 16 AND RIB 20 WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTATCTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR SDR EE4Y2022121916834Skin · corrodedDURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-575-01-1-001 CORROSION ON LH WING TOP SKIN PANEL 2 LOWER SURFACE. BETWEEN RIB 13 AND RIB 16. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRSDR EE4Y2022121916830Skin · crackedDURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-575-01-1-002, ON RH WING TEOH ARE HOLE # 207 WAS FOUND WITH CRACK INDICATION. DUE THE DAMAGE IS BEYOND THE SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED DOSSIER 81140719 WITH RSDR EE4Y2022121916829Skin · corrodedDURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-500-03-1-002, CORROSION AT RH WING TEOH BETWEEN RIB 7 AND RIB 8 WAS FOUND. DUE THE DAMAGE IS BEYOND SRM LIMITS AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONS UNDER DOSSSDR EE4Y2022121916822Skin · corrodedDURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-500-03-1-002, CORROSION AT RH WING TEOH AREAS BETWEEN RIB 13 AND RIB 16 WAS FOUND. THE DAMAE WAS FOUND BEYOND SRM LIMITS. AIRBUS WAS CONTACTED TO REQUEST REPAIR INSTRUCTIONS. AIRBUS PROVIDED REPAIR INSTRUCTIONSDR EE4Y2022121916827Skin · corrodedDURING THE STRUCTURAL INSPECTION PER WORK CARD ZL-500-03-1-002 , IT WAS FOUND AT RH WING TEOH AREAS BETWEEN RIB 10 TO RIB 13 WITH CORROSION. DAMAGED WAS FOUND BEYOND SRM LIMITS AND AIRBUS WAS CONTACTED IN ORDER TO OBTAIN REPAIR INSTRUCTIONS.CORRECTIVE ACTIONSSDR AALA202303076022Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 14. MAINTENANCE REPAIRED SKIN PANEL PER EA 341317.SDR SWIA2023011967129Landing · scratchedSCRATCHES NOTED ON LOWER RT WING ACCESS PANEL LANDING. BLENDED OUT DAMAGE IAW REO 601R-57-21-030 REV L BLEND IS WITHIN LIMITS IAW REO 601R-57-21-030 REV -L.SDR CALA2022121603395Skin · crackedL/H WING LOWER SKIN HAS CRACK AT O/B OF RIB 19 AND FWD OF FUEL. SUPPORT TASK NSA HANGER N/R 5867043 AND NSA EMX N/R 42071. REPAIRED L/W LOWER SKIN O/B OF RIB 19 AND FORWARD OF FUEL PANEL WAS TRANSCRIBED FROM NSA EMX N/R 00092, HANGER N/R 5867043, WORK 12/14/20SDR CALA2022121603394Skin · crackedL/H WING LOWER SKIN HAS CRACK AT O/B OF RIB 19 AND FWD OF FUEL. SUPPORT TASK NSA HANGER N/R 5867043 AND NSA EMX N/R 42071. REPAIRED L/W LOWER SKIN O/B OF RIB 19 AND FORWARD OF FUEL PANEL WAS TRANSCRIBED FROM NSA EMX N/R 00092, HANGER N/R 5867043, WORK 12/14/20SDR DALA2022121508134None · noneSHIP 182 DURING LAST C-CHECK (02JAN2019) AT STAG, ER/A 574076-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 182. CORRECTIVE ACTION: ACCOMPLISH ER/A 574076-14AD REV. A SECTION III EXTERNAL HFEC INSPECTION AT AREA 'A' AND AREA 'B' PRIOR TO 6,000 CYCLES OR 18,000 FSDR SWAA2023013080594Access Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AROUND HOLES LT WING 2022-691624<[01] TOOL USED CALIPER P/N 500-196-30 S/N A21033526 DUE DATE 15 NOV 23;[02] TOOL USED HOT BONDER P/N HCS9200B-AV S/N 18175478 DUE DATE 24/SEP/23.;[03] TOOL USED: SCALE P/N: SPX621 S/N: 834SDR FDEA202212112906Skin · crackedRIGHT FIXED LEADING EDGE SKIN HAS A .250 IN. CRACK AT SLAT TRACK NR 10 CUT OUT AFT INBD CORNER. INSTALLED A REPAIR FILLER AND DOUBLER IAW SRM 57-40-02-2R FIGURE 201. MAJOR REPAIR.SDR SWAA2022121380468Panel · crackedRIGHT WING INBD FIXED TE LOWER PANEL HAS AN 8 INCH CRACK. COMPLIED WITH EA 22-157-03635. ACFT OK TO CONTINUE IAW TLD FOR 2 FERRY FLIGHT CYCLES.SDR SWAA2023010480313Panel · bulgedRT WING LOWER MID SPAN T/E PANEL 661BB HAS BULGING FASTENER HOLES SHOWING CRACKS, VIEWED FROM INNER SKIN. PREPARED PANEL #661BB AT DAMAGED AREA FOR REPAIR IAW SRM 51-70-04-2R-9 PARA 4.C. REPAIRED DAMAGED FASTENER4S HOLES RT WING LOWER MID SPAN T/E PANEL ISDR FDEA202212090101Skin · crackedL/H WING LEADING EDGE SKIN AT SLAT TRACK #15 CUT OUT AFT INBOARD CORNER HAS A .500 IN. CRACK. (MARKED) 0004311346 : SCHRADER SR., STEPHEN D - 15-JAN-2023 01:23 REPAIRED L/H WING LEADING EDGE SKIN AT SLAT TRACK # 15 PER SRM 57-40-02-2R. "MAJOR REPAIR"SDR FDEA202212090025Skin · crackedRIGHT WING LEADING EDGE SKIN AT FUEL ACCESS PANEL FWD INBOARD CORNER HAS A .600 INCH CRACK. INSTALLED REPAIR DOUBLER IAW DWG ARB1232 AND IAW SRM 57-40-02-2R AND SRM 51-31- 01-OG. ORIG SUBMISSION DATE: 1/4/2023SDR FDEA202212090006Skin · wornRT WING: DROOP L/E - DEEP GROOVE WORN THROUGH SKIN ON UPPER, OUTBD SURFACE OF DLE. REPAIRED DAMAGED DLE SKIN IN REFERENCE TO MD11 SRM 57-40-01 FIG 202 REPAIR 15. MAJOR REPAIR. REPAIRED DAMAGED DLE SKIN IAW SRM 57-40-01 FIG 202 REPAIR 15. MAJOR REPAIRSDR FDEA2023010290005Skin · wornRT WING: DROOP L/E - DEEP GROOVE WORN THROUGH SKIN ON UPPER, OUTBD SURFACE OF DLE (MARKED AND DOT 58) REPAIRED DAMAGED DLE SKIN IN REFERENCE TO MD11 SRM 57-40-01 FIG 202 REPAIR 15SDR SWAA2022122980119Plate · crackedCRACK ON CORRUGATE PLATE LOCATED AT LEVEL ORSS 261 TRAILING EDGE AT LT WING 2022-688491<[01] REJECT. ELONGATED HOLE LOWER SURFACE SKIN COUNTERSINK AT LEVEL ORSS 261 TRAILING EDGE AT LT WING (4 EA). FAULT RAISED TTG8Q00GNDKE.;[02] FAULT TTG8Q00GNDKE HAS ALREADYSDR DALA2022121308086Skin · damagedER/A 603439-14, RIGHT WING UPPER SURFACE SKIN BBL 70.5 TO WSTA 220, REAR SPAR TO S14 CORRODED. REPAIRED IAW REF ERA 603439-14.SDR DALA2022121208012Skin · corrodedSHIP 5638 CORROSION ON UPPER SKIN BTW STA WBL 80 TO WBL 132 AT AND STRINGER U-13 TO U-14 FRONT SPAR RH WING (RH-AD). CORRECTIVE ACTION: SUMMARY OF NRC00190: UPPER SKIN BTW STA BBL 70.5 TO WSTA 220, REAR SPAR TO S-14 RH WING (RH-AD) WAS REPAIRED PERMANENTLY PERSDR SWAA2022122979795Plate · crackedCRACK ON CORRUGATE PLATE LOCATED AT LEVEL ORSS 269 TRAILING EDGE AT RT WING 2022-688466<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 269 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 115A2001 SHEET : 18 REV :? SEE INDIVIDUSDR SWAA2022122979781Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL IRSS 229 AT LT WING 2022-688437<[01] REPLACED CORRUGATED PLATE AND FASTENERS ON TRAILING EDGE LOCATED AT LEVEL IRSS 229 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9.SEE STEP SIGNOFF BELOW;[02] CERTIFIED WORKSDR SWAA2022121579831Skin · chafedLEFT WING LOWER SKIN IS CHAFED UNDER NR 1 ENGINE PYLON FAIRING SEAL. DUE TO MISSING RUBSTRIP FROM APPROXIMATELY STRINGER 9 SEAM TO 20 INCHES FORWARD OF SEAM; INBOARD SIDE.SDR 2024FA0000120Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWSDR FDEA2023012360150Skin · crackedLEFT WING, CRACK ON WING LEADING EDGE AT FWD I/B CORNER OF FUELING PANEL. REPAIRED LEFT WING, LEADING EDGE CUT OUT CORNER AT FWD I/B OF FUELING PANEL REF MD11 SRM 57-40-01-2R REPAIR 18 FIGURE. 201 MAJOR REPAIR.SDR FDEA202212062952Skin · crackedLEFT WING, CRACK ON WING LEADING EDGE AT FWD I/B CORNER OF FUELING PANEL. REMOVED DAMAGED AND INSTALLED NEW DOUBLER AND FILLER AT L/H WING LEADING EDGE SKIN AT SLAT TRACK #11 IAW SRM 57-40-02-2R, REPAIR 7, FIG 201, SHEET 1.SDR CALA2022120703309Skin · corrodedL/H LOWER WING SKIN O/B OF ACCESS PANEL 534BB HAS CORROSION. SUPPORT TASK NSA EMX N/R 00091. REMOVED CORROSION FROM L/W LOWER WING SKIN O/B OF ACCESS PANEL ACCOMPLISHED CIR C/W. DATA WAS TRANSCRIBED FROM NSA EMX N/R 534BB IAW B37-80 SRM 57-20-01 AND B737-800 SSDR FDEA2023012350149Skin · corrodedRH WING UPPER SURFACE - APPROX XORS 417 AT REAR SPAR - FILLER BULGING. BLENDED AND REMOVED CORROSION IAW SRM 51-21-01-0G, APPLIED REPAIR IAW EA# 1-5710-T0372292 "WING - BASIC WING STRUCTURE - RT WING REAR SPAR UPPER CAP AFT LEG STA. XORS 412 TO XORS 420
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