JASC 5730
Service difficulty reports · 27,269
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 IPXA12M76009Doubler · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR STA XOS 701. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 698 - 703 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)SDR UALA2012101205823Access Panel · leakingFUEL SEEPING JUST RIGHT SIDE PANEL OF NR 6 STICK PANEL. INSTALLED NEW ACCESS PANEL, NO LEAKS NOTED. PARTS ORDERED DUE TO ARRIVE FLT 1673 0100.SDR IPXA12M75957Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XOS 639. REPAIRED RT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 636-648 IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA12M75936Doubler · crackedINSPECTION TYPE: 2C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS 627. REPAIRED BETWEEN XOS 625-629 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)SDR SWAA2012111509446Access Panel · crackedRIGHT WING FUEL ACCESS PANEL 632JB HAS FUEL STICK BASE CRACKED. REPLACED PANEL PER AMM. PANEL TO BE INSTALLED ON TASK CARD # JPANEL-633-CLOSE.SDR KGBR2012101000001Skin · corrodedCORROSION FOUND ON TOP OF CENTER WING SKIN AT CWS 2380 & 2900 LT, IN THE AREAS OF THE ENGINE FAIRING.SDR UALA2012101005751Skin · damagedRIGHT WING FUEL TANK LANDING 640MB HAS 1 EA MISDRILLED FASTENER HOLES. REPAIRED HOLE IAW ECRA 5720-02330 WITHOUT DEVIATION.SDR DALA1250340182Skin · crackedRIGHT WING AFT PITCH LOAD FITTING O/B FWD BOLT HOLE CRACKED. REPAIRED IAW ERA 502734-14._(ERA 502734-14)SDR A6WA20121016558Skin · chafedBUTE DOOR 594PB INNER SKIN CHAFED. CHAFED DOOR IS OUT OF LIMITS .008 RECEIVED DRILLED & LOCATED NEW SKIN IAW CRJ 200 SRM 51-40-11. INSTALLED DOOR IAW CRJ 200 SRM 51-42-06.SDR UALA2012101005772Panel · damagedRT WING OTBD MID INBD DEFLECTION ROLLER GUIDE TRACK BOTTOM PANEL DROPPED. PANEL ATTACHED RIVETS AND BRACKET FOUND BROKEN. INTERIM REPAIRED AND INSPECTION PER ECRA 2700-01549. PANEL INTERIM REPAIR AND SPEED TAPE 2 LAYERS APPLIED. REQUEST RECHECK INTERIM RESDR QXEA2012100501191Access Panel · chafedRT WING FUEL PANEL LANDING AT 624AT HAS CHAFING DAMAGE WITH MINOR CORROSION. BLENDED CORROSION AND CHAFING DAMAGE IAW RD 8/4-57-445. MIN REMAINING THICKNESS NOTED .075, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1SDR QXEA2012100501190Access Panel · chafedRT WING FUEL PANEL LANDING AT 624BT HAS MINOR CHAFING. BLENDED CHAFING DAMAGE IAW RD 8/4-57-445. MIN REMAINING THICKNESS NOTED .078, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801, PT 1 AND 51-00-06-910-801 PT 1. REMAINING THICKNESS FOUND TO BE SDR QXEA2012100501189Access Panel · corrodedRT WING FUEL PANEL LANDING AT 624CT HAS CORROSION. BLENDED CORROSION IAW RD 8/4-57-445. MIN REMAINING THICKNESS NOTED .077, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. REMAINING THICKNESS FOUND TO BE WITHIN LIMISDR QXEA2012100501187Access Panel · corrodedRT WING FUEL PANEL LANDING AT 624ET HAS CORROSION. BLENDED CORROSION IAW RD 8/4-57-445. MIN REMAINING THICKNESS NOTED .071, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. REMAINING THICKNESS FOUND TO BE WITHIN LIMISDR QXEA2012100501159Access Panel · chafedLT WING FUEL PANEL LANDING AT 524FT HAS MINOR CHAFING. BLENDED DAMAGED AREA IAW SRM 57-20-30-02-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MIN REMAINING THICKNESS NOTED .079" REF NTM 51-00-04-910-801 PT 1. REMAINING THICKNESS FOUNDSDR FOTR3391612032012Skin · corrodedLT WING UPPER SURFACE HAS AREA OF CORROSION AT REAR SPAR 35" OTBD OF FUSELAGE BS 1060. REPAIRED ON FAS WO 21197, NR 33916.SDR QXEA2012100401188Access Panel · corrodedRT WING FUEL PANEL LANDING AT 624DT HAS CORROSION. BLENDED CORROSION IAW RD 8/4-57-445. MIN REMAINING THICKNESS NOTED .075, CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. REMAINING THICKNESS FOUND TO BE WITHIN LIMSDR QXEA2012100401158Access Panel · corrodedLT WING FUEL PANEL LANDING AT 525AT HAS CORROSION. REMOVED CORROSION IAW REF SRM 57-20-30-02-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MIN REMAINING THICKNESS NOTED .082" REF NTM 51-00-04-910-801 PT 1. REMAINING THICKNESS FOUND TSDR QXEA2012100301154Access Panel · chafedLT WING FUEL PANEL LANDING AT 524AT HAS CHAFING. BLENDED DAMAGED AREA AS PER PER SRM 57-20-30-02-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MIN REMAINING THICKNESS NOTED .078" REF NTM 51-00-04-910-801 PT 1. REMAINING THICKNESS FOUNSDR QXEA2012100301153Access Panel · chafedLT WING FUEL PANEL LANDING AT 524BT HAS MINOR CHAFING. BLENDED DAMAGED AREA IAW SRM 57-20-30-02-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MIN REMAINING THICKNESS NOTED .080" REF NTM 51-00-04-910-801 PT 1. REMAINING THICKNESS FOUNDSDR QXEA2012100301152Access Panel · damagedLT WING FUEL PANEL LANDING AT 524CT HAS FRETTING DAMAGE. BLENDED DAMAGED AREAS IAW SRM 57-20-30-02-02. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MIN REMAINING THICKNESS NOTED .075" REF NTM 51-00-04-910-801 PT 1. REMAINING THICKNESS FOSDR QXEA2012100301151Access Panel · chafedLT WING FUEL PANEL LANDING AT 524DT HAS MINOR CHAFING. BLENDED DAMAGED AREA IAW SRM 57-20-30-02-01. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801 PT 1. MIN REMAINING THICKNESS NOTED .079" REF NTM 51-00-04-910-801 PT 1. REMAINING THICKNESS FOUNSDR FOTR1215201235711Skin · corrodedRIGHT WING UPPER SKIN AT REAR SPAR EXFOLIATED AT WS 167. REPAIRED.SDR IPXA2M76163Skin · crackedINSPECTION TYPE: 4C, LT WING FIXED L/E SKIN IS CRACKED AT XOS 610 AT FWD. INBD CORNER OF PANEL 519CB. REPAIRED LT WING FIXED L/E SKIN AT STA XOS610, INBD CORNER OF PANEL 519 CB REF STASA EA 011-5730-01-A4341 REV. I/R, UPS EO MD11-5730- 49000-A AND FAA FORM 8SDR IPXA12M76109Skin · chafedINSPECTION TYPE: 4C, LEFT WING FIXED L/E REPAIR DOUBLER AT ANTI-ICE TELESCOPIC DUCT CUT OUT IS CHAFED. REMOVED, FABRICATED AND REPLACED LEFT WING FIXED L/E TELESCOPIC DUCT CUT OUT REPAIR REF SRM 57-40-01, REPAIR 10, FIG 201.SDR IPXA12M76008Skin · crackedINSPECTION TYPE: 4C, LT WING FIXED LE SKIN CRACKED AT WD OB CORNER OF PANEL 518FB. REPAIRED LT WING FIXED L/E SKIN AT FWD OTBD CORNER OF PANEL 518FB REF SRM 57-40-02, REPAIR 7, FIG 202.SDR IPXA12M76006Skin · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E SKIN CRACKED AT NR 14 SLAT TRACK CUT OUT. REPAIRED RT WING FIXED L/E SKIN AT NR 14 SLAT TRACK CUT OUT REF MD11- 57-40-02 REPAIR 7, FIG 202.SDR IPXA12M76001Skin · crackedINSPECTION TYPE:4C, LT WING NR 14 SLAT TRACK CUT OUT IS CRACKED AT OTBD AFT CORNER. REPAIRED LT WING NR 14 SLAT TRACK CUT OUT AT AFT OTBD CORNER REF SRM 57-40-02, REPAIR 7, FIG 201.SDR IPXA12M75997Skin · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E SKIN CRACKED AT INBD FWD CORNER OF PANEL 619CB. REPAIRED RT WING FIXED L/E SKIN AT FWD IB CORNER OF PANEL 619CB REF SRM 57-40-02, REPAIR 7, FIG 202.SDR IPXA12M75995Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS 638-645. REPAIRED RT WING FIXED L/E BEADED DOUBLER AT XFS638-645 REF SRM 57 -40-02, REPAIR 15, FIG 203.SDR IPXA12M75994Doubler · crackedINSPECTION TYPE: 4C, LT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS 669-675. REPAIRED LT WING FIXED L/E BEADED DOUBLER AT XFS 669-675 REF SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA12M75993Doubler · crackedINSPECTION TYPE: 4C, RT WING FIXED L/E BEADED DOUBLER CRACKED BETWEEN XFS669-675. REPAIRED RT WING FIXED L/E BEADED DOUBLER AT XFS669-675 REF SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA12M75880Skin · crackedINSPECTION TYPE:4C, RT WING FIXED L/E SKIN IS CRACKED AT ANTI-ICE TELESCOPIC DUCT CUT-OUT. REPAIRED RT WING FIXED L/E SKIN AT ANTI-ICE TELESCOPIC CUT-OUT IAW SRM 57-40-01, REPAIR 10, FIG 201.SDR FDEA201210023529Access Panel · corrodedRT WING T/E LOWER ACCESS PANEL NR 641JB CUT-OUT FORWARD TEE FITTING, FOUND CORROSION. TEE FITTING REPAIRED IAW EA 1-5710-163502. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.SDR DALA1249810942Skin · wornDURING HMV, WEAR WAS FOUND ON LT WING LOWER SKIN AFT SECTION XRS=118 OF SETTLEMENT FAIRING AREA. BLENDED OUT AREA AND LEAVE AS IS CONDITION IAW ERA 506631-14 REV ORIG.SDR UALA2012100205571Skin · damagedMEASURE THE REMAINING SKIN THICKNESS IN THE BLEND OUT AREAS AND RECORD IT ON THE WING SURFACE. REF AVO ESC120524-5325-1. RIGHT WING REWORKED AREAS: 4 EACH, SKIN THICKNESS MEASURMENTS IN THOUSANDS OF AN INCH: BY LOCATION, WBL 90 & 90 INCHES FROM TRAILING EDSDR UALA2012100305596Skin · corrodedON RIGHT WING PERFORM STEP 1. REMOVE EXISTING FASTENERS LOCATED IN THE CORRODED AREAS. REF AVO ESC120524-5325-1. REMOVED 6EA FASTENERS LOCATED IN CORRODED AREA TOP RIGHT WING. REAMED 6 EA FASTENERS TO 1ST OVER, .324". REAMED 6EA FASTENER HOLES TO 2ND OVERSDR UALA2012092905516Skin · damagedON LEFT WING PERFORM STEP 5. MEASURE REMAINING SKIN THICKNESS IN THE BLEND OUT AREAS AND RECORD IT ON THE WING SURFACE. REF AVO ESC120524-5325-1. BY- 92992 AT REWORK AREAS: WBL 150.5 NORMAL THICKNESS .424 INCH, .016 INCH REMOVED FOR CORROSION. IN REWORK AREASDR UALA2012092905522Skin · damagedLEFT WING TIP DAMAGED AT THE FIXED L/E DUE TO AIRCRAFT DAMAGE THE EDGE OF THE SKIN IS TORN 1.75 INCH AND BENT UP ALONG 4 INCH.SDR GTIA20120928491Skin · corrodedRT WING LOWER SURFACE BETWEEN RIBS 25-&26 HAS CORROSION DAMAGE. PERFORMED PERMANENT BLEND OUT REPAIR OF CORROSION DAMAGE IAW EA 57-20-1219 REV ORIGINAL DATE 9-26-2012.SDR FDEA201209283504Skin · damagedRT WING LOWER SKIN HOLE 'S' BUSHINGS TO BE FABRICATED IAW ORIGINAL RAS INSTRUCTION. RT HOLE 'S' REWORKED IAW JPF STEP 2 IAW SRM 51-40-21. 3 BUSHINGS INSTALLED AT 19.1MM DIA IAW RDAS 70566845-003-2012 INSTRUCTION FOR RT SIDE HOLE NR1.SDR FDEA201209283501Skin · crackedLEFT WING LOWER SKIN HOLE G SHOWS EVIDENCE OF A CRACK INDICATION AND MECHANICAL DAMAGE IN THE MAIN BORE. THIS IS A PREVIOUSLY REWORKED HOLE. HOLE G REWORKED UNTIL MECHANICAL DAMAGE REMOVED AND NO CRACK INDICATION STARTING AT A BORE DIAMETER OF 0.530"/13.462MSDR FDEA201209283500Skin · damagedLEFT WING LOWER SKIN HOLE 'S' SHOWS EVIDENCE OF MECHANICAL DAMAGE FROM STEEL BUSHES THROUGH THE FULL BORE DEPTH. THIS IS A PREVIOUSLY REWORKED HOLE. HOLE 'S' REWORKED UNTIL MECHANICAL DAMAGE REMOVED STARTING AT A BORE DIAMETER OF 0.751"/19.075MM TO FINAL DSDR FDEA201209283497Skin · crackedLEFT WING LOWER SKIN HOLE F SHOWS EVIDENCE OF A CRACK INDICATION. THIS HOLE IS A PREVIOUSLY DIA 0.529 HOLE F REWORKED UNTIL CRACK REMOVED IAW SRM 51-40-30 AND EA 6-5710-162973, PAGE 3. HOLE F FINAL DIAMETER IS 0.561"/14.249MM.SDR ASOA2012102302394Skin · crackedLT WING LOWER WING PLANK CRACKED AT WS 149.58. COMPLIED WITH REO 601R-57-21-130. CRACK INDICATION ON SHIM. R & R SHIM AT WS 148.019 AT LOWER T/E PANEL, SRM 51-42-06. FOUND TO BE SATISFACTORY. MAJOR REPAIRSDR FDEA201209273470Access Panel · crackedRT WING L/E LOWER SURFACE ACCESS PANEL 619AB CUTOUT, FORWARD EDGE FOUND CRACKED AT STA XOS 608. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209273471Skin · crackedRT WING FIXED L/E LOWER SURFACE AT STATION XOS 775 (NR 12 SLAT TRACK LOWER CUTOUT) FOUND CRACKED. REPAIRED AS PER SRM 57-40-02 FIGURE 201 REPAIR 7 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR FDEA201209273469Access Panel · crackedLT WING - L/E LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBD CORNER FOUND CRACKED. REPAIR CARRIED OUT AT LEFT HAND WING LEADING EDGE LOWER SURFACE ACCESS PANEL 519CB CUTOUT INBOARD CORNER AS PER SRM 57-40-02 FIGURE 202 REPAIR 7 REVISION 50. REPAIR CLASSIFIEDSDR UIEA2012100100447Skin · damagedNR 1 FLAP TRACK FAIRING HAS DAMAGE TO THE SKIN, MEASURING 5.375 INCHES LONG, BY 2.5 INCHES WIDE. DAMAGE IS BEYOND THE LIMITS OF SRM 57-53-70, FIG 101 ALLOWABLE DAMAGE 1 AND SRM 51-70-02, FIG 101 ALLOWABLE DAMAGE GENERAL. REPAIRED IAW EO 4457A433.SDR FDEA201209263444Doubler · crackedRT WING REFUELING ACCESS DOOR COMPARTMENT UPPER BEADED DOUBLER CRACKED BETWEEN XOS 640 AND XOS 648. REPAIRED AS PER SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.
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