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 DHL2003801046Skin · damagedLT WING CTR L/E UPPER SKIN HAS ELONGATED HOLES BETWEEN STA XOLDI 6.225 AND XS 466.651 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1 AND SRM 57-3-3 FIG 5. REMOVED DAMAGED CTR L/E UPPER SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (7075-T6 AL0.SDR DHL2003801045Skin · damagedLT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 379.000 AND 385.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 3. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2- FIG 38. CLEANSDR DHL2003801055Skin · damagedLT WING CTR L/E UPPER SKIN SURFACE HAS ELONGATED HOLES BETWEEN STA XFS 341.500 AND 347.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED DOUBLER (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLESDR DHL2003801044Skin · damagedLT WING CTR L/E UPPER SKIN HOLES ELONGATED, XFS 335.250 TO XFS 335.250 TO XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 1. FABRICATED DOUBELR (7075-T6 AL0.063) IAW SRM 57-2-1 FIG 38. CLEANED, TREATED AND PRIMED INNER SURFACE IAW SRM 5SDR P5CA0300862Skin · corrodedLEVEL 1 CORROSION STA 1240 LBL 950 APPROX 3.0 X .5. REPAIR PER SRM 57-30-01 REWORK PER 8110-3 PAO-SIN-03-00017F, PAO - SIN - 0700013H.SDR PCA0300847Panel · delaminatedLEFT WING OUTBOARD COVE LP PNL DELAMINATION INOP TRAILING EDGE. REPAIRED PER SRM 51-40-12.SDR PCA0300846Panel · delaminatedLEFT WING TRAILING EDGE FIX PNL DELAMINATION. REPAIRED PER SRM 51-30-02 MM 51-30-02, 57-22-01.SDR PCA0300845Panel · delaminatedRIGHT WING TRAILING EDGE FIXED PNL (DELAMINATION). REPAIRED PER SRM 51-30-02, MM 51-30-02, 57-22-01.SDR A6WA200360011Skin · dentedDENT MAPPING 8 DENT OUT OF LIMITS OF SRM. REPAIR REQUESTED FROM BAE SYSTEMS, REF AVMAX FAX 1538-6080002. (M)SDR TSAA0357061Access Door · corrodedREMOVED CORROSION DAMAGE BY BLENDOUT REPAIR PER GUIDANCE IN SRM 57-30-3, FIGURE 5, DETAL III. APPLIED ALODINE AND TWO COATS OF BMS 10-20, TYPE II TO BLENDOUT LOCATIONS. FILLED DEPRESSION WITH BMS 5-26, TYPE II SEALANT TO RESTORE SURFACE TO ORGINAL CONTOUR. SDR EVAS092011Skin · corrodedDURING C08 CHECK, FOUND CORROSION ON RT WING EXTENTION LOWER SKIN UPPER SURFACE AT ERSS STA 1635. REMOVE THE CORROSION AND PERFORM NDI INSPECTION, ON FURTHER DEFECTS FOUNDSDR P5CA0300824Skin · crackedLEFT WING NR 2 STRUT 11B, SKIN CRACKED. FUEL EMERGENCY DRAIN REPAIRED PER SRM 54-34-03 FIG 23.SDR DHL2003801035Skin · crackedLT INBOARD STUB WING LWR SURFACE DOUBLER WITH 0.500 INCH CRACK IN STA XFS 260.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1A PG 3 FIG 1. REMOVED DAMAGED DOUBLER IAW SRM 51-1-21 PG 1. FABRICATED NEW DOUBLER (7075-T6 AL0.080) IAW SRM 57-2-1A PG 3 SDR UPS03440619Skin · bulgedINSPECTION TYPE:C, RT WING UPPER SURFACE RABBET AREA FOUND BULGED AT WS 1460 ( AFT NO.26 V/C FLAP ). CORR BLEND OUT 0.087 X 2 X 4 INCHES. REMAINING THICKNESS RANGED FROM .050 TO .071 INCH. RHW.UPPER.SKIN.SURFACE.REPAIR.AS PER.RS.R57-25-35006.A .WS.1460.SDR DL73K030348Skin · crackedTHE LT WING UPPER SKIN WAS FOUND WITH A 1.5 INCH CRACK EXTENDING FWD FROM THE AFT EDGE OF THE SKIN AT THE REAR SPAR AT WBL 170. THE CRACK WAS REMOVED WITHA 2 X 1 INCHES CUTOUT IN THE SKIN AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 384859-SDR DHL2003801037Skin · crackedLT WING- LT INBOARD STUB WING UPPER SKIN CRACKED 5.000 INCHES AT STA XS 250.000. REMOVED DAMAGED LT INBOARD STUB WING UPPER SKIN IAW SRM 51-1-21 PG 1 AND SRM 51-1-20D PG 21. FABRICATED NEW SKIN (7075-T6 AL0.063) IAW SRM 57-7-3 PG 11. CLEANED, TREATED AND PRSDR DHL2003801057Skin · damagedLT WING CTR L/E UPPER SKIN HOLES ELONGATED BETWEEN XS 484.895 AND XS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-3-3 PG 12, FIG 4. REMOVED SKIN WITH HOLES ELONGATED IAW SRM 57-3-3 PG 12, FIG 4 AND SRM 51-1-21 PG 1. FABRICATED SDR DHL2003801056Skin · corrodedRT WING CTR L/E UPPER SKIN CORRODED FROM XFS 322.750 TO XFS 341.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 1 FIG 38. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION FROM RT WING CTR L/E UPPER SKIN IAW SRM 51-1-8 PG 17-18. FOUND SDR DHL2003801052Skin · crackedRT WING CTR L/E INNER DOUBLER WITH 0.500 INCH CRACK IN STA XOLDI 6.250. REMOVED INNER DOUBLER CRACKED IAW SRM 51-1-20D PG 9. FABRICATED NEW DOUBLER (2024-T3 AL0.080) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED DOUBLER AND AREA PG 9-10 AND SRM 51-1-2SDR SWIA200311946Panel · crackedRIGHT LOWER WING PLANK AT WS 148.19 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED RIGHT LOWER WING PLANK IAW CRJ REO 601R-57-21-130 REV D AND 601R-57-21-131 REV NC. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-130. NO CRACKS NOTED.SDR UPS03840387Skin · crackedLOWER WING SKIN CRACK OUTBOARD NR 1 ENGINE PYLON STA XW 508. FERRIED TO SAA FOR REPAIR. *S/D* CUT OUT CRACKED AREA ON SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED WING SKIN FILLER, REPAIR FILLER AND DOUBLER IAW 8110-3 APPROVED SAA SK 77SDR ASAA0310254Skin · damagedOKC - DURING D-CHECK, FOUND RIGHT WING LEADING EDGE SKIN AT WING STATION 227 WORN AND CHAFED. REMOVED DAMAGED AND INSTALLED REPAIR PER SRM. (M)SDR ASAA0310230Skin · corrodedOKC - DURING D-CHECK, FOUND TANK SKIN AT WING STATION 117L, STRINGER 9L CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR ANGLE PER SRM. (M)SDR CA030328004Panel · missing(CAN) CAPTAIN DISCOVERED THAT LT LOWER WING FUEL BOOST PUMP PANEL MISSING. SUSPECT PANEL DEPARTED IN FLIGHT. AIRCRAFT OPERATED I.A.W. CDL 57-30-4.SDR ASAA0310170Skin · chafedOKC - DURING D-CHECK, FOUND LEFT WING FIXED LEADING EDGE SKIN AT WING STATION 225-345.14 CHAFFED. REMOVED AND REPLACED SKIN PER SRM. (M)SDR ASAA0240150Skin · chafedPAE - DURING C-CHECK, FOUND LEFT WING INBOARD EXHAUST GATE UPPER SKIN IS CHAFED ON FORWARD OUTBOARD EDGE. REPAIRED IAW SRM. (M)SDR 2003FA0000614Access Panel · leakingFUEL BAY ACCESS PANELS CAUSE A FUEL LEAK WHEN INSTALLED AS SPARES REPLACEMENT. AT ALL FASTENER HOLES ON EACH DOUBLER THERE IS PROTRUSION CAUSED BY THE OLD PANELS DESIGNED WITH A MILLED AREA ON BACK SIDE OF COUNTER SUNK FASTENER HOLES. WHEN ORIGINAL PANEL SCRSDR P5CA0300783Access Panel · brokenGROUND DAMAGE TO RT WING TIP BETWEEN WS 155-25 & WBL 1243-75. TAIL JACK WAS DRAGGED UNDER WING TIP CAUSING DAMAGE TO HEADING EDGE, TRAILING EDGE A FUEL TANK EDGE A FUEL TANK ACCESS PANEL & UNDERSIDE OF WING. PERFORMED DYE PENETRANT CK, FOUND NO CRACKS MATERISDR 2003F00410Access Panel · crackedAT C-CHECK, FOUND CRACK ON RIGHT WING, NR 6 SLAT LOWER ACCESS PANEL NR 6589. FABRICATED NEW PANEL. ALODINED, PRIMED AND INSTALLED NEW ACCESS PANEL AT RIGHT LOWER NR 6 SLAT. (M)SDR 2003F00401Panel · crackedAT C-CHECK, FOUND CRACK ON RIGHT WING, OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD ATTACH BRACKET. FABRICATED BRACKET. TREATED, PRIMED AND INSTALLED BRACKET ON RIGHT WING OUTBOARD TRAILING EDGE WING FIXED PANEL INBOARD. (M)SDR LR7A03030Skin · crackedDURING SCHEDULED C4 INSPECTION PER JOB CARD HC5711 FOUND UPPER SURFACE OWS 173-241 T/E PANELS CRACKED LT AND RT. SKIN PANELS REPLACED IAW LAC MEA 382-57-03-020. NR 2232.SDR GTIA030222Access Panel · crackedFTW - FOUND LEFT WING LOWER FUEL TANK ACCESS PANEL NR 5 HAS CRACK AT FASTENER HOLE, DAMAGED COUNTER SINK. PART REPLACED WITH NEW PANEL. (M)SDR ABXA030114Skin · corrodedDURING ROUTINE MAINTENANCE, CORROSION WAS DISCOVERED ON THE LEFT WING, UPPER PLATING. REPAIRED AREA IAW REA D857-46919.SDR 2003F00493Skin · crackedAT C-CHECK, FOUND CRACK ON LEADING EDGE WING SKIN AT NR 5 OUTBOARD SLAT TRACK. STOP DRILLED CRACK. FABRICATED DOUBLER. ALODINED AND PRIMED AREA REPAIR DOUBLER. INSTALLED AT RIGHT WING NR 5 OUTBOARD SLAT TRAKC LEADING EDGE CUT OUT. (M)SDR GTIA030212Panel · tornFTW - FOUND LEFT WING FUEL PANEL NR 1365C LANDING FUEL STRIP TORN. CUT OUT DAMGAED AREA AT XRS290 IAW EA 57300304. FABRICATED -7 FILLER AND -3 DOUBLER. FABRICATED -5 DOUBLER. INSTALLED -5 DOUBLER. INSTALLED -7 FILLER AND -3 DOUBLER. (M)SDR ABXA030250Skin · crackedHOLE NR 2 ON RIGHT WING AT XFS 515, SHOWED CRACK INDICATION IN SKIN DURING INSPECTION. REPAIRED AREA IAW ABX REA D857-46040MR.SDR ASAA0310089Skin · chafedOKC - DURING D-CHECK, FOUND RIGHT WING LEADING EDGE SKIN AT WING STATION 497-536 CHAFED. REMOVED DAMAGED SECTION OF SKIN AND REPAIRED PER SRM. (M)SDR ASAA0310091Skin · chafedOKC - DURING D-CHECK, FOUND RT WING LEADING EDGE SKIN AT WING STATION 337-367 CHAFED AND DENTED. REMOVED DAMAGED AREA AND REPAIRED SKIN PER SRM. (M)SDR DLM88030212Panel · leakingFUEL LEAK LEFT WING INNER COVER SECOND PANEL FROM FUSELAGE. REPAIRED LEAK.SDR 03FDEA00231Access Panel · damagedLT WING, LOWER ACCESS CUTOUT FOR PANEL 550GB. TWO SCREW HOLES FOR PANEL HAVE DAMAGED EDGES. REMOVED ANCHOR NUTS TO ACCESS DAMAGED HOLES. REMOVED DAMAGED AREA AND REAMED HOLES TO 0.495 AND 0.467. ENSURED CLEANED HOLES ARE CRACK FREE BY HFEC IAW NTM 51-10-01. SDR SWIA200311912Access Panel · corrodedRIGHT WING FUEL PANEL REBATES HAVE CORROSION UNDER PANELS 610AB, 640AB, 640CB, 640DB, 640FB, 650AB. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-57-21-030 REV A, UNDER PANEL 610AB MAX MAT'L LOSS .001, 640AB MAX MAT'L LOSS .007, 640CB MATSDR SWIA200311911Panel · crackedRIGHT LOWER WING PLANK WS 148.019 FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-13 IAW WS 148.019. NO CRACKS NOTED. DAMAGED AREA OF RIGHT LOWER WING PLANK REPAIRED IAW REO 601R-57-21-130 REV D AND REO 601R-57-21-1SDR SWIA200311910Access Panel · corrodedLEFT AND RIGHT WING FUEL PANELS 610AB, 650AB, 640AB, 640CB, 640DB, 640FB, 540CB, 510AB, 540AB, 540DB, 540FB, 550AB HAVE CORROSION. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-57-21-079 REV NC. PANEL 640FB CORROSION BEYOND LIMITS, 650ASDR SWIA200311909Access Panel · corrodedLEFT WING FUEL PANEL REBATES HAVE CORROSION UNDER PANELS 510AB, 540AB, 540CB, 540DB, 540FB, 550AB. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-57-21-030 REV A UNDER PANEL 510AB MAX MAT'L LOSS .002, 540CB MAX MAT'L LOSS .008, 540DB MAX MSDR SWIA200311908Panel · crackedLEFT LOWER WING PLANK WS 148.019 FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA OF LEFT WING PLANK IAW REO 601R-57-21-130 REV D AND REO 601R-57-21-131 REV NC. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-131. NO CRACKS NOTED.SDR 2003UALA00241Skin · dentedLEFT WING #2 SLAT SKIN HAS A SHARP DING. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND REPAIRED SKIN.SDR UPS03840318Skin · corrodedINSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 766.25 TO XFS 772.5. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW SRM 57-2-1 FIG 38.SDR DHL2003604707Skin · corrodedLT INNER WING CENTER EXTENDED L/E UPPER SKIN CORRODED AROUND STA. XFS.341.500 TO XOLDI 6.2246. REMOVED FASTNERS. REMOVED CORROSION FOUND OUT OF LIMITS. TRIMMED OUT CORRODED AREA. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED ANDSDR DHL2003804660Panel · crackedLT WING LOWER SKIN SURFACE HAS 1.5 INCH CRACK AT STA XRS 455.000, BETWEEN S-63L AND S-64-L PERFORMED MAJOR REPAIR IAW EO DHL 030115, ED-3216 , REMOVED FASTNERS IAW IAW SRM 512-1-20D PG. 21 TRIMMED OUTDAMAGED SKIN SEGMENT IAW EO DHL 030115 , ED-3216. FABRICASDR BJNA030220Skin · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON THE LT WING OUTBOARD BOOST PUMP CUTOUT AREA. BLENDED OUT THE CORROSION, HOWEVER THE REMAINING MATERIAL THICKNESS WAS BELOW MINIMUM REQUIRED, AND THE CUT OUT OF MATERIAL WAS BEYOND SRM L
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