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 DALA1112879222Rub Strip · corrodedHMV2 LT WING UPPER FUEL PANEL CUT OUT NR 520AT HAS SURFACE CORROSION ON EXTERNAL RIM. REPLACED RUB STRIP PER SRM 57-10-05.SDR ASAA1148810Exhaust Gate · chafedRIGHT I/B EXHAUST GATE UPPER SURFACE CHAFED. TRIMEED DAMAGED SKIN FABRICATED TREATED PRIMED TOP COATED AND INSTALLED REPAIR DOUBLER + FILLERS IAW ASA EA 400 57EA 04516.SDR REXA201100003Skin · dentedBIRD STRIKE CAUSED DOUBLE DENT IN RT WING LEADING EDGE AT WS 50.54-WS 66.20. ONE DENT 3.25"L X 5.0"W X .218" DEEP, SECOND DENT 1.75"L X 1.25"W X .094" DEEP. FERRY FLY A/C FROM OMA TO MEM IAW BOMBARDIER REO 601R-57-41-737A WHERE RT WING LEADING EDGE SKIN P/N SDR IPXA1564266Skin · crackedINSPECTION TYPE:C3, RT WING FIXED L/E, FSS-228, ABOUT 3 FT INBD OF NR2 PYLON, THERE IS A CRACK ABOUT 3" LONG (MARKED). CUT OUT DAMAGED AREA AND CORE, CURED IN CORE, CURED REPAIR PLIES IAW SRM 57-41-01-1A, SRM 51-70-08-0G, ER 10-05875, SRM 51-70-17-0G.SDR C2XA10IA347Skin · crackedDURING MAINTENANCE INSPECTION THE LEFT WING SKIN WAS FOUND TO BE CRACKED AT THE INBOARD SPOILER CENTER HINGE POINT CUTOUT. MAINTENANCE STOP DRILLED THE CRACK, AND PLACED THE AIRCRAFT ON DMI, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. MAINTENANCE PESDR EE4Y1012008Skin · corrodedRT WING, FRONT SPAR AREA STA XFS 129 , L/E LOWER PLATING WITH CORROSION. NOTE: THE CORROSION REQUIRES A MAJOR REPAIR.SDR DALA1107380175Skin · crackedHFEC OPEN HOLE INSP CARRIED OUT AND FOUND CRACK INDICATION ON LT WING PYLON SIDE LOAD FITTING MOST INBD HOLE WITH CRACK INDICATION ON WING SKIN TOP SURFACE AT APPROX 2 O'CLOCK BY PLAIN VIEW AS MARKED. REPAIR ON 01 EA HOLE ACCOMPLISHED IAW PRI 487833-14 AD, RESDR UALA2011010700121Skin · crackedNR 9 SLAT'S OTBD TRACK CUTOUT, HAS A CRACK EXTENDING OUT OF TOP OF CUT-OUT 1.5" LONG. INTERIM REPAIR PER UA EVA 80424 WITH PERMANENT BY 38009 TOTAL TIME. AREA HAS BEEN TAPED. WILL NEED 4 SHIFT SMB FOR LAY-UP REPAIR. TOUGH ACCESS FROM PANEL BEHIND SLAT.SDR USAA2011010390031Access Panel · corrodedMAJOR REPAIR - S4 CHECK - CORROSION ON LEFT WING FUEL ACCESS PANEL 550DB BETWEEN RIB 25 AND RIB 26. REPLACED LEFT WING FUEL ACCESS PANEL 550DB IAW TASK CARD 26C50057092.SDR USAA2011010390030Access Panel · corrodedMAJOR REPAIR - S4 CHECK - CORROSION ON LEFT WING FUEL ACCESS PANEL 540NB, BETWEEN RIB 18 AND RIB 19. REPLACED LEFT WING FUEL ACCESS PANEL 540NB IAW TASK CARD 26C50057092.SDR 2010FA0001272Skin · cracked(EH4R) A CRACK APPROX 1.5 INCHES IN LENGTH, RUNNING FORE AND AFT IN THE LT WING UPPER L/E SKIN AT WS 61.00 WAS DISCOVERED DURING ROUTINE MX INSP. INSP OF INSIDE L/E STRUCTURE FROM WS 49.12 TO WS 79.60 WAS PERFORMED. THE FOLLOWING DISCREPANCIES WERE FOUND: TSDR AALA20110221TUL01Skin · corrodedRIGHT OVERWING WALKWAY HAS SEVERAL AREAS OF LIGHT CORROSION AROUND FASTENERS. REMOVED CORROSION AND FASTENERS AND RE-INSTALLED FASTENERS PER EA B757-57-015152 DATED 02/15/11.SDR ASOA201002019Skin · crackedLT WING OTBD L/E 530KL, SECOND SHROUDS FROM OTBD END HAS A NUTPLATE RIVET PULLING THROUGH SHROUD AT OTBD END & SKIN IS CRACKING. REMOVED 3 EA NUTPLATES FROM SHROUD IAW SRM 51-45-00 AND 51-42-06. INSTALLED 3 EA NUTPLATES ON SHROUD 2 EACH PN MS21061L08K NUTPLSDR E07A20101221001Skin · bentDURING DESCENT, GEAR UP, FLAPS ZERO, AT APPROX 10, 000 FT THE CREW FELT A RUMBLE. DISCONNECTED AUTOPILOT AND FELT A LT ROLL. CONTINUED DESCENT, LANDED UNEVENTFUL. POSTFLIGHT INVESTIGATION REVEALED THE SKIN AFT OF THE LT GEAR WELL FOLDED BACK.SDR FDEA201012204726Skin · crackedRT WING FIXED L/E SLAT TRACK NR12 CUT OUT INBD LOWER FOUND CRACKED. REPAIR CARRIED OUT AT RT WING L/E SLAT TRACK NR12 CUT OUT INBD LOWER AREA IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 45. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 111.SDR FDEA201012204725Skin · crackedLT WING FIXED L/E SLAT TRACK NR12 CUT OUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 201, REV 45. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.SDR FDEA201012204724Access Panel · crackedRT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND 12 EA FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT IAW DWG SG11570004 REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.SDR FDEA201012204723Access Panel · crackedLT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND 04 EACH FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.SDR CA101230010Skin · damagedRIVETS HOLDING LEADING EDGE OF AIRFOIL LOOSENED UP CAUSING AIR PRESSURE TO CATCH SKIN AND PEEL IT BACK BLOCKING AIRFLOW INTO ENGINE. PILOT REPORTED 300LBS TORQUE PRESSURE LOSS.SDR MALA100205Skin · gougedROUTINE-900, RT WING FIXED L/E PANEL AT WS129.00 HAS GOUGE FROM SLAT T/E. RT WING SLAT T/E DAMAGE FROM LOOSE SCREW ON FIXED L/E AT WS 144.75. COMPLIED WITH BLENDING, NDT AN TOUCH UP IAW REO 690-57-40-007.SDR USAA2011011390202Panel · corrodedS4 CHECK- MAJOR REPAIR - CORROSION ON COUNTERSUNK HOLES OF LEFT LOWER WING FUEL PANEL 550AB BETWEEN RIB 22 TO RIB 23 & BETWEEN S8L TO S11L. REPLACED LEFT LOWER WING FUEL PANEL 550AB BETWEEN RIB 22 TO RIB 23 & BETWEEN S8L TO S11L IAW A319 SRM 51-72-11 & CARD 2SDR UIEA2010121100189Skin · damagedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE OTBD RT WS1585 - L/E NOSE EXTERNAL SKIN MEASURING 2.5 IN. L X 1.5 IN. W AND 0.125 IN. DEPTH (REF. FIG 1). DAMAGED AREA FOUND BEYOND THE SRM 57-41-01, FIG 101, DETAIL III ALLOWABLE DAMAGE (GENERAL) LIMITS. (DISPOSSDR REXA201000293Skin Panel · dentedLT WING LOWER SKIN BETWEEN WS 353.00 AND 389.00 HAS 5 DENTS. REPLACED SKIN PANEL IAW BOMBARDIER SERVICES ENGINEERING ORDER 601R-57-19981.SDR FDEA201012054584Skin · crackedRT WING, RIB 9 LWR T/E SKIN PANEL HAS A CRACK APPROX 0.080", NDT VERIFIED CRACK TO BE APPROX .5" INCH LONG. REPAIRED RT WING SKIN IAW WITH DWG NR R57340199 AND EA 6-5730-145507 INSTUCTIONS.SDR FDEA201012054583Skin · crackedLT WING, RIB 9, LOWER T/E SKIN HAS APPR 0.80" INCH CRACK FROM FASTENER HOLE TO T/E OF SKIN. REPAIRED IAW DWG R57340199 AND EA 6-5730-145507 INSTRUCTIONS.SDR UIEA2010120500186Winglet · damagedDURING TAXI, ENROUTE FOR TAKEOFF. ACFT CAME IN CONTACT WITH ANOTHER ACFT ON THE TAXI WAY. THE WINGLET WAS DAMAGED. (REMOVED WINGLET AND DISPATCHED IAW CDL 57-28-1).SDR UHLA2010120400294Skin · crackedMAJOR REPAIR - CRACK IN LT TRAILING EDGE WING SKIN APPROX 45MM O/B OF RIB 10 AND 14MM LONG. REPAIRED TRAILING EDGE WING IAW ETD 2010-170/11370.SDR REXA201000291Skin · dentedDENT (1 L X 0.058 INCH DEEP) WITH A CREASE RT ON WING FIXED LEADING EDGE BETWEEN WS 350.348 - WS 386.348. DAMAGE IS LOCATED 12 INCHES INBOARD OF THE OUTBOARD WINGTIP NAV LENS. FERRY FLIGHT FROM RDU TO MEM WHERE TEMP REPAIR WAS PERFORMED IAW CRJ200 SRM 51-41-3SDR DALA1034436306Plate · damagedDURING LINE CHECK FOUND SPLICE PLATE HAS 6 EA OF ELOGATED RIVET HOLES ILES 330.00 POS FWD AND LOWER RIB HAS 1.5 INCH CRACK. REPAIRED ILES 330.00 POS FWD RIB LOWER RIB AND SPLICE PLATE IAW SRM 51-10-02.SDR DALA1034426306Skin · crackedDURING LINE CHECK FOUND LT WING L/E SKIN HAS CRACK OTBD OF LANDING LIGHT LENS. REPLACED ILES 330.00 POSITION L/E SURFACE SKIN ( LT OTBD LANDING LIGHT OTBD SIDE ) IAW SRM57-41-01, REP-5, DETAIL-2.SDR QXEA2010113000828Access Panel · damagedC2 CHECK - LT WING FUEL PANEL AND CUTOUT 524AT HAVE MINOR FRETTING. REMOVED DAMAGE FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .078" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-250-801. MATERSDR QXEA2010113000827Access Panel · damagedC2 CHECK - LT WING FUEL PANEL AND CUTOUT 524FT HAS FRETTING AND ARCING. REMOVED DAMAGE FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .080" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-250-801. MSDR QXEA2010113000825Access Panel · corrodedC2 CHECK - RT WING FUEL PANEL AND CUTOUT 624FT HAS FRETTING AND ARCING. REMOVED CORROSION FROM FUEL PANEL MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .088" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-25SDR A6WA201140031Panel · chafedLT WING PANEL 599BB HAS CHAFING DAMAGED ON LOWER SIDE. REPAIRED LT WING PANEL 599BB IAW REO 601R-57-60-013.SDR QXEA2010112900810Access Panel · corrodedC2 CHECK - RT WING FUEL PANEL AND CUTOUT 624ET HAS MINOR FRETTING AND ARCING. REMOVED CORROSION FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .084" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-25SDR QXEA2010112900809Access Panel · corrodedC2 CHECK - RT WING FUEL PANEL AND CUTOUT 624DT HAS MINOR FRETTING. REMOVED CORROSION FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .083" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-250-801. MATSDR QXEA2010112900808Access Panel · corrodedC2 CHECK - RT WING FUEL PANEL AND CUTOUT 624CT HAS MINOR FRETTING. REMOVED CORROSION FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .085" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-250-801. MATSDR QXEA2010112900807Access Panel · corrodedC2 CHECK - RT WING FUEL PANEL AND CUTOUT 624BT HAS FRETTING. REMOVED CORROSION FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .084" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-250-801. MATERIAL SDR QXEA2010112900806Access Panel · corrodedC2 CHECK - RT FUEL PANEL AND CUTOUT 626AT HAS FRETTING AND ARCING. BLENDED PANEL 624AT IAW RD 8/4-57-442. REMOVED CORROSION FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .078" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CSDR FDEA201011284505Skin · corrodedRT WING TOP SKIN - AFTER REMOVAL OF OVERWING FILL PORT ADAPTOR, FOUND CORROSION ON SKIN CUTOUT. CORROSION REPAIR CARRIED OUT ON RT WING TOP SKIN IAW EA F-5730-137696 (RT WING TOP SKIN FUEL PORT CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR UALA2010112904388Access Panel · leakingLT UNDER WING TANK ACCESS PLATE 533CB HAS EVIDENCE OF FUEL LEAKAGE. REPLACED SEAL. LEAK CHECKED PANEL, NO LEAKS FOUND.SDR ASMF201012001Access Panel · crackedDURING TRANSIT CHECK, TECH DETECTED A FUEL LEAK IN LT WING MAIN TANK DUE TO A CRACK IN THE FUEL TANK ACCESS DOOR PANEL NR 532DB; SO IT WAS REPLACED AND LEAK TEST WAS PERFORMED IAW MM 28-11-11, ALL CORRECT.SDR QXEA2010113000829Access Panel · damagedC2 CHECK - LT WING FUEL PANEL AND CUTOUT 524BT HAVE MINOR FRETTING AND ARCING. REMOVED DAMAGE FROM WING MATING SURFACE IAW RD 8/4-57-445. MINIMUM REMAINING THICKNESS .073" REF NTM 51-00-02-250-801. CONFIRMED AFFECTED AREA IS CRACK FREE REF NTM 51-00-01-250-SDR FDEA201011254490Access Panel · crackedHFEC OPEN HOLE INSP CARRIED OUT ON LT WING ON PSE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. FOUND 05 EA HOLES WITH CRACK INDICATION. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR ISDR FDEA201011254489Skin · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT ON RT WING ON PSE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. FOUND 15 EA HOLES WITH CRACK INDICATIONS. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MSDR COEA2010112402807Skin · leakingMAJOR REPAIR: RT WING FUEL LEAK AT LOWER SKIN TO RIBS 15-16 JOINT, STRINGERS 1-2 & 6. FASTENERS REMOVED, HOLES INSPECTED AND FILLED WITH SEALANT THEN BLIND BOLTS INSTALL FOLLOWING ATR INSTRUCTIONS. SRAS DO/TS-4176/10...6141 VALIDATED AS PERMANENT REPAIR.SDR FOTR/20198/13818Skin · dentedEVALUATE DENTS 2EA AT LT INBD FORE FLAP LOWER SURFACE 62" FROM INBD EDGE. REMOVED DAMAGE SANDED, CLEANED, AND PREPPED AREA IAW SRM 51-40-20. FABRICATED DOUBLER 6" X 9" FROM 2024-T3 .016, PO 9007046 IAW 51-40-20.CLEANED, SEALED, FINISHED REPAIR IAW SRM 51-40-2SDR USAA2010121793132Access Panel · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON RIGHT WING FUEL PANEL 640RB BETWEEN RIB 21 AND RIB 22, WS 11664 - WS 11198. REPLACED RIGHT WING FUEL PANEL 640RB BETWEEN RIB 21 AND RIB 22, WS 11664 - WS 11198 IAW A320 SRM 57-27-11.SDR USAA2010121793131Access Panel · corrodedSAL - MAJOR REPAIR - S5 CHECK - CORROSION ON RIGHT WING FUEL PANEL 640MB BETWEEN RIB 17 AND RIB 18, WS 9704 - WS 9235. REPLACED RIGHT WING FUEL PANEL 640MB BETWEEN RIB 17 AND RIB 18, WS 9704 - WS 9235 IAW TASK CARD 26C60057091.SDR UALA2010112204298Skin · damagedSKIN HAS IMPACTED AREAS WITH DELAMINATION OF APPROX 1 INCH DIAMETER, WITHOUT PENETRATION. LEFT WING TRAILING EDGE BETWEEN WING TIP AND AILERON: 25 SPOTS IN 11 AREAS. AREAS WITH PERMANENT DEFLECTION AVG DEPTH APPROX .010 INCH AND NO EXPOSED FIBERS NOTED AT TH
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