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 FDEA201211244146Skin · crackedRT WING L/E FOUND LOWER FIXED PANEL NR 11 SLAT TRACK CUT-OUT SKIN EDGE CORNER CRACKED. REPAIRED IAW SRM 57-40-02, FIGURE 201, REPAIR 7, REVISION 51. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211244139Skin · crackedLEFT WING NR 11 L/E SLAT TRACK CUT-OUT FOUND CRACKED AT XOS 720. REPAIRED IAW SRM 57-40-02, FIG 201, REPAIR 7, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR QXEA2012112401425Panel · corrodedLT WING UPPER DRY BAY PANEL 521BT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-425 AND RD 8/4-57-1276. CORROSION FOUND TO BE EXTENSIVE THROUGH COUNTERSINKS REPLACED PANEL WITH NEW.SDR FDEA201211234131Access Panel · corrodedLEFT WING, T/E LOWER ACCESS PANEL NR 541JB CUTOUT FORWARD EDGE LOWER CAP. LOWER SURFACE FOUND CORRODED. CUTOUT FORWARD EDGE LOWER CAP DAMAGED. R & R WITH NEW CAP IAW SRM 51-31-01, REV 51. REPAIR CLASSIFIED AS MAJOR IAW MM 6-2-100, REV 115.SDR DALA1257160183Skin · crackedRT WING AFT PITCH LOAD FITTING FWD TENSION BOLT AREA INBD HOLE FOUND CRACKED. REPAIRED IAW ERA 507540AD, REV ORIG.SDR ASOA2012112602510Skin · crackedCRACK .325" LONG FOUND AND CONFIRMED IAW HFEC INSPECTION AT RT WING BOTTOM AT WS 148.19. REPAIRED IAW EC/TC REO 601R-57-21-130 01 AND REO 601R-57-21-130, REV J.SDR ASOA2012112602509Skin · crackedCRACK .325 LONG FOUND AND CONFIRMED IAW HFEC INSPECTION AT RT WING BOTTOM AT WS 148.19. STOP DRILLED CRACK TO .250" IAW REO 601R-57-21-138, REV A.SDR SWAA2012121710717Skin · crackedCRACK ON EXTERNAL SKIN AT LEADING RIGHT WING WBL 254.00. REPAIRED EXTERNAL SKIN AT LEADING EDGE R/T WING WBL 254.00 IAW B737-300 SRM 51-70-16-0G-0.SDR REXA2012112501523Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLES FOR PANELS 640BB, 640FB, 650GB, AND 650EB CORRODED IN THE NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV J.SDR REXA2012112501522Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLES FOR PANELS 510AB AND 540DB CORRODED IN THE NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV J.SDR DALA12013330936Skin · delaminatedRT WING UPPER T/E PANEL IS DELAMINATED AT APPROX 414 (XRS). REMOVED DAMAGED SKIN AND CORE FROM RT WING FIXED L/E IAW SRM 51-70-2. FABRICATED CORE, BONDED CORE. FABRICATED INTERNAL DOUBLER, SKIN, AND REPAIR DOUBLER IAW SRM 51-70-2D AND ER/A 497176-14MA. APPLIESDR 7AHR20121119008Skin · corrodedBOTTOM OF RT WING BEHIND SLAT HAS CORROSION FORWARD OF SPAR. REMOVED CORROSION AFT LOWER WING AFT OF SLAT FORWARD OF SPAR XRS91 TO XRS69. 3 EA AREAS IAW SRM 51-10-3, PAGE 34. PERFORMED AN ULTRASONIC THICKNESS TEST ON ALL 3 AREAS, OTBD AREA MEASURES OUT OF LSDR 7AHR20121119001Skin · corrodedCORROSION ON RT WING UPPER SKIN FORWARD OF AILERON. REMOVED CORROSION IAW SRM 51-10-03, AFTER CORROSION REMOVAL, AMOUNT OF CORROSION FOUND TO BE OUT OF SRM LIMITS. REMOVED FASTENERS AND DAMAGED MATERIAL IAW SRM 51-70-2. FABRICATED REPAIR FILLERS AND DOUBLERSDR QXEA2012111701394Panel · corrodedRT WING UPPER DRY BAY PANEL 621BT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND IN LIMITS REF RD 8/4-57-425. CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-06-910-801. PANEL FOUND WITHIN LIMITS PER RD 8/4-57-425. APPLIED ALODINE AND PRIMER IAW RD 8/SDR FDEA201211154022Skin · delaminatedRIGHT WING OTBD FIXED L/E OTBD TRAILING SECTION DELAMINATED. REMOVED THE ORIGINAL T/E DOUBLER IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201 FIG 215. INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215.SDR ERAA20120099Skin Panel · crackedCRACK AT RIGHT WING LADDER PLATE AT YW42.0 AND STR 4.SDR FDEA201211144007Skin · delaminatedRT WING OTBD FIXED T/E UPPER SURFACE DELAMINATED. REMOVED THE DAMAGE T/E SKIN IAW SRM 51-40-21 MADE THE REPAIR INSERT & DOUBLER IAW SRM 57-51-12/201, FIG215 WET INSTALLED THE INSERT & DOUBLER IAW SRM 57-51-12/201, FIG 215 SEALED THE EDGE WITH SEALANT IAW SRMSDR SWIA201232217Skin · crackedONE HOLE FOUND CRACKED IN LEFT TRUNNION LOWER WING PLANK SKIN, ONE HOLE AFT OF STRAP. (C-CHECK) REPAIRED IAW REO.SDR FDEA201211133986Skin · delaminatedSKIN DOUBLER AT RT WING TIP UPPER SKIN UNDERNEATH STATIC DISCHARGE DELAMINATION FOUND AROUND THE ORIGINAL DOUBLER AT RT WING TIP UPPER SKIN. UNDERNEATH STATIC DISCHARGE, REPAIRED IAW SRM 57-51-12/201, FIG 215 AND CLASSFIED AS MAJOR IAW GMM6-2-100.SDR 2012F00255Skin · corrodedTHE CENTER WING LOWER SKIN PANEL JUST UNDERNEATH THE FEEDER JET PUMP HAS AN AREA OF PITTING CORROSION APPROX 70 MM BY 70 MM. THE CORROSION WAS REMOVED IAW THE SRM AND EVALUATED IAW 51-10-10 AND FOUND AN AREA 30 MM BY 40 MM WAS FOUND TO BE OUT OF LIMITS.SDR AALA20121116011Skin Panel · corrodedCORROSION ON OVERWING WALKWAY PANEL AROUND FASTENER 16 INCHES FORWARD OF STRINGER 14 AT THE INBOARD SIDE. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.SDR AALA20121116010Skin Panel · corrodedCORROSION ON RIGHT OVERWING WALKWAY 10 INCHES FORWARD OF STRINGER 14 AT INBOARD SIDE OF THE WALKWAY. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.SDR AALA20121116009Skin Panel · corrodedCORROSION ON RIGHT OVERWING WALKWAY AT OUTBOARD CORNER OF THE WALKWAY. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.SDR AALA20121116008Skin Panel · corrodedCORROSION ON THE RIGHT OVERWING WALKWAY APPROXIMATELY 18 INCHES FORWARD OF THE AFT SPAR. REMOVED CORROSION AND REPAIRED FOLLOWING PROCEDURES PER EA B757-57-027077.SDR AALA20121116007Skin Panel · corrodedCORROSION AROUND FASTENER ON OVERWING WALKWAY AREA FORWARD OF AFT SPAR. REMOVED CORROSION AND REPAIRED PER EA B757-57-027077.SDR FDEA201211093922Skin · corrodedRIGHT WING UPPER SKIN L/E, BBL 70.50 TO WS 806.50 CORROSION BLEEDING INTO SEALANT GAP AND ARROUND FASTENERS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, FIG 101, DETAIL A. REPAIRED WING, RT OUTER WING UPPER SKIN AT WS 435 ALONG THE FWD SDR FDEA201211083907Doubler · crackedLEFT WING L/E COMPARTMENT BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02 FIGURE 203, REPAIR 15, TYPE A, REVISION 50. REPAIR CLASSIFIED AS MAJOR GMM REVISION 115.SDR USAA2012111200008Access Panel · corrodedS2 CHECK - LEVEL 2 FRETTING CORROSION ON LOWER LEFT WING FUEL ACCESS PANEL 540JB BETWEEN RIB 14 TO RIB 15 & BETWEEN S8L TO S11L. REPLACED LOWER LEFT WING FUEL ACCESS PANEL 540JB IAW A319 SRM 51-23-06.SDR FDEA201211073905Skin · corrodedLT WING UPPER SKIN L/E WS 369.50 CORROSION BLEEDING INTO SEALANT GAP AND AROUND FASTENERS. REPAIRED WINGS PLATES AND SKIN IAW EA F-5730-163713. MAJOR REPAIR.SDR IXXA2013020700001Skin · damagedRT WING L/E NR 4 STUB WING CORRODED, XW 454 - XW 485. REMOVED FASTENERS FROM REPAIRED AREA IAW SRM 51-1-21. REMOVED CORROSION FROM DAMAGED AREA IAW SRM 51-1-8. TRIMMED OUT DAMAGED AREA IAW DWG ED-5545 NOV 14, 2012. FABRICATED DOUBLER 0.071" FILLER 0.063" BOSDR FDEA201211063876Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND CRACK INDICATIONS AT FASTENER HOLES. REPAIRED IAW SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 50. REPAIR CLASSIFIED AS MASDR FDEA201211063874Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 683.4 AND 713.6. FOUND CRACKED INDICATION AT FASTENER HOLES. FASTENER HOLES CRACKED AT RIGHT WING LOWER SKIN ACCESS DOOR COUTOUT REPAIRED IAW SRM 5SDR AALA20121106012Skin · crackedSTATION 826 CENTER WING SKIN CAP CRACKED. INSTALLED DOUBLER PER SRM 51-70-05 AND EA MD80-57-026832.SDR FDEA201211063883Skin · dentedLT OTBD FLAP BOTTOM SKIN HAS A CLUSTER OF SHARP DENTS JUST INBD OF VANE ROLLER ACCESS PANEL 557DB. INSPECTED DAMAGE AREA FOUND TO BE SERIES OF GOUGE SHARP CREASE DENTS TO INCLUDE ONE LOSE FASTENER - OUT OF LIMITS IAW SRM 57-10-00 PG 162A TO 48, HFEC DENT IAW SDR SWAA2012121710739Skin · crackedLOWER RIGHT WING SKIN CRACKED AT 2 AFT BOOST PUMP. REPAIRED LOWER RIGHT WING SKIN CRACK IAW EA.SDR SWAA2012111509426Skin · crackedSKIN CRACK LOWER RIGHT WING 2.25" IN LENGHT PROPAGATING FROM OUTBOARD FWD CORNER OF NR 2 AFT BOOST PUMP ACCESS HOLE. REPAIRED PER EA 1-357-7626 REPAIR GOOD FOR 2 NON REV FLIGHT CYCLES MX NOTE TRACKING 73846.SDR FDEA201211023812Skin · crackedFASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS= 683.4 AND XORS= 713.6. REPAIRED IAW SRM 57-20-02, FIG 201 REPAIR 5, REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMMSDR FDEA201211023811Skin · crackedFASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN XORS= 683.4 AND XORS=713.6. REPAIRED IAW SRM 57-20-02, FIG 201, REPAIR 5 REV 50. REPAIR CLASSIFIED AS MAJOR IAW GMMSDR XV6A2012110200009Skin Panel · crackedRIGHT LEADING EDGE OUTBOARD (WING RT) LEAKING FUEL. A CRACK IN THE LOWER WING PANEL HAS BEEN FOUND WITH AN APPROX LENGTH OF 30 MM, LOCATED INBOARD RIB 12 AT THE RUN-OUT OF STRINGER 14. REPAIRED CRACK IN RIGHT LEADING EDGE OUTBOARD IAW 328-100-SPR A000104718SDR FDEA201211023817Skin · corrodedLEFT WING UPPER SKIN UPPER SURFACE CORRODED. FOUND TO BE OUT OF LIMITS, WITHIN 1.5 IN. OF ANY CHORD WISE ROW OF FASTNERS IAW SRM 57-20-01, FIG 101, NOTE "A". THIS REPAIR IS A CATEGORY A , MAJOR REPAIR.SDR CA121102001Skin · cracked(CAN) DURING SCHEDULED INSPECTION, CRACKS WERE FOUND ON THE INBOARD LEADING EDGE SKIN THAT DOVE TAILS ONTO THE TOP OF THE MAIN SPAR INSIDE THE CABIN. CRACKS WERE AT FS 91.50 AND WS 23.16. THE CRACK ON THE RIGHT WING IS RUNNING FROM THE AFT EDGE FORWARD ABOUT 3SDR SWAA2012111509427Panel · crackedON POST DOCK WALKAROUND NOTED RIGHT WING FUEL BOOST PUMP PANEL 7403R, NR 2 AFT FUEL BOOST PUMP, STRUCTURE CUTOUT HAS A 2.25" CRACK AT FWD OUTBOARD CORNER REF WING BODY STA 135.5 TO 157.0 MOD. REPAIRED PANEL PER EA.SDR FDEA201211013808Skin · damagedLEFT WING TOP OTBD WINGTIP HAS A LIGHTING STRIKE. FOUND LIGHTENING STRIKE TO BE ON SCREW AND SPLICE STRAP. REMOVED AND REPLACED OUTBOARD RIB LT WING SPLICE STRAP AND SCREW IAW SRM 51-40-02 AND DWG 112N5027. MAJOR REPAIRSDR SWAA2012111509360Panel · crackedRIGHT WING, LEADING EDGE PANEL 621CB, FWD INBD CORNER, FASTENER HOLE CRACKED. REPAIRED FASTENER HOLE IAW SRM.SDR SWIA201232214Skin · corrodedRIGHT WING LOWER PLANK ACCESS 610AB HAS CORROSION AT INBOARD SIDE. (C-CHECK) REPAIRED IAW REO.SDR SWIA201232213Skin · corrodedLEFT WING, LOWER PLANK ACCESS 540DB HAS CORROSION AT INBOARD SIDE. (C-CHECK) REPAIRED IAW REO.SDR SWIA201232212Skin · corrodedRIGHT WING LOWER PLANK ACCESS 650FB HAS CORROSION AT INBOARD AND OUTBOARD SIDES. (C-CHECK) REPAIRED IAW REO.SDR QXEA2012102901357Access Panel · corrodedWING DRY BAY PANEL LANDING 521AT HAS AREAS OF CORROSION. REMOVED CORROSION IAW RD 8/4-57-441. REMOVED GANG CHANNELS IAW SRM 51-42-05-02-01. OPENED DAMAGED HOLES TO .397" IAW RD 8/4-57-879. MEASURED FUEL PANEL LANDING, REMAINING THICKNESS .172" FOUND TO BE WITHSDR EE4Y2012110500328Panel · corrodedFOUND RT WING NR 5 RIB FIXED T/E AND BETWEEN INNER REAR SPAR AFT FACE AND FALSE REAR SPAR FWD FACE LOWER PANEL 3 INNER SURFACE WITH CORROSION. DAMAGE WAS REPAIRED IAW MESSAGE 70568919/006 DATED 30/10/2012 AND TD J1 S2 21517 2012 AND UNDER NRI A1A166 6-58.SDR DALA1506450984Skin · crackedLT UPPER WING SKIN STATION XFS = 533.220 CRACKED. REPAIRED IAW ERA 508040-14, LOG 0623358.
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