JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 ABXA020060Fitting · corrodedFORWARD CARGO AT STA. 70, STRING 25 LEFT, LONGERON END FITTING WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-20D AND 51-3-0.SDR ABXA010910Fitting · rustedSTEEL BEAM ABOVE THE RIGHT CLEARVIEW WAS RUSTED ON THE AFT END, BOTH INSIDE AND OUTSIDE OF BEAM. REPLACED BEAM IAW DC-9 SRM 51-30-1 AND 51-30-5.SDR ABXA010896Fitting · crackedEMPENNAGE INTERIOR LONGERON 17 LEFT, END FITTING WAS CRACKED AT F.S. 1769. REPLACED END FITTING IAW DC-8 SRM 51-1-21, 51-3-2 AND 51-1-20D.SDR ABXA010894Fitting · crackedEMPENNAGE INTERIOR LONGERON 17 RIGHT, WAS CRACKED AT F.S. 1769. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-20D.SDR ABXA020051Skin · corrodedAFT CARGO, FORWARD BULKHEAD, F.S. 1065, LONGERON 37 LEFT, AT DRAIN VALVE WAS CORRODED. REPAIRED AREA IAW REA B653-43879.SDR C2XA02TY085Skin · nickedTYS During a scheduled inspection the L/H #1 passenger window frame was found to be nicked. Maintenance accomplished a blend out repair which included a NDT inspection IAW EMB GST#1393/02, EMB-145 M.M. 56-20-00, CPM 51-21-04, 51-21-05, and 51-21-06. The reSDR C2XA02TY084Skin · nickedTYS During a scheduled inspection the #1 right hand passenger window frame was found to be damaged (nicked). Maintenance accomplished a blend out repair which included a NDT inspection IAW EMB GST#1392/02, EMB-145 M.M. 56-20-00, CPM 51-21-04, 51-21-05 and 5SDR 2002UALA00828Seat Track · crackedLH OB SEAT TRACK CRACKED AT OB FASTENER HOLE STATION 1200. MAJOR REPAIR ACCOMPLISHED.SPLICED IN NEW SEAT TRACK SECTION.SDR COMA0260300Fitting · crackedTHE FLOOR SUPPORT FITTING AT FS460, RBL9 WAS CRACKED.REMOVED THE CRACKED FITTING AND INSTALLED A NEW FITTING I/A/W WVAC EO 601R-53-3182.SDR COMA0260299Post · crackedTHE BOTTOM FLANGE OF VERTICAL POST WAS CRACKED AT FS559 AT RBL9.REMOVED THE CRACKED FLANGE AND FABRICATED AND INSTALLED A REPAIR ANGLE I/A/W REO 601R-53-41-057.SDR COMA0260298Intercostal · crackedTHE UNDER FLOOR SUPPORT INTERCOSTALS HAD CRACKED ATTACH FLANGES AT FS484, RBL36 AND LBL36.CUT OFF THE CRACKED FLANGE, FABRICATED AND INSTALLED A REPAIR ANGLE I/A/W WVAC EO 601R-53-3181.SDR ASO2002F00005Stringer · corrodedDURING C CHECK INSPECTION , STRINGER 18 LEFT WAS FOUND CORRODED BETWEEN FRAMES 16 AND STA 6653.1. THE STRINGER SPLICE AT FRAME 16 WAS ALSO FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED STRINGER AND STRINGER SPLICE IAW SRM.SDR ASO2002F00002Beam · crackedDURING (C) CHECK, INSPECTION WHILE COMPLYING WITH VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, THE LEFT SIDE WAS FOUND TO HAVE A CRACK. MAINTENANCE PERFORMED A TEMPORARY REPAIR. THIS REPAIR IS VALID FOR UP TO ONE YEAR FROM DATE OF INCORPORATION.SDR DHL2002807569LongeronAFT FUESLAGE INTERIOR LONG 17R CRACKED AT STA 776.000.REMOVED CRACKED LONGERON PER SRM 51-120D PG 21.CLEANED TREATED AND PRIMED AREA PER SRM 51-1-8B.INSTALLED NEW LONGERON PER SRM 51-120D PG 9.SDR DHL2002807567FittingAFT FUESLAGE INTERIOR FITTING CRACKED 2 IN AT STA 1776.000 L-17 R.REMOVED CRACKED FITTING PER SRM 51-1-20D PG 21.CLEANED TERATED AND PRIMED PER SRM 51-1-8B.INSTALLED NEW FITTING PER SRM 51-1-20 PG 9SDR ABXA010840Rib · crackedF.S. 870, RIGHT WHEEL WELL, LOWER OUTBOARD RIB REPAIR WAS CRACKED. FABBED AND INSTALLED NEW REPAIR, AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-20D AND ABX DWG 5616306.SDR ABXA010838Spar Cap · corrodedF.S. 857, BUTT LINE 54 RIGHT, 16" BELOW THE RIGHT MAIN LANDING GEAR WHEEL WELL CEILING, FORWARD BULKHEAD SKIN WAS CORRODED. FABRICATED REPAIR DOUBLER AND SHIM IAW REA D857-43109MR. INSTALLED PARTS AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D AND REA D857-43SDR ABXA010837Fitting · crackedFORWARD CARGO AT F.S. 350, BETWEEN LONGERON 36 - 35 LEFT, 'Z' FITTING WAS CRACKED. REPLACED 'Z' FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 51-1-20D, 51-3-2 AND 53-2-0.SDR ABXA010836Fitting · corrodedFORWARD CARGO AT F.S. 330, 'T' BOLT LATCH ATTACH FITTING WAS CORRODED BETWEEN LONGERON 33 RIGHT. REMOVED AND REPLACED BACKUP FITTING IAW DC-8 MM.SDR C2XA02SH006Cowling · crackedSHV - DURING C-CHECK INSPECTION, THE LOWER RIGHT HAND APU COWLING MOUNT OPENING WAS FOUNDS TO BE CRACKED. MAINTENANCE STOP DRILLED THE CRACK, AND INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA IN ACCORDANCE WITH EMB-145 SRM 51-40-02, AND THE AIRCRAFT WAS APPRSDR COMA0260251Doubler · crackedR/H F.S. 718.00 FRAME AND DOUBLER ARE CRACKED.REMOVED CRACKED FRAME AND DOUBLER R/H F.S. 718.00 AND INSTALLED NEW FRAME AND DOUBLER I/A/W CANADAIR REO 601R-53-61-193.SDR COMA0260242Beam · crackedLEFT ENGINE SUPPORT BEAM CRACKED.PERFORMED REPAIR TO LEFT ENGINE SUPPORT BEAM I/A/W BOMBARDIER REO 601R-53-61-366 REVC.SDR ABXA020092Shear Tie · corrodedCORRODED SHEAR TIE AT STATION 720 BETWEEN STRINGERS 37 RIGHT - 37 LEFT. REPLACED SHEAR TIE IAW B767 AMM.SDR ABXA020091Shear Tie · corrodedDEEP CORROSION ON SHEAR TIE AT STATION 764 BETWEEN STRINGERS 36 - 37. REPLACED SHEAR TIE IAW B767 AMM.SDR ABXA020088Shear Tie · corrodedDEEP CORROSION ON SHEAR TIES AT STATION 742, BETWEEN STRINGERS 36 LEFT - 39 RIGHT. REPLACED SHEAR TIES INAW B767 AMM.SDR COMA0260232Floor Support · crackedTHE FLOOR MEMBER AT FS 280.0 WAS CRACKED 3/4" TO THE RIGHT OF THE FLOOR SUPPORT AT RBL9.TRIMMED OUT THE DAMAGED AREA AND FABRICATED AND INSTALLED REPAIR PARTS I/A/W WVAC EO 601R-53-3098A.SDR COMA0260231Beam · elongatedTHE FOUR FASTENER HOLES AT FS 333 AND RBL9 THAT ARE COMMON TO THE FLOORBEAM AND THE TRANSVERSE BEAM ARE ELONGATED.THE DAMAGED AREA WAS CUT OUT AND REPAIR PARTS WERE FABRICATED AND INSTALLED I/A/W WVAC EO 601R-53-3097C.SDR ABXA010842FittingRIGHT LOWER CUSP AT F.S. 6700, LONGERON 20 RIGHT, HAD POPPED RIVET HEADS FROM CORROSION BULGE. CUTOUT DAMAGED AREA AND INSTALLED NEW DOUBLER AND FILLER, AND REPAIRED AREA IAW DC-8 SRM 51-3-0, 53-2-0, 51-1-20D, 53-3-1 AND 51-1-8.SDR ABXA010815Control Column · crackedCAPTAIN'S CONTROL COLUMN SHOWED CRACK INDICATIOIN AND WAS BLENDED BEYOND LIMITS. REPLACED CAPTAIN'S CONTROL COLUMN IAW DC-9 SRM 51-30-1 AND 51-30-2.SDR ABXA010832Fitting · corrodedSURFACE CORROSION FOUND IN CARGO DOOR TORQUE BOX AT STA. 345, LONGERON 35 RIGHT, LOWER CARGO COMPARTMENT. REPLACED 'Z' FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-24, REA D853-43-83MR AND REA D853-43076MR.SDR ABXA010833Doubler · corrodedAFT CARGO, LONGERON 32 RIGHT, B/S 1200, WAS CORRODED. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21 AND REA D853-43071MR.SDR ABXA010789Seat Track · crackedFORWARD CARGO AT F.S. 340 - 360, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-8 SRM 51-1-8, 51-3-0, 51-1-21 AND ZANTOP DWG. #86302.SDR ABXA010788Fitting · crackedFORWARD CARGO AT F.S. 200 - 220, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REPLACED FITTING IAW DC-8 SRM 51-1-20D.SDR ABXA010787Frame · crackedFORWARD CARGO AT F.S. 180, ABOVE LONGERON 36 FRAME, UPPER CHORD WAS CRACKED AND BENT. REPAIRED AREA IAW DC-8 SRM STD-5310-002 AND SRM 51-1-8.SDR ABXA010786Seat Track · crackedFORWARD CARGO AT F.S. 580 - 600, LEFT BUTT LINE 50, SEAT TRACK WAS CRACKED. REPLACED SEAT TRACK IAW DC-9 SRM 51-3-0, 51-1-8 AND ZANTOP DWG. #86302.SDR AALA20020421Door Frame · corrodedTUL - FOUND DOOR BEAM HAS SEVERAL AREAS OF CORROSION. INSTALLED FULL LENGTH DOUBLER PER AARD 53-10-00-3. (M)SDR ABXA010830Longeron · corrodedFORWARD ACCESSORY COMPARTMENT AT F.S. 640 - 660, LONGERON 31 RIGHT, WAS CRACKED. FABBED REPAIR STRAP AND REPAIRED AREA IAW DC-8 SRM 53-2-0, 53-4-1, 51-1-20D AND REA D853-43068MR.SDR C2XA03SH055Support · corrodedSHV DURING C CHECK GALLEY FLOOR PROFILE Z ASSEMBLY WAS FOUND TO HAVE CORROSION. MAINTENANCE REMOVED DAMAGE AND REPLACED AFFECTED ASSEMBLY IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APROVED TO RETURN TO SERVICE.SDR ABXA010785Fitting · crackedFORWARD CARGO, F.S. 380 - 400, LONGERON 31 LEFT, SPLICE FITTING WAS CRACKED. REMOVED AND REPLACED FITTING AT STA. 390, LONGERON 31 LEFT IAW DC-8 SRM 51-1-24 AND 51-1-20D.SDR ABXA010790Fitting · crackedFORWARD LOWER CARGO, STATION 272, FITTING WAS CRACKED FORWARD OF C1 DOOR. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D, 51-3-1 AND 51-1-24.SDR ABXA010792Seat Track · crackedFORWARD CARGO AT F.S. 580 - 600, AT LEFT BUTT LINE 55, SEAT TRACK WAS CRACKED. REMOVED AND REPLACED SEAT TRACK IAW DC-8 SRM 51-3-0, 51-1-24 AND 51-1-8.SDR ABXA010769Frame · corrodedAFT LOWER CARGO FRAME AT F.S. 973, LONGERON 30, 29 LEFT AND 28 LEFT, HEAVILY CORRODED AND DOUBLE DRILLED HOLE. REPAIRED FUSELAGE FRAME IAW REA D953-43402-MR.SDR COMA0260142VibratorFLIGHT 5980 VERY LOUD NOISE AND VIBRATION FROM FORWARD HALF OF AIRCRAFT.COULD NOT DUPLICATE. INSPECTION OF AIRCRAFT FOUND NO DEFECTS.SDR ABXA010770Frame · crackedLONGERON 17 LEFT WAS CRACKED BEHIND FUSELAGE FRAMES AT STATION 256, 275, 408 AND 427. REPAIRED AREA IAW DC-9 SSRM K05864.SDR COMA0260135Angle · misdrilledTHE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR HAS SHORT EDGE DISTANCE ON THE UPPER FASTENER HOLES.FABRICATED AND INSTALLED A NEW ANGLE I/A/W WVAC EO 601R-53-2987A.SDR COMA0260134Stiffener · crackedTHE VERTICAL J STIFFENER AT FS280 RBL9 WAS CRACKED.REMOVED CRACKED J STIFFENER. FABRICATED AND INSTALLED A NEW J STIFFENER I/A/W WVAC EO 601R-53-2990.SDR COMA0260133Bracket · misdrilledTHE INBOARD FLANGE OF A BRACKET ASSEMBLY HAS SHORT EDGE DISTANCE WITH A HOLE COMMON TO THE FLOOR BEAM AT FS349 AND RBL27.FABRICATED AND INSTALLED A NEW BRACKET I/A/W WVAC EO 601R-53-2991.SDR COMA0260119Fitting · crackedA FLOOR SUPPORT FITTING WAS CRACKED AT FS460 AND RBL9.REMOVED THE CRACKED FITTING AND INSTALLED A NEW FITTING P/N 600-31068-19 I/A/W WVAC EO 601R-53-2988.SDR COMA0260115Bracket · incorrectTHE INBOARD FLANGE OF A BRACKET ASSEMBLY HAS SHORT EDGE DISTANCE ON THE FASTENER COMMON WITH THE FLOOR BEAM AT FS349 RBL27.FABRICATED AND INSTALLED A NEW BRACKET I/A/W WVAC EO 601R-53-2991.SDR ASOA02156SBeam · crackedDURING (C) CHECK INSPECTION, WHILE COMPLYING WITH EO, VISUAL INSPECTION OF THE ENGINE SUPPORT BEAMS, BOTH SIDES WERE FOUND TO HAVE A CRACK. MAINTENANCE COMPLIED WITH EO TO SERVICE AS THE PERMANENT REPAIR FOR THE ENGINE SUPPORT BEAM CRACK.
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