JASC 5346

Service difficulty reports · 921

Reports filed under 5346 · Fuselage, Powerplant Attach Fittings, 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 = '5346'
  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.

SDR COMA0160478Beam · crackedCRACKS FOUND IN ENGINE SUPPORT BEAM LOWER WEB BETWEEN FS 625.30 - 640.00 ON THE LEFT/RIGHT SIDE OF THE SUPPORT BEAMREPAIRS WERE ACCOMPISHED IN ACCORDANCE WITH REO 601R-53-61-366 REV B.Jul 13, 2001 · N926CA · Cndair CL6002B19SDR COMA0160468Beam · crackedCRACKS FOUND IN ENGINE SUPPORT BEAM LOWER WEB BETWEEN F.S. 640.0 - 625.30 ON LEFT HAND AND RIGHT HAND SIDES.REPAIRED CRACKS I/A/W REO 601R-53-61-366 REV B AND WVAC E.O.'S 601R-53-2560-1A AND 601R-53-2545B.Jul 13, 2001 · N965CA · Cndair CL6002B19SDR COMA0160441Beam · crackedDURING INCORPORATION OF COMAIR EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND THE RIGHT SIDE CRACKED ON LOWER WEB FWD.REPAIRED ENGINE SUPPORT BEAM I/A/W CRJ REO 601-53-61-366 REV B AND WVAC EO 601R-53-2542.Jul 2, 2001 · N967CA · Cndair CL6002B19SDR COMA0160422Beam · crackedDURING INCORPORATION OF COMAIR EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND THE RIGHT SIDE CRACKED ON LOWER WEB FWD.REPAIRED ENGINE SUPPORT BEAM I/A/W CRJ REO 601-53-61-366 REV B AND WVAC EO 601R-53-2542.Jul 2, 2001 · N967CA · Cndair CL6002B19SDR COMA0160420Beam · crackedDURING INCORPORATION OF COMAIR EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND THE L/H SIDE CRACKED ON LOWER WEB FWD.PERFORMED A TEMPORARY MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/A/W CRJ REO 601R-53-61-358.Jul 1, 2001 · N967CA · Cndair CL6002B19SDR COMA0160401Beam · crackedDURING INCORORATION OF COMAIR EO 53-021 (VISUAL INSP. OF THE ENGINE SUPPORT BEAM) THE ENGINE SUPPORT BEAM WAS FOUND CRCKED 1.5" ON RH SIDE LOWER WEB I/B CORNER AT FS 621.0 - FS 640.0PERFORMED A TEMPORARY MAJOR REPAIR TO ENGINE SUPPORT BEAM LOWER WEB I/B CORNERJun 25, 2001 · N936CA · Cndair CL6002B19SDR RRXA11244Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK SCALLOPS AT STA.952 AND LBL25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM51-1-20DJun 8, 2001 · N606AL · Doug DC873FSDR RRXA11243Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK SCALLOPS AT STA.300 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20Jun 8, 2001 · N606AL · Doug DC873FSDR RRXA11232Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA.160 AND LBL25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3, 51-3-0.Jun 6, 2001 · N606AL · Doug DC873FSDR RRXA11217Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO MAIN CABIN SEAT TRACK SCALLOPS AT STA.338 AND LBL45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 Jun 4, 2001 · N606AL · Doug DC873FSDR COMA0160379Beam · crackedLT SIDE OF ENGINE SUPPORT BEAM IS CRACKED AT PANEL CUTOUT AT FS 625.0. REMOVED DAMAGED AREA AND REPAIRED WITH PO 28317/2 .071 AND PO 29987/2 .063 7075 T6, IAW WVAC EO 601R-53-2437.May 9, 2001 · N914CA · Cndair CL6002B19SDR RRXA11113Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO CO-PILOTS AFT RT SEAT TRACK, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.Apr 28, 2001 · N996CF · Doug DC862FSDR RRXA11112Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT PILOTS AFT RT, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.Apr 28, 2001 · N996CF · Doug DC862FSDR RRXA11111Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT CO-PILOTS LEFT FWD TRACK, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.Apr 28, 2001 · N996CF · Doug DC862FSDR RRXA11109Seat Track · wornDURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT CO-PILOTS RT FWD, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.Apr 28, 2001 · N996CF · Doug DC862FSDR COMA0160380Beam · crackedENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDE LOWER WEB HAS A CRACK AT THE FORWARD INBOARD CORNER OF THE LOWER ACCESS PANEL. REPAIRED IAW WVAC EO 601R-53-2304C.Mar 20, 2001 · N971CA · Cndair CL6002B19SDR 20000510SH019Fitting · crackedDURING ENGINEDECK REPLACEMENT, FOUND FUSELAGE FITTING AT LEFT FORWARD ENGINE MOUNT ATTACHMENT CRACKED. CRACKS EMANATE FROM INISDE REAR BOLT HOLE. POSSIBLE CAUSE IS HOLES NOT PROPERLY DEBURRED. SUBMITTER STATED TO PREVENT RECURRENCE, HOLES SHOULD BE DEBURREMar 2, 2000 · N302FD · Bell 412SDR CA960808002Bracket · broken(CAN) DURING INSPECITON, BRACKET WAS FOUND BROKEN AT ENGINE ATTACHMENT POINT.Jul 11, 1996 · Piper PA31350SDR 97ZZZX3069Fitting · corrodedDURING PROCESS OF REMOVING RT THRUST STRUT FOR NDT, DISCOVERED SEVERE INTERGRANULAR CORROSION AT AFT/UPPER THRUST STRUT/FUSELAGE ATTACH FITITNG, PN 1159BM20518-XX. BRACKET IS LOCATED IN PYLON. AREA AFFECTED SURROUNDS STRUT ATTACH BOLT/BUSH BRACKET LOCATION, Jan 11, 1996 · N8490P · Gulstm G1159BSDR MWEA95292Fitting · crackedDURING INSPECTION, FOUND FITTING FOR AFT UPPER ENGINE MOUNT CRACKED AT STA 859. MAINTENANCE FABRICATED NEW FITTING IAW DAC DRAWING 5917717 AND INSTALLED IAW SRM 53-01 PG 1. RETURNED A/C TO SERVICE.Sep 5, 1995 · N600ME · Doug DC914SDR UPS202975Ring Chord · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON RING CHORD ON NR 2 ENGINE AT BS 1352, AT EXISTING REPAIR. REPLACED PER UPS EO B727-7100-2729C.Apr 18, 1995 · N921UP · Boeing 727180C
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