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 COMA0160526Fastener · improperWHILE ACCOMPLISHING CANADAIR REO 601R-53-61-345, THE REPAIR CALLS OUT FOR THE USE OF TWO HST 10AG8 HI LITES FOR INSTALLATION IN THE STANDOFF . PROPER GRIP LENGTH IF NOT AVAILABLE.INSTALLED HL18PB8-XX HI-LOK SWITCH HL70-8 COLLARS IN PLACE OF THE HST10AG8 HI LITSDR USAA010950SkinPIT - FOUND SKIN WITH OVAL WEAR MARK, .071 INCH .375 INCH DIAMETER, RIGHT A/C BAY ABOVE ACM VALVE CENTER TANK LOWER SKIN. REAMED DAMAGE TO .25 INCH DIAMETER, INSTALLED FASTENER SAME SIZE AS HOLE PER EA 71719. (M)SDR ASOA01119Skin · corrodedWHILE PERFORMING HANGAR INSPECTION IN MCN, BELLY SKIN CORROSION WAS FOUND AT THE TCAS ANTENNA, FRAME 21 AT STRINGERS 21 LEFT TO 19 RIGHT. MAINTENANCE REPAIRED CORROSION IAW ASA EO120-53-0164. THIS EO OUTLINES THE REPAIR FOR N285AS. AIRCRAFT OK FOR SERVICE. SDR COMA0160571Angle · corrodedSERVICE DOOR SILL ANGLE IS CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2589A.SDR COMA0160524ClipAT FS 280 EXISTING HOLE FALLS INTO RADIUS OF INBOARD CLIPS 2 EACH AT RBL9.REMOVED, FABRICATED AND INSTALLED I/A/W WVAC E.O. 601R-53-2613.SDR COMA0160527Angle · corrodedSERVICE DOOR SILL ANGLE IS CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2589A.SDR COMA0160525Beam · misdrilledTRANSVERSE BEAM AT FS 333, RBL9 HAS TWO EXISTING MISDRILLED FASTENER HOLES IN LOWER FLANGE.REPAIRED I/A/W WVAC EO 601R-53-2577.SDR TSAA0153098Skin · crackedIDENTIFIED 1.25 INCH SKIN CRACK AT FORWARD SERVICE DOOR LOWER AFT SECTION. (M)SDR C2XA01BT147Venturi · corrodedYUL---CO4372, DURING 1C INSPECTION YUL MAINTENANCE FOUND LAV VENTURI TO BE CORRODED....REMOVED AND REPLACED WITH NEW VENTURI IAW ATR42 SRM 51-25-01.SDR COMA0160503Web · crackedENGINE SUPPORT BEAM APPEARS TO BE CRACKED IN THE AFT CENTER AREA OF THE UPPER SURFACE PROTRUDIG FROM BOTH ENDS OF FASTENER HOLE CAREA MARKED BUTTLINE 8.5K.PERFORMED TEMPORARY REPAIR TO ENGINE SUPPORT BEAM UPPER AND LOWER WEBS PER REO 601R-53-61-345.SDR UIEA01090Fitting · corrodedDURING INSPECTION FOUND BS 1480 LEFT AND RIGHT INBOARD HORIZONTAL SUPPORT FITTINGS CORRODED AT THE ATTACHMENT TO THE BODY GEAR TRUNNION, VERTICAL SUPPORT FITTING. REMOVED BUSHINGS FROM BOLT HOLES. BLENDED LOCAL CORROSION. SPOT FACED AREA AROUND BOLT HOLES. SDR DL72S011242Skin · cracked.25 INCH CRACK IN EMPENAGE SKIN AT AFT I/B CORNER OF GROUND AIR CONNECTION ACCESS DOOR CUTOUT. REPAIRED PER M/M 53-30-000-8 PG 2.SDR USAA010937SkinCLT - FOUND PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 430 BETWEEN S24R AND S25R. PREVIOUSLY INSTALLED .21875 INCH RIVET PER SRM 53-00-01, FIG 207. (M)SDR USAA010939SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 605, BETWEEN S27R AND S28R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M)SDR USAA010940SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 625 BETWEEN S26R AND S27R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M)SDR USAA010941SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 644 BETWEEN S23R AND S24R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M)SDR USAA010942SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 685 BETWEEN S26R AND S27R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M)SDR USAA010944SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 693, BETWEEN S23R AND S24R. PREVIOUSLY INSTALLED .25 INCH RIVET PER SRM 53-00-01, FIG 207. (M)SDR USAA010946SkinCLT - FOUND FUSELAGE SKIN WITH PREVIOUSLY RECORDED LIGHTNING STRIKE, BS 1360 TO 1380, BETWEEN S26/S27R. TWENTY PREVIOUSLY INSTALLED NR 6 RIVETS PER SRM 53-00-01, FIG 207. (M)SDR USAA010947Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED 4.6 INCHES BY 3.2 INCHES, BS 1280 S29L. CORROSION REMOVED, INSTALLED REPAIR DOUBLER PER EA 62117A. (M)SDR USAA010948Plate · corrodedCLT - FOUND SILL WEB PLATE CORRODED, 8 INCH AREA, BS 1675, L-4 DOOR. CORROSION LEVEL 2, TASK NR C53-251-02. REMOVED AND REPLACED WEB PLATE PER SRM 51-10-02. (M)SDR USAA010926Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 1 INCH BY 1 INCH AREA, BS 440, LBL 45. CORROSION LEVEL 1, TASK NR C53-231-02. DAMAGE REMOVED, SPLICED IN REPAIR SECTION PER SRM 53-00-52. (M)SDR USAA010920Web · crackedCLT - FOUND CREASE BEAM WEB CRACKED APPROXIMATELY .25 INCH, JUST FORWARD OF BS 1380, RBL 64. INSTALLED REPAIR DOUBLER AND CREASE BEAM ANGLE PER SRM 51-70-13. (M)SDR USAA010915Doubler · corrodedCLT - FOUND A 2 INCH AREA OF FRAME CORRODED, BS 640, MID CHORD, BETWEEN S25R AND S26R. CORROSION REMOVED, INSTALLED REPAIR DOUBLER PER SRM 51-10-02. (M)SDR USAA010913Frame · gougedCLT - FOUND FRAME GOUGED APPROXIMATELY .25 INCH, BS 1340 AT S26L. REPAIR DOUBLER INSTALLED PER TYPICAL REPAIR 53-60-01. (M)SDR USAA010912Stringer · crackedCLT - FOUND STRINGER CRACKED, BS 466, STRINGER 21R. DAMAGE REMOVED, INSTALLED REPAIR DOUBLER PER SRM 53-00-03. (M)SDR USAA010918Frame · dentedCLT - FOUND FRAME DENTED APPROXIMATELY .5 INCH, BS 700 AT S23L. INSTALLED REPAIR DOUBLER PER EA 85014. (M)SDR USAA010914Frame · dentedCLT - FOUND FRAME DENTED APPROXIMATELY .25 INCH IN DIAMETER, BS 620 AT S24L. INSTALLED REPAIR DOUBLER PER EA 69875. (M)SDR USAA010917Frame · dentedCLT - FOUND FRAME DENTED APPROX .25 INCH IN DIAMETER, BS 600 BETWEEN S23L AND S24L. INSTALLED REPAIR DOUBLER PER EA 69874. (M)SDR USAA010916Frame · dentedCLT - FOUND FRAME DENTED APPROX .25 INCH IN DIAMETER, BS 580 ABOVE S23L. INSTALLED REPAIR DUOBLER PER EA 69872. (M)SDR USAA010935SkinCLT - FOUND LIGHTNING STRIKE ON FUSELAGE SKIN, BS 373 BETWEEN S25R AND S26R. PREVIOUSLY INSTALLED .21875 RIVET PER SRM 53-00-01, FIG 207. (M)SDR UIEA01076Web · crackedDURING INSPECTIN FOUND FRAME WEB CRACKED AT BS 380 FROM STRINGER 23L CUTOUT. TRIMMED AWAY CRACKED AREA. FABRICATED REPLACEMENT DOUBLER AND TWO ANGLES. INSTALLED PER STANDARD PRACTICES. CONTINUE CURRENT INSPECTION REQUIREMENTS PER SB 747-53A2265 UNTIL SB 53SDR UIEA01077Frame · crackedDURING INSPECTION FOUND FRAME CRACKED AT BS 400, STRINGER 15L CUT OUT. CRACK IS APPROXIMATELY .30 INCH LONG RUNNING FROM STRINGER CUT OUT TO FASTENER HOLE. HFEC INSPECTED EXISTING FASTENER HOLE FOR CRACK CONTAINMENT. NO ADDITIONAL CRACKS FOUND. FABRICATED SDR UIEA01078Frame · crackedDURING INSPECTION FOUND FRAME AND CHORD CRACKED AT BS 440, STRINGER 13AL/14L. CRACK IS APPROX 1 INCH LONG. CHORD IS COMPLETELY SEVERED. HFEC INSPECTED EXISTING FASTENER HOLE IN FRAME FROM CRACK CONTAINMENT. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMESDR UIEA01079Frame · crackedDURING INSPECTIN FOUND FRAME WEB CRACKED AT BS 460, STRINGER 13AL AT TWO LOCATIONS COMMON TO THE FRAME AND DOUBLER. HFEC INSPECTED EXISTING FASTENER HOLES IN WEB FOR CRACK CONTAINMENT. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMENT DOUBLERS, FILLERS ANDSDR UIEA01080Web · crackedDURING INSPECTION FOUND FRAME WEB CRACKED AT BS 500, STRINGER 9L AND STRINGER 8 TO 10AR. STOP DRILLED ALL CRACKS. FABRICATED REPLACEMENT DOUBLERS. INSTALLED DOUBLER AT STRINGER 9L LOCATION AND AT STRINGER 8 TO 10AR LOCATION PER STANDARD PRACTICES OF THE SRMSDR UIEA01081Frame · crackedDURING INSPECTION FOUND FRAME WEB CRACKED AT BS 480 BETWEEN STRINGER 15 AND 16R CUT OUTS. STOP DRILLED CRACKS. FABRICATED REPLACEMENT DOUBLER. INSTALLED DOUBLER PER STANDARD PRACTICES OF THE SRM. CONTINUE CURRENT INSPECTION REQUIREMENTS PER SB 747-53A2265 SDR UIEA01082Frame · crackedDURING INSPECTION FOUND FRAME AN INNER CHORD CRACKED AT BS 440 STRINGER 15R TO EXISTING FASTENER. HFEC INSPECTED EXISTING FASTENER HOLE TO INSURE CONTAINMENT OF CRACK. NO ADDITIONAL CRACKS FOUND. FABRICATED REPLACEMENT DOUBLER AND NEW CLIP. PROCURRED NEW RSDR UIEA01085Fitting · corrodedDURING INSPECTION FOUND BOTH LEFT AND RIGHT MAIN LANDING BODY GEAR UPPER TRUNNION FITTING HAVE CORROSION IN THE FORWARD BOLT HOLE POCKET. REMOVED CORROSION PER SRM 51-10-01. MEASURED AND SPOT FACED AREA. PERFORMED PENETRANT INSPECTION PERFORMED. NO CRACKS SDR UIEA01086ShimDURING INSPECTION FOUND SHIMS MIGRATING FROM BS 1240 LEFT/RIGHT BULKHEAD UPPER CHORD FITTING. REMOVED BOLTS IN AFFECTED AREA, TRIMMED SECTION OF MIGRATED SHIM. FABRICATED REPLACEMENT SHIM FROM SOLID MATERIAL, ALODINED AND PRIME PAINTED. REINSTALLED REMOVED SDR UIEA01087Fitting · corrodedDURING INSPECTION FOUND LEFT AND RIGHT BODY GEAR INBOARD TRUNNION SUPPORT FITTINGS CORRODED AT BS 1480 AFT SIDE OF LUG AT LONGERON ATTACH POINT. CLEANED CORROSION, SPOT FACED AFFECTED AREAS, FLAP PEENED, TREATED, PRIME PAINTED. PENETRANT INSPECTION PERFORMEDSDR UIEA01088Web · corrodedDURING INSPECTION FOUND WEB CORRODED BEHIND BS 1480 INBOARD BODY GEAR VERTICAL TRUNNION SUPPORT. CORROSION BLENDED PER SRM 51-10-01. PERFORMED HFEC OF BLENDED AREA TO INSURE CRACK AND CORROSION FREE. NO CRACKS OR CORROSION. MEASURED BLEND AREAS. FABRICATESDR USAA010934Frame · crackedPIT - FOUND FRAME CRACKED 4 INCHES, FS 21736 BETWEEN STRINGER 3 AND THROUGH UPPER C-CHANNEL. INSTALLED TWO REPAIR ANGLES PER EA 71597. (M)SDR ABXA010434Track · corrodedLEVEL 1 CORROSION AND EXFOLIATION ON CENTER TRACK AT F.S. 325. REPLACED SEAT TRACK SECTION IAW DC-9 SSRM K05406.SDR ABXA010432Web · crackedRIGHT CUSP WEB WAS CRACKED 7 INCHES AFT OF STATION 917 FLOORBEAM. REPAIRED CRACK IAW DC-9 SRM 53-01, FIGURE 2.SDR ABXA010430Frame · crackedCRACK IN FRAME F.S. 389, LONGERON 29 RIGHT, UPPER SURFACE, JUST INBOARD OF DOOR CUT OUT WEB. REPAIRED FRAME AT STATION 389, LONGERON 29 RIGHT IAW DC-9 SRM 53.SDR ABXA010429Frame · crackedCRACK IN FRAME AT F.S. 408, LONGERON 29 RIGHT, UPPER SURFACE, JUST INBOARD OF DOOR CUT OUT WEB. REMOVED DAMAGED FRAME SECTION. SPLICED SECTION IAW DC-9 SRM 53-03, FIGURE 2A. SPLICES D05904-3-7S-11 FROM DRAWING K05906.SDR ABXA010428Intercostal · corrodedLEVEL ONE CORROSION ON UPPER SURFACE OF INTERCOSTALS AT LONGERON 28 RIGHT AND 28 LEFT, BETWEEN F.S. 579 AND F.S. 598. BLENDED AND TREATED CORROSION ON INTERCOSTAL AT LONGERON 28 RIGHT - 28 LEFT, F.S. 579-598, IAW DC-9 SRM 53.SDR ABXA010427Longeron · crackedLONGERON 3 LEFT WAS CRACKED AT F.S. 160. REPAIRED AREA IAW DC-9 SRM 53-02, FIGURE 18.SDR COMA0160520Plate · incorrectTWO SPLICE PLATES P/N 601R310300-77 WERE FABRICATED INCORRECTLY BY MANUFACTURE.REMOVED AND REPLACED SPLICE PLATES I/A/W WVAC EO 601R-53-2609.
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