JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400' 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 = '5400' 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 AALA960535Angle · corrodedTUL - FOUND T-ANGLE AT TOP OF PYLON HAS CORROSION AT WEB ATTACH AREA. REPLACED ANGLE PER SRM 51-72-10. (M)SDR UPS96806039Strap · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED STRAP CRACKED AT NR 3 PYLON INSIDE FWD TANK AT NR 2 STR. REPLACED STRAP PER SRM 51-1-20D.SDR UPS96806032Angle · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 PYLON I/B DRAG ANGLE CRACKED BEYOND STOP DRILL. REPAIRED ANGLE PER SRM ADDENDUM DC8-5740-0716.SDR 96ZZZX1806Pylon Support · crackedTHE RT PYLON SUPPORT IS CRACKED 14.50 INCHES FROM THE FORWARD TRANSMISSION ISLAND AFT. THE CRACK WAS DISCOVERED DURING REPLACEMENT OF THE RT CYCLIC SERVO. THE FOLLOWING COMPONENTS OF THE PYLON STRUCTURE WERE CRACKED: BEAM (W.O. 65.00). PYLON SUPPORT ASSY, RSDR 96ZZZX1805Beam · crackedTHE RT PYLON SUPPORT IS CRACKED 14.50 INCHES FROM THE FORWARD TRANSMISSION ISLAND AFT. THE CRACK WAS DISCOVERED DURING REPLACEMENT OF THE RT CYCLIC SERVO. THE FOLLOWING COMPONENTS OF THE PYLON STRUCTURE WERE CRACKED: BEAM (W.O. 65.00). PYLON SUPPORT ASSY, RSDR EISA96038Skin · crackedSEVERAL CRACKS ON RIGHT SIDE, UPPER S-DUCT. CUT OUT CRACKED SECTION OF S-DUCT. FABRICATED AND INSTALLED DOUBLER WET PER SRM 54-10-3. (M)SDR DL72W960762S-Duct · crackedFOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING LT SIDE JUST ABOVE AND AFT OF ACCESS PLATE 9523. REPAIRED PER M/M 54-30-0 PG 801 FIG 802, INSTALLED PERMANENT REPAIR.SDR 96UAL900210Spar Web · crackedNR 3 PYLON UPPER SPAR WEB HAD A CRACK INDICATION IN A FASTENER HOLE COMMON TO THE SPAR CHORD. REPAIRED PER DC-10 SRM 54-20-00 FIGURE 27.SDR DL76L960956Upper Spar · crackedTWO CRACKS WERE FOUND IN THE NR 1 ENGINE PYLON UPPER SPAR WEB AT THE OUTBOARD DRAIN HOLE AT NAC STA 156 AND WL 149.21. THE CRACKS WERE STOP DRILLED AND REINFORCED WITH A FILLER AND DOUBLER PER DL ERA 273499-14, REV A.SDR 9607706634Web · crackedDURING P-CHECK, FOUND A CRACK IN THE NR 3 PYLON MID SPAR WEB. REPAIRED WEB (P/N 65B90421-41) PER EA 66-99587.SDR UPS96805680Angle · damagedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT. REWORKED NR 2 AND NR 3 PYLON FOOTSTOOL FITTING T-DOUBLER/SKATE ANGLE IAW UPS EO DC8-57-061.SDR 96FDEA00607Rib · chafingNR 3 ENG LOWER COWL HAS TWO AREAS OF CHAFING ON NR 5 RIB. REMOVED AND REPLACED NR 3 ENGINE LOWER COWL NR 5 RIB.SDR 96ZZZX2536Fitting Assy · brokenMAJOR INSPECTION FOUND FORWARD LEG OF FITTING BROKEN THROUGH BOLT HOLE. AIRCRAFT TOTAL TIME 7775.6 HOURS. REPORTED AS: N NR NXA-SQH (MEXICO).SDR 96ZZZM792Angle · crackedDURING OP-15, FOUND .75 INCH CRACK IN LEFT PYLON ATTACHED ANGLE VERTICAL LEG TOP SIDE, STATION 980. STOP DRILLED CRACK AND REPAIRED PER SRM 54-04.SDR CAL960302Gusset · crackedKUL - INSPECTION FOUND A 1.5 INCH CRACK IN NR 2 ENGINE PYLON RIGHT GUSSET. THE GUSSET WAS REPAIRED IAW ECRA 5410-01393. (M)SDR ABXA9600357Angle · crackedDURING C-CHECK INSPECTION, FOUND A CRACK IN THE UPPER PYLON ATTACH ANGLE AT STA 980. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10.SDR MALA964909Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT UPPER INBOARD WING SKIN TO NACELLE ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (M)SDR MALA964908Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LEFT LOWER INBOARD WING SKIN TO NACELLE ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (M)SDR IXXA9630Fitting · crackedDURING THE D-CHECK INSPECTION, FOUND A CRACK ON THE NR 1 PYLON SUPPORT FITTING AT FS YN 387 IN 2EA LOCATIONS. MANUFACTURED FITTING PER DACO DRAWING 5756790 AND INSTALL FITTING PER DACO DRAWINGS 5756791, 5756801, AND DACO SRM 51-00, 51-1-20, 51-3-0, AND 51-1-8SDR 96UAL900144Spar Web · crackedDURING ENGINE CHANGE THE NR 3 PYLON CENTER SPAR WEB WAS FOUND TO BE CRACKED. THE CRACK IS AT STATION 416 AND PROPAGATES 2 INCHES FROM LIGHTENING HOLE TO EDGE OF WEB. A PERMANENT REPAIR WAS MADE PER DC-10-30 STRUCTURAL REPAIR MANUAL.SDR USAA960164Doubler · crackedCLT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND A 3 INCH CRACK AT NR 1 ENGINE PYLON PANEL 5724L DOUBLER. INSTALLED DOUBLER PER SRM TYPICAL REPAIR 54-50-04D. (M)SDR ABXA9600342Angle · crackedDURING C-CHECK INSPECTION, FOUND A CRACK AROUND FASTENER ON THE LEFT PYLON UPPER ATTACH ANGLE. REPAIRED IAW DC-9 SRM 54-04, FIG 10.SDR 96ZZZM317Angle · crackedDURING AN 18 MONTH INSPECTION OF THE LEFT PYLON, 1 INCH CRACKS WERE FOUND IN THE LEADING EDGE ATTACHMENT ANGLES, P/N 115921901-19 AND -20. THE ANGLES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 96ZZZM316Angle · crackedDURING AN 18 MONTH INSPECTION OF THE LEFT PYLON, 1 INCH CRACKS WERE FOUND IN THE LEADING EDGE ATTACHMENT ANGLES, P/N 115921901-19 AND -20. THE ANGLES WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR 96ZZZX1835Skin · delaminatedDURING C-CHECK, LT PYLON ABOVE AFT HINGE POINT FOUND DELAMINATED. REPAIRED IAW DC9 SRM CH 54. AIRCRAFT TT: 22,205 HRS. AIRCRAFT TC: 42,206.SDR P5CA9600055Strap · crackedFOUND CRACKED STRAP ON BOTH SIDES OF NR 3 SKIRT FORWARD EDGE. REPAIRED IAW SRM 54-12-02.SDR A6WR95070Rivets · shearedDURING SCHEDULED INSPECTION FOUND 2 RIVETS SHEARED OFF IN NR 2 PYLON BOX AT POSITIONS C AND D. REPLACED FASTENERS IAW AVRO RIL HC546H9009. (X)SDR A6WR95069Rivets · shearedDURING SCHEDULED INSPECTION, FOUND 4 RIVETS SHEARED OFF IN NR 3 PYLON BOX AT POSITIONS A, B, C, AND D. REPLACED FASTENERS IAW AVRO RIL HC546H9009. (X)SDR A6WR95068Bracket · crackedDURING SCHEDULED INSPECTION, FOUND NR 2 PYLON LORD MOUNT EYE BOLT BRACKET CRACKED. REPLACED BRACKET. (X)SDR A6WR95067Bracket · crackedDURING SCHEDULED INSPECTION, FOUND NR 1 PYLON SHOULDER COWL LORD MOUNT ATTACHMENT BRACKET CRACKED. REPLACED BRACKET. (X)SDR A6WR95060Pylon · rivets shearedDURING SCHEDULED INSPECTION, FOUND 3 RIVETS SHEARED OFF IN NR 4 PYLON BOX AT POSITIONS B, C, D. REPLACED FASTENERS IAW AVRO RL HC546H9009. (X)SDR A6WR95059Bracket · brokenDURING SCHEDULED INSPECTION, FOUND BOTH LEFT SIDE BRACKETS SUPPORTING PRESSURE REGULATING/ISOLATION VALVE BROKEN IN NR 4 PYLON. REPLACED BRACKETS. REFERENCE: OPERATOR CONTROL NR 96ZZZX760. (X)SDR 96ZZZX760Bracket · brokenDURING SCHEDULED INSPECTION, FOUND BOTH LEFT SIDE BRACKETS SUPPORTING PRESSURE REGULATING/ISOLATION VALVE BROKEN IN NR 4 PYLON. REPLACED BRACKETS. REFERENCE: OPERATOR CONTROL NR A6WR95059.SDR C2XA96IA023Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT NACELLE FRAME NR 2 UPPER ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA96IA022Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME NR 2 UPPER ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR ABXA9600330Angle · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE CRACKED NEAR THE CENTER. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10.SDR ABXA9600329Angle · crackedDURING C-CHECK INSPECTION, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE CRACKED NEAR THE FORWARD END. REPAIRED IAW DC-9 SRM 54-04, FIGURE 10.SDR P5CA9600114Bracket · crackedNR 4 PYLON AFT FAIRING DOOR FOURTH BRACKET ANGLES CRACKED. ANGLES REPLACED AND BRACKET ASSY REINSTALLED IAW MM 54-32-01.SDR MALA964800Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LT LOWER INBOARD WING TO NACELLE ATTACH ANGLE. THEY STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X)SDR MALA964795Attach Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT INBOARD LOWER WING TO NACELLE ATTACH ANGLE. THEY STOP DRILLED A CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP 54-20-9101. (X)SDR ABXA9700693Fitting · crackedDURING C-CHECK, THE PYLON FRONT SPAR UPPER BEAVER TAIL FITTING WAS CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-1.SDR 96ZZZX845S-Duct · crackedDURING 2C INSPECTION, NOTICED CRACKED SPOT WELDS ON THE FORWARD S-DUCT OUTER SKIN. SUBMITTED FINDINGS TO FALCON JET. DOOR '350A' MUST BE REMOVED TO VIEW THIS AREA. THIS PROBLEM IS NOT CURRENTLY ADDRESSED IN AN AD OR SB.SDR P5CA9600120Rib · brokenRIGHT LOWER SLOT SEAL FAIRING SUPPORT RIB ON NR 4 ENGINE FOUND BROKEN OFF. REPLACED IAW SRM 54-30-01.SDR P5CA9600115Bracket · crackedNR 3 PYLON LT AFT FAIRING DOOR, AFT MOST BRACKET ANGLES FOUND CRACKED. ANGLE REPLACED IAW MM 54-32-01.SDR P5CA9600109Fairing · crackedFOUND NR 3 ENGINE FORWARD FAIRING CRACKED AT FRAME. REPAIRED IAW MM 51-40-03 AND REINSTALLED PER MM 71-40-08.SDR MALA954773Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LEFT UPPER INBOARD NACELLE TO WING SKIN ATTACH ANGLE. THEY REPLACED THE ATTACH ANGLE IAW FAC SRM 51-00-00. (M)SDR MALA954772Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT NACELLE OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP. (M)SDR MALA954771Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT NACELLE OUTBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE. STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW FAC ARP. (M)SDR MALA954770Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE RIGHT NACELLE INBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE. REPLACED THE FORWARD 12 INCHES OF THE ATTACH ANGLE IAW SRM 51-00-00. (M)SDR C2XA95IA421Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RT NACELLE FRAME NR 2 ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
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