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 AALA202406048511Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.SDR SWIA20240710430Stand Off · crackedR/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 7/9/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 & SKY CARD 51-900-1002-SKY.SDR SWAA2024041571305Bracket · cracked#1 ENGINE O/B COOLING TUBE BRACKET IS CRACKED<SDR WUXA202403260101Cowling · crackedCOWLING CRACKING IN MULTIPLE LOCATIONS BOTH #1 AND #2 ENGINES. INTERNAL CRACKING AROUND RIVETS AND NUT-PLATES. CRACKING IN ROOT OF BEND RADIUS ON ANGLE BRACKETS. CRACKS ADJACENT TO CAMLOCKS ON COWLING PANELS. CRACKS PROTRUDING DIRECTLY FROM CAMLOCKS ON COWLINGSDR 2024F00071Support · corrodedBTH-206L1-MM-1-5-31 ( TAIL BOOM) ,BTH-206L1-MM-1-27-60 PAR 5. REMOVAL AND INSPECTION OF TAIL BOOM STABILIZER REVEALED WEAR AND CORROSION EXCEEDING MANUFACTURES LIMITS. REMOVED AND REPLACED COMPONENT PER MANUFACTURES INSTRUCTIONS. NO FURTHER DEFECTS NOTED .SDR FXGA2024040800001Mount · crackedLEFT AND RIGHT ENGINE INERTIAL SEPARATOR MOUNTING STRUCTURE, NS 41 TO NS 50 CRACKED.SDR JR2R20240313346Landing · damagedACCESS PANEL 411BL LANDING HAS DAMAGED FASTENER HOLESDR COEA2024022106738Skin · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, A CRACK WAS DISCOVERED IN THE #2 ENGINE LOWER FWD COWL OUTBOARD UNDER THE EXHAUST. CORRECTIVE ACTION: A TEMPORARY REPAIR WAS PERFORMED PER FXTB DOCUMENT #01/30/2024. REPLACED THE LOWER FWD COWL MID SKIN AND INLET FRASDR CALA2024022200493Bracket · wornNUMBER 2 ENGINE I/B FAN COWL HAS EXCESSIVE PLAY AT HLD OPEN ROD STOWAGE BRACKET (6222) STOWAGE BRACKET DAMAGED AND FOUND TO BE OUT OF LIMITS IAW B767 SRM 54-23-90-1A-1. NEW REPLACEMENT BRACKET FABRICATED IAW B767 ENGINEERING DWG 314T3114 AND NEW BRACKET INSTALSDR ASAA2024020948069Fitting · corrodedLESSOR ITEM: PYLON #2 R/H FITTING BASEPLATE P.N. D5461020320100 HAS FRETTING GROUNDED - YES. ALL WORK ACCOMPLISHED ON NON ROUTINE 35903.AC FLIGHT HOURS 34712:52, AC CYCLES 11812, W.V. 015SDR DALA2024020701624Electrical Box · crackedSHIP 3124 CRACK ELECTRIC JUNCTION BOXES FWD POSITION OB SIDE ON RH PYLON. CORRECTIVE ACTION: REPAIRED PER E.R/A # 563665-14MA. (0189822)SDR DALA2024020501528Door · openSHIP 3897 -ATB- DUE TO LEFT ENGINE NOSE COWL T12 BLEED OVERPRESSURE DOOR OPEN. CORRECTIVE ACTION: PERFORMED LEFT ENGINE NOSE COWL ANTI-ICE DUCT BORESCOPE INSP. NO RUPTURED DUCTS. PERFORMED T12 ACCESS DOOR LATCH RELEASE TEST. LEFT ENGINE RELEASE TESTS ARE WITHISDR HNAA2024022600132Nacelle · none71-2255 UNRECORDED REPAIR ON RH NACELLE UPPER COWLING AFT OF XN1046.5 NEAR IB EDGE. R&R'D REPAIR IAW EO1-05-24-0050SDR HNAA2024022600131Nacelle · noneUNDOCUMENTED REPAIR ON LH NACELLE UPPER COWLING. R&R'D REAIR IAW EO1-05-24-0050SDR IPXA2024011173868Unknown · unknownNR 1 PYLON PRE-COOLER AERA STRUCTURE ANGLE FRAME HAS MULTIPLE CRACKED. 74-095 OK TO WORKSDR DALA2024011000397Unknown · unknownSHIP 3124 CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. CORRECTIVE ACTION: REPLACED FITTING SPIGOT ON R/H PYLON AS PER A319 SRM 54-51-12-300-001. (0147566)SDR IPXA2024010822914Unknown · unknown*** SDR FILED OPEN *** FAULT - CRACK - BEAM, NO.2 NACELLE AFT LOWER FAIRING R/H UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373 (REPLACE)SDR IPXA2024010707633Unknown · unknownENGINE 1 INLET COWL HAS 1 DENT NEAR THE 11:00 POSITION NEAR THE LEADING EDGE.***PLEASE ORDER PARTS AND TOOLING*** ACCOMP ALL MX AND INSP STEPS OF EO 89109-REQ1. DEF. DENT FOR 180 DAYS. DENT IS LOCATED AT 1:00 POSITION NOT 11:00 POSITION. OPENSDR UIEA2023122701026Rub Strip · unknownENG 2, CORE COWL RH PANEL 428AR, WEAR STRIP UPPER WITH EVIDENCE OF CORROSION(<P>ENG 2, CORE COWL RH PANEL 428AR, WEAR STRIP UPPER WAS REPLACED PER SRM 51-10-02-0G-0 PARA 9 REV 124 15 DEC 23. NO FURTHER DEFECTS NOTED</P>)SDR SWAA2024011536078Panel · damagedPANEL 422AB HAS ELONGATE HOLE<[01] REMOVED AND OVERSIZED FASTENER PER SRM 54-10-01-2R-16;[02] LOCATED AND DRILLED NEW PANEL 422AB PER SRM 51-40-05. APPLIED FINISH TO NEW PANEL PER AMM 51-21-99. OK TO INSTALL.;[03] CORRECTIVE ACTION # 1 WRITTEN IN ERROR.;[04] VSDR IPXA2024011278974Frame · crackedFAULT - CRACK - CLIP, INTERNAL AFTER OUTBOARD SIDE FRAME OF NO.1 PYLON AFTER FAIRING, NAC STA 376.20 (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 313T2303 SH. 136 REV. -. JOB SDR JJBA20231226032Unknown · unknownRH ENGINE TOP COWL AFT SPRING SEAL CRACKED. REPLACED.SDR JJBA20231226029Unknown · unknownLH ENG PYLON BLEED SYSTEM, LH PRECOOLERS FWD STRUCTURE BRACKET IS CRACKED. REPLACEDSDR 2023FA0000829Unknown · unknownENGINE #2, TRANSLATING COWL. NAC STA 194.3 TO 230, CORROSION ON UPPER BIFURCATION OUTBOARF PANEL.SDR 2023FA0000822Unknown · unknown.ENGINE #2, INLET COWL, ACOUSTIC PANEL, PERFORMED SKIN, UNDOCUMENTED 3 EXISTING FILLING REPAIRSSDR MK1Y202312207018Unknown · unknownREPAIR - ENGINE #2 LH CORE COWL WEAR STRIP WITH CORRPSION DAMAGESDR 2023FA0000793Unknown · unknownREPAIR - LH THRUST REVERSER SKIN AFT EDGE EXISTING TRIM OUTS BETWEEN 8/11 O'CLOCKSDR 2023FA0000792Unknown · unknownREPAIR - ENGINE #1, INLET COWL, INNER LIP SKIN, EXISTING FLUSH DOUBLER, P/N 224-2101-573HLSDR 2023FA0000791Unknown · unknownREPAIR - #1 ENGINE EXHAUST NOZZLE OUTER SLEEVE OUTER SKIN DAMAGESDR MK1Y20231127013Unknown · unknownEVALUATION - ENGINE #2 - LOWER TRUCK FAIRING, INBD SIDE - FOUND EXISTING DOUBLER REPAIR, BETWEEN NAC STA 202.5 - NAC STA 215.5 AND AT 6 O'CLOCKSDR MK1Y20231127012Unknown · unknownEVALUATION - STRUT #2 - UPPER INBD SIDE - HINGE FITTING ACCESS PANEL 425GZ - FOUND EXISTING DOUBLER REPAIRSDR MK1Y20231127010Unknown · unknownEVALUATION - PREVIOS REPAIR ON THE ENGINE #2 INLET COWL, LOWER PANEL ASSY, ANTI-ICE EXHAUST DUCT, AT 6 HRSSDR DALA2023112009546Unknown · unknownSHIP 3119 ELONGATED HOLE ACCESS PANEL 424CR ON RH PYLON. CORRECTIVE ACTION: COMPLIED WITH ERA 613110-14 REV. ORIGINAL. (0069915)SDR IPXA2023112413955Skin · corroded*MAJOR REPAIR* FAULT: #1 ENGINE PYLON O/B AFT. SKIN HAS CORROSION AT INNER SKIN APP. STA 154. NO DOT. VERIFIED COMPLIED WITH FINAL EA 757-5450-27-A3447 REV -. AND UPS EO 88763-REQ1SDR NACA2023111300003Unknown · unknownFOUND COUPLING OF COOLING DUCT AT 4 OCLOCK POSITION LOOSE. REMOVED AND REPLACED LPT COOLING DUCT AT 4 OCLOCK POSITION ON #1 ENGINE IAW AMMM 75-24-03SDR R61A2023120400709Rib · crackedRH PYLON AFT FAIRING FOUND TO HAVE 3X CRACKED ANGLE RIB ON HEAT SHIELD. REMOVED & REPLACED 3X ANGLE RIBS ON HEAT SHIELD AT R/H PYLON AFT FAIRING IAW EMB 170/175 SRM 51-42-03.SDR CALA2023111003331Panel · missingDURING WALK AROUND NOTICED LEFT ENGINE NACELLE STRUT PANEL 436AR PANEL MISSING, INBOARD SIDE. #1 ENG PYLON ACCESS PANEL 436AR MISSING, PANEL 4 IN DIAM ROUND. INSTALLED NEW PANEL 436AR REF AMM 54-53-01.SDR DALA2023110609132Unknown · unknownSHIP 3119 EXCESSIVE PLAY FWD BEARING AFT FIXED FAIRING ON RH PYLON (1 EA). CORRECTIVE ACTION: REPLACED HINGE FITTING FWD POSITION ON AFT FIXED FAIRING ON RH PYLON AS PER SRM 51-42-11-801, A319 SRM 51-44-11-801, A319 SRM 51-72-11-911-001, A319 SRM 51-21-11-801 SDR DALA2023110609131Unknown · unknownSHIP 3119 EXCESSIVE PLAY FWD BEARING AFT FIXED FAIRING ON LH PYLON (1 EA). CORRECTIVE ACTION: REPLACED HINGE FITTING FWD POSITION ON AFT FIXED FAIRING ON LH PYLON AS PER. (0050892)SDR DALA2023110609130Unknown · unknownSHIP 3119 EXCESSIVE PLAY BEARING ATTACHMENT BRACKET AFT FIXED FAIRING ON RH PYLON (1EA). CORRECTIVE ACTION: REPLACED BEARING (1E/A) AND SLEEVE (1/A) ATTACHMENT BRACKET AFT FIXED FAIRING ON RH PYLON AS PER A319 AMM 54-52. (0050886)SDR DALA2023103108960Unknown · unknownSHIP 3119 EXCESSIVE PLAY BEARING AFT FIXED FAIRING ON LH PYLON (2 EA). CORRECTIVE ACTION: REPLACED BEARINGS (2 EA) ON AFT FIXED FAIRING ON LH PYLON AS PER A319 AMM 54-52. (0042104)SDR DALA2023103108959Unknown · unknownSHIP 3119 EXCESSIVE PLAY BEARING AFT FIXED FAIRING ON RH PYLON (2 EA). CORRECTIVE ACTION: REPLACED BEARINGS (2 EA) ON AFT FIXED FAIRING ON RH PYLON, AS PER A319 AMM 54-52. (0042084)SDR SWAA2023103115865Fairing · cracked#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY HAS CRACK.<[01] REMOVED AND REPLACED CRACK #2 ENGINE PYLON AFT. STRUT SUPPORT FITTING PER SRM 51-40-02SDR SWAA2023103115651Fairing · crackedRH #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING CRACKED.<[01] REMOVED AND REPLACED #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY ON<BR> N/R TTG8Q00PAG6G.SDR DALA2023103008923Unknown · unknownSHIP 3119 EXCESSIVE PLAY BEARING ON LINK MOVABLE FAIRING ON RH PYLON. CORRECTIVE ACTION: REPLACED BEARINGS (2 E/A) OF LINK MOVABLE FAIRING ON RH PYLON AS PER A319 AMM 54-52. (0037315)SDR DALA2023103008922Unknown · unknownSHIP 3119 EXCESSIVE PLAY BEARING ON LINK MOVABLE FAIRING ON LH PYLON (2 EA). CORRECTIVE ACTION: REPLACED BEARINGS (2 E/A) OF LINK MOVABLE FAIRING ON LH PYLON AS PER A319 AMM 54-52. (0037312)SDR 2023FA0000653Unknown · unknownDURING MAINTENANCE INSPECTION SHOP FOUND ON ENG #2, STRUT INBD SIDE (LEFT), UNDOCUMENTED DOUBLER REPAIR ON PANEL 447ELX OUTER SKIN, B/T NAC STA 296 & NAC STA 302. EXISTING REPAIR DIMENSIONS: FILLER: 1.5”X5.5”; DOUBLER: 6.7”X5”.SDR 2023FA0000652Unknown · unknownENGINE #2 INLET COWL: FOUND DENTS BEYOND OF SRM 54-12-01 LIMITS ON THE EXTERIOR NOSE LE SKIN OF THE INLET COWL. DENT NO 1 – LOCATED 12 O’CLOCK 15” FROM THE AFT LIP A=0.88”, Y=0.047”, A/Y=18; DENT NO 2SDR 2023FA0000650Unknown · unknownENGINE #2, CORE COWL, BETWEEN NAC STA 293.25 – NAC STA 298.75: DURING AIRCRAFT CONVERSION MAINTENANCE INSPECTIONS, FOUND AN EXISTING UNDOCUMENTED DOUBLER REPAIR ON THE INBOARD SIDE OF THE #2 ENGINE, CORE COWL AT THE TITANIUM FAIRING CUTOUT AREA. THE DOUBLER RESDR 2023FA0000649Unknown · unknownDURING AIRCRAFT MAINTENANCE INSPECTION, SHOP FOUND THREE UNDOCUMENTED EXISTING FILLER REPAIRS AND MULTIPLE NEW DENTS ON #1 INLET COWL ACOUSTIC PANELS.
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