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 ASAA2022090439787Nut Plate · damagedUPON J9 HARNESS REPLACEMENT FOUND 3:00 O'CLOCK STRUT FAIRING NUTPLATE DAMAGED. GROUNDED - YES. REMOVED AND REPLACED NUTPLATE. REF B737-900 SRM 51-40-02.SDR IXXA2022090301Rub Strip · bentPYLON PANEL 441AT RUB STRIP BENTSDR DALA2022090205901None · noneSHIP 654 MIGRATED BUSHING ON LH PYLON FITTING (UPPER LINK FWD END) AT NAC STA 163. CORRECTIVE ACTION: SUMMARY OF NRC 00444: BUSHINGS ON LH PYLON FITTING (UPPER LINK FWD END) AT NAC STA 163 ( ENG 1) WERE REPLACED PER B757-200 SRM. (2388595)SDR IXXA2022083101Support · crackedFAIRING SUPPORT FRAME CRACKEDSDR SWIA202266822None · crackedRH ENGINE PYLON RIB AT FS 605.00 IS CRACKED ON LOWER FLANGE AT OUTBOARD EDGE (MARKED). (C-CHECK RO 11/10/2022) REPAIRED RIGHTHAND ENGINE PYLON RIB AT FS605.00 AT LOWER FLANGE AT OUTBOARD EDGE IAW REO 601R-54-61-138 REV -- DATE 2022-09-23 STEPS. 1-15 (SESDR DALA2022090205899None · noneSHIP 662 MIGRATED INB. BUSHING ON RH PYLON FITTING ( UPPER LINK FWD END) AT NAC STA 163. CORRECTIVE ACTION: SUMMARY OF NRC 00322: BUSHINGS (2 EAS) OF ATTACH FITTING AT RH PYLON WERE REPLACED PER B757-200 SRM. (2387686)SDR IXXA2022082601Attach Bracket · cracked#1 PYLON OUTBOARD ATTACH BRACKET FOR FAIRING CRACKED.SDR IPXA2022082985728None · crackedINSPECTION TYPE:SEG#2 ENG PYLON ARC WEB REAR AT BUTTERFLY PANELS HAS CRACKS.WELD REPAIR PER SRM 54-50-00SDR IPXA2022082985719None · crackedINSPECTION TYPE:SEGENG 2 FAIRING 485AL AFT SKIN I/B SIDE WITH 2EA CRACKS.WELD REPAIR PER EO A300-5450-21297-LSDR IPXA2022082985720Precooler · crackedINSPECTION TYPE:SEGENG 1 PRECOOLER PANEL 413BL HAS SEVERAL CRACKS.WELD REPAIR PER SRM 54-52-51SDR IPXA2022082985721Precooler · crackedINSPECTION TYPE:SEGENG 2 PRECOOLER PANEL 423BL HAS SEVERAL CRACKSWELD REPAIR PER SRM 54-52-51SDR SWAA2022081741980Fairing · damagedLOWER PYLON FAIRING BELOW ACCESS PANEL 434BL SHOWS FRETTING WEAR FROM PYLON DRAIN TUBE / [01] REMOVED AND REPLACED LOWER PYLON FAIRING AT PYLON DRAIN TUBE PER SRM 51-40-02 AND SRM 51-40-05.SDR REXA2022100302162Separator · wornPANEL 422DB HAS BOTH SEPARATORS KNIFE-EDGED REMOVED AND INSTALLED (2) EA NEW SEPARATORS P/N: 601R37138-24 AND -26 ON PANEL 422DB REF CRJ200 SRM 51-42-06SDR REXA2022100302161Separator · wornPANEL 412DB HAS BOTH SEPARATORS KNIFE-EDGED REMOVED AND INSTALLED (2) EA NEW SEPARATORS P/N: 601R37138-25 AND -27 ON PANEL 412DB REF CRJ200 SRM 51-42-06SDR UIEA2022080500814Panel · damagedMDDR 169109 - #2 ENG INBOARD PYLON PANEL 464 CBR MISSING/DAMAGE(<P>#2 ENG INBOARD PYLON PANEL 464 CBR P/N: 313U8660-11 DAMAGED AREA REPAIRED IAW RI-54-00-15813 REV.A</P>)SDR SWAA2022080838762Nozzle · cracked#2 ENGINE PRIMARY EXHAUST NOZZLE PERFORATED FACE SHEET HAS A CRACK IN ZONE 2 AT THE 6:00 POSITION MEASURING 1 INCH IN LENGTH; 13 INCHES FWD OF THE AFT WELD LINE. / [01] REMOVED AND REPLACED #2 ENGINE PRIMARY EXHAUST NOZZLE IAW AMM 78-11-01.SDR SWAA2022080940112Strut · cracked#2 ENGINE RTF STRUT #1 HAS .500 CRACK AT LOCATION C2 FWD SIDE OF WELD AT CENTER OF CUTOUT / [01] ENGINEERING ADDED EA# M-21-172-00811; REFERENCE BARCODE# TTG8Q00E05YP.SDR CALA2022080301942Screw · missingPDA 3 SCREW MISSING FROM OUTBOARD SIDE OF #1 PYLON APPROX 2 FT FROM LEADING EDGE REPLACED MISSING SCREWSDR IXXA2022090405None · elongated#2 ENG/PYLON PANEL 446CL HAS 2 EA ELONGATED FASTENER HOLESSDR IXXA2022090401None · gouged#1 ENG. I/B CORE COWL #2 RIB FROM AFT HAS GOUGE. 00-114 REF VT-SAA NR B000315SDR IXXA2022090404Stiffener · worn#2 ENG INBD PYLON ACCESS PANEL AFT LANDING 434AL WORNSDR UIEA2022072600781Pylon · abnormalDEVIATION FOUND DURING PERFORM SB 747-54A2245 ON BOTH SIDES OF #1 & #4 PYLON(1) ACCOMPLISHED EI T2022A54M-1980 REV 1. 2) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR IXXA20220903001None · chafed#2 ENG UPPER PYLON LANDIN FOR FAIRING 441AT HAS AREAS OF CHAFFING. 18-027SDR IXXA20220802801Channel · cracked#2 AFT STRUT OUTBD J CHANNEL CRACKED AT 2 PLACES AT APPROX NAC 400.18-003 REF VT-SAA RN B000365 ATI-54-822-00-02SDR FDEA202207201775None · crackedLH PYLON O/B SIDE PANEL AT RIB8 FOUND 1EA CRACK REPAIRED THE CRACKED LH PYLON O/B SIDE PANEL AT RIB8 PER EO: 6-5450-7-5003 I PT3 & A300-600 SRM54-51-31-201-2. EO TITLE: NACELLES/PYLONS - INSPECTION OF PYLON SIDE PANELS AT RIB8. AIRBUS SB A300-54-6015 R03 &SDR CALA2022072001813None · crackedTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/20/22. PDA 2 #1 ENG OUTBD T-R TO PYLON FLEX SEAL - AFT MOST LOCATION - CRACKED AND MISSING PIECE AT FWD CORNER. REPLACED #1 ENG OUTBD T-R TO PYLON FLEX SEAL, ALL OK.SDR IXXA2022071503Flange · brokenINBOARD FLANGE OF STINGER ATTACH FLANGE.IS BROKEN.SDR AALA202207182104Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: AFTER REMOVAL OF NUMBER 2 PYLON PANEL 444CL DISCOVERED BOTH UPPER AND LOWER HINGES ON THE PYLON TO BE WORN ATTRIBUTING TO EXCESSIVE PLAY ON 444CL. REMOVED AND REPLACED 2EA HINGE BASE PART NUMBER 659W1190-1 BATCH: 0003970270 AT NO SDR AALA202207185353Fitting · wornAIRCRAFT IN BASE MAINTENANCE: AFTER THE REMOVAL OF NUMBER 2 ENGINE PYLON AFT FAIRING UPPER AFT MOUNT BOLT DISCOVERED THE WING ATTACH LUG IS WORN. REMOVED AND REPLACED 1EA LVG (FITTING ASSEMBLY) PART NUMBER 112W7110-6 PER B777-200 SRM 51-40-02-06.SDR 2022F00294None · corrodedKSHV-DURING INSPECTION OF #2 ENGINE INLET POSSIBLE CORROSION WAS FOUND UNDER ACOUSTIC PANEL. MAINTENANCE REMOVED AND REPLACED CORRODED #2 ENGINE INLET T-BRACKET WITH A NEW FABRICATED ONE IAW MD-11 DRAWING AJC8118. AIRCRAFT IS GOOD FOR CONTINUED SERVICE.SDR IPXA2022070883967Web · crackedINSPECTION TYPE:SEGPYLON 1 WEB BEHIND BUTTERFLY PANELS 413 AL AND 414 AR IS CRACKED.ACCOMPLISHED WELD REPAIR PER SRM 54-50-00.SDR IXXA2022082602Stiffener · elongated#2 AFT STRUT INTERIOR AT APPROX NAC 400 OUTBD STIFFENER HAS BOLTS WORN THROUGH.SDR MK1Y20220706017Repair · discoveredENG@ 2 - STRUT FAIRING - OUTBRD SIDE - NAC STA 304.5 - NAC STA 307.9 - - DURRING MAINTENANCE AT IAI - EXISTING UNDOCUMENTED REPAIR WAS FOUND ON STRUT OF ENGINE #2, OUTBRD SIDE FAIRUNG SKIN.SDR MK1Y20220706010Repair · discoveredSTRUT # 2, INBD SIDE, SKIN 313T3310: DURING MAINTENANCE PRACTICES AT IAI IN TLV, AN EXISTING UNDOCUMENTED DOUBLER REPAIR WAS FOUND ON STRUT # 2 INBD SIDE, ON SKIN 313T3310. THE SKIN IS MADE FROM TWO BONDED SKINS OF ALCLAD 2024-T3 0.063” AND 0.040” IN THICKNESSSDR MK1Y20220706007Repair · discovered: ENGINE #1, STRUT FAIRING, INBD SIDE, NAC STA 304.1 – NAC STA 311.1: DURING MAINTENANCE INSPECTION AT IAI, THE EXISTING UNDOCUMENTED REPAIR WAS FOUND ON THE STRUT FAIRING AT DATUM LOCATION.SDR MK1Y20220706004Repair · discoveredENGINE #2, STRUT ACCESS PANEL 446BR, NAC STA 249 – NAC STA 253:
DURING MAINTENANCE INSPECTION AT IAI, EXISTING UNDOCUMENTED REPAIR WAS FOUND ON ENGINE #2, STRUT, ACCESS PANEL NO. 446BR.SDR FDEA202206301748None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #1 PYLON O/B SIDE, AT RIB 8 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERSDR FDEA202206301749None · unknownAIRCAFT REPAIR ASSESSMENT EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #2 PYLON O/B SIDE, AT RIB 8 POSITION COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERSDR FDEA202206301747None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #1 PYLON I/B SIDE, AT RIB8 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERMSDR FDEA202206241580Clevis · noneREPAIR ASSESSMENT: R/H PYLON, APPROX. XORS346, AFT CLEVIS HAS PREVIOUS REWORK TO ARB7524-2. REF. DOT #57. PART WAS PREVIOUSLY TRIMMED, OK FOR SERVICE PER BOEING SERVICE REQUEST 1- 638111991-1, 1-638111991-2..SDR FDEA202206211489Shear Tie · cracked#2 PYLON UNDER PANEL #447BL FWD UPPER BRACKET CRACK AT NAC STA 296 REMOVED & REPLACED SHEAR TIE IAW B767 SRM 51-40-02 & BAC DWG 313T2310, SHEET 95, REVISION -SDR 2022F00263None · noneRIGHT ENGINE PYLON PANEL (P/N 7412311-4 MISMATCH). ACCOMPLISHED TEXTRON AVIATION LETTER DQ35192M1 DATED JUNE 15, 2022; 680A-0063 (N525QS) RIGHT ENGINE PYLON PANEL (P/N 7412311-4 MISMATCH).SDR 2022F00259None · noneLEFT ENGINE PYLON SKIN DAMAGE (WAVY). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ35118M1 DATED JUNE 10, 2022; 680A-0063 (N525QS) LEFT ENGINE PYLON SKIN DAMAGE (WAVY).SDR UIEA2022060200564Panel · cracked#1 PYLON AFT FAIRING O/B #3 FRAME MONOLITHIC PANEL AFT UPPER CORNER FASTENER HOLE FWD CRACK(<P>#1 PYLON AFT FAIRING O/B #3 FRAME MONOLITHIC PANEL AFT UPPER CORNER REPAIRED AS PER RI-54-52-15664 REV A</P>)SDR UIEA2022060200563Panel · cracked#1 PYLON AFT FAIRING I/B #3 FRAME MONOLITHIC PANEL FWD UPPER CORNER FASTENER HOLE FOUND CRACK(I/B #3 FRAME#1 PYLON AFT FAIRING MONOLITHIC PANEL FWD UPPER CORNER REPAIRED AS PER RI-54-52-15663 REV A)SDR IPXA2022062283366Skin · corrodedINSPECTION TYPE:SEG3#2 ENGINE PYLON OUTBD INNER SKIN AT APPROXIMATELY STA PPS 130 HAS SURFACE CORROSION FWD OF PRECOOLER OPENINGREPLACED PYLON SKIN PER BOEING DWG 311N5002 AND B757-200PF SRM 51-40-02-0GSDR CALA2022060601445Screw · missingPDA 3 ONE SCREW MISSING ON RH OUTB. PYLON PANEL P/N: 711Z8350-7 ITEM DEFERRED IAW ECRA # 5450-02741 OK TO CARRY FOR PERMANENT REPAIR WITHIN 10 FLIGHT CYCLES WITH TOMC-APPROVAL FROM SC1ELBYC COMMENT REPETITIVE RECHECKS PRIOR TO EACH DEPT PER ECRA 5450-02741. PHSDR FDEA202206021361Skin · corrodedRH PYLON BOLT HOLE #2 HAS DAMAGE INDICATION. CLEANED HOLE #2 BY REAMING TO .624 IAW SRM 51-40-05 AND EA # F-5730-T0368661 P1. PERFORMED ROTO-PROBE AT HOLE #2 IAW NTM 51-00-16. NO DAMAGE NOTED. WING- PLATES AND SKINS-RH WING, UPPER SKIN AND DRAG FITTING, HOSDR UIEA2022052600546Bushing · elongated#3 PYLON TORQUE BOX INNER AREA NAC STA 298.93 BLEED AIR DUCT R/H SUPPORT ROD LWR DUCT SIDE ATTACHED BOLT HOLE FOUND ELONGATION LINE REAM 2EA AFFECTED BUSHING HOLES AND FABRICATE 2 EACH BUSHING AS PER HX RI-36-11-15646 REV A</P>)SDR DALA2022060603935Bushing · corrodedSHIP 666 CORRISION ON INB. BUSHING AT FWD UPPER LINK ATTACH FITTING (RH PYLON). CORRECTIVE ACTION: SUMMARY OF NRC 00404. INB. BUSHING AT FWD UPPER LINK ATTACH FITTING (RH PYLON) WAS REPLACED BY A NEW BUSHING PER B757-200 SRM. (2259747)
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