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 IPXA2023070502656Pylon · unknownFAULT: #1 PYLON DRAG FITTING REMOVAL APPLIED TOPCOAT I/B UPPER DRAG FITTING SKIN IAW E.O B757-5710-69618-I. REVIEWEDSDR V0XD20230622002Duct · cracked#1 ENGINE UPPER COWL DRAIN ASSEMBLY CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED #1 ENGINE DRAIN ASSEMBLY IAW EMB 145 SRM 51-40-02.SDR UIEA2023052300518Unknown · unknownCORROSION - #2 ENG LH CORE COWL OUTER SURFACE(<P>1) REPAIR DAMAGE AREA IAW EI T2023A71M-1181 REV 0. 2) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR ABXA202306 23131Seal Depressor · gougedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE REPORTED GOUGE DAMAGE ON THE NO. 2 STRUT, OUTBOARD FIRE SEAL DEPRESSOR (113T4011-14). THE POST-BLEND MEASUREMENT IS 0.051 REMAINING MATERIAL FROM INITIAL THICKNESS OF 0.075-INCH THICK (MEASURED). NO PSDR IPXA2023070544029Pylon · corrodedFAULT: #1 ENGINE PYLON OUTBD SIDE INNER SKIN FWD OF VENT PANEL OPENING HAS EXFOLIATION CORROSION. DOT 8-001 PLACED ON OUTSIDE VERIFIED REPAIR COMPLETED PER E.O. 87155-REQ1 AND VTMAE E.A. 757-5450-27-A3238 REV. JOB COMPLETED. REVIEWED.SDR FDEA202305171059Skin · burnedL/H STRUT OUTBD HAS SIGN OF BURNT AT PPS. 174.3 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.Z # F-5450-T0374528 L/H STRUT STRUCTURE - OUTBOARD SIDE SKIN PANEL - BURN DAMAGE MAJOR REPAIRSDR FDEA202305170889Fitting · cracked#1 PYLON, I/B DRAG BRACE FITTING REQUIRES REPLACEMENT. ALSO O/B FITTING. REMOVED AND REPLACED I/B & O/B DRAG BRACE FITTINGS ON # 1 PYLON PER EA # T F-5730- T0374307 P1. "WINGS-PLATES AND SKINS- LH WING UPPER SKIN AT PYLON DRAG FITTING, CRACK FINDINGS *THIS SDR HNAA2023062600225Unknown · unknown00198 L/H LOWER PYLON SKIN T/E HAS 1EA. DENT ON THE I/B SIDE THAT MEASURES 1" DIA.X 0.008" DEEP. REPAIRED LH LOWER PYLON SKIN T/E 1EA DENT ON THE IB SIDE IAE EMB145 SRM 54-50-01 REPAIR #4SDR SWAA2023061248061Panel · crackedENG # 1 FORWARD THUMBNAIL PANEL # 431AT WITH CRACKED I/B AND O/B EDGE METAL FINGER SEALS<[01] REMOVED AND REPLACED ENG #1 FORWARD THUMBNAIL PANEL # 432AT IN REF WITH SRM 51-40-02;[02] REMOVED AND REPLACED ENG #1 FORWARD THUMBNAIL PANEL # 432AT I/B AND O/B METASDR SWAA2023061248154Panel · crackedENG # 2 FORWARD THUMBNAIL PANEL # 441AT WITH CRACKED I/B AND O/B EDGE METAL FINGER SEALS<[01] REMOVED AND REPLACED ENG#2 FORWARD THUMBNAIL PANEL # 441AT I/B AND O/B EDGE METAL FINGER SEALS;[02] REMOVED AND REPLACED ENG#2 FORWARD THUMBNAIL PANEL # 441AT I/B ANDSDR DALA2023051303794Unknown · unknownAIRCRAFT 3116, CORROSION SPIGOT RECEPTACLE FITTING LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT RECEPTACLE FITTING LH PYLON MEASURE OF FIRST CASE DIAMETER IS 4.341 INCHES TOOL USED: DIGITAL CALIPER P/N500-196-30 S/N A20230758. (LP 2764257)SDR SWAA2023052546994Skin · pulled#1 ENGINE INLET HAS FASTENER PULLED THROUGH LIP SKIN OUTER SURFACE 2 O'CLOCK POSITION.<[01] PERFORMED NDT ON FASTENER HOLE PER NDT PART 6; 51-00-00 PROCEDURE 16. NO DEFECTS NOTED.;[02] REMOVED LOOSE FASTENER. REAMED HOLE AND COUNTERSUNK FOR OVERSIZE FASTENER ISDR UIEA2023050900437Unknown · unknownLEFT NACELLE STRUT # 1 AFT FAIRING O/B FWD INSPECTION PANEL HAS ONE SCREW LOOSE .(<P>SECURED SCREW AT L/H NACELLE STRUT #1 AFT FAIRING IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR DALA2023050803560Unknown · unknownSHIP 3242 ON WALK AROUND FOUND FAIRING MISSING ON TOP OF ENG #1. CORRECTIVE ACTION: INSTALLED NEW PANEL. OK FOR SERVICE. (4697218)SDR CALA2023051201485Panel · missingPDA 3 #2 ENGINE PHLON OUTBD AFT PANEL 486AR IS MISSING ONE EA SCREW INSTALLED MISSING SCREW ON PANEL 486AR, #2 ENGINE OUTBD PYLON. REF AMM 54-53-11SDR DALA2023050803598Unknown · unknownSHIP 6707 A.D.//A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW; HOLE #1 GOUGES ON FITTING BTW 1 AND 4 O'CLOCK POSITION, HOLE #2 CORROSION ON SKIN BTW 3 AND 5 O'CLOCK POSITION AND FITTING BTW 9 AND 11 O'CLOCK POSITION, SDR MK1Y20230503022Unknown · unknownSTRUT #2, AFT FAIRNG - TRAILING EDGE, RH AND LH, NAC STA 410 TO 413: DURING MAINTENANCE INSPECTION AT IAI FACILITES, SHOP DISCOVERED UNDOCUMENTED DOBULER REPAIR IN STRUT #2, SKIN PANELS, ON BOTH SIDES.SDR MK1Y202305173015Unknown · unknownDURING CONVERSION OF S/N 25354, MAINTENANCE WAS REQUIRED TO REPLACE ENGINE #2 INLET COWL. THE REPLACEMENT INLET COWL P/N 224-2101-563, S/N 0634RV860 PROVIDED BY COSTUMER. THE NOTED INLET COWL WAS INSTALLED ON A/C AND POLISHED. MAINTENANCE REPORTED CORROSION/PISDR YENA2023005020485Unknown · unknownDURING HEAVY MAINTENANCE: REF TOMX W/O 2195 NR 00310. CRACK SUSPECT IN INBOARD FITTING SPAR AT RH PYLON; REF TOMX W/O 2195 NR 00310. INBOARD FITTING SPAR AT RH PYLON WAS REPLACED PER EMB-190 S.R.M. 51-43-03 AND S.R.M. 51-43-04.SDR CALA2023050301348Seal · missingPDA 3 #1 ENGINE INBOARD TR FLEX SEAL SEGMENT DEPARTED AIRCRAFT. REPLACED DAMAGED PANEL.SDR GTIA2023050437154Unknown · damagedGOUGE ON PYLON #1 CANTILEVER. RAF01 3117468-02 CREATED -VERIFIED LTPR J/C # 5001231319-0010 HAS BEEN ACCOMPLISHED AND COMPLIED WITH EA 5452-2310 REV. 00.SDR CALA2023050301318Spar Web · crackedDURING A MAINTENANCE 8C CHECK VISIT AT HAECO-HKG INSPECTION FOUND #1 PYLON STRUT [P/N: 311T2290-81, S/N: 000436], FWD UPPER SPAR WEB P/N: 311T2111-9 WAS FOUND WITH CRACK AT LH NAC STA 223 POWER FEEDER CABLE. TO INSPECT THE #1 PYLON FWD UPPER SPAR WEB AT LH NACSDR FDEA202305020795Stiffener · cracked#2 PYLON HYDRAULIC BAY FWD BULKHEAD UPPER STIFFENER ANGLE IS CRACKED IN THE CORNER. REMOVED AND REPLACED STIFFENER ANGLE PER BAC DWG 313N302 REV BSDR SWAA2023053043795Bracket · broken#2 ENGINE STRUT O/B FIRE SEAL BRACKET (P/N 311A2683-16) UPPER FLANGE IS BROKEN<[01] REMOVED #2 ENGINE STRUT O/B FIRE SEAL BRACKET P/N 311A2683-16 IAW SRM 51-40-2-0G-0;[02] UPDATED PARTS REQUIREMENTS;[03] ADDED; AND UPDATED STEP #1;[04] INSTALLED NEW #2 ENGINE SDR HALA2023042800020Unknown · unknown(S/M) S/C FOUND ON RH UPPER PYLON T/E ON UPR SFC (MARKED). REPAIRED PER E105-B10616-PERM.SDR FDEA202304240751Unknown · cracked#1 PYLON APPROX NAC STA 377 AFT OF PANEL 437BL, INSIDE AFT FAIRING HAS LEFT SUPPORT BRACKET CRACKED REMOVED AND REPLACED CLIP IAW B767 SRM 51-40-02 AND BAC DWG 313T2303, SHEET 176, REVISION ASDR SWAA2023042630388Fairing · crackedCRACK; #1 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY<[01] R&R #1 ENGINE PYLON AFT STRUT SUPPORT FAIRING TIP ASSY PER SRM 51-10-02 AND SRM 51-40-02. EDGE SEALED NEW PART PER AMM 51-31-00SDR SWIA202305222Bracket · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 5/18/2023) REMOVED AND REPLACED INBD STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF. REO 670-54-21-971 REV. A, 2017/05/11 AND BOMBARDIER DWG CN624-2005 REV. T. COMPLIED WITH SKYCARD 51SDR SWIA202305221Bracket · crackedR/H UPPER TRANSCOWL INBD "A" BRACKET IS CRACKED (C-CHECK RO 5/18/2023) R/H UPPER TRANSCOWL INBD CRACKED A" BRACKET HAS BEEN REMOVED AND REPLACED BY COMPLYING FULLY W/REO# 670-54-21-971, REV A, DATED 5/11/17 AS WELL AS SKYCARD 51-900-1002-SKY.SDR DALA2023041803069Universal · looseSHIP 6702 REF RH ENG DRAG FTG CLAMP -UP 757-INSP SECTION 02, CARD 5720- 01100-02B STEP 13, FASTENER #18 FOUND LOOSE NO DOT. CORRECTIVE ACTION: INSTALLED NEW FASTENER AT HOLE #18 IAW B757-200 SRM 51-40-02 AND EO#5720-01100-05B ERA 576632-14AD. (2717865)SDR VNAA202304270010Acoustic Liner · dentedDENT AT 7:00 O'CLOCK POSITION CLOSE TO THE LEADING EDGE ON METAL PERFORATE ACOUSTIC LINER OF RIGHT FORWARD CORE COWLSDR EE4Y2023041017578Pylon · damagedDURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR LOCATED AT LH PYLON, HEAT SHIELD BAY 8 WAS FOUND. MENTIONED REPAIR IS SIMILAR TO SRM 54-50-23 REPAIR 52, EXCEPT THE EXISTING TRIM IS LARGER THAN THE SRM FIGURE 2. WAS REPAIRED FOLLOWING EMB REPAIR INSTRUCTIONSDR EE4Y2023041017571Pylon · corrodedDURING THE ACCOMPLISHMENT OF SB 190-57-0056, CUSTOMER FOUND THE RH PYLON, INBOARD AND OUTBOARD SPARS LUGS
BUSHING WITH CORROSION. WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER ETD2023-190-004146 REV A AND COOPESA EO# COO-EO-2023-17184-R00 AND APPROVED ON ASDR EE4Y2023041017570Pylon · corrodedDURING THE ACCOMPLISHMENT OF SB 190-57-0056, WAS FOUND THE LH PYLON, INBOARD AND OUTBOARD SPARS LUGS
BUSHING WITH CORROSION. WAS REPAIRED FOLLOWING REPAIR INSTRUCTIONS UNDER EDT2023-190-004140 REV / AND COOPESA EO# COO-EO-2023-17181-R00 AND APPROVED ON ANAC FSDR SWAA2023041124770Fairing · cracked#1 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY CRACKED ON SUPPORT FITTING.<[01] REMOVED DAMAGED #1 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY . PER SRM 51-40-02;[02] LOCATED AND DRILLED NEW STRUT FAIRING PER SRM 51-40-05.SDR DALA2023041102837Unknown · unknownSHIP 6805 AWR IN REF TO ER/A 600262-14 REV. ORIGINAL, SECTION.III: PERMANENT REPAIR, STEP 1: SUNKED FASTENERS (10EAS) AND CORROSION ON FASTENER (1EA) WERE FOUND ON SURROUNDING STRUCTURE AT AFT STRUT FAIRING RH. CORRECTIVE ACTION: SUMMARY OF NRC 00179 FASTENERSSDR DALA2023042703313Unknown · unknownSHIP 6805 ER/A 607761-14; PYLON #2 / AFT STRUT FAIRING / SKIN, INBD & OUTBD SIDE / NAC STA. 274 TO 279 / FASTENER CORROSION. CORRECTIVE ACTION: REF ERA 607761-14. (2708770)SDR FDEA202304060576Attach Angle · cracked#1 PYLON AFT FAIRING, 2EA FRAME ATTACH CLIPS ARE CRACKED ON INBD AND OUTBD SIDES AT NAC STA 376 REMOVED AND REPLACED CLIPS IAW B767 SRM 51-40-02 AND BAC DWG 313T2303, SHEET 146, REV -SDR FDEA202304060570Panel · delaminated#1 PYLON PANEL 432AL AFT 2 CORNERS ARE DELAMINATED AND DAMAGED. ACCOMPLISHED PERMANENT REPAIR OF PANEL PER B757 SRM 51-40-02, 54-50-70-0G, 51-70-17-0G AND BOEING DWG 313N5003.SDR HNAA2023042800131Unknown · unknownE968207 RH ENGINE YOKE ASSY HAS POSSIBLE CRACK AT FWD OTBD LOWER CORNER. REPAIRED IAW PIEDMONT FCD1-54-21-0017 REV D, REPLACEMENT OF RH FWD YOKE LINKAGE FITTINSSDR FDEA202304030555Unknown · unknown#1 PYLON AFT FAIRING MID-FRAME IS CRACKED IN UPPER INBD CORNER AT APPROX NAC STA 330. REPAIRED #1 PYLON AFT FAIRING MID FRAME IAW B767-300 SRM 54-52-71-2R & BAC DWG 313T2303 REV - REMOVED AND REISTALLED LATCH BEAM IAW BAC DWG 313T2303 REV -SDR FDEA202304030554Unknown · cracked#2 PYLON, OB SIDE, FRAME JUST AFT OF HYDRO BAY DOOR HAS A CRACKED ANGLE REMOVED AND REPLACED CLIP IAW B767 SRM 51-40-02 & BAC DWG 313T2303, SHEET 146, REV-SDR SWAA2023040422769Fairing · crackedREPAIR - CRACK; #2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY<[01] REMOVED TRAILING EDGE FITTING;[02] REMOVED AND REPLACED AFT. END STRUT FARING SEGMENT PER SRM 51-20-02.;[03] CORRECTIVE ACTION STEP 2. IT SHOULD BE: <BR>REMOVED AND REPLACED AFT. END STRUT FARSDR 2023FA0000179Unknown · unknownDURING MAINTENENCE INSPECTION FOUND A BLEND OUT, DENTS AND FILLING REPAIRS ON ENGINE #1 (PW4000) INLET COWL ACOUSTIC PANEL BETWEEN 5 AND 7 O'CLOCK.SDR 2023FA0000164Unknown · unknownDURING MAINTENENCE INSPECTION FOUND UNDOCUMENTED REPAIRS ON ENGINE #2 (PW 4000) INLET COWL ACOUSTIC PANEL BETWEEN 3 AND 11 O'CLOCK - A HI-LOCK REPAIR, A BLEND OUT, SIX DENTS AND FIVE FILLINGS.SDR IPXA2023032892371Pylon · crackedINSPECTION TYPE:CK1C#1 PYLON RIB FWD OF PRE-COOLER CRACKED, (RIB 3)REMOVED AND INSTALLED RIB ARCH IAW SRM 51-40-21.SDR COEA2023051606913Panel · chafedWP 242864 NR 400019 HEAVY CHECK COE/MAJOR REPAIR: R/H ENGINE NACELLE INBOARD REBATE PANEL FOR 485AL AND 487AB HAS CHAFE DAMAGE. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00214475_01...20634 ISSUE A, DATED 5/5/2023.SDR A6WA202303258530Bonding Plate · corrodedL/H PYLON UPPER SURFACE OUTBOARD BONDING PLATE IS CORRODED. *********AIRCRAFT REMOVED FROM SERVICE********* REPLACED PYLON BONDING PLATE IAW TS 15-335 DATED 12/22/2015.SDR VNAA202302040033Fireshield · damagedDURING FORWARD CORE COWL FIRESHIELD DAMAGE REPAIR WITH NRC 00089, HONEYCOMB CORE FORWARD EDGE WAS DRILLED (4 BY 4 INCH SQUARE)SDR FDEA202303240500Fitting · corrodedDURING ROTO -TEST OF HOLES 3 AND 8 OF THE L/H WING NDT RECEIVED CORROSION INDICATIONS DOCUMENTED ON F-5730-E0340076 P1, JPF STEP 7. COMPLIED WITH EA # F-5740-T0373064 P1. TITLE: WINGS - ATTACH FITTINGS - LH WING, UPPER SKIN, DRAG FITTINGS, CRACK INDICATION
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