JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 SWIA2020021148427Liner · chafed*RH ENGINE FWD CORE COWL INTERNAL LINER CHAFED THROUGH AT FWD SIDE OF DRAIN PAN FROM CONTACT WITH ENGINE HARNESS. (C-CHECK) RO 2/07/2020 REMOVED AND REPLACED R/H ENG INTERNAL FWD CORE COWL DRAIN PANS IAW CRJ700 SRM AND AMM.SDR REXA2020010710042Hinge Fitting · cracked"DAMAGE T: DURING LH ENGINE COWLS CLOSE UP THE FAIRING 433BB HIT THE LWR TRANSCOWL INBD FAIRING. BOTH THE TRANSCOWL FAIRING AND THE FAIRING 433BB ARE BENT AND WITH SCRATCHES.
"TRANSCOWL HINGE FAIRING WAS REPAIRED PER CRJ-9SDR ABXR2020010131349Beam · crackedUPPER FWD PYLON TRANSVERSE BEAM CRACKED ON OUTBOARD SIDE OF THE NR 2 PYLON.SDR HYIA20191231001Beam · damagedDURING MAINTENANCE, WORKING FASTENERS WERE IDENTIFIED ON THE RH OUTBOARD BEAM'S, AFT ENGINE MOUNT'S FORWARD MOUNTING BLOCK. THIS BLOCK P/N 5654130-202 WAS INSTALLED AS PART OF THE SK414-19B SERVICE KIT AND IS LOCATED ON THE OUTBOARD FACE OF THE BEAM. UPON RESDR DALA2019123107630Access Door · missingFND ON ARRIVAL, NBR 2 ENG MISSING STARTER VALVE ACCESS DOOR. REPLACED NBR 2 ENGINE LOWER FWD COWL PER MD88 AMM 71-10. COWL ROBBED OFF SHIP 963. (LP6748864)SDR SWAA2022041235387Fairing · crackedWHILE OPENING #1 SAIL TAIL TO ROB FOR A/C 8664 FOUND AFT FAIRING CRACKED AT NAC STA 352.750. P/N 313A2752-2 / REMOVED AND REPLACED #1 SAIL TAIL AFT FAIRING ASSEMBLY IAW SRM 51-40-02-0G-0 AND DWG 313A2400 REV. B PN: 313A2752-1 ATAG: CM376SDR REXA2020010770005Spigot · worn"INITIAL INSPECTION : WEAR ON SPIGOT AT LATCH DOOR ASSEMBLY OF LOWER HALF TRANSCOWL LH ENGINE ( MOT 1 )
"SUMMARY OF NRC 00049: SPIGOT AT LATCH DOOR ASSEMBLY OF LOWER HALF TRANSCOWL LH ENGINE WAS REPLACED PER CRJ-900 SRM 5SDR REXA2020010700002Latch · damaged"INITIAL INSPECTION : ELONGATED HOLE ON COAMING LATCH DOOR AT LOWER HALF TRANSCOWL RH ENGINE ( MOT 2 )
"SUMMARY: ON NRC. 00038 COAMING LATCH DOOR, DOUBLER COAMING LATCH DOOR AND PAD BEARINGAT ON LOWER HALF TRANSCOWL RH ESDR DALA2019122707562Strut · crackedNR 1 STRUT FOUND CRACKED AT THE FWD CORNER OF THE FWD MIDSPAR WEB CUTOUT. THE NR 1 STRUT FWD MIDSPAR WEB CUTOUT AT THE FWD CORNER CRACKED AREA REPAIRED IAW PRI583697-14 REV.0.SDR REXA2020010750004Latch · damaged"INITIAL INSPECTION : ELONGATED HOLE ON COAMING LATCH DOOR AT UPPER HALF TRANSCOWL LH ENGINE ( MOT 1 )
""SUMMARY:ON NRC 00046: DOUBLER COAMING LATCH DOOR WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01 AND SRM 51-42-06SDR REXA2020010740003Spigot · worn"INITIAL INSPECTION : WEAR ON SPIGOT AT LATCH DOOR ASSEMBLY OF UPPER HALF TRANSCOWL RH ENGINE ( MOT 2 )
"SUMMARY OF NRC 0040: SPIGOT AT LATCH DOOR ASSEMBLY OF UPPER HALF TRANSCOWL RH ENGINE WAS REPLACED PER CRJ-900 SRM 51SDR SWIA2020011447668Frame · chafedR/H AFT PYLON FAIRING FRAME 1 INBD PIP PIN ATTACH POINT HAT BUSHING MIGRATED OUT. (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED R/H AFT PYLON FAIRING FRAME 1 REF EMB SRM.SDR DALA2019122427528Clamp · crackedLH ENG DRAG FTG CLAMP-UP & DIAG BRACE, STEP 27. CRACK INDICATION WAS IN HOLE NR 13, WAS FOUND. REPLACED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR DALA2019122327489Shim · migratedMIGRATED SHIM ON DRAG FITTING/FRONT SPAR, AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE. REPLACED PER ERA 583990-14AD REV. ORIG. SECTION 1 AND ETI-57-19-190 REV 13.SDR ABXR2019122100331Doubler · corroded#1 PYLON CORRODED STA 204SDR DALA2019122007449Strut · crackedMTC TASK - NO.1 STRUT FWD UPPER SPAR I/B CHORD AT NAC STA 230 FOUND CRACK. C/A THE CRACK AT NO.1 STRUT FWD UPPER SPAR I/B CHORD NAC STA 230. REPAIRED AS PER PRI 583479-14 REV.O COMPARED AND COMPLETED WITH THE ERA #583479-14 REV. ORIGINAL ASSOCIATED ER/A 14-583SDR REXA2019123051839Door · damagedWORN AND BENT CUTOUT OF THE COWLING LATCH DOOR FOR THE RT NACELLE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01, AND SRM 51-42-21-001-001-A01.SDR REXA2019123051838Latch · wornWEAR FOUND ON THE COAMING LATCH DOOR AT THE TRANSCOWL FOR THE RT ENGINE. THE COAMING LATCH DOOR WAS REPLACED IAW SRM 51-42-13-001-001-A01.SDR REXA2019123041837Pad · wornWEAR WAS FOUND ON THE BEARING PAD LATCH DOOR FOR THE RT ENGINE TRANSCOWL. THE PAD LATCH DOOR FOR THE RT ENGINE TRANSCOWL WAS REPLACED IAW SRM 51-42-06-001-001-A01.SDR 2DYA201912163001Fairing · brokenDURING "C" CHECK AT SEMAN-PERU DAMAGE WAS FOUND ON THE OUTER ALUMINUM FAIRING AS WELL AS DAMAGE TO THE COMPOSITE MATERIAL ON ENGINE #2 BETWEEN THE 7 O'CLOCK AND 12 O'CLOCK POSITIONS. AN ENGINEERING ORDER WAS WRITTEN TO ACCOMPLISH A LIMITED USE REPAIR FOR RETUSDR SWIA2020020348145Panel · gouged*PANEL 442AT TRAILING EDGE GOUGES/KNIFE EDGES (MARKED) (C-CHECK) RO:1/29/2020REMOVED AND REPLACED WORN R/H UPPER FAN COWL 442AT AFT EDGE STRIP P/N 228-50080-108 REF. CRJ 200 CMM.SDR SWIA2020020348141Structure · damaged*LH ENGINE NOSE INLET COWL LEADING EDGE HAS NUMEROUS NICKS AND 1 DENT (MARKED) (C-CHECK) RO:1/29/2020REMOVED L/H NOSE INLET-COWL ASSEMBLY REF CRJ-200 AMM. INSTALLED 1EA. SERVICEABLE, L/H NOSE INLET-COWL ASSEMBLY. REF. CRJ-200, AMM, ALL CHECKS GOOD. SDR GTIA2019121524859Structure · gougedGOUGE FOUND AT CANTILEVER STRUCTURE ( PYLON ) AT RIB 7-9 LH RH. DAMAGE LENGTH 8MM X WIDTH 5MM X 0.68 DEPTH, ORIGINAL STRUCTURE THICKNESS 0.8MM. RAF-01 2481725-2 OPENED.-SEE LOG PAGE 2481726-1 FOR CORRECTIVE ACTION.SDR FDEA2019120433167Structure · crackedRH PYLON TOP AFT SECTION I/B METAL STRIP CRACKED REPLACED STRIP P/N A5451532700103 ON R/H PYLON TOP AFT SECTION I/B SIDE IAW A300-600 SRM 51-40-21 AND AIRBUS DWG A54515326 ISSUE ESDR SWIA2020011947831Structure · dentedADM # 1714 LEADING EDGE OF THE RH ENG PYLON APPROX 5.125 IN FROM THE IB EDGE TO FUSELAGE. DENT DIA = .5 INCH DEPTH = .03125 INCH. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (SDR SWIA2020021848509Door · dentedADM # 6568. L/H ENGINE FWD LOWER FAN COWL DOOR BETWEEN FS 1031.00 AND FS 1047.00 AT THE 4 O'CLOCK POSITION. 1 DENT WITH IN LIMITS DEPTH OF DENT WAS .058 " LENTH WAS 1 INCH WIDTH WAS 18/32 INCH. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWOSDR 7C7A2019112500521Cowl Door · damagedDAMAGE LOWER COWL LHS EDGE MEMBER (P/N 87140380) BETWEEN XN 55.00 AND XN 60.00. PERMENANT REPAIR FOR DAMAGE LOWER COWL CONSISTS OF HAD DRESSING THE DAMAGED AREA BACK TO ORIGINAL CONTOUR, INSPECTING THE REWORK AREA FOR CRACK INDICATIONS(NONE PERMITTED), AND RESDR SWIA2019112246790Bushing · deteriorated* L/H ENGINE PYLON TIE BAR UPPER AND LOWER RUBBER BUSHINGS MIGRATED HALF WAY OUT OF TIE BAR AND ARE DETERIORATED. (C-CHECK) RO: 11/21/2019 REMOVED AND REPLACED 2 EA. BUSHINGS, LH PYLON TIE BAR UPPER AND LOWER PN J23553-5, IAW AMM. PERFORMED OPERATIONAL TESSDR SWIA2019112246784Beam · gouged* L/H ENGINE UPPER FWD CORE COWL LATCH BEAM GOUGED AT LUG 3. (C-CHECK) RO: 11/21/2019 REPAIRED L/H ENGINE UPPER FWD CORE COWL LATCH BEAM GOUGE AT LUG 3 IAW REO. ALL STEPS COMPLIED WITH. COMPLIED WITH SKYCARD. COMPLETED PAPER FORM M-337.SDR FDEA2019112213025Hinge · crackedRH PYLON TOP O/B METAL SEAL I/B T/R HINGE PANEL CRACKED REMOVED, REPAIRED, AND REINSTALLED #2 PYLON O/B EXTRUSION EDGING IAW AIRBUS DWG A54612094, ISSUE D AND A300-600 SRM 54-56-10, CONFIG-1, FIGURE 201. FEDEX EA: 6-5450-T0350729 P1. NACELLES/PYLONS - PYSDR FDEA2019112213023Skate Angle · cracked#1 PYLON BELLOW PANEL#411DL T/R SUPPORT SKATE ANGLE CRACK. REMOVED, REPAIRED, AND REINSTALLED #1 PYLON SUPPORT SKATE ANLGE EDGING IAW A300-600 DWG# A54612094 ISSUE D. FEDEX EA# 6-5450-T0350728 P1. NACELLES/PYLONS - PYLON FILLETS/ FAIRINGS PYLON FILLETSSDR FDEA201911192996Blowout Panel · gouged#1 ENGINE, INBOARD THRUST REVERSER, HINGE LATCH PANEL, UPPER FACE GOUGED 2 SPOTS REMOVED AND REPLACED BLOW OUT DOOR ASSY IAW MRAS CMM 78-32-00, FIG 703. EXHAUST SYSTEM - THRUST REVERSER GEN - #1 ENGINE I/B T/R HINGE LATCH PANEL - FASTENER. FASTENER.SDR REXA2019112671669Latch · cracked"INITAL INSPECTION : CRACKED COAMING LATCH DOOR AT LOWER HALF TRANSCOWL, RH ENGINE ( MOT 2 )
"SUMMARY: ON NRC. 00076, COAMING LATCH DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01
"SDR FDEA2019111542961Plate · cracked#1 ENG O/B CORE COWL L/E PLATE CRACKED AT LWR END REMOVED AND REPLACED FILLER PER FEDEX EA # F7110-T0350560P1SDR DALA2019111416644Structure · crackedONE CRACK AT 3 O'CLOCK AT RH, THE OTHER CRACK AT 9 O'CLOCK AT LH , ON NO.2 NACELLE REPAIRED PER 582281-14. (LP 1354911)SDR DALA2019111416643Structure · crackedONE CRACK AT AFT HOLES AT NSTA221.25 AT 3 O'CLOCK AT RH AT NO.1 NACELLE REPAIRED PER ERA 582284-14AD. (LP 1354604)SDR SWIA2019122747192Hinge · broken*RH ENGINE CORE COWL BLOW-OFF DOOR 444CB LATCH HINGE BROKEN. (C-CHECK) RO 12/24/2019 REMOVED AND REPLACED THE LATCH OF THE R/H ENGINE CORE COWL BLOW-OFF DOOR # 444CB. AS PER CRJ 700 SRM.SDR DALA2019111206577Spar Web · crackedFOUND CRACK ON NACELLE NO.2 FORWARD UPPER SPAR WEB AT WIRE BUNDLE CUTOUT. REPAIRED PER ERA 582362-014. (LP 1349229)SDR DALA2019111206568Spar Web · crackedFOUND CRACK ON NACELLE NO.2 FORWARD UPPER SPAR WEB AT FUEL SUPPLY LINE CUTOUT REPAIRED PER 582362-014 (LP 1349247)SDR DALA2019110605366Spar · not reportedDURING INSPECTION MAINTENANCE FOUND #2 PYLON FWD UPPER SPAR WEB / NAC STA 221.25-237.5 EQUIPMENT CUTOUTS. C/W ERA 582362-14 (LP 1348278)SDR SWIA2019122747401Rub Strip · chafed* RH ENGINE COWL PANEL 442AT AFT RUB STRIP CHAFED THROUGH. (C-CHECK) RO:12/24/2019 R/H ENGINE FAN COWL 442AT'S AFT EDGE STRIP HAS BEEN REMOVED AND REPLACED PER BOMBARDIER CMMSDR SWIA2019122747382Plate · corrodedLH UPPER PYLON TRAILING EDGE INBOARD BONDING PLATE HAS CORROSION . REMOVED AND REPLACED BONDING PLATE AT LH UPPER PYLON TRAILING EDGE INBOARD SIDE REF SRM AND DWG RESTORED FINISH REF SRMSDR SWIA2019122747375Panel · gougedR/H LOWER NACELLE PANEL 422DB HAS KNIFE EDGE ON SEPERATOR PLATE (C-CHECK) RO:12/24/2019 REMOVED AND REPLACED 2 EA SEPARATOR PLATES ON RH LOWER NACELLE PANEL 422DB REF CRJ200 SRM.SDR SWIA2019122747294Splice Plate · corrodedTOP OF RH PYLON AT F.S. 742.0 HAS CORROSION ON SPLICE PLATES (C-CHECK) RO:12/24/2019REMOVED AND REPLACED (2EA) SPLICE PLATES ON TOP OF R/H PYLON AT F.S. 742.0 IAW CRJ200 SRM AND CRJ200 AMM BOND CHECK GOOD OHMMETERSDR DALA2019102986246Support Beam · worn(AIRCRAFT 5640, L/P 1332181) WEAR ON OUTBD FAN COWL SUPPORT BEAM STA NAC 102 AT ENGINE 1 PYLON (MOT 1). CORRECTIVE ACTION: FAN COWL SUPPORT BEAM WAS REPAIRED PER ETI-57-19-145 REV: 1 AND ER/A: 582388-14 REV: ORIGINAL SEC. I.SDR C77A2020020530043Heat Shield · damagedDURING THE B6 BASIC CHECK AT EAMS, DAMAGE WAS DISCOVERED AT SCREW HOLES ON THE SPLIT RH PYLON HEAT SHIELD #1 PORTIONS (P/N 171-11315-401 AND P/N 171-11316-401). REFERENCE ETD2019-170-142741 FIGURE 1 FOR DETAILS. EAMS REQUESTED AND RECEIVED A PERMANENT REPAIR ISDR CALA2019102501827Screw · missingNMBR 1 ENGINE MISSING 2 FASTENERS AND A SCREW REPLACED MISSING SCREWS REF AMM 54-00-00.SDR DALA2019102836206Structure · damagedSHIP 6716 DURING INSPECTION, THE 4 AND 5 HOLES WITH CORROSION AND DEEP SCRATCHES WERE FOUND, AND HOLES 1, 2, 7, 8 AND 10 PRESENT ONLY DEEP SCRATCHES. CORRECTIVE ACTION: IN REFERENCE NRC S/N: 00499 HOLES #1,#2, #4, #5, #7, #8 AND #10 WERE REWORKED, THEREFORE WISDR GR4D20191023007Strap · corrodedRH PYLON UPPER SURFACE GVFS 808, STRAP,BOND-CONDUCTIVE,PYLON IS CORRODED IN MULTIPLE LOCATIONS. REQUIRED REPLACEMENT DUE TO EXTENT OF CORROSIONSDR GR4D20191023006Strap · corrodedLH PYLON UPPER SURFACE GVFS 860, STRAP,BOND-CONDUCTIVE,PYLON IS CORRODED IN MULTIPLE LOCATIONS. REQUIRED REPLACEMENT DUE TO EXTENT OF CORROSION
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