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 HYIA20170203001Beam · crackedTHE RIGHT NACELLE CROSSOVER BEAM ASSEMBLY WAS FOUND TO BE CRACKED AT AFT FACE IN THE AREA OF TURBOCHARGER MOUNT BRACKET HOLE LOCATIONS DURING DURING DISASSEMBLY OF TURBO CHARGER ASSEMBLY TO FACILITATE OTHER MAINTENANCE. CRACK LOCATED ADJACENT TO OB MOST TURBOCSDR SCNA20170201042Rub Strip · wornNR 2 NACELLE PANEL 441DL HAS WEAR MARKS. REMOVED AND REPLACED PANEL RUB STRIP.SDR IPXA2017021514073Strap · chafedINSPECTION TYPE: 3C, NR 2 PYLON SUPPORT FITTING CHAFED ABOVE AFT RT END OF PRECOOLER. REPAIRED THE SUPPORT FITTING IAW EO MD11-5410-63264-A, AND EA 011-5410-01-A6627.SDR IPXA2017021714130Hinge Fitting · chafedINSPECTION TYPE: 3C, NR 1 ENGINE OTBD FAN COWL FORWARD HINGE FITTING INBD AFT EDGE CHAFED. REPAIRED IAW EA 011-7110-01-A6617 REV. IR, AND EO MD11-7110-63265-A.SDR UIEA2017020100130Frame · damagedNR 4 PYLON FOUND HEAT DAMAGED ON AFT FAIRING NR 1 FRAMES. REPAIRED IAW R1-54-00-116REV A.SDR U2RA201701250002Bearing · corrodedNR 3 PYLON OUTBOARD DUAL SIDE BRACE UPPER BEARING RACE CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE BEARING IAW SERVICE BULLETIN 747-54A2218.SDR P5CA2017012600039Frame · crackedCRACKED FRAME ON NR 1 ENGINE NACELLE, NAC STATION 329. REMOVED THE DAMAGED FRAME IAW SRM 51-40-02-0G-0 REV 67. 2. INSTALLED A NEW FRAME IAW SRM 51-40-02-0G-0 REV 67 AND DWG 313T2303, SHEET 140, REV AND DWG 313T23, SHEET 144, REV, AND DWG 313T2303, SHEET 145SDR DALA2017012300548Web · crackedNR 2 PYLON UPPER WEB CRACKED AT GENERATOR CABLE FEED THROUGH. REPAIR C/W PER ERA 554545-14 REV 0 ON NR 72 AT C CK.SDR DALA2017012000546Structure · crackedNR 1 PYLON CRACKED AT CUTOUT FOR GENERATOR FEEDER CABLES. REPAIRED IAW ERA 554502-14 REV 0.SDR HYIA20170828004Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .171 IN LENGTH.SDR HYIA20170828003Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LT OUTBOARD NACELLE FITTING THE CRACK WAS DISCOVERED ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS .108 IN LENGTH.SDR P5CA2017011200018Rivet · wornNR 2 NACELLE HAS A WEAR STRIP RIVET WORN. REMOVED DAMAGE RIVET IAW SRM 51-40-02-0G-0 REV.67. INSTALLED NEW RIVET IAW SRM 51-40-02-0G-0 REV.67 AND CMM 71-13-23 REV 40.SDR P5CA2017011200017Rivet · wornWORN RIVETS NR 1 NACELLE. REMOVED DAMAGED RIVETS IAW SRM 51-40-02-0G-0 REV 67. INSTALLED NEW RIVETS IAW SRM 51-40-02-0G-0 REV 67 AND CMM 71-13-24 REV 43.SDR DALA2017011100249Structure · damagedHOLES ELONGATED ALONG FWD EDGE OF GENERATOR CABLE PASS THROUGH CUTOUT APPROX NACELLE STA 227 NBR 1 PYLON UPPER SURFACE. REPAIRED PER PRI 553929-14 REV 0-3. PRI 553929-14 REV 0-3 INSTRUCTIONS MATCH FINAL ERA 553929-14 REV A INSTRUCTIONS. (2844045)SDR DALA2017011100248Structure · crackedPYLON CRACKED AT CUTOUT WHERE POWER FEED WIRES PASS THRU TO UPPER PYLON. REMOVED AND REINSTALLED O/B T/R ON AMDS 7831-4202. PRI 553929-14 INSTRUCTIONS REV. 0-4 MATCH FINAL ERA 553929-14 REV. A INSTRUCTIONS. (2844042)SDR IPXA2017012513230Former · crackedINSPECTION TYPE:3C, NR 1 ENG LT T/R CORE COWL AFT UPPER FORMER IS CRACKED. REMOVED AND REPLACE LT T/R CORE COWL AFT UPPER FORMER IAW SRM 54-05-41. (MINOR)SDR DALA2016122210049Skate Angle · crackedNR 1 ENGINE PYLON SKATE ANGLE CRACKED. N: REMOVED AND REPLACED THE SKATE ANGLE.SDR FDEA201612174486Strut · damagedLEFT PYLON ABOVE FWD ENGINE MOUNT INSIDE FWD ACCESS PANEL HAS SEVERAL OPEN HOLES ON BOTH SIDES. COMPLIED WITH EA # F-5430-TO330415 P1, DRILLED & INSTALLED FASTENERS. MAJOR REPAIR.SDR REXA2016121102445Rub Strip · chafedLEFT ENGINE COWL PANEL 432AB TRAILING EDGE RUB STRIP IS CHAFED. REMOVED AND REPLACED THE RUB STRIP IAW IAW CMM 71-14-01.SDR REXA2016120902439Rub Strip · crackedRIGHT ENGINE COWL PANEL 442AT TRAILING EDGE RUB STRIP IS KNIFED EDGES AND CRACKED. REMOVED AND REPLACED RUB STRIP IAW CMM 71-14-01.SDR UIEA2016112200894Panel · bent#1 ENG O/B COWL CENTER ATTACH POINT, HINGED ACCESS PANEL BENT HAS SHARP EDGES FWD END (NRI3277)(<P>REMOVED DAMAGE FORM FWD EDGE OF ACCESS HINGED ACCESS PANEL IAW SRM 54-42-01. 80" MATERIAL REMOVED FROM EDGE. AREA FOUND TO BE WITHIN LIMITS IAW 54-42-01 FIG 101 SDR IXXA20170201034Beam · crackedNUMBER 2 PYLON LOWER BEAM UNDER RIGHT HYDRAULIC BAY DOOR CHAFED AND CRACKED AT FORWARD END. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-02 AND DRAWING 313T1380.SDR FDEA201612034318Support Frame · crackedNR 3 ENGINE PYLON, SUPPORT FRAME IS CRACKED. REPAIRED IAW EA 8-5410-T0330096 AND SRM 54-00-01 FIG 12 VOL 1.SDR V0XD2016120617Door · gougedRIGHT ENGINE NACELLE BLOWOFF DOOR STRIKER PLATE GOUGED OUT OF LIMITS. REMOVED AND INSTALLED A NEW NACELLE BLOW OFF DOOR STRIKER PLATE IAW SRM 51-42-13, AND SRM 51-42-06.SDR FDEA201611294290Spar · crackedNR 1 PYLON ACCESSED THROUGH PANEL 411CL LOWER SPAR OF CANTILEVER STRUCTURE IS CRACKED. REPAIRED IAW SRM 54- 52-11 FIG 201. MAJOR REPAIR.SDR FDEA201611294289Spar · crackedNR 2 PYLON LOWER SPAR OF CANTILEVER STRUCTURE IS CRACKED BETWEEN RIBS 8-11. REPAIRED NR 2 PYLON LOWER SPAR IAW SRM 54-52-11 FIG 201. MAJOR REPAIR.SDR UIEA2016113000937Hinge · wornNR 1 ENGINE FAN HOLD OPEN ROD PIVOT HINGE HAS EXCESSIVE PLAY. REPLACED IAW AMM 71-11-04..SDR U2RA201611280001Nose Cowl · chafedINLET COWL, COWL TO STRUT MATING FLANGE SURFACE AT 12 O'CLOCK POSITION WORN. ACCOMPLISHED INTERIM REPAIR IAW EO 5410ERO2253.SDR ASAA2016111818745Bracket · brokenNR 1 ENGINE RIGHT FAN COWL ALIGNMENT BRACKET AT THE 6 O'CLOCK POSITION FOUND BROKEN. ACFT GROUNDED. REMOVED THE BRACKET, POSITIONED NEW BRACKET IAW AMM 20-50-11.SDR REXA2016111802249Skin · damagedFAN COWL AFT HINGE SKIN ROLLED UNDER HINGE FAIRING. REPAIRED THE SKIN IAW EA CRJ954-05064. OPS CHECKED GOOD.SDR FDEA201611154023Spar · crackedLOWER SPAR OF CANTILEVER STRUCTURE IS CRACKED BETWEEN RIB A11 & RIB J08 REPAIRED AREA ON NR 1 PYLON LOWER SPAR BETWEEN RIBS A11 & J08 IAW SRM 54- 52-11 FIG 201. MAJOR REPAIRSDR IPXA2016111610699Rib · chafedINSPECTION TYPE: M15, NR 3 PYLON INTERNAL RIB CHAFED BEYOND ALLOWABLE LIMITSREMOVED AND REPLACED RIB PER SRM 54-01-42.SDR FDEA201611104202Hinge · damagedFOUND NR 1 ENGINE INBD AFT HINGE BOLT HOLE DAMAGED. REPAIRED IAW EA TF-5450-T0328068P2.SDR ASOA201611076126Heat Shield · damagedHOLE WORN THROUGH RT ENGINE LOWER CORE COWL INNER HEAT SHIELD. REPAIRED HOLE TO LOWER CORE COWL IAW REO 670-54-23-959 AND ECTC REO 670-54-23-959. AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR DALA2016110308238Structure · chafedNR 2 PYLON APRON UPPER SIDE AT THE NR 4 UPPER COWL HINGE APRON HAS CHAFED FLANGE. BLENDED CHAFE DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 54-00-00 FIG 103. REPAIRED IAW SRM 54-50-02 REPAIR 2.SDR JR2R20161102159Stiffener · crackedLEFT NOSE COWL INNER BARRELL STIFFENER CRACKED AT THE 6 O-CLOCK POSITION. REPLACED STIFFENER IAW EA 40-2016-344.SDR ASAA2016102918508Nut Plate · damagedNR 1 ENGINE SHROUD SEGMENT 2:00 O'CLOCK POSITION THIRD BOLT DOWN, NUTPLATE DAMAGED. ACFT GROUNDED. REMOVED AND REPLACED DAMAGED NUTPLATE, IAW SRM 51-40-02.SDR IXXA20161130177Skate Angle · corrodedNR 1 PYLON OUTBOARD SKATE ANGLE INBOARD SURFACE HAS SEVERAL BROKEN AND RUSTED NUTPLATES AND SURFACE CORROSION ALONG THE ENTIRE LENGTH. REMOVED CORROSION ALONG THE LENGTH OF OUTBOARD SKATE ANGLE. STARTING MATERIAL .125. BLENDED .077. MATERIAL LEFT .118. WITHIN SDR SIMA20161025001Yoke · crackedRT FWD LOWER YOKE CRACKED FWD UPPER EDGE. REMOVED AND INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386SDR DALA2016102407460Pylon · crackedNUMBER 1 PYLON UPPER AND LOWER AFT COWL ATTACH POINTS HAVE CRACKS IN CUTOUTS ON SKIRT FAIRING. REMOVED BRACKETS, FITTINGS, GUSSETS, AND SHIMS. BLENDED OUT CRACKS IN RADIUS. PERFORMED PENETRANT INSPECTION OF CUTOUT LOCATIONS IAW ER/A 552108-14 REV. A SECTION 1 SDR DALA2016102307459Pylon · crackedLEFT ENGINE PYLON APRON FOUND TO BE CRACKED IN FOUR LOCATIONS. REPAIRED IAW ER/A 552108-14.SDR IPXA2016110810420Web · crackedINSPECTION TYPE: 3C, NR 2 PYLON CARRY THRU WEB IS CRACKED. REPAIRED IAW SRM 55-30-02 REPAIR 7 FIG. 201.SDR IPXA2016111710732Structure · crackedINSPECTION TYPE: 3C, NR 2 ENGINE LT CORE COWL AFT FRAME CRACKED AT NAC STA. 300. REPAIRED CRACKED FRAME IAW EA 011-7110-01-A6530 REV. IR AND EO MD11-7110-62434-A.SDR FDEA201610193662Fitting · crackedNR 3 PYLON AFT BULKHEAD FITTING HAS A CRACK INDICATION AT THE FOURTH HOLE FROM OTBD SIDE. REPAIRED IAW EA 8-5400-T0329061.SDR FDEA201610193661Bolt · looseNR 3 PYLON, UPPER AFT SECTION OF SPAR WEB, HAS 15 LOOSE BOLTS. REAMED HOLES TO FIRST OVERSIZE AND INSTALLED B/P BOLTS IAW SRM 54-20-00 F. 27, VOL ISDR IPXA2016111610718Structure · crackedINSPECTION TYPE: 3C, PREVIOUS FRAME REPAIR FOUND DAMAGED INSIDE NR 1 LT CORE COWL. REPAIRED THE NR 1 CORE COWL IAW EA 011-7110-01-A6531 REV. IR AND EO MD11-7110-62443-A.SDR REXA2016101802122Access Panel · damagedBOTH SEPARATOR PANELS ON PANEL 412DB ARE KNIFE EDGED. REMOVED & REPLACED THE SEPERATOR PANELS IAW SRM 51-42-06.SDR SWIA201642710Cowling · dentedLEFT ENGINE, LOWER FAN COWL HAS A CREASE THAT IS OUT OF LIMITS. REPAIRED THE FAN COWL IAW EA.SDR FDEA201610113545Nacelle · contaminatedDURING TAKE OFF, TOWER REPORTED SMOKE FROM THE NR 1 ENGINE. NO OTHER INDICATIONS OF FIRE. INSPECTED THE NR 1 ENGINE INTAKE AND EXHAUST. NO DAMAGE NOTED. OPENED COWLING AND INSPECTED FAN/CORE/EXHAUST SECTIONS. NO EVIDENCE OF FIRE FOUND. NO FLUID LEAKS FOUNSDR GTIA2016100301617Structure · scratchedLT ENGINE CNA HAS A SCRATCH L75MM X W20MM X .5MMD COMPLIED WITH BLEND OUT REPAIR IAW RD CV16-6388 AND EO 7811-1605 REV 00.
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