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 REXA2013060901015Fairing · chafedRT ENGINE UPPER AFT HINGE FAIRING CHAFED. REPAIRED RT ENG UPPER AFT HINGE FAIRING IAW SRM 51-24-16 AND 51-40-11.SDR UALA2013061103998Liner · damagedNR 2 ENGINE HAS DAMAGE TO ACCOUSTICAL MATERIAL AT THE 5:30 POSITION NEAR NACELLE LIP.SDR DALA13028331402Fitting · crackedNR 2 PYLON CRACK INDICATION FOUND ON RT UPPER LINK PITCH LOAD FITTING AT MOST OTBD AFT FASTENER HOLE REPAIRED IAW PRI 514654-14AD, REV 0, REV 1, REV 2 AND REV 3. REPAIR COMPARED AND COMPLIED WITH ER/A 514654-14AD.SDR DALA13028251402Fitting · damagedDURING HFEC OPEN HOLE INSPECTION ON RT WING NR 2 PYLON AFT DIAGONAL BRACE FITTING, FOUND OTBD FASTENER HOLE (01 EA) WITH HOLE EDGE DAMAGE ON LOWER WING SURFACE SIDE. OTBD FASTENER HOLE DAMAGE REWORKED IAW PRI 514643-14AD, REV 0 AND REV 1.SDR FDEA201306041193Plate · crackedLEFT PYLON, VERTICAL PLATE AT AFT FAIRING TO MAIN PYLON JUNCTION ON LT SIDE CRACKED AT TOP AND WORN THROUGH SIDE STRUCTURE OF AFT FAIRING ASSY. PLATE REPLACED AND DAMAGED AFT FAIRING STRUCTURE REPAIRED IAW EA 6-5751-167425 AND TD-J2-S1-03624-2013 FUCTIONALSDR ASAA2013052995059Seal Depressor · chafedNR 1 ENGINE PYLON METAL FIRE SEAL FLANGE CHAFED. ACFT GROUNDED. R & R SEAL DEPRESSOR ON NR 1 ENG PYLON IAW AMM 20-50-11-912-002, FIG 203, PAGE 8.SDR REXA2013052600941Fairing · crackedHINGE LINE FAIRING 442BB CRACKED AT FASTENER HOLE AND GOUGED. FABRICATED REPLACEMENT FAIRING 442BB IAW SRM 51-40-11 + SRM 51-21-16.SDR UALA2013052803711Structure · crackedNR 2 ENGINE, NR 4 GAP COVER STRIP IS CRACKED. REMOVED DAMAGE AND BLENDED AREA IAW SRM 54-50-70. HFEC INSP REQUIRED. REWORKED DIMENSIONS ARE 3.75" FROM INBD EDGE 7.4375 WIDE AND .056" GAP. TOTAL AREA OF EXPOSURE IS .4165 SQ" ACCOMPLISHED HFEC INSPECTION IAW SDR ASAA2013052395287Support Beam · chafedNR 2 PYLON INBD FAN COWL SUPPORT BEAM CHORD CHAFED. REPAIRED NR 2 PYLON INBD FAN COWL SUPPORT BEAM CHORD IAW EA 400-54EA-10558.SDR ASAA2013052395285Support Beam · chafedNR 2 PYLON OTBD FAN COWL SUPPORT BEAM CHORD CHAFED. ACFT GROUNDED. REPAIRED NR 2 PYLON OTBD FAN COWL SUPPORT BEAM CHORD IAW EA 400-54EA-10558.SDR ASOA2013070308559Cowling · gougedGOUGE DAMAGE ON THE INTERIOR OF THE RT ENGINE FWD CORE COWL. REPAIRED IAW GREO 670-54-23-959. REPAIR CLASSIFIED AS MAJOR.SDR ASAA2013052295256Support Beam · chafedNR 1 ENG PYLON FAN COWL SUPPORT BEAM INBD CHORD CHAFED. ACFT GROUNDED. REPAIRED NR 1 ENG PYLON INBD FAN COWL SUPPORT BEAM IAW ASA EA NR 400 54EA 10557.SDR UALA2013052403608Shield · damagedNR 2 ENGINE HYDRAULIC AND FUEL HOSE SHIELD DAMAGED. REPLACED NR 2 ENG HYD AND FUEL HOSE SHIELD.SDR SIMA20130517014Yoke · crackedLEFT PYLON FWD LOWER YOKE NR 1 CRACKED. R & R YOKE IAW EO-EM-53MR-386.SDR UALA2013051603403Nose Cowl · dentedNR 2 ENGINE NOSE COWL L/E HAS A DENT APPROXIMATELY ONE O'CLOCK POSITION. INSTALLED DOUBLER REPAIR ON NOSE COWL L/E IAW SRM 54-11-01, FIG 201, REPAIR 1. MAJOR REPAIR.SDR FDEA201305100971Web · crackedHOLES OUT OF LIMITS ON WEB AUB7366-501. R & R UPPER PYLON SPAR WEB IAW DWG AUB7301 AND SRM 51-33-01, VOL. II INSTRUCTIONS.SDR UALA2013050903246Latch · damagedLEFT PYLON HYDRAULIC BAY ACCESS DOOR AFT 4TH LATCH DAMAGED. REMOVED AND REPLACED LATCH, OPS NORMAL.SDR UALA2013050803220Fastener · damagedRIGHT ENGINE FAN COWL SHOWS EVIDENCE OF LIGHTNING DISCHARGE. DAMAGE IS LOCATED AT THE 3:00 O'CLOCK POSITION AND IS LOCATED APPROX 5-8" FWD OF THE AFT EDGE, DAMAGE MEASURES 5-8" BY 5-8". REPLACED SCREW LOCATED AT THE AFT LOWER CORNER OF THE FAN COWL OPERATIONASDR C77A20130505013Heat Shield · chafedLT PYLON NR 1 HEAT SHIELD IS CHAFED ON THE T/E. BLENDED SMOOTH THE CHAFED AREA ON UPPER HEAT SHIELD AND FABRICATED DOUBLER AND FILLER IAW SRM II 51-40-02-51.SDR UALA2013042902995Structure · damagedNR 1 PYLON DUAL SIDE BRACE O/B BORE DAMAGED. REPAIRED IAW ECRA 5410-01722.SDR UALA2013042902958Bearing · damagedNR 1 PYLON DUAL SIDE BRACE O/B BORE EXCEEDED MAX LIMIT. SPLIT SLEEVE AND STANDARD BEARING INSTALLED IAW EVA 80605. INSTALLED NEW BEARINGS IAW ECRA 5410-01722.SDR C77A20130430025Heat Shield · chafedRT AFT PYLON NR 4 HEAT SHIELD HAS L/E AND T/E DAMAGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.SDR C77A20130430024Heat Shield · chafedRT AFT PYLON NR 3 HEAT SHIELD HAS L/E AND T/E DAMAGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.SDR C77A20130430023Heat Shield · chafedRT AFT PYLON NR 2 HEAT SHIELD HAS L/E AND T/E DAMAGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.SDR C77A20130430022Heat Shield · chafedRT AFT PYLON, NR 1 HEAT SHIELD IS CHAFED IN THE LWR CENTER AREA. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.SDR C77A20130430021Heat Shield · chafedLT AFT PYLON NR 3 HEAT SHIELD HOLE IN THE AFT JOGGLE AND CHAFED ON THE AFT EDGE. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW SRM PART II 54-31-00.SDR C77A20130430020Heat Shield · chafedLT AFT PYLON, NR 1 HEAT SHIELD CHAFED IN THE LWR CENTER AREA. REMOVED CHAFED AREA AND INSTALLED FILLER AND DOUBLER IAW PRINCIPLES OF SRM PART II 54-50-23, REPAIR 16P ON WO 670776-407 IAW ETD 2013-170-006437 AND COMPASS EA E175-54-132, REV IR WO 722744.SDR V0XR2013042500001Frame · corrodedLEFT CHIN COWL HAS CORROSION ALONG AFT FRAME AND 2 AFT RIBS. R & R AFT FRAME AND RIBS ON LT CHIN COWL WITH NEW FABRICATED FRAME CLEATS AND RIBS IAW DWGS 87144018 AND 87144019, SRM 51-24-35, 51-42-05, 51-42-45, 51-40-35, 51-25-10, AND 51-21-10.SDR DALA1316080683Support Beam · crackedNR 2 PYLON FAN COWL SUPPORT BEAM WEB ATTACH ANGLES CRACKED INBD AND OTBD. REPAIRED SRM 54-51-01D, FIG 101.SDR DALA1316070683Cowl Door · dentedCOWL DENT ON LT NACELLE. REPAIRED IAW SRM 54-11-01, FIG 101.SDR UALA2013042402845Fairing · delaminatedRIGHT ENGINE PYLON INBD AFT FAIRING HAS DELAMINATION. PERFORMED METAL BOND REPAIR PER AMM.SDR UALA2013042302791Fastener · missingCREW REPORTED TWO MISSING RIVETS ON NR 1 ENGINE FORWARD OUTER RING IN 5 AND 1 O'CLOCK POSITIONS. REPLACED FASTENERS PER MT 71-002.SDR UALA2013042202781Fastener · missingWHILE PERFORMING MF8840, FOUND ONE MISSING FASTENER ON NR 2 ENGINE OUTBD PYLON HEATSHIELD. REPAIRED.SDR UALA2013041802650Nose Cowl · dentedSHALLOW DENT ON RIGHT NOSE COWL L/E TOTAL OF FOUR DENTS ON INLET COWL LEADING EDGE, ALL SMOOTH, NO CRACKS. TWO DENTS IN THE 7:00 REGION, TWO IN 5:00 REGION, DENTS ARE SMOOTH AND NO RIVETS IMPACTED. DENTS OUT OF LIMITS IAW SRM 54-10-01.SDR UALA2013041802694Rivet · shearedNR 1 ENGINE NOSE COWL INNER LIP AT 6 O'CLOCK POSITION ONE RIVET HEAD SHEARED OFF. REPLACED RIVET PER MT71-0 02.SDR DALA13017893135Structure · gougedLT PYLON PYRAMID AFT ALIGNMENT PINHOLE GOUGED. BLENDED DAMAGE AREA IAW SRM 51-73-00. CHECKED LIMITS DIMENSION; D1=0.030", D2=0.010", S1=0.0015" FOUND TO BE WITHIN LIMITS IAW SRM 54-51-18, FIG 105 (SHT-1). PERFORMED FPI IAW NTM 51-80-00 PT8 NO CRACK INDICATISDR DALA13017883135Structure · damagedLT PYLON PYRAMID CTR ALIGNMENT PIN HOLE GOUGED. BLENDED DAMAGE AREA IAW SRM 51-73-00. CHECKED LIMIT DIMENSIONS; D1=0.025", D2=0.015". S1=0.0018" FOUND TO BE WITHIN LIMITS IAW SRM 54-51-18, FIG 105 (SHEET 1). PERFORMED FPI IAW NTM 51-80-00 PT8 NO CRACK INDICSDR UALA2013041502592Fastener · missingTWO RIVETS MISSING ONE POPPED ALONG UPPER INBOARD OF NR 1 ENGINE TAILCONE. INSTALLED NEW RIVETS PER MT 78-001.SDR UALA2013041502593Latch · detachedSTRANGE PIECE OF METAL PROTRUDING FROM NR 1 ENGINE JUST BEHIND DRAIN VENT. OPENED FAN COWLING, WAS ABLE TO SEE A LOOSE LATCH MECHANISM. THAT HAS BEEN PROPERLY SECURED. CHECKED ALL THE OTHER LATCHES, FOUND SECURE. CLOSED AND LATCHED THE FAN COWL. PROPERLY SDR HYIA20130416004Beam · damagedDURING A SCHEDULED MX EVENT DAMAGE WAS NOTED TO THE LT NACELLE OTBD ENGINE BEAM RADIUS. DAMAGE WAS MAPPED AND SUBMITTED FOR ENGINEERING ASSISTANCE. REPAIRS WILL BE COMPLETED IAW REPAIR DEFINITION SUPPLIED AND SUBSTATIATED.SDR FDEA201304090754Shim · migratedNR 1 PYLON UPPER SURFACE UPPER LINK FITTING HAS SHIM MIGRATION. EVALUATED MIGRATED SHIM MAXIMUM MIGRATION IS 0.120, FOUND TO BE WITHIN LIMITS IAW SRM 54-50-90, REPAIR 6 FIG 201. THIS IS CLASSIFIED AS REPAIR CATEGORY B.SDR FDEA201304090753Shim · migratedNR 1 PYLON UPPER INBD SURFACE, UPPER LINK FWD FITTING HAS SHIM MIGRATION AT PPSTA 174.30 EVALUATED MIGRATED SHIM, MAXIMUM MIGRATION IS 0.100 FOUND TO BE WITHIN LIMITS IAW SRM 54-50-90, REPAIR 6, FIG 201, CLASSIFIED AS REPAIR CATEGORY B.SDR UALA2013040802319Liner · wornNR 2 ENGINE NACELLE, HAS A FOUR INCH PATCH OF ACOUSTIC MATERIAL MISSING, WORN AWAY AT 1 O`CLOCK POSITION. REPAIRED IAW MT 71-006 AND SRM 54-10-00 REPAIR 15.SDR DALA1310376801Bushing · migratedNR 1 PYLON UPPER DIAGONAL BRACE WING FITTING (MOUNTED UNDER WING) OTBD BUSHING MIGRATED OUT OF INNER RACE REQS ENGINEERING DISPOSITION. REPAIRED IAW ERA 513675-14AD REV ORIG.SDR UALA2013032902028Fastener · missingNR 1 ENGINE PYLON LOWER FAIRING MISSING THREE RIVETS, I/B SIDE. COMPLIED WITH MAINT TEMP 54-003. INSTALL TEMP REPAIR WITH BLIND RIVETS.SDR UALA2013032902032Fastener · looseNR 1 PYLON HEAT SHIELD HAS FASTENER LOOSE UPPER EDGE 7TH ONE BACK FROM FWD EDGE. REPLACED FASTENERS.SDR UALA2013032701945Blowout Panel · blownRIGHT ENGINE HIGH PRESSURE BLOWOUT PANEL IN ENGINE PYLON IS BLOWN OPEN. SECURED BLOWOUT PANELSDR UALA2013032601914Nose Cowl · damagedFOUND EVIDENCE OF BIRD STRIKE AT GATE, RT NOSE COWL. DAMAGED AND LEADING EDGE PYLON PANEL DAMAGED. RT ENG RING COWL AT 10:0 0 HAS A DENT 18 INCH BY 8 INCH. NO SKIN TEAR DENT ONLY. REMOVED NOSE-AIR INTAKE COWL PER AMM 71-11-11-0401. STARTED TO INSTALL ROBBSDR HNAA2013032500161Stringer · damagedHEAT SHIELD LOWER STRINGER AND REAR STRAP IS DAMAGED ON RT NACELLE R & R LOWER HEAT SHIELD STRINGER AND REAR STIFFENER WITH LOCALLY FABRICATED MATERIAL IAW DWG 85410733 AND 8541-732.SDR LR7A2013032300624Angle · crackedDURING SCHEDULED B-3, FOUND NR 4 ENGINE AFT NACELLE FIREWALL ASSY INBD SIDE HAD CRACKED ATTACH ANGLE AND WEB AT CLAMSHELL DOOR AFT HINGE ATTACH POINTS. REPAIRED TO WEB AND ANGLE ACCOMPLISHED IAW MEA 382-54-13-045.
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