JASC 5415
Service difficulty reports · 1,305
Reports filed under 5415 · Nacelle/Pylon, Attach Fittings, 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 = '5415' 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 = '5415' 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 C77A20130406008Attach Fitting · wornRT ENGINE OTBD FWD ENGINE PYLON FAIRING ATTACH POINT BORE IS ELONGATED. REAMED ATTACH POINT BORE AND INSTALLED BUSHING IAW SRM PART II 51-40-02 AND NE32-003.SDR UALA2013032801995Clamp · missingNR 2 ENGINE FIRE LOOP AT 7 O'CLOCK JUST BEHIND BREATHER, INSULATOR TOP CLAMP AND SCREW IS MISSING. INSTALLED NEW CLAMP AND SCREW.SDR C77A20130327025Attach Fitting · chafedRT PYLON OTBD AFT LOWER LINK FITTING HAS CHAFING MEASURING 2.4" X 1.1" X D=0.003". BLENDED CHAFED AREA, TREATED AND PRIMED IAW SRM 51-10-03 & 51-12-01 ON WO 693815-411 IAW ETD 2013-170-004652 AND COMPASS EA E170-54-016, REV IR WO 710308.SDR V0XR2013031200001Attach Fitting · crackedLEFT NACELLE FWD SIDE OF OUTBOARD FINGERNAIL ATTACH RAIL CRACKED. REPAIRED MOST FWD OUTBOARD TAB OF LEFT NACELLE WHERE THE FINGERNAIL ATTACHES, STA XN216.02 IAW DEHAVILLAND RD 8-54-163 BY REMOVING CRACKED TAB, FABRICATING NEW STRAP, AND INSTALLING WITH RIVETSSDR DALA13011913134Pin · corrodedNR 1 ENG PYLON, REAR SHACKLE UPPER PIN AND SLEEVE HAS PITTING CORROSION. PIN AND SLEEVE INSTALLED ON WC 5450-6010-LT. OUT OF LIMITS DIMENSION OF OLD OUT OF LIMITS PINS WERE 1.5" X 0.25" X 0.062" OUT OF LIMITS IAW AMM 54-51-00.SDR V0XR2013030700007Attach Angle · crackedCRACK IN ATTACH ANGLE AT AFT UNDERSIDE OF RIGHT FINGERNAIL. REMOVED AND REPLACED ATTACH ANGLE AT AFT UNDERSIDE OF RIGHT FINGERNAIL IAW DASH 8-100 SRM 51-40-07, AND 51-42-05. W/O 50335, W/C 4278SDR Y2PA20130306008Fitting · crackedUNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON REAR SPAR UPPER CAP FITTING AT STATION Y 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING IAW SRM 51-30-1, 51-30-3 AND 51-30-5.SDR Y2PA20130306007Fitting · crackedUNSCHEDULED LANDING, EMERGENCY DESCENT, ETC. LT PYLON REAR SPAR UPPER CAP FITTING AT STATION 1038 FOUND CRACKED DURING C-CHECK INSPECTION. MX REPLACED FITTING IAW SRM 51-30-1, 51-30-3 AND 51-30-5.SDR Y2PA20130306005Attach Angle · crackedEMERGENCY PROCEDURE, UNSCHEDULED LANDING, EMERGENCY DESCENT. RT PYLON UPPER PYLON TO FUSELAGE ATTACH ANGLE 12, AFT OF LEADING EDGE HAS 1 CRACK AT CORNER, DISCOVERED DURING C-CHECK INSPECTION. MX REPAIRED IAW SRM 54-04, FIG 10.SDR SWAA2013022213005Attach Angle · crackedRT PYLON AFT UPPER ATTACH ANGLE CRACKED. TRIMMED DAMAGED AREA PER BOEING DRAWING SG95530003.SDR FDEA201302070290Skin · bulgedNR 2 NACELLE STRUT PYLON STRUCTURE INBD SKIN AT PPSTA 185.0 FOUND BULGING. REPAIRED IAW EA F-5450-16290, PART 1. AD 2004-12-07, EO F-5450-7-5003, SB 757-54-0035 R4. MAJOR REPAIR.SDR QXEA2013012300101Attach Bracket · crackedLT NACELLE INBD ATTACH BRACKET FOR PANEL 413DR IS CRACKED. REMOVED 2 ATTACH BRACKETS REF SRM 51-42-05-02-01. INSTALLED NEW NUTPLATES ON NEW ATTACH BRACKET IAW SRM 51-42-75-02-01. MATCH DRILLED NEW ATTACH BRACKET TO EXISTING BRACKET HOLES IAW SRM 51-40-07-02SDR DALA1301321521Fitting · mismanufacturedDURING ACCOMPLISHMENT OF PYLON MODIFICATION, FOUND 2 EA HOLES ON SIDE-LOAD FITTING HAVING SHORT EDGE MARGIN. SHORT EDGE MARGIN CONDITION FOUND TO BE ACCEPTABLE AND TO REMAIN AS IS IAW ERA 570077-14AD, REV 0, STEP 2.SDR DALA13003653213Shackle · damagedDURING INSPECTION, FOUND RT PYLON AFT SHACKLE FWD PIECE, FWD FACE CHAFED AROUND THREE BUSHINGS. REPLACED WITH SERVICEABLE PART. SHACKLE INSTALLED ON W/C 5450-6010-RT DUE TO NO SPECIFIC ALLOWABLE DAMAGE SPECIFIED IAW SRM 54-51-17.SDR SWAA2013011611495Attach Fitting · crackedLEFT WING UPPER SURFACE, NR 1 PYLON PANEL 57710 ATTACH, AFT ATTACH POINT IS CRACKED AND BROKEN. REMOVED AND REPLACED AFT ATTACH NUT PLATE STRIPS ON FIXED FAIRING (PNL) AFT OF PNL 57710L IAW SRM 51-40-02-0G-0. LEAK CHECK GOOD IAW AMM 28-11-00.SDR FDEA201212184318Mount · corrodedNR 1 ENG PYLON MOUNT HAS CORROSION ON AFT OTBD AND INBD SPOT FACES AND AFT OTBD AND INBD TENSILE BOLT HOLES. REMOVED CORROSION AFT I/B & O/B SPOT FACE & INNER BORE OF HOLES, FOUND TO BE WITHIN LIMITS IAW SRM 54-51-01 CONFIG 2 FIG 104, REMOVED CORROSION AT SDR QXEA2012120201561Cleat · crackedRT ENGINE NACELLE FORWARD LT SPINE COWL CLEAT IS CRACKED. REMOVED CRACKED CLEAT IAW SRM 51-41-00-00-01 AND 51-42-05-02-01. MATCH DRILLED NEW CLEAT TO EXISTING STRUCTURE IAW SRM 51-40-07-02-01. INSTALLED NEW CLEAT IAW SRM 51-41-05-00-01 AND 51-42-05-02-01.SDR SWAA2012120710351Fairing · brokenBROKEN FAIRING ASSY LOWER BIFURCATION AFT LOWER POSITION INBOARD T/R ENGINE NR 2. REPAIRED FAIRING ASSY LOWER BIFURCATION AFT LOWER POSITION I/B T/R ENGINE NR 2 IAW EA N. 1-354-1515 R0 AND EO N. AEM-HC54-060/12 REV 0. FOR DETAIL SEE TLD N. T030220SDR U2RA201211120001Fitting · chafedNR 1 PYLON MID-BULKHEAD RT FITTING, CHAFING, LENGTH 3", WIDTH 1" DEPTH .095", ORIGINAL MATERIAL THICKNESS .388", REMAINING MATERIAL THICKNESS .293". MFG FOUND CONDITION ACCEPTABLE AS IS.SDR DALA1253740680Drag Brace · damagedPERMANENT REPAIR NR 1 PYLON DIAGONAL DRAG BRACE FITTING. ACCOMPLISHED ERA 363122-14AD REC C PERMANENT REPAIR ON NRC 207536.SDR DALA12009223126Fitting · gougedNR 1 PYLON MATING FACE OF FWD PYLON PYRAMID FITTING LOWER SURFACE AFT CENTER HOLES HAS GOUGE. BLENDED DAMAGE AREA IAW SRM 51-73-00, DIMENSION AFT HOLE D1= .020" D2=.046" S1=0.0004 MID HOLE D1=.035" D2=.046"S1=0.0008. FOUND TO BE WITHIN LIMITS IAW SRM 54-51-1SDR 2012FA0000751Fitting · crackedPERFORMING TASK 5545172-01-1R. CRACK WAS IDENTIFIED ON THE NR 2 ENG PYLON INBD FITTING AT RIB 11, REPORTED TO BE .50". REPLACEED INBD AND OTBD PYLON CORNER FITTINGS AT RIB 11.SDR 2012FA0000749Fitting · crackedWHILE PERFORMING TASK 545172-01-1L, A CRACK WAS IDENTIFIED ON THE NR 1 PYLON OTBD FITTING AT RIB 11. REPORTED TO BE .50". REPLACED INBD AND OTBD PYLON CORNER FITTINGS AT RIB 11.SDR DALA12006983129Attach Fitting · wornLEFT PYLON OUTBOARD PYLON TO WING ATTACH FITTING OUTBOARD LUG WORN. ACCOMPLISHED PERMANENT REPAIR PER ER/A 505941-14. REMOVED DAMAGE IAW SRM 51-73-00 DVI AND HFEC PER NTM 51-90-00 AND 51-10-08. NO OTHER DAMAGE NOTED.SDR UIEA2012090700392Skin · damagedNR 2 PYLON PANEL 462EL ONE BOLT HOLE ELONGATED. NR 2 PYLON PANEL 462EL PATCH REPAIRED IAW RS NR R-54-00-37414, REV A.SDR ABXR201208070059Fitting · crackedNR 2 PYLON FWD UPPER INBD ATTACH FITTING ABOVE FWD ENGINE MOUNT BULKHEAD FITTING CRACKED .5 INCHES NAC STA 204. INSTALLED NEW FITTING IAW DWG 311T2210 AND SRM 52-40-2.SDR DALA12003193130Attach Fitting · gougedRT PYLON FWD LT SIDE ATTACH FITTING HARDWARE 1 SLEEVE HAS GOUGE ON HEAD (PANEL RACK). RT PYLON FORWARD LEFT SIDE ATTACH FITTING SHACKLE 1 PIN SLEEVE REPLACED AND INSTALLED ON JOB CARD 5450-6010-RT. NO DAMAGE ALLOWED IAW AMM 54-51-17 PB601 TR17594. DAMAGE DISDR NOCA06112Attach Bracket · crackedNR 1 PYLON EDP SHUTOFF VALVE ATTACH BRACKET IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED WITH NEW PYLON EDP SHUTOFF VALVE ATTACH BRACKET IAW EO 767-54-022, SB 767-54-0081 & 51-40-02-06-0.SDR NOCA201207110002Attach Fitting · chafedRIGHT PYLON STRAP UPPER AFT ATTACH POINT FASTENER PLUG CHAFING THRU SKIN. FABRICATED AND INSTALLED FILLER AND SPLICE PER DWG 313T3310 REV G & SRM 54-52-70/201.SDR C77A20120601029Nut · looseLT PYLON OTBD AFT ATTACHMENT WASHER IS LOOSE. REMOVE CASTELLATED NUT, CHECKED RUN-ON TORQUE, REINSTALLED AND TORQUED NUT TO SPECIFIED TORQUE VALUE LISTED IN ETD AND RESAFTIED ON WO 490404-413 IAW ETD 2012-170-007252 AND EA E175-54-099 REV IR ON WO 568510.SDR USAA2012052500022Attach Fitting · severedPYLON FITTING INSPECTION - NR 1 ENGINE INBOARD C DUCT AFT MOUNT PYLON ATTACH FITTING CENTER LUG UPPER MATERIAL SEVERED. REPLACED NR 1 ENGINE INBOARD C DUCT AFT MOUNT PYLON ATTACH FITTING AT PP STA 174.30 IAW EA 202636, EA 202610A AND EO 5408R114.SDR UALA2012060103040Attach Fitting · wornNR 2 PYLON TO ENGINE LT AND RT SIDE MOUNT FITTING WEAR WAS BLENDED REF ECRA:5451-01086. PERFORMED HFEC INSPECTION WITH NO DEFECTS FOUND.SDR CA120531004Fitting · fractured(CAN) THIS ENGINE PYLON MIDSPAR FITTING WAS FRACTURED DURING A 400 CYCLE REPEAT INSPECTION ON THE ENGINE PYLON.SDR ASOA20120406055TFitting · crackedNR 1 PYLON FWD YOKE LWR FWD FITTING CRACKED. R & R NR 1 ENG FWD LWR FITTING.SDR FDEA201203150951Attach Bracket · crackedREVERSE FLOW CONTROLLER MOUNTING PLATE CRACKED, MOUNTING PLATE FABRICATED IAW DWG 312N5857.SDR USAA2012040500004Pin · crackedC4 CHECK - CRACK IN LOWER FUSE PIN OF RIGHT ENGINE NACELLE STRUT DIAGONAL BRACE AT PPS 300, PPWL 161.70. REPLACED LOWER FUSE PIN OF DIAGONAL BRACE AT PPS 300, PPWL 161.70 IAW B757 AMM 54-51-02.SDR SIMA20120307003Fitting · crackedDURING MAINTENANCE INSPECTION FOUND THE LEFT ENGINE FORWARD PYLON YOKE LOWER FITTING CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED LEFT ENGINE FORWARD PYLON YOKE LOWER FITTING IAW EO EM-54MR-386. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS SDR USAA2012030500001Hinge Fitting · crackedPHX VISUAL - NR 2 ENGINE OUTBOARD `C` DUCT AFT MOUNT PYLON ATTACH FITTING, CENTER LUG CRACKED APPROX 1 INCH. REPLACED NR 2 ENGINE OUTBOARD THRUST REVERSER AFT HINGE FITTING IAW EA 201955 & EO 5408R114.SDR ABXA20120215208Fitting · dentedLEFT ENGINE BACK UP FITTING OUTBOARD OF RIB 8 HAS 3 SMALL TOOLING MARKS. REMOVED TOOLING MARKS IAW REA B657-59674, AIRCRAFT WAS GROUNDED.SDR USAA2012021700022Rib · wornS2 CHECK - NR 1 PYLON AT RIB 18A INBOARD PYLON TO WING ATTACHMENT FITTING SLEEVE HAS WORN PROTECTIVE COATING & SCRATCHES. REPLACED NR 1 PYLON AT RIB 18A INBOARD PYLON TO WING ATTACHMENT FITTING SLEEVE IAW AMM 54-51-17.SDR HNAA2012021000572Attach Angle · crackedOTBD AFT ATTACH ANGLE FOR FILLET PANEL IS CRACKED. FABRACATED NEW ANGLE IAW DWG 85418256. REMOVED OLD CRACKED ANGLE. INSTALL NEW ANGLE IAW DWG 85410042.SDR IPXA2M71726Fitting · looseINSPECTION TYPE:4C, FOUND LOOSE FASTENERS AT NR 4 BANJO FITTING TO PYLON LT SIDE. REPAIRED NR 4 BANJO FITTING TO PYLON LT SIDE REF STA, SA, EA 011-5530- 01-A3642 AND EO MD11-5530-45993-A.SDR IPXA2M71720Fitting · looseINSPECTION TYPE: 4C, FOUND LOOSE FASTENERS AT NR 4 BANJO FITTING TO PYLON RT SIDE. REPAIRED NR 4 BANJO FITTING TO PYLON RT SIDE REF ST,SA, EA 011- 5530-01-A3641 REV I/R AND EO-5530-45894-A.SDR FDEA201201090048Fitting · looseNR 1 NACELLE STRUT INBD BATHTUB FITTING MOUNTING BOLTS, FOUND LOOSE. BATHTUB FITTING R & R IAW EA F-5450-154642A.SDR USAA2012010300013Pin · wornS2 CHECK - THREADS WORN ON NR 1 ENGINE PYLON AFT MOUNT PIN AT FRAME 18A, WS 6261. REPLACED NR 1 ENGINE PYLON AFT MOUNT PIN IAW A330 AMM 54-51-17-400-8040.SDR USAA2011122900003Clevis Pin · wornS2 CHECK - EVIDENCE OF WEAR & MISSING PLATING ON NR 2 PYLON FORWARD ATTACH LUG INBOARD UPPER & LOWER PINS. REPLACED NR 2 PYLON FORWARD ATTACH LUG INBOARD UPPER & LOWER PINS IAW A330 AMM 54-51-17.SDR FDEA201112215412Attach Fitting · corrodedNR 2 ENGINE PYLON TO WING LOWER ATTACH FITTING AT RIB NR 18 HAS 4 SQ IN OF CORROSION AT INNER RACE. R & R RIB 18 FITTING ON NR 2 PYLON IAW AMM 54-51-75-04-02.SDR FCPR20121121001Bracket · crackedWHILE PERFORMING OTHER MX, FOUND RT ENGINE FUEL FLOW TRANSDUCER BRACKET CRACKED. REPLACED BRACKET WITH NEW.SDR FDEA201111074773Mount · corrodedNR 2 PYLON FORWARD MOUNT INBD AFT BOLT HOLE SPOT FACE FOUND CORRODED. REPAIRED IAW EA 6-5450-155829. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.SDR FDEA201110214607Support Bracket · crackedNR1 ENG PYLON AFT END REAR SPAR INTERFACE HYD LINES SUPPORT BRACKET HAS 4 EA CRACKS AT FASTENERS 3 EA 1" AND 1 EA .3" LONG R & R NR 1 ENG PYLON AFT END AT WING REAR SPAR SUPPORT BRACKET IAW SRM 51-72-10.
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