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 SWAA062110Crossbeam · wornDURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENGINE FWD MOUNT CROSS BEAM FREEPLAY OUT OF LIMITS. REMOVED AND REPLACED FWD MOUNT CROSSBEAM PER MM.SDR HALA0600434Attach Angle · crackedAPPROX 1.25 INCH CRACK ON UPPER PYLON TRAILING EDGE ATTACH ANGLE AT STA CANTED 1178 LT. REPAIRED PER HALM105 FILE 477101.SDR SWAA061753Pin · corrodedDURING SCHEDULED 10Y CHECK, FOUND RT WING PYLON INBOARD MID SPAR FUSE PIN CORRODED. REMOVED AND REPLACED MID SPAR FUSE PIN PER MM.SDR USAA060709Attach Bracket · crackedNR 1 PYLON STRUT FAIRING FWD END CRACKED. REMOVED & REPLACED ATTACH BRACKET. PART FABRICATED ON TRAVELER T6/590134 PER SRM 51-40-02, 51-40-05, DEFECT SIZE: 15 INCHES.SDR CNMA20060009Lug · damagedFOUND DAMAGE TO THE NR 2 ENGINE LEFTHAND BOOTSTRAP LUG. PERFORMED REPAIR IAW REPAIR DRAWING 5420250-1 REV 1 DATED 5-6-2006 REF REPORT 5420250-ER REV 1 DATED 5-5-2006.SDR GTIA200600018Attach Fitting · crackedNR 2 PYLON OUTBOARD SIDE HAS CRACK ON UPPER METAL STRIP FOR ATTACHMENT OF PANEL 424CR. INSTALLED REPAIR DOUBLER ON NR 2 PYLON OUTBOARD SIDE EXTRUSION PROFILE.SDR USAA060683Attach Fitting · crackedABOVE MIDSPAR ATTACH FITTING OUTBOARD SIDE CRACKED. INSTALLED MFG FILLER AND BOTH DOUBLERS IAW 57-41-02, DEFECT SIZE: 3 INCHES.SDR ABXA060249Attach Angle · crackedNR 2 ENGINE PYLON TRAILING EDGE FAIRING AFT OUTBOARD ATTACH ANGLE WAS CRACKED. REMOVED AND REPLACED ANGLE IAW B767 SRM 51-40-02.SDR QXEA200601016Attach Fitting · wornYYC - C4 LEFT NACELLE AFT HEAT SHIELD, OUTLET SHROUD ATTACHMENT TABS ARE WORN THROUGH AT STATION 262 - 280 ON INBOARD SIDE AND OUTBOARD SIDE. REPAIRED IAW RD 8-54-163, ISSUE 2.SDR QXEA200601175Attach Angle · chafedPDX: LT WING TO NACELLE ATTACH ANGLE IS CHAFED ON THE LOWER FWD CORNER FROM CONTACT WITH 512AL. MAINTENANCE REPAIRED IAW Q400 SRM 51-14-00, SRM 51-21-10 AND SRM 51-25-10.SDR QXEA200600977Attach Angle · chafedPDX: LT WING TO NACELLE ATTACH ANGLE IS CHAFED ON THE LOWER FWD CORNER FROM CONTACT WITH 515AL. MAINTENANCE BLENDED CHAFED AREA IAW Q400 SRM 51-14-00. ETCHED AND ALONDINED AREA IAW Q400 SRM 51-21-10. PRIMED AND PAINTED AREA IAW SRM 51-25-10.SDR DL757060268Fitting · misalignedAN ATTACH HOLE IN THE LT PYLON WING ATTACH LINK FITTING IS MISALIGNED. INSTALLED A TAPERED RADIUS FILLER TO PROPERLY ALIGN FASTENER.SDR AWXA200600749Attach Fitting · galledDURING C12 CHECK DISCOVERED RT WING INBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 248R. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RC2SDR AWXA200600748Attach Fitting · galledDURING C12 CHECK DISCOVERED RT WING OUTBOARD STRUT ATTACH FITTING LUGS FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263R . MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06SDR AWXA200600750Attach Fitting · galledDURING C12 CHECK DISCOVERED LT WING OUTBOARD STRUT ATTACH FITTING FOR PYLON GALLED FROM BUSHING CONTACT ON THE INBOARD AND OUTBOARD SIDES OF LUG AT WBL 263L. MAINTENANCE REMOVED OUTBOARD BUSHING IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 19-5704-06114-RCSDR 06FDEA1149Fitting · shearedNR 1 AND NR 3 PYLONS HAVE SHEARED BOLTS AT FWD PYLON TO WING MOUNT FITTING, FASTENERS ARE COMMON TO OUTER SKIN AND TOMB-STONE FITTING AND UPPER CHORD ANGLE. REMOVED AND REPLACED FASTENERS IAW DC10-SRM 51-31-01-VOL 2 AND DC10-30 AMM 20-50-02.SDR DL76L100108Attach Fitting · damagedNACELLES/PYLONS ATTACH FITTING - MID SPAR FITTING REPAIR IAW EO 01-074944-12 ME03 POSITION 1 C/W 01-074944-12 ME03 POSITION 1.SDR UPS06246094Mount · corrodedINSPECTION TYPE:C NR 3 PYLON FWD MOUNT, FWD I/B HOLE HAS PITTING CORROSION. REPAIRED IAW EO B727-5440-11592-A.SDR C1HA200686001Support Fitting · crackedNR 3 ENGINE PYLON; DURING OPEN HOLE HFEC OF FWD SUPPORT FITTING PER TASK CARD AD 2005-19-24-02, FOUND CRACK IN HOLE P OF ANGLE 69-16977-2. REMOVED AND REPLACED FWD SUPPORT FITTING PART 69-16977-2 REF BAC PRINT 65 -72772.SDR AU510001510Bracket · crackedRT ENGINE FIREWALL BRACKET CRACKED ON BOTH SIDES OF ANCHOR NUT. FOUND DURING INSPECTION IAW AD/BEECH76/10-2.SDR AU510001874Support Fitting · crackedLT AND RT ENGINE FORWARD SUPPORT FITTING ASSEMBLIES CRACKED. LT PYLON FITTING CRACKED AT HOLE `F`. RT PYLON FITTING CRACKED AT HOLE `P`. FOUND DURING INSPECTION IAW AD/B727/151 AND BOEING SB 727-54A0010.SDR GTIA050258Attach Angle · crackedFTW - RIGHT PYLON T/E ATTACHED ANGLE IS CRACKED APPROX 16 INCHES FROM T/E ROOT. REMOVED DAMAGE AREA. FABRICATED REPAIR. TREATED, PRIMED AND INSTALLED REPAIR ANGLE. (M)SDR GTIA050259Attach Angle · crackedLEFT PYLON T/E ATTACH ANGLE IS CRACKED APPROX 16 INCHES FROM THE T/E ROOT. REMOVED DAMAGED SECTION. FABRICATED REPAIR ANGLE AND FILLER. TREATED, PRIMED AND INSTALLED REPAIR ANGLE AND FILLER. (M)SDR 05FDEA02129Fitting · corrodedNR 1 PYLON TO WING ATTACHMENT FITTING SHACKLE OUTBD/INBD LOWER BUSHING HAS CORROSION CHROME PLATING WORN.SDR SWIA200515386Track · crackedRT ENG INBOARD LOWER MAIN TRACK ASSEMBLY IS CRACKED, ITEM FOUND AT C-CHECK. MAIN TRACK ASSEMBLY REPLACED IAW CRJ AMM 78-34-11-400-801 & 78-34-11-000-801.SDR DXTA200500791Nut Plate · defectiveFUSELAGE FAIRING PANEL ATTACH NUTPLATES FAIL DRAG TORQUE OF 12-15 IN POUNDS. NO NOTED TORQUE ON NUTPLATES. EVALUATED ACFT ACCESS PANEL NUTPLATES FOR DEFECTS. INSTALLED NUT PLATES IAW 680 MM 51-40-03. INSTALLED PANELS IAW 680 MM. INSTALLED NUTPLATES IN RT LSDR AALA20050477Fitting · out of limitsAFW - LEFT HAND STRUT OUTBOARD MIDSPAR FITTING HAS BEEN MACHINED TO 1.871 INCH DIAMETER ON NR 1 LUG. REPAIRED LEFT HAND STRUT OUTBOARD MIDSPAR FITTING ON NR 1 LUG PER SRM 54 51 90 2 FIGURE 203 SERVICE BULLETIN 767 54 0059.SDR ABXA050108Attach Angle · crackedUPPER PYLON ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED AREA IAW DC-9 SRM 54-04.SDR 05FDEA01175Fitting · corrodedNR 2 ENG FWD MOUNT FITTING HAS 2 EA BOLTS MOUNT HOLES AND 1EA SPIGOT HOLE CORRODED REF N00630. REMOVED AND REPLACED SPIGOT FITTING IAW SRM 51-72-10.SDR 05FDEA01174Attach Bracket · crackedNR 2 PYLON O/B SIDE RIB 9 PRECOOLER COMPT 1 EA ATTACH BRACKET CRACKED REF N00532. REMOVED AND REPLACED FITTING RT IAW SRM 51-72-10.SDR USAA050475Attach Fitting · damagedCLT - FOUND FITTINGS DAMAGED, FORWARD OUTBOARD MID BULKHEAD AND UPPER ATTACH FITTING HOLES, RT PYLON FORWARD OUTBOARD MID AND UPPER ATTACH FITTING HOLES. REPAIRED OVERSIZED HOLES AND FABRICATED REPAIR BUSHINGS IAW EA 96400. (M)SDR USAA050480Fitting · gougedPIT - FOUND GOUGED .4 INCH BY .4 INCH BY .020 INCH, AFT BOLT HOLE, NR 2 PYLON, INBOARD MID BULKHEAD. REAMED HOLE, FLAP PEEN, RE-SLEEVE AND BUSH PER EA 96439 AND 96450. (M)SDR ABXA050078Attach Angle · crackedNR 1 PYLON UPPER ATTACH ANGLE HAD 1 MISSING FASTENER AND CRACKED AT STA 1056. REPAIRED AREA IAW DC-9 SRM 54-04.SDR USAA050378Attach Fitting · damagedCLT - DROP IN FITTING, .020 INCH, ELONGATED. RT PYLON MID BULKHEAD UPPER LINK ATTACH FITTING. REWORKED HOLES IAW EA. (K)SDR SWAA050488Angle · crackedDURING SCHEDULED CHECK, FOUND NR 2 ENGINE UPPER PYLON ATTACH ANGLE, CRACKED. REMOVED AND REPLACED ATTACH ANGLE PER EA.SDR DL757050101Fitting · damagedFITTING REWORK REQUIRED FOR NR 2 AND NR 5 HOLES ON THE RIGHT WING SUPPORT FITTING. REPAIRED IAW ERA 389530-14AD.SDR DL757040995Fitting · damagedREPAIR OF OVERSIZED HOLE IN NR 2 PYLON SIDE LINK FITTING. REPAIRED IAW VA 69201AD.SDR CX7A194J0453Cowling · departedPORTION OF ENGINE COWLING DEPARTED A/C DURING FLIGHT. INSTALLED UPPER COWL FAIRING.SDR AALA20041114Fitting · oversizedAFW - RIGHT HAND PYLON LINK LOWER BEARINGS ON BOTH SIDES LOOSE IN THE LOWER FITTINGS. VISUALLY CHECKED BORE HOLES FOR CRACKS. INSTALLED BEARINGS WET WITH BMS5 26 SEALANT IPC/DRAWING NUMBER 311T2287 14 AND 13.SDR ASOA04838Attach Bracket · crackedDURING A C-CHECK, THE RT ENGINE LOWER NACELLE FORWARD LT CHANNEL NEAR THE UPPER COWLING ATTACHMENT BRACKET WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CRACKED LT UPPER EDGING OF THE RT ENGINE LOWER NACELLE IAW SRM 51-25-01.SDR 04FDEA02720Bearing · corrodedNR 3 PYLON TOMBSTONE FITTING UPPER BEARING PITTED. REMOVED AND REPLACED NR 3 PYLON UPPER SPHERICAL BEARING IAW DC10-30 MM 54-40-02-2.SDR 04FDEA02718Bearing · migratedNR 1 ENG PYLON AFT SPHERICAL BEARING ATTACH BOLT TORQUE STRIP BROKEN & THE BEARING MIGRATES. REMOVED AND REPLACED BEARING IAW DC 10-30 FEDEX MM 54-40-02-2, REMOVED CORROSION IAW DC10-30 FEDEX MM 54-40-02, REMOVED FUEL DRAIN LINE IAW FEDEX DC 10-30 MM 0- 50-01SDR 04FDEA02699Fitting · corrodedNR 1 PYLON TOMBSTONE FITTING UPPER BEARING STIFF AND PITTED. REMOVED UPPER SPHERICLE BEARING FROM NR 1 PYLON TOMBSTONE CHECKED DIAMETRICAL CLEARANCE OF NEW BEARING INSIDE DIA AND PLUG IS .0001 MAX CLEARNCE .012. CLEARANCE CHECK OK IDENTIFIED MOUNT BOLT TO BESDR DL757040875Fitting · damagedNR 2 PYLON LOWER SPAR FITTING HAD FOUR OVERSIZED FASTENERS. REPAIRED IAW ERA 092712-14AD.SDR 04FDEA02649Fitting · migratedNUMBER 1 ENGINE PYLON AFT SPHERICAL ATTACH BOLT TORQUE STRIPE BROKEN AND THE BEARING IS MIGRATING. REMOVED BEARING IAW DC10MM 54-40-02, REMOVED CORROSION IAW DC10 MM 54-40-02. REMOVED AFT BULKHEAD FITTING AUB 7025-33 IAW DC10-30 SRM 51-31-01 VOL II, LOCATED,SDR 04FDEA02648Fitting · migratedNUMBER 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATING. REMOVED SPHERICAL BEARING HONED HOLE REMOVED AFT BULKHEAD FITTING, LOCATED AND DRILLED NEW FITTING IAW DAC DWG AUB 7025, INSTALLED NEW FITTING P/N AUB 7025-33 IAW DAC DWG AUB 7025 IAW FEDEX DC10 SRM 51-38SDR UIEA200400137Fitting · crackedFOUND DURING D-CHECK AT SIN, DAMAGE WAS FOUND AT FASTENER HOLE IN THE FITTING AFT VERTICAL FLANGE. THE DAMAGE WAS COMPLETELY REMOVED BY OVERSIZING THE HOLE TO .4521-4541 INCHES DIAMETER. AN OVERSIZE FASTENER AS THE SAME DESIGN TYPE REQUIRED, WAS INSTALLED ATSDR 0401266638Frame · crackedDURING H-CHECK FOUND CRACK IN NR 1 PYLON REAR ENGINE MOUNT BULKHEAD FRAME WEB. REPAIRED PER EA 66-165160.SDR SWIA200413326Frame · crackedLEFT OUTBOARD NACELLE BRACKET ATTACHED TO GEAR DOOR HINGE POINT FRAME AND CRADLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER ON LEFT OUTBOARD HALF FRAME ATTACH BRACKET IAW 120 SRM 51-10-02 PG 2 SEC 2B.SDR CALA0400471Support Angle · crackedINSPECTION FOUND A 3 INCH CRACK IN SUPPORT ANGLE AT RT NACELLE STA 363.65 ON I/B SIDE RADIUS. A NEW SUPPORT ANGLE WAS INSTALLED IAW SRM 54-50-71 AND 51-40-02.
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