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 USAA2010032990672Attach Fitting · corrodedSAL - C6 - MAJOR REPAIR - CORROSION ON LOWER SURFACE OF LEFT FITTING BASE PLATE ATTACH ENGINE PYLON. REPAIRED LOWER SURFACE OF LEFT FITTING BASE PLATE ATTACH ENGINE PYLON IAW EA 132924.SDR WRLA20100315347Mount Fitting · corrodedENGINE PYLON FWD MOUNT TRUSS FITTING HAS CORROSION IN 2 AFT BOLT HOLES. REWORKED REPAIR IAW SERVICE GENERAL REPAIR DRAWING SG11540000.SDR DALA1011650661Fitting · corrodedNR 2 ENGINE UPPER LINK WING FITTING OTBD LUG HAS SPOTS OF CORROSION. REMOVED FITTING, COMPLIED WITH EA 06-075079-030 REV D PG 2 SHT1, REINSTALLED FITTING AT ST AEROSPACE SAT REF NON ROUTINE CARD 159680. (DL757101346)SDR FDEA201003100747Fitting · damagedRT WING AT NR 2 PYLON MOUNT AREA INBD STRUT MOUNT FITTING, BUSHING HAS SCRATCH AND WEAR MARKS. ACCOMPLISHED OVER SIZED LUG HOLE REPAIR IAW FINAL EA NR F-5720-131160, WINGS- FITTINGS-(AD 2004-12-07) NR 2 ENG PYLON INBD SIDE LOAD FITTING BUSHING O/S HOLE ANDSDR FDEA201003100746Fitting · gougedRT WING NR 2 PYLON MOUNTING AREA OTBD STRUT MOUNT FITTING HAS GOUGES ON 2 PLACES AT INNER AND OUTER SURFACE. ACCOMPLISHED FINAL EA F-5740-131580, WINGS-(AD 2004-12-7/EO F-5450-7-5003) RT OTBD SIDE LOAD FITTING GOUGED THIS IS MAJOR REPAIR.SDR DL757100812Fitting · damagedNR 2 PYLON SIDE LINK ATTACH FITTING HOLE NR 3 IS GREATER THAN 91 DEGREES. C/W ER/A 480025-14 AD REV ORIGINAL AT SAA DURING HMV ON N/R CARD 159219.SDR QXEA2010030100135Attach Fitting · wornPDX- C1 CHECK, RIGHT MAIN GEAR ALTERNATE EXTENSION ACTUATOR UPPER ATTACH POINT HAS PLAY. REMOVED BOLT FROM THE AIRCRAFT, REAMED THE HOLE TO 1.185 INCH MANUFACTURED A REPAIR BUSHING AND INSTALLED IAW RD 8/4-54-654. OPERATION SYSTEM CHECKS GOOD.SDR DL757100814Fitting · gougedNR 2 PYLON INBD AT NAC 200 BOTTOM CORNER OF BULKHEAD FITTING IS GOUGED. REPAIRED IAW ERA 480028-14 AD REV ORIG AT SAA NRC 155338.SDR DL757100805Fitting · gougedNR 2 PYLON OTBD AT NAC STA 200 BOTTOM CORNER OF BULKHEAD FITTING IS GOUGED. FOUND AFTER REMOVAL OF PYLON FROM RT WING. ACCOMPLISHED ER/A 480027-14 AD REV ORIGINAL AT SAA ON N/R CARD 155339.SDR IPXA10558453Bracket · crackedINSPECTION TYPE:C2, LT ENGINE PYLON: CRACKED ANGLE BRACKET AT STA 149.5 LT SIDE TOP OF PYLON FWD SIDE OF CROSSOVER FRAME. REMOVED CRACK ANGLE BRACKET. FABRICATED REPLACEMENT ANGLE BRACKET INSTALLED NEWLY FABRICATED ANGLE BRACKET.SDR DL757100581Attach Fitting · damagedNR 2 PYLON NEW SIDE LINK ATTACH FITTING P.N. 012N88887-10 HOLE NR 3 ANGLE MEASURE 94.4 DEGREE PER STEP 16 CONTACT ENGINEERING FOR INSTRUCTIONS / ACCOMPLISHED ERA 479772-14AD REV ORG AT SAA SAT REF NON ROUTINE 148876.SDR FDEA201001310294Fitting · crackedLT ENG PYLON, 2 EACH CRACKS FOUND IN LT AFT INBD BOLT HOLE ON HORIZ FLANGE. (REF: EO F-5450-7-5006 P1 PG 13 STEP 2 FOR DETAILS). LT PYLON AFT BULKHEAD R & R IAW EA NR F-5450-135814. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR CA100208005Fitting · worn(CAN) DURING REMOVAL OF THE ENGINE MOUNT FROM THE NACELLE THE LOWER MOUNT ATTACHMENT FITTINGS WERE FOUND LOOSE INSIDE THE NACELLE ON BOTH THE LT & RT SIDES. THE LT INBD AND OTBD LOWER FITTINGS WERE REPAIRED BY REMOVING THE FITTINGS NDT REINSTALLING THEN DRILLISDR FDEA201001260260Fitting · crackedNR 1 PYLON, ONE EACH CRACK FOUND AT FWD OTBD HOLE OF MID BULKHEAD. REFER EO F-5450-7-5005 P1 PG 19 STEP 1.8 FOR DETAILS. CRACKED FWD OTBD HOLE ON NR 1 PYLON MID BULKHEAD REPAIRED IAW EA NR F-5450-135810 (LT PYLON MID-BULKHEAD LOWER FLANGE INBD CRACK REPAIR). SDR FDEA201001260259Fitting · crackedRT ENGINE PYLON, 2 EACH CRACKS FOUND IN RT AFT INBD BOLT HOLE ON HORIZONTAL FLANGE. REF EO F-5450-7-5006 P2, PG 12 STEP 2. RT PYLON AFT BULKHEAD R & R IAW EA F-5450-135815 (AFT BULKHEAD FITTING REMOVAL AND INSTALLATION). REPAIR IS CLASSIFIED AS MAJOR IAW GSDR DL757100401Fitting · gougedNR 2 NACELLE STRUT LT LWR CORNER OF AFT BULKHEAD FITTING GOUGED. REPAIRED IAW ERA 479121-14AD REV ORIG.SDR A6WA201040159Bracket · brokenLT JET PIPE FIRE LOOP MOUNT COVER FWD MOUNT STANDOFF BRACKET BROKEN. REMOVED BROKEN BRACKET AND REPALCED WITH FABRICATED BRACKET.SDR USAA2010011490107Pin · wornMAJOR REPAIR - WEAR ON UPPER PIN OF RIGHT PYLON TO WING AFT ATTACH FITTING AT RIB 10. REPLACED UPPER PIN OF RIGHT PYLON TO WING AFT ATTACH FITTING AT RIB 10 IAW A320 AMM 54-51-17.SDR USAA2009123093450Pin · corrodedSAL - MAJOR REPAIR - Q4 CHECK - CORROSION ON THE NR 2 ENGINE RIGHT OUTBOARD MIDSPAR FUSE PIN. REPLACED THE NR 2 ENGINE RIGHT OUTBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01.SDR USAA2009123093449Pin · corrodedSAL - MAJOR REPAIR - Q4 CHECK - CORROSION ON THE NR 2 ENGINE RIGHT INBOARD MIDSPAR FUSE PIN. REPLACED THE NR 2 ENGINE RIGHT INBOARD MIDSPAR FUSE PIN IAW B737 AMM 54-10-01.SDR UALA2009122303983Bracket · damagedLH ENG STRUT PLUMBING INSP: FOUND PRESSURE LINE CLAMP BLOCK FASTENERS SHEARED AND FASTENER HOLES ELONGATED IN CLAMP BLOCK BRACKET AT NAC STA 149.5. REPLACED BRACKET, BLOCKS AND CHANNEL RETAINER.SDR USAA2010050790920Pin · corrodedCLT - MAJOR REPAIR - Q4 CHECK - CORROSION ON LEFT WING PYLON OUTBOARD FUSE PIN. REPLACED THE LEFT WING PYLON OUTBOARD FUSE PIN IAW B737 AMM 54-10-01.SDR USAA2010050790919Pin · corrodedCLT - MAJOR REPAIR - Q4 CHECK - CORROSION ON LEFT WING PYLON INBOARD FUSE PIN. REPLACED THE LEFT WING PYLON INBOARD FUSE PIN IAW B737 AMM 54-10-01.SDR DL757100340Fitting · damaged1 PYLON WEB LWR SPAR AND LWR SPAR FITTING AT STA 199 FOUND OVERSIZED HOLE / ACCOMPLISHED ERA 478210-14AD AT SAA SAT REF NON ROUTINE 137086.SDR A6WA200940795Bracket · crackedRT ENGINE FAN CASE, P2T2 SENSOR LINE OTBD BRACKET CRACKED RT ENGINE FAN CASE P2T2, SENSOR LINE OTBD BRACKET REPLACED IAW SHORTS CMM 20-42-06. (K)SDR A6WA200940797Bracket · crackedRT ENGINE TAILPIPE FAIRING FIRELOOP COVER FWD BRACKET RT ENGINE TAILPIPE FAIRING FIRELOOP COVER FWD BRACKET REPLACED IAW SHORTS CMM 20-42-06. (K)SDR A6WA200940793Retainer · crackedLT PYLON PANEL 412DB FOUND WITH SEAL RETAINER CRACKED, LT PYLON PANEL 412DB SEAL RETAINER REPLACED IAW SRM 51-42-06. (K)SDR DL757100350Fitting · chafedNR 2 NACELLE STRUT AFT BULKHEAD FITTING LOWER OTBD CORNER HAS DEEP CHAFING DAMAGE. ACCOMPLISHED ERA 478035-14 REV ORIG AT SAA SAT REF NON ROUTINE CARD 139671.SDR C2XA09TY261Yoke · crackedTYS - A/C CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE NR 2 ENGINE FWD/LOWER YOKE WEBBING CRACKED. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE FWD/LOWER YOKE IAW EC 5450-01028 AND TASK CARD 6271001. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASDR A6WA200940713Bracket · crackedRT ENG INBD T/R STOW/THROTTLE LOCK OUT SWITCH BRACKET AT 9 O`CLOCK POS FOUND CRACKED. RT ENG INBD T/R STOW/THROTTLE LOCK OUT MICRO SWITCH BRACKET AT 9 O`CLOCK POS REPAIRED/ REPLACED IAW SRM 51-42-06. (K)SDR C2XA09SH314Yoke · crackedSHV - DURING C-CHECK, NR 2 ENG FWD LOWER ENG YOKE CRACKED. REMOVED AND REPLACED NR 2 FWD LOWER ENG YOKE IAW EC 5450-01028. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR FDEA200908243079Fitting · corrodedNR 2 PYLON LT AFT T/R FITTING FOUND CORRODED. FITTING REMOVED AND REPLACED IAW SOPM 20-50-01 REV 108. REPAIR IS CLASSIFIED IAW GMM 6-2-100 CRITERIA.SDR FDEA200908243078Fitting · corrodedNR 1 PYLON RT T/R AFT FITTING FOUND CORRODED. CORROSION ON RT T/R FITTING ON NR 1 PYLON FOUND EXCEEDED SRM DAMAGE LIMITS. FITTING REMOVED AND REPLACED IAW AMM 20-11-00 REV 4. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.SDR ABXR200908240017Fitting · damagedDURING THE REPETITIVE INSP NR 1 ENG PYLON SUPPORT FITTING IAW SB 2000-5410A0 2000-19-24, HOLES I, J, K, AND L WERE VISUALLY FOUND ELEGONGATED AND HOLES WERE FOUND PREVIOUSLY OVERSIZED TO MAX ALLOWABLE DIA. 0.2817 INCH. ENG MOUNT WAS REMOVED AND RE-INSTALLED ASDR FDEA200908203055Fitting · looseRT PYLON DIAGONAL BRACE FITTING SHIM TOTAL CUMULATIVE MOVEMENT APPROX 0.75 INCHES FOUND LOCATED AT RT TOP BETWEEN VERTICAL FLANGE AND BULKHEAD. REPAIR CARRIED OUT IAW EA F-5450-131090 : RT PYLON STRUT-TO-DIAGONAL BRACE FITTING SHIM MIGRATION REPAIR. REPAIRSDR C2XA09TY224Fitting · crackedNR 2 ENG FWD LWR PYLON CRACKED AT STOP DRILLED HOLE. REMOVED AND REPLACED NR 2 ENG FWD LWR YOKE LINKAGE FITTING.SDR LR7A2009080400094Attach Bracket · crackedDURING SCHEDULED C-8 CHECK IAW JOB CARD HC7201, FOUND NR 3 ENG OIL COOLER EXHAUST DUCT LT UPPER FRAME CRACKED AT FS442.7. REPAIRED IAW LAC MEA 382-54-09-021.SDR FDEA200907152622Fitting · chafedFOUND NICKS AND CHAFING MARKS ON LT PYLON AFT ATTACH LUGS REPAIR PERFORMED BY BLEND OUT THE DAMAGE , NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1009953/2009 ISS.A , APPROVED BY EA 6-5740-129166.SDR FDEA200907102571Attach Fitting · chafedFOUND NICKS AND CHAFING MARK ON RT PYLON AFT ATTACH FITTINGS. REPAIR PERFORMED BY BLEND OUT THE DAMAGES IAW RAS/BAE/1009953/2009 ISS.A, APPROVED BY EA 6-5740-129167.SDR IPXA09556743Access Panel · chafedINSPECTION TYPE: C2 NR 1 ENG PYLON ACCESS PANEL 434 BR HAS CHAFE DAMAGED SURFACE. REMOVED AND REPAIRED WITH FABRICATION REPLACEMENT PART.SDR IPXA09556725Attach Angle · crackedINSP TYPE: C2 ENG NR 1 NAC STRUT STA 284 INBD FRAME HAS ATTACH ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02.SDR FDEA200906152095Fitting · corrodedFOUND CORROSION ON PYLON NR 1 LOWER FITTING, RIB 12. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200906152094Fitting · corrodedFOUND CORROSION ON PYLON NR 2 LOWER FITTING, RIB 12. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR SWIA200922012Support Fitting · crackedRIGHT NACELLE POWER LEVER CABLE PULLEY SUPPORT FITTING CRACKED. (C CHECK) REPLACED SUPPORT FITTING.SDR FDEA200905261800Fitting · crackedCRACK AT 3 O'CLOCK POSITION FOUND ON LOWEST FASTENER HOLE ON NR 4 BANJO FITTING RT SIDE AFT LOCATION COMMON TO THE CARRY THROUGH CAP. COMPLIED WITH EA NR 1-5530-49623, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 107.SDR QXEA2009051500336Attach Angle · crackedPDX - C5 - THE RT INBD FWD ATTACH ANGLE FOR THE SPINE COWL ON THE NR 1 ENGINE NACELLE IS CRACKED. REMOVED NR 1 ENGINE INBOARD FWD ATTACH ANGLE FOR THE SPINE COWL IAW SRM 51-42-05-2-01 PARA 4E. FABRICATED NEW NR 1 ENGINE RT INBD FWD ATTACH ANGLE FOR THE SPINESDR 2009FA0000389Attach Angle · crackedLT INBD ENGINE NACELLE TO WING STRUCTURAL ATTACH POINT (ANGLE). CRACKED AT MID-POINT IN RADIUS. DISCOVERED DURING SID INSPECTION.SDR C2XA09TY051Yoke · crackedTYS - DURING C-CHECK THE NR 1 ENGINE LOWER FORWARD YOKE WAS FOUND CRACKED AT ENGINE MOUNT WEBBING. THE NR 1 ENGINE LOWER FORWARD YOKE MOUNT WEBBING AFT SECTION WAS REMOVED AND REPLACED IAW EC 5450-01019. A/C IS STILL IN C-CHECK.SDR IPXA09555030Support · damagedINSPECTION TYPE:C3 UPON REMOVAL FOUND NR 2 PYLON FAN COWL SUPPORT BEAM O/B RAIL EDGE DAMAGE APPROXIMATELY 2 INCHES FROM AFT END. REPAIRED FAN COWL SUPPORT BEAM O/B RAIL IAW ER 09-1804.SDR IPXA09555029Support · crackedINSPECTION TYPE:C3 NR 2 PYLON FWD RT FAN COWL BEAM O/B RAIL CRACKED 8 INCHES FROM FRONT END. REPAIRED FAN COWL SUPPORT BEAM RAIL IAW ER 09-1804.
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