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.

SDR AALA20040317Fitting · oversizedTUL - OUTBOARD LOWER FORWARD HOLE OVERSIZED WHEN CRACK REMOVED AT NR 1 MID BULKHEAD FITTING. AREA IS 0.640 BY 0.640 WITH A DEPTH OF 0.250. FABRICATED BUSHING AND INSTALLED PER ESO 90309. 757 SRM 54-50-02, 51-20-07, 757 AARD 54-50-003, SERVICE BULLETIN 757-54Mar 3, 2004 · N656AA · Boeing 757223SDR CALA0400141Support Fitting · crackedINSPECTION FOUND NR 2 ENGINE PYLON O/B MID SPAR FITTING PANEL AFT RETAINER (SUPPORT FITTING) CRACKED AT UPPER AREA, PYLON STA 279.5. THE SUPPORT FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.Feb 20, 2004 · N14347 · Boeing 7373T0SDR CALA0400135Attach Fitting · crackedINSPECTION FOUND A .25 INCH CRACK IN NR 2 PYLON PANEL 5842 FORWARD ATTACH RAIL. THE ATTACH RAIL WAS REMOVED AND REPLACED IAW SRM 51-10-02.Feb 19, 2004 · N14347 · Boeing 7373T0SDR UIEA200400016Attach Fitting · crackedDURNG D-CHECK AT SIN ON NR 1 PYLON DIAGONAL BRACE ATTACH FITTING, HFEC INSPECTOIN FOUND CRACK IN HOLE LOCATION REF 'A'. HOLE OVERSIZED TO .0405, BUT CRACK REMAINS. THE DEFECT WAS COMPLETELY REMOVED BY OVERSIZING THE HOLE TO .434 INCHES PRIOR TO FURTHER OVERSFeb 13, 2004 · N517MC · Boeing 747243BSDR SWIA200412979Cradle · crackedRIGHT OUTBOARD EXHAUST CRADLE OUTBOARD CORNER IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. INSTALLED EXTERNAL DOUBLER IAW EMB SRM 51-10-02.Jan 25, 2004 · N197SW · Emb EMB120ERSDR SWIA200412976Attach Bracket · crackedATTACH BRACKET CRACKED AT LEFT NACELLE OUTBOARD OF WHEEL WELL AT 3RD RIVET FROM BOTTOM (INTERIOR OF WALL). DISCOVERED DURING C-CHECK INSPECTION. REPAIRED BRACKET LOCATED AT LEFT NACELLE OUTBOARD OF WHEEL WELL IAW EMB120 SRM 54-10-03 PAGE 202 FIG 201 SHEET 1.Jan 25, 2004 · N197SW · Emb EMB120ERSDR UPS04441936Fitting · corrodedNR 4 PYLON DIAGONAL BRACE UNDERWING FITTING, HOLE NR 10 I/B ROW MOST AFT CORROSION FOUND ON BACKUP FITTING BORE AREA. DEFECTIVE AREA FASTENER HOLE CORROSION REPAIR CARRIED OUT AS PER HX RS R57-24-35102 AND EO B747-5740-19955-A. FINAL HOLE 0.562 INCH TO CLEANJan 25, 2004 · N672UP · Boeing 747123SDR UPS04441908Fitting · corrodedINSPECTION TYPE: C, NR 3 PYLON DIAGONAL BRACE FWD ATTACH FITTING BASE AREA PITTING CORROSION FOUND. NR 3 PYLON DIAGONAL BRACE ATTACH FITTING LOWER SURFACE CORROSION REPAIR CARRIED OUT AS PER HX RS R-54-54-35098. (FAA 8110-3 DATED FEB 5, 2004 & EO B747-5440-Jan 25, 2004 · N672UP · Boeing 747123SDR SWIA200412814Attach Bracket · crackedRIGHT HYDRAULIC RESERVOIR OUTBOARD ATTACH BRACKET CRACKED. DISCOVERED DURING LINE INSPECTION. REMOVED AND REPLACED ATTACH BRACKET IAW EMB 51-10-06 AND 51-40-02.Jan 25, 2004 · N585SW · Emb EMB120ERSDR CALA0300721Fitting · corrodedINSPECTION FOUND NR 2 ENGINE PYLON OB CROSSBEAM MOUNT FITTING CORRODED. THE FITTING WAS REPAIRED IAW ECRA 5440-01235.Dec 23, 2003 · N12322 · Boeing 7373T0SDR AUS20031333Fitting · cracked(AUS) ENGINE MOUNT FITTINGS PN 68-1.2025-1 AND PN 68-1.2025-2 CRACKED AROUND RIVET HOLES.Dec 15, 2003 · Parten P68BSDR ABXA030485Attach Angle · crackedNR 1 ENGINE UPPER PYLON ATTACH ANGLE WAS CRACKED AT STA 1056 AND HAD 1 SHEARED FASTENER. REPAIRED IAW DC-9 SRM 54-04.Dec 12, 2003 · N956AX · Doug DC941SDR ABXA030490Attach Angle · crackedNR 1 ENGINE UPPER PYLON ATTACH ANGLE WAS CRACKED AT STA 1114. REPAIRED AREA IAW DC-9 SRM 54-04.Dec 12, 2003 · N956AX · Doug DC941SDR SWIA200312760Rib · crackedLT PYLON FS 605 RIB CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIB IAW CRJ SRM 51-40-11. P/N: 601-37004-85.Nov 28, 2003 · N592SW · Cndair CL6002B19SDR KBM2003F00096Bearing · wornRT SIDE PYLON MOUNT FORWARD/AFT BEARING WORN. INSTALLED 2 NEW BEARINGS.Nov 19, 2003 · N73DP · Bell 206BSDR SWIA200312671Bulkhead · crackedRIGHT ENGINE AFT OUTBOARD SIDE LOWER NACELLE BULKHEAD CRACKED AT HYDRAULIC LINE CONNECTIONS. LOCATION REF: S/B 120-29-0049 PAGE 15, FIG 2, DET D. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED OUTBOARD LOWER RIGHT NACELLE FIREWALL IAW EMBRAER INSTRUCTIONS Nov 14, 2003 · N568SW · Emb EMB120ERSDR CALA0300648Fitting · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 1 PYLON FORWARD FITTING AT LOWER I/B CORNER. THE NR 1 PYLON FORWARD FITTING WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.Nov 14, 2003 · N14320 · Boeing 7373T0SDR 03FDEA01843Mount · corrodedCOMPLY WITH EA 6-5450-73844A PYLONS/NACELLS - NR 1 ENGINE PYLON FWD MOUNT CORROSION REPAIR. CLOSING ACTION ON 10/31/03 ON N/R S00016. COMPLIED WITH EA 6-5450-73844A.Oct 31, 2003 · N660FE · Airbus A300F4605RSDR UPS03441483Attach Fitting · crackedINSPECTION TYPE: C, NR 2 PYLON DIAGONAL BRACE STEEL ATTACH FITTING HORIZONTAL FLANGE ATTACH BOLTS 6EA TORQUE CHECK FOUND LOOSE AS MARKED. THE BOLT HOLE ID MEASURED, NR 5, 7, 9 ARE 0.314 INCH NR 8, 10 ARE 0.313 INCH & NR 15 IS 0.316 INCH NDT HFEC INSP CONFIRMOct 18, 2003 · N525UP · Boeing 747212BSDR DL733030855Beam · corrodedCORROSION WAS FOUND IN THE AFT LUG BORE OF THE NR 1 PYLON CROWN BEAM FITTING AT NAC STA 257.25. THE BORE WAS OVERSIZED TO REMOVE THE CORROSION, HFEC INSPECTED, AND STEEL REPAIR BUSHINGS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 385679-14.Sep 17, 2003 · N312WA · Boeing 737347SDR ARWA20030903Fitting · crackedDURING (A) CHECK INSPECTION THE FOLLOWING WAS FOUND; NR 3 PYLON UPPER SECTION, FRONT SPAR AND FOOT STOOL SPLICE FITTING WITH 3 INCH CRACK.Sep 5, 2003 · N29UA · Doug DC861SDR SWIA200312411Channel · crackedLT MLG INSIDE WELL FORWARD OUTBOARD CRACK ON NACELLE. (DISCOVERED DURING C-CHECK INSPECTION) LT MLG OUTBOARD CHANNEL REPLACED SRM120 51-10-02.Aug 25, 2003 · N214SW · Emb EMB120ERSDR AMTA200301134Attach Fitting · damagedNR 1 PYLON UPPER LINK ATTACH FITTING TO MID-BULKHEAD SHIMS MIGRATING. COMPLIED WITH ER/A 757-54R-5285. (M)Aug 24, 2003 · N555TZ · Boeing 75733NSDR USAA030166Fitting · corrodedFOUND PITTING ON LOWER BEARING BORE .5 INCH BY .5 INCH. MACHINED BEARING BORE PER 71-21-14, MAJOR REPAIR PER 925-90. (M)Aug 19, 2003 · N655US · Boeing 7672B7SDR SWIA200312404Channel · crackedBLUE HYDRAULIC PACK LOWER SUPPORT CHANNEL CRACKED IB EDGE. (DISCOVERED DURING C-CHECK INSPECTION) REPLACED LOWER SUPPORT CHANNEL WITH SERVICEABLE UNIT FOR BLUE HYDRAULIC PACK.Aug 9, 2003 · N298SW · Emb EMB120ERSDR EIA2003104Skin · tornNR 4 PYLON I/B SKIN TORN OUT AFT OF AFT ENGINE MOUNT. DAMAGED AREA REPAIRED PER ECRA 485-54-138-2, REV A.Jul 25, 2003 · N485EV · Boeing 747212BSDR AWXA200300830Angle · crackedDURING B-02 CHECK A .75 INCH CRACK WAS FOUND ON PANEL ATTACH ANGLE AT OUTBOARD SIDE OF NR 1 PYLON, RIB 8. MAINTENANCE CUT OUT DAMAGE ON ATTACH ANGLE AT OUTBOARD SIDE OF NR 1 PYLON, RIB 8; FABRICATED A REPAIR ANGLE AND FILLER; INSTALLED REPAIR PARTS IAW A319 SJul 18, 2003 · N821AW · Airbus A319132SDR AWXA200300800Attach Angle · crackedMCN - MAJOR REPAIR - DURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON RT PYLON UPPER ATTACH ANGLE AT SCREW HOLE FORWARD OF RIB 8. MAINTENANCE CUT OUT DAMAGE ON RT PYLON ATTACH ANGLE FORWARD OF RIB 8; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A3Jun 28, 2003 · N624AW · Airbus A320231SDR AWXA200300799Attach Angle · crackedDURING C-03 CHECK A .5 INCH CRACK WAS FOUND ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7. MAINTENANCE CUT OUT DAMAGE ON LT PYLON PANEL ATTACH ANGLE AT INBOARD SIDE, AFT OF RIB 7; FABRICATED A FILLER AND SPLICE; INSTALLED REPAIR PARTS IAW A320 Jun 28, 2003 · N624AW · Airbus A320231SDR ABXA030306Attach Angle · crackedRIGHT PYLON LEADING EDGE INBOARD ATTACH MOUNT HAD CRACKED REPAIR ANGLES. REMOVED, FABRICATED NEW ANGLE AND INSTALLED IAW DC-9 SSRM DWG K05159.Jun 19, 2003 · N966AX · Doug DC941SDR SWIA200312161Support · crackedRT HYDRAULIC PACK LOWER SUPPORT, CRACKED IB EDGE. (DISCOVERED DURING C-CHECK)REPLACED RIGHT HYD PACK LOWER SUPPORT.Jun 10, 2003 · N563SW · Emb EMB120ERSDR SWIA200312090Floorbeam · crackedFS 280 LBL 9.0 FLOORBEAM INBOARD ATTACH ANGLE CRACKED. (DISCOVERED DURING C-CHECK) ANGLE REPLACED IAW CRJ SRM 51-40-11. P/N: 601R311011-73SAJun 4, 2003 · N591SW · Cndair CL6002B19SDR ABXA030215Attach Angle · crackedNR 2 ENGINE LOWER PYLON ATTACH ANGLE WAS CRACKED AT STA 1030. REPLACED ATTACH ANGLE IAW DC-9 SRM 51-30-1.May 28, 2003 · N970AX · Doug DC941SDR SWIA200312122Bracket · crackedLEFT LOWER OUTBOARD HYDRAULIC PACK BRACKET CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED LEFT LOWER OUTBOARD HYDRAULIC PACK BRACKET WITH NEW ONE.May 22, 2003 · N189SW · Emb EMB120ERSDR SWIA200312117Bracket · crackedRT ELECTRIC HYDRAULIC PUMP ATTACH BRACKET CRACKED. FOUND DURING C-CHECK INSPECTION. NEW BRACKET INSTALLED IAW SRM 120 51-10-02.May 22, 2003 · N189SW · Emb EMB120ERSDR QXEA0300435Attach Fitting · wornNR 2 NACELLE MID FRAME ASSEMBLY INBOARD LOWER COWL ATTACH LUG HAS ROUGH WEAR IN HOLE. REPAIRED IAW HORIZON AIR EA 6-71-86 AND RD8/4-54-124.Apr 4, 2003 · N407QX · Bombdr DHC8401SDR DL733030313Fitting · corrodedTHE AFT LUG OF THE CROWN BEAM FITTING ON THE NR 2 ENGINE PYLON WAS FOUND WITH CORROSION IN THE HOLE BORE. THE BORE WAS OVERSIZED TO 3.10 INCH TO REMOVE THE CORROSION. A STEEL REPAIR BUSHING WAS INSTALLED AND THEN A NEW BEARING. THE REPAIR WAS ACCOMPLISHED PMar 29, 2003 · N309WA · Boeing 737347SDR AUS20030253Sleeve · corroded(AUS) RT PYLON SPIGOT BEARING SLEEVE PITTED AND CORRODED ON INSIDE SURFACE. FOUND DURING INSPECTION IAW J9-IA57-0824(2).Mar 3, 2003 · Airbus A320211SDR P5CA0300725Brace · gougedNICK/GOUGE FOUND AT SAILBOAT AREA OF PYLON #1 DIAGONAL BRACE - LOCATED APPROX 10:00 O'CLOCK POSITION, 29" FROM FWD END AT ZONE 5. DAMAGED AREA BLEND-OUT CARRIED OUT - FINAL DIMENSION LENGTH 2.0, WIDTH 1.525, DEPTH 0.100. THESE FIGURES ARE WITHIN LIMITS PER BOEJan 14, 2003 · N922FT · Boeing 7472U3BSDR P5CA0300722Fitting · crackedSIX CRACKS TOTAL FOUND NR 4 REAR ENG MOUNT BATHTUB FITTING: I/B FASTENER HOLE HAS 3 CRACKS - (1) .125 INCH, (1) .1875 INCH & (1) .75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1) .125 INCH, (1) .5 INCH & (1) .75 INCH RADIALLY. CRACKED BATHTUB FITTING Jan 12, 2003 · N922FT · Boeing 7472U3BSDR P5CA0300721Fitting · crackedFIVE CRACKS TOTAL FOUND NR 3 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1.5 INCH & (1) .75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX .5 INCH & (2) .125 INCH EA RADIALLY. CRACKED BATHTUB FITTINGJan 12, 2003 · N922FT · Boeing 7472U3BSDR P5CA0300720Fitting · crackedFIVE CRACKS TOTAL FOUND NR 2 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1 INCH & (1) .875 INCH RADIALLY/ O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX .75 INCH & (2) 1 INCH EA RADIALLY. CRACKED BATHTUB FITTING REPJan 12, 2003 · N922FT · Boeing 7472U3BSDR P5CA0300718Fitting · crackedTWO CRACKS FOUND AROUND INBOARD AND OUTBOARD FASTENER HOLES NR 1 PYLON REAR ENGINE MOUNT BULKHEAD BATHTUB FITTING. - I/B: (1) .75 INCH, (1) .125 INCH RADIALLY. O/B: (1) .75 INCH, (1) .5 INCH RADIALLY. CRACKED BATHTUB FITTING REPLACED AS PER S/B 747-54-2113 R2Jan 9, 2003 · N922FT · Boeing 7472U3BSDR AWXA200600746Bushing · migratedDISCREPANCY WAS "RT WING NR 2 ENGINE PYLON UPPER LINK, FRONT SPAR ATTACH O/B LUG BUSHING IS MIGRATED O/B LUG I/B BUSHING APPROX .040"". MAINTENANCE PLACED ITEM ON MONITOR TO BE REINSPECTED EVERY 3000 CYCLES AND TO TERMINATE IN 12,000 CYCLES IAW AWA ER 19-5449Dec 20, 2002 · N910AW · Boeing 7572G7SDR EVAS091023Bearing · looseDURING ROUTINE MAINT INSPECTION, FOUND BEARING FREELY ROTATED AND GAP BETWEEN BEARING OUTER RACE AND FITTING LUG ON NR 1 PYLON LT SIDE LOAD FITTING & NR 2 PYLON RT SIDE LOAD FITTING REPLACED SIDE LOAD FITTING BEARING.Dec 11, 2002 · N16605 · Boeing 767300SDR AUS20021411Bolt · corroded(AUS) NR 1 STRUT FUSE PIN SECONDARY RETENTION BOLT SHOWED EVIDENCE OFCORROSION UNDER THE HEAD. FOUND DURING INSPECTION IAW AD/B747/85.Dec 10, 2002 · Boeing 747438SDR CA021030005Attach Angle · cracked(CAN) DURING ROUTINE 100 HOUR INSPECTION FOUND CRACKED LT AND RT PLATES LOCATED ON INBOARD SIDE OF NACELLE JUST AFT OF FIREWALL. PLATES ATTACH SKIN OF NACELLE TO FRAME. AIRCRAFT IS OPERATED FOR LOW LEVEL TERRAIN FOLLOWING SURVEY. PREVIOUSLY FOUND SAME PLATES COct 15, 2002 · Piper PA31350SDR 02FDEA00741Fitting · corrodedLT PYLON AFT THRUST AND SIDE LOAD FITTING CORRODED AT BEARING FACE. R&R FITTING PER EA 6-5450-66460.Oct 15, 2002 · N419FE · Airbus A310SDR 02FDEA00739Fitting · corrodedSIGNS OF CORROSION AT L/PYLON THRUST & SIDE LOAD FITTING SLEEVE. R&R FITTING PER EA 6-5450-66458.Oct 15, 2002 · N419FE · Airbus A310SDR 02FDEA00738Fitting · corrodedR/SING PYLON FWD THRUST AND SIDE LOAD FITTING AREA, FOUND BEARING AREAS WITH BROWNISH STAINS AT TOP & BOTTOM OF FITTING. R&R FITTING PER EA 6-5450-66461.Oct 15, 2002 · N419FE · Airbus A310
Back to JASC 5415