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 C2XA09SH068Attach Fitting · corrodedSHV - DURING C-CHECK NR 2 ENG INLET ATTACHMENT FLANGE HAS MULTIPLE SCREW HOLES WITH CORROSION. MAINTENANCE REPAIRED NR 2 ENG INLET ATTACHMENT FLANGE SCREW HOLES IAW EC5420-01158. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.Mar 1, 2009 · N12900 · Emb EMB145SDR DL757090305Fitting · damagedWHILE ACCOMPLISHING DAL EA 06-070332-03AD ON THE RT PYLON OUTBOARD SIDE LOAD FITTING, TOOLING DAMAGE WAS INCURRED AT ONE FASTENER LOCATION. THE DAMAGE WAS REPAIRED PER BOEING INSTRUCTIONS AND AN AMOC TO AD 2003-18-05 WAS OBTAINED.Feb 24, 2009 · N651DL · Boeing 757232SDR FDEA200902240684Attach Fitting · corrodedFOUND CORROSION ON PYLON NR 1 RIB 18, ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION IAW SB 54-6018, APPROVED BY EA 6-5450-120174.Feb 24, 2009 · N750FD · Airbus A300B4622RSDR FDEA200902240683Attach Fitting · corrodedFOUND CORROSION ON PYLON NR 1 RIB 18, ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION IAW SB 54-6018.Feb 24, 2009 · N750FD · Airbus A300B4622RSDR DL76S090115Fitting · fracturedDURING ACCOMPLISHMENT OF INSPECTIONS PER ROUTINE OPN 5281AD (EA 01-074944-12AD, ME-02) THE AFT MOST INBOARD BOLT THROUGH THE NR 2 PYLON INBOARD MIDSPAR FITTING WAS FOUND FRACTURED. THE BOLT WAS SUCCESSFULLY REMOVED. IN ADDITION, THE LOCK FASTENERS COMMON TO Jan 27, 2009 · N135DL · Boeing 767332SDR USAA2009012690158Attach Fitting · corrodedPHL - ENGINE CHANGE - MAJOR REPAIR - EXFOLIATION OF CADMIUM COATING ON MATING SURFACE OF LEFT PYLON TO ENGINE ATTACH FITTING MATING SURFACE. REPAIRED CADMIUM COATING ON MATING SURFACE OF LEFT PYLON TO ENGINE ATTACH FITTING MATING SURFACE IAW A320 AMM 20-2015-Jan 24, 2009 · N278AY · Airbus A330323SDR FDEA200812195234Fitting · corrodedNR 2 PYLON TO WING ATTACHMENT FITTING LUG INNER RACE BEARING AT RIB 18 RUSTED. R & R AFT ATTACH FITTING IAW AMM 54-51-75-4-02 TW - T8312G.Dec 19, 2008 · N428FE · Airbus A310SDR FDEA200812105118Attach Fitting · crackedRIGHT WING AFT OTBD PYLON FAIRING SUPPORT ATTACH FITTING ON THE WING, RIB 9, STRINGERS 8 - 9, IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3 A57250004, ISSUE "E" AND SRM 51-40-21, PARA 7 AND PART 5.Dec 10, 2008 · N428FE · Airbus A310203SDR 08FDEA04904Skin · damagedWHILE DRILLING THE NR 1 PYLON INBD FWD 311N5193-2 SKIN PANEL NUMEROUS FASTENER HOLES WERE OVERSIZED AND ELONGATED. THE NUMEROUS FASTENER HOLES THAT WERE OVERSIZED AND ELONGATED WERE REPAIRED AND A NEW 311N5193-2 SKIN PANEL INSTALLED PER MAE EA NR 757-5452-1Nov 17, 2008 · N915FD · Boeing 757236SDR FDEA200810274585Fitting · mislocatedNR 1 PYLON , WHEN THE 311N5220-52 BATHTUB FITTING WAS LOCATED AND DRILLED C/M TO THE INBD LOWER SPAR 3 EA HOLES WERE MISLOCATED CAUSING A MISALIGNMENT C/M TO THE LWR SPAR. REAMED OTBD HOLE "A" TO 0.3267 DIA. AND INSTALLED 1 EA. BACB30US5K(*) X BOLT. REAMED OTOct 27, 2008 · N920FD · Boeing 75723ASDR SWIA200820196Mount · crackedLEFT MLG HYDRAULIC PACK LOWER O/B MOUNT CRACKED. C-CHECK, REPLACED MOUNT. Oct 19, 2008 · N582SW · Emb EMB120ERSDR 08FDEA04416Attach Angle · crackedNR 3 PYLON L/E HEAT EXCHANGER ACCESS AREA FWD ATTACH ANGLE IS CRACKED. REMOVED & INSTALLED PANEL IN REF TO SRM 51-31-01. REMOVED & INSTALLED ANGLE IN REF TO SRM 51-35-01. FABRICATED ANGLE IN REF SRM 51-21-01. PART MARKED FX AUB 7083-13 IN REF TO GMM 7-0Oct 17, 2008 · N390FE · Doug MD1010FSDR 08FDEA04410Attach Bracket · chafedNR 1 ENGINE PYLON, FWD APRON PANEL ATTACHING BRACKET AT STA YN 281 HAS A 1/2 INCH CHAFED HOLE ON THE EDGE. REMOVED & REPLACED FAIRING SUPPORT PER DWG AUB 7083; REV " K " & SRM 51-31-01; VOL II.Oct 17, 2008 · N390FE · Doug MD1010FSDR 08FDEA04385Mount · wornWITH REFERENCE TO SNRM N01236, DURING BEARING REMOVAL AT NR 1 PYLON AFT MOUNT FITTING BORE FOUND WORN. REMOVED AND REPLACED AS PER SRM 51-31-01 VOL. II. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.Oct 17, 2008 · N576FE · Doug MD11FSDR HNAA2009012500028Attach Fitting · corrodedCORROSION AROUND 1 FASTENER ON THE REAR SPAR ATTACHMENT TO OTBD NACELLE. REPAIR ATTACHMENT TO OTBD NACELLE WITH HI LOCKS IAW STRUCTURAL REPAIR MANUAL 51-40-00.Oct 15, 2008 · N327EN · Dhav DHC8311SDR 08FDEA04003Fitting · corrodedFOUND CORROSION ON PYLON NR 2 UPPER AND LOWER SPIGOT FITTING AROUND BEARING SEAT. REPAIR PERFORMED BY INSTALLATION OF CORROSION RESISTENT FITTING IAW SB A300-54-6017, APPROVED BY EA 6-5451-123011.Sep 23, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA04002Fitting · corrodedFOUND CORROSION ON PYLON NR 1 UPPER AND LOWER SPIGOT FITTING AROUND BEARING SEAT. REPAIR PERFORMED BY INSTALLATION OF CORROSION RESISTENT FITTING IAW SB A300-54-6017, APPROVED BY EA 6-5451-123011.Sep 23, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA03998Fitting · damagedFOR A REPAIR THE NEW PYLON SPIGOT FITTING FOR PYLON NR 2 HAVE BEEN DELIVERED WITHOUT ATTACHMENT HOLES AND SURFACE PROTECTION. REPAIR PERFORMED BY DRILL SPIGOT FITTING BY COPY OF OLD PART, PERFORM SPRAYING SURFACE PROTECTION AND INSTALL FITTING PER DRAWING RSep 23, 2008 · N744FD · Airbus A300B4622RSDR 08FDEA03997Fitting · damagedFOR A REPAIR THE NEW PYLON SPIGOT FITTING FOR PYLON NR 1 HAVE BEEN DELIVERED WITHOUT ATTACHMENT HOLES AND SURFACE PROTECTION. REPAIR PERFORMED BY DRILL SPIGOT FITTING BY COPY OF OLD PART, PERFORM SPRAYING SURFACE PROTECTION AND INSTALL FITTING PER DRAWING RSep 23, 2008 · N744FD · Airbus A300B4622RSDR DALA1100880180Attach Fitting · crackedPYLON WING TO STRUT ATTACH FITTINGS, NR 2 PYLON FWD UPPER SPAR BUSHING. REPAIRED IAW ERA 470658-14.Sep 17, 2008 · N180DN · Boeing 767332SDR 08FDEA03809Mount · chafedFOUND CHAFING MARKS ON PYLON NR 1 FWD MOUNT FITTING ON PYRAMID. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARK, NDT FOR CRACK FREE CONDITION AND CADMIUM PLATING IAW RAS/70512885/011/2008 ISS A, APPROVED BY EA 6-5451-123062.Sep 11, 2008 · N744FD · Airbus A300B4622RSDR DALA1166540657Fuse Pin · damagedPYLON STRUT ATTACH FUSE PIN MIDSPAR FUSE PIN REPAIRED IAW ERA 470008-14.Aug 12, 2008 · N657DL · Boeing 757232SDR 08FDEA03300Attach Fitting · corrodedCORROSION FOUND IN BOLT HOLES OF FORWARD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION FREE CONDITION. REPLACE THE TAPERED SHIM AND PROTECT RIB 8 WITH CADMIUM PLATING IAW RAS/70511822/004/2008 ISS A, APPROVED BY EAug 7, 2008 · N743FD · Airbus A300B4622RSDR 08FDEA03299Attach Fitting · corrodedCORROSION FOUND IN BOLT HOLES OF FORWARD PYLON TO ENGINE ATTACH FITTING. REPAIR PERFORMED BY REWORK OF CORROSION, NDT FOR CORROSION FREE CONDITION, AND PROTECT RIB 8 WITH CADMIUM PLATING IAW RAS/70511822/004/2008 ISS A, APPROVED BY EA 6-5451-120089.Aug 7, 2008 · N743FD · Airbus A300B4622RSDR KCSA081362Gusset · chafedNR 4 PYLON EDP PRESSURE LINE UNION FITTING CHAFING INSIDE PYLON. (A)Jul 31, 2008 · N715CK · Boeing 747209BSDR UPS08553011Support Bracket · crackedINSPECTION TYPE-C2, THE UPR CONDUIT SUPPORT BRACKET IS CRACKED IN NR2 ENG PYLON HYD BAY AT AFT OB EDGE, NAS STA 278. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-0G, DRW PL313N3033.Jul 30, 2008 · N423UP · Boeing 75724APFSDR 08FDEA03171Skin · chafedNR 2 ENGINE BEAVER TAIL LEFT SIDE SKIN IS CHAFED UNDER NR 2 AND 3 RIBS. REMOVED DAMAGE IAW DC/MD-10 SRM 54-20-00; VOL I, FIG 9. FABRICATED REPAIR IAW DC/MD-10 SRM 54-20-00; VOL I; FIG 9. INSTALLED IAW DC/MD-10 SRM 51-31-01; VOL II.Jul 30, 2008 · N372FE · Doug MD1010FSDR CA080716003Bracket · cracked(CAN) CRACK DISCOVERED DURING ENGINE VISUAL INSPECTION ON THE HIGH PRESSURE FUEL ASSEMBLY SUPPORT, CRACK ON THE TOP HOLDING HOLE, FROM HOLE TO THE EDGE OF SUPPORT.Jul 14, 2008 · Snias AS350BASDR CA080715005Bracket · cracked(CAN) DURING THE 100 HRS INSPECTION ON THE ENGINE, THE AME DISCOVERED 2 CRACKS ON THE ENGINE HIGH PRESSURE FUEL FILTER SUPPORT, 1 AT THE TOP AND 1 AT THE BOTTOM ASSEMBLY HOLDING HOLES GOING FROM EACH HOLE TO THE EDGE OF SUPPORT.Jul 11, 2008 · Snias AS350BASDR 08FDEA02655Bearing · wornNR 1 PYLON; AFT CENTER PYLON ATTACH BEARING HAS PLAY IN ALL DIRECTIONS. REMOVED AND INSTALLED A NEW BEARING ASSEMBLY REF A300-600 AMM 54-51-75-4.Jul 3, 2008 · N674FE · Airbus A300F4605RSDR 08FDEA02651Fitting · corrodedNR 2 ENGINE PYLON SPIGOT RECEPTICLE FITTING BEARING RACE CORRODED. REMOVED LEVEL 1 CORROSION, REMOVED AND REPLACED NR 2 ENGINE PYLON UPPER AND LOWER SPIGOT FITTINGS IAW FEDEX EA 6-5450-121273, RELEASE DATE 20 MAY, 2008.Jul 3, 2008 · N423FE · Airbus A310203SDR 08FDEA02650Fitting · corrodedNR 1 ENGINE PYLON SPIGOT RECEPTICLE FITTING BEARING RACE CORRODED. REMOVED LEVEL 1 CORROSION, REMOVED AND REPLACED NR 1 ENGINE PYLON UPPER AND LOWER SPIGOT FITTINGS IAW FEDEX EA 6-5450-121272, RELEASE DATE 20 MAY, 2008.Jul 3, 2008 · N423FE · Airbus A310203SDR 08FDEA02558Fitting · corrodedLT PYLON LOWER LUG FITTING, RIB 18, HAS PITTING CORROSION ON 4 FASTENER HOLES REMOVED LEVEL 1 CORROSION AND REPAIRED LT PYLON RIB 18 LUG FITTING IAW FED EX EA 6-5450-121279, RELEASE DATE 29 MAY, 2008Jun 29, 2008 · N423FE · Airbus A310203SDR 08FDEA02557Fitting · corrodedRT PYLON LOWER LUG FITTING, RIB 18, HAS 4 EA HOLES WITH CORROSION REMOVED LEVEL 1 CORROSION AND REPAIRED RIB 18 FITTING IAW FED EX EA 6-5450-121280, RELEASE DATE 29 MAY, 2008Jun 29, 2008 · N423FE · Airbus A310203SDR 08FDEA02444Attach Fitting · corrodedPYLON TO ENGINE AFT ATTACHMENT BEAM CORROSION ON MATING FACE. CLEAN THE BEAM CAREFULLY PER AMM 12-21-12. PERFORMED DVI FOR CORROSION (FOUND CORROSION). REMOVED CORROSION USING ABRASION BY HAND AS PER SRM 51-74-10,PARAGRAPH 7.B. MEASURED THE REWORKED AREA AJun 25, 2008 · N456FE · Airbus A310222SDR C8GA200800Fitting · damagedFLT 720 FROM TOL TO MCO. DURING CLIMB OPERATION OUT OF TOL THE NR 2 ENG LOW OIL PSI LIGHT ILLUMINATED AND OIL QUANTITY WENT TO EMPTY. THE NR 2 ENGINE WAS SHUT DOWN, AN EMERGENCY WAS DECLARED AND THE ACFT LANDED IN TOL WITHOUT INCIDENT. POST FLIGHT INSPECTIOJun 11, 2008 · N708AA · Boeing 727223SDR 08FDEA02211Mount · looseNR 1 PYLON LOWER AFT END (AT THE PYLON MOUNT) BRACKET IS LOOSE AND CRACKED AT THE BOTTOM, (FASTENERS ARE WORKING).Jun 10, 2008 · N357FE · Doug MD1010FSDR 2008UALA03260Fitting · crackedNR 1 PYLON "DELTA" FITTING CRACKED ON OUTBOARD SIDE. ACCOMPLISHED MAJOR REPAIR AT GSO. REPLACED DELTA FITTING PER SRM 51-40-02. LEAK CHECKED ALL LINES PER MM 29-00-98, LEAK CHECKS GOOD.Jun 6, 2008 · N544UA · Boeing 757222SDR 08FDEA02150Bracket · crackedNR 1 PYLON THRU PANEL 438 AR; STAND OFF BRACKET FOR THE FIREX LINE IS CRACKED.Jun 4, 2008 · N357FE · Doug MD1010FSDR 08FDEA02706Fitting · wornPYLON NR 2, WING/PYLON AFT ATTACH FITTING AT RIB 18 WITH PLAY AT BEARING HOUSING. THE FEDEX EA 6-5451-117329 WAS ACCOMPLISHED.May 26, 2008 · N721FD · Airbus A300B4622RSDR 08FDEA01825Attach Fitting · chafedNR 2 PYLON AFT LOWER FAIRING PANEL NR 485 AL, FWD UPPER LT ATTACH PLATE IS CHAFED ON THE INNER SURFACE. REMOVED CHAFED ATTACH PLATE & INSTALLED A NEW ATTACH PLATE PER SRM 51-40-21 PARA 6. LOCATED & DRILLED PER SRM 51-40-44. ALODINED PER AMM 51-23-10-0.May 12, 2008 · N815FD · Airbus A310324SDR 08FDEA01823Attach Angle · chafedNR 2 PYLON AFT LOWER FAIRING PANEL NR 485 AL, LT UPPER ATTACH ANGLE IS CHAFED IN SEVERAL PLACES. REMOVED DAMAGED LONGERON & INSTALLED NEW LONGERON PER SRM 51-40-21 PARA 6 - 7. LOCATED DRILLED HOLES PER SRM 51-40-44. ALODINED & PRIMED PER AMM 51-23-00.May 12, 2008 · N815FD · Airbus A310324SDR 08FDEA01820Support Bracket · crackedPYLON NUMBER TWO UPPER AFT WING TO STRUT FAIRING SUPPORT BRACKET CRACKED, ADJACENT TO PPS 174.3. EVALUATE AND RECTIFY. REPLACED PYLON NUMBER TWO UPPER AFT WING TO STRUT FAIRING SUPPORT BRACKET IN ACCORDANCE WITH EA NR F-5450-118812 AND B757-200 SRM 51-00-0May 12, 2008 · N916FD · Boeing 75727BSDR 08FDEA01539Fitting · corrodedFOUND ON PYLON NR 2 CORROSION ON PYLON TO WING SHACKLES 6/7/8 OUT OF SRM 54-51-71 LIMIT. REPAIR PERFORMED BY SMOOTH BLEND OUT THE CORROSION, NDT FOR CRACK FREE IAW RAS/AS/0037/2008 ISS A, APPROVED BY EA 6-5451-117148.Apr 25, 2008 · N745FD · Airbus A300B4622RSDR DL76L091892Attach Fitting · damagedNACELLES/PYLONS ATTACH FITTING - MIDSPAR FITTING REPAIR IAW EO 01-074944-12 ME02 C/W EO 01-074944-12 ME02. ME02 WAS NOT COMPLETED ME04 WAS COMPLETED ON 04/24/08.Apr 24, 2008 · N176DN · Boeing 767332SDR 08FDEA01525Attach Angle · crackedNR 2 PYLON ATTACH ANGLE AND RIB 3-A (OUTBD) IS CRACKED. REMOVED SHIM IAW A300-600 SRM 51-40-21 PG 7. PART IS IDENTIFIED AS A SHIM WITH A CRACK 1 INCH LONG IAW SRM 54-52-31 FIG 2 ITEM 15. FABRICATED SHIM. SHIM IS INSTALLED IAW SRM 51-40-2 PG 7.Apr 24, 2008 · N661FE · Airbus A300F4605RSDR A6WA200840370Bracket · crackedLT ENGINE INLET, QTY (2) BRACKETS CRACKED AT 4 & 5 O`CLOCK POSITION NEAR LOWER OUTBOARD T/R ACTUATOR (LOOKING AFT). QTY (2) BRACKETS AT 4 & 5 O`CLOCK POSITION NEAR THE LOWER OUTBOARD T/R ACTUATOR OF THE LT ENGINE INLET REPLACED IAW CRJ 200 SRM 51-42-06. (S)Apr 22, 2008 · N441ZW · Cndair CL6002B19SDR AALA200800895Fitting · damagedAFW - LEFT PYLON INBOARD SIDE CORE COWL HINGE FITTING AT STATION 305 FORWARD LUG HAS ELONGATED HOLE, SIZE OF DISCREPANCY IS .6932 INCH BY .6932 INCH. REPAIRED PER MRB 767 3176.Apr 9, 2008 · N335AA · Boeing 767223SDR 08FDEA01354Attach Fitting · corrodedFOUND CORROSION IN PYLON NR 2 REAR ATTACH FITTING. REPAIR PERFORMED IAW SB A300-54-6018 (REAM UP THE HOLE, CADMIUM PLATING), APPROVED BY EA 6-5451-114851.Apr 8, 2008 · N741FD · Airbus A300B4622RSDR 08FDEA01353Attach Fitting · corrodedFOUND CORROSION IN PYLON NR 1 REAR ATTACH FITTING REPAIR PERFORMED IAW SB A300-54-6018 (REAM UP THE HOLE, CADMIUM PLATING), APPROVED BY EA 6-5451-114851.Apr 8, 2008 · N741FD · Airbus A300B4622R
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