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 ABXA0100011Strap · crackedUPPER RIGHT PYLON TO FUSELAGE ATTACH ANGLE AT STATION 1095 WAS REPORTED TO BE CRACKED. MAINTENANCE REMOVED SPLICE STRAP AND DYE CHECKED THE AREA. NO CRACKS WERE NOTED IAW ABX GMM CHAPTER 3 SECTION 5.01.Jan 16, 2001 · N952AX · Doug DC941SDR AWXA0001007Fitting · gougedLEFT PYLON I/B AT FRAME TOP SURFACE AT PANEL 5735L GOUGED BEYOND LIMITS AT I/B FASTNER. BLENDED GOUGE IAW 57-20-01 AND EO 03-1754-00355; ALL FABED SHIM AND FLAP PEENED IAW SOPM 20-10-03 AWA ER 03-5754-00333-001; HFC NO CRACKS NOTED ; INSTALLED SHIM IAW 51-40-0Dec 4, 2000 · N334AW · Boeing 737300SDR UPS00434377Fitting · crackedINSPECTION TYPE:C, INSPECTION OF BATH FITTING IN NR 3 PYLON REVEALS CRACKS AT VERTICAL FASTENERS. BATH TUB FITTING REPLACED IAW SRM 51-30-02.Nov 6, 2000 · N675UP · Boeing 747123SDR DL72L001975Mount · crackedROUTINE HFEC BOLT HOLE INSPECTIONS OF THE NR 3 ENGINE PYLON FWD ENGINE MOUNT SUPPORT FITTING REVEALED A CRACK INDICATION IN HOLE G. THE CRACKING IS TYPICAL OF BAC S/B 727-54A0010AND AD 97-05-08. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK AND A .0312 INCH INSOct 10, 2000 · N507DA · Boeing 727232SDR UPS00233837Fitting · corrodedINSPECTION TYPE:C, CORROSION EVIDENT IN NR 1 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW UPS EO B727-5440-11592.Sep 25, 2000 · N922UP · Boeing 72731CSDR UPS00233830Fitting · corrodedINSPECTION TYPE:C CORROSION EVIDENT IN NR 3 PYLON, ENG FWD MOUNT FITTING HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592Sep 25, 2000 · N922UP · Boeing 72731CSDR ABXA000445Fitting · crackedPYLON BULKHEAD SUPPORT UPPER FITTING WAS CRACKED AT FLOORBEAM 965, BUTT LINE 35 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Sep 8, 2000 · N900AX · Doug DC932SDR ABXA000444Fitting · crackedPYLON BULKHEAD SUPPORT LOWER FITTING WAS CRACKED AT FLOORBEAM 965, BUTT LINE 35 RIGHT. REPLACED FITTING IAW DC9 SRM 51-30-1 AND 51-30-5.Sep 8, 2000 · N900AX · Doug DC932SDR AU001066Pin · cracked(AUS) LT ENGINE PYLON MIDSPAR INBOARD FUSE PIN CRACKED. CRACK LENGTH APPROXIMATELY 14MM (0.55IN). FOUND DURING EDDY CURRENT INSPECTION.Sep 7, 2000 · Boeing 767277SDR ABXA000436Attach Angle · crackedNR 2 ENGINE PYLON SUPPORT ANGLE CRACKED AT STA YN 156. REPAIRED CRACK IAW DC9 SRM DWG K05159.Sep 5, 2000 · N900AX · Doug DC932SDR UIEA00037Fitting · crackedDURING VISUAL INSPECTION OF NR 1 PYLON, SUPPORT FITTING (P/N 65B94161-1) AT NAC 222 WAS DISCOVERED LOOSE. FURTHER INSPECTION AND DISASSEMBLY REVEALED THE ATTACHING BOLTS ON THE UPPER AND LOWE LEFT SIDE ATTACH POINTS WRE WORN AND THE SUPPORT FITTING BUSHINGS EAug 29, 2000 · N526MC · Boeing 7472D7BSDR DL733001656Bushing · wornTHE STRUT CROWN BEAM ON THE NR 1 ENGINE PYLON WAS FOUND WITH A MIGRATED BUSHING. THE BUSHING WAS REMOVED AND WEAR DAMAGE DISCOVERED IN THE BORE. THE BORE WAS OVERSIZED TO REMOVE ALL DAMAGE AND AN OVERSIZE BUSHING INSTALLED. THE REPAIR WAS ACCOMPLISHEDAug 26, 2000 · N309WA · Boeing 737347SDR CALA0001323Angle · crackedINSPECTION FOUND FOUR INCH CRACKS IN TWO ANGLES ON I/B FAIRING OF NR 2 ENGINE UPPER T/R BUCKET. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.Aug 25, 2000 · N35832 · Doug DC982SDR CALA0001317Angle · crackedINSPECTION FOUND CRACKS IN FIRST AND THIRD ANGLES ON INBOARD T/R FAIRING ON UPPER BUCKET OF NR 1 ENGINE. THE CRACKS WERE APPROXIMATELY 3 INCHES LONG. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-30-1, 51-30-2, AND 51-10-2.Aug 25, 2000 · N35832 · Doug DC982SDR QXEA0002350Mount · chafedYXX- LEFT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. BLENDED AREA.Aug 18, 2000 · N822PH · Dhav DHC8102SDR QXEA0002351Mount · chafedYXX- RIGHT HAND MAIN LANDING GEAR RETRACT ACTUATOR MOUNT SURFACE ON NACELLE FRAME CHAFED. REPAIRED IAW DHC-8 RD 8-54-523 AND SRM 51-00-06.Aug 16, 2000 · N822PH · Dhav DHC8102SDR DL733001552Attach Fitting · corrodedREMOVAL OF A MIGRATED SPHERICAL BEARING ON THE AFT LUG FITTING OF THE NR 2 ENGINE STRUT CROWN BEAM REVEALED CORROSION IN THE LUG BORE. THE LUG BORE WAS OVERSIZED BY .10 INCHES TO REMOVE THE CORROSION, A 15-5 STEEL BUSHING INSTALLED, AND A NEW SPHERICAL BEARINAug 12, 2000 · N2310 · Boeing 737347SDR MWEA00590Attach Angle · gougedMKE - THE LOWER RIGHT INBOARD PYLON ATTACH ANGLE IS GOUGED AT STATION 990. FABRICATED AND INSTALLED DOUBLER REPAIR. (M)Aug 3, 2000 · N502ME · Doug DC932SDR MWEA00603Attach Angle · crackedMKE - RIGHT UPPER PYLON ATTACH ANGLE IS CRACKED AT THE FORWARD END. FABRICATED AND INSTALLED REPAIR DOUBLER. (M)Aug 3, 2000 · N502ME · Doug DC932SDR UPS00833603Angle · crackedINSPECTION TYPE:C123, NR 1 PYLON INTERIOR RIGHT SIDE AFT OF TOMBSTONE FITTING HAS A ANGLE CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5756791 AND SRM 51-3-0.Jul 19, 2000 · N806UP · Doug DC873FSDR RRXA10690Mount · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMANGE TO NR 3 ENGINE PYLON AFT MOUNT, DAMAGE EXCEEDED LIMITATIONS IAW DC-10 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-10 SRM 51-21-01. RECEIVED PART AND INSTALLED IAW DC-10 SRM 20-50-02. (CORROSION DAMAGE RECORDEDJul 10, 2000 · N68042 · Doug DC1010FSDR ABXA000320Attach Angle · crackedDURING C-CHECK, FOUND THE LEFT PYLON UPPER ATTACH ANGLE BETWEEN STATION 1056 AND STATION 1072 CRACKED. REPAIRED ANGLE IAW DC9 SRM 54-04.Jun 28, 2000 · N978AX · Doug DC941SDR P5CA0000216Fastener · missingNR 3 ENG STRUT TO DIAGONAL BRACE ATTACH FITTING ON FORWARD SIDE, ONE FASTENER MISSING AND SOME FOUND LOOSE. DETAILED VISUAL INSPECTION CARRIED OUT AND MISSING AND LOOSE FASTENERS REPLACED. NDT PERFORMED AND CONFIRMED NO CRACKS PER BOEING SB 747-54-2186.Jun 23, 2000 · N853FT · Boeing 747122SDR P5CA0000207Bolt · shearedON PYLONS NR 1, 3 AND 4, SHEARED .375 BOLTS ON HORIZONTAL FIRE WALL ADJACENT TO THE AFT MOUNT LUGS. BOLTS ARE VERTICAL THROUGH AFT MOUNT FITTING AND LOWER PYLON SKIRT CHORDS. REMOVED AND REPLACED ALL 8 BOLTS PER PYLON. REPLACED WITH OVERSIZED TO .4375 PER BJun 14, 2000 · N852FT · Boeing 747122SDR ABXA000311Attach Angle · crackedDURING C-CHECK, FOUND RT PYLON UPPER ATTACH ANGLE CRACKED AT STATION 996. REPAIRED IAW DC9 SRM 54-04.Jun 13, 2000 · N906AX · Doug DC931SDR CA000530007Bolt · sheared(CAN) NR 3 ENGINE PYLON TO WING ATTACH BOLT (LWR OTBD) HEAD FOUND SHEARED OFF. BOLT REPLACED.May 18, 2000 · Bag BAE146200ASDR CALA0000715Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN RT WING NR 3 PYLON PANEL NR 487DR ANGULAR BRACKET. A NEW ANGLE BRACKET WAS INSTALLED IAW SRM 51-31-01.May 18, 2000 · N68060 · Doug DC1030SDR AU000116Pin · cracked(AUS) RT ENGINE PYLON MIDSPAR FITTING INBOARD FUSE PIN CRACKEDINTERNALLY. CRACK LENGTH 19.050MM (0.75IN). FOUND DURING EDDY CURRENT INSPECTION.Apr 7, 2000 · Boeing 767204SDR ABXA000163Angle · crackedNR 1 PYLON LOWER ATTACH ANGLE CRACKED AT STATION 1066. REPAIRED ANGLE IAW DC9 SRM 54-04.Mar 23, 2000 · N969AX · Doug DC941SDR RRXA000950Hinge · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 1 PYLON TOP PLYLON CAP HINGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED HINGE FROM MS20253P2-7200 STOCK AND INSTALLED IAW DC-8 SRM 51-1-2 AFeb 24, 2000 · N994CF · Doug DC862SDR UPS00431713Bracket · damagedINSPECTION TYPE:C 44, SUPPORT BRACKET FOR CTR GUIDE FOUND DAMAGED AT BS 960, BL0. NEW SUPPORT BRACKETS FABRICATED AND INSTALLED IAW SRM 51-20-01, AND 51-30-02.Jan 3, 2000 · N674UP · Boeing 747123FSDR MALA976643Seal · failedWHILE AT LEVEL CRUISE 31,000 AP-ON A/T ON .7 MACH CREW NOTICED THRUST LEVERS 1,3,4 MOVING TOWARD IDLE, TRIED MOVING NR 2 BUT IT WAS STUCK SELECTED A/T OFF NR 2 ENGINE STILL STUCK. 91 PERCENT N1 TURNED ON NR 2 ENGINE ANTI-ICE AND AFTER 2 MINUTES, 30 SECONDS RENov 26, 1999 · N511XJ · Bac AVRO146RJ85ASDR RRXA991131Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK, NR 1 PYLON, I/B TRIPLER (ANGLE) CRACKED 1.5. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM.. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND REPLACED ANGLES IAW DC8 SRM 51-1-6 AND 51-1-7, 51-1-20D.Jun 2, 1999 · N606AL · Doug DC873FSDR 99ZZZX2221Bolt · inadequateDURING INSPECTION, NOTED THERE WAS INSUFFICIENT CLEARANCE BETWEEN THE HEAD OF THE BOLT/PIN AND RETAINER PLATE AS REQUIRED (.013 INCH - .078 INCH) IAW PSP601-2 CH 71-00-00 PG 419 PARA(26). NOTE: THIS REQUIREMENT HAS JUST BEEN INITIATED INTO THIS LAST PROVISIApr 22, 1999 · N914X · Cndair CL6002B16SDR AU991002Fuse Pin · cracked(AUS) NR 2 ENGINE STRUT INBOARD MID-SPAR FUSE PIN CRACKED. CRACK LENGTH 0.508 MM (0.020 INCH). NR 2 ENGINE OUTBOARD MID-SPAR FUSE PIN CRACKED. CRACK LENGTH 38.1 MM (1.5 INCH). FOUND DURING INSPECTION IAW QANTAS ENGINEERING INSTRUCTION EI 767-054-0026.Mar 25, 1999 · Boeing 767238SDR AU990293Pin · cracked(AUS) RIGHT INBOARD ENGINE PYLON MID-SPAR FUSE PIN CRACKED. CRACK LENGTH 11 MM (0.433 INCH). FOUND DURING EDDY CURRENT INSPECTION.Mar 24, 1999 · Boeing 767277SDR QXEA9900436Fitting · corrodedPDX - LEFT-HAND NACELLE HAS MINOR FRETTING CORROSION UNDER MAIN LANDING GEAR RETRACTION ACTUATOR ATTACHMENT FITTING. REPAIRED IAW RD 8-54-735.Feb 15, 1999 · N823PH · Dhav DHC8102SDR QXEA9900088Beam · corrodedPDX - SEVERAL SPOTS OF CORROSION ON THE FORWARD ENGINE MOUNTING BEAM. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 5A (1).Nov 28, 1998 · N492US · Fokker F28MK4000SDR QXEA9900086Beam · corrodedPDX - SURFACE CORROSION ON WEB OF AFT ENGINE MOUNTING BEAM IN RIGHT-HAND STUB WING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 5A(1).Nov 28, 1998 · N492US · Fokker F28MK4000SDR QXEA9900089Strut · corrodedPDX - NR 2 ENGINE DIAGONAL THRUST STRUT FOUND TO HAVE AREAS OF SURFACE CORROSION AND MINOR SCORING AND SCRATCHES. REPAIRED IAW FOKKER SRM 54-40-03.Nov 24, 1998 · N492US · Fokker F28MK4000SDR CA981027013Angle · cracked(CAN) DURING 100 HOUR ANNUAL INSPECTION, THE RIGHT INBOARD UPPER NACELLE AREA REVEALED SMOKING RIVETS ATTACHING STIFFENER ANGLE TO ENGINE MOUNT ATTACHMENT ASSY P/N 50-980089. CLOSER INSPECTION REVEALED APPROXIMATELY A 2 INCH CRACKING STIFFENER ANGLE. DURING Oct 20, 1998 · Beech 99ASDR AU981092Plate · cracked(AUS) RIGHT ENGINE INBOARD ENGINE MOUNT PLATE LOOSE AND RIVETS MISSING. PART TC: 9,754.Aug 10, 1998 · Piper PA31SDR SCNA98529Fitting · wornDURING HEAVY CHECK, THE LEFT WING PYLON SUPORT FITTING (FOOTSTOOL) WAS FOUND TO HAVE TWO EACH WEAR MARKS APPROXIMATELY 1.5 AND AFT OF THE LEADING EDGE AND IS 5 LONG AND APPROXIMATELY .002 DEEP. THE SECOND MARK IS AT THE AFT END OF THE HOLE RUNNING 360 DEG ARJul 18, 1998 · N152SY · Doug DC1015SDR AU980992Stiffener · cracked(AUS) ENGINE MOUNT STIFFENER LOCATED ON THE FORWARD RT SIDE CRACKED. PART TC: 7,193.Apr 28, 1998 · Bell 206B3SDR COMA9810106Fitting · wornDURING LEFT ENGINE CHANGE, FOUND THE INBOARD, FORWARD SUPPORT ROD, FORWARD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLACED INBOARD, FORWARD NACELLE SUPPORT ROD FORWARD FITTING.Apr 18, 1998 · N254CA · Emb EMB120RTSDR COMA9810105Fitting · wornDURING LEFT ENGINE CHANGE, FOUND PLAY IN ONE BEARING OF THE INBOARD NACELLE SUPPORT ROD CLUSTER FITTING. REPLACED INBOARD NACELLE SUPPORT ROD CLUSTER FITTING.Apr 18, 1998 · N254CA · Emb EMB120RTSDR COMA9810104Fitting · wornDURING LEFT ENGINE CHANGE, FOUND THE SECOND FROM AFT NACELLE SUPPORT ROD ATTACH FITTING ON THE INBOARD SIDE TO HAVE EXCESSIVE PLAY AT THE BEARING. REPLACED THE FITTING.Apr 18, 1998 · N254CA · Emb EMB120RTSDR COMA9810103Fitting · wornDURING LEFT ENGINE CHANGE, FOUND THE MOST AFT, INBOARD NACELLE SUPPORT ROD ATTACH BEARING TO HAVE EXCESSIVE PLAY. REPLACED THE FITTING.Apr 18, 1998 · N254CA · Emb EMB120RTSDR AU980821Pin · cracked(AUS) LT ENGINE MID SPAR INBOARD FUSE PIN INNER BORE CONTAINED TWO LONGITUDINAL CRACKS. TOTAL CRACK LENGTH 8.89 MM (0.35 INCHES). FOUND DURING EDDY CURRENT INSPECTION IAW ER B76-54-40-4I.Mar 6, 1998 · Boeing 767277SDR EIAA980140Fitting · corrodedDURING 'C5/D' CHECK INSPECTION, ALL PYLON WING UPPER LINK FITTING OUTER LUG FACES FOUND CORRODED. PYLON NR 1 AND NR 4, CORROSION BLENDED OUT. BUSHINGS FABRICATED AND INSTALLED IAW SB 54-2164 AND HAECO RS R57-04-33646. PYLON NR 2 AND NR 3, CORROSION BLENDED Feb 4, 1998 · N471EV · Boeing 747273C
Back to JASC 5415