JASC 5400

Service difficulty reports · 1,907

Reports filed under 5400 · Nacelle/Pylon Structure, 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 = '5400'
  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 P5CA9600321Fairing · missing tipNUMBER 3 ENGINE FORWARD FAIRING LEADING EDGE TIP IS MISSING. REPLACED MISSING TIP IAW MM 54-51-01.Jul 1, 1996 · N857FT · Boeing 747132SDR UPS96820652Drag Angle · crackedINSPECTION TYPE: C. NR 3 PYLON DRAG ANGLE HAS SHEARED FASTENER HEAD, AND CRACK INDICATIONS. REPAIRED NR 3 PYLON DRAG ANGLE FASTENER, AND CRACK INDICATIONS IAW REO 02062, REV IR.Jun 27, 1996 · N851UP · Doug DC873FSDR MALA965052Angle · damagedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND RIGHT OUTBOARD UPPER NACELLE TO WING TRANSIT ANGLE HAD FASTENER PULLING THROUGH SKIN. COMPLETED REPAIR BY FABRICATING AND WET INSTALLING REPAIR DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993 AND FAIJun 22, 1996 · N446MA · Swrngn SA227ACSDR UPS96820649Spar Cap · crackedINSPECTION TYPE: C. CRACKS IN FRONT UPPER SPAR CAP AND 508 BULKHEAD FITTING. REPAIRED FRONT UPPER SPAR CAP AND 508 BULKHEAD FITTING, NR 1 PYLON POSITION IAW TIMCO REO-02058 AND ENGINEEERING FILE DC8-57-0690.Jun 21, 1996 · N851UP · Doug DC873FSDR VTZA96227Fillet · damagedFLT NR 6193 - IAD-JFK - DURING CLIMB-OUT, RETURNED TO IAD DUE TO AN AIRFRAME/ENGINE VIBRATION FOR THE RIGHT SIDE OF THE AIRCRAFT. AIRCRAFT DECLARED AN EMERGENCY AND LANDED AT IAD WITH NO FURTHER INCIDENTS. MAINTENANCE PERFORMED AN INSPECTION AND FOUND THE RIJun 20, 1996 · N301UE · Jetair JETSTM4101SDR GLBA96135Drain Line · out of positionORD - RIGHT POWER LEVER HANGS UP DURING TAKEOFF. MAINTENANCE FOUND LOOSE DRAIN LINE CAUSING LINKAGE TO HANG-UP. SECURED LINE AND OPS GOOD. (M0Jun 14, 1996 · N267UE · Emb EMB120RTSDR MALA965030Angle · wornDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT NACELLE INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE REPAIR DOUBLER WORN. REMOVED EXISTING REPAIR AND INSTALLED NEW 6.5 INCH REPAIR DOUBLER OVER AREA IAW FAIRCHILD SRM 51-00-00 PAGE 4 PART FJun 12, 1996 · N425MA · Swrngn SA227ACSDR 96FDEA01108Cowl Web · crackedSNRM 4206, NR 2 ENG NOSE COWL CRACK AT AFT BULKHEAD AS VIEWED THROUGH ACCESS PANEL 361 KL. *S/D* REMOVED AND REPLACED WEB SECTION AS PER SRM 54-00-01.Jun 12, 1996 · N68058 · Doug DC1010FSDR AALA960887Eng Inlet · corrodedTUL - NR 2 ENGINE INLET CORRODED AT 11:00 POSITION. REMOVED CORRODED AREA AND MADE FLUSH REPAIR PER SRM 54-30-3 PAGE 2A AND 2B. (M)Jun 8, 1996 · N705AA · Boeing 727223SDR UPS96420359Repair Doubler · incorrect repairINSPECTION TYPE: C. PYLON NR 3, FOUND REPAIR DOUBLER ON NAC STA 180 LT NOT INSTALLED IAW SRM (EDGE MARGINS ON MID SPAR TOO SMALL). FOUND DURING REMOVAL OF DOUBLER THAT DOUBLER WAS MADE FROM SOFT STEEL MAT: REWORK MID SPAR STIFFENER AND REPLACED GUSSET APPRJun 4, 1996 · N682UP · Boeing 747121SDR C2XA96IA135Channel · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT MAIN LANDING INBOARD LOWER NACELLE CHANNEL DEFORMED AND CRACKED BETWEEN NACELLE FRAME 14 AND FRAME 15. MAINTENANCE REMOVED AND REPLACED NACELLE CHANNEL. (M)Jun 4, 1996 · N57734 · Emb EMB120RTSDR P5CA9600300Latch Mount · damagedFOUND NR 2 ENGINE OUTBOARD COWL NR 3 LATCH MOUNT DAMAGED. REMOVED AND REPLACED LATCH MOUNT ANGLE IAW SRM 51-30-02.Jun 2, 1996 · N853FT · Boeing 747122SDR P5CA9600298Skin · crackedFOUND NR 2 ENGINE FORWARD FAIRING HAS CRACK IN SKIN ON INBOARD SIDE. REMOVED PREVIOUS REPAIR IAW SRM 51-30-02, INSTALLED DOUBLER AND FILLER IAW SRM 51-10-01.Jun 2, 1996 · N853FT · Boeing 747122SDR MALA965036Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND LEFT INBOARD UPPER NACELLE TO WING TRANSIT ANGLE FORWARD EDGE CRACKED. COMPLETED REPAIR BY STOP DRILLING CRACK, FABRICATING AND WET INSTALLING REPAIR DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993. May 27, 1996 · N422MA · Swrngn SA227ACSDR MALA965035Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, FOUND LEFT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE FORWARD EDGE CRACKED ON PREVIOUS REPAIR. REMOVED PREVIOUS REPAIR, FABRICATED AND WET INSTALLED REPAIR DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993. WHILE COMPMay 27, 1996 · N422MA · Swrngn SA227ACSDR AALA960831Angle · corrodedTUL - CORRODED AT CENTER OF ANGLE 2 INCHES OF A 20 INCH PIECE. REMOVED AND REPLACED WTIH NEW ANGLE PER AARD 51-01-00-05, PAGE 1, PARAGRAPH 2. TST: 20,962 HOURS. CYCLES 8,396. (X)May 23, 1996 · N41063 · Airbus A300B4605RSDR 96FDEA01001Stiffener Ring · crackedSNRM 4260, CIRCUMFERENTIAL STIFFENER RING CRACKED AT THE NR 2 ENG NOSE COWL L/E AS SEEN THROUGH ACCESS PANEL 361 FL. REPLACED NOSE COWL LEADING EDGE ASSY IAW MM 54-22-01 WITH LEASED UNIT. DAMAGED NOSE COWL L/E ROUTED TO VENDOR OR SHOP FOR REPAIR (S/N 572826)May 20, 1996 · N68049 · Doug DC1010CFSDR 97ZZZX344Rib · crackedATW - NR 2 PYLON CENTER BOX BETWEEN RIBS 4 AND 5 HAS A CRACK ON THE LOWER FLANGE OF RIB NR 5 THAT IS APPROXIMATELY .4375 INCH LONG. CORRECTIVE ACTION: NR 2 PYLON RIB NR 5 CRACK HAS BEEN REPORTED TO AVRO RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC546H9018. May 18, 1996 · N293UE · Bag BAE146200ASDR 97ZZZX343Rib · crackedNR 3 PYLON CENTER BOX BETWEEN RIBS 3 AND 4 HAS A CRACK IN LOWER FLANGE OF RIB 4 THAT IS APPROXIMATELY .25 INCH LONG. CORRECTIVE ACTION: NR 3 PYLON RIB 4 LOWER FLANGE APPROXIMATELY .25 INCH CRACK HAS BEEN REPORTED TO AVRO/RDO AND IS ACCEPTABLE FOR SERVICE PERMay 16, 1996 · N293UE · Bag BAE146200ASDR 97ZZZX282Rib · crackedATW - NR 4 PYLON CENTERBOX BETWEEN RIBS 3 AND 4 HAS A CRACK IN LOWER FLANGE OF RIB 4 THAT IS APPROXIMATELY .3125 INCH LONG HAS BEEN REPORTED TO AVRO BAE RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC546H9018. GENERATED W/C FOR REINSP.May 16, 1996 · N293UE · Bag BAE146200ASDR 97ZZZX280Rib · crackedATW - NR 2 PYLON CENTER BOX BETWEEN RIBS 3 AND 4 HAS A CRACK ON THE LOWER FLANGE OF RIB NR 4 THAT IS APPROXIMATELY .4375 INCH LONG. CORRECTIVE ACTION: NR 2 PYLON RIB NR 4 CRACK HAS BEEN REPORTED TO AVRO RDO AND IS ACCEPTABLE FOR SERVICE PER RIL HC546H9018. May 16, 1996 · N293UE · Bag BAE146200ASDR 96FDEA00975Spar Chord · shearedSNRM 4358, NR 3 PYLON UPPER LT SPAR CHORD AFT AREA EXHIBITS TWO SHEARED HOCK BOLTS HEADS INSIDE PYLON.May 15, 1996 · N304FE · Doug DC1030FSDR 96FDEA00974Spar Chord · shearedSNRM 4145, NR 1 PYLON UPPER SPAR WEB STA 363, 1 FASTENER HEAD HAS SHEARED OFF.May 15, 1996 · N304FE · Doug DC1030FSDR DHL9670917CStrap · corrosionAT C-CHECK, FOUND NR 2 ENGINE INLET S-DUCT HAS CORROSION ON REINFORCEMENT STRAP AT STA 1203 AT 12 O'CLOCK POSITION. INSTALLED S/S REPLACEMENT STRAP PER AVITAS EO 96PMSI-123RO-6.May 12, 1996 · N709DH · Boeing 72782CSDR 96FDEA00941Thrust Link · looseSNRM 4361, NR 3 PYLON FWD ENG MOUNT AREA LOWER THRUST LINK LT SIDE OF PYLON HORIZONTAL ROW OF .3125 BOLTS ARE LOOSE, AS VIEWED FWD LOWER LT SIDE OF PYLON AT APPROX YN222 TO 226, 3 BOLTS LOOSE. *S/D* REPLACED NUTS WITH NEW AND RETORQUED PER EO 8-5410-7-4319.May 9, 1996 · N304FE · Doug DC1030FSDR 96FDEA00940Thrust Link · looseSNRM 4360, NR 3 PYLON FWD ENG MOUNT, LWR THRUST LINK RT SIDE OF PYLON HAS VERTICAL ROW OF .25 BOLTS AND HORIZONTAL ROW OF .3125 IN BOLTS LOOSE, TOTAL OF 18 BOLTS LOOSE AT APPROX PYLON STA YN 222 TO 226. *S/D* REPLACED NUTS WITH NEW AND RETORQUED PER EO 8-541May 9, 1996 · N304FE · Doug DC1030FSDR 96FDEA00939Thrust Links · looseSNRM 4359, NR 3 PYLON FWD ENG MOUNT LOWER THRUST LINKS, 7 MOUNTING BOLTS ARE LOOSE ON PYLON BOTTOM LT AND RT SIDES APPROXIMATE PYLON STA YN 222. *S/D* RT SIDE TORQUED PER MM 20-50-02, REMOVED AND REPLACED NUTS ON BOTTOM OF FWD THRUST LINK LT AND RT AND RETORMay 9, 1996 · N304FE · Doug DC1030FSDR 96FDEA00938Fasteners · looseSNRM 4353, NR 3 PYLON INSIDE ACCESS PANEL 488 BL PYLON FWD BULKHEAD AT STA YN 342, BOTTOM ROW OF FASTENERS ARE ALL LOOSE.May 9, 1996 · N304FE · Doug DC1030SDR 96FDEA00935Screws · looseSNRM 4342, NR 3 PYLON HAD 8 TRI-WING SCREWS LOOSE ON PYLON AFT MOUNT BULKHEAD, STA YN420 RT SIDE OF PYLON.May 9, 1996 · N304FE · Doug DC1030FSDR 96FDEA00934Screws · looseSNRM 4343, NR 3 PYLON HAD 5 TRI-WING SCREWS LOOSE ON LT SIDE OF PYLON AT AFT MOUNT BULKHEAD, STA YN 420.May 9, 1996 · N304FE · Doug DC1030FSDR 96FDEA00933Bolt · shearedSNRM 4126. NR 1 PYLON FORWARD ENGINE MOUNT TRUSS FITTINGS HAVE NUMEROUS LOOSE BOLTS AT BOTTOM, TOP, AND SIDES. APPROXIMATELY 50 PERCENT OF THE FASTENERS ARE LOOSE. ONE BOLT IN THE BOTTOM RIGHT IS SHEARED. YN222 STA. S/D: TORQUED BOLTS PER E.O. 8-5410-7-4May 9, 1996 · N304FE · Doug DC1030FSDR 96FDEA00968Bolt · shear offDURING ACCOMPLISHMENT OF EO 8-5410-7-3321 PART 1, FOUND FLATHEAD BOLT SHEAR OFF ON NR 1 PYLON AFT SUPPORT BULKHEAD.May 7, 1996 · N304FE · Doug DC1030SDR UPS96820072Wing Slot · crackedINSPECTION TYPE 'C', 32 PYLON STUB WING SLOT SECTION O/B END HAS SEVERAL CRACKS INSIDE OF AREA. STOP DRILLED CRACKS AND INSTALLED FILLER AND DOUBLER IAW UPS EO DC8-57 -0667.May 4, 1996 · N805UP · Doug DC873FSDR UPS96820070Slot Section · crackedINSPECTION TYPE 'C', NR 3 PYLON STUB WING SLOT SECTION OUTER I/B END HAS CRACKS. FAB REPAIR FILLER AND DOUBLERS, ALODINED, PRIMED AND INSTALLED IAW TIMCO REO 01915 AND UPS EO DC8-57-0668.May 4, 1996 · N805UP · Doug DC873FSDR DHL9670904CSkin · corrodedAT C-CHECK, FOUND S-DUCT HAS CORROSION AROUND FASTENERS AND SKIN BULGE AT 12 O'CLOCK POSITION, 24 FWD OF PRODUCTION BREAK. CUT OUT DAMAGED AREA, INSTALLED DOUBLER 8.5 BY 9.5 PER SRM 54-10-3.May 2, 1996 · N709DH · Boeing 72782CSDR DL72S961034Seal Striker · crackedFOUND ON C-2 LETTER CHECK, SEAL STRIKER FOR L/E OF RT FORWARD COWLS DAMAGED AT 3.00 AND 9.00 POSITIONS. REPAIRED PER M/M 53-11-0, PAGE 801.Apr 30, 1996 · N469DA · Boeing 727232SDR C2XA96IA112Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT ENGINE NACELLE FRAME 2 TO NACELLE PAN ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. ACFT TT: 14,059.3 HRS. CYCLES, 18,999. (X)Apr 30, 1996 · N27716 · Emb EMB120RTSDR C2XA96IA104Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME 2 ANGLE WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE AND THE AIRCRAFT WAS RETURNED TO SERVICE. AIRCRAFT TT: 14,059.3 HRS. CYCLES, 18,999. (X)Apr 30, 1996 · N27716 · Emb EMB120RTSDR 96ZZZX2732Thrust Link · damagedNR 1 PYLON THRUST LINK, LOWER FORWARD FLANGE, IS GOUGED. REMOVED AND REPLACED THRUST LINK IAW SB 54-92-00 AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862SDR 96ZZZX2706Thrust Link · chafedNR 4 ENGINE PYLON THRUST LINK CHAFED. REMOVED AND REPLACED THRUST LINK IAW SB 54-92-00, SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862SDR 96ZZZX2683Brace · damagedDURING C-CHECK, FOUND NR 2 INBOARD PYLON SIDE, BRACE DAMAGED AND GOUGED. REMOVED AND REPLACED NEW THRUST LINK BRACE IAW SB 54-90-00 AND SRM 51-1-20D.Apr 26, 1996 · N8969U · Doug DC862SDR UIEA960513j55200 · s-ductATB FLT NR GTI127/ORD/TRN, AFTER TAKEOFF NR 1 ENGINE HAD A FIRE WARNING FOLLOWING INDICATIONS WERE OBSERVED, FIRE WARNING LIGHT AND HIGH NACELLE TRMP (ABCLAMPOVE 9.0) ALSO GOT START VALVE OPEN LIGHT. AFTER ENGINE SHUTDOWN GOT OIL FILTER BYPASS LIGHT. DUMPED Apr 25, 1996 · N640FE · Boeing 747245FSDR MALA964955Angle · broken rivetDURING AN INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED LOWER RIGHT OUTBOARD WING TO NACELLE TRANSIT ANGLE HAS A RIVET HEAD BROKEN HALF OFF AND A .125 INCH CRACK EMANATING FROM RIVET. LOCATION IS 9 RIVETS AFT OF DE-ICE BOOT EDGE. COMPLETED REPAIR BY REMOVINApr 17, 1996 · N60NE · Swrngn SA227ACSDR IXXA9658Rib · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 2 PYLON STUB WING UPPER CENTER RIB WAS FOUND CRACKED. REPAIR TO THE RIB WAS ACCOMPLISHED BY FABRICATING AND INSTALLING REPAIR DOUBLER AND ANGLE IAW THE AIRCRAFT SRM 57-2-0 AND SRM 51-1-20D. (X)Apr 16, 1996 · N728PL · Doug DC862SDR IXXA9657Rib · crackedDURING ROUTINE C-CHECK INSPECTION, THE NR 2 PYLON STUB WING, INBOARD RIB, FORWARD SECTION, WAS FOUND WITH 2 CRACKS. THE RIB ASSEMBLY WAS REMOVED AND REPLACED IAW THE AIRCRAFT SRM 51-2-0. (X)Apr 16, 1996 · N728PL · Doug DC862SDR DL72S960882Skin · crackedFOUND ON B-1 LETTER CHECK, THREE .5 INCH CRACKS EXTENDING FROM FASTENERS FWD OF PANEL 9501 RT SIDE AND TWO .5 INCH CRACKS EXTENDING FROM FASTENERS BELOW PANEL 9501 RT SIDE. REPAIRED PER M/M 54-30-0 PG 801 AND 802.Apr 16, 1996 · N485DA · Boeing 727232SDR SCNA96092Cowl Rivets · looseDURING HEAVY MAINTENANCE VISIT, LOOSE AND WORKING RIVETS WERE FOUND AT SEVERAL LOCATIONS NEAR THE NR 2 RIGHT FORWARD COWL, LATCH POSITIONS ABOVE THE CUTOUT, BS 1333 TO 1343 AND BS 1363 TO 1383. FABRICATED FILLER DOUBLER AND SPLICE, INSTALLED IN ACCORDANCE WITApr 14, 1996 · N284SC · Boeing 7272J4SDR UPS96805981Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT STUB WING AT NR 2 PYLON RIB CRACKED ON UPPER SIDE APPROX AT STA XRS 440. STOP DRILLED CRACK, FAB REPAIR DOUBLERS AND INSTALLED IAW DC8-SRM 57-2-0 AND 57-3-0.Apr 12, 1996 · N803UP · Doug DC873FSDR DL72S960848Skin · crackedA 1 INCH CRACK IN NR 2 ENG INLET OUTER SKIN LT SIDE 8 O'CLOCK POSITION APPROX 36 INCHES AFT OF L/E. INSTALLED DOUBLER PER SRM 55-30-0.Apr 12, 1996 · N533DA · Boeing 727232SDR DL72W960808S-Duct Skin · crackedFOUND ON MV1 CHECK, TIME LIMITED REPAIR INSTALLED, 1 INCH CRACK IN S-DUCT HOUSING RT SIDE JUST FWD OF SADDLE PANEL, VERT STAB FRONT SPAR. INSTALLED PERMANENT REPAIR PER M/M 54-30-0 PG 801 FIG 802.Apr 8, 1996 · N2810W · Boeing 727247
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