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 WRLA98070Ring · bentNR 2 ENGINE BELLMOUTH RING DAMAGED DURING 'TAIL STRIKE' ACCIDENT. BELLMOUTH RING REPAIRED BY DOUGLAS AIRCRAFT COMPANY PER ROHR ROD SKETCH PWRS065, REV 2. (M)Jan 13, 1998 · N275WA · Doug MD11SDR 98ZZZX877Web · corrodedDURING ANNUAL INSPECTION, FOUND LOWER AREA OF NACELLE WEB IN EXHAUST TUNNEL EXFOLIATED. ONLY ONE OF THE TUNNELS ON THIS AIRCRAFT WAS CORRODED, BUT SKIN CRACKS WERE FOUND IN AREA OF EXHAUST CLAMP ON ONE OTHER TUNNEL. ACTT: 3,998.1 HOURS.Jan 12, 1998 · N2699D · Cessna 340ASDR 98ZZZX2743Bracket · crackedATW - NR 3 ENGINE SHOULDER COWL - TERMINAL BOARD SUPPORT BRACKET FORWARD, CRACKED. REPLACED NR 3 ENGINE FORWARD TERMINAL BOARD SUPPORT BRACKET ON SHOULDER COWL.Jan 6, 1998 · N156TR · Bag BAE146200ASDR 97FDEA00905Fitting · crackedNR 3 PYLON TRUSS FITTING OUTBOARD HALF HAS CRACK INDICATION UPPER AFT HOLE AT FORWARD END OF FITTING. CRACK INDICATION AT 6 O'CLOCK POSITION IN HOLE. REF EO 8-5410-7-3323. *S/D* CLEANED HOLE PER SRM 54-10-01 ET. INSPECTED (AFTER) CLEANING. NO CRACK INDIDec 30, 1997 · Doug DC1010SDR DL72S980029Skin · crackedS-DUCT INTERIOR SKIN CRACKED AND BENT UPWARD FROM 10 O'CLOCK TO 1 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF SKIN. FAB REPAIR DOUBLER AND FILLER PER ERA 331180-14. INSTALLED DOUBLER PER ERA 331180. INSTALLED TAPERED SHIM AND CLOSED OUTER SKIN PER ERA 331Dec 22, 1997 · N403DA · Boeing 727232SDR ABXA9702008Angle · crackedDURING MOD/D-CHECK, FOUND THE LT PYLON INTERIOR OUTBD AFT ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-2, 51-30-5, AND DACO DWG 9958221.Dec 22, 1997 · N959AX · Doug DC941SDR ABXA9702007Web · crackedDURING MOD/D-CHECK, FOUND THE LT PYLON INTERIOR OUTBD AFT WEB CRACKED. REPLACED WEB IAW DC9 SRM 51-30-2, 51-30-5, AND DACO DWG 9958221.Dec 22, 1997 · N959AX · Doug DC941SDR ABXA9701948Intercostal · crackedDURING C-CHECK, FOUND THE INTERCOSTAL WEB ON NR 1 ENGINE PYLON CRACKED BELOW THE ENGINE WIRE BUNDLES AND BLEED AIR DUCT. REPAIRED THE WEB IAW DC9 SSRM DWG K05159.Dec 9, 1997 · N948AX · Doug DC931SDR ABXA9701947Angle · crackedDURING C-CHECK, FOUND THE INTERCOSTAL ANGLE ON NR 1 PYLON CRACKED BELOW THE ENGINE WIRE BUNDLES AND BLEED AIR DUCT. REPLACED ANGLE IAW DACO DWG 9958193.Dec 9, 1997 · N948AX · Doug DC931SDR QXEA9700888Blow Out Door · openSEA - AIRCRAFT DIVERTED TO PDX AFTER CREW REPORTED MODERATE VIBRATION THAT OCCURED ALL OF A SUDDEN IN CRUISE. FOUND NR 2 STUB WING BLOW OUT DOOR OPEN. OPERATIONAL CHECK DOOR TENSION AND BLED AIR SYSTEM FOR LEAKS. NO DEFECTS FOUND. NO PARTS REPLACED, OPERATDec 8, 1997 · N483US · Fokker F28MK4000SDR P5CA9701850Brace · chafedCHAFING DAMAGE ON NR 1 PYLON DIAGONAL BRACE FORWARD END LOWER SIDE CAUSED BY HYD DOOR FORWARD LATCH CLEARANCE. REPAIRED PER SRM 51-10-01.Dec 4, 1997 · N921FT · Boeing 747283BSDR TWRA97203Structure · crackedON A2 SVC, FOUND SEVERAL CRACKS IN NR 3 PYLON, NAC STATION 219 STRINGER ABOVE PANEL 473CL, APPROX 1 INCH CRACK IN STRINGER HORIZ FLANGE. RIGHT FRAME AT NAC 269 1 INCH CRACK OUT OF BRACKED RIVET HOLE APPROX 20 INCHES FROM BOTTOM OF PYLON. INBOARD SIDE, SIDE EXDec 2, 1997 · N617FF · Boeing 747121SDR CALA9701696Web · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 3 PYLON UPPER SPAR WEB UNDER ENGINE FUEL AND HYDRAULIC LINES AT STA YN222. REPAIRED IAW ECRA 5410-01465.Dec 1, 1997 · Doug DC1030SDR UPS97825276Pylon · crackedINSPECTION TYPE-C/CK, REPAIR CRACKED NR 4 PYLON STUB WING PER EO UPS DC8 5720 9700 A AND OPS 295. FABRICATED REPAIR PER DAC DWG SRO 8570014 AND UPS REO DC8 5720 970D. INSTALLED PER DAC DWG SRO 8570014 AND UPS REO DC8 5720 970D.Nov 19, 1997 · N718UP · Doug DC871FSDR ABXA9701889Cap · crackedNR 2 PYLON CAP IS CRACKED AT SCREW HOLE, OUTBOARD UPPER SIDE, JUST FWD OF TOMBSTONE FITTING. REPAIRED IAW SRM 54-2-2.Nov 14, 1997 · N808AX · Doug DC862SDR ABXA9701800Rear Spar · crackedDURING C-CHECK, FOUND THE RT PYLON UPPER REAR SPAR IN THE AFT ACCESSORY COMPARTMENT CRACKED. REPAIRED REAR SPAR ANGLE IAW ABX REA D953-21647.Nov 10, 1997 · N941AX · Doug DC932SDR SIMA973082Brackets · chafedSAW - DURING MBV-2 INSPECTION MAINTENANCE, THE UPPER AFT ENGINE PANEL AFT BRACKETS CHAFING THE NR 4 AND NR 5 UPPER ZEE MOUNT TUBES ON THE NR 1 AND NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED THE ZEE MOUNT TUBES IAW JIC 54-21-61. MAINTENANCE REMOVED AND REPNov 4, 1997 · N246AE · Aerosp ATR42300SDR P5CA9701820Doubler · crackedCRACKED DOUBLER NR 3 PYLON I/B SIDE AFT OF AFT MOUNT. REPAIRED PER POLAR MA 5430-07:01.Nov 4, 1997 · N858FT · Boeing 747123SDR ABXA9701782Angle · crackedDURING C-CHECK, FOUND THE LT PYLON INTERIOR LOWER OUTBOARD SPLICE ANGLE AT BOTTOM OF ENGINE MOUNT BOLT CRACKED. REPLACED ANGLE IAW DC9 SRM 51-30-5 AND MM 20-16-00.Nov 4, 1997 · N941AX · Doug DC931SDR 97ZZZM1151Brackets · chafedSAW - DURING MBV-2 INSPECTION MAINTENANCE, THE UPPER AFT ENGINE PANEL AFT BRACKETS CHAFING THE NR 4 AND NR 5 UPPER ZEE MOUNT TUBES ON THE NR 1 AND NR 2 ENGINE. MAINTENANCE REMOVED AND REPLACED THE ZEE MOUNT TUBES IAW JIC 54-21-61. MAINTENANCE REMOVED AND REPNov 4, 1997 · N246AE · Aerosp ATR42300SDR 98ZZZM368Rib · crackedIN PYLON NR 4 RIB NR 5 IS CRACKED IN THE LOWER FLANGE RADIUS NEAR THE PYLON CENTERLINE. VIEW THROUGH ACCESS PANEL NR 482CL, .250 INCH LONG. REF RIL HC546H9018 .25 INCH CRACK REPORTED RIB 5 NR 4 PYLON MAY REMAIN IN SERVICE GENERATED W/C FOR REINSPECTION. (M)Nov 3, 1997 · N616AW · Bag BAE146300ASDR 9721436627Web · crackedDURING PERIODIC CHECK, FOUND A CRACK ON THE MID SPAR WEB OF THE NR 2 PYLON AT AFT INBOARD CORNER, FOUR INCHES FORWARD OF TORQUE BULKHEAD. REPAIRED PER EA 66-152600.Nov 1, 1997 · N627US · Boeing 747251BSDR CALA9701525Fasteners · shearedINSPECTION FOUND SIX FASTENER HEADS SHEARED AT LOWER AFT FACE OF NR 4 BANJO FITTING, NR 2 PYLON. THE FASTENERS WERE REMOVED AND REPLACED WITH NEW FASTENERS IAW SRM 51-42-00.Oct 30, 1997 · N12064 · Doug DC1030SDR SIMA972991Rod · chafedDURING MBV-2 INSPECTION MAINTENANCE DISCOVERED, THE AFT BRACKET ON THE UPPER AFT ENGINE PANEL (485AT) WAS CHAFFING THE NR 4 AND NR 5 ZEE MOUNT TUBES IAW JIC 54-21-61. MAINTENANCE REMOVED AND REPLACED BRACKET IAW EO E9-5300-0111. AIRCRAFT WAS RETURNED TO SERVOct 26, 1997 · N233RM · Aerosp ATR42300SDR 97ZZZM1163Bracket · chafedDURING MBV-2 INSPECTION MAINTENANCE DISCOVERED, THE AFT BRACKET ON THE UPPER AFT ENGINE PANEL (485AT) WAS CHAFFING THE NR 4 AND NR 5 ZEE MOUNT TUBES IAW JIC 54-21-61. MAINTENANCE REMOVED AND REPLACED BRACKET IAW EO E9-5300-0111. AIRCRAFT WAS RETURNED TO SERVOct 26, 1997 · N233RM · Aerosp ATR42300SDR 97ZZZM1162Rod · chafedDURING MBV-2 INSPECTION MAINTENANCE DISCOVERED, THE AFT BRACKET ON THE UPPER AFT ENGINE PANEL (485AT) WAS CHAFFING THE NR 4 AND NR 5 ZEE MOUNT TUBES IAW JIC 54-21-61. MAINTENANCE REMOVED AND REPLACED BRACKET IAW EO E9-5300-0111. AIRCRAFT WAS RETURNED TO SERVOct 26, 1997 · N233RM · Aerosp ATR42300SDR UPS97824904Rib · crackedINSPECTION TYPE-C, RT STUB WING NR 3 PYLON RIB CRACKED. REPAIRED IAW SRM 57-2-0.Oct 22, 1997 · N801UP · Doug DC873FSDR ABXA9701704Angle · crackedDURING C-CHECK, FOUND THE RIGHT PYLON UPPER ATTACH ANGLE WAS CRACKED. REPAIRED IAW DC-9 SRM 54-04.Oct 21, 1997 · N936AX · Doug DC931SDR MWEA97805Fitting · crackedDURING C-CHECK, FOUND CRACK ON LEFT PYLON AFT UPPER SPAR TO FUSELAGE CLIP. MTC REMOVED AND REPLACED FITTING IAW DAC DRAWING 4919864 SRM 51-10-4 AND SRM 51-30-5.Oct 20, 1997 · N602ME · Doug DC932SDR 97FDEA00763Bolt · shearedNR 1 PYLON INSIDE ACCESS PANEL 438HL STA YN 342, BULKHEAD TO UPPER SPAR WEB FWD END 1 ATTACH BOLT HAS SHEARED AND SEVERAL OTHER BOLTS ARE LOOSE. *S/D* HFEC INSPECTED AREA OF SHEARED AND LOOSE FASTNERS, NO CRACK INDICATIONS NOTED. INSTALLED NEW BOLT PER M/Oct 20, 1997 · N601FE · Doug MD11FSDR 97FDEA00762Bolt · shearedNR 3 PYLON INSIDE ACCESS PANEL 488HL BS YN 342, BULKHEAD TO UPPER SPAR WEB FWD END 3 ATTACH BOLTS HAVE SHEARED AND THE OTHERS ARE LOOSE. * S/D* HFEC BOLT HOLES NO CRACK INDICATIONS NOTED. INSTALLED AND TORQUED NEW BOLTS PER M/M 20-50-02. RETORQUED REMAIOct 20, 1997 · N601FE · Doug MD11FSDR P5CA9701781Fasteners · looseMISSING FASTENERS ON NR 2 PYLON AFT INBD SKIRT. REPAIRED PER SRM 51-30-02.Oct 19, 1997 · N854FT · Boeing 747122SDR P5CA9701769Jamb Nut · looseLOOSE RETURN LINE NR 3 PYLON JAM NUT HOLE ELONGATED. REPAIRED PER SRM 51-10-03.Oct 19, 1997 · N854FT · Boeing 747122SDR DL757972199Drag Strut · brokenPYLON NR 2 ENGINE DIAGONAL DRAG BRACE. REPAIR FOR SEVERED LUG. THE DIAGONAL DRAG BRACE ON THE NR 2 ENGINE WAS FOUND WITH A SEVERED LUG. THE DRAG BRACE WAS REPLACED AND THE PYLON INSPECTED PER ER/A373001-14.Oct 17, 1997 · N620DL · Boeing 757232SDR DL72S972072Web · crackedFOUND ON F2 LETTER CK, .75 INCH CRACK LOWER RT CORNER OF WEB STA 1303 ABOVE NR 2 ENGINE S-DUCT. REPAIRED PER SRM 53-10-4.Oct 16, 1997 · N524DA · Boeing 727232SDR P5CA9701751Slot Seal · damagedELONGATED ALIGNMENT HOLE, NR 1 ENG OUTBD SLOT SEAL ASSY. REMOVED AND REPLACED PER 51-30-02 DOUBLER.Oct 13, 1997 · N851FT · Boeing 747122SDR P5CA9701748Fasteners · missingLOOSE/MISSING FASTENERS NR 1 PYLON INBD SLOT SEAL AREA. REMOVED AND REPLACED SRN 51-30-02.Oct 13, 1997 · N851FT · Boeing 747122SDR P5CA9701745Fasteners · missingMISSING FASTENERS .25 INCH CRACK, NR 3 PYLON INBD SLOT SEAL AREA. REMOVED AND REPLACED PER SRM 51-30-02.Oct 13, 1997 · N851FT · Boeing 747122SDR P5CA9701744Fasteners · looseLOOSE FASTENERS NR 3 PYLON OUTBD ABOVE SLEEVE. REMOVED AND REPLACED PER SRM 51-30-02.Oct 13, 1997 · N851FT · Boeing 747122SDR P5CA9701730Fasteners · looseLOOSE FASTENERS, NR 2 ENGING PYLON UPPER OUTBD AFT EXTERNAL. REMOVED AND REPLACED PER SRM 51-30-02.Oct 13, 1997 · N851FT · Boeing 747122SDR P5CA9701729Fasteners · missingMISSING FASTENERS ON NR 2 PYLON INBD AFT SMALL FAIRING. REMOVED AND REPLACED PER SRM 51-30-02.Oct 13, 1997 · N851FT · Boeing 747122SDR P5CA9701728Rivets · looseWORKING RIVETS OTBD LWR AFT PANEL NR 2 PYLON. REMOVED AND REPLACED PER SRM 51-30-02.Oct 13, 1997 · N851FT · Boeing 747122SDR ABXA9701598Angle · crackedNR 4 PYLON UPPER SPAR LATERAL STIFFENER IS CRACKED. INSTALLED REPLACEMENT ATTACH ANGLE IAW DC8 SRM 54-2-1.Oct 10, 1997 · N843AX · Doug DC861SDR P5CA9701681Clip · crackedCRACK ON NR 3 PYLON UPPER CLIP NEAR WING LEADING EDGE. FABRICATED AND INSTALLED CLIP PER BOEING SRM 51-30-02.Oct 9, 1997 · N850FT · Boeing 747122SDR ABXA9701636Doubler · crackedNR 4 PYLON OUTBOARD SIDE 24 FWD OF WING L/E AT TOP, SKIN HAS TWO LARGE CRACKS AROUND ACCESS PANEL LAND. REMOVED CRACKED OTBD DOUBLER, FABRICATED REPLACEMENT DOUBLER IAW DWG 5765901 AND INSTALLED IAW SRM 51-1-21, 51-1-20D, 51-3-8 AND 51-1-11.Oct 6, 1997 · N843AX · Doug DC861SDR ABXA9701635Web · crackedNR 4 PYLON INBOARD LOWER CHORD CRACKED AT STA YOP 234. REPAIRED NR 4 PYLON INBD LOWER CHORD AT STA YOP 234 IAW ABX REA NO D854-20847MR.Oct 6, 1997 · N843AX · Doug DC861SDR P5CA9701597Clips · crackedCRACKED SUPPORT CLIPS ON FORWARD AND AFT INNER WEB ON NR 1 PYLON. FABRICATED AND INSTALLED REPLACEMENT CLIPS PER BAC SRM 51-30-01 AND 51-30-03.Sep 28, 1997 · N858FT · Boeing 747123SDR EISA97202Stiffener · crackedRIGHT PYLON VERTICAL STIFFENER CRACKED THROUGH AT BOTTOM HOLE. REMOVED STIFFENER AND FABRICATED NEW. INSTALLED PER SRM 55-30-04. TT, 55,940:30 HOURS. TC: 32,713. (X)Sep 22, 1997 · N15DF · Boeing 727264SDR 98ZZZM72Rivet · shearedRIVET HEAD SHEARING TOP SIDE OF RIB LE ABOVE NR 3 PYLON MARKED. REPLACED RIVET.Sep 17, 1997 · N615AW · Bag BAE146300ASDR P5CA9701584Clip · crackedCRACKED ATTACH CLIP FORWARD OF DIAGONAL LINK ON NR 2 PYLON. REPLACED DAMAGED ATTACH CLIP PER BAC SRM 51-10-01.Sep 15, 1997 · N856FT · Boeing 747132
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