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 C2XA96IA006Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT ENGINE NACELLE FRAME 2 ATTACH ANGLE INBOARD SIDE CRACKED AT RIVETS. MAINTENANCE REMOVED AND REPLACED ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Dec 24, 1995 · N31711 · Emb EMB120RTSDR C2XA96IA005Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME 2 ATTACH ANGLE CRACKED ON OUTBOARD END. MAINTENANCE REMOVED AND REPLACED THE ATTACH ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Dec 24, 1995 · N31711 · Emb EMB120RTSDR C2XA95IA397Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME, NR 2 UPPER ANGLE, CRACKED AT FASTENER LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1995 · N16729 · Emb EMB120RTSDR C2XA95IA396Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE NACELLE FRAME, NR 2 UPPER ANGLE, CRACKED AT FASTENER LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1995 · N16724 · Emb EMB120RTSDR C2XA95IA395Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT ENGINE NACELLE FRAME NR 2 UPPER ANGLE CRACKED AT FASTENER LOCATIONS. MAINTENANCE REMOVED AND REPLACED THE ANGLE. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Dec 18, 1995 · N16724 · Emb EMB120RTSDR AALA952068Lug · corrodedTUL - CORROSION IN BORE OF LUG OF PYLON. LUG BORED AND RE-BUSHED ON SHOP HAND-WRITE C8HF. CORROSION REMOVED. TST, 21,241.75 HOURS. CYCLES, 8,851. (X)Dec 11, 1995 · N91050 · Airbus A300B4605RSDR P2RA950043Rib · crackedPHX - DURING B-CHECK, NR 2 ENGINE PYLON AFT FAIRING SUPPORT STRUCTURES INNER RIB CRACKED ENTIRE LENGTH OF THE RIB. REPAIRED PANEL RIB PER SRM 54-50-00 AND 51-30-2. (M)Dec 9, 1995 · N14977 · Airbus A300B4203SDR USAA951250Angle · crackedPIT - DURING C-3 CHECK INSPECTION, FOUND 1.50 INCH CRACK TOP DRAG ANGLE OF PYLON AT STA 980. INSTALLED DOUBLER REPAIR PER SRM 53-04, FIGURE 10, AND USAIR EA NR 31737. (X)Dec 8, 1995 · N973VJ · Doug DC931SDR MWEA95472Bracket · crackedDURING D-CHECK, FOUND AN ATTACH BRACKET CRACKED AT STA 1038 IN THE PYLON UPPER INBOARD CORNER. FABRICATED A NEW BRACKET IAW DAC DWG 4919864 AND INSTALLED IAW THE SRM 51-30.Dec 8, 1995 · N401ME · Doug DC932SDR MWEA95471Bracket · crackedDURING D-CHECK, FOUND AN ATTACH BRACKET CRACKED AT STA 1038 IN THE LT PYLON UPPER INBOARD CORNER. FABRICATED A NEW BRACKET IAW DAC DWG 4919864 AND INSTALLED IAW THE SRM 51-30.Dec 8, 1995 · N401ME · Doug DC932SDR 9520926633Spar Web · crackedDURING PCK, FOUND A CRACK IN THE NR 3 PYLON MID-SPAR WEB, STATION 301. REPAIRED WEB (P/N 65B90421) PER EA 66-104418.Dec 8, 1995 · N633US · Boeing 747227BSDR ABXA9600031Tee Doubler · crackedDURING 826AX MOD, DISCOVERED NR 1 PYLON TEE DOUBLER LEAKS FUEL. REPAIRED NR 1 TEE DOUBLER THAT WAS CRACKED IAW ABX REA D854-13070MR.Dec 5, 1995 · N826AX · Doug DC863SDR C2XA95IA364Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT ANGLE REF.EMB FAX EST435/95. (M)Dec 4, 1995 · N16702 · Emb EMB120RTSDR MALA954727Bypass Door · will not openFLT NR 3094 - EN ROUTE FROM MSP-BMI - THE NR 1 ENGINE INTAKE BYPASS DOOR WOULD NOT OPEN. DUE TO EN ROUTE WEATHER, THE AIRCRAFT RETURNED TO MSP. MAINTENANCE PERSONNEL DEFERRED THE SYSTEM UNDER MEL 71-1 AND THE AIRCRAFT WAS RETURNED TO SERVICE. ALL SYSTEMS OPNov 27, 1995 · N833MA · Dhav DHC8102SDR DL72S954698Angle · damagedUPON HMV, FOUND NR 2 ENG PYLON CIRCUMFERENTIAL ANGLE FOR MOUNTING SURFACE OF FWD COWL HAS TEMPORARY REPAIR INSTALLED. FABRICATED AND INSTALLED NEW ANGLE PER MM 53-11-0.Nov 23, 1995 · N496DA · Boeing 727232SDR AALA951992Rib · crackedTUL - FOUND VERTICLE STRUCTURE RIB CRACKED APPROXIMATELY 1 INCH FROM FORWARD EDGE AFT, NEAR TOP OF RIB. STOP DRILLED CRACK. INSTALLED DOUBLER REPAIR PER SRM 51-70-07-R1, PG 201, 202 AND 203. (M)Nov 21, 1995 · N1447L · Fokker F28MK0100SDR C2XA95IA329Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT ANGLE REF EMB FAX EST435/95. (M)Nov 15, 1995 · N15730 · Emb EMB120RTSDR C2XA95IA328Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RT ENGINE FRAME NR 2 SUPPORT ANGLE CRACKED AT FASTENERS. MAINTENANCE REMOVED AND REPLACED ENGINE FRAME NR 2 SUPPORT ANGLE REF EMB FAX EST 435/95. (M)Nov 15, 1995 · N15730 · Emb EMB120RTSDR DL76L954526Fairing · damagedTHE NR 2 PYLON SAILBOAT FAIRING IS DAMAGED REQUIRING REPLACEMENT. DL ERA 272101-14 DOCUMENTS PARTS REPLACEMENT INFORMATION.Oct 26, 1995 · N172DN · Boeing 767332SDR 96ZZZM330Attach Struct · damagedNR 3 MOTOR (PYLON) AFT MOUNT FOR SHOULDER COWL HAS MOUNTING HOLES ENLONGATED WHERE SHOULDER COWL ATTACHES TO LORD MOUNT, SEE REPAIR HC710H9003 FOR FIX. REPAIRED NR 3 ENGINE SHOULDER COWL AFT DOOR LORD MOUNT ATTACH STRUCTURE IAW BAE FAX PJN/1954-91. (M)Oct 20, 1995 · N610AW · Bag BAE146200ASDR DL72W954277Duct Housing · damagedDURING HMV, FOUND TEMP REPAIR ON RT SIDE OF NR 2 ENGINE INLET DUCT HOUSING. REPAIRED PER SRM 54-10-3 FIG 4.Oct 19, 1995 · N2814W · Boeing 727247SDR A6WR95021Pylon · rivets poppedDURING STRUCTURAL INSPECTION, FOUND THE HEADS POPPED OFF OF 3 RIVETS ON THE ANGLE BETWEEN RIBS 3 AND 4 ON THE CENTER BOX OF NR 4 PYLON. REPLACED THE RIVETS. (X)Oct 13, 1995 · N880DV · Bag BAE146200ASDR A6WR95020Pylon · rivets poppedDURING STRUCTURAL INSPECTION, FOUND THE HEADS POPPED OFF OF 2 RIVETS IN THE CENTER BOX FLOOR OF NR 3 PYLON. REPLACED THE RIVETS. (X)Oct 13, 1995 · N880DV · Bag BAE146200ASDR A6WR95019Pylon · rivets poppedDURING STRUCTURAL INSPECTION, FOUND THE HEADS POPPED OFF OF THE FIRST 3 RIVETS ON THE ANGLE BETWEEN RIBS 3 AND 4 ON THE CENTER BOX OF NR 2 PYLON. REPLACED THE RIVETS. (X)Oct 13, 1995 · N880DV · Bag BAE146200ASDR A6WR95018Pylon · rivets poppedDURING STRUCTURAL INSPECTION, FOUND THE HEADS POPPED OFF OF 2 RIVETS ON THE ANGLE BETWEEN RIBS 3 AND 4 ON THE CENTER BOX OF NR 1 PYLON. REPLACED THE RIVETS. (X)Oct 13, 1995 · N880DV · Bag BAE146200ASDR A6WR95014Rib · flange crackedDURING STRUCTURAL INSPECTION, FOUND ON NR 2 PYLON CENTER BOX, 3 RIVET HEADS POPPED OFF ON FLOOR AND THE BOTTOM OUTBOARD FLANGE ON RIB NR 4 CRACKED. INSTITUTED 1,000 CYCLE RE-INSPECTION IAW BAE RILHC546H9018. (X)Oct 12, 1995 · N881DV · Bag BAE146200ASDR C2XA95IA286Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND THE RIGHT NACELLE FRAME NR 2, MID SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Oct 11, 1995 · N22727 · Emb EMB120RTSDR C2XA95IA285Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND THE LEFT NACELLE FRAME NR 2, MID SUPPORT ANGLE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Oct 11, 1995 · N22727 · Emb EMB120RTSDR P5CA9500820Corner · tornNR 3 ENGINE INBOARD COWL OUTBOARD FORWARD TOP CORNER ON REPAIR TORN. REMOVED DAMAGED REPAIR, REPAIRED TORN DOUBLER IAW SRM 54-30-02. INSTALLED DOUBLER IAW SRM 51-10-01 AND 54-30-02.Oct 9, 1995 · N857FT · Boeing 747132SDR P5CA9500819Latch · crackedNR 1 ENGINE LEFT HAND CORE COWL THIRD LATCH FROM LEADING EDGE HAS CRACKED REPAIR. FABRICATED AND INSTALLED DOUBLER IAW SRM 54-30-01.Oct 9, 1995 · N857FT · Boeing 747132SDR P5CA9500818Clip · brokenNR 1 ENGINE LEFT HAND CORE COWL HAS BROKEN FRAME SUPPORT CLIP AT PRE-COOLER EXHAUST CUTOUT. FABRICATED NEW SUPPORT CLIP AND INSTALLED IAW SRM 51-10-01.Oct 9, 1995 · N857FT · Boeing 747132SDR P5CA9500815Angle · crackedNR 2 ENGINE INBOARD CORE COWL FORWARD LOCK LATCH CUTOUT ANGLE CRACKED. INSTALLED NEW DOUBLER AND ANGLE IAW SRM 51-30-02.Oct 9, 1995 · N857FT · Boeing 747132SDR P5CA9500811Skirt Fairing · crackedNR 2 ENG OUTBOARD SKIRT FAIRING AFT PANEL CRACKED. REMOVED DAMAGED PANEL AND ADJACENT SPLICE IAW SRM 51-10-01. FABRICATED AND INSTALLED NEW PARTS IAW SRM 51-10-01Oct 9, 1995 · N857FT · Boeing 747132SDR P5CA9500810Skirt Fairing · crackedNR 1 ENGINE OUTBOARD SKIRT FAIRING FORWARD PANEL CRACKED WITH 2 EACH FASTENERS MISSING. REMOVED DAMAGED PANEL IAW SRM 51-10-01, FABRICATED AND INSTALLED NEW PANEL IAW 51-10-01.Oct 9, 1995 · N857FT · Boeing 747132SDR P5CA9500809Skirt Fairing · crackedNR 1 ENGINE SKIRT FAIRING AT DRAIN TUBE CUTOUT HOLE AREA CRACKED. BLENDED DAMAGE IAW SRM 51-10-01.Oct 9, 1995 · N857FT · Boeing 747132SDR C2XA95IA275Angle · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT NACELLE FRAME NR 2, MID-SUPPORT ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 7, 1995 · N15725 · Emb EMB120RTSDR C2XA95IA274Angle · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE FRAME NR 2, MID-SUPPORT ANGLE WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE ANGLE, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)Oct 7, 1995 · N15725 · Emb EMB120RTSDR 95FDEA01549Heat Shield · crackedNR 1 PYLON HEAT SHIELD IS CRACKED FWD OF PRECOOLER AIR DUCT, GI 44B0517 NR NR0009.Oct 6, 1995 · N401FE · Airbus A310203SDR HALA95132Angle · crackedHNL - IN C-CHECK, RIGHT PYLON TO FUSELAGE TOP ATTACH ANGLE HAS A CRACK APPROX 1.5 INCHES LONG BELOW AFT PRESSURE BULKHEAD TEE CAP. REPLACED PYLON ANGLE. REPLACED FASTENERS IN VERTICAL LEG THROUGH FUSELAGE PER SRM 54-04. INSTALLED HORIZONTAL LEG FASTENERS PEOct 2, 1995 · N672MC · Doug DC951SDR 95FDEA01466Spar Web · crackedTHE NR 1 PYLON CENTER SPAR WEB WAS FOUND CRACKED. CRACK EMANATED FROM LAST LIGHTENING HOLE DIAGONALLY TO THE I/B AFT CORNER ATTACH BOLT HOLE, CRACK TERMINATES AT EXISTING FASTENER HOLE. FABRICATED AND INSTALLED REPAIR PER SRM 54-00-01 PAGE 11.Sep 30, 1995 · N68054 · Doug DC1010FSDR EISA95304S-Duct · crackedUPON A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, THE S-DUCT AT RIB NR 1 STAINLESS STEEL REPAIR HAS WORKING FASTENERS, 45 EACH. DURING REMOVAL OF FASTENERS AND REPAIR FOUND CRACK HAD EXCEEDED LENGTH OF REPAIR. REMOVED SECTION WITH CRACK. FORMED ANDSep 29, 1995 · N357NE · Boeing 72782SDR 95UAL900161Spar · crackedDURING NR 2 ENGINE CHANGE, FOUND NR 2 LOWER HORIZONTAL SPAR WITH 6 INCH CRACK. CRACK WAS LOCATED BETWEEN NAC STA 210 AND 216, ADJACENT TO INBOARD CHORD. REPAIRED PER ADAPTION OF SRM 54-10-03.Sep 29, 1995 · N148UA · Boeing 747SP21SDR MALA954652Formers · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT INBOARD AND RIGHT INBOARD NACELLE FORMERS CRACKED. THEY REPAIRED THE CRACKS BY STOP DRILLING AND INSTALLING A DOUBLER IAW FAIRCHILD SRM 54-90-10. (M)Sep 27, 1995 · N439MA · Swrngn SA227ACSDR MALA954648Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT NACELLE OUTBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND INSTALLED A DOUBLER OVER THE SPLICE AREA IAW FAIRCHILD ARP 54-20-9101. (M)Sep 26, 1995 · N2693C · Swrngn SA227ACSDR MALA954647Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND THE LEFT NACELLE OUTBOARD UPPER WING SKIN TO NACELLE ATTACH ANGLE CRACKED. THEY STOP DRILLED THE CRACK AND INSTALLED DOUBLER OVER THE SPLICE AREA IAW FAIRCHILD ARP 54-20-9101. (M)Sep 26, 1995 · N2693C · Swrngn SA227ACSDR P5CA9500788Bracket · crackedSUPPORT BRACKET CRACKED, NR 3 ENGINE BLEED AIR RELIEF VALVE, 9 O'CLOCK POSITION. WELD REPAIRED PER BAC5975.Sep 22, 1995 · N853FT · Boeing 747122SDR MALA954637Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, THE LEFT OUTBOARD WING SKIN TO NACELLE ATTACH ANGLE WAS FOUND TO BE CRACKED AT THE ELEVENTH RIVET. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE IAW ARP 54-20-9101, REVISION B. (M)Sep 15, 1995 · N426MA · Swrngn SA227ACSDR DLM88953705Angle · crackedFOUND ON B2 LETTER CHECK, CRACK IN ATTACH ANGLE UPPER AFT END, NR 1 PYLON .75 INCH. REPAIRED PER MM 54-04A.Sep 14, 1995 · N909DL · Doug MD88SDR 95FDEA01334Spar · corrodedNR 1 PYLON UPPER SPAR RT CHORD, AFT 16, HAS RUST ON TOP OF HORIZONTAL FLANGE AND INBOARD SIDE OF TOP VERTICAL FLANGE. CLEANED AND TREATED CORROSION PER SRM 51-21-01, PAGE 36.Sep 13, 1995 · N301FE · Doug DC1030FSDR 95ZZZX6270Fairing · wornMAINTENANCE REPORT, NR 2 ENGINE NOSE COWL WORN 50 PERCENT OF DEPTH IN .040 INCH 2024T3 SKIN UNDER MATING SURFACE OF FORWARD WING TO NACELLE FAIRING. FABRICATED DOUBLER .040 INCH 2024T3, 2 FASTENER ROWS WIDER THAN EXISTING DAMAGE AND REPAIRED PER SHIVA ENT., ISep 11, 1995 · N302VA · Boeing 737247
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