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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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.SDR 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.SDR 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.SDR 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.SDR 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)SDR 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 OPSDR 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.SDR 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)SDR 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)SDR 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)SDR DL76L954526Fairing · damagedTHE NR 2 PYLON SAILBOAT FAIRING IS DAMAGED REQUIRING REPLACEMENT. DL ERA 272101-14 DOCUMENTS PARTS REPLACEMENT INFORMATION.SDR 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)SDR 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.SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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.SDR 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.SDR 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.SDR P5CA9500815Angle · crackedNR 2 ENGINE INBOARD CORE COWL FORWARD LOCK LATCH CUTOUT ANGLE CRACKED. INSTALLED NEW DOUBLER AND ANGLE IAW SRM 51-30-02.SDR 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 51-10-01SDR 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.SDR P5CA9500809Skirt Fairing · crackedNR 1 ENGINE SKIRT FAIRING AT DRAIN TUBE CUTOUT HOLE AREA CRACKED. BLENDED DAMAGE IAW SRM 51-10-01.SDR 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)SDR 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)SDR 95FDEA01549Heat Shield · crackedNR 1 PYLON HEAT SHIELD IS CRACKED FWD OF PRECOOLER AIR DUCT, GI 44B0517 NR NR0009.SDR 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 PESDR 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.SDR 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 ANDSDR 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.SDR 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)SDR 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)SDR 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)SDR P5CA9500788Bracket · crackedSUPPORT BRACKET CRACKED, NR 3 ENGINE BLEED AIR RELIEF VALVE, 9 O'CLOCK POSITION. WELD REPAIRED PER BAC5975.SDR 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)SDR DLM88953705Angle · crackedFOUND ON B2 LETTER CHECK, CRACK IN ATTACH ANGLE UPPER AFT END, NR 1 PYLON .75 INCH. REPAIRED PER MM 54-04A.SDR 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.SDR 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., I
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