JASC 5412
Service difficulty reports · 1,087
Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, 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 = '5412' 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 = '5412' 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 UPS06547780Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD INBD LOWER CORNER CHAFED. FINISHED REPAIR PER SOPM 20-43-03, AND EA NR 757-5453-27-A1509 STEPS 3 3,4,6, AND 7.SDR QXEA200602076Firewall · crackedPDX C4 RIGHT HAND ENGINE FIRE WALL HAS CRACK INBOARD AT 2 O'CLOCK POSITION WHERE FIRE BLANKET ATTACHES TO FRAME ANGLE. REPAIRED IAW RD 8-54-651.SDR QXEA200602002Firewall · crackedPDX C4 RIGHT NACELLE FIREWALL CRACKED, OUTBOARD SIDE APPROXIMATELY 10" DOWN FORM ROOF. REPAIRED IAW DHC-8-200 RD 8-54-611.SDR KCSA061249Bulkhead · chafedNR 3 PYLON NAC STA 221.0 BULKHEAD WEB CHAFED AROUND HYDRAULIC FITTINGS.SDR KCSA061247Repair · chafedNR 1 PYLON NAC STA 221.9 BULKHEAD REPAIR CHAFED AT HYDRAULIC LINE UNION FITTINGS.SDR KCSA061239Doubler · damagedNR 4 PYLON HYDRAULIC PRESSURE LINE BULKHEAD FITTING JAMNUT LOOSE AFT OF STA. 221.9 BULKHEAD CAUSING DAMAGE TO BULKHEAD DOUBLER.SDR SWIA200616953Firewall · crackedLEFT UPPER AFT WHEEL WELL, CRACK ON FIREWALL ACCESS 434 F2, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED FIREWALL IAW EMB 120 SRM 51-10-02 AND 51-40-02.SDR HALA0600660Stiffener · crackedNR 1 ENG STRUT - PYLON AFT BULKHEAD INTERIOR - HORIZONTAL STIFFENER CRACKED AT LOWER FLANGE, AT SECOND FASTENER FROM O/B END, APPROX 18 INCHES BELOW WING PLANK. REMOVED NR 1 ENG STRUT AFT FAIRING HORIZONTAL STIFFENER 18 INCHES BELOW WING PLANK ON AFT SIDE INTSDR KCSA061213Fire Seal · damagedNR 1 PYLON, INBD FIRE SEAL DAMAGED ALONG THE ENTIRE LENGTH OF THE SEAL.SDR KCSA061205Bulkhead · chafedNR 3 PYLON NAC STA 221.90 BULKHEAD WORN AT HYDRAULIC PRESSURE LINE ABOVE MID SPAR.SDR KCSA061204Bulkhead · chafedNR 1 PYLON NAC STA 221.90 BULKHEAD WORN AT HYDRAULIC PRESSURE LINE ABOVE MID SPAR.SDR 0601616743Frame · crackedDURING H-CHECK FOUND CRACKS IN NR 1 PYLON REAR MOUNT BULKHEAD FRAMES. REPAIRED PER EA 67-206278.SDR KCSA061193Bulkhead · chafedNR 4 PYLON NAC STA 221.90 BULKHEAD WEB HAS A WORN CHAFED AREA AROUND HYDRAULIC LINES.SDR KCSA061192Bulkhead · gougedNR 1 PYLON BULKHEAD WEB HAS A TOOL MARK NEXT TO HYDRAULIC LINES AT NAC STA 221.90.SDR KCSA061191Bulkhead · crackedNR 2 PYLON NAC STA 221.9 BULKHEAD FORWARD SIDE FITTING P/N 65B91314-3 IS CRACKED.SDR KCSA061190Bulkhead · crackedNR 2 PYLON REAR ENGINE MOUNT BULKHEAD FRAME TOP UPPER AFT INBOARD SIDE IS CRACKED AT NAC STA 221.90SDR UIEA200600169Skin · crackedFOUND NR 2 PYLON ACCESS PANEL 463AR CUT-OUT CRACK. REPAIR C/OUT ON NR2 PYLON ACCESS DOOR CUT-OUT 463AR PER BOEING RESPONSE MSG 1-200482351-2. CRACKED FASTENER HOLE AT NAC STA 284 REAMED THROUGH SKIN AND STRAP PER BOEING MSG 1-200482351-7. NIL CRACK FOUND AFSDR UPS06547339Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD OUTBOARD LOWER CORNER IS CHAFED. COMPLIED WITH EA 757-5453-27-A1482 INSTRUCTIONS 1-8.SDR KCSA061181Bulkhead · wornNR 1 PYLON HYDRAULIC PRESSURE LINE JAM NUT WORN INTO INTERNAL BULKHEAD AT NAC STA 221.90.SDR 1060607019Web · wornHOLE WORN ON WEB OF LT FIREWALL. LOOSE FASTENER FOUND TO HAVE CAME LOOSE AND WORE OUT THE HOLE. EXTRA CARE HAS BEEN TAKEN TO ENSURE THE FASTENER TO BE CHECKED FOR PROPER TORQUE. HOLE REPAIRED IAW MFG FR-CO-01357 REV 1.SDR UPS06547264Bulkhead · chafedNR 1 PYLON AFT BULKHEAD HAVE CHAFED AREA ON INBOARD AND OUTBOARD LOWER CORNERS. COMPLIED WITH EO NR B757-5410-24560-A AND EA NR 757-5453-27-A1479 R REV.SDR UPS06547265Bulkhead · chafedNR 2 PLYON AFT BULKHEAD O/B AREA HAS CHAFED. COMPLIED WITH EO NR B757-5410-24560-A AND EA NR 757-5453-27-A1479 REV.SDR QXEA200601400Firewall · crackedPDX C4 RIGHT HAND UPPER RETRACTION ACTUATOR FITTING ATTACH BOLT ACCESS HOLE IN THE FIREWALL HAS RADIAL CRACKS TO THE NUT PLATES IN THREE LOCATIONS. REPAIRED IAW RD 8-54-2196.SDR UPS06547140Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LOWER CORNER LT AND RT CHAFING. REPAIRED IAW EA 757-5453-27-A1460.SDR UPS06547144Bulkhead · gougedINSPECTION TYPE:C NR 2 ENG PYLON AFT BULKHEAD I/B SIDE LWR CORNER EXTERNAL SURFACE PITTED AND GOUGED. REPAIRED IAW EA 757-5453-27-A1460.SDR UPS06547143Bulkhead · tool damageINSPECTION TYPE:C NR 2 ENG PYLON AFT BULKHEAD LWR FLANGE HAS TOOL MARKS ON 3 EA HOLES AND ON I/B CORNER EDGE. ACCOMPLISH EA 757-5453-27-A1460 AND UPS EO B757-5410-24523-A.SDR KCSA061169Bulkhead · crackedNR 3 PYLON INTERNAL UPPER REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED AT NAC STA 221.90, LT SIDE.SDR KCSA061168Bulkhead · crackedNR 3 PYLON INTERNAL UPPER REAR ENGINE MOUNT BULKHEAD FRAME IS CRACKED AT NAC STA 221.90, RT SIDE.SDR EIA2006230Skin · crackedNR 4 PYLON, NAC STA. 247, NR 3 STIFFENER AND SKIN CRACKED. FABBED AND INSTALLED REPAIRS IAW ECRA 489-54-007-2 (MZJ).SDR USAA060708Stiffener · crackedNR 2 PYLON I/B, FWD OF AFT BULKHEAD CRACKED. REMOVED & INSTALLED FABRICATED PART PER SRM 51-40-05, 51-70-11, 51-40-02, DEFECT SIZE: 1.75 INCH.SDR USAA060707Stiffener · crackedNR 2 PYLON I/B, FWD OF AFT BULKHEAD CRACKED. REMOVED & INSTALLED FABRICATED PART PER SRM 51-40-05, 51-70-11, 51-40-02, DEFECT SIZE: 1.75 INCH.SDR UPS06547039Bulkhead · chafedINSPECTION TYPE:N/A NR 2 PYLON MIDSPAR BULKHEAD LOWER RIGHT CORNER IS HEAILY CHAFED. COMPLIED WITH EA 757-5453-27-A1439 AND UPS EO B757-5410-24414.SDR 0600936719Strap · crackedDURING L-CHECK FOUND CRACK IN NR 2 PYLON BULKHEAD STRAP AT NAC STA 224 AND SKIN CRACK AT NAC STA 221.9. REPAIRED PER EA 67-206237 SECT I, SECTION II CALLS FOR REPEAT INSPECTIONS AT L-CHECK INTERVALS OR 18 MONTHS WHICHEVER COMES FIRST.SDR UPS06547220Bulkhead · gougedINSPECTION TYPE:C NR 1 PYLON BULKHEAD INBD SIDE HAS DEEP GOUGES LOWER CORNER. COMPLIED WITH EA 757-5453-27-A1415.SDR 061126Bulkhead · crackedNR 3 PYLON REPAIR STOP DRILLED 2" VERTICAL CRACK ON THE AFT ENGINE MOUNT BULKHEAD UPPER I/B AFT FLANGE RADIUS.SDR 06FDEA1365Panel · missingNR 1 ENGINE PYLON MISSING FWD BLOWOUT PANEL. INSTALLED NEW BLOW OUT PANEL IN NR 1 ENGINE PYLON PANEL NR 5402 IAW FED EX MM 54-30-011-8.SDR 061122Stiffener · crackedNR 4 PYLON INTERNAL FORWARD BULKHEAD HORIZONTAL STIFFENER IS CRACKED AT NAC STA 180.SDR 061084Doubler · crackedNR 3 PYLON BULKHEAD DOUBLER AT APPROX NAC STA 300 IS CRACKED JUST OUTBOARD OF THE DIAGONAL BRACE ATTACHMENT.SDR KCSA061101Bulkhead · wornNR 1 PYLON NAC STA 221 BULKHEAD WORN AROUND HYDRAULIC FITTING.SDR QXEA200601054Firewall · damagedYYC - C4 LEFT NACELLE FIREWALL ABOVE OIL COOLER HAS CHAFING ON CENTER EDGE AND CRACK INTO PANEL. REPAIRED IAW DHC-8-200 SRM 51-40-11.SDR QXEA200601053Firewall · damagedYYC - C4 RIGHT NACELLE FIREWALL ABOVE OIL COOLER HAS FORWARD EDGE CHAFED THROUGH IN THE CENTER AND INBOARD EDGE IS BENT. REPAIRED IAW DHC-8-200 SRM 51-40-11.SDR DL76G060247Fitting · damagedNR 2 PYLON NAC STA 253.70 FORWARD UPPER SPAR FITTING ASSY BORES WERE FOUND ELONGATED. HOLES WERE OVERSIZED AND A BUSHING INSTALLED.SDR DL757071117Bulkhead · damagedDURING HMV AT YVR, AN EXISTING REPAIR WITH INSUFFICIENT FASTENER EDGE DISTANCE AND SPACING WAS FOUND AND REPLACED WITH A PERMANENT REPAIR.SDR DL757060248Fitting · damagedTHE NR 2 ENGINE PYLON BULKHEAD FITTING AT NAC STA 116.05 WAS FOUND WITH EXISTING REPAIRS THAT REQUIRED REPLACEMENT. EXISTING REPAIRS REMOVED AND A LARGER REPAIR FITTING WAS INSTALLED.SDR 2006FA0000333Bulkhead · corrodedDURING 500 HR. VISUAL INSPECTION PER AD2000-01-16 PARA (D) FOUND LEFT ENGINE AFT CANTED BULKHEAD NR 5695005-11 AND SUPPORT DOUBLER NR 5695005-6 CORRODED AND HEAT DAMAGED COMPLETELY THROUGH STRUCTURE. DAMAGE LOCATED NEAR OB SECTION ABOVE EXHAUST ELBOW CUT OUT SDR 2006FA0000332Bulkhead · corrodedDURING 500 HR. VISUAL INSPECTION PER AD2000-01-16 PARA (D) FOUND LEFT ENGINE AFT CANTED BULKHEAD #5695005-11 AND SUPPORT DOUBLER #5695005-6 CORRODED AND HEAT DAMAGED COMPLETELY THROUGH STRUCTURE. DAMAGE LOCATED NEAR OUTBOARD SECTION ABOVE EXHAUST ELBOW CUT OUSDR UPS06547235Bulkhead · chafedINSPECTION TYPE:C NR 1 PYLON AFT BULKHEAD LOWER FLANGE HAS DEEPLY CHAFED AREAS ON LT & RT SIDES. ROUTED TO FAB SHOP TO MILL CHAFED AREAS. AFTER MILLING LEFT SIDE IS A .160 RIGHT SIDE IS AT .165 REF PRELIMINARY EA 757-5453-27-A1370 03-16-06; HFEC INSP PER NTSDR UPS06547234Bulkhead · chafedINSPECTION TYPE:C NR 2 PYLON AFT BULKHEAD LOWER FLANGES LT & RT SIDES HAVE DEEP CHAFFED AREAS. MILLED DAMAGED AREAS AND INSTALLED REPAIR COSETS, FILLERS AND REPAIR WASHERS IAW 757-5453-27-A1370 WORKED PER EA 757-5453-27-A1370 REV DATED 3-14-06 JP 00827 4-10-0SDR USAA060443Firewall · crackedLEFT ENGINE LAPF FWD FIREWALL LOWER I/B CORNER CRACKED. CRACK STOP DRILLED, DOUBLER FABRICATED PER PW CMM 54-56-11 REPAIR 14, DEFECT SIZE: 0.75 INCH.SDR USAA060441Firewall · crackedLEFT ENGINE LAPF FWD FIREWALL LOWER O/B CORNER CRACKED. CRACK STOP DRILLED, DOUBLER FABRICATED PER PW CMM 54-56-11 REPAIR 14, DEFECT SIZE: 0.500 INCH CRACK.
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