JASC 7270
Service difficulty reports · 65
Reports filed under 7270 · Turbine Engine Bypass Section, 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 = '7270' 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 = '7270' 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 HYIA20230512001Sensor · failedPILOT REPORTED LEFT ENGINE LOST FUEL PRESSURE WHEN CLIMBING THROUGH 7000 FEET. CREW NOTICED IT WAS WHEN THE LEFT FUEL PUMP WOULD CYCLE ON AUTOMATICALLY AND THE FUEL PRESSURE WENT INTO RED ARC ACCOMPANIED BY A 'LOW FUEL PRESSURE CAS MESSAGE'. MAINTENANCE INSPECSDR 2021FA0000336None · noneLH ENGINE LPT BORESCOPE PORT PLUG BROKEN BOLT. REFERENCE PRATT & WHITNEY CANADA LETTER DAA2021-891-PW306D1-CN0121, CRM CASE: PWC-201057-M8D8 DATED NOVEMBER 18,2021.SDR CA190617027Duct · damaged(CAN) DURING ROUTINE INSPECTION, NOTICED THAT THERE WAS SOME DAMAGE ON LH ENGINE ON THE OUTER BYPASS DUCT JUST AFT OF THE IGNITION BOX. BORESCOPED THE ENGINE AND ENGINE RUNS CARRIED OUT FOR VIBE CHECK WHICH INDICATED A SERVICEABLE ENGINE. REMOVED THE ENGINE FRSDR HALA2015101300211Guide Vane · looseDURING ENGINE A-CHECK, FOUND MULTIPLE FASTENERS LOOSE ON EXIT GUIDE VANE PANELS. PERFORMED MINOR REPAIRS TO NR 1 ENGINE OGV INFILL PANELS IAW ERA 540402-14 ORIGINAL, VISUAL INSPECTION WITHIN 15 FLT CYCLES DUE. ENGINE OK FOR SERVICE.SDR SIMA20141024003Duct · damagedTRANSFERRED FROM NRWC 942-SGF-02022 ITEM 1. LT ENG INNER RT BYPASS DUCT HAS LARGE BURN HOLE IN IT. R & R LT ENG ASSEMBLY IAW WC 71-000-00. OPERATIONS CHECK & LEAK CHECKED GOOD.SDR QXEA2012100601181Actuator · missingNR 2 LOWER COWLING BYPASS DOOR AND ACTUATOR FOUND MISSING FROM THE ACFT ON POST FLIGHT WALKAROUND BY MX. REPLACED THE LOWER COWL AND ALSO THE DEBRIS DOOR ACTUATOR IAW AMM TASK 71-61-06-400-801. RETURNED TO SERVICE.SDR 2012FA0000647Duct · delaminatedAFT BYPASS DUCT WAS FOUND DELAMINATED DURING A SCHEDULED INSPECTION.SDR 2011FA0000636Panel · damagedAPPROX 4" DIAMETER HOLE IN INNER BYPASS DUCT PANEL OVER NR1 IGNITOR OF RT ENGINE.SDR CHQA200900178Engine · leakingFLIGHT 6047, CMH TO JFK. ON CLIMBOUT BETWEEN 500 TO 1,000 FT A BURNING ODOR THAT SMELLED LIKE OIL WAS NOTICED IN THE COCKPIT WITH NO ASSOCIATED WARNINGS. THE FLIGHT ATTENDANT REPORTED MOMENTS LATER A BURNING ODOR AND SLIGHT HAZE IN THE CABIN. THE FLIGHT CRESDR CA070613001Duct · misrepaired(CAN) ENGINE FRONT BYPASS DUCT FOUND AT INSPECTION WITH NON STANDARD REPAIR OUTSIDE OEM LIMITATION. PATCH REPAIR ON OUTSIDE WALL 8 INCH LONG BY 2.5 INCH WIDE OUTSIDE SCOPE OF XRS3025. PART REJECTED AND REMOVED FROM ENGINE. (TC NR 20070613001)SDR DXTA200601576Duct · separatedRIGHT ENGINE REAR INNER BYPASS DUCT SEPARATED FROM AIRCRAFT DURING TAKEOFF ROLL. REMOVED REAR INNER BYPASS DUCT ASSEMBLY DUE TO DAMAGED CONE. INSTALLED AN OVERHAULED ASSEMBLY (OVERHAULED BY PRATT AND WHITNEY ENGINE SERVICES, CRS NR LM1R301K, UNDER WO NR 6128SDR DXTA200601573Duct · separatedRIGHT ENGINE REAR INNER BYPASS DUCT SEPARATED FROM AIRCRAFT DURING TAKEOFF ROLL.SDR DELA200600002Skin · crackedDURING ROUTINE LINE MAINTENANCE WALK INSPECTION, 2 CRACKS WERE NOTED IN 2 SEPARATE SKINS OF THE LT SIDE INNER BY PASS DUCT. BOTH CRACKS EMANATED FROM A DPI SWITCH ACCESS COVER DOUBLER RIVET AND PROPAGATED OUTWARD FROM THE DOI SWITCH CUT OUT AREA. BOTH SKINS, SDR CA060531014Panel · fractured(CAN) DURING GROUND INSPECTION METAL DEBRIS WAS FOUND LODGED IN THE ENGINE BYPASS DUCTING. THE ENGINE'S INNER BYPASS DUCT PANELS WERE FOUND FRACTURED. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060531014)SDR BHK2006F00000Fan Blade · brokenTHE MID SPAN DAMPENER APPEARS TO HAVE BROKEN OFF AND WENT THROUGH THE BYPASS OF THE ENGINE. THIS CAUSED DAMAGE TO SOME OTHER BLADES AND GUIDES AND ALSO THE INLET HOUSING. THE ENGINE WAS REMOVED AND HAS BEEN SENT FOR FURTHER EVALUATION. (K)SDR CLC2006F00004Duct · brokenON CLIMB OUT, NR 1 ENGINE FIRE DETECTOR ILLUMINATED. RETURNED TO DEPARTURE, INSPECTION OF AC ENGINE FOUND BLOWN DUCT. REMOVED AND REPLACED DUCT. (K)SDR 249TR0067Flange · crackedLEFT ENGINE FLANGE CRACKED OUTBOARD MOUNT FLANGE FOR THE PRECOOLER. REPAIRED PER JT8D MM 72-00.SDR EIA2004005Guide Vane · missingON POST FLIGHT WALKAROUND FOUND FAN EXIT GUIDE VANE MISSING AT 6:30 POSITION ON NR 4 ENGINE. VANE STRUCK T/E OF T/R SLEEVE CAUSING TEAR AT 6:30 POSITION AND PUT A HOLE IN THE LT INBOARD COWL. TRANSFERRED TO COI NR 053 MAX 50 HRS FLY BACK ENGINE SCHEDULED ATSDR HALA0301199Bypass Valve · malfunctionedFLT 119 - HNL - 'ENG RT SYSTEM FAIL' ILLUMINATE EN ROUTE, STAYED ON ENTIRE TIME. INTERROGATED EEC-2. FOUND FAULT 731304, BYPASS AND VENT VALVE MECHANICAL FAULT. TROUBLESHOT PER FIM 73-13, TASK 804. REPLACED BYPASS AND VENT VALVE PER AMM 73-13-04. LEAK ANDSDR B3OR20031119Duct · crackedDURING A PHASE 3 AND 4 INSPECTION, IT WAS DISCOVERED THAT THE FORWARD INNER BY-PASS DUCT HAD A CRACK. THE CRACK WAS LOCATED AT THE 6 O'CLOCK POSITION AND WAS ABOUT AND INCH-AND-A-HALF LONG. THE DUCT WAS REMOVED AND A NEW FORWARD INNER BY-PASS DUCT WAS INSTALLESDR UO22003F00007Duct · crackedNR 2 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.SDR UO22003F00006Duct · crackedNR 3 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.(K)SDR UO22003F00005Duct · crackedNR 1 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.SDR UO22003F00010Duct · crackedNR 1 ENGINE AFT BY-PASS DUCT CRACK AROUND 9 O’CLOCK RIB DUCT, ALLOWED MOMENTARY DISENGAGEMENT OF OIL TRANSFER TUBE AND ORING FAILURE. OIL LEAK CAUSED LOSS OF OIL PRESSURE AT TAKEOFF. PILOT SHUT DOWN ENGINE AND LANDED AT NEAREST AIRPORT. AT REPLACEMENT OF SDR UO22003F00009Duct · crackedNR 2 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 OCLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAL MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K)SDR UO22003F00008Duct · crackedNR 3 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 O`CLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAN MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K)SDR C2XA03IA083Manifold · dislodgedIAH - AFTER ROTATION THE CREW REPORTED THAT THE NR 1 ENGINE EXCEEDED ALLOWABLE TEMPERATURE LIMITS. THE AIRCRAFT RETURNED TO IAH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 1 ENGINE AND FOUND THAT THE UPPER BYPASS DUCT PANEL AND MANIFOLD ASSEMBLY SDR COMA0360162FanFLIGHT 5490 VIB WARNING WHEN T/O THRUST APPLIED.COULD NOT DUPLICATE - INSPECTED ENGINE AND FOUND NO DISCREPANCIES, C/W A FAN TRIM BALANCE AND REDUCED VIB FROM .9 TO .4SDR AUS20021139Panel · damaged(AUS) RH ENGINE BIRDSTRIKE. INVESTIGATION FOUND ENGINE NACELLE FAN DUCT EXTENSION UPPER ACOUSTIC PANEL MISSING.SDR CA020503001Duct · cracked(CAN) DURING PHASE I & II INSPECTION, LT ENGINE FRONT & REAR INNER BYPASS DUCT FOUND CRACKED. PARTS REMOVED FROM ENGINE INSPECTED & FOUND PARTS HAD BEEN REPAIRED PREVIOUSLY, WELDED AT OVERHAUL & CRACK NEXT TO WELDED AREA.PROBABLE CAUSE, HI-TIME PARTS, PREVIOUSSDR C2XA02TY031Duct · corrodedTYS DURING A SCHEDULED 1-C INSPECTION CORROSION WAS FOUND BETWEEN THE OUTER BYPASS AND THE FAN CASE ON NR 2 ENGINE. MAINTENANCE CLEANED THE AFFECTED AREA, APPLIED A CHEMICAL COATING AND APPLIED CORROSION RESISTANT PAINT IAW EC7000-01001. WORK WAS ACCOMPLISHSDR CA020215010Duct · cracked(CAN) DURING DAILY INSPECTION, RT ENGINE FRONT & REAR INNER BYPASS DUCT FOUND CRACKED AND PIECE OF REAR UNDER BYPASS DUCT MISSING. AFTER REMOVAL OF THOSE ITEMS FROM THE ENGINE, THE INSPECTION REVEALED THAT THEY WERE PARTS WHICH WAS PREVIOUSLY WELDED/OVERHAUL ASDR B3OR20020005Duct · crackedAIRCRAFT WAS INDUCTED INTO A PHASE1,2,5A & B INSPECTION.DURING THE INSPECTION OF THE NUMBER 2 ENGINE, THE FRONT BY-PASS DUCT WAS FOUND CRACKED AND A PIECE MISSING FROM IT. THE DUCT WAS REMOVED AND REPLACED WITH A SERVICEABLE DUCT.SDR CA020211014Bypass Jacket · damaged(CAN) A/C CAME IN FOR OVERNIGHT WITH NO MAINT PROBLEMS REPORTED. DURING OVERNIGHT SERVICE CHECK, DAMAGE NOTED ON BYPASS DUCT & CORE ENGINE. INITIAL INSPECTION FOUND DAMAGE IN BPD (BYPASS DUCT) AFT LOOKING FWD. AT 9 TO 2 O'CLOCK POS FROM BPD STATOR VANES TO ENDSDR C2XA01TY218Bypass Jacket · corrodedTYS DURING A SCHEDULED 1-C INSPECTION THE NR 1 FANCASE TO BYPASS HAD CORROSION. MAINTENANCE CLEANED UP THE CORROSION. APPLIED CHEMICAL FILM COATING TO THE MAGNESIUM IAW RR AE3007A MM 70-00-00-300-818 AND APPLIED CORROSION RESISTANT PAINT IAW EC7220-01009. SDR C2XA01TY202Bypass Jacket · corrodedTYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 AND NR 2 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCHUP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATISDR C2XA01TY203Bypass Jacket · corrodedTYS DURING A SCHEDULE INSPECTION, BETWEEN THE FAN CASE AND THE OUTER BYPASS, OXIDATION WAS FOUND ON NR 1 ENGINE. MAINTENANCE REMOVED THE OXIDATION, PERFORMED TOUCH UP OF PERMANENT RESIN COATING ON ACCESS, GEAR BOX MOUNTS, PLACED A CHEMICAL-FILM COATING FOR MSDR C1HA200182013EngineAFTER DEPARTURE IN CANCUN, #3 ENGINE BYPASS LIGHT ILLUMINATED ALSO LOUD VIBRATION IN #3 ENGINE PULLED POWER TO FLIGHT IDLE. ACTION TAKEN: REPLACED #3 ENGINE, TRIMMED AND OPS CHECKED GOOD IAW CHAMPION AIR TASK CARD 7101.SDR AUS20010968Acoustic Panel · missing(AUS) RT ENGINE COLD STREAM DUCT ACOUSTIC PANELS MISSING.SDR COMA0160679Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ONT HE LEFT ENGINE.SDR COMA0160678Fan Blade · damagedFLIGHT #5575. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160677Fan Blade · damagedFLIGHT #5575. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160676Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERD MULTIPLE BIRD STRIKES ON #1 ENIGNE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160675Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DELCARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFETY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160674Fan Blade · damagedFLIGHT #5775. DURING CLIMB OUT OF CVG AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES ON #1 ENGINE, CREW DECLARED AN EMERGENCY AIRCRAFT RETURNED TO THE FIELD AND LANDED SAFELY.REPLACED DAMAGED FAN BLADE ON THE LEFT ENGINE.SDR COMA0160234Warning System · illuminatedRT ENGINE FAN VIB ICON ON EICAS. INSPECTED ENGINE AND FOUND NO DEFECTS. COULD NOT DUPLICATE.SDR COMA0160110Plug · chafedLEFT ENGINE FAN VIB INDICATED 2.7. FOUND BLADES RUBBING AT ACCESS PLUG. ADJUSTED GAP AT ACCESS PLUG.SDR COMA0160098Spinner · vibrationLEFT ENGINE FAN VIB INDICATED 2.7. REPLACED THE AFT FAN SPINNER (OUT OF BALANCE).SDR 20000503SH004Case · damagedIT LOOKED LIKE THE Y-DUCT OF THE BLEED AIR MANIFOLD ASSY FAILED AT THE WELD CAUSING THE FAIRING ASSY OF THE FAN DUCT TO ALSO FAIL CAUSING DAMAGE TO THE INTERMEDIATE CASE AND REAR CASE HALVES, AND DAMAGE TO THE BYPASS LINERS (DIFFUSED SECTION). (X)SDR CA000516033Fan · failed(CAN) FOLLOWING A/C ROTATIONAT 100AGL THE NUMBER 2 ENGINE AUTOMATICALLY SHUTDOWN WITH AN OVERSPEED INDICATION. N1 FAN WOULD NOT ROTATE. ENGINE REPLACED.
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