Rolls-Royce SPEY-555-15

Service difficulty reports · 261

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'SPEY55515'
  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 CA960826016Cockpit Pack · cabin smoke(CAN) ONE MINUTE AFTER TAKEOFF FLIGHT ATTENDANT INFORMED CREW OF SMOKE IN CABIN, AND LAVATORY SMOKE DETECTOR HAD SOUNDED. AIRCRAFT RETURNED TO GATE. FLIGHT TEST CONFIRMED COCKPIT PACK EMITTING SMOKE. OPERATED ON MEL.Jul 27, 1996 · Fokker F28MK1000 · Cabin Cooling SystemSDR CA960619032Duct Crossover · liberated(CAN) REJECTED TAKEOFF DUE TO INSUFFICIENT POWER FROM #1 ENGINE. INSPECTION FOUND THE OUTER CROSSOVER DUCT ATTACH POINT HAD PULLED OUT OF THE BYPASS DUCT. REPLACEMENT ENGINE INSTALLED. ENGINE GROUND RUN SERVICEABLE AND AIRCRAFT RETURNED TO SERVICE.Jun 2, 1996 · Fokker F28MK1000 · Turbine Engine Bypass SectionSDR AU960582Hinge · cracked(AUS) RH WING OUTBOARD LIFT DUMPER NO5 PANEL INBOARD HINGE LUG CRACKEDApr 29, 1996 · Fokker F28MK1000 · SpoilersSDR AU960950Spar Web · cracked(AUS) LH OUTER WING REAR SPAR WEB CRACKED AT APPROXIMATELY STN 5115 RUNNING FROM LOWEST RIVET - CRACK LENGTH 5MM (0.196IN) - FOUND DURING EDDY CURRENT INSPECTION IAW ER F28-57-10-22C PART 2Apr 24, 1996 · Fokker F28MK4000 · Wing SparSDR CA960522004Governor · req adjust(CAN)AIRCRAFT FAILED TO MAKE 100 PERCENT RATED THRUST ON TAKEOFF, TAKEOFF REJECTED LP GOVERNOR ADJUSTED TO 102 PERCENTApr 18, 1996 · Fokker F28MK1000 · Turbine GovernorSDR USAAF96031Tube · crackedCLT - FLT 242 - AFTER TAKEOFF, CREW RECEIVED A NR 2 BLEED FAULT MESSAGE AND THEN A NR 2 DUCT LEAK MESSAGE. FLIGHT RETURNED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND A CRACKED LINE IN THE NR 2 ENGINE SUB WING TEST BLOCK AREA. A TEMPORARY Mar 25, 1996 · N881US · Fokker F28MK0100 · Compressor Bleed ControlSDR AU960989Door · cracked(AUS) LH AND RH OVERWING EMERGENCY EXIT DOOR OUTER RADIUS CRACKED IN THE FOLLOWING AREAS:-1. RH FORWARD EMERGENCY EXIT CRACKED IN FORWARD AND AFT LOWER CORNERS - CRACK LENGTH 25.4MM (1IN) 2. LH REAR EMERGENCY EXIT CRACKED IN LOWER AFT CORNER - CRACK LENGTH 6.3Mar 5, 1996 · Fokker F28MK4000 · Emergency ExitsSDR AU960990Web · cracked(AUS) REAR PRESSURE BULKHEAD WEB LOCATED BETWEEN HORIZONTAL BEAMS II AND III AND VERTICAL BEAMS 425L AND 1050L CRACKED VERTICALLY - CRACK LENGTH 52MM (2IN) - FOUND DURING EDDY CURRENT INSPECTION IAW ER F28-53-10-15K PART 4Mar 5, 1996 · Fokker F28MK4000 · Fuselage Main, BulkheadSDR CA960311033Fuel Flow Reg · faulty(CAN)DURING CLIMB, #1 ENGINE EXCEEDED MAXIMUM TGT FOR THIS STAGE OF FLIGHT. THE ENGINE WAS SHUT DOWN, AND AIRCRAFT RETURNED TO BLOCKS. THE FUEL FLOW REGULATOR WAS REPLACED, GROUND RUN WAS CARRIED OUT AND F OUND SERVICEABLE.Mar 3, 1996 · Fokker F28MK1000 · Fuel Controlling SystemSDR QXEA9500408Hmu · malfunctionedPDX - STRONG FUEL SMELL IN COCKPIT AND CABIN AFTER STARTING NR 1 ENGINE. NR 1 HMU REPLACED I/A/W MAINT. MANUAL. HMU OPS CHECKED GOOD ON GROUND RUN. NO FUEL SMELL NOTED IN COCKPIT OR CABIN. AIRCRAFT RETURNED TO SERVICE.Nov 27, 1995 · N802PH · Dhav DHC8102 · Fuel Control/Reciprocating EnginesSDR USAA950762Governor · leakingSRQ - FLT NR 0139 - DURING A GO-AROUND PROCEDURE DUE TO THUNDERSTORMS, THE LEFT ENGINE WOULD NOT PRODUCE SELECTED THRUST. CAPTAIN DECIDED TO DIVERT TO SRQ WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE LP SHAFT GOVERNOR. LEAK CHECKED GOOD. (Jul 20, 1995 · N898US · Fokker F28MK0100 · Turbine Governor
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