# Service difficulty reports: Rolls-Royce DART-535-2 A list on [Rolls-Royce DART-535-2](https://openairdocs.org/engine/rolls-royce-dart-535-2.md). Newest first. General aviation reporting is voluntary. - [SDR CA141021012](https://openairdocs.org/sdr/CA141021012.md): Elt · false activation · Oct 19, 2014 · Braero HS7482B · Emergency Locator Beacon > (CAN) ELT ACTIVATED WHILE AIRCRAFT WAS ON THE APRON, REASON UNKNOWN. - [SDR CA140806005](https://openairdocs.org/sdr/CA140806005.md): Elt · malfunctioned · Jul 26, 2014 · Braero HS7482B · Emergency Locator Beacon > (CAN) ELT ACTIVATED WHILE ACFT WAS ON THE GROUND, REASON UNKNOWN. - [SDR CA140715001](https://openairdocs.org/sdr/CA140715001.md): Elt · false activation · Jul 13, 2014 · Braero HS7482B · Emergency Locator Beacon > (CAN) ELT ACTIVATED WHILE ON GROUND. REASON UNKNOWN. - [SDR CA140523007](https://openairdocs.org/sdr/CA140523007.md): Elt · false activation · May 2, 2014 · Braero HS7482B · Emergency Locator Beacon > (CAN) ELT ACTIVATED FOR UNKNOWN REASON WHILE ON GROUND. - [SDR CA140307006](https://openairdocs.org/sdr/CA140307006.md): Elt · false activation · Mar 7, 2014 · Braero HS7482B · Emergency Locator Beacon > (CAN) ELT ACTIVATED WHILE ON THE GROUND. REASON UNKNOWN. - [SDR CA021030003](https://openairdocs.org/sdr/CA021030003.md): Actuator · failed · Oct 17, 2002 · Braero HS7482B · Steering Unit > (CAN) NOSEWHEEL STEERING INTERMITTENTLY STIFF. NOSE WHEEL STEERING ACTUATOR WAS DISASSEMBLED. O-RING ON PISTON ROD WAS FOUND CUT, ALLOWING PRESSURE TO EQUALIZE ON EITHER SIDE OF THE RAM. BACKUP RINGS WHICH ARE INSTALLED ON EITHER SIDE OF THE O-RING WERE MISSIN - [SDR CA001030009](https://openairdocs.org/sdr/CA001030009.md): Radar · failed · Oct 12, 2000 · Braero HS7482B · Central Display > (CAN) ON DEPARTURE, DURING CLIMB RADAR INDICATOR EMITTED SMOKE AFTER SELECTED ON. ELECTRICAL FIRE CHECK LIST CARRIED OUT AIRCRAFT RETURNED TO POINT OF DEPARTURE. THE INDICATOR WAS VERIFIED AS THE SOURCE OF THE PROBLEM AND NO WIRING ANOMOLIES WERE OBSERVED. THE - [SDR CA000804022](https://openairdocs.org/sdr/CA000804022.md): Case · cracked · Jul 24, 2000 · Braero HS7482B · Turbine Engine Compressor Section > (CAN) DURING HOT SECTION INSPECTION, COMPRESSOR OUTLET CASING FOUND TO BE CRACKED BEYOND MAINTENANCE MANUAL LIMITS. CIRCUMFERENTIAL CRACK 7 IN, MAX ALLOWABLE IS 6 IN. AS VIEWED FROM REAR OF ENGINE THROUGH COMPRESSOR NR 1 OUTLET, WITH COMBUSTION CHAMBER REMOVE - [SDR CA000606022](https://openairdocs.org/sdr/CA000606022.md): Window · separated · May 26, 2000 · Braero HS7482B · Passenger Compartment Windows > (CAN) THE CREW REPORTED HEARING AN UNUSUAL ONE TIME NOISE WHILE THEY WERE ENROUTE YYH TO YZF. AFTER ARRIVING YZF A PORTION OF THE RT EMERGENCY EXIT OUTER WINDOW PANE WAS OBSERVED TO HAVE DEPARTED THE AIRCRAFT. DAMAGE TO THE RT HORIZONTAL STABILIZER LEADING EDG - [SDR CA991209063](https://openairdocs.org/sdr/CA991209063.md): Fire Detector · failed · Nov 24, 1999 · Braero HS7482B · Detection System > (CAN) ON TAXI, NR 1 ENGINE FIRE WARNING ILLUMINATED. INVESTIGATION REVEALED FAILED FIRE WIRE AND FERRULE. PARTS REPLACED. - [SDR CA990308010](https://openairdocs.org/sdr/CA990308010.md): Gearbox · making metal · Feb 19, 1999 · Braero HS7482B · Turbine Engine Accessory Drive > (CAN) DURING REMOVAL OF THE ALTERNATOR, FERROUS METAL WAS FOUND IN THE ALTERNATOR AREA. THE GEARBOX WAS REPLACED. - [SDR CA981230020](https://openairdocs.org/sdr/CA981230020.md): Line · leaking · Dec 18, 1998 · Braero HS7482B · Hydraulic System, Main > (CAN) HYDRAULIC FLOW LIGHTS CAME ON IN-FLIGHT, EMERGENCY DECLARED. WHEN U/C LOWERED, THE STANDBY LIGHT WENT OUT, HYDRAULIC PRESSURE WAS NORMAL. AIRCRAFT LANDED OK. STANDBY HYD PUMP BLEED NIPPLE LEAKING, RESEALED, PUMPS BLED AND FLUID REPLENISHED. ON APPROA - [SDR CA970624002](https://openairdocs.org/sdr/CA970624002.md): Supercharger · shaft sheared · Jun 13, 1997 · Braero HS7482B · Cabin Cooling System > (CAN) LH ACCESSORY GEARBOX LOW ON OIL. THE OIL SUPPLY LINE TO THE CABIN SUPERCHARGER WAS BROKEN OFF AT THE FITTING. THE SUPERCHARGER WAS REMOVED, THE QUILL SHAFT WAS FOUND SHEARED AND THE SCROLLS BINDING. THE SUPERCHARGER DRIVE BEARINGS LOCATED ON THE GEARBOX - [SDR CA970203011](https://openairdocs.org/sdr/CA970203011.md): Comb Chamber · broken · Jan 24, 1997 · Braero HS7482B · Turbine Engine Combustion Section > (CAN) DURING INSPECTION THE NOSE CONE OF ONE OF THE COMBUSTION CHAMBERS WAS FOUND BROKEN AWAY FROM THE COMBUSTION CHAMBER BODY. - [SDR CA970115004](https://openairdocs.org/sdr/CA970115004.md): Engine · making metal · Dec 23, 1996 · Braero HS7482B · Engine (Turbine/Turboprop) > (CAN) ENGINE WAS SHUTDOWN DURING APPROACH DUE TO ILLUMINATED OIL PRESSURE WARNING LIGHT. POST FLIGHT INSPECTION FOUND METAL IN THE OIL FILTER. THE ENGINE WAS REMOVED. - [SDR CA961203012](https://openairdocs.org/sdr/CA961203012.md): Bearing · failed · Nov 25, 1996 · Braero HS7482B · Turbine Engine Accessory Drive > (CAN) FORWARD TUNNEL SHAFT BEARING FAILED CAUSING FORWARD END CAP OF SHAFT TO DISCONNECT FROM INPUT SHAFT. SUSPECT BEARING FAILURE ATTRIBUTED T OIL STARVATION; PLUGGED JET AND/OR PUMP FAILURE. GEARBOX SHIPPED FOR TEARDOWN. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'DART5352' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/rolls-royce-dart-535-2/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.