N2611

Service difficulty reports · 19

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N2611' AND registry_match = 'registration'
  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 YTRA2016060715801Fuel Control · failedIN THE COURSE OF A PRACTICE AUTOROTATION, THE ENGINE FLAMED OUT WHEN THE THROTTLE WAS ROLLED TO THE IDLE DETENT POSITION.Jun 6, 2016 · N2611 · Bell 206L1 · Fuel Control/Reciprocating EnginesSDR 3HCR03222012Bushing · misinstalledGOVERNOR ALLOWS ENGINE TO OVERSPEED. FAILED SHOP TEST. DIASSEMBLED AND FOUND UNIT IMPROPERLY ASSEMBLED. SPOOL BUSHING ANTI-ROTATION TANG WAS ENGAGED IN LEVER SLOT.Mar 22, 2012 · N2611 · Bell 206L1 · Turbine GovernorSDR YTRA1105401Engine · malfunctionedIN CRUISE FLIGHT THE PILOT REPORTED HIGH FREQUENCY VIBRATION AND WHINING NOISE FROM THE ENGINE COMPARTMENT. THIS WAS FOLLOWED BY AN ENGINE CHIP LIGHT INDICATION AND NOISE AT WHICH POINT THE ENGINE LOST POWER AND PROCEDED TO SHUT DOWN.Feb 22, 2011 · N2611 · Bell 206L1 · Engine (Turbine/Turboprop)SDR YTRA1000702Longeron · crackedCRACKED AFT UPPER LT LONGERON AT TAILBOOM ATTACH POINT.Jan 6, 2010 · N2611 · Bell 206L1 · Rotorcraft Tail BoomSDR ALG2005F00016Sensor · corrodedJUST AFTER TAKEOFF, THE LOW ROTOR CAUTION LIGHT ILLUMINATED. 2 OR 3 SECONDS LATER, THE LOW ROTOR RPM HORN SOUNDED. ROTOR TACH INDICATIONS WERE NORMAL, PILOT RETURNED TO BASE. UPON LANDING, THE MECHANIC REMOVED AND REPLACED BOTH THE LOW ROTOR RPM AND ENGINE Jan 14, 2005 · N2611 · Cessna STC206C · Rotor Drive Indicating SystemSDR ALG2005F00015Sensor · corrodedJUST AFTER TAKEOFF, THE LOW ROTOR CAUTION LIGHT ILLUMINATED. 2 OR 3 SECONDS LATER THE LOW ROTOR RPM HORN SOUNDED. ROTOR TACH INDICATIONS WERE NORMAL, PILOT RETURNED TO BASE. UPON LANDING, THE MECHANIC REMOVED AND REPLACED BOTH THE LOW ROTOR RPM AND ENGINE. Jan 14, 2005 · N2611 · Bell 206L1 · Rotor Drive Indicating SystemSDR ALG2004F00026Bleed Valve · inoperativeWHILE TAKING OFF, HEARD POP AND AIRCRAFT YAWED, SYMPTOMS OF A COMPRESSOR STALL. LANDED STRAIGHT AHEAD AND HAD TOWER CALL AIRLOG OPS. MAINTENANCE REMOVED BLEED VALVE AND INSTALLED SERVICEABLE BLEED VALVE (PN 23073353)(SN FF44236). ALL WORK DONE IAW 206L-1MM May 20, 2004 · N2611 · Cessna STC206C · Compressor Bleed ValveSDR ALG2004F00025Bleed Valve · inoperativeWHILE TAKING OFF IN HMA HEARD POP AND AIRCRAFT YAWED, SYMPTOMS OF A COMPRESSOR STALL. LANDED STRAIGHT AHEAD AND HAD TOWER CALL OPS. MAINTENANCE REMOVED BLEED VALVE AND INSTALLED SERVICEABLE BLEED VALVE PN 23073353 SN FF44236. ALL WORK IAW 206L1MM.May 20, 2004 · N2611 · Bell 206L1 · Compressor Bleed ValveSDR ALGA093984Blade · corrodedFOUND MAIN ROTOR TRAILING EDGE EXTRUSION EXFOLIATED APPROXIMATELY 2.5.Mar 21, 2004 · N2611 · Bell 206L1 · Main Rotor BladesSDR 99ZZZX2651Tube · crackedDURING CRUISE FLIGHT FROM OFFSHORE, PILOT NOTICED N2 DROPPING. LANDING WAS MADE - NO DAMAGE TO AIRCRAFT. DURING TROUBLESHOOTING, FOUND PC LINE FROM ACCUMULATOR TO FUEL CONTROL CRACKED AT FLARE ON POWER CONTROL SIDE CAUSING ENGINE TO SPOOL DOWN. REPLACED LINJun 22, 1999 · N2611 · Bell 206L1 · Engine Fuel DistributionSDR 99ZZZX1247Retainer · brokenUPON TEAR-DOWN OF TRANSMISSION FOR INSPECTION, FOUND SCREEN ASSY FULL ON PLASTIC OR NYLON PIECES. INSPECTED PLANETARY ASSY FOUND 3 EACH GEAR ASSYS WITH NO RETAINERS REMAINING, ONE EACH RETAINER WAS IN PLACE. ONCE REMOVED, IT FELL APART. UPGRADE RETAINERS TO Feb 25, 1999 · N2611 · Bell 206L1 · Main Rotor GearboxSDR 98ZZZX2541Horn · mismanufacturedINSTALLED OVERHAULED T/R HUB AND BLADES ON AIRCRAFT. NOTICED AFTER RIGGING T/R HORNS, P/N 206-011-809-107, THEY WERE CONTACTING T/R HUB, P/N 206-011-810-139. REMOVED AND REPLACED ASSY. INSPECTION OF REMOVED UNITS AND OF UNITS IN STOCK SHOWED THAT MACHINING Jun 9, 1998 · N2611 · Bell 206L1 · Tail Rotor Control SystemSDR 98ZZZX298Drive Link · wornEXCESSIVE PLAY AT TWO PLACES. SEE BELL MM L-3 FIG 62-21. ON TEAR-DOWN, FOUND BEARINGS AND SPACERS WORN BEYOND LIMITS. TOTAL TIME OF PARTS LESS THAN 1,000 HOURS/1 YEAR SINCE REPLACEMENT.Nov 12, 1997 · N2611 · Bell 206L1 · Main Rotor Mast/SwashplateSDR 97ZZZX4972Duplex Bearing · brinelledTHIS IS NR 6 AND NR 7 DUPLEX BEARING CHANGE FOR BRINELLING ON RACES PARTICULARLY THE LOWER INNER RACE. ALL HAVE BEEN CHANGED WITH LESS THAN 100-HOUR TT SINCE NEW.Oct 2, 1997 · N2611 · Bell 206L1 · Main Rotor Mast/SwashplateSDR 96ZZZX6183Blade · bearing wornT/R BLADES REMOVED DUE TO FEATHERING BEARINGS WORN AND EXCESSIVE AXIAL MOVEMENT OF THE BLADES. INSPECTED BLADE FEATHERING BEARINGS PER BELL 206L MM, CH 65-30-00, PG 65-49 PARA 65-62 ITEM 6 AXIAL LOOSENESS EXCEEDED .190 INCHES AT BLADE TIP. BEARINGS REPLACED.Oct 7, 1996 · N2611 · Bell 206L1 · Tail Rotor BladesSDR 96ZZZX6182Blade · bearing wornT/R BLADES REMOVED DUE TO FEATHERING BEARINGS WORN AND EXCESSIVE AXIAL MOVEMENT OF THE BLADES. INSPECTED BLADE FEATHERING BEARINGS PER BELL 206L MM, CH 65-30-00, PG 65-49 PARA 65-62 ITEM 6 AXIAL LOOSENESS EXCEEDED .190 INCHES AT BLADE TIP. BEARINGS REPLACED.Oct 7, 1996 · N2611 · Bell 206L1 · Tail Rotor BladesSDR 96ZZZX2605Bulb · failedON DAILY AIRWORTHY INSPECTION, FOUND STROBE LIGHT BULB BURNED OUT. HAD REPLACED BULB LAST WEEK. CAUSE OF PROBLEM UNKNOWN AT THIS TIME.Apr 25, 1996 · N2611 · Bell 206L1 · Exterior LightingSDR 96ZZZX1417Blade · bearing defectDURING ROUTINE MAINTENANCE, FOUND TAIL ROTOR BLADE INBOARD BEARING CRACKED ON BLADE, SN 452, AND SMALL INDICATION ON INBOARD BEARING, SN 446.Dec 8, 1995 · N2611 · Bell 206L1 · Tail Rotor BladesSDR 96ZZZX1416Blade · bearing defectDURING ROUTINE MAINTENANCE, FOUND TAIL ROTOR BLADE INBOARD BEARING CRACKED ON BLADE, SN 452, AND SMALL INDICATION ON INBOARD BEARING, SN 446.Dec 8, 1995 · N2611 · Bell 206L1 · Tail Rotor Blades
Back to N2611