# Service difficulty reports: N2611

A list on [N2611](https://openairdocs.org/aircraft/N2611.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR YTRA2016060715801](https://openairdocs.org/sdr/YTRA2016060715801.md): Fuel Control · failed · Jun 6, 2016 · N2611 · Bell 206L1 · Fuel Control/Reciprocating Engines
  > IN THE COURSE OF A PRACTICE AUTOROTATION, THE ENGINE FLAMED OUT WHEN THE THROTTLE WAS ROLLED TO THE IDLE DETENT POSITION.
- [SDR 3HCR03222012](https://openairdocs.org/sdr/3HCR03222012.md): Bushing · misinstalled · Mar 22, 2012 · N2611 · Bell 206L1 · Turbine Governor
  > GOVERNOR ALLOWS ENGINE TO OVERSPEED. FAILED SHOP TEST. DIASSEMBLED AND FOUND UNIT IMPROPERLY ASSEMBLED. SPOOL BUSHING ANTI-ROTATION TANG WAS ENGAGED IN LEVER SLOT.
- [SDR YTRA1105401](https://openairdocs.org/sdr/YTRA1105401.md): Engine · malfunctioned · Feb 22, 2011 · N2611 · Bell 206L1 · Engine (Turbine/Turboprop)
  > IN 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.
- [SDR YTRA1000702](https://openairdocs.org/sdr/YTRA1000702.md): Longeron · cracked · Jan 6, 2010 · N2611 · Bell 206L1 · Rotorcraft Tail Boom
  > CRACKED AFT UPPER LT LONGERON AT TAILBOOM ATTACH POINT.
- [SDR ALG2005F00016](https://openairdocs.org/sdr/ALG2005F00016.md): Sensor · corroded · Jan 14, 2005 · N2611 · Cessna STC206C · Rotor Drive Indicating System
  > JUST 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
- [SDR ALG2005F00015](https://openairdocs.org/sdr/ALG2005F00015.md): Sensor · corroded · Jan 14, 2005 · N2611 · Bell 206L1 · Rotor Drive Indicating System
  > JUST 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.
- [SDR ALG2004F00026](https://openairdocs.org/sdr/ALG2004F00026.md): Bleed Valve · inoperative · May 20, 2004 · N2611 · Cessna STC206C · Compressor Bleed Valve
  > WHILE 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
- [SDR ALG2004F00025](https://openairdocs.org/sdr/ALG2004F00025.md): Bleed Valve · inoperative · May 20, 2004 · N2611 · Bell 206L1 · Compressor Bleed Valve
  > WHILE 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.
- [SDR ALGA093984](https://openairdocs.org/sdr/ALGA093984.md): Blade · corroded · Mar 21, 2004 · N2611 · Bell 206L1 · Main Rotor Blades
  > FOUND MAIN ROTOR TRAILING EDGE EXTRUSION EXFOLIATED APPROXIMATELY 2.5.
- [SDR 99ZZZX2651](https://openairdocs.org/sdr/99ZZZX2651.md): Tube · cracked · Jun 22, 1999 · N2611 · Bell 206L1 · Engine Fuel Distribution
  > DURING 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 LIN
- [SDR 99ZZZX1247](https://openairdocs.org/sdr/99ZZZX1247.md): Retainer · broken · Feb 25, 1999 · N2611 · Bell 206L1 · Main Rotor Gearbox
  > UPON 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
- [SDR 98ZZZX2541](https://openairdocs.org/sdr/98ZZZX2541.md): Horn · mismanufactured · Jun 9, 1998 · N2611 · Bell 206L1 · Tail Rotor Control System
  > INSTALLED 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
- [SDR 98ZZZX298](https://openairdocs.org/sdr/98ZZZX298.md): Drive Link · worn · Nov 12, 1997 · N2611 · Bell 206L1 · Main Rotor Mast/Swashplate
  > EXCESSIVE 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.
- [SDR 97ZZZX4972](https://openairdocs.org/sdr/97ZZZX4972.md): Duplex Bearing · brinelled · Oct 2, 1997 · N2611 · Bell 206L1 · Main Rotor Mast/Swashplate
  > THIS 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.
- [SDR 96ZZZX6183](https://openairdocs.org/sdr/96ZZZX6183.md): Blade · bearing worn · Oct 7, 1996 · N2611 · Bell 206L1 · Tail Rotor Blades
  > T/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.
- [SDR 96ZZZX6182](https://openairdocs.org/sdr/96ZZZX6182.md): Blade · bearing worn · Oct 7, 1996 · N2611 · Bell 206L1 · Tail Rotor Blades
  > T/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.
- [SDR 96ZZZX2605](https://openairdocs.org/sdr/96ZZZX2605.md): Bulb · failed · Apr 25, 1996 · N2611 · Bell 206L1 · Exterior Lighting
  > ON DAILY AIRWORTHY INSPECTION, FOUND STROBE LIGHT BULB BURNED OUT. HAD REPLACED BULB LAST WEEK. CAUSE OF PROBLEM UNKNOWN AT THIS TIME.
- [SDR 96ZZZX1417](https://openairdocs.org/sdr/96ZZZX1417.md): Blade · bearing defect · Dec 8, 1995 · N2611 · Bell 206L1 · Tail Rotor Blades
  > DURING ROUTINE MAINTENANCE, FOUND TAIL ROTOR BLADE INBOARD BEARING CRACKED ON BLADE, SN 452, AND SMALL INDICATION ON INBOARD BEARING, SN 446.
- [SDR 96ZZZX1416](https://openairdocs.org/sdr/96ZZZX1416.md): Blade · bearing defect · Dec 8, 1995 · N2611 · Bell 206L1 · Tail Rotor Blades
  > DURING ROUTINE MAINTENANCE, FOUND TAIL ROTOR BLADE INBOARD BEARING CRACKED ON BLADE, SN 452, AND SMALL INDICATION ON INBOARD BEARING, SN 446.

## 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 n_number = 'N2611' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N2611/reports

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