# Service difficulty reports: N430CV, cancelled Jul 22, 2013

A list on [N430CV, cancelled Jul 22, 2013](https://openairdocs.org/deregistered/N430CV-2013-07-22.md).

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

Page 1 of 2 · 73 reports

- [SDR AC2A117358](https://openairdocs.org/sdr/AC2A117358.md): Hmu · malfunctioned · Sep 12, 2007 · N430CV · Bell 430 · Fuel Control/Turbine Engines
  > ENGINE STARTING HOT.
- [SDR AC2A114642](https://openairdocs.org/sdr/AC2A114642.md): Battery · inoperative · Mar 21, 2007 · N430CV · Bell 430 · Battery/Charger System
  > INSPECTED BATTERY, BATTERY WOULD NOT ACCEPT CHARGE, BATERY OUTPUT VOLTAGE IS 5 VDC.
- [SDR AC2A109121](https://openairdocs.org/sdr/AC2A109121.md): Stud · cracked · May 7, 2006 · N430CV · Bell 430 · Main Rotor Head
  > DURING AN INSPECTION FOUND ALL 4 DOWN STOPS CRACKED/ REPLACED ALL FOUR DOWN STOPS.
- [SDR AC2A099729](https://openairdocs.org/sdr/AC2A099729.md): Battery · weak · Feb 21, 2005 · N430CV · Bell 430 · Battery/Charger System
  > BATTERY IS WEAK. CHARGED AND TESTED. FAILED FIRST CHECK. CHARGED WITH CONDITIONING CHARGE AND RETESTED, FAILED SECOND CHECK. RECHARGED BATTERY AND APPLIED FOR WARRANTY, S/O NR S3034.
- [SDR AC2R099709](https://openairdocs.org/sdr/AC2R099709.md): Battery · failed · Oct 30, 2004 · N430CV · Bell 430 · Battery/Charger System
  > PART FAILED TEST TWO CHARGE AND CAPACITY TESTS. (LESS THAN 25 MINIUTES). REPLACED BATTERY AND BOOSTED GENERATOR VOLTAGE TO 28.5 VDC.
- [SDR AC2A096517](https://openairdocs.org/sdr/AC2A096517.md): Battery Pack · failed · Jul 14, 2004 · N430CV · Bell 430 · Battery/Charger System
  > BATTERY PACK FAILED CAPACITY TEST. REPLACED BATTERY.
- [SDR AC2A096516](https://openairdocs.org/sdr/AC2A096516.md): Housing · broken · Jul 14, 2004 · N430CV · Bell 430 · Emergency Lighting
  > HOUSING IS BROKEN. AUTOMATIC ON FUNCTION IS INOPERATIVE. ONE CELL IS DEAD. REPLACED ASSEMBLY WITH A NEW PART. TOO EXPENSIVE TO REPAIR OLD UNIT.
- [SDR AC2A094950](https://openairdocs.org/sdr/AC2A094950.md): Turbine · seized · Apr 10, 2004 · N430CV · Bell 430 · Cabin Cooling System
  > TURBINE IS SEIZED.
- [SDR AC2A094949](https://openairdocs.org/sdr/AC2A094949.md): Guide · corroded · Apr 10, 2004 · N430CV · Bell 430 · Windshield/Door Rain/Ice Removal
  > PIVOT POINT OF GUIDE ARM CORRODED SWELD AND BROKE.
- [SDR AC2A094948](https://openairdocs.org/sdr/AC2A094948.md): Guide Arm · corroded · Apr 10, 2004 · N430CV · Bell 430 · Ice/Rain Protection System
  > PIVOT POINT OF GUIDE CORRODED, SWOLLEN AND BROKE.
- [SDR AC2A092339](https://openairdocs.org/sdr/AC2A092339.md): Cam Follower · broken · Jan 8, 2004 · N430CV · Bell 430 · Passenger/Crew Doors
  > ROLLER WAS BROKEN. REPLACED WITH NEW ROLLER.
- [SDR AC2A092338](https://openairdocs.org/sdr/AC2A092338.md): Disk · worn · Jan 8, 2004 · N430CV · Bell 430 · Main Rotor Brake
  > BRAKE DISC IS WORN. REPLACED WITH SERVICEABLE PART.
- [SDR AC2A092337](https://openairdocs.org/sdr/AC2A092337.md): Drive Shaft · corroded · Jan 8, 2004 · N430CV · Bell 430 · Tail Rotor Drive Shaft
  > TAIL DRIVESHAFT IS DISCOLORED AND PAINT IS BLISTERED FROM HEAT, CORROSION PIT FORMING AT BLISTERS. REPLACED WITH SERVICEABLE DRIVESHAFT.
- [SDR AC2A092336](https://openairdocs.org/sdr/AC2A092336.md): Stud · broken · Jan 8, 2004 · N430CV · Bell 430 · Tail Rotor Gearbox
  > GEARBOX HAD TWO BROKEN MOUNTING STUDS. REMOVED GEARBOX FROM AIRCRAFT AND REPLACED STUDS, CHECKED GEARBOX PER MANUFACTURERS LETTER AND RE-INSTALLED GEARBOX.
- [SDR AC2A092335](https://openairdocs.org/sdr/AC2A092335.md): Stud · cracked · Jan 8, 2004 · N430CV · Bell 430 · Main Rotor Head
  > STUD IS CRACKED WHERE THREADED PORTION TRANSITIONS INTO FLANGE. REPLACED WITH NEW STUDS.
- [SDR AC2A086265](https://openairdocs.org/sdr/AC2A086265.md): Hydromech Unit · leaking · Apr 10, 2003 · N430CV · Bell 430 · Fuel Control/Turbine Engines
  > REMOVED FOR HMU BACKLASH CHECK. FOUND TO BE LEAKING FUEL FROM DRIVE SPLINE SEAL. REPLACED HMU.
- [SDR AC2A086261](https://openairdocs.org/sdr/AC2A086261.md): Pressure Switch · false indication · Apr 9, 2003 · N430CV · Bell 430 · Main Rotor Gearbox
  > WHEN AIRCRAFT IS FLOWN THROUGH RAIN THE TRANSMISSON OIL, RED WARNING LIGHT COMES ON. THE LIGHT GOES OUT SHORTLY AFTER AIRCRAFT IS NOT IN RAIN. THE PRESSURE AND TEMPERATURE ARE IN THE NORMAL RANGE WHEN THE LIGHT COMES ON. CLEANED TRANSMISSION OIL PRESSURE SW
- [SDR AC2A082961](https://openairdocs.org/sdr/AC2A082961.md): Lens · cracked · Dec 22, 2002 · N430CV · Bell 430 · Exterior Lighting
  > TAILBOOM STROBE LENS IS CRACKED. REPLACED LENS.
- [SDR AC2A081584](https://openairdocs.org/sdr/AC2A081584.md): Blade · cracked · Nov 30, 2002 · N430CV · Bell 430 · Main Rotor Blades
  > LEADING EDGE ABRASION STRIP IS CRACKED CHORDWISE, ABOUT MIDWAY DOWN BLADE. REPLACED WITH NEW SERVICEABLE MAIN ROTOR BLADE.
- [SDR AC2A081583](https://openairdocs.org/sdr/AC2A081583.md): Fitting · broken · Nov 30, 2002 · N430CV · Bell 430 · Rotorcraft Tail Boom
  > ONE OF THE EARS BROKE OFF THE FITTING. REPLACED WITH SERVICEABLE FITTING ASSEMBLY.
- [SDR AC2A081582](https://openairdocs.org/sdr/AC2A081582.md): Crosstube · corroded · Nov 30, 2002 · N430CV · Bell 430 · Main Landing Gear Strut/Axle/Truck
  > CORROSION ON AFT CROSSTUBE, RIGHT HAND SIDE JUST OUTBOARD OF CLAMP. REPLACED WITH SERVICEABLE CROSSTUBE.
- [SDR AC2A081581](https://openairdocs.org/sdr/AC2A081581.md): Support · cracked · Nov 30, 2002 · N430CV · Bell 430 · Main Landing Gear
  > PART IS CRACKED. REPLACED WITH SERVICEABLE FITTING ASSEMBLY.
- [SDR AC2A081580](https://openairdocs.org/sdr/AC2A081580.md): Controller · failed · Nov 30, 2002 · N430CV · Bell 430 · Exterior Lighting
  > SEARCH LIGHT WILL NOT STOW. REPLACED WITH SERVICEABLE SEARCH LIGHT ASSEMBLY.
- [SDR AC2A081231](https://openairdocs.org/sdr/AC2A081231.md): Display · defective · Oct 19, 2002 · N430CV · Bell 430 · Integrated Flight System
  > PART IS DEFECTIVE. DURING CRUISE FLIGHT PILOT DETECTED A STRONG BURNING ODOR, ACCOMPANIED WITH A "FAIL" INDICATION ON THE EADI. FOLLOWING EMERGENCY PROCEDURES, THE ODOR STOPPED WHEN THE EFIS WAS TURNED OFF. PART WAS REPLACED WITH SERVICEABLE UNIT.
- [SDR AC2A0000342](https://openairdocs.org/sdr/AC2A0000342.md): Cushion · broken · Feb 21, 2002 · N430CV · Bell 430 · Passenger Compartment Equipment
  > ENERGY ABSORBING MATERIAL BROKEN. REPLACED WITH NEW SERVICEABLE SEAT.
- [SDR AC2A0000337](https://openairdocs.org/sdr/AC2A0000337.md): Ring Assembly · loose · Feb 19, 2002 · N430CV · Bell 430 · Air Distribution System
  > GUIDE RINGS SNAP LOOSE PREVENTING PROPER OPERATION. SPRING RING LOSES TENSION PREVENTING PROPER OPERATION. REMOVE AND REPLACED.
- [SDR AC2A077542](https://openairdocs.org/sdr/AC2A077542.md): Bearing · cracked · Dec 26, 2001 · N430CV · Bell 430 · Tail Rotor Blades
  > TAIL ROTOR BLADE BEARINGS WERE CRACKED. REPLACED TWO BEARINGS.
- [SDR AC2A077541](https://openairdocs.org/sdr/AC2A077541.md): Arm · broken · Dec 26, 2001 · N430CV · Bell 430 · Windshield/Door Rain/Ice Removal
  > LOWER MOUNTING POINT BROKEN. THE MATERIAL THAT THIS PART IS MADE OF IS VERY SUSEPTIBLE TO CORROSION. CORROSION CAUSED THIS PART TO FAIL. UPPER ROD END CORRODED VERY EASILY ALSO. REPLACED WITH NEW PART.
- [SDR AC2A0000298](https://openairdocs.org/sdr/AC2A0000298.md): Arm · corroded · Dec 12, 2001 · N430CV · Bell 430 · Windshield/Door Rain/Ice Removal
  > GUIDE ARM ASSEMBLY, LOWER MOUNTING POINT BROKEN. THE MATERIAL THAT THIS PART IS MADE OF IS VERY SUSEPTIBLE TO CORROSION. CORROSION CAUSED THIS PART TO FAIL. UPPER ROD END CORRODED VERY EASILY ALSO. REPLACED WITH NEW PART.
- [SDR AC2A077540](https://openairdocs.org/sdr/AC2A077540.md): Servo · malfunctioned · Dec 11, 2001 · N430CV · Bell 430 · Rotorcraft Servo System
  > WHEN FD IS COUPLED IN HDG & ALT THE A/C GOES INTO A CLIMBING RIGHT TURN WITH FULL LEFT PEDAL APPLIED. REPLACED WITH NEW YAW SERVO.
- [SDR AC2A077539](https://openairdocs.org/sdr/AC2A077539.md): Tube · chafed · Dec 11, 2001 · N430CV · Bell 430 · Engine Bleed Air System
  > ENGINE COWL ASSY P/N: 430-061-804-101 FORWARD HINGE P/N: 230-061-808-101 IS RUBBING ON BLEED AIR TUBE P/N: 23056648 WHEN COWLING IS OPENED. REPLACED TUBE. PROBLEM WILL CONTINUE DUE TO DESIGN OF COWLING HINGE.
- [SDR AC2A0000297](https://openairdocs.org/sdr/AC2A0000297.md): Servo · failed · Dec 7, 2001 · N430CV · Bell 430 · Rotorcraft Servo System
  > YAW SERVO, WHEN FD IS COUPLED IN HDG AND ALT THE AIRCRAFT GOES INTO A CLIMBING RIGHT TURN WITH FULL LEFT PEDAL APPLIED. REPLACED WITH NEW YAW SERVO.
- [SDR AC2A077537](https://openairdocs.org/sdr/AC2A077537.md): Arm · broken · Dec 5, 2001 · N430CV · Bell 430 · Windshield/Door Rain/Ice Removal
  > WINDSHIELD WIPER GUIDE ARM IS BROKEN. REPLACED WITH NEW PART.
- [SDR AC2A0000294](https://openairdocs.org/sdr/AC2A0000294.md): Guide · broken · Nov 30, 2001 · N430CV · Bell 430 · Windshield/Door Rain/Ice Removal
  > GUIDE ARM ASSEMBLY IS BROKEN. REPLACED WITH NEW PART.
- [SDR AC2A0000302](https://openairdocs.org/sdr/AC2A0000302.md): Bearing · failed · Nov 27, 2001 · N430CV · Bell 430 · Tail Rotor Head
  > TAIL ROTOR BEARING, REPLACE BEARINGS ON TAIL ROTOR.
- [SDR AC2A0000299](https://openairdocs.org/sdr/AC2A0000299.md): Bearing · cracked · Nov 27, 2001 · N430CV · Bell 430 · Tail Rotor Blades
  > TAIL ROTOR BLADE BEARINGS WERE CRACKED. REMOVED AND REPLACED TWO BEARINGS.
- [SDR AC22002F00000](https://openairdocs.org/sdr/AC22002F00000.md): Tube · chafed · Nov 24, 2001 · N430CV · Bell 430 · Engine Bleed Air System
  > TUBE ASSEMBLY, ENGINE COWL ASSY, FORWARD HINGE IS RUBBING ON BLEED AIR TUBE WHEN COWLING IS OPENED. REPLACED TUBE: PROBLEM WILL CONTINUE DUE TO DESIGN OF COWLING HINGE.
- [SDR AC22001F00008](https://openairdocs.org/sdr/AC22001F00008.md): Switch · failed · Oct 25, 2001 · N430CV · Bell 430 · Integrated Flight System
  > EADI (TOP TUBE) WOULD NOT SHUT OFF. TUBE WOULD ILLUMINATE WHEN BATTERY SWITCH PLACED ON. REPLACED SWITCH. CURED PROBLEM.
- [SDR AC2A077050](https://openairdocs.org/sdr/AC2A077050.md): Solenoid · stuck · Oct 15, 2001 · N430CV · Bell 430 · Air Distribution System
  > DIVERTER VALVE NOT OPENING OR CLOSING. TOO MUCH COLD AIR COMING OUT OF LOWER VENTS. REPLACED WITH NEW SOLENOID. IT FIXED PROBLEM.
- [SDR AC22001F00000](https://openairdocs.org/sdr/AC22001F00000.md): Solenoid · failed · Oct 5, 2001 · N430CV · Bell 430 · Air Distribution System
  > DIVERTER VALVE NOT OPENING OR CLOSING. TOO MUCH COLD AIR COMING OUT OF LOWER VENTS. REPLACED WITH NEW SOLENOID. IT FIXED PROBLEM.
- [SDR AC2A076117](https://openairdocs.org/sdr/AC2A076117.md): Cushion · damaged · Oct 1, 2001 · N430CV · Bell 430 · Passenger Compartment Equipment
  > FOAM WAS BUSTED AND SEPARATED FROM FRAME. REPLACED SEAT CUSHION.
- [SDR AC2A076115](https://openairdocs.org/sdr/AC2A076115.md): Pressure Switch · inoperative · Sep 19, 2001 · N430CV · Bell 430 · Engine/Transmission Coupling
  > PRESSURE SWITCH IS INOPERABLE. REPLACED WITH NEW SWITCH.
- [SDR AC2A076114](https://openairdocs.org/sdr/AC2A076114.md): Seat Belt · damaged · Sep 19, 2001 · N430CV · Bell 430 · Flight Compartment Equipment
  > SEAT BELT WAS UNTHREADING. REPLACED WITH NEW SEAT BELT.
- [SDR AC2A076113](https://openairdocs.org/sdr/AC2A076113.md): Frame · cracked · Sep 18, 2001 · N430CV · Bell 430 · Nacelle/Pylon, Frame/Spar/Rib
  > CRACKS IN FRAME. REMOVED AND REPLACED FRAME ASSY.
- [SDR AC2A076112](https://openairdocs.org/sdr/AC2A076112.md): Strap · cracked · Sep 18, 2001 · N430CV · Bell 430 · Miscellaneous Hardware
  > CRACKED IN BENT RADIUS. REMOVED AND REPLACED
- [SDR AC2A076111](https://openairdocs.org/sdr/AC2A076111.md): Receptacle · worn · Sep 17, 2001 · N430CV · Bell 430 · Miscellaneous Hardware
  > PREMATURE WEAR R&R RECEPTICLE
- [SDR AC2A076110](https://openairdocs.org/sdr/AC2A076110.md): Clip · cracked · Sep 17, 2001 · N430CV · Bell 430 · Main Rotor Gearbox
  > PART IS CRACKED. SOME REMOVED TO REDUCE RISK OF ENG. F.O.D. R & R CLIPS
- [SDR AC2A075853](https://openairdocs.org/sdr/AC2A075853.md): Seal · deformed · Sep 5, 2001 · N430CV · Bell 430 · Engine/Transmission Coupling
  > DURING 600 HOUR INSPECTION, DISASSY. COUPLING FOUND SEAL DEFORMED. REPLACED SEAL.
- [SDR AC2A075852](https://openairdocs.org/sdr/AC2A075852.md): Bearing · cracked · Sep 5, 2001 · N430CV · Bell 430 · Tail Rotor Head
  > CRACKED BEARINGS. REPLACED THE FOUR BEARINGS.
- [SDR AC2A075849](https://openairdocs.org/sdr/AC2A075849.md): Bearing · brinelled · Sep 5, 2001 · N430CV · Bell 430 · Tail Rotor Gearbox
  > INNER RACE WORN. IT WAS BRINNELING. REPLACED WITH NEW.

Next page: https://openairdocs.org/deregistered/N430CV-2013-07-22/reports.md?page=2

## 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 = 'N430CV' AND deregistration_id = 'N430CV-2013-07-22'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N430CV-2013-07-22/reports

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