# N406MA: Bell 222B, registration cancelled 2013-02-12

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 12, 2013
- Status when cancelled: Third renewal notice
- Airframe: [Bell 222B](https://openairdocs.org/model/bell-222b) (registry code 1182124)
- Engine: [NONE](https://openairdocs.org/engine/none) (registry code 00000)
- Data sheets: [TCDS H9SW](https://openairdocs.org/tcds/H9SW) (OpenAirDocs)
- Serial number: 47134
- Type of aircraft: Rotorcraft
- Engine type: None
- Certificate issued: August 14, 2008
- Last registry action: August 14, 2008
- Mode S code: A4C3FF
- Owner when cancelled: [Air Methods Corporation](https://openairdocs.org/faa-owner/AIR%20METHODS%20CORPORATION)
- Location: [Englewood, CO](https://openairdocs.org/faa-place/CO/Englewood)
- Owner type: Corporation
- Owner's area on the map: 39.5732° N, 104.8649° W: Placed by OpenAirDocs at the center of ZIP code 80112, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N406MA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=406MA
- Page: https://openairdocs.org/deregistered/N406MA-2013-02-12

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Bell 222B: https://openairdocs.org/model/bell-222b.md

## Service difficulty reports (4)

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

- [SDR N406MA0204](https://openairdocs.org/sdr/N406MA0204), Feb 27, 2004: WIRE. CHAFED. DURING FLIGHT TAIL ROTOR CAUTION LIGHT ILLUMINATED. RETURNED TO BASE. FOUND POWER WIRE TO CHIP DETECTOR WAS FOUND TO HAVE CHAFED THROUGH AND SHORTED. REPAIRED W
- [SDR N406MA](https://openairdocs.org/sdr/N406MA), Feb 18, 2004: DETECTOR. BROKEN. WHILE ENROUTE TO A SCENE CALL, CLIMBING THROUGH 3800 FT EAST OF ROMNA, CA. I NOTICED NR 2 ENGINE OIL TEMP PEGGED ABOVE MAX. TEMP HAD BEEN NORMAL ON LAUNCH AND T
- [SDR HAIW6HR0080](https://openairdocs.org/sdr/HAIW6HR0080), Apr 29, 1997: PUMP. WORN EXCESS. PART IS WORN EXCESSIVELY. PUMP LEAKS AT SHAFT SEAL.
- [SDR HAIW6HR0077](https://openairdocs.org/sdr/HAIW6HR0077), Mar 23, 1997: GENERATOR. ARCED. PART IS ARCED. COMMUTATOR APPEARS TO HAVE BURNED SPOTS. STATIC IS HEARD THRU ALL HEAD SETS. REQUEST WARRANTY REPAIR SINCE THIS UNIT HAS ONLY BEEN IN SERVICE 22.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19990127010989I](https://openairdocs.org/incident/19990127010989I), Jan 27, 1999: Bell 222B (N406MA), Henderson, NV, Minor damage. The pilot was repositioning for takeoff. As he turned the helicopter by ground taxi from a westerly to a northerly heading, the main rotor blades struck the…

## Other aircraft with N406MA

- [Registered now](https://openairdocs.org/aircraft/N406MA): Piper PA-28-181, S/N 2881123, built 2019

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