# N212LA: 1987 Bell 206B, registration cancelled 2018-05-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 30, 2018
- Status when cancelled: Sale reported, canceled
- Airframe: [Bell 206B](https://openairdocs.org/model/bell-206b) (registry code 1181511)
- Engine: [Allison 250-C20 series](https://openairdocs.org/engine/allison-250-c20-series) (registry code 03020)
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW), [TCDS E4CE](https://openairdocs.org/tcds/E4CE) (OpenAirDocs)
- Serial number: 3957
- Year built: 1987
- Type of aircraft: Rotorcraft
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: January 19, 1987
- Last registry action: July 19, 2017
- Mode S code: A1C1EB
- Location: [Show Low, AZ](https://openairdocs.org/faa-place/AZ/Show%20Low)
- Owner type: Individual
- Owner's area on the map: 34.3021° N, 110.0159° W: Placed by OpenAirDocs at the center of ZIP code 85901, within about 9 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N212LA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=212LA
- Page: https://openairdocs.org/deregistered/N212LA-2018-05-30

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 206B: https://openairdocs.org/model/bell-206b.md

## Service difficulty reports (5)

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

- [SDR ULX2004F00007](https://openairdocs.org/sdr/ULX2004F00007), Mar 10, 2004: HOUSING. CRACKED. CRACKED AT DRIVE FLANGE WELD. POSSIBLE CAUSE- AERODYNAMIC AND MECHANICAL FORCES AT DRIVE FLANGE. RECOMMENDATION- USE OF STRONGER BASE MATERIAL AND STRICTER CONT
- [SDR ULX2004F00018](https://openairdocs.org/sdr/ULX2004F00018), Mar 1, 2004: FLYWEIGHT. MALFUNCTIONED. N2 RPM UNSTABLE. WILL NOT HOLD N2 RPM STABILIZED. PROBABLE CAUSE: FLYWHEEL WEIGHT MALFUNCTION.
- [SDR 98ZZZX1266](https://openairdocs.org/sdr/98ZZZX1266), Feb 2, 1998: DOUBLER. CORRODED. FUEL BOOST PUMP MOUNTING FLANGE BECAME DEBONDED ALLOWING THE BOOST PUMPS TO FLEX WITH THE FUEL CELL. REMOVAL OF THE FUEL CELL REVEALED EXTENSIVE CORROSION OF TH
- [SDR 97ZZZX4708](https://openairdocs.org/sdr/97ZZZX4708), Jun 25, 1997: BLADE. BEARING BINDING. ACFT TT: 13,497.8 HOURS. 104.2 HR. TWO NEW T/R BLADES P/N 206-016-201-131, SN CS-2814 AND SN CS-2815 WERE INSTALLED. PILOT'S COMPLAINT ABOUT T/R PEDAL PROBLEM. 
- [SDR 97ZZZX4707](https://openairdocs.org/sdr/97ZZZX4707), Jun 25, 1997: BEARING. BINDING. ACFT TT: 13,497.8 HOURS. 104.2 HR. TWO NEW T/R BLADES P/N 206-016-201-131, SN CS-2814 AND SN CS-2815 WERE INSTALLED. PILOT'S COMPLAINT ABOUT T/R PEDAL PROBLEM. 

## Other aircraft with N212LA

- [Registered now](https://openairdocs.org/aircraft/N212LA): Airbus Helicopters AS350B3, S/N 9919, built 2026

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