# Beech C-12C

- Type: Aircraft model (FAA registry)
- Registry code: 1152903
- Manufacturer (registry): BEECH
- Model: C-12C
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 15
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Registered aircraft: 3
- Page: https://openairdocs.org/model/beech-c-12c

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft (3)

- [N200NY](https://openairdocs.org/aircraft/N200NY): [New York State Police](https://openairdocs.org/faa-owner/NEW%20YORK%20STATE%20POLICE), [Latham, NY](https://openairdocs.org/faa-place/NY/Latham), built 1976, S/N BC-25
- [N225LH](https://openairdocs.org/aircraft/N225LH): [Alabama Law Enforcement Agency](https://openairdocs.org/faa-owner/ALABAMA%20LAW%20ENFORCEMENT%20AGENCY), [Montgomery, AL](https://openairdocs.org/faa-place/AL/Montgomery), S/N 76-22557
- [N851EM](https://openairdocs.org/aircraft/N851EM): [Los Angeles Police Department](https://openairdocs.org/faa-owner/LOS%20ANGELES%20POLICE%20DEPARTMENT), [Los Angeles, CA](https://openairdocs.org/faa-place/CA/Los%20Angeles), built 1976, S/N 73-22259

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports (2)

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

- [Incident 19971031036639I](https://openairdocs.org/incident/19971031036639I), Oct 31, 1997: Beech C12C (N200NY), Rochester, NY. Smoke in acft. Landed roc.
- [Incident 19840516028239I](https://openairdocs.org/incident/19840516028239I), May 16, 1984: Beech 200BEECH (N200NY), Ronkomkoma, NY. First officer suffered a uncontrollable medical problem while making the takeoff. Captain aborted the takeoff.

## Service difficulty reports (6)

As reported by operators and repair stations, by the model named in the report.

- [SDR USAR201408070005](https://openairdocs.org/sdr/USAR201408070005), Aug 1, 2014: MOUNT. FRACTURED. ENGINE MOUNT TRUSS FRACTURED ON THE UPPER LT AFT LEG OF THE TRUSS. THE FRACTURE IS AT THE TUBING DRAIN HOLE RIVET PLUG. NO PREVIOUS REPAIRS OR ALTERATIONS ARE N
- [SDR 2009FA0001037](https://openairdocs.org/sdr/2009FA0001037), Feb 5, 2009: COMPUTER. MALFUNCTIONED. A NEW AUTOPILOT SYS WAS INSTALLED ON 2/5/09 AT ACTT 15821.5. PERFORMANCE OF AUTOPILOT WHICH IS CERTIFIED FOR CATEGORY 1 APPROACHES IS VERY POOR AND ERRATIC. AUT
- [SDR B3OR2003004](https://openairdocs.org/sdr/B3OR2003004), Jun 5, 2003: PITCH HORN. CORRODED. DURING A 15 DAY CORROSION INSPECTION, A MECHANIC NOTICED "PAINT BUBBLING" ON THE LT ELEVATOR CONTROL PITCH HORN. UPON FURTHER INVESTIGATION BY SCRAPING-OFF THE 
- [SDR 2](https://openairdocs.org/sdr/2), Jul 27, 2001: ACTUATOR. DAMAGED. DURING A LANDING GEAR RETRACTION CHECK THE L/H LANDING GEAR WHENT FROM THE UP POSITION TO THE DOWN AND LOCK POSITION BY OT SELF. AFTER FURTHER INVESTIGATION FOU
- [SDR B3OR20010003](https://openairdocs.org/sdr/B3OR20010003), Jan 30, 2001: SERVO. BINDING. DURING A FLIGHT, THE PILOT EXPERIENCED SLUGGISH ELEVATOR CONTROL WHEEL MOVEMENT. ELEVATOR CONTROL WOULD MOVE FREELY IN NOSE UP DIRECTION BUT THE MOVEMENT IN THE
- [SDR 99ZZZX3927](https://openairdocs.org/sdr/99ZZZX3927), Sep 29, 1999: CASE. CRACKED. FLOW DIVIDERS WERE BEING SWAPPED TO TROUBLESHOOT STARTING PROBLEM AND A CRACK WAS NOTICED AT THE WELD AREA OF THE FLOW DIVIDER/FUEL NOZZLE MOUNTING BOSS. WHEN T

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