# N152CS: 2014 Johnson Carl S TITAN MUSTANG T-51

- Status: Valid registration
- Airframe: [Johnson Carl S TITAN MUSTANG T-51](https://openairdocs.org/model/johnson-carl-s-titan-mustang-t-51) (registry code 056320N, 2 seats)
- Engine: [Honda J35A](https://openairdocs.org/engine/honda-j35a) (registry code 33801)
- Serial number: M09HV6SOHK0152
- Year built: 2014
- Type: Fixed wing single engine
- Engine type: Reciprocating
- Kit: Titan Aircraft T-51 MUSTANG
- Airworthiness: Experimental, amateur built
- Airworthiness date: February 14, 2014
- Certificate issued: June 15, 2015
- Expires: June 30, 2028
- Mode S code: A0D1E0
- Registered owners: [Johnson Carl S](https://openairdocs.org/faa-owner/JOHNSON%20CARL%20S), [Johnson Ross P](https://openairdocs.org/faa-owner/JOHNSON%20ROSS%20P)
- Location: [Sidney, IA](https://openairdocs.org/faa-place/IA/Sidney)
- Owner type: Partnership
- Owner's area on the map: 40.7725° N, 95.6231° W: Placed by OpenAirDocs at the center of ZIP code 51652, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=152CS
- Page: https://openairdocs.org/aircraft/N152CS

From the FAA registry file of October 21, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Johnson Carl S TITAN MUSTANG T-51)

None in force.

### Matched by engine (Honda J35A)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N152CS.

## FAA accident and incident reports

None matched to N152CS.

## Service difficulty reports (3)

As reported by operators and repair stations.

- [SDR 011607N152CS1](https://openairdocs.org/sdr/011607N152CS1), Jan 14, 2007: ACTUATOR. FAULTY. AFTER TAKE-OFF FROM SAT, CREW NOTICED POWER BRAKE FAIL AND POWER BRAKE PRESS LOW ANNUNCIATORS. CREW PERFORMED AFM PROCEDURE CHECKS FOR THIS INDICATION WITH NO E
- [SDR 120706N152CS1](https://openairdocs.org/sdr/120706N152CS1), Dec 7, 2006: CONNECTOR. LOOSE. AFTER TAKEOFF, THE POWER BRAKE LOW PRESSURE AND ANTI-SKID WARNING INDICATION LIGHTS ILLUMINATED. THE AIRCRAFT DIVERTED AND DECLARED AN EMERGENCY. UPON LANDING, 
- [SDR 032805N152CS1](https://openairdocs.org/sdr/032805N152CS1), Mar 28, 2005: TRIM SCALE. BROKEN. UPON ROTATION AIRCRAFT REQUIRED EXCESSIVE BACK PRESSURE ON YOKE TO MAINTAIN CLIMB PITCH AND UNABLE TO CLIMB TO ASSIGNED ALTITUDE. DECLARED EMERGENCY AND RETURNE

## Related

- Other Johnson Carl S TITAN MUSTANG T-51 aircraft: https://openairdocs.org/model/johnson-carl-s-titan-mustang-t-51/aircraft.md
- STCs for the Johnson Carl S TITAN MUSTANG T-51: https://openairdocs.org/model/johnson-carl-s-titan-mustang-t-51/stcs.md
- The Honda J35A engine: https://openairdocs.org/engine/honda-j35a.md

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