# N101JB: 1966 Cessna 310K, registration cancelled 2018-03-16

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 16, 2018
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Cessna 310K](https://openairdocs.org/model/cessna-310k) (registry code 2074228)
- Engine: [Continental I0-470 series](https://openairdocs.org/engine/continental-i0-470-series) (registry code 17027)
- Data sheets: [TCDS 3A10](https://openairdocs.org/tcds/3A10) (OpenAirDocs)
- Serial number: 310K0110
- Year built: 1966
- Type of aircraft: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: February 2, 1976
- Certificate issued: April 15, 2014
- Last registry action: April 15, 2014
- Mode S code: A00935
- Owners when cancelled: [Lakepoint Aviation II LLC](https://openairdocs.org/faa-owner/LAKEPOINT%20AVIATION%20II%20LLC), [Cornejo Aviation LLC](https://openairdocs.org/faa-owner/CORNEJO%20AVIATION%20LLC)
- Location: [Augusta, KS](https://openairdocs.org/faa-place/KS/Augusta)
- Owner type: Co-owned
- Owner's area on the map: 37.6554° N, 96.9760° W: Placed by OpenAirDocs at the center of ZIP code 67010, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N101JB
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=101JB
- Page: https://openairdocs.org/deregistered/N101JB-2018-03-16

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 Cessna 310K: https://openairdocs.org/model/cessna-310k.md

## Service difficulty reports (3)

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

- [SDR 2014FA0000670](https://openairdocs.org/sdr/2014FA0000670), Aug 27, 2014: THROTTLE CABLE. FAILED. LEFT THROTTLE CABLE SEPARATED FROM STATIONARY SWEDGE IN THE ENGINE COMPARTMENT REDUCING ENGINE POWER DURING ROTATION PHASE OF A TOUCH AND GO PROCEDURE. ACFT HAD
- [SDR 20010413CW006](https://openairdocs.org/sdr/20010413CW006), Mar 21, 2001: BULKHEAD. CRACKED. DURING REPLACEMENT OF AIRCRAFT HEATER, DUCTING MECHANIC NOTICED THE RIGHT BULKHEAD AT STA 29.93 UNDER HEATER WAS CRACKED. REMOVED HEATER TO GAIN ACCESS TO BULKH
- [SDR 20010413CW005](https://openairdocs.org/sdr/20010413CW005), Mar 21, 2001: BULKHEAD. CRACKED. DURING REPLACEMENT OF AIRCRAFT HEATER DUCTING, MECHANIC NOTICED THE RIGHT BULKHEAD AT STA 29.93 UNDER HEATER WAS CRACKED. ALSO CHECKED LEFT SIDE BULKHEAD AT STA

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB CEN14LA461](https://openairdocs.org/ntsb/CEN14LA461), Aug 27, 2014: Cessna 310K (N101JB), El Dorado, KS, substantial damage. Probable cause: A fatigue failure of the left engine’s throttle cable, which resulted in the loss of left engine power.

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