Aircraft Description
N67JM is a 1973 Cessna 177B, a single-engine reciprocating (piston) aircraft registered to Eck Gary A in Osceola, IN. This aircraft holds a standard airworthiness certificate issued by the Federal Aviation Administration on May 31, 1973. The registration certificate was issued on April 20, 2012. The registration is set to expire on April 30, 2028. Powered by a Lycoming O&VO-360 SER engine producing 180 horsepower, N67JM is. The aircraft's Mode S transponder code is A8DA33 (hex), used for ADS-B identification and flight tracking. N67JM was last tracked by AviatorDB at coordinates 41.6663, -86.0305 on March 14, 2026. The FAA registry record for N67JM was last updated on May 5, 2023. AviatorDB monitors aircraft positions through ADS-B surveillance data and updates records as new position data is received.
The Cessna 177 Cardinal was an ambitious four-seat general aviation aircraft designed to replace the popular Cessna 172 Skyhawk with modern features including a cantilever wing and all-flying stabilator. First flown in 1967 and introduced in 1968, it was a high-wing single-engine monoplane that seated four occupants with improved visibility and comfort over its predecessor. Spanning over 35 feet with sleek aerodynamic lines, the Cardinal suffered from initial underpowering that hampered its commercial success. Manufactured by Cessna Aircraft Company from 1968 to 1978, approximately 4,295 units were produced across all variants. AviatorDB tracks 80,556 Cessna aircraft currently registered in the FAA database. The ICAO type designator for this aircraft model is C177.
AviatorDB has found no NTSB accident or incident reports involving N67JM. AviatorDB cross-references all FAA registration data with NTSB accident and incident reports, providing a comprehensive safety overview for every registered aircraft in the United States.
Registered Owner
Powerplant & Avionics
NTSB Accident History (1)
| Date | NTSB # | Damage | Highest Injury | Probable Cause |
|---|---|---|---|---|
| Aug 28, 1999 | FTW99LA241 | Destroyed | Minor | The pilot's improper use of the emergency fuel boost pump, which resulted in excessive fuel flow to the engine and subsequent total loss of left engine power. Factor's were the high density altitude, the pilot exceeding the airplane's weight and balance, the partial loss of left engine power as a result of the faulty magnetos, and the pilot's inadequate preflight inspection by not performing an engine run-up. |
Additional Details
Last Known Position
Data Source
Data provided by the US Federal Aviation Administration. View on FAA.gov
Last updated: 2026-05-01 01:32:20 UTC