We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type data
Airframe
Manufacturer
Cessna
Model
170B
Year
1952
Serial number
20361
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A1E498
Engine
Make and model
Cont Motor C145 Series
Type
Reciprocating
Power
145 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records
2023 – nowIndividual ownerMendota, IL · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026
NTSB events (1)
Accident · substantial damage
Aug 21, 1985 · West Chicago, IL
DURING APPLICATION OF PWR DURING A TOUCH-AND GO LANDING THE ACFT 'STARTED TO GET SIDEWAYS' ON THE RWY. THE PLT ALLOWED THE ACFT TO DRIFT OFF THE LEFT SIDE OF THE RWY INTO THE GRASS. A GROUND LOOP SUBSEQUENTLY OCCURRED WHICH SUBSTANTIALLY DAMAGED THE ACFT. WINDS AT THE TIME WERE FROM 80 DEGS AT 5 KTS WITH NO GUSTS. THE LANDING WAS BEING MADE ON RWY 15.
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (1)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
Reciprocating engine · connecting rod · brokenSep 25, 1995
NR 6 CONNECTING ROD FRACTURED APPROXIMATELY 2 INCHES BELOW PISTON SKIRT. BREAK SHOWED EVIDENCE OF PROGRESSION OVER TIME. FINAL FRACTURE WAS APPROXIMATELY ONE-HALF THE DIAMETER OF THE ROD WITH SOME MINOR CORROSION EVIDENT ALONG THE BEGINNING OF THE CRACK. AREA OF BREAK WAS CONSISTENT WITH A STRESS…
From FAA Service Difficulty Reports; matched by N-number and serial number.