1977 CESSNA TURBO 210M
Aircraft Summary
General
Year
1977
Manufacturer
CESSNA
Model
TURBO 210M
Condition
Used
Description
Sandel 3308 HSI, Garmin 430 GPS/Com/Nav/ILS, KX165 NAV/Com/ILS, ADSB, DME, ETR 419/619 TBA, PTR
1,150, Good P & I
FUEL CAPACITY: 341 LTRS
MTOW: 1,818 KGS
BASIC WEIGHT: TBA
LENGTH: 28’2”
HEIGHT: 9’8”
WING SPAN: 34’9”
RANGE: 715 NM
TAKEOFF OVER 50’ OBST: 2,160’
LAND OVER 50’ OBST: 1,500’
MAX SPEED: 204 KTS CRUISE 170/192 ALT DEP
DATA AS AT 7.5.2026
Airframe
Total Time
6699
Engine
Engine Manufacturer
CONTINENTAL
Engine Model
TSIO520R
Engine Time
981
Engine Time Since
SOH
Engine TBO
1600
Props
Prop Manufacturer
HARTZELL
Prop Time
850
Prop Time Since
SOH
Avionics
Avionics/Radios
KING KMA24 AUDIO AND MARKERS
GARMIN GNS430 GPS/NAV/COM/VOR/LOC/ILS
KING KX155 NAV/COM/VOR/LOC/ILS
SANDEL SN3308 HSI SYSTEM
KING KT74 ADSB TRANSPONDER
KING KN62 DME
KING KR87 ADF/RMI
JPI 700 COLOUR DIGITAL ENGINE MONITOR
KING KFC200 COUPLED AUTOPILOT
Additional Equipment
Additional Equipment
VORTEX GENERATOR KIT
STOL SHORT TAKEOFF / LANDING KIT
ARTICULATING SEATS PILOT /COPILOT
ELECTRIC ELEVATOR TRIM
6 PLACE INTERCOM
GYRO SUCTION GAUGE
STROBE LIGHTS
PAX INDIVIDUAL FRESH AIR VENTS
PAX READING LIGHTS
Interested in operating costs?
has the answerRecommended For You
View All(Recommended For You)
N761TY1978 CESSNA TURBO 210M
N732SJ1977 CESSNA TURBO 210M
N3432F1978 CESSNA TURBO 210M
N761WT1978 CESSNA TURBO 210M
Aircraft.com does not own the rights to the images displayed on this site. We do not have information regarding the original seller or source of these images unless explicitly stated.