I-CEPI - 1971 ROBIN DR300/180
Aircraft Summary
General
Year
1971
Manufacturer
ROBIN
Model
DR300/180
Serial Number
609
Registration #
I-CEPI
Condition
Used
Description
Very good 4 seats touring aircraft. Private aircraft in very good condition and always hangared.
The current owner purchased it from the first owner in 1972 when the aricraft had 48 hours total time!
Never used for training or glider towing.
Airframe
Total Time
2961
Airframe Notes
Total Fuel Capacity: 205 Fuel Capacity
Total of 4 fuel tanks, one 40 Liter in each wing and two tanks 75 liters and 50 liters in the fuselage
Maximum Take Off Weight: 1070 Kg
Empty Weight: 604.8 Kg,weighed 12/04/2017
Baggage Compartment Weight: 60 Kg
Cruise Speed: 125 kts
Endurance: Over 6 hours
Consumption: 31 Liter per Hour
Very good short field and climb performance!
Engine
Engine Manufacturer
LYCOMING
Engine Model
O-360-A4M
Engine Serial Number
L-15165-36A
Engine Horsepower
180 HP
Engine Time
1353
Engine Time Since
SOH
Engine TBO
2000
Engine Notes
Overhauled: 12/04/1993
Props
Prop Notes
Propeller, two bladed metal Sensenich 76EM8S5-0-64, Serial Number: 16251K
Total Time: 2961 hours
Time Since Overhaul: 1185 hours
Avionics
Avionics/Radios
King KMA134 Audio Panel with Marker Beacon
Sigtronics Intercom System
Garmin GTR225A COM 760 Channels, 8.33 KHZ
Collins VHF251E COM
Collins VIR351 NAV
Narco NAV122 VOR/Glide Slope
ARC300 ADF
Narco AT50A Transponder C
FLARM Traffic Detector
Kannad 406 ELT
Additional Equipment
Additional Equipment
Cabin fire extinguisher
First aid kit
Aircraft cover
Exterior
Exterior Notes
White with orange accents
Original and in good condition with normal wear
Interior
Number of Seats
4
Interior Notes
Original brown vinyl, in good condition with normal wear
Inspection Status
Inspection Status
Annual inspection and ARC renewed April 2024
2000 hours inspection completed at Total Time: 2853 hours
Damage history: Collision with trees after landing damaging both wings occurred on 12/06/1997
Aircraft repaired by Robin with the replacement of both wings with new ones. Work completed 09/04/1999 at Total Time: 2149 hours
Shock Load Inspection (VNIP) performed 16/09/1998
Hours Since Shock Load Inspection: 812 hours
Airworthy
Yes
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