Section 1 Flashcards
Height and length of aircraft
8’ 6”
24’1”
Elevator and wing span
10’
33’4’’ (with strobe lights)
32’ 8.5’’ (Without strobe lights)
Propeller diameter
69’’ max
67.5 “ min
Wheel base
58”
Propeller ground clearance
12”
Wing area
159.5 sq. Feet
Minimum turning radius
24’ 8”
Engine description
Single engine by avco lycoming. Engine model - 0-235 - L2C
Normally aspirated , direct drive, air cooled, horizontally opposed 4 piston 4 stroke engine with 233.3 cu. Inch displacement, carburettor equipped.
Power rating - 110 BHP at 2550 RPM
Propeller description
Manufactured by McCauley accessory division
Model no. 1A103/TCM6958
2 blade fixed pitch propeller
Max diameter 69”
Min diameter 67.5”
Approved fuel grade and colour
Avgas 100LL (blue)
Avgas 100 (green)
Standard tank fuel capacity
26 USG total
Usable total 24.5 USG
(Unusable 1.5USG total, 0.75 in each tank)
Long range tank fuel capacity
Total 39 USG in each tank 19.5 USG
37.5 total usable
1. 5 total unusable
Oil used
Mil-l-6082 (25 hrs, then repeatedly changed)
Mil-l- 22851 after so hrs
Oil capacity
6Q sump
7Q total
MTOW, MLW, Ramp wt.
1670 lbs, 1675 lbs
