ITEM GENERAL CESSNA 150 CESSNA 152 CESSNA 172
Engine -Normally aspirated (continental O-2385L2C Thru O-360A4M
- Lycoming - Direct drive O-200A) s/n 15285094 Skyhawk II (5Y-
- Continental - Air cooled -Lycoming NNE)
-Horizontally opposed O-320-E2D O-235-N2C
-Equipped with carburetor Beginning with s/n
- 4 cylinders 15285590
Power -equipped with 2 150 BHP at 2700 -O-235-L2C 110 O-320-E2D 150
magnetos RPM BHP at 2550 RPM BHP at 2700
-right magneto fires RPM
bottom r/h and top l/h -O-235-N2C 108 O-360-A4M
spark plugs BHP at 2550 RPM 180BHP at
-left magneto fires bottom 2700RPM
l/h and top r/h spark plugs
-each cylinder has 2 spark Left impulse Both magnetos has Left impulse
plugs magneto impulse magneto
- firing order is 1-3-2-4
Oil Check engine oil with the Oil pressure Oil pressure Oil pressure
-Straight mineral oil dipstick five to ten -Normal operation -Normal operation -Normal
-Ashless dispersant minutes after the engine 60-85PS 60-90 PSI operation 60-85
has been stopped. -Min idling 25PSI -Min idling 25PSI PSI
New or newly overhauled I -Max cold starting -Min idling
engines should be -Max cold starting 115PSI 25PSI
operated on aviation 100PSI -Max cold
grade straight mineral oil starting 100PSI
until the first oil change.
After the 25hrs of Temperature Temperature Temperature
operation, drain engine oil -Within the green -Within the green -Within the green
, refill sump with straight arc arc arc
mineral oil and use until a
total of 50hrs have Oil capacity Oil capacity Oil capacity
accumulated or oil -8qts without -6qts without -8qts without
consumption has external filter external filter external filter
stabilized, then change to -9qts with external -7qts with external -9qts with
ashless dispersant oil filter filter external filter
CHT
O-360-A4M
5000F
Fuel Quantity in US Gal
Commonly used type Total 26 26 42
of fuel is Usable 22.5 24.5 38
100LL(blue)
Other types are Consumption Gal/Hr 7 6 O-360 =8
-100 (green) O-320 =7
-80 (red)
Propeller Diameter 69” 69” 76”
-Two bladed fixed Type Sensenich sensenich -O-360 sensenich
pitch propeller -O-320
McCauley
Landing gear Main landing gear - Flat spring-steel -The aircraft is - On 1969-1970
main landing gear equipped with a Model aircraft, a
struts are installed fixed tricycle non-retractable
on 1969 thru 1970 landing gear, tricycle landing
model consisting of gear equipped
- Beginning with tubular spring-steel with
1971 models, main gear struts Cessna flat
tubular spring- spring-steel main
steel main gear gear struts
struts are installed. - Beginning
with 1971 Model
aircraft, a non-
retractable
tricycle landing
gear equipped
with Cessna
tubular spring-
steel main
gear struts
Nose landing gear All models are Nose landing gear An air/oil
equipped is equipped with steerable nose
with air/oil, air/oil, steerable gear shock strut is
steerable nose gear nose gear shock used.
shock struts. struts.
Tire size
Main gear 6.00x6 6.00x6 6.00x6
Nose gear 5.00x5 5.00x5 5.00x5
Ply rating 4 ply rating 4 ply rating 4 ply rating
Tire pressure
Main wheel 21 psi 21 psi -Thru 1970-26psi
-beginning with
1971 -29psi
30 psi 30 psi -Thru 1970-
Nose wheel 26psi
-beginning with
1971-31psi
Turning angle of the nose 8.5o with rudder 8.5o with rudder 8.5o with rudder
wheel 30o with rudder 30o with rudder and 30o with rudder
and brakes brakes and brakes
Type of brakes system Independent brake Independent brake Independent
system system brake system
Airframe -wing span 392.5” 400.00” 434”
These aircraft are
high-wing monoplanes - Tail Span 120” 120” 132”
of all-metal semi
monocoque - Track Width
91.25” 91.28” 105.5”
construction, with
fibre glass fairing -Length
284.5” 284.84” 323”
wing and stabilizer
-Fin Height (Maximum With
tips Nose Gear Depressed And
Flashing Beacon Installed on
Fin) 96” 102” 105.5”
Stall warner Pneumatic type Port leading edge Port leading edge Port leading edge
(wing) (wing) (wing)
Identification plate Fire proof metal plate Port tail cone Port tail cone Port tail cone
with aircraft and owner
details
Controls Aileron
Primary controls Up 20 20 20
-ailerons fully Down 14 14 15
mechanical fraise Elevator
differential Up 25 25 28
-rudder fully Down 15 18 23
mechanical Rudder
-elevators fully Left 23 23 17
mechanical Right 23 23 17
Secondary controls
-Flaps electrically Flaps 40 30 40
operated single
slotted fowler type.
- elevator trim tab Trim tab
fully mechanical Up 10 10 28
Down 20 20 13
Speed ranges Max at sea level 144 mph 110knots 144 mph
Cruise at 75% power 138 mph (8000ft) 107 knots (8000ft) 138 mph (8000ft)
