CESSNA 172 Skyhawk

Aircraft
Name: 
172 Skyhawk
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
High wing (wing struts)
Tail: 
Regular tail, mid set
WTC
L
APC
A
Type Code: 
L1P
Engine: 
Piston
Engine Count: 
Single
Position: 
Nose mounted
Landing gear: 
Tricycle fixed
Manufacturered as
CESSNA 172
CESSNA 172 Cutlass
CESSNA 172 Skyhawk
CESSNA Cutlass
CESSNA Hawk XP
CESSNA Mescalero
CESSNA P172 Skyhawk Powermatic
CESSNA R172
CESSNA R172 Hawk XP
CESSNA Skyhawk
CESSNA Skyhawk Powermatic
CESSNA T-41 Mescalero
FMA P-172
AVIONES COLOMBIA 172
REIMS F172
REIMS F172 Skyhawk
REIMS FP172
REIMS FR172 Hawk XP
REIMS FR172 Reims Rocket
REIMS Hawk XP

C172

Light utility aircraft. In service since 1956 (172R since 1996). Exists in many civil and military models. Worldwide about 37.000 aircraft built between 1955 and 1985. Non retractable gear. Last major Skyhawk Model CESSNA 172N. Licence production F172 by REIMS, France. New version 172R and 172SP based on the 172N with quiet engines, GPS/IFR GPS and single axis autopilot were put in production in 1996. US-mil. type: T-41 Mescalero as basic trainer and observation aircraft. Note: Has 2 side windows and rounded rear window.

Technical Data
Wing span: 
10.90 m
Length: 
8.20 m
Height: 
2.70 m
Powerplant: 

1 x 145 HP Continental O-300-A or 1 x 175 HP Continental GO-300-C or 1 x 145 HP Continental O-300-C or 1 x 160 HP Lycoming O-320-H2AD or 1 x 195 HP Continental IO-360-KB piston engine with 2 blade propeller.

Engine Model: 
Continental O-300, Continental O-360, Lycoming O-320
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
514 m
MTOW: 
1100 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL150)
IAS: 
n/a
ROC: 
n/a
Initial Climb (to FL240)
IAS: 
n/a
ROC: 
n/a
MACH Climb
MACH: 
n/a
ROC: 
n/a
Cruise
TAS: 
114 kts
MACH: 
n/a
Ceiling: 
150
Range: 
580 NM
Initial Descent (to FL240)
MACH: 
n/a
ROD: 
n/a
Descent (to FL100)
IAS: 
n/a
ROD: 
n/a
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
n/a
Distance: 
n/a

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