Maximum Range
640
Maximum Cruise Speed
124
Maximum Occupants
4
Useful Load
878
Takeoff Ground Roll
960
Cessna
Skyhawk
The Cessna Skyhawk is the ultimate training aircraft and the most popular single-engine aircraft ever built.
With forgiving flight characteristics, great visibility, a sophisticated glass cockpit outfitted with G1000 avionics, slow landing speed and a forgiving stall – the Cessna Skyhawk is a flight training favorite ideally suited for student pilots.
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EXTERIOR
Extend The Training Time
The mastery in his design makes Skyhawk the world’s leading training aircraft. This superior platform thanks to student-oriented design, tolerant flight features, durable and robust construction; It provides the ideal conditions for a true pilot training.
AVIONICS
COMMAND THE NEXT GENERATION
ADVANCED DISPLAY TECHNOLOGY
The Cessna Skyhawk is powered by the latest technology in integrated cockpit avionics, the Garmin G1000 NXi. With an improved graphical interface, more powerful hardware, higher resolution displays, added functionality to improve situational awareness, and optional wireless technology, managing the flight deck has never been easier.
NEW FEATURES AND OPTIONS
- Standard ADS-B Out and In
- Optional wireless data base and flight plan loading
- Integrated VFR Sectional Charts
- IFR High and Low Charts with Night Mode
- Enhanced HSI features
- COM frequency decoding
- Vertical Situation Display
- Selectable Visual Approaches
- Optional Surface Watch for runway safety
- Enhanced graphics and faster processing
- Improved joystick with smoother panning
- Simplified maintenance
Specifications
Cessna Skyhawk
Dimensions
| Length | 27 ft 2 in (8.28 m) |
| Height | 8 ft 11 in (2.72 m) |
| Wingspan | 36 ft 1 in (11.00 m) |
| Wing Area | 174 sq ft (16.17 sq m) |
Cabin Interior
| Height | 48 in (1.22 m) |
| Width | 40 in (1.00 m) |
| Length | 11 ft 10 in (3.61 m) |
| Maximum Occupants | 4 |
Baggage Capacity
| Weight | 120 lb (54.4 kg) |
| Volume | 30 cu ft (0.85 cu m) |
Weights
| Maximum Ramp Weight | 2,558 lb (1,160 kg) |
| Maximum Takeoff Weight | 2,550 lb (1,157 kg) |
| Maximum Landing Weight | 2,550 lb (1,157 kg) |
| Usable Fuel Weight | 318 lb (144 kg) |
| Usable Fuel Volume | 53 gal (201 l) |
| Basic Empty Weight | 1,680 lb (762 kg) |
| Useful Load | 888 lb (403 kg) |
| Maximum Payload | 870 lb (395 kg) |
| Full Fuel Payload | 560 lb (254 kg) |
Performance
| Maximum Cruise Speed | 124 ktas (230 km/h) |
| Maximum Range | 640 nm (1,185 km) |
| Takeoff Distance | 1,630 ft (497 m) |
| Ground Roll | 960 ft (293 m) |
| Landing Distance | 1,335 ft (407 m) |
| Ground Roll | 575 ft (175 m) |
| Service Ceiling | 14,000 ft (4,267 m) |
| Maximum Climb Rate | 730 fpm (223 mpm) |
| Maximum Limit Speed | 163 kias (302 km/h) |
| Stall Speed | 48 kcas (89 km/h) |
Powerplant
| Manufacturer | Lycoming |
| Model | IO-360-L2A |
| Power Output | 180 hp (180 hp) |
| Propeller Manufacturer | McCauley |
| Description | 2 blade metal, fixed pitch |
EMAIR Aviation Inc. reserves the right to change about the technical information presented in the introductory pages of the Cessna vehicles.
