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We operate our airplanes with full confidence that our customers are protected. We maintain our aircraft at the best aircraft mechanics and maintenance facilities available. We believe in using the highest grade oil, quality fuel and genuine parts.
Our airplanes are fully insured by one of the largest and well recognized insurance company. In fact, unlike most flying school aircrafts and other aircraft rental companies, we have insurance coverage that protects the customer's liability, beyond the deductible, for physical damage to the airplane in the unlikely event of a problem.
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Cessna 152
First delivered in 1977 as the 1978 model year, the 152 was a modernization of the proven Cessna 150 design.
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- Two seat training/touring
- Aircraft, high wing
- Useful load: 515 lbs.
- Standard empty Weight: 985 lbs.
- Max. speed sea level: 109 knots
- Service ceiling: 14,700 feet
- Fuel capacity: 26.1 US Gallons
- Fuel tanks: 2
- Range: 414 nm (no reserve)
- Rate of climb, sea level: 715 feet per minute
- Engine: Avco Lycoming O-235-L2C, 112 horsepower
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CESSNA 182 SKYLANE
It’s been hailed as the best all-around piston aircraft in general aviation. With power, versatility and performance to
spare, our speed enhanced Skylane. It is the ideal sport-utility combination and can be used also for advance
single engine aircraft training. It works hard for business. Climbing 980 fpm and cruising to 167 mph, the Skylane is
powered by a big 230-hp Continental – no adventure is beyond your reach.
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| Performance & Specification |
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| GROSS WEIGHT |
2800 lbs |
| SPEED, BEST POWER MIXTURE |
Top Speed at Sea Level
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167 mph |
Cruise, 75% Power at 6500 ft |
159 mph |
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| RANGE NORMAL LEAN MIXTURE |
Cruise, 75% Power at 6500 ft
58 Gallons, No Reserve 4.3 hrs
159 mph
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685 mi |
Optimum Range at 10,000 ft
58 Gallons, No Reserve 7.6 hrs
119 mph |
905mi |
Cruise, 75% Power at 6500 ft
77 Gallons, No Reserve 5.7 hrs
159 mph |
905 mi |
Optimum Range at 10,000 ft
77 Gallons, No Reserve 10.0 hrs
119 mph |
1190 mi |
| RATE OF CLIMB AT SEA LEVEL |
980 fpm |
SERVICE CEILING |
18,900ft |
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| TAKE-OFF |
| Ground Run |
625 ft |
Total Distance Over 50-Foot Obstacle |
1205 ft |
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| LANDING |
| Landing Roll |
590 ft |
BAGGAGE |
120 lbs |
| Total Distance Over 50-Foot Obstacle |
1350 ft |
WING LOADING: Pounds/Sq. Foot |
16.1 |
| EMPTY WEIGHT (Approximate) |
1550 lbs |
POWER LOADING: Pounds/Sq. Foot |
12.2 |
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| FUEL CAPACITY: Total |
| Standard Tanks |
.65 gals |
Optional Long Range |
.84 gals |
| OIL CAPACITY: Total |
12 qts |
| PROPELLER: 3-Bladed Constant Speed (Dia.) |
79 inches |
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| ENGINE |
Continental Engine
230 rated GP at 2600 RPM |
O-470-R |
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CESSNA 207/T207 SKYWAGON
Powered by a big 300-hp, fuel injected Continental, the normally aspirated Skywagon 207 has the power, size and load-carrying muscle to handle any assignments. With double cargo doors, room for seven, a whopping 1200-lbs useful load and a cruise speed 168 mph, it’s the thoroughbred of workhorse airplanes. Or we can remove the rear seats to haul a bulk load of cargo or equipment. And, the Skywagon is so versatile you can land nearly anywhere you please, including on grass, dirt or pavement. It has a STOL capability which means short field landing and short field take-off. It’s the ideal means of transportation in any role or on any mission. This machine is clearly in a class itself. |
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| Performance & Specification |
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| GROSS WEIGHT |
3800 lbs |
| SPEED, BEST POWER MIXTURE |
Top Speed at Sea Level
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168 mph |
Cruise, 75% Power at 6500 ft |
159 mph |
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| RANGE NORMAL LEAN MIXTURE |
Cruise, 75% Power at 6500 ft
58 Gallons, No Reserve 3.7 hrs
159 mph
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585 mi |
Optimum Range at 10,000 ft
58 Gallons, No Reserve 5.3 hrs
131 mph |
695mi |
Cruise, 75% Power at 6500 ft
77 Gallons, No Reserve 4.9 hrs
158 mph |
775 mi |
Optimum Range at 10,000 ft
77 Gallons, No Reserve 7.0 hrs
131 mph |
925 mi |
| RATE OF CLIMB AT SEA LEVEL |
810 fpm |
SERVICE CEILING |
13,300 ft |
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| TAKE-OFF |
| Ground Run |
1100 ft |
Total Distance Over 50-Foot Obstacle |
1970 ft |
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| LANDING |
| Landing Roll |
765 ft |
BAGGAGE |
120 lbs |
| Total Distance Over 50-Foot Obstacle |
1500 ft |
WING LOADING: Pounds/Sq. Foot |
21.7 |
| EMPTY WEIGHT (Approximate) |
1860 lbs |
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| FUEL CAPACITY: Total |
| Standard Tanks |
.65 gals |
Optional Long Range |
.84 gals |
| OIL CAPACITY: Total |
12 qts |
| PROPELLER: 3-Bladed Constant Speed (Dia.) |
79 inches |
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| ENGINE |
Continental Fuel Injected Engine
300 rated BHP at 2850 (5-Minute Take-Off Rating) |
IO-520-F |
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Piper Seneca I
The Piper Seneca is one of the most popular twin-engine travel airplanes of all times. Since 1972, more than 4,500
pieces were sold - a proof of its superior quality and safety.
The airplane is a twin-engine, six passenger, complex, VFR & IFR multi-engine aircraft that can travel approximately
450 nm without refuelling. It cruises approximately 140 kts / 165 mph. The Seneca I is the perfect aircraft for travel
because of its long-range capability and the best airplane to obtain the multi-engine rating in due to its docile
characteristics and simplistic system design.
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- Six seat training/touring
- Aircraft, low wing
- Useful load: 1,575 lbs.
- Standard empty Weight: 2,625 lbs.
- Max. speed sea level: 170 knots
- Service ceiling: 18,800 feet
- Fuel capacity: 98 US Gallons
- Fuel tanks: 2
- Range: 804 miles (no reserve)
- Rate of climb, sea level: 1,460 feet per minute
- Engine: Avco Lycoming I-235-L2C, 200 horsepower
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BN-Islander / BN2B - Islander
The ubiquitous Islander is the best-selling commercial aircraft produced in Western Europe. Adaptable, versatile
and durable, it has an unsurpassed record of solving transportation problems simply and economically in some of
the world's harshest environments.
Ten seats, twin engines and a design driven by the requirement for ease of operation provide exceptional levels of
utilisation. Constant refinement ensures that the Islander continues to excel in modern-day roles including
environmental protection, transportation, air ambulance, fisheries protection, photo surveying, policing and
parachuting to name but a few.
In addition to this 300HP Lycoming version of the Islander, there is also a 260HP Lycoming version. |
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The Britten-Norman BN-2 Islander
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BN-2B-20 - Max speed 280km/h (150kt), max cruising speed 264km/h (142kt), economical cruising speed 245km/h
(132kt). Initial rate of climb 1130ft/min. Service ceiling 17,200ft. Range at economical cruising speed and standard
fuel 1136km (613nm), with optional fuel 1965km (1060nm). BN-2B-20 - Two 225kW (300hp) Textron Lycoming IO-
40-K1B5s.
The first production machines were powered by 195kW (260hp) IO-540s and were simply designated BN-2, the first
flew in 1967. A small number were built before production switched to the BN-2A which introduced fairings to the
main undercarriage legs, wing leading edge and flap droop, and an increased max takeoff weight. From 1970 the
base A model was the BN-2A-6 and the BN-2A-7 had extended wingtips, while the BN-2A-2 and BN-2A-3 were
powered by the 225kW (300hp) IO-540, the latter with the extended wingtips.
Appearing in 1972 were the 195kW (260hp) powered BN-2A-26 and extended wingtips BN-2A-27, and the 225kW
(300hp) BN-2A-20 and extended wingtips BN-2A-21, all four models having higher weights. Further improvements
came with the BN-2B range with higher weights, improved interior and instrument panel and shorter diameter
props. The 26, 27, 20 and 21 variants were available as before. The 27 and 21 were later dropped while the BN-2B-
20 and BN-2B-26 remain in production. The turboprop (Allison 250) powered BN-2T has been built since 1981.
In September1979 Britten-Norman became Pilatus Britten-Norman, in July 1998 it was renamed back to Britten-
Norman, and from April 2000 it became B-N Group. |
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