Presenting the KOLIBER 160 & 235A

Falcon Wings Aviation proudly presents the KOLIBER 4-place airplane manufactured by PZL of Warsaw, Poland&ecedil;. The KOLIBER continues a long, proud tradition in the design and manufacture of aircraft since 1928.

Initial KOLIBER type certification was received in 1982. Since that time, deliveries have been made to many countries, including Australia, Britain, Denmark, Germany, the Netherlands, Norway, and Sweden. It is now FAA approved in the USA under FAR 23 Type Certificate #A69EU.

Each KOLIBER II is delivered ready to fly with IFR gyro instrumentation and avionics plus full night flight capability. Optional avionics packages are available.

KOLIBER II is truly a remarkable airplane, equally at home for training student pilots or for cross-country pleasure and business flights. KOLIBER II is surprisingly docile, with an ability to fly at speeds down to 39 kts. at full gross takeoff weight. In fact, aided by aerodynamically activated leading edge slats, KOLIBER II will not stall in the conventional sense with power off. Instead, it simply descends without a stall "break". In order to actually stall, power must be applied. Durable, all=metal construction, hydro-pneumatic dampened main landing gear and tricycle design allow for flights in moderate cross-wind conditions.

Fuel economy is extraordinary and the dependable Textron-Lycoming 150 hp engine has a substantial Time Between Overhaul (TBO) of 2000 flight hours! Maintenance can be accomplished by most general aviation mechanics using simple tools and equipment found at any light airplane service facility.

ONLY KOLIBER II OFFERS SO MANY OUTSTANDING FEATURES

New, Expanded "T" Layout Instrument Panel New, Improved Electrical System New Night Flying Capability Exclusive Leding Edge Slats Protect Against Inadvertant Stalls Dual Flying Controls for Instruction Confidence Extremely Short Takeoff and Landing

IFR Avionics and Gyro Instrumentation Included Large, Sliding Canopy can be opened in Flight for Ventilation, Aerial Photography or Parachute Jumping Three-Point Seat Belt/Shoulder Harness Large, Insulated passenger Compartment Dependable 150 HP, Textron-Lycoming Engine Most Replacement Parts are American Sourcing

Performance and Specifications

Maximum takeoff weight	1874 lb		Obstacle (50 ft) landing distance	1040 ft
Typical useful load	669 lb		Landing roll distance	450 ft
Takeoff roll distance	550 ft		Demonstrated Crosswind Component	23 mph/20 kts
Obstacle (50 ft.) takeoff distance	1300 ft		Stall Speeds at 1874 lb
Initial Rate of Climb	670 ft/min		Power on	45 mph/39 kts. CAS
Maximum Speed	121 mph/105 kts. (75% power)		Power off (30 deg. flaps)	51 mph/44 kts. CAS
Maximum Range	688 sm/518 nm @ 111 mph/96 kts		Service Ceiling at 1874 lb	12,139 ft
(65% power)	42.5 US gallons

Dimensions

Wing Span 32.0 ft./9.74 m.

Length 24.2 ft./7.37 m.

Height to Top of Fin 9.2 ft./2.80 m.

Contact:

FALCON WINGS AVIATION P.O. Box 4084 Gettysburg, PA 17325 (717) 642-8593 falconwings@desupernet.net

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