PPP666888CCC SSSeeerrriiieeesss (((PPP666888CCC ––– PPP666888CCC TTTCCC))) “““ ttthhheee nnneeewww gggeeennneeerrraaatttiiiooonnn ooofff aaa mmmooodddeeerrrnnn sssuuucccccceeessssssfffuuullllllyyy dddeeesssiiigggnnneeeddd tttwwwiiinnn””” The Vulcanair Aircraft P68C Series is a six seater, twin engine, high wing, fixed landing gear aircraft. The aircraft is offered standard with numerous improvements, such as a modern glass cockpit, new autopilot, new adjustable seats, a standard pilot door, sturdier main gear and brakes, and a higher maximum zero fuel weight. The redundancy of the second engine with a fuel consumption comparable to many six-cylinder single engine piston aircraft place the P68C Series is in a class of its own. Since its inception the aircraft was designed to be a twin. As a result the P68 is a docile and stable aircraft in the whole flight envelope with superior flight qualities which can only be appreciated once the aircraft is flown. Structural simplicity, aluminium construction, absence of complicated systems, ruggedness, accessibility to servicing points reduce the maintenance costs of the P68C Series to a bare minimum.

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AAAiiirrrcccrrraaafffttt CCCooonnnfffiiiggguuurrraaatttiiiooonnn The standard interior configuration is for 6 passengers (1+5). In addition, through the quickly removable seats, the large cabin volume can be configured with less seats for more space according to personal preferences. Club seating is certified and can be configured in minutes. By removing all pax seats the aircraft becomes a valid small cargo hauler being able to carry from mountain bikes to stretchers. That is why the P68C is very adapted for air taxi companies or simply to be your next “personal airliner”. The P68C is also a very stable platform for aerial photography, reconnaissance and emergency missions. Its optional and retrofittable 2.1 x 1.5 ft. hatch (63 x 46 cm.) has been expressly designed for the installation of a variety of airborne surveillance equipment.

DDDiiimmmeeennnsssiiiooonnnsss CABIN Cabin length Cabin width Ave. Cabin height Total Volume CARGO COMPART. Length Ave. width Ave. height Total Volume

COCKPIT AREA 1.451 m 4.760 ft 1.160 m 3.806 ft 1.150 m 3.773 ft PAX CONF. 0.816 m 2.677 ft 1.010 m 3.300 ft 1.000 m 3.281 ft 0.824m3 28.98 cu.ft

PASSENGER CABIN 1.780 m 5.840 ft 1.160 m 3.806 ft 1.200 m 3.937 ft 2.478 m3 87.51 cu. ft CARGO CONF. 2.596 m 8.507 ft 1.100 m 3.609 ft 1.120 m 3.674 ft 3.198 m3 112.8 cu. ft

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PPPeeerrrfffooorrrmmmaaannnccceeesss Engines Lycoming IO-360-A1B6 (200 hp) and TIO-360-C1A6D (210 hp)

Max Ramp Weight Max Take-Off Weight Max Landing Weight Well Equipped Empty Weight Max Zero Fuel Weight Useful Load Max Fuel Capacity Max Usable Fuel Number of Seats Luggage Capacity P68C - IO-360-A1B6 (200 hp) Avg. Cruise Speed @ 75% Rate of Climb (2 eng.@MTOW) Rate of Climb (1 eng. @MTOW) Stall Speed (full flaps) Service Celling (2 engines) Service Celling (1 engine) Range, FL 100, 55% Pwr. (incl 45’ Res) Take-Off Run Landing Run Max Endurance, FL 100, 65% Pwr, ISA Load Factor

2100 kg 2084 kg 1980 kg 1420 kg 1967 kg

680 kg 696 lt 670 lt

6 0.56 cu.m

301 km/h 6 m/s 1 m/s

106 km/h 5490 m 1520 m

2960 km 240 m 200 m

›10 h +3.74g

4630 lb 4594 lb 4365 lb 3130 lb 4336 lb 1499 lb

184 U.S. gal 177 U.S. gal

6 20 cu.ft

160 Ktas 1100 fpm

200 fpm 57 Kcas

18000 ft 5000 ft

1598 nm 787 ft 656 ft

›10 h / -1.50g

For the lovers of more performance or if operating from hot and high airports the P68C is also offered in its turbocharged version:

P68C TC - TIO-360-C1A6D (210 hp) Avg. Cruise Speed @ 75% Rate of Climb (2 eng.@MTOW) Rate of Climb (1 eng. @MTOW) Stall Speed (full flaps) Service Celling (2 engines) Service Celling (1 engine) Range, FL 100, 55% Pwr. (incl 45’ Res) Take-Off Run Landing Run Max Endurance, FL 100, 65% Pwr, ISA Load Factor

315 km/h 7.6 m/s

1.1 m/s 106 km/h

6100 m 3350 m

2280 km 230 m 200 m

8 h +3.80 g

170 Ktas

1500 pm 220 fpm 57 Kcas 20000 ft

1100 ft 1230 nm

755 ft 656 ft

8 h / - 1.52g

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