Filomuz
| Occupancy | |
|---|---|
| Crew | 1 |
| Passengers | 5 |
| Operating Weights | |
| Max T/O Weight | 4750 Lb |
| Max Landing Weight | 4513 Lb |
| Operating Weight | 3597 Lb |
| Empty Weight | 3212 Lb |
| Fuel Capacity | 732 Lb |
| Payload W/Full Fuel | 444 Lb |
| Max Payload | 1153 Lb |
| Range | |
| Normal Range | 423 nm |
| Max Range | 886 nm |
| VFR Normal Range | 466 nm |
| VFR Max Range | 911 nm |
| Service Ceiling | 25000 ft |
| Distances | |
| Balanced Field Length | 1701 ft |
| Landing Distance | 4500 ft |
| Performance | |
| Rate of Climb | 1400 fpm |
| Rate of Climb | 172 fpm |
| Max Speed | 204 kts |
| Normal Cruise | 200 kts |
| Economy Cruise | 170 kts |
| Power Plant | |
| Engines | 2 |
| Engine Mfg | Continental |
| Engine Model | TSIO-360-RB |
| Speed * | |
|---|---|
| VNE Never Exceed Speed | 165 knots |
| VNO Speed for normal Operations | 165 knots |
| Maximum Range (5,000 ft at 55% power) | 620 NM |
| CLIMBRATE(MSL) | 700 FT/min |
| SERVICE CEILING | 14,500 FT |
| TAKEOFF PERFORMANCE | |
| Ground Roll | 820 ft |
| Total Distance over 50 ft obstacle | 1411 ft |
| LANDING PERFORMANCE | |
| Ground Roll | 689 ft |
| Total Distance over 50 ft obstacle | 1640 ft |
| MAXIMUM WEIGHT | |
| Takeoff or landing | 750 kg. / 1653 lb |
| STANDARD EMPTY WEIGHT | |
| AT01-100C | ab 500 kg. / 1102 lb |
| MAXIMUM USEFUL LOAD | |
| AT01-100C | 250 kg. / 551 lb |
| BAGGAGE ALLOWANCE | 40 kg. / 88,2 lb |
| SEATS | 2 |
| FUEL CAPACITY | |
| Standard Tanks | 120lt |
| Fuelgrade (EN228 SUPER / Super Plus, AVGAS 100LL, AVGAS UL91) | |
| OIL CAPACITY | 3 lt |
| ENGINE: Bombardier Rotax 912 S3 | 100PS |
| PROPELLER: MT-Propeller MTV-21-A / 170-05 | 66,9 in |
| DIMENSIONS | |
| Lenght | 24,28 ft / 7,40 mt |
| Lenght | 7,87 ft / 2,40 mt |
| Wingspan | 33,79 ft / 10,30 mt |
| Wing area | 113.00 ft2 / 10.50 m2 |
| Cabin width | 3,97 ft / 1,20 mt |
| Baggage Compartment Capacity | 17.70 ft3 / 500 lt |
| Speed * | |
|---|---|
| Maximum at Sea Level | 123 knots |
| Cruise, 80% Power at 8,000 ft | 122 knots |
| CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve. | |
| 80% Power at 8,000 ft (Range) | 580 NM |
| 53 Gallons usable fuel (Time) | 4.8 hours |
| Range at 10,000 FT, 60% power (Range) | 687 NM |
| RATE OF CLIMB AT SEA LEVEL | 720 FPM |
| SERVICE CEILING | 13,500 FT |
| TAKEOFF PERFORMANCE | |
| Ground Roll | 945 ft |
| Total Distance over 50 ft obstacle | 1685 ft |
| LANDING PERFORMANCE | |
| Ground Roll | 550 ft |
| Total Distance over 50 ft obstacle | 1295 ft |
| STALL SPEED | |
| Flaps up, power off | 51 kcas |
| Flaps down, power off | 47 kcas |
| MAXIMUM WEIGHT | |
| Ramp | 2457 lbs |
| Takeoff | 2450 lbs |
| Landing | 2450 lbsas |
| STANDARD EMPTY WEIGHT | 1639 lbs |
| MAXIMUM USEFUL LOAD | 818 lbs |
| BAGGAGE ALLOWANCE | 120 lbs |
| WING LOADING: Lbs/Sq Ft | 14.1 |
| POWER LOADING: Lbs/HP | 15.3 |
| FUEL CAPACITY | 56 gal |
| OIL CAPACITY | 8 qts |
| ENGINE: Textron Lycoming (160 BHP at 2400 RPM) | IO-360-L2A |
| PROPELLER: Fixed Pitch, Diameter | 75 in |
| Speed * | |
|---|---|
| Maximum at Sea Level | 110 knots |
| Cruise, 75% Power at 8,000 ft | 107 knots |
| CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve at 45% power | |
| 75% Power at 8,000 ft (Range) | 350 NM |
| 24.5 Gallons usable fuel (Time) | 3.4 hours |
| 75% Power at 8,000 ft (Range) | 580 NM |
| 37.5 Gallons usable fuel (Time) | 5.5 hours |
| Maximum Range at 10,000 ft (Range) | 415 NM |
| 24.5 Gallons usable fuel (Time) | 5.2 hours |
| Maximum Range at 10,000 ft (Range) | 690 NM |
| 37.5 Gallons usable fuel (Time) | 8.7 Hours |
| RATE OF CLIMB AT SEA LEVEL | 715 FPM |
| SERVICE CEILING | 14,700 FT |
| TAKEOFF PERFORMANCE | |
| Ground Roll | 725 ft |
| Total Distance over 50 ft obstacle | 1340 ft |
| LANDING PERFORMANCE | |
| Ground Roll | 475 ft |
| Total Distance over 51 ft obstacle | 1200 ft |
| STALL SPEED (CAS) | |
| Flaps up, power off | 48 knots |
| Flaps down, power off | 43 knots |
| STANDARD EMPTY WEIGHT | |
| 152 | 1101 lb |
| 152 II 1 | 1133 lbs |
| MAXIMUM USEFUL LOAD | |
| 152 | 574 lbs |
| 152 II 1 | 54 lbs2 |
| BAGGAGE ALLOWANCE | 120 lbs |
| WING LOADING (Pounds / s.f.) | 10.5 |
| POWER LOADING (Pounds / HP) | 15.2 |
| FUEL CAPACITY | |
| Standard Tanks | 26 GAL |
| Long Range Tanks | 39 GAL |
| OIL CAPACITY | 6 qts |
| ENGINE: Avco Lycoming 110 bhp at 255o rpm | O235-L2C |
| PROPELLER: Fixed Pitch, diameter | 69 in |