cpt_shawky
31-07-2007, 07:35 AM
الأخوة الأعزاء هذه بعض صور لطائرات الكلية المصرية للطيران
تمتلك الكلية 28 طائرة من مختلف طائرات التدريب منفرد ومتعدد المحركات وساقوم بوضع بيانات كل طائرة وبعض الصور لها
-= MISR FLYING COLLEGE =-
http://www.cars-club.com/up/7-1/carsclub_54643082.jpg
http://www.cars-club.com/up/sp/carsclub_74946335.jpg
:fly:
الطائرة بارون 58
Raytheon Beechcraft Baron (58)
The multi-engine Baron 58 is an all-metal complex aircraft stretched version of the Baron 55 with a six-person seating capacity including a crew of one or two The Misr Flying College fleet has two Baron 58s.
Beechcraft Baron 58
Specifications:
Speeds
Maximum speed at sea level 208 knots (386 km/hr)
Cruise, 80% power 8000 feet 192 knots (356 km/hr)
Performance
Range, 80% power at 8000 feet 1575 NM
Time 4.8 hours
Rate of climb at sea level: 1735 feet per minute
Service ceiling 20,688 feet
Weights & Loads
Maximum ramp weight 5524 pounds
Maximum takeoff weight 5500 pounds
Useful load 1578 pounds
Fuel
Fuel capacity 200 gallons
Usable fuel 194 gallons
Engine & Propeller
Engine: Teledyne Continental IO-550-C
Horsepower 300 BHP at 2700 RPM
Oil Capacity 12 quarts
http://www.cars-club.com/up/sp/carsclub_79987772.jpg
http://www.cars-club.com/up/sp/carsclub_62746017.jpg
http://www.cars-club.com/up/sp/carsclub_22037433.jpg
http://www.cars-club.com/up/sp/carsclub_25423192.jpg
http://www.cars-club.com/up/sp/carsclub_84818909.jpg
http://www.cars-club.com/up/sp/carsclub_62364408.jpg
الطائرة بونانزا ف-33-أ
Raytheon Beechcraft Bonanza (F33A)
The Bonanza F33A aircraft is an all metal, single-engine piston, low-wing monoplane constant speed propeller and retractable landing gear with a four-person seating capacity including a crew of one or two used for complex training. The Misr Flying College fleet has four Bonanza F33As.
Beechcraft Bonanza F33A
Specifications:
Speeds
Maximum speed at sea level 196 knots
Stall speed, flaps up 56 knots
Stall speed flaps down 47 knots
Performance
Weights & Loads
Maximum ramp weight 3412 pounds
Maximum takeoff weight 3400 pounds
Useful load xxx pounds
Baggage allowance 270 pounds
Fuel
Fuel capacity 80 gallons
Usable fuel 74 gallons
Engine & Propeller
Engine: Teledyne Continental IO-520-BB
Horsepower 285 BHP at 2700 RPM
Oil Capacity 12 quarts
http://www.cars-club.com/up/sp/carsclub_61921487.jpg
http://www.cars-club.com/up/sp/carsclub_75594775.jpg
http://www.cars-club.com/up/sp/carsclub_36914163.jpg
http://www.cars-club.com/up/sp/carsclub_53057268.jpg
http://www.cars-club.com/up/sp/carsclub_59139880.jpg
الطائرة كوماندور114-ب
Commander (114B)
The Commander 114B aircraft is an all metal, single-engine piston, low-wing monoplane constant speed propeller and retractable landing gear with a four-person seating capacity including a crew of one or two used for complex training. The Misr Flying College fleet has four Commander 114Bs
Commander 114B
Specifications:
Speeds
Maximum speed at sea level 164 knots (304 km/hr)
Cruise, 75% power 8000 feet 160 knots
Stall speed, flaps up 63 knots
Stall speed flaps down 54 knots
Performance
Range, 75% power at 8000 feet 630 NM
Time 4.5 hours
Rate of climb at sea level: 1070 feet per minute
Service ceiling 16,800 feet
Weights & Loads
Maximum ramp weight 3260 pounds
Maximum takeoff weight 3250 pounds
Useful load 1158 pounds
Baggage allowance 200 pounds
Fuel
Fuel capacity 70 gallons
Usable fuel 68 gallons
Engine & Propeller
Engine: Lycoming IO-540-T4B5
Horsepower 260 BHP at 2700 RPM
Oil Capacity 08 quarts
Propeller McCauley 3 Blades B3D32C419
http://www.cars-club.com/up/sp/carsclub_58800669.jpg
http://www.cars-club.com/up/sp/carsclub_84316933.jpg
http://www.cars-club.com/up/sp/carsclub_59921104.jpg
http://www.cars-club.com/up/sp/carsclub_54532511.jpg
http://www.cars-club.com/up/sp/carsclub_43020577.jpg
الطائرة سسنا 172-ر
Cessna Skyhawk (172R)
Commonly referred to as the Skyhawk, the Cessna 172R aircraft is an all metal, single-engine piston, high-wing monoplane with a four-person seating capacity including a crew of one or two. The Misr Flying College fleet has twelve Cessna 172s.
Cessna 172R
Specifications:
Speeds
Maximum speed at sea level 123 knots
Cruise, 80% power 8000 feet 122 knots
Stall speed, flaps up 51 knots
Stall speed flaps down 47 knots
Performance
Range, 80% power at 8000 feet 580 NM
Time 4.8 hours
Rate of climb at sea level: 720 feet per minute
Service ceiling 13,500 feet
Weights & Loads
Maximum ramp weight 2457 pounds
Maximum takeoff or landing weight 2450 pounds
Useful load 837 pounds
Baggage allowance 120 pounds
Fuel
Fuel capacity 56 gallons
Usable fuel 53 gallons
Engine & Propeller
Engine: Avco Lycoming IO-360-L2A
Horsepower 160 BHP at 2400 RPM
Oil Capacity 8 quarts
http://www.cars-club.com/up/sp/carsclub_86393819.jpg
تمتلك الكلية 28 طائرة من مختلف طائرات التدريب منفرد ومتعدد المحركات وساقوم بوضع بيانات كل طائرة وبعض الصور لها
-= MISR FLYING COLLEGE =-
http://www.cars-club.com/up/7-1/carsclub_54643082.jpg
http://www.cars-club.com/up/sp/carsclub_74946335.jpg
:fly:
الطائرة بارون 58
Raytheon Beechcraft Baron (58)
The multi-engine Baron 58 is an all-metal complex aircraft stretched version of the Baron 55 with a six-person seating capacity including a crew of one or two The Misr Flying College fleet has two Baron 58s.
Beechcraft Baron 58
Specifications:
Speeds
Maximum speed at sea level 208 knots (386 km/hr)
Cruise, 80% power 8000 feet 192 knots (356 km/hr)
Performance
Range, 80% power at 8000 feet 1575 NM
Time 4.8 hours
Rate of climb at sea level: 1735 feet per minute
Service ceiling 20,688 feet
Weights & Loads
Maximum ramp weight 5524 pounds
Maximum takeoff weight 5500 pounds
Useful load 1578 pounds
Fuel
Fuel capacity 200 gallons
Usable fuel 194 gallons
Engine & Propeller
Engine: Teledyne Continental IO-550-C
Horsepower 300 BHP at 2700 RPM
Oil Capacity 12 quarts
http://www.cars-club.com/up/sp/carsclub_79987772.jpg
http://www.cars-club.com/up/sp/carsclub_62746017.jpg
http://www.cars-club.com/up/sp/carsclub_22037433.jpg
http://www.cars-club.com/up/sp/carsclub_25423192.jpg
http://www.cars-club.com/up/sp/carsclub_84818909.jpg
http://www.cars-club.com/up/sp/carsclub_62364408.jpg
الطائرة بونانزا ف-33-أ
Raytheon Beechcraft Bonanza (F33A)
The Bonanza F33A aircraft is an all metal, single-engine piston, low-wing monoplane constant speed propeller and retractable landing gear with a four-person seating capacity including a crew of one or two used for complex training. The Misr Flying College fleet has four Bonanza F33As.
Beechcraft Bonanza F33A
Specifications:
Speeds
Maximum speed at sea level 196 knots
Stall speed, flaps up 56 knots
Stall speed flaps down 47 knots
Performance
Weights & Loads
Maximum ramp weight 3412 pounds
Maximum takeoff weight 3400 pounds
Useful load xxx pounds
Baggage allowance 270 pounds
Fuel
Fuel capacity 80 gallons
Usable fuel 74 gallons
Engine & Propeller
Engine: Teledyne Continental IO-520-BB
Horsepower 285 BHP at 2700 RPM
Oil Capacity 12 quarts
http://www.cars-club.com/up/sp/carsclub_61921487.jpg
http://www.cars-club.com/up/sp/carsclub_75594775.jpg
http://www.cars-club.com/up/sp/carsclub_36914163.jpg
http://www.cars-club.com/up/sp/carsclub_53057268.jpg
http://www.cars-club.com/up/sp/carsclub_59139880.jpg
الطائرة كوماندور114-ب
Commander (114B)
The Commander 114B aircraft is an all metal, single-engine piston, low-wing monoplane constant speed propeller and retractable landing gear with a four-person seating capacity including a crew of one or two used for complex training. The Misr Flying College fleet has four Commander 114Bs
Commander 114B
Specifications:
Speeds
Maximum speed at sea level 164 knots (304 km/hr)
Cruise, 75% power 8000 feet 160 knots
Stall speed, flaps up 63 knots
Stall speed flaps down 54 knots
Performance
Range, 75% power at 8000 feet 630 NM
Time 4.5 hours
Rate of climb at sea level: 1070 feet per minute
Service ceiling 16,800 feet
Weights & Loads
Maximum ramp weight 3260 pounds
Maximum takeoff weight 3250 pounds
Useful load 1158 pounds
Baggage allowance 200 pounds
Fuel
Fuel capacity 70 gallons
Usable fuel 68 gallons
Engine & Propeller
Engine: Lycoming IO-540-T4B5
Horsepower 260 BHP at 2700 RPM
Oil Capacity 08 quarts
Propeller McCauley 3 Blades B3D32C419
http://www.cars-club.com/up/sp/carsclub_58800669.jpg
http://www.cars-club.com/up/sp/carsclub_84316933.jpg
http://www.cars-club.com/up/sp/carsclub_59921104.jpg
http://www.cars-club.com/up/sp/carsclub_54532511.jpg
http://www.cars-club.com/up/sp/carsclub_43020577.jpg
الطائرة سسنا 172-ر
Cessna Skyhawk (172R)
Commonly referred to as the Skyhawk, the Cessna 172R aircraft is an all metal, single-engine piston, high-wing monoplane with a four-person seating capacity including a crew of one or two. The Misr Flying College fleet has twelve Cessna 172s.
Cessna 172R
Specifications:
Speeds
Maximum speed at sea level 123 knots
Cruise, 80% power 8000 feet 122 knots
Stall speed, flaps up 51 knots
Stall speed flaps down 47 knots
Performance
Range, 80% power at 8000 feet 580 NM
Time 4.8 hours
Rate of climb at sea level: 720 feet per minute
Service ceiling 13,500 feet
Weights & Loads
Maximum ramp weight 2457 pounds
Maximum takeoff or landing weight 2450 pounds
Useful load 837 pounds
Baggage allowance 120 pounds
Fuel
Fuel capacity 56 gallons
Usable fuel 53 gallons
Engine & Propeller
Engine: Avco Lycoming IO-360-L2A
Horsepower 160 BHP at 2400 RPM
Oil Capacity 8 quarts
http://www.cars-club.com/up/sp/carsclub_86393819.jpg