Aircraft

 

Piper PA-28R-200 Arrow IIAC_Image_Piper_PA-28R-200_Arrow

N1147X is a 1975 Piper Arrow equipped with a 200 hp engine, retractable gear, 3-bladed constant speed prop, four seats and two 25-gallon fuel tanks. The aircraft is equipped for night and IFR operations and is a suitable trainer for both Instrument Ratings and Complex Aircraft Endorsements. Avionics include dual NAVCOMs, Garmin GNS 530 GPS, KT165 Mode C Transponder, and Piper Autoflight Autopilot. N1147X does not have the automatic gear extension feature installed on earlier Arrows.

Length: 24′ 7″
Height: 8′ 0″
Wingspan: 30′ 0″
Wing Area: 160.0 sq. ft.
Empty Weight: 1702 lbs.
Gross Weight: 2650 lbs.
Seats: 4
Powerplant: Lycoming IO-360-C1C, 200 HP, Four Cylinder
Range: 810 NM
Cruise Speed: 139 knots / 160 mph
Max Speed: 147 knots / 170 mph
Stall Speeds: 55 knots / 64 mph (gear and flaps down)
61 knots / 71 mph (gear and flaps up)
Sea Level Climb: 910 ft/min
GPS: Garmin GNS 530
IFR Certified: Yes
Cessna T-41C MescaleroT-41C

The T-41C Mescalero was designed and manufactured by Cessna, and delivered to the USAF for preliminary flight screening of pilot candidates. It is an all metal, single engine, high wing monoplane. The propeller is all metal, fixed pitch, and designed for best climb. The T-41C is powered by a horizontally-opposed, fuel-injected, six-cylinder, IO-360-D engine rated at 210 BHP at 2,800 RPM. In 1968 and 1969, the US Air Force Academy acquired 52 T-41C’s with the 210 HP engines and climb props for better high altitude performance at the USAF Academy in Colorado Springs. N7869N is on government loan to PRNFC.

Length: 26′ 11″
Height: 8′ 9.5″
Wingspan: 36′
Wing Area: 174.2 sq. ft.
Empty Weight: 1432 lbs.
Gross Weight: 2500 lbs.
Seats: 4
Powerplant: Continental IO-360, 210 HP, Fuel-Injected Six Cylinder
Range: 580 NM
Cruise Speed: 126 knots / 145 mph
Max Speed: 158 knots / 182 mph
Stall Speed: 52 knots / 60 mph
Sea Level Climb: 1100 ft/min
GPS: Garmin GNC 300XL
IFR Certified: No
Cessna C-172H/T-41A MescaleroT-41A

The T-41A Mescalero was designed and manufactured by Cessna, originally based on the successful 172F and delivered to the USAF for preliminary flight screening of pilot candidates. It is an all metal, single engine, high wing monoplane. The propeller is all metal and fixed pitch. The T-41A is powered by a horizontally-opposed, six-cylinder, O-300-D engine rated at 145 BHP at 2,700 RPM. N4980R is on government loan to the the PRNFC.

Length: 26′ 11″
Height: 8′ 9.5″
Wingspan: 36′ 2″
Wing Area: 174.2 sq. ft.
Empty Weight: 1369 lbs.
Gross Weight: 2300 lbs.
Seats: 2
Powerplant: Continental O-300, 145 HP, Six Cylinders
Range: 550 NM
Cruise Speed: 113 knots / 130 mph
Max Speed: 151 knots / 174 mph
Stall Speed: 51 knots / 59 mph
Sea Level Climb: 645 ft/min
GPS: None
IFR Certified: Limited (no pitot heat)
Cessna C-172N Skyhawk172

N7607E is a Cessna 172 equipped with a 160 hp engine and 38 gallon fuel capacity. The aircraft is equipped with two COM/NAV radios, a DME, and a marker beacon. N7607E is PRNFC’s primary initial trainer.

Length: 26′ 11”
Height: 8′ 9″
Wingspan: 36′
Wing Area: 174.2 sq. ft.
Empty Weight: 1393 lbs.
Gross Weight: 2300 lbs.
Seats: 4
Powerplant: Lycoming O-320-E2D, Four Cylinder
Range: 569 NM / 655 st. miles
Cruise Speed: 120 knots / 138 mph
Max Speed: 158 knots / 182 mph
Stall Speeds:  50 knots / 57 mph (flaps up)
 44 knots / 51 mph (flaps down)
Sea Level Climb: 770 ft/min
GPS: Garmin Aera 500
IFR Certified: No
Beechcraft T-34B MentorT-34

Our two T-34B Mentors, N84639 and N4028E, are single-engine, basic trainer aircraft designed and manufactured by Beechcraft Aircraft Company (now known as Hawker Beechcraft) for the United States Air Force and United States Navy. Originally derived from the Beechcraft Bonanza aircraft, around 2,300 T-34s were built between 1953 and 1959.

Length: 25′ 11”
Height: 9′ 8″
Wingspan: 32′ 10″
Wing Area: 178 sq. ft.
Empty Weight: 2295 lb.
Gross Weight: 2985 lb.
Seats: 2
Powerplant: Continental 0-047-4, 225 HP, Six Cylinder
Range: 660 NM
Cruise Speed: 130 knots
Max Speed: 219 knots / 251 mph
Stall Speeds: 50 knots / 58 mph (gear and flaps down)
62 knots / 71 mph (gear and flaps up)
Sea Level Climb: 1,000 ft/min
GPS: Garmin GPSMAP 296
IFR Certified: No