Catalog excerpts
PIPER AIRCRAFT IS PREPARING PILOTS FOR THE FUTURE OF AVIATION Piper Trainers give future career pilots the experience needed to prepare them to meet the growing demand for professional pilots while providing flight schools with the most cost-effective training platforms. SENECA | SEMINOLE | ARROW | ARCHER TX | ARCHER DX
Open the catalog to page 1PIPER TRAINERS
Open the catalog to page 2HIGHER LEARNING. Each Piper Aircraft interior is designed with maximum comfort and durability in mind. The ergonomic seating provides a relaxed environment allowing the pilot and instructor to focus on the task at hand. Heavyduty vinyl and wear-resistant synthetic leathers are hand-fitted to the seats and side-walls, purposed to withstand repetitive use. Air conditioning is an available option with most aircraft. Carpet or Vinyl Flooring Options Standard Interior: Seminole, Archer TX, Archer DX, Arrow Get acquainted with the softer side of rugged vinyl. The Archer TX’s interior is designed...
Open the catalog to page 3Piper Aircraft, Inc. is the first aircraft manufacturing company to place the Garmin G1000 NXi system into its training aircraft. Enhanced Automatic Flight Control System (AFCS)* The Garmin G1000 NXi as installed in the Seneca, Seminole and Archer brings a higher level of performance and capability to the flight deck. Beginning with a zero-time avionics start up, the crew is able to start their procedures without waiting for the avionics to “warm up”. Once in operation, the G1000 NXi high resolution glass displays the enhanced HSI map, surface watch, 3-D Synthetic Vision and other features...
Open the catalog to page 4ENGINE (2) Turbocharged Continental TSIO-360-RB Horsepower: 220 hp each Number of Cylinders: 6 TBO: 2,000 hours PROPELLER McCauley 3-Blade: Constant Speed | Full-Feathering | Counter-Rotating WEIGHTS Maximum Takeoff Weight: 4,750 lbs | 2,155 kg Maximum Ramp Weight: 4,773 lbs | 2,165 kg Standard Equipped Weight: 3,442 lbs | 1,561 kg Standard Useful Load: 1,331 lbs | 604 kg MAXIMUM CRUISE SPEED 200 ktas | 370 km/h FUEL CAPACITY 122 US gal | 462 liters (Usable) RANGE WITH 45 MIN. RESERVE 828 nm | 1,534 km MAXIMUM APPROVED ALTITUDE 25,000 ft | 7,620 m SINGLE ENGINE SERVICE CEILING 16,500 ft |...
Open the catalog to page 5ENGINES (2) Lycoming O-360-A1H6 Horsepower: 180 hp each Number of Cylinders: 4 TBO: 2,200 hours PROPELLERS Hartzell 2-Blade: Constant Speed | Full-Feathering WEIGHTS Maximum Takeoff Weight: 3,800 lbs | 1,724 kg Maximum Ramp Weight: 3,816 lbs | 1,731 kg Standard Equipped Weight: 2,625 lbs | 1,191 kg Standard Useful Load: 1,191 lbs | 540 kg CRUISING SPEED 162 ktas | 300 km/h (75% power) FUEL CAPACITY 108 US gal | 409 liters (Usable) RANGE WITH 45 MIN. RESERVE 700 nm | 1,296 km SERVICE CEILING 15,000 ft | 4,572 m Single Engine: 3,800 ft | 1,158 m TAKEOFF DISTANCE Ground Roll: 1,100 ft | 335...
Open the catalog to page 6ENGINE Lycoming IO-360-C1C6 Horsepower: 200 hp Number of Cylinders: 4 TBO: 2,200 hours PROPELLER McCauley | 2-Blade | Constant Speed WEIGHTS Maximum Takeoff Weight: 2,750 lbs | 1,247 kg Maximum Ramp Weight: 2,758 lbs | 1,251 kg Standard Equipped Weight: 1,798 lbs | 816 kg Standard Useful Load: 960 lbs | 435 kg CRUISING SPEED 137 ktas | 254 km/h (75% power) FUEL CAPACITY 72 US gal | 273 liters (Usable) RANGE WITH 45 MIN. RESERVE 880 nm | 1,630 km SERVICE CEILING 16,200 ft | 4,938 m TAKEOFF DISTANCE Ground Roll: 1,000 ft | 305 m Total Over 50 ft Obstacle: 1,600 ft | 487 m LANDING...
Open the catalog to page 7PIPER ARCHER TX ENGINE Lycoming O-360-A4M Horsepower: 180 hp Number of Cylinders: 4 TBO: 2,200 hours PROPELLER Sensenich | 2-Blade | Fixed Pitch WEIGHTS Maximum Takeoff Weight: 2,550 lbs | 1,157 kg Maximum Ramp Weight: 2,558 lbs | 1,160 kg Standard Equipped Weight: 1,688 lbs | 766 kg Standard Useful Load: 870 lbs | 395 kg CRUISING SPEED 128 ktas | 237 km/h (75% power) FUEL CAPACITY 48 US gal | 182 liters (Usable) RANGE WITH 45 MIN. RESERVE 522 nm | 967 km SERVICE CEILING 14,100 ft | 4,298 m TAKEOFF DISTANCE Ground Roll: 1,135 ft | 346 m Total Over 50 ft Obstacle: 1,608 ft | 490 m LANDING...
Open the catalog to page 8ENGINE Continental CD-155 Horsepower: 155 hp Number of Cylinders: 4 PROPELLER MT 3-Blade | Constant Speed WEIGHTS Maximum Takeoff Weight: 2,550 lbs | 1,157 kg Maximum Ramp Weight: 2,558 lbs | 1,160 kg Standard Equipped Weight: 1,764 lbs | 800 kg Standard Useful Load: 794 lbs | 360 kg CRUISING SPEED 123 ktas | 228 km/h (75% power) FUEL CAPACITY 48 US gal | 182 liters (Usable) RANGE WITH 45 MIN. RESERVE 848 nm | 1,570 km SERVICE CEILING 16,100 ft | 4,877 m TAKEOFF DISTANCE Ground Roll: 919 ft | 280 m Total Over 50 ft Obstacle: 1,673 ft | 510 m LANDING DISTANCE Ground Roll: 920 ft | 280...
Open the catalog to page 9EXPERIENCE THE FREEDOM OF FLIGHT IN A PIPER AIRCRAFT
Open the catalog to page 10Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries and G1000® and G3000® are registered trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.
Open the catalog to page 11All Piper Aircraft catalogs and technical brochures
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