Specifications Performance Turbo Arrow IV PA 28RT-201 T

Piper PA-28RT Arrow IV Turbo · Performance Data

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Overview

This document provides detailed performance specifications for the Piper PA-28RT Arrow IV Turbo, model PA 28RT-201 T, manufactured by Piper Aircraft Corporation in 1984. It is intended for pilots and aviation enthusiasts seeking comprehensive data on the aircraft's capabilities, including engine specifications, weight limits, dimensions, fuel capacity, and performance metrics. The document outlines critical performance figures such as maximum speed, cruising speeds, fuel consumption rates, and takeoff and landing distances, making it a valuable resource for flight planning and operational understanding.

Engine: Continental TSIO-360-FB, 200 hp @ 2575 RPM
Maximum Speed: 178 knots (328 km/h) at gross weight
Cruise Range: Over 1,560 nautical miles (2,893 km)
Takeoff Distance: 790 feet (1463 m) ground run
Fuel Consumption at 75% power: 12.0 gph (45.4 lph)

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Source

Originally published by aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Performance Data
Year: 1984
Pages: 7
File size: 4.0 MB
Publisher: aeroresourcesinc.com

Specifications & performance

Extracted from this document.

Specifications

Engine (hp): 200
Height (ft): 8.3
Length (ft): 26
Propeller: Hartzell
Wingspan (ft): 36
Engine model: TSIO-360-FB
Max speed (kt): 178
Cruise speed (kt): 66
Empty weight (lb): 1,692
Fuel capacity (gal): 38.5
Rate of climb (fpm): 830
Service ceiling (ft): 20,000
Max takeoff weight (lb): 2,900

Performance

Fuel burn (gph): 12
Landing over 50ft: 775
Takeoff over 50ft: 900
Landing distance (ft): 725
Takeoff distance (ft): 900
Stall speed clean (kt): 164
Stall speed landing (kt): 168

V-speeds

VS1: 61
VSO: 61

Weight & balance

Useful load (lb): 1,208
Max ramp weight (lb): 2,912
Baggage allowance (lb): 200
Basic empty weight (lb): 1,692
Max landing weight (lb): 2,900
Max takeoff weight (lb): 2,900

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the Piper PA-28RT Arrow IV Turbo.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

More Piper PA-28RT Arrow IV Turbomanuals & documents

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In this document

Engine Specifications

The Piper PA-28RT Arrow IV Turbo is powered by a Continental TSIO-360-FB engine, rated at 200 horsepower at 2575 RPM for both takeoff and continuous operation. It features six cylinders and has a recommended time between overhaul (TBO) of 1800 hours.

Weights and Dimensions

The aircraft has a ramp weight of 2912 lbs (1321 kg) and a gross weight of 2900 lbs (1315 kg). The standard empty weight is 1692 lbs (767 kg), providing a useful load of 1208 lbs (548 kg). The wing area is 170 ft² (15.8 m²) with a wing loading of 17.0 lbs/ft² (83.0 kg/m²).

Performance Metrics

The maximum speed at gross weight is 178 knots (328 km/h) at an altitude of 14,000 feet. The aircraft achieves cruising speeds of 166 knots (307 km/h) at 75% power and 162 knots (300 km/h) at 55% power. The cruise range at long-range cruise power is over 1,560 nautical miles (2,893 km).

Fuel Consumption

At high-speed cruise power (75%), the fuel consumption is 12.0 gallons per hour (45.4 liters per hour). For economy cruise power (65%), it is 11.0 gallons per hour (41.6 liters per hour), and at long-range cruise power (55%), it is 10.8 gallons per hour (40.9 liters per hour).

Takeoff and Landing Distances

The takeoff distance at sea level with zero wind and standard temperature is 790 feet (1463 m) for ground run and 900 feet (1667 m) to clear a 50-foot obstacle. The landing distance is 695 feet (1278 m) for ground roll and 775 feet (1435 m) to clear a 50-foot obstacle.

Full document text

••• •• - - - I~ -- I , ( .. Piper Aircraft Corporation 1984 Spec ificati on sl Perform an ce Turbo Arrow IV PA 28RT-201 T ~"'-1"'4 :---110.32"-- T3'1.12" _J 211.15" 1'3.12" ! Piper Aircraft Corporation Turbo Arrow IV PA 28RT-201 T Specifications 38/96.5 - 34.5/87.6 22/55.9 x 20/55.8 36/91.4 x 35/88.9 7.86/2.40 10.47/3.19 ENGINE Manufacturer Model Rating (hp @ rpm) (Take-off) Rating (hp @ rpm) (Continuous) Number of Cylinders Recommended TBO (hrs.) PROPELLER Manufacturer Number of Blades Type Diameter (in./cm.) WEIGHTS Ramp Weight (Ibs./kg.) Gross Weight (Ibs.lkg.) Standard Empty Weight (Ibs.lkg.) (Includes; unusable fuel, full operating fluids and full oil) Standard Useful Load (Ibs./kg.) WING AREA AND LOADINGS Wing Area (ft2/m2) Wing Loading (lbs./ft.2) (kg./m2) Power Loading (Ibs./hp) (kg./hp) Continental TSIO-360-FB 200 @ 2575 200 @ 2575 6 18001 Hartzell 2 Constant Speed 76/193 2912/1321 2900/1315 1692/767 1208/548 170/15.8 17.0/83.0 14.5/6.6 DIMENSIONS Wing Span (ft.lm) Length (It./ m) Height (fUm) Cabin Length (Instrument Panel to Rear Bulkhead) (in./cm.) Cabin Width (in.lcm.) Cabin Height (in./cm.) Headroom (Seat to Ceiling) Front Seat (in.lcm.) Rear Seat (in.lcm.) Baggage Door Size (in.lcm.) Cabin Door Size (in.lcm.) Wheel Base (ft.lm) Wheel Tread (ft.lm) FUEL CAPACITY Two 38.5 gal. tanks (gaL/L) Usable Fuel (gaL/L) OIL CAPACITY (qts.lL) BAGGAGE Volume (ft3/m3) (with 2 cu. ft. hat shelf) Capacity (Ibs./kg.) 35.4/10.8 27.3/8.3 8.3/2.5 93.25/236.9 41.75/106.1 44.75/113.7 77/291.4 72/272.5 8/7.57 26/.74 200/91 Performance MAXIMUM SPEED (kts.lkmh) (TAS at Gross Weight) CRUISING SPEEDS (TAS at Gross Weight) Optimum Altitude High Speed Cruise Power (75%) (kts./kmh) Economy Cruise Power (65%) (kts./kmh) Long Range Cruise Power (55%) (kts./kmh) CRUISE RANGE (Cruising range includes 45-minute fuel reserve at long range cruise power plus allowance for fuel used during taxi, take-off climb at MCP, cruise at optimum altitude and stated mixture plus descent) 178/328 (14,000 ft.) (205 mph) IAS CAS 61/113 58/107 66/122 63/117 20,000+ /6100+* Best Powe r 9.2/34.8 940/286 10.8/40.9 1110/337 1620/493 645/196 1560/475 Best Economy 12.0/45.4 14.0/53.0 12.7/48.1 11.0/41.6 FUEL CONSUMPTION High Speed Cruise Power (75%) (gph.llph) Economy Cruise Power (65%) (gph.llph) Long Range Cruise Power (55%) (gph.llph) RATE OF CLIMB (At Sea Level and Gross Wt.) Full Throttle (fpm/mpm) STALL SPEED Flaps Down, Full 40° (kts.lkmh) Flaps Up (kts.lkmh) SERVICE CEILING (100 fpm) (ft./m) TAKE-OFF DISTANCE (Sea Level, Zero Wind, Standard Temperature, 25° Flaps) Ground Run (ft./m) Total over 50-ft. obstacle (ft.lm) LANDING DISTANCE (Sea.Level, Zero Wind, Standard Temperature) Ground Roll (ft.lm) Total over 50-ft. obstacle (ft.lm) 168/311 164/302 153/284 830/1537 900/1667 Best Economy Best Economy 790/1463 Best Power 172/318 167/308 157/291 Best Power 695/1278 775/1435 725/1343 High Speed Cruise Power (75%) (nm/km) Economy Cruise Power (65%) (nm/km) Long Range Cruise Power (55%) (nm/km) *20,000 ft. is maximum approved altitude for the Turbo Arrow IV.

All Piper PA-28RT Arrow IV Turbo performance data