PA-28R-201 ARROW III
Piper PA-28R Arrow III · Specifications
Overview
This document provides specifications for the Piper PA-28R Arrow III, detailing vital statistics such as engine performance, operating weights, fuel and electrical systems, and cruise performance metrics. It serves as a technical reference for pilots and aviation enthusiasts interested in the operational capabilities and design features of the Arrow III. The specifications include critical information on engine type, fuel capacity, weight limits, and performance data at various power settings, making it a comprehensive guide for understanding the aircraft's performance and maintenance requirements.
- Engine Model: Lycoming IO-360-C1C6, 200 HP, 2700 RPM
- Maximum Gross Takeoff Weight: 2750 lbs
- Total Fuel Capacity: 77 gallons, Usable: 72 gallons
- Average Cruise TAS: 137 KTS @ 75% power
- Average Fuel Consumption: 10.2 GPH @ 75% power
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at www.beverlyflightcenter.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Specifications
- Pages ·
- 2
- File size ·
- 14 KB
- Copy found at ·
- www.beverlyflightcenter.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp) ·
- 200
- Propeller ·
- constant speed, variable pitch, non-feathering
- Engine model ·
- Lycoming IO-360-C1C6
- Max speed (kt) ·
- 137
- Fuel capacity (gal) ·
- 77
- Max takeoff weight (lb) ·
- 2,750
Performance
- Fuel burn (gph) ·
- 10.2
Weight & balance
- Baggage allowance (lb) ·
- 200
- Max landing weight (lb) ·
- 2,750
- Max takeoff weight (lb) ·
- 2,750
What is the PA-28R-201 ARROW III?
The PA-28R-201 ARROW III is a specifications for the Piper PA-28R Arrow III.
How many pages is the PA-28R-201 ARROW III?
The copy of the PA-28R-201 ARROW III on file runs 2 pages.
Most owners only have the POH. Here's the essential set for the Piper PA-28R Arrow III.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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- PREFLIGHT PA28R-201 PIPER ARROW III PREFLIGHTChecklist
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- Pilot’s Operating Handbook and FAA Approved Airplane Flight ManualWeight & Balance
- Pilot's Operating HandbookPilot's Operating Handbook
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- Piper PA-28R Arrow III Pilot's Operating HandbookPilot's Operating Handbook
- Performance Data for the Piper PA-28R Arrow IIIPerformance Data
- EMERGENCY PROCEDURESEmergency Procedures
- N809M Piper Arrow III - ChecklistChecklist
- Piper Arrow III Nice AirChecklist
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In this document
Engine Specifications
The Piper PA-28R Arrow III is powered by a Lycoming IO-360-C1C6 engine, which is a direct-drive, horizontally opposed, fuel-injected, four-cylinder, air-cooled engine. It delivers a maximum horsepower of 200 and operates at a maximum RPM of 2700.
Operating Weights
The maximum gross takeoff weight and maximum gross landing weight for the Arrow III are both 2750 lbs. The baggage compartment has a maximum capacity of 200 lbs.
Fuel System
The fuel system of the Arrow III requires 100LL fuel (100/130 minimum grade) with a total fuel capacity of 77 gallons. Of this, 72 gallons are usable (36 gallons in each wing), and there are 5 gallons of unusable fuel. The aircraft features two fuel tanks and three fuel drains.
Cruise Performance
At a pressure altitude of 5000 feet and standard outside air temperature, the Arrow III achieves an average cruise true airspeed (TAS) of 137 knots at 75% power, 127 knots at 65% power, and 113 knots at 55% power. Average fuel consumption is 10.2 gallons per hour at 75% power, 9.2 GPH at 65% power, and 8.0 GPH at 55% power.
Electrical System
The electrical system includes a 12-volt battery rated at 35 amperes and a 60-ampere alternator providing 14 volts. This setup supports the aircraft's electrical needs effectively.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
PA-28R-201 ARROW III Vital Statistics Engine Engine Model: Lycoming IO-360-C1C6 Type: direct-drive, horizontally opposed, fuel-injected, four-cylinder, air cooled Horsepower: 200 Maximum RPM: 2700 Operating Weights Maximum Gross Takeoff Weight: 2750 lbs. Maximum Gross Landing Weight: 2750 lbs. Baggage Compartment: 200 lbs. maximum Oil System Type: wet sump Minimum Level: 2 quarts Maximum Level: 8 quarts Fuel System Fuel Grade: 100LL (100/130 minimum grade) Total Capacity: 77 Gallons Total Usable: 72 Gallons (36 each wing) Total Unusable: 5 Gallons Fuel Tanks: 2 Fuel Drains: 3 Fuel Pumps: one engine-driven; one electric auxilary Electrical System Battery: one at 35 amperes, 12 volts Alternator: one at 60 amperes, 14 volts Vacuum System Pumps: one engine-driven Normal suction: 4.8 to 5.2 In/Hg Flap System Type: manual Settings: 0°, 10°, 25°, 40° Propeller System Type: constant speed, variable pitch, non-feathering Landing Gear System Type: electro-hydraulic Reservoir: self-contained, independent of brake system Power source: reversible electric motor Features: downlocks and emergency extension Tire Sizes: 5.00 X 5 nose; 6.00 X 6 main Strut Inflation: 2.5 inches nose; 2.75 inches main Brake System Type: hydraulic Reservoir: external, independent of landing gear system Features: disk brakes on main gear; parking brake Pitot Static System Pitot Source: probe under left wing Static Source: one static port on either side of rear empennage Features: alternate air system; pitot heat Cruise Performance (based on 5000 feet Pressure Altitude, Standard OAT) Average Cruise TAS: 137 KTS @ 75% power, Best Economy Leaning 127 KTS @ 65% power, Best Economy Leaning 113 KTS @ 55% power, Best Economy Leaning Average Fuel Consumption: 10.2 GPH @ 75% power, Best Economy Leaning 9.2 GPH @ 65% power, Best Economy Leaning 8.0 GPH @ 55% power, Best Economy Leaning