1972 PA-28R-200
Piper PA-28R Arrow II · Specifications
Overview
This document provides specifications for the Piper PA-28R-200, also known as the Cherokee Arrow II. It is intended for pilots and aviation enthusiasts who require detailed information about the aircraft's performance, weight, fuel capacity, and engine specifications. The document outlines critical data necessary for flight planning and operational understanding of the aircraft. Key specifications include engine details, fuel requirements, weight limits, and performance metrics, which are essential for safe and efficient operation of the aircraft.
- Engine: Lycoming IO-360-C1C, 200 HP, 4 cylinders.
- Fuel capacity: 50 gallons, minimum octane 100, average burn 10.15 gallons/hour at 75% power.
- Max takeoff/landing weight: 2,650 lbs; standard empty weight: 1,499 lbs; max useful load: 1,151 lbs.
- Max speed: 186 KCAS; max structural cruising speed: 148 KCAS; stall speed clean: 62 knots.
- Best rate of climb: 900 FPM; service ceiling: 15,000 ft.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Specifications
- Year ·
- 1972
- Pages ·
- 2
- File size ·
- 28 KB
- Copy found at ·
- airmart.com
What is the 1972 PA-28R-200?
The 1972 PA-28R-200 is a specifications for the Piper PA-28R Arrow II, dated 1972.
How many pages is the 1972 PA-28R-200?
The copy of the 1972 PA-28R-200 on file runs 2 pages.
What year was the 1972 PA-28R-200 published?
The 1972 PA-28R-200 — the Piper PA-28R Arrow II specifications on file — is dated 1972.
Most owners only have the POH. Here's the essential set for the Piper PA-28R Arrow II.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Piper PA-28R Arrow IImanuals & documents
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In this document
Engine Specifications
The Piper PA-28R-200 is equipped with a Lycoming IO-360-C1C engine, featuring 4 cylinders and a displacement of 361 cubic inches. It produces 200 horsepower and utilizes fuel injection.
Fuel Capacity and Consumption
The aircraft has a fuel capacity of 50 gallons, requiring a minimum octane rating of 100. Under standard conditions, the average fuel burn at 75% power is 10.15 gallons per hour.
Weights and Capacities
The maximum takeoff and landing weight for the normal category is 2,650 lbs. The standard empty weight is 1,499 lbs., allowing for a maximum useful load of 1,151 lbs. The baggage capacity is limited to 200 lbs. The oil capacity is 8 quarts.
Performance Specifications
The aircraft has a maximum speed of 186 KCAS and a maximum structural cruising speed of 148 KCAS. The stall speed in a clean configuration is 62 knots, while the landing configuration stall speed is 56 knots. The best rate of climb is 900 feet per minute, with a service ceiling of 15,000 feet.
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
1972 PA-28R-200 Piper Cherokee Arrow II Engine: Model Lyc. IO-360-C1C No. Cylinders 4 Displacement 361 cu. in. HP 200 Carbureted or Fuel Injected Fuel Injected Fixed Pitch/ Constant Speed Propeller Constant Speed Fuel: Fuel Capacity 50 gallons Min. Octane Fuel 100 Avg. Fuel Burn at 75% power in standard conditions per hour 10.15 gallons Weights and Capacities: Takeoff/Landing Weight Normal Category 2,650 lbs. Takeoff/Landing Weight Utility Category N/A Standard Empty Weight 1,499 lbs. Max. Useful Load Normal Category 1,151 lbs. Max. Useful Load Utility Category N/A Baggage Capacity 200 lbs. Oil Capacity 8 quarts Performance Do Not Exceed Speed 186 KCAS Max. Structural Cruising Speed 148 KCAS Stall Speed Clean 62 Knots Stall Speed Landing Configuration 56 Knots Climb Best Rate 900 FPM Wing Loading 15.6 lbs./sq ft. Power Loading 13.25 lbs./hp. Service Ceiling 15,000 ft.