Airplane Flight Manual
Piper PA-28R Arrow IV · Flight Manual
Overview
This Airplane Flight Manual (AFM) provides essential information for the operation of the Piper PA-28R Arrow IV. It is designed for pilots and aviation enthusiasts, detailing the aircraft's specifications, performance data, operating procedures, and safety information. The manual serves as a comprehensive guide to ensure safe and efficient flight operations, covering various aspects such as weight and balance, engine performance, and emergency procedures. Pilots will find critical data necessary for flight planning and in-flight decision-making, making it an invaluable resource for both training and operational use.
- Wingspan: 36 ft 0 in (10.97 m)
- Maximum Takeoff Weight: 2,800 lbs (1,270 kg)
- Cruise Speed: 138 knots (158 mph)
- Stall Speed: 54 knots (62 mph)
- Service Ceiling: 15,000 ft (4,572 m)
Document
Source
Originally published by tampabayaviation.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Flight Manual
- Pages
- 168
- File size
- 49 MB
- Publisher
- tampabayaviation.com
Most owners only have the POH. Here's the essential set for the Piper PA-28R Arrow IV.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Aircraft Specifications
The Piper PA-28R Arrow IV features a low-wing design with a wingspan of 36 feet 0 inches (10.97 meters) and a length of 26 feet 10 inches (8.18 meters). The maximum takeoff weight is 2,800 lbs (1,270 kg), and the useful load is approximately 1,000 lbs (454 kg). The aircraft is powered by a Lycoming IO-360-C1C engine, providing 180 horsepower.
Performance Data
The Arrow IV has a maximum cruise speed of 138 knots (158 mph) and a stall speed of 54 knots (62 mph). The service ceiling is 15,000 feet (4,572 meters), and the range is approximately 600 nautical miles (1,111 km) with standard fuel reserves.
Operating Procedures
Pilots are required to perform a thorough preflight inspection, including checks of fuel levels, oil quantity, and control surfaces. The engine start procedure involves ensuring the mixture is rich, the throttle is open 1/4 inch, and the ignition switch is in the 'Start' position.
Emergency Procedures
In the event of an engine failure during takeoff, pilots should maintain control of the aircraft, pitch for best glide speed, and identify a suitable landing area. For electrical failures, the pilot should check circuit breakers and switches before considering a return to the airport.
Weight and Balance
Proper weight and balance calculations are critical for safe flight operations. The manual includes charts and formulas to assist pilots in determining the center of gravity and ensuring the aircraft is within weight limits.
Safety notes
- Always perform a preflight inspection before each flight.
- Ensure weight and balance calculations are accurate to avoid performance issues.
- In case of engine failure, maintain control and glide to a suitable landing area.