Piper PA-28R Arrow III Pilot's Operating Handbook
Piper PA-28R Arrow III · Pilot's Operating Handbook
Overview
This Pilot's Operating Handbook (POH) is specifically designed for the Piper PA-28R Arrow III. It serves as a comprehensive guide for pilots operating this aircraft, detailing essential information regarding performance, operating procedures, and safety protocols. The handbook includes specifications, limitations, and emergency procedures, ensuring that pilots have the necessary knowledge to operate the aircraft safely and efficiently. It is intended for both new and experienced pilots, providing a thorough understanding of the aircraft's systems and capabilities.
- Wingspan: 35 ft 10 in
- Maximum Takeoff Weight: 2,550 lbs
- Cruise Speed: 138 knots
- Stall Speed: 57 knots
- Service Ceiling: 15,000 ft
Document
Source
Originally published by www.istriacorp.com.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 212
- File size
- 48 MB
- Publisher
- www.istriacorp.com.au
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
- Type Certificate (TCDS)
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- PREFLIGHT PA28R-201 PIPER ARROW III PREFLIGHTChecklist
- AIRPLANE PARTS CATALOG ARCHER III PA-28-181 (SERIAL NUMBERS 2843001 AND UP)Parts Catalog
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- Pilot’s Operating Handbook and FAA Approved Airplane Flight ManualWeight And Balance
- Pilot's Operating HandbookPilot's Operating Handbook
- PA-28R-201 ARROW IIISpecifications
- Piper Arrow SpecsSpecifications
- Performance Data for the Piper PA-28R Arrow IIIPerformance Data
- EMERGENCY PROCEDURESEmergency Procedures
- PA-28R Arrow III – Operations ManualAvionics Manual
- N809M Piper Arrow III - ChecklistChecklist
In this document
Aircraft Specifications
The Piper PA-28R Arrow III features a low-wing design with a wingspan of 35 feet 10 inches and a length of 24 feet 8 inches. The maximum takeoff weight is 2,550 lbs, and it is powered by a Lycoming IO-360-C1C engine, producing 180 horsepower.
Performance Data
The aircraft has a maximum cruise speed of 138 knots and a stall speed of 57 knots. The service ceiling is 15,000 feet, and it has a range of approximately 600 nautical miles with standard fuel capacity.
Operating Procedures
Pilots should perform a thorough preflight inspection, including checking fuel levels, oil levels, and control surfaces. The recommended engine start procedure includes ensuring the mixture is rich and the throttle is set to 1/4 inch open.
Emergency Procedures
In the event of an engine failure, pilots should establish best glide speed and look for a suitable landing area. The emergency landing procedure includes securing the cabin, shutting off fuel, and preparing for landing.
Weight and Balance
Proper weight and balance calculations are crucial for safe flight operations. The handbook provides charts and formulas to determine the center of gravity and ensure the aircraft is within limits.
Safety notes
- Always perform a preflight inspection before flight.
- Ensure weight and balance calculations are within limits.
- In case of engine failure, establish best glide speed immediately.