Piper PA-32R Saratoga Pilot's Operating Handbook
Piper PA-32R Saratoga · Pilot's Operating Handbook
Overview
The Piper PA-32R Saratoga Pilot's Operating Handbook (POH) provides essential information for pilots operating this aircraft model. It covers various aspects of the aircraft's operation, including performance data, limitations, emergency procedures, and normal operating procedures. This handbook is designed to assist pilots in understanding the capabilities and limitations of the Saratoga, ensuring safe and efficient flight operations. It includes detailed specifications, weight and balance information, and checklists necessary for preflight, takeoff, landing, and emergency situations.
- Maximum takeoff weight: 3,600 lbs (1,632 kg)
- Cruise speed: 140 knots (161 mph)
- Stall speed: 60 knots (69 mph)
- Fuel capacity: 84 gallons (318 liters)
- Rate of climb: 1,000 feet per minute
Document
Source
Originally published by takeflightsandiego.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Pages
- 352
- File size
- 40 MB
- Publisher
- takeflightsandiego.com
Most owners only have the POH. Here's the essential set for the Piper PA-32R Saratoga.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
More Piper PA-32R Saratogamanuals & documents
- AAIB Bulletin: G-KNOW AAIB-28013Other Documents
- AIRWORTHINESS DIRECTIVE AD/PA-32/42 Amdt 3Airworthiness Directives
- Piper PA-32R Saratoga Turbo SP ChecklistChecklist
- SERVICE BULLETIN NO. 811AService Bulletins
- EMERGENCY PROCEDURES PIPER PA32R/301 SARATOGA (AFM 02.02.1981)Flight Manual
- 1980 PIPER TURBO SARATOGA SP | SN 32R-8029057 | ZS-AVESpecifications
- Normal Procedures for the Piper PA-32R SaratogaNormal Procedures
In this document
Aircraft Specifications
The PA-32R Saratoga features a low-wing design with a maximum takeoff weight of 3,600 lbs (1,632 kg). It is powered by a Lycoming IO-540-U4A5 engine, producing 260 horsepower. The aircraft has a wingspan of 36 feet 0 inches (10.97 m) and a length of 26 feet 10 inches (8.18 m). The fuel capacity is 84 gallons (318 liters), providing a range of approximately 600 nautical miles.
Performance Data
The PA-32R Saratoga has a stall speed of 60 knots (69 mph) in landing configuration. The maximum cruise speed is approximately 140 knots (161 mph) at 75% power. The rate of climb is about 1,000 feet per minute at sea level. Takeoff distance over a 50-foot obstacle is approximately 2,600 feet (792 m), while landing distance over a 50-foot obstacle is around 2,400 feet (732 m).
Weight and Balance
The maximum useful load for the PA-32R Saratoga is 1,200 lbs (544 kg). The center of gravity limits are from 34.0 inches to 40.0 inches aft of the datum. Pilots must ensure that the aircraft is within weight and balance limits before flight to maintain safe handling characteristics.
Emergency Procedures
In the event of an engine failure during takeoff, the recommended procedure is to maintain control of the aircraft, establish a glide attitude, and land straight ahead if possible. For electrical failures, pilots should switch off non-essential electrical equipment and land as soon as practical.
Normal Operating Procedures
Pilots should perform a preflight inspection, including checking fuel and oil levels, control surfaces, and overall aircraft condition. During takeoff, maintain a speed of 70 knots (81 mph) until reaching a safe altitude. For landing, approach speed should be approximately 70 knots (81 mph) with a landing configuration established.
Safety notes
- Always ensure the aircraft is within weight and balance limits before flight.
- In case of engine failure, maintain control and land straight ahead if possible.
- Perform thorough preflight inspections to ensure aircraft safety.