PIPER PA-32 SARATOGA II TC

Piper PA-32 Saratoga II TC · Weight And Balance

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Overview

This document provides detailed specifications and performance data for the Piper PA-32 Saratoga II TC, a six-seat aircraft powered by a Textron Lycoming TIO-540-AHIA engine with 300 horsepower. It outlines critical dimensions, weight limits, fuel capacities, and performance metrics essential for pilots and aviation enthusiasts. The information is based on manufacturer's calculations and standard conditions, making it a reliable reference for understanding the aircraft's capabilities and limitations.

Max gross weight: 3,600 lb
Empty weight: 2,478 lb
Useful load: 1,137 lb
Takeoff distance over 50-ft obstacle: 1,810 ft
Max operating altitude: 20,000 ft
Cruise speed at high-speed power: 176 kt at 10,000 ft
Max demonstrated crosswind component: 17 kt

Document

Source

Originally published by airmart.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Weight And Balance
Pages: 1
File size: 34 KB
Publisher: airmart.com

Specifications & performance

Extracted from this document.

Specifications

Range (nm): 750
Engine (hp): 300
Height (ft): 8
Length (ft): 27
Propeller: Hartzell three-blade, constant speed
Wingspan (ft): 36
Engine model: Textron Lycoming, TIO-540-AHIA
Max speed (kt): 176
Cruise speed (kt): 160
Empty weight (lb): 2,478
Fuel capacity (gal): 107
Rate of climb (fpm): 950
Service ceiling (ft): 20,000
Max takeoff weight (lb): 3,600

Performance

Fuel burn (gph): 20
Landing over 50ft: 1,700
Max crosswind (kt): 17
Takeoff over 50ft: 1,810
Landing distance (ft): 880
Takeoff distance (ft): 1,110
Stall speed clean (kt): 67
Stall speed landing (kt): 63

V-speeds

VA: 134
VR: 80
VY: 80
VFE: 110
VNE: 191
VNO: 167
VS1: 67
VSO: 63

Weight & balance

Useful load (lb): 1,137
Max ramp weight (lb): 3,615
Baggage allowance (lb): 100
Basic empty weight (lb): 2,478
Max landing weight (lb): 3,600
Max takeoff weight (lb): 3,600

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In this document

Specifications

The specifications section details the aircraft's powerplant, dimensions, weights, and capacities. The Piper PA-32 Saratoga II TC is powered by a Textron Lycoming TIO-540-AHIA engine, producing 300 hp. It has an empty weight of 2,478 lb and a maximum gross weight of 3,600 lb, with a useful load of 1,137 lb. The aircraft features a wingspan of 36 ft 2 in and a wing area of 178.3 sq ft.

Performance

This section outlines the performance capabilities of the Piper PA-32 Saratoga II TC, including takeoff and landing distances, climb rate, and cruise speeds. The takeoff distance over a 50-ft obstacle is 1,810 ft, while the landing distance over a 50-ft obstacle is 1,700 ft. The aircraft can achieve a rate of climb of 950 feet per minute at sea level.

Limiting and Recommended Airspeeds

The document specifies various airspeeds critical for safe operation. For instance, the best rate of climb (VY) with gear down and flaps up is 80 KIAS, while the never exceed speed (VNE) is 191 KIAS. These speeds are essential for pilots to ensure safe flight operations.

Safety notes

All specifications are based on manufacturer's calculations.
Performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.

Full document text

PIPER PA-32 SARATOGA II TC SPECIFICATIONS Powerplant: Textron Lycoming, TIO-540-AHIA, 300 hp Recommended TBO: 2,000 hr Propeller: Hartzell three-blade, constant speed, 77- to 78-in dia Length: 27 ft 10.5 in Height: 8 ft 6 in Wingspan: 36 ft 2 in Wing area: 178.3 sq ft Wing loading: 20.2 lb/sq ft Power loading: 12 lb/hp Seats: 6 Cabin length: 10 ft 4 in Cabin width: 4 ft Cabin height: 3 ft 6 in Empty weight: 2,478 lb Max ramp weight: 3,615 lb Max gross weight: 3,600 lb Useful load (std.): 1,137 lb Payload w/full fuel: 525 lb Max takeoff weight: 3,600 lb Max landing weight: 3,600 lb Fuel capacity: 107 gal (102 gal usable), 642 lb (612 lb usable) Oil capacity: 12 qt Baggage capacity: Forward - 100 lb, 7 cu ft; Aft - 100 lb, 17.3 cu ft PERFORMANCE Takeoff distance, ground roll: 1,110 ft Takeoff distance over 50-ft obstacle: 1,810 ft Max demonstrated crosswind component: 17 kt Rate of climb, sea level: 950 fpm Cruise speed/range w/45-min reserve, std fuel (fuel consumption): @ High-speed power, peak TIT, 10,000 ft - 176 kt/750 nm (20 gph) @ Long-range power, peak TIT, 16,000 ft - 160 kt/995 nm (12.5 gph) Max operating altitude: 20,000 ft Landing distance over 50-ft obstacle: 1,700 ft Landing distance, ground roll: 880 ft LIMITING AND RECOMMENDED AIRSPEEDS VY (best rate of climb): Gear down, flaps up - 80 KIAS Gear up, flaps up - 95 KIAS V A (design maneuvering): 134 KIAS V FE (max flap extended): 110 KIAS VLE (max gear extended): 132 KIAS VLO (max gear operating): Extend - 132 KIAS Retract - 110 KIAS V NO (max structural cruising): 167 KIAS VNE (never exceed): 191 KIAS VR (rotation): 80 KIAS VS1 (stall, clean): 67 KIAS VSO (stall, in landing configuration): 63 KIAS For more information, contact Piper Aircraft, 2926 Piper Drive, Vero Beach, Florida 32960; telephone 772/567-4361; http://www.piper.com/ All specifications are based on manufacturer's calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.

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