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Specifications for the Piper Pilot 100i

Piper Pilot 100i · Specifications

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Overview

This document provides detailed specifications for the Piper Pilot 100i, a single-engine piston aircraft designed primarily for flight training. It outlines the aircraft's dimensions, weight capacities, fuel specifications, engine details, and avionics features. The Pilot 100i is positioned as an affordable yet capable training aircraft, emphasizing reliability and safety. Key performance metrics such as range, takeoff and landing distances, and cruise speed are also included, making this document a valuable resource for flight schools and aviation enthusiasts interested in the capabilities of the Piper Pilot 100i.

  • Usable fuel capacity: 48 US gallons (182 liters)
  • Maximum takeoff weight: 2,550 lb (1,157 kg)
  • Maximum range: 522 nautical miles (967 km)
  • Takeoff distance (over 50' obstacle): 1,608 ft (490 m)
  • Maximum cruise speed: 128 ktas (237 km/h)

Document

Source

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

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Document details

Type
Specifications
Year
2020
Pages
2
File size
178 KB
Publisher
www.piper.com

Specifications & performance

Extracted from this document.

Specifications

Range (nm)
522
Engine (hp)
180
Height (ft)
7
Length (ft)
24
Propeller
Sensenich 2-Blade
Wingspan (ft)
35
Engine model
Lycoming IO-360-B4A
Max speed (kt)
128
Empty weight (lb)
1,590
Fuel capacity (gal)
48
Max takeoff weight (lb)
2,550

Performance

Landing over 50ft
1,400
Takeoff over 50ft
1,608
Landing distance (ft)
1,400
Takeoff distance (ft)
1,608

Weight & balance

Useful load (lb)
968
Max ramp weight (lb)
2,558
Basic empty weight (lb)
1,590
Max takeoff weight (lb)
2,550
Documentation completeness
2/7

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In this document

Fuel Capacity

The Piper Pilot 100i has a usable fuel capacity of 48 US gallons (182 liters), providing sufficient range for training flights.

Dimensions

The aircraft has a wingspan of 35 feet 5 inches (10.8 meters), a height of 7 feet 3 inches (2.2 meters), and a length of 24 feet (7.3 meters), making it a compact and manageable aircraft for flight training.

Engine Specifications

The Pilot 100i is powered by a Lycoming IO-360-B4A engine, producing a flat-rated horsepower of 180 hp, which contributes to its performance and reliability.

Weights

The maximum takeoff weight of the Piper Pilot 100i is 2,550 pounds (1,157 kg), with a maximum ramp weight of 2,558 pounds (1,160 kg). The standard empty weight is 1,590 pounds (721 kg), allowing for a useful load of 968 pounds (439 kg).

Performance Metrics

The aircraft has a maximum range of 522 nautical miles (967 kilometers), a takeoff distance over a 50-foot obstacle of 1,608 feet (490 meters), and a landing distance over a 50-foot obstacle of 1,400 feet (427 meters). The maximum cruise speed is 128 knots true airspeed (237 km/h).

Full document text

VA L U E T R A I N E R | S I N G L E E N G I N E P I S T O N $ 298,900* 2021 Standard Equipped List Price INTERIOR AVIONICS 221 Piper Aircraft, Inc. | 2926 Piper Drive, Vero Beach, FL 32960 | 772.299.2403 | © 2020 Piper Aircraft, Inc. SIMPLICITY AND VALUE DEFINE THE PILOT 100i. YOUR FLIGHT TRAINING BUSINESS PLAN IS EASILY ACHIEVABLE WITH THIS UNRIVALED PRIMARY TRAINING AIRCRAFT. MEET YOUR FINANCIAL TARGETS WITHOUT NO COMPROMISES IN CAPABILITY, QUALITY, SAFETY OR RELIABILITY WITH THE PILOT 100i. FUEL CAPACITY Usable 48 US gal | 182 L DIMENSIONS Wingspan: 35 ft 5 in | 10.8 m Height: 7 ft 3 in | 2.2 m Length: 24 ft | 7.3 m ENGINE Lycoming IO-360-B4A Flat-Rated Horsepower at 180 hp PROPELLER Sensenich 2-Blade Fixed Pitch WEIGHTS Maximum Takeoff Weight: 2,550 lb | 1,157 kg Maximum Ramp Weight: 2,558 lb | 1,160 kg Standard Empty Weight: 1,590 lb | 721 kg Standard Useful Load: 968 lb | 439 kg SPECIFICATIONS AND PERFORMANCE Max Range 522 nm 967 km Takeoff Distance (Over 50’ Obstacle) 1,608 ft 490 m Landing Distance (Over 50’ Obstacle) 1,400 ft 427 m Max Cruise Speed 128 ktas 237 km/hr S TA N DA R D F EAT U R E S • GARMIN G3X Touch - Single 10.6” PFD with Connext® technology, configurable as a split PFD/MFD • Garmin G5 Standby • GFC500 Autopilot with Electronic Stability Protection • GNX 375 2” Touchscreen Nav/Xpndr w/ADS B In & Out • GNC 255A NAV/Comm Radio • GTR 20 2nd VHF COM Radio • GMA 245R Remote Audio Panel w/Bluetooth • Moving Map, Terrain, Obstacle, and Traffic Alerts, Synthetic Vision, Airport Directory, Flight Data Logging • Wet Compass • USB Charging Ports • LED Wing Tip Lights • Pilot, Co-Pilot, and Observer Seat with Headset Jacks and PTT • Vinyl Floor Covering • School Color Scheme with two Vinyl Trim Colors and Logo A D D I T I O N A L O P T I O N S • Am-Safe Seatbelts • ESP Disconnect at startup Additional Special Options | Quoted upon request