Specifications for the Piper Pilot 100i
Piper Pilot 100i · Specifications
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)
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at www.piper.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Specifications
- Year ·
- 2020
- Pages ·
- 2
- File size ·
- 178 KB
- Copy found at ·
- 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
What is the Specifications for the Piper Pilot 100i?
The Specifications for the Piper Pilot 100i is a specifications for the Piper Pilot 100i, dated 2020.
How many pages is the Specifications for the Piper Pilot 100i?
The copy of the Specifications for the Piper Pilot 100i on file runs 2 pages.
What year was the Specifications for the Piper Pilot 100i published?
The Specifications for the Piper Pilot 100i — the Piper Pilot 100i specifications on file — is dated 2020.
Most owners only have the POH. Here's the essential set for the Piper Pilot 100i.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More Piper Pilot 100imanuals & documents
See all 13 →- Piper Pilot 100i Model GuideModel Guide
- SERVICE BULLETIN NO. 1423AService Bulletins
- CUSTOMER SERVICE INFORMATION FILEWiring Diagrams
- CUSTOMER SERVICE INFORMATION FILETraining Manual
- SERVICE BULLETIN NO. 1375BMaintenance Manual
- SERVICE BULLETIN NO. 1399Service Bulletins
- SERVICE BULLETIN NO. 1355Service Bulletins
- Emergency Procedures for the Piper Pilot 100iEmergency Procedures
- Pilot's Operating Handbook for the Piper Pilot 100iPilot's Operating Handbook
- Weight & Balance for Piper Pilot 100iWeight & Balance
- Weight & Balance for Piper Pilot 100iWeight & Balance
- Piper Pilot 100i Weight & BalanceWeight & Balance
Related documents
- Piper Pilot 100i Model GuidePiper Pilot 100i · Model Guide
- Piper Pilot 100 Model GuidePiper Pilot 100 · Model Guide
- Specifications for the Piper M500Piper M500 · Specifications
- Piper M600 SLS Pilot's Operating HandbookPiper M600/SLS · Pilot's Operating Handbook
- Piper M500 Pilot's Operating HandbookPiper M500 · Pilot's Operating Handbook
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).
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
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