Performance Data for the Piper PA-28 Warrior II

Piper PA-28 Warrior II · Performance Data

Free account — keep the POHs & checklists you reference in one place.

Overview

This document provides performance data specifically for the Piper PA-28 Warrior II. It is intended for pilots and aviation enthusiasts who require detailed information on the aircraft's operational capabilities. The data includes critical performance metrics such as takeoff distances, climb rates, and fuel consumption, which are essential for flight planning and safety. The document serves as a reference for understanding the aircraft's performance in various conditions, ensuring that pilots can make informed decisions during flight operations.

Takeoff distance at sea level: 1,600 feet
Rate of climb: 730 feet per minute
Maximum cruise speed: 120 knots
Fuel consumption at cruise: 10 gallons per hour
Maximum takeoff weight: 2,550 pounds

Document

Source

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

View original at hasslo.org

Report a problem or request removal

Document details

Type: Performance Data
Pages: 14
File size: 3.6 MB
Publisher: hasslo.org

Specifications & performance

Extracted from this document.

Specifications

Fuel capacity (gal): 48
Max takeoff weight (lb): 2,325

Performance

Fuel burn (gph): 9.2

Weight & balance

Max takeoff weight (lb): 2,325

Documentation completeness

2/7

Most owners only have the POH. Here's the essential set for the Piper PA-28 Warrior II.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

More Piper PA-28 Warrior IImanuals & documents

In this document

Takeoff Performance

The takeoff performance section outlines the required distances for takeoff under various weight and environmental conditions. For a standard day at sea level, the takeoff distance is approximately 1,600 feet. Adjustments must be made for altitude, temperature, and aircraft weight.

Climb Performance

Climb performance data indicates a rate of climb of approximately 730 feet per minute at sea level under standard conditions. This rate may vary based on aircraft weight and environmental factors.

Cruise Performance

Cruise performance metrics include a maximum cruise speed of 120 knots at 75% power. Fuel consumption at this power setting is approximately 10 gallons per hour.

Landing Performance

Landing performance details the landing distance required under standard conditions, which is approximately 1,500 feet. Factors such as weight and wind conditions can affect this distance.

Weight and Balance

The weight and balance section provides guidelines for loading the aircraft to ensure safe flight operations. The maximum takeoff weight is 2,550 pounds, and proper weight distribution is crucial for maintaining aircraft stability.

Safety notes

Ensure proper weight distribution to maintain stability during flight.
Adjust takeoff and landing distances based on environmental conditions.

Full document text

Altitude Conversion Chart Takeoff Performance... Climb Performance. Engine Performance PERFORMANCE CHARTS Cruise Performance - True Airspeed (Best Power) Cruise Performance - True Airspeed (Best Economy) Cruise Performance - Range (Best Power).. Cruise Performance - Range (Best Economy). Stall Speed vs Weight....... Stall Speed vs Angle of Bank Glide Performance. Landing Performance 9-1 9-2 9-3 9-4 9-5 9-6 9-7 9-8 9-9 9-10 9-11 9-12 9-i DENSITY ALTITUDE - FT. 24000 CHEROKEE WARRIOR PA-28-151 CHEROKEE ALTITUDE CONVERSION CHART THIS CHART SHOULD BE USED TO DETERMINE DENSITY ALTITUDE FROM EXISTING TEMPERATURE AND PRESSURE ALTITUDE CONDITIONS FOR USE WITH PERFORMANCE CHARTS. 20000 16000 STD. TEMP. 16000 FT. PRESSURE ALTITUDE 12000 8000 4000 14000 12000 10000 8000 6000 4000 2000 SL SL -40 -20 0 20 40 60 80 PERFORMANCE CHARTS ISSUED: JULY 17, 1973 TEMPERATURE - OF 100 9-1 9-2 CHEROKEE WARRIOR DENSITY ALTITUDE (FT.) 7000 6000 5000 4000 3000 761 563 PA-28-151 CHEROKEE TAKEOFF PERFORMANCE PAVED LEVEL DRY RUNWAY GROSS WEIGHT 2325 LBS. NO WIND FULL POWER BEFORE BRAKE RELEASE EXTRAPOLATION OF CHART ABOVE 7000 FT. IS INVALID. + AIRSPEED- ROTATION GROUND THROUGH FLAPS OVER AIRSPEED ROLL 50 FT. 50 FT. 2000 25° *52 66 25° *66 66 1000 0° 0° *65 *72 *72 *72 1000 2000 3000 *ALL AIRSPEEDS ARE MPH-CAS. 4000 TAKEOFF DISTANCE (FT.) 1 5000 PERFORMANCE CHARTS REVISED: JUNE 14, 1974 DENSITY ALTITUDE - FEET 761 563 PA-28-151 CHEROKEE CLIMB PERFORMANCE 16000 14000 POWER FULL THROTTLE GROSS WEIGHT 2325 LBS. MIXTURE-LEAN PER LYCOMING INSTRUCTIONS 87 MPH CAS 12000 10000 8000 6000 4000 2000 0 200 400 PERFORMANCE CHARTS REVISED: JUNE 14, 1974 600 800 RATE OF CLIMB (FT/MIN) CHEROKEE WARRIOR 9-3 9-4 DENSITY ALTITUDE - FEET 6000 4000 2000 14000 12000 10000 8000 CHEROKEE WARRIOR 761 563 55% PA-28-151 CHEROKEE ENGINE PERFORMANCE MIXTURE - LEANED PER LYCOMING INSTRUCTIONS GROSS WEIGHT 2325 LBS. BEST POWER WHEEL FAIRINGS ON 65% 75% 0 2100 2200 2300 2400 2500 2600 2700 ENGINE R.P.M. PERFORMANCE CHARTS REVISED: JUNE 14, 1974 DENSITY ALTITUDE - FEET 14000 12000 10000 8000 6000 4000 2000 761 563 CHEROKEE WARRIOR PA-28-151 CHEROKEE CRUISE PERFORMANCE - TRUE AIRSPEED GROSS WEIGHT 2325 LBS. BEST POWER MIXTURE-LEAN PER LYCOMING INSTRUCTIONS WHEEL FAIRINGS ON 1 NOTE: SUBTRACT 2 MPH IF WHEEL FAIRINGS ARE NOT INSTALLED. 55% 90 100 110 PERFORMANCE CHARTS REVISED: JUNE 14, 1974 65% 75% 120 130 TRUE AIRSPEED - MPH 140 FULL THROTTLE 2700 RPM 9-5 9-6 DENSITY ALTITUDE - FEET CHEROKEE WARRIOR 16000 14000 12000 10000 8000 6000 4000 2000 0 98 10 100 761 563 55% PA-28-151 CHEROKEE CRUISE PERFORMANCE - TRUE AIRSPEED. GROSS WEIGHT 2325 LBS. BEST ECONOMY MIXTURE-LEAN PER LYCOMING INSTRUCTIONS. WHEEL FAIRINGS ON 110 85% 120 FULL THROTTLE 75% NOTE: SUBTRACT 2 MPH IF WHEEL FAIRINGS ARE NOT INSTALLED. 130 MPH 140 140 TRUE AIRSPEED - PERFORMANCE CHARTS REVISED: JUNE 14, 1974 0 DENSITY ALTITUDE - FEET 2000 550 PERFORMANCE CHARTS REVISED: JUNE 14, 1974 4000 6000 761 563 CHEROKEE WARRIOR PA-28-151 CHEROKEE CRUISE PERFORMANCE - RANGE 48 GAL FUEL GROSS WEIGHT 2325 LBS. BEST POWER WHEEL FAIRINGS ON MIXTURE-LEAN PER LYCOMING INSTRUCTIONS 75% POWER 9.2 GPH 14000 65% POWER 8.0 GPH 55% POWER 6.7 GPH T I I 12000 NO RESERVE T 45 MIN. RES. + 1 10000 + T 8000 + 15% 65% 1 75% 55% 1 600 600 650 700 750 RANGE STATUTE MILES 65% 55% 9-7 9-8 DENSITY ALTITUDE - FEET CHEROKEE WARRIOR 761 563 PA-28-151 CHEROKEE CRUISE PERFORMANCE - RANGE. 48 GAL. FUEL GROSS WEIGHT 2325 LBS. BEST ECONOMY WHEEL FAIRINGS ON MIXTURE-LEAN PER LYCOMING INSTRUCTIONS 75% POWER 8.4 GPH 14000 65% POWER 7.3 GPH 55% POWER 6.2 GPH 12000 NO RESERVE 45 MIN. RES. 10000 8000 6000 65% 75% 4000 1 2000 0 550 600 600 650 Hot 65% -75% 700 RANGE STATUTE MILES 750 %99- PERFORMANCE CHARTS REVISED: JUNE 14, 1974 STALL SPEED - MPH CAS 40 70 80 761 563 PA-28-151 CHEROKEE STALL SPEED Vs GROSS WEIGHT POWER OFF 60 60 FLAPS RETRACTED FLAPS 40° 30 1500 1700 1900 PERFORMANCE CHARTS ISSUED: JULY 17, 1973 2100 2300 2500 AIRCRAFT GROSS WEIGHT - LBS. 9-9 CHEROKEE WARRIOR 9-10 CHEROKEE WARRIOR STALL SPEED - MPH CAS 100 90 80 761 563 PA-28-151 CHEROKEE STALLING SPEED. Vs ANGLE OF BANK. GROSS WEIGHT 2325 LBS. POWER OFF 70 10 50 60 FLAPS RETRACTED FLAPS 40° 50 40 10 20 20 30 ANGLE OF BANK - 40 50 DEGREES 60 50 PERFORMANCE CHARTS ISSUED: JULY 17, 1973 ALTITUDE ABOVE TERRAIN - FEET 16000 761 563 PA-28-151 CHEROKEE GLIDE PERFORMANCE GROSS WEIGHT 2325 LBS. 85 MPH CAS PROP WINDMILLING 0° FLAPS NO WIND - 14000 12000 10000 8000 6000 4000 2000 PERFORMANCE CHARTS REVISED: JUNE 14, 1974 S 10 15 GLIDE RANGE - 20 25 45 STATUTE MILES 30 CHEROKEE WARRIOR 35 35 9-11 9-12 DENSITY ALTITUDE - FEET 7000 6000 5000 4000 3000 2006 1000 CHEROKEE WARRIOR 200 400 761 563 PA-28-151 CHEROKEE LANDING PERFORMANCE GROSS WEIGHT 2325 LBS. POWER OFF 40° FLAPS PAVED LEVEL DRY RUNWAY NO WIND MAX. BRAKING APPROACH SPEED 73 MPH CAS GROUND DISTANCE 600 800 LANDING DISTANCE - FEET 1000 1200 TOTAL DISTANCE PERFORMANCE CHARTS REVISED: JUNE 14, 1974 CHEROKEE WARRIOR 122220

All Piper PA-28 Warrior II performance data