Cessna 172 Performance Data
CESSNA 172S Skyhawk · Performance Data
Overview
This document provides performance data for the Cessna 172 aircraft, detailing expected performance under various conditions. It includes information on takeoff distances, climb rates, cruise performance, and landing distances. The data is intended for flight planning purposes and is not FAA approved, serving as a reference to help pilots understand the aircraft's capabilities. The document emphasizes the importance of adjusting performance figures based on environmental factors such as elevation, wind conditions, and runway type.
- Maximum weight for takeoff is 2550 lbs.
- Takeoff distances decrease by 10% for every 9 knots of headwind.
- Climb performance requires mixture to be leaned above 3000 feet for maximum efficiency.
- Landing distances increase by 45% on dry grass runways.
- Flaps 30° are recommended for short field landings.
Document
Source
Originally published by www.gocivilairpatrol.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Performance Data
- Pages ·
- 5
- File size ·
- 1.3 MB
- Publisher ·
- www.gocivilairpatrol.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp) ·
- 180
- Max takeoff weight (lb) ·
- 2,550
Weight & balance
- Max takeoff weight (lb) ·
- 2,550
What is the Cessna 172 Performance Data?
The Cessna 172 Performance Data is a performance data for the CESSNA 172S Skyhawk.
How many pages is the Cessna 172 Performance Data?
The copy of the Cessna 172 Performance Data on file runs 5 pages.
Where does the Cessna 172 Performance Data come from?
This copy of the Cessna 172 Performance Data was originally published by www.gocivilairpatrol.com and is hosted on Sprinkle as a free, searchable reference copy.
Most owners only have the POH. Here's the essential set for the CESSNA 172S Skyhawk.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA 172S Skyhawkmanuals & documents
See all 50 →- SkyView Autopilot Servo Installation & Maintenance ManualAvionics Manual
- Cessna 172 Roll Servo Cable Guard, Rev BService Bulletins
- Supplemental Type CertificateSupplemental Type Certificate
- ELECTRICAL POWER - ALTERNATOR CONTROL UNIT (ACU) AND CONNECTOR OBSOLESCENCEService Bulletins
- CESSNA 172S MANEUVER GUIDEPilot's Operating Handbook
- Cessna 172-S Training SupplementTraining Manual
- CAP TXWG Cessna 172S IntroductionOther Documents
- Weight and BalanceWeight And Balance
- Supplemental Type CertificateSupplemental Type Certificate
- LANDING GEAR - MAIN LANDING GEAR BUSHING INSPECTIONMaintenance Manual
- Cessna 172S-G1000 ChecklistChecklist
- Cessna 172S G1000 Skyhawk Normal ProceduresNormal Procedures
In this document
Takeoff Distance
The takeoff distance for the Cessna 172 at maximum weight of 2550 lbs is detailed, with specific adjustments for altitude and wind conditions. For example, distances decrease by 10% for every 9 knots of headwind and increase by 10% for tailwinds up to 10 knots. Additional figures are provided for maximum weights of 2400 lbs and 2200 lbs.
Maximum Rate of Climb
The maximum rate of climb is specified under conditions of flaps up and full throttle, with mixture leaned above 3000 feet. Important notes include adding 1.4 gallons of fuel for engine start and taxi, and adjustments for temperature variations.
Cruise Performance
Cruise performance data is provided for the Cessna 172 at a weight of 2550 lbs, although specific figures are not detailed in the document.
Landing Distance
Landing distances are outlined for short field conditions with flaps set to 30°, power off, and maximum braking on a paved, level, dry runway. Adjustments for wind and runway type are also noted, including a 45% increase in distance for dry grass runways.
Safety notes
- Data provided is not FAA approved and should be used as a reference only.
Full document text
1 Cessna 172 180 HP Performance Data Performance data information on the following pages are presented so that you may know what to expect from the airplane under various conditions. The data tables provided here are NOT FAA APPROVED and shall be used as a reference only information to facilitate the planning of flights with reasonable accuracy. 2 TAKEOFF DISTANCE MAXIMUM WEIGHT 2550 LBS SHORT FIELD 1. Prior to takeoff from fields above 3000 feet elevation, the mixture should be leaned to give maximum RPM in a full throttle, static run-up. 2. Decrease distances 10% for each 9 knots headwind. For operation with tailwinds up to 10 knots, increase distances by 10% for each 2 knots. 3. For operation on a dry, grass runway, increase distances by 15% of the "ground roll" figure. Figure 1 - Takeoff Distance 2550 MAXIMUM WEIGHT 2400 AND 2200 LBS SHORT FIELD Figure 2 - Takeoff Distance 2400 and 2200 REFERENCE ONLY 3 MAXIMUM RATE OF CLIMB CONDITION: Flaps up Full Throttle Mixture leaned above 3000 feet for maximum performance TIME, FUEL, AND DISTANCE TO CLIMB CONDITION: Flaps up Full Throttle Standard Temperature NOTES: 1. Add 1.4 gallons of fuel for engine start, taxi and takeoff allowance. 2. Mixture leaned above 3000 feet for maximum RPM. 3. Increase time, fuel and distance by 10% for each 10°C above standard temperature. 4. Distances shown are based on zero wind. REFERENCE ONLY 4 CRUISE PERFORMANCE CONDITION: 2550 LBS REFERENCE ONLY 5 LANDING DISTANCE SHORT FIELD CONDITIONS: Flaps 30° Power Off Maximum Braking Paved, Level, Dry Runway Zero Wind 1. Decrease distances 10% for each 9 knots headwind. For operation with tailwinds up to 10 knots, increase distances by 10% for each 2 knots. 2. For operation on a dry, grass runway, increase distances by 45% of the "ground roll" figure. 3. If a landing with flaps up is necessary, increase the approach speed by 9 KIAS and allow for 35% longer distances. REFERENCE ONLY