V-Speeds Reference for Cessna 172N Skyhawk
CESSNA 172N SKYHAWK · V Speeds Reference
Overview
This document serves as a V-Speeds Reference for the Cessna 172N Skyhawk, providing essential airspeed and performance data for pilots. It outlines critical stall speeds, approach speeds, and operational limits necessary for safe flight operations. The information is intended for reference purposes and should be cross-checked with the Pilot's Operating Handbook (POH) for comprehensive details. This document is particularly useful for flight planning and in-flight decision-making, ensuring pilots are aware of the aircraft's performance characteristics under various conditions.
- Stall speed normal takeoff: 47 kts
- Best glide speed (no flaps): 65 kts
- Maximum structural cruising speed: 128 kts
- Never exceed speed: 160 kts
- Normal approach speed (flaps 0°): 60-70 kts
- Fuel capacity: 40 gallons usable
- Maneuvering speed: 97 kts at 2300 lbs gross weight
Document
Source
Originally published by reginaflyingclub.ca. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- V Speeds Reference
- Pages
- 1
- File size
- 53 KB
- Publisher
- reginaflyingclub.ca
Specifications & performance
Extracted from this document.
Specifications
- Max speed (kt)
- 160
- Fuel capacity (gal)
- 43
Performance
- Max crosswind (kt)
- 15
- Best glide speed (kt)
- 60
- Stall speed clean (kt)
- 47
- Stall speed landing (kt)
- 41
V-speeds
- VA
- 97
- VFE
- 85
- VNE
- 160
- VNO
- 128
- VS1
- 47
- VSO
- 41
Common. One of the most common aircraft types we track.
Most owners only have the POH. Here's the essential set for the CESSNA 172N SKYHAWK.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Stall Speeds
The stall speeds for the Cessna 172N are critical for safe operation. The normal takeoff stall speed is indicated, along with best rate and angle of climb speeds. Specific stall speeds for various configurations, such as balked approach and precautionary landing, are also provided.
Airspeeds & Performance
This section details various airspeeds for the Cessna 172N, including approach speeds with different flap settings. Key speeds include 60-70 knots for normal approach and landing with flaps at 0°, and 55-65 knots with flaps at 40°. The maximum entry speed for maneuvers is noted as 95 knots.
Operational Limits
The document outlines operational limits such as maximum structural cruising speed (128 knots) and never exceed speed (160 knots). It also includes caution and normal operating ranges for airspeeds, ensuring pilots are aware of safe operating parameters.
Fuel and Weight Specifications
Fuel capacity is specified as 40 gallons usable from two standard wing tanks, each holding 21.5 gallons. The aircraft is certified in the utility category when under 2000 lbs and within the center of gravity envelope.
Maintenance Notes
Important maintenance notes include tire pressures for the nose wheel (31 psi) and mains (29 psi), as well as hydraulic fluid levels for the nose gear shock strut, ensuring proper aircraft upkeep.
Safety notes
- Mag check maximum drop of 125 rpm at 1700 rpm
- 50 rpm maximum differential between magnetos
- Suction gauge should read 4.6 to 5.4 inches of mercury at 1700 rpm
Full document text
This document is for reference purposes only. Refer to the POH for proper documentation. Cessna 172N YQR / GTM Stall Speed Normal Takeoff Best Rate Best Angle Balked Approach (Overshoot) Precautionary Landing Steep Turns Best Glide Speed (no flaps) Never Exceed Speed (glide, dive, or smooth air) Maximum Structural Cruising Speed Maximum Flap Extension Speed Caution Range Normal Operating Range Flap Operation Range Maximum Crosswind Mag Check - Max drop of 125 rpm at 1700 rpm - 50 rpm max differential between magnetos Suction Gauge 4.6 to 5.4 inches of mercury at 1700 rpm Fuel - 2 standard wing tanks, 21.5 gallons each Stall - alarm sounds 5-10 mph before the stall Fuel 100LL Oils 20W50 (year-round) Tire Pressure Nose wheel – 31 psi, Mains – 29 psi Nose Gear Shock Strut - Keep filled with hydraulic fluid - Inflated with air to 45 psi Airspeeds & Performance Flaps Up, Power Off – 47 kts Flaps Down, Power Off – 41 kts 70 kts 68-73 kts 59-61 kts Enroute Normal 75-85 kts Retract to 20° flaps and 55 kts Normal Approach & Landing (Flaps 0°) 60-70 kts Normal Approach & Landing (Flaps 40°) 55-65 kts 60 kts and 20° Flaps Max Entry Speed – 95 kts 65 kts 160 kts 128 kts 85 kts Maneuvering Speed 97 kts (at 2300 lbs gross weight) 89 kts (at 1950 lbs gross weight) 80 kts (at 1600 lbs gross weight) 128-160 kts (yellow arc) 47-128 kts (green arc) 41-85 kts (white arc) 15 kts - 40 gallons useable (43 gallons total) - aircraft certified in the utility category when under 2000 lbs and CofG within utility envelope
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