AIRCRAFT WEIGHT & BALANCE (CESSNA) PFC-QA-104
CESSNA 402C · Weight And Balance
Overview
This document provides weight and balance information for various Cessna aircraft models, specifically the Cessna 152 and Cessna 172 series. It includes details on loading areas, weight calculations, and standard passenger weights. The document is intended for pilots and ground crew to ensure safe loading and compliance with weight limits. It also outlines the Vref calculation process for determining final approach speeds based on weight. The effective date of the document is June 1, 2022, and it serves as an initial issue for reference.
- C152 Max Gross Weight: 1670 lbs
- C172P Max Gross Weight: 2400 lbs
- C172R Max Gross Weight: 2450 lbs
- C172SP Max Gross Weight: 2550 lbs
- Standard passenger weight for males (15 Mar – 14 Dec): 206 lbs
- Vref calculation is essential for safe landing speeds.
Document
Source
Originally published by www.pacificflying.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Year
- 2022
- Pages
- 2
- File size
- 2.5 MB
- Publisher
- www.pacificflying.com
Specifications & performance
Extracted from this document.
Specifications
- Max takeoff weight (lb)
- 2,550
Weight & balance
- Max takeoff weight (lb)
- 2,550
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In this document
Loading Area and Weight Calculations
The document outlines the loading area and weight calculations for various Cessna models, including empty weight, pilot and passenger weights, baggage, and total zero fuel weight. It emphasizes the importance of using actual weights when possible.
Maximum Gross Weights
Maximum gross weights for the Cessna models are specified: C152 at 1670 lbs, C172P at 2400 lbs, C172R at 2450 lbs, and C172SP at 2550 lbs. Standard passenger weights are also provided for summer and winter seasons.
Vref Calculation
The Vref calculation section explains how to determine the calm wind final approach speed adjusted for landing weight. It includes formulas for calculating Vref based on Vso and landing weight, and notes on converting between KCAS and KIAS.
Safety notes
- Always use actual weights when possible for accurate calculations.
- Ensure compliance with maximum gross weight limits for safe operation.
Full document text
AIRCRAFT WEIGHT & BALANCE (CESSNA) PFC-QA-104 PFC-QA-104 Weight & Balance-Cessna Page 1 of 2 Effective Date: 01 June 2022 Revision: Initial Issue Aircraft Type: Registration: LOADING AREA WEIGHT (LBS) ARM MOMENT Empty weight Pilot and passenger Passengers (rear) Baggage Total (Zero Fuel Weight) Useable fuel (6.0 lbs/us gal) Total takeoff Weight Enroute fuel burn Total landing Weight WEIGHTS Max Gross Weights Standard Passenger Weights C152 1670 Lbs Summer (15 Mar – 14 Dec) Winter (15 Dec – 14 Mar) C172P 2400 Lbs 206 Lbs Male/Gender X (>12 Yrs) 212 Lbs C172R 2450 Lbs 172 Lbs Female (>12 Yrs) 178 Lbs C172SP 2550 Lbs 75 Lbs Child (2-11 Yrs) 75 Lbs 30 Lbs *Infant (<2 Yrs) 30 Lbs *Add in where infant exceeds 30 Lbs Reduce weight by 13 Lbs if no carry-on baggage for male/female Actual Weights should be used when possible Vref Calculation Published Vref at Max Gross Wt (POH): ________ KIAS The purpose of the Vref calculation is to find the calm wind final approach speed adjusted for the lower landing weight. 1. Vso at Max Gross Wt & Forward C of G ________ x 1.3 = ________ Vref KCAS Calm wind at Max Gross Wt. 2. Vref at Max Gross Wt ________ x � (𝐿𝐿𝑎𝑎𝑛𝑛𝑛𝑛𝑛𝑛𝑛𝑛𝑛𝑛 𝑊𝑊𝑊𝑊) (𝑀𝑀𝑎𝑎𝑀𝑀 𝐺𝐺𝐺𝐺𝐺𝐺𝐺𝐺𝐺𝐺 𝑊𝑊𝑊𝑊) = ________ Vref KCAS Calm wind at Landing Wt. 3. Using the POH/AFM, convert the adjusted Vref KCAS ________ to Vref KIAS ________ NOTE 1: Convert KIAS to and from KCAS by using the POH/AFM airspeed calibration chart. NOTE 2: Always apply KCAS to the above formula. In most cases, applying indicated airspeed (KIAS) to the formula will result in a speed that is too slow. AIRCRAFT WEIGHT & BALANCE (CESSNA) PFC-QA-104 PFC-QA-104 Weight & Balance-Cessna Page 2 of 2 Effective Date: 01 June 2022 Revision: Initial Issue C172 P C172 R C172 SP C152
What's in the CESSNA 402C TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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