Loading Summary
CESSNA 210N · Weight And Balance
Overview
This document provides a detailed weight and balance summary for the Cessna 210N, specifically for aircraft N611TM. It includes information on ramp, takeoff, and landing weights, as well as center of gravity (CG) calculations. The document is intended for pilots and ground crew to ensure safe loading and compliance with weight limits. It outlines the maximum allowable weights and the distribution of weight across various sections of the aircraft, which is critical for maintaining stability and performance during flight.
- Maximum ramp weight: 3,800 lbs
- Current ramp weight: 2,324.6 lbs
- Center of gravity (CG) range: 37 to 53 inches, current CG: 42.6 inches
- Front seats capacity: 450 lbs
- Total weight distribution includes various sections with specific weight limits.
Document
Source
Originally published by 1979cessna210.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight And Balance
- Year ·
- 2019
- Pages ·
- 2
- File size ·
- 28 KB
- Publisher ·
- 1979cessna210.com
Specifications & performance
Extracted from this document.
Specifications
- Max takeoff weight (lb) ·
- 3,800
Weight & balance
- Max ramp weight (lb) ·
- 3,800
- Baggage allowance (lb) ·
- 200
- Max takeoff weight (lb) ·
- 3,800
What is the Loading Summary?
The Loading Summary is a weight and balance for the CESSNA 210N, dated 2019.
How many pages is the Loading Summary?
The copy of the Loading Summary on file runs 2 pages.
Where does the Loading Summary come from?
This copy of the Loading Summary was originally published by 1979cessna210.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the Loading Summary published?
The Loading Summary — the CESSNA 210N weight and balance on file — is dated 2019.
Most owners only have the POH. Here's the essential set for the CESSNA 210N.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
More CESSNA 210Nmanuals & documents
- CHECKLISTS - Aircraft SpruceChecklist
- CHECKMATE CHECKLISTS - Aircraft SpruceChecklist
- B&C Standby Alternator System for the Cessna 210Wiring Diagram
- CAP – Cessna Short- and Soft-Field OperationsTraining Manual
- Wheels up landing involving Cessna 210, VH-UPNOther Documents
- TYPE ACCEPTANCE CERTIFICATEType Certificate
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- Pilot's Operating Hbndbook - flight examinersPilot's Operating Handbook
- Cessna T210N - AirMartSpecifications
- Airplane Flight ManualFlight Manual
In this document
Loading Summary
The loading summary indicates the ramp, takeoff, and landing weights for the Cessna 210N. The maximum ramp weight is 3,800 lbs, with the current ramp weight recorded at 2,324.6 lbs. The center of gravity (CG) is noted to be 42.6 inches, which falls within the acceptable range of 37 to 53 inches.
Weight Distribution
The document details the weight distribution across various sections of the aircraft, including fuel tanks, seats, and baggage areas. The front seats can accommodate up to 450 lbs, while the middle seat can also hold 450 lbs. The back seat and forward baggage area can hold up to 340 lbs, and the baggage/aft wheel well can hold 200 lbs.
Takeoff and Landing Audits
The takeoff and landing audits provide a breakdown of the weight and CG for both scenarios. The takeoff weight is recorded at 2,324.6 lbs with a CG of 42.5591 inches. The landing weight is the same, ensuring consistency in weight management.
Safety notes
- Ensure weight does not exceed maximum limits to maintain aircraft performance and safety.
Full document text
Loading Summary N611TM Cessna 210 C210 N July 2, 2019 5:53:22 PM GMT Graph takeoff landing CG fore aft Weight Notices Loading Appears OK Ramp (max 3,800 lb) Ramp Weight 2,324.6 lb Ramp Fuel 0 gal 100LL Takeoff (max 3,800 lb) Takeoff Weight 2,324.6 lb CG (37 to 53) 42.6 in Takeoff Fuel 0 gal 100LL Landing (max 3,800 lb) Landing Weight 2,324.6 lb CG (37 to 53) 42.6 in Fuel Remaining 0 gal 100LL Zero Fuel Zero Fuel Weight 2,324.6 lb CG (37 to 53) 42.6 in Station Limits Fuel Tanks 0 of 89 gal 100LL Front Seats 0 of 450 lb Middle Seat 0 of 450 lb Back Seat/Forward Baggage 0 of 340 lb Wheel Well 0 of 50 lb Baggage/Aft Wheel Well 0 of 200 lb Page 1 of 2 http://foreflight.com Created by ForeFlight on an iPhone Loading Summary N611TM Cessna 210 C210 N July 2, 2019 5:53:22 PM GMT Takeoff Audit 37.0000 in 0.0000 lb Front Seats 0.0000 in-lb 42.5591 in 2324.6000 lb Empty Aircraft 98933.0000 in-lb 43.0000 in 0.0000 lb Fuel Tanks 0.0000 in-lb 71.0000 in 0.0000 lb Middle Seat 0.0000 in-lb 101.0000 in 0.0000 lb Back Seat/Forward Baggage 0.0000 in-lb 117.0000 in 0.0000 lb Wheel Well 0.0000 in-lb 138.0000 in 0.0000 lb Baggage/Aft Wheel Well 0.0000 in-lb 42.5591 in 2324.6000 lb Takeoff Summary 98933.0000 in-lb Landing Audit 37.0000 in 0.0000 lb Front Seats 0.0000 in-lb 42.5591 in 2324.6000 lb Empty Aircraft 98933.0000 in-lb 43.0000 in 0.0000 lb Fuel Tanks 0.0000 in-lb 71.0000 in 0.0000 lb Middle Seat 0.0000 in-lb 101.0000 in 0.0000 lb Back Seat/Forward Baggage 0.0000 in-lb 117.0000 in 0.0000 lb Wheel Well 0.0000 in-lb 138.0000 in 0.0000 lb Baggage/Aft Wheel Well 0.0000 in-lb 42.5591 in 2324.6000 lb Landing Summary 98933.0000 in-lb Page 2 of 2 http://foreflight.com Created by ForeFlight on an iPhone