Revised Weight and Balance and Equipment list due to Trip Considerations

CESSNA 414 · Weight And Balance

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Overview

This document provides a revised weight and balance and equipment list for the Cessna 414 aircraft, specifically for the aircraft identified as N414TRIP. It outlines the weight changes due to various equipment additions and modifications, including pilot and passenger seating, catering storage, baggage, and fuel loads. The document is essential for pilots and operators to ensure compliance with weight limits and to maintain safe operational parameters during flight. It includes critical weight data such as zero fuel weight, computed takeoff weight, and center of gravity calculations, which are vital for flight planning and safety.

Original weight: 4,851.05 lbs
Total weight after modifications: 6,760.10 lbs
Max ramp weight: 6,800 lbs
Max takeoff weight: 6,765 lbs
Max landing weight: 6,430 lbs
Max zero fuel weight: 6,165 lbs
Required fuel burn to land at max landing weight: 335 lbs (approx. 58 gallons)

Document

Source

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

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Document details

Type: Weight And Balance
Pages: 1
File size: 575 KB
Publisher: oncenterline.net

Specifications & performance

Extracted from this document.

Specifications

Empty weight (lb): 4,851
Fuel capacity (gal): 100
Max takeoff weight (lb): 6,765

Weight & balance

Useful load (lb): 5,777
Max ramp weight (lb): 6,800
Basic empty weight (lb): 4,851
Max landing weight (lb): 6,430
Max takeoff weight (lb): 6,765

About this document

What is the Revised Weight and Balance and Equipment list due to Trip Considerations?

The Revised Weight and Balance and Equipment list due to Trip Considerations is a weight and balance for the CESSNA 414.

How many pages is the Revised Weight and Balance and Equipment list due to Trip Considerations?

The copy of the Revised Weight and Balance and Equipment list due to Trip Considerations on file runs 1 pages.

Where does the Revised Weight and Balance and Equipment list due to Trip Considerations come from?

This copy of the Revised Weight and Balance and Equipment list due to Trip Considerations was originally published by oncenterline.net and is hosted on Sprinkle as a free, searchable reference copy.

Documentation completeness

6/7

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In this document

Weight Changes

The document details the weight of the aircraft before and after changes, with the original weight being 4,851.05 lbs. Various items were added, including pilot and co-pilot seats, passenger seats, catering storage, and baggage, resulting in a total weight of 6,760.10 lbs after modifications.

Weight Limits

Key weight limits for the Cessna 414 are specified: the maximum ramp weight is 6,800 lbs, maximum takeoff weight is 6,765 lbs, and maximum landing weight is 6,430 lbs. The maximum zero fuel weight is 6,165 lbs.

Fuel Requirements

For takeoff at maximum weight, the required fuel burn to land at maximum landing weight is 335 lbs, approximately equivalent to 58 gallons of fuel, which allows for about 1 hour and 30 minutes of flight time. Main tanks must be full at takeoff if the weight exceeds 6,350 lbs.

Center of Gravity Calculations

The computed takeoff center of gravity is 155.17 inches, which is crucial for ensuring the aircraft's stability and control during flight.

Notes and Modifications

The document notes that the aircraft has been modified to RAM IV configuration, which may affect performance and weight distribution.

Safety notes

Ensure main tanks are full at takeoff if weight exceeds 6,350 lbs.
Monitor weight and balance to maintain safe operational parameters.

Full document text

m Any Date F u e l l o a d f u l l m a i n s a n d a u x - 5 g a l " w e t " l o c k e r AIRCRAFT: Cessna 414 414-0840 N414TRIP Revised Weight and Balance and Equipment list due to Trip Considerations ITEM AIRCRAFT BEFORE CHANGE WEIGHT 4 8 5 1 . 0 5 ARM 157.69 MOMENT 7 6 4 9 6 2 . 0 6 EQUIPMENT ADDED P i l o t a n d C o - p i l o t 3 4 0 . 0 0 P a x S e a t s 3 a n d 4 340.00 C a t e r i n g i n s t o r a g e a r e a 1 0 . 0 0 N o s e S t o r a g e - " F l y a w a y k i t " Baggage 4 x 30# each 120.00 W a t e r 2 . 5 g a l l o n s 2 1 . 2 5 M i s c i t e m s - f l i p p e r s e t c 3 0 . 0 0 F u e l m a i n t a n k s f u l l 1 0 0 g a l 585.00 F u e l a u x t a n k s f u l l 6 3 g a l 368.55 F u e l l o c k e r t a n k 5 g a l ( w e t ) 2 9 . 2 5 TOTAL 6760.10 1 3 7 . 0 0 1 7 5 . 0 0 2 7 9 . 0 0 2 8 2 . 0 0 71.00 71.00 71.00 71.00 1 5 2 . 0 0 164.00 1 6 6 . 0 0 1 5 6 . 0 6 4 6 5 8 0 . 0 0 5 9 5 0 0 . 0 0 5 5 8 0 . 0 0 2820.00 3 1 9 5 . 0 0 8520.00 1 5 0 8 . 7 5 2130.00 88920.00 60442.20 4 8 5 5 . 5 0 1 0 5 5 0 1 3 . 5 1 ZERO FUEL WEIGHT COMPUTED TAKE OFF WEIGHT COMPUTED TAKE OFF C. G. REMAINING USEFUL LOAD 5 7 7 7 . 3 0 l b s . 6 7 6 0 . 1 0 l b s . 1 5 5 . 1 7 i n s . 4 . 9 0 l b s . NOTES: J . I . A l f r e d A & P 2015910I . A . A s m o d i f i e d t o R A M I V c o n f i g u r a t i o n MAX Ramp Weight 6800 # MAX Takeoff weight 6 7 6 5 # MAX Langing weight 6430 # M A X Z e r o f u e l w e i g h t 6165 # I f T a k e - O f f i s m a d e @ m a x t a k e o f f w e i g h t o f 6 7 6 5 # R e q u i r e d f u e l b u r n o f f t o l a n d @ m a x l a n d i n g w e i g h t i s 3 3 5 # o r a p p r o x 5 8 g a l l o n s a p p r o x 1 + 3 0 f l i g h t t i m e M a i n t a n k s r e q u i r e d t o b r f u l l a t t a k e o f f w e i g h t s a b o v e 6 3 5 0 # .

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