Revised Weight and Balance and Equipment list due to Trip Considerations
CESSNA 414 · Weight And Balance
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.
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
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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 # .
What's in the CESSNA 414 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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