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RV-14 SAMPLE - 1 Pages

  1. P. 1

Catalogue excerpts

ror>iz. \SAN’S AIRCRAFT 14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 • FAX 503-678-6560 • www.vansaircraft.com • info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm Van's aircraft has received a number of requests from builders for an example weight and balance for the RV-14. The weight and balance documents for the RV-14 (N144VA) and RV-14A (N214VA) as of January 7, 2016 are provided below. These are provided as SAMPLES ONLY. Arms and weights will vary between aircraft and require individual calculation. Refer to the RV-14 and RV-14A Weight and Balance Data Quick Reference files available from the Van's Aircraft downloads page to calculate the W&B for your aircraft For rough estimations of locations within the aircraft, use the 1:1 scale 3 view drawings also found on the downloads page. For Taildragger Aircraft, use either the "AFT" or "TAILWHEEL'' locations to measure the aft weight. DATUM:    72    INCHES FORWARD OF WING LEADING EDGE WING LEADING EDGE 14.5 INCHES AFT OF AFT SIDE OF FIREWALL CG RANGE LIMITS:    FWD LIMIT:    82.08    18% EMPTY AIRCRAFT LEFT WHEEL AFT TAILWHEEL RIGHT WHEEL DATUM:    72    INCHES FORWARD OF WING LEADING EDGE WING LEADING EDGE 14.5 INCHES AFT OF AFT SIDE OF FIREWALL CG RANGE LIMITS:    FWD LIMIT:    82.08    18% EMPTY AIRCRAFT LEFT WHEEL NOSE WHEEL RIGHT WHEEL All Weights (lb), Arms (in), Moments (in-lb)

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