Weight and Balance Report Aviat A-1 Husky N2881P
AVIAT HUSKY A-1 · Weight & Balance
Overview
This document provides the weight and balance report for the Aviat Husky A-1 aircraft, detailing the aircraft's weight with and without skis installed. It includes information on the empty weight, useful load, and center of gravity (CG) limits.
- Maximum Gross Weight: 1800.0 lbs
- New Empty Weight with wheels: 1236.3 lbs
- New Empty Weight with skis: 1246.5 lbs
- Useful Load with wheels: 563.7 lbs
- Useful Load with skis: 553.5 lbs
- Datum is located 60.0 inches forward of the wing leading edge
- CG Limits are detailed in the Airplane Flight Manual
- New Empty Weight CG with wheels: 73.04 inches aft of Datum
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at chicagogliderclub.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Weight & Balance
- Year ·
- 2020
- File size ·
- 27 KB
- Copy found at ·
- chicagogliderclub.org
- Language ·
- en
Specifications & performance
Extracted from this document.
Specifications
- Maximum gross weight (lb) ·
- 1800.0
- Useful load with skis (lb) ·
- 553.5
- Empty weight with skis (lb) ·
- 1246.5
- Useful load with wheels (lb) ·
- 563.7
- Empty weight with wheels (lb) ·
- 1236.3
Performance
- Datum location (in) ·
- 60.0
Weight & balance
- New empty weight cg (in) ·
- 73.04
- New empty weight cg skis (in) ·
- 72.75
What is the Weight and Balance Report Aviat A-1 Husky N2881P?
The Weight and Balance Report Aviat A-1 Husky N2881P is a weight & balance for the AVIAT HUSKY A-1, dated 2020.
What year was the Weight and Balance Report Aviat A-1 Husky N2881P published?
The Weight and Balance Report Aviat A-1 Husky N2881P — the AVIAT HUSKY A-1 weight & balance on file — is dated 2020.
Common. More common than 80% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the AVIAT HUSKY A-1.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
AVIAT HUSKY A-1 for sale now
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More AVIAT HUSKY A-1manuals & documents
- AVIAT HUSKY A-1 Model GuideModel Guide
- Service Bulletin No. 11 rev. AService Bulletins
- INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR AVIAT AIRCRAFT A-1, A-1A, A-1B, A-1C-180, A-1C-200Maintenance Manual
- Service Bulletin No. 25Service Bulletins
- Husky InstructionsParts Catalog
- SERVICE BULLETIN No. 16Service Bulletins
- SERVICE BULLETIN No. 14 AVIAT AIRCRAFT INC.Service Bulletins
- Husky A-1B Pilot's Operating HandbookPilot's Operating Handbook
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—In this document
Weight and Balance Report with Wheels Installed
Details the weight and balance of the aircraft with wheels, including the new empty weight and CG.
Weight and Balance Report with Skis Installed
Details the weight and balance of the aircraft with skis, including changes in weight and CG.
Equipment List
Lists equipment included in the weight calculations and their respective weights and moments.
Maximum Gross Weight
States the maximum gross weight of the aircraft as 1800.0 lbs.
Datum Information
Describes the location of the datum for CG calculations.
CG Limits
Refers to the CG limits as detailed in the Airplane Flight Manual.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Refer to CG Envelope in Airplane Flight Manual for loading information.
- Ensure weight does not exceed maximum gross weight of 1800.0 lbs.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
Weight and Balance Report with wheels Installed Christen A-1 Husky (Aviat Aviation, Inc) N2881P Serial #1011 May 20, 2020 Item Weight Arm Moment Airplane as weighed by Christen Industries 6/12/1987 1226.0 88965.2 This weight includes 2 Gallons Oil, 2 Gallons Unusable Fuel and equipment listed in actual Weight and Balance Equipment List dated June 22, 1987 pages 8 and 9. Turn Coordinator 1.2 48.00 57.6 Rate of Climb .7 48.00 33.6 TOST Tow Release Installation 8.6 145.90 1254.8 Remove: KT 76A Transponder with Altitude Encoder -6.0 51.00 -306.0 Install: Stratus ESG and WAAS GPS Antenna + Altitude Encoder 4.8 51.00 244.8 PS Engineering PM 1000II Intercom 1.0 48.00 48.0 New Empty Weight 1236.3 90298.0 New Empty Weight CG 73.04” aft of Datum Datum is located 60.0 inches forward of the wing leading edge (Fuselage Station FS 0.00) Maximum Gross Weight 1800.0 Lbs Useful Load 563.7 Lbs CG Limits – See CG Envelope in Airplane Flight Manual Section V: Loading Information, Page 7 _________________________________________________________________________________________ Weight and Balance Report with Federal Fluidyne A-2000-A Skis installed Christen A-1 Husky (Aviat Aviation, Inc) N2881P Serial #1011 May 20, 2020 Item Weight Arm Moment Airplane as weighed by Christen Industries 6/12/1987 1226.0 88965.2 This weight includes 2 Gallons Oil, 2 Gallons Unusable Fuel and equipment listed in actual Weight and Balance Equipment List dated June 22, 1987 pages 8 and 9. Turn Coordinator 1.2 48.00 57.6 Rate of Climb .7 48.00 33.6 TOST Tow Release Installation 8.6 145.90 1254.8 Remove: KT 76A Transponder with Altitude Encoder -6.0 51.00 -306.0 Install: Stratus ESG and WAAS GPS Antenna + Altitude Encoder 4.8 51.00 244.8 PS Engineering PM 1000II Intercom 1.0 48.00 48.0 Remove Wheels (19.3# each wheel) -38.6 61.50 -2373.9 Install Federal Fluidyne A-2000-A Skis 48.8 56.50 2757.2 New Empty Weight 1246.5 90681.3 New Empty Weight CG 72.75” aft of Datum Datum is located 60.0 inches forward of the wing leading edge (Fuselage Station FS 0.00) Maximum Gross Weight 1800.00 Lbs Useful Load with Skis installed 553.5 Lbs CG Limits – See CG Envelope in Airplane Flight Manual Section V: Loading Information, Page 7 Prepared by Ronald N Ridenour 1985138A&P_____________________________________





