Weight & Balance for Cessna 205
Cessna 205 · Weight And Balance
Overview
This document provides essential weight and balance information for the Cessna 205 aircraft. It is designed for pilots and aviation enthusiasts who need to understand the loading limits and weight distribution for safe flight operations. The manual outlines the maximum weight capacities, center of gravity limits, and procedures for calculating weight and balance before flight. Proper adherence to these guidelines is crucial for maintaining aircraft performance and safety.
- Maximum takeoff weight: 2,800 lbs
- CG limits: 34.0 to 39.0 inches from datum
- Total fuel capacity: 60 gallons
- Use loading charts for weight calculations
- Ensure weight does not exceed limits for safe flight
Document
Source
Originally published by www.airglas.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 80
- File size
- 3.4 MB
- Publisher
- www.airglas.com
Common. Rarer than 10% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 205.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 205 to your watchlist and track it in one place.
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In this document
Weight Limitations
The maximum takeoff weight for the Cessna 205 is 2,800 lbs. This includes the weight of the aircraft, passengers, cargo, and fuel. It is essential to ensure that the total weight does not exceed this limit to maintain safe flight operations.
Center of Gravity (CG) Limits
The center of gravity limits for the Cessna 205 are between 34.0 inches and 39.0 inches from the datum. It is important to calculate the CG accurately to ensure stability and control during flight.
Loading Procedures
Before flight, pilots must calculate the weight and balance by considering the weight of passengers, baggage, and fuel. The document provides a sample loading chart to assist in these calculations.
Fuel Capacity
The Cessna 205 has a total fuel capacity of 60 gallons, which is critical for determining weight and balance during flight planning.
Weight and Balance Calculation Example
An example calculation is provided to illustrate how to determine the total weight and CG based on different loading scenarios. This helps pilots understand the practical application of the weight and balance principles.
Safety notes
- Exceeding weight limits can lead to compromised aircraft performance.
- Improper CG can affect aircraft stability and control.
Full document text
DOCUMENT AE00-1FM Revision C Airglas, Inc. 3500 O'Malley Road Anchorage, AK 99519 Phone 907-344-1450 Fax 907-349-4938 airglas.com FAA-APPROVED SUPPLEMENTAL FLIGHT MANUAL OR AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR CESSNA MODELS 150 Series, 172 Series, 177 Series, 182 Series, and 210-5 Series. EQUIPPED WITH AN AIRGLAS PA32-206LA NOSE FORK Registration Number: Serial Number: This document must be carried in the airplane at all times when the Airglas PA32-206LA Nose Fork Assembly is installed in accordance with Supplemental Type Certificate Number SA02069AK. The information contained in this document supplements or supersedes the information made available to the operator by the manufacturer in the form of clearly stated placards, markings, or manuals as required by CAR 3.777(b), or in the form of an FAA approved Airplane Flight Manual as required by FAR 21.5, only in those areas listed herein. For limitations, procedures, and performance information not contained in this document, consult the basic placards, markings, or manuals, or the basic FAA approved Airplane Flight Manual. FAA Approved: Date: Asay August A. Asay Manager, Anchorage Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska FEB - 9 2015 Page 1 of 80 DOCUMENT AE00-1FM Revision C Revision Pages No. Affected Initial 1-5 Release A 1-5 B 1-5 C All Date: FEB - 9 2015 FAA Approved LOG OF REVISIONS Description Original Added other tire sizes Added 150,152,172,175,177,205 Changed address. Added additional tire combinations and associated CG charts. Removed registration and serial numbers from pages 2-6. Minor formatting and typographical corrections. FAA Approved A. Asay Date 09-03-00 G. Holt 11-30-01 G. Holt 06-05-06 See Cover Page 2 of 80 DOCUMENT AE00-1FM Revision C SECTION I. General This aircraft is equipped with an Airglas PA32-206LA Nose Fork. This nose fork replaces the OEM nose fork and allows up to an 8.50x6 tire to be used (other size tires are acceptable). The nose fork is made out of 4130 Chromoly steel that is heat treated. The tire inflation pressure is unchanged from the manufacturer's recommendations. SECTION II. 1. 2. Limitations Nose wheel tire - A tire clearance of at least 1/2 inch from the four (4) bolts on the nose fork is required. Tire size: The main gear and nose gear tires must be the same size or one of these combinations: Main Tire 8.50 x 6 8.50 x 6 8.50 x 6 8.00 x 6 7.00 x 6 Nose tire 8.00 x 6 7.00 x 6 6.00 x 6 7.00 x 6 6.00 x 6 3. Center of Gravity Envelope - The Center of Gravity envelope is limited to the envelopes specified in on pages 4 and 5. WARNING There are limitations on the forward C.G. envelope of some aircraft with the Airglas, Inc., PA32- 206LA Landes Nose Fork installed. Consult pages 4 thru 5 of this supplement (Weight and Balance). With the Landes Nose Fork assembly installed the aircraft must be loaded in accordance with the Center of Gravity envelope specified on pages 4 thru 5. SECTION III. Emergency Procedures No Change SECTION IV. Normal Procedures 1. PREFLIGHT INSPECTION -- A. Nose Fork wheel & tire attaching hardware Secure B. Nose Fork block attaching hardware Secure C. Nose Fork tire -- Proper inflation 13 Date: FEB - 9 2015 FAA Approved Page 3 of 80 DOCUMENT AE00-1FM Revision C 2. INFLIGHT PROCEDURES Landing: The nose fork and 8.50-6 tire increase the length of the nose gear by approximately 4". Pilots should ensure that all landings are accomplished in a nose high attitude similar to the soft field approach attitude. CAUTION During landing there is an increased possibility of wheel barrowing or porpoising during landing. Pilots should ensure that all landings are accomplished in a nose high attitude similar to the soft field approach attitude. SECTION V. Performance Information Cruise: Cruise speeds are reduced up to 8 mph True Airspeed due to the increased size of the 8.50-6 tires. Pilots should reduce maximum range data by 5%. SECTION VI. Weight and Balance/Equipment List 1. Aircraft weight and balance records and equipment list have been updated to reflect this installation. 2. Cessna 150 and 152 models with the PA32-206LA Nose Fork Installed: The C.G. envelope is not limited for Cessna 150 and 152 models regardless of tire size. 3. Cessna 172 models with the PA32-206LA Nose Fork Installed: The C.G. envelope is not limited for Cessna 172 models operated in the Utility Category regardless of tire size. The C.G. envelope is not limited for Cessna 172 models operated in the Normal Category when all three tires are the same size. The C.G. envelope is limited for Cessna 172 models operated in the Normal Category when the nose tire is smaller than the main tires. See tables 1 thru 35 of approved envelopes for specific tire size. 4. Cessna 175 models with the PA32-206LA Nose Fork Installed: The C.G. envelope is not limited for Cessna 175 models operated in the Normal Category when all three tires are the same size. The C.G. envelope is limited for Cessna 175 models operated in the Normal Category when the nose tire is smaller than the main tires. See tables 36 thru 44 of approved envelopes for specific tire size. 5. Cessna 177 models with the PA32-206LA Nose Fork Installed: The C.G. envelope is not limited for Cessna 177 models operated in the Utility Category regardless of tire size. The C.G. envelope is not limited for Cessna 177 models operated in the Normal Category when all three tires are the same size. The C.G. envelope is limited for Cessna 177 models operated in the Normal Category when the nose tire is smaller than the main tires. See tables 45 thru 53 of approved envelopes for specific tire size. 6. Cessna 182 models with the PA32-206LA Nose Fork Installed: The C.G. envelope is not limited for Cessna 182 models operated in the Normal Category when all three tires are the same size. The C.G. envelope is limited for Cessna 182 models operated in the Normal
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Category when the nose tire is smaller than the main tires. See tables 54 thru 77 of approved envelopes for specific tire size. Date: FEB - 9 2015 FAA Approved Page 4 of 80 DOCUMENT AE00-1FM Revision C SECTION VI. Weight and Balance/Equipment List-continued- 7. Cessna 210-5 (205) and 210-5A (205A) models with the PA32-206LA Nose Fork Installed: The C.G. envelope is not limited for Cessna 210-5 models operated in the Normal Category when all three tires are the same size. The C.G. envelope is limited for Cessna 210-5 models operated in the Normal Category when the nose tire is smaller than the main tires. See tables 78 thru 80 of approved envelopes for specific tire size. SECTION VII. Systems Descriptions This airplane is equipped with an Airglas, Inc., PA32-206LA Nose Fork Assembly. The tire inflation pressure is unchanged from the manufacturer's recommendations. The tire and wheel are unchanged and wear indications should follow that specific manufacturer's recommendations. SECTION VIII. Handling, Servicing and Maintenance All handling procedures for this modification are standard. The PA32-206LA Nose Fork Assembly may be serviced and maintained in accordance with Part 43 of the Federal Aviation Regulations (FAR 43). Servicing and maintenance in accordance with FAR 43 is adequate to insure the continued airworthiness of this modification. Information on installing the PA32- 206LA Nose Fork Assembly can be found in the Landes Nose Fork Installation Instructions, original issue dated November 5, 1996 or later FAA-approved revision. FEB - 9 2015 Date: Page 5 of 80 FAA Approved DOCUMENT AE00-1FM Revision C Appendix A: Approved Center of Gravity Envelopes for Specific Tire Combinations. 4250- 4000 3750 3500 3250 (1733 lbs, 36.4 inches) 3000 (2200 lbs, 40.8 inches) (2200 lbs, 46.4 inches) 2750 2500 2250 2000 Loaded Airplane Weight (lbs) 1750 1500 1250 1000 750 500 250 (1733 lbs, 46.4 inches) 0 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 Airplane C.G. Location, Inches Aft of Datum - C.G. points TABLE 1 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172,A, (+36.4) to (+46.4) at 1733 lb. or less NORMAL CATEGORY (+40.8) to (+46.4) at 2200 [b. ALL 3 TIRES SAME SIZE CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1733 lbs, 36.45 inches) 3000 (2200 lbs, 40.8 inches) (2200 lbs, 46.4 inches) 2750 2500 2250 2000 1750 1500 1250 1000 750 Loaded Airplane Weight (lbs) 500 250 0 32 33 34 35 36 37 38 39 40 41 42 43 Airplane C.G. Location, Inches Aft of Datum TABLE 2 (1733 lbs, 46.4 inches) 44 45 46 47 48 49 50 C.G. points APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172,A, NORMAL CATEGORY (+36.45) to (+46.4) at 1733 lb. or less (+40.8) to (+46.4) at 2200 lb. 8.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are changed in Center of Gravity from the Type Certificate Data Sheet. FEB - 9 2015 Date: FAA Approved 51 554 52 Page 6 of 80 DOCUMENT AE00-1FM Revision C 4250 4000 3750 3500 3250 3000 (2200 lbs, 40.8 inches) (2200 lbs, 46.4 inches) 2750 (1733 lbs, 36.4 inches) 2500 2250 2000 1750 Loaded Airplane Weight (lbs) 1500 1250 1000 750 500 (1733 lbs, 46.4 inches) 250 0- 32 33 34 35 36 37 38 39 40 41 42 43 44 45 Airplane C.G. Location, Inches Aft of Datum 46 47 C.G. points 48 49 TABLE 3 50 50 51 52 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172,A, NORMAL CATEGORY 7.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES (+36.4) to (+46.4) at 1733 lb. or less (+40.8) to (+46.4) at 2200 lb. CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1733 lbs, 36.4 inches) 3000 (2200 lbs, 40.8 inches) (2200 lbs, 46.4 inches) 2750 2500 2250 2000 1750 1500 1250 Loaded Airplane Weight (lbs) 1000 750 500 250 10+ 32 33 34 35 36 37 38 39 40 41 (1733 lbs, 46.4 inches) 42 43 44 45 46 47 48 49 50 51 C.G. points Airplane C.G. Location, Inches Aft of Datum TABLE 4 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172,A, NORMAL CATEGORY 6.00 X 6 NOSE TIRE (+36.4) to (+46.4) at 1733 lb. or less (+40.8) to (+46.4) at 2200 lb. 8.50 x 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. FEB - 9 2015 Date: FAA Approved 52 52 Page 7 of 80 DOCUMENT AE00-1FM Revision C Loaded Airplane Weight (lbs) 4250 4000 3750 3500 3250 (1733 lbs, 36.45 inches) 3000 (2200 lbs, 40.8 inches) (2200 lbs, 46.4 inches) 2750 2500 2250 2000 1750 1500 1250 1000 (1733 lbs, 46.4 inches) 750 500 250 0- 32 33 34 35 36 37 38 39 40 41 42 43 44 45 Airplane C.G. Location, Inches Aft of Datum 46 47 C.G. points 48 49 Loaded Airplane Weight (lbs) TABLE 5 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172,A, | (+36.45) to (+46.4) at 1733 lb. or less NORMAL CATEGORY (+40.8) to (+46.4) at 2200 lb. 7.00 X 6 NOSE TIRE 8.00 X 6 MAIN TIRES 5-0 CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are changed in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1733 lbs, 36.4 inches) 3000 (2200 lbs, 40.8 inches) (2200 lbs, 46.4 inches) 2750 2500 2250 155 51 52 552 (1733 lbs, 46.4 inches) 2000 1750 1500 1250 1000 750 500 250 0- 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 Airplane C.G. Location, Inches Aft of Datum C.G. points FEB - 9 2015 Date: FAA Approved TABLE 6 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172,A, NORMAL CATEGORY 6.00 X 6 NOSE TIRE (+36.4) to (+46.4) at 1733 lb. or less (+40.8) to (+46.4) at 2200 lb. 7.00 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft not listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. Page 8 of 80 DOCUMENT AE00-1FM Revision C 4250 4000- 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2200 lbs, 40.4 inches) (2200 lbs, 46.4 inches) 2750 2500 (1850 lbs, 46.4 inches) Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 250 0 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 C.G. points Airplane C.G. Location, Inches Aft of Datum TABLE 7 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172B (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.4) to (+46.4) at 2200 lb. ALL 3 TIRES SAME SIZE CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1850 lbs, 36.45 inches) 3000 (2200 lbs, 40.4 inches) (2200 lbs, 46.4 inches) 2750 2500 2250 2000 1750 1500 1250 1000 750 Loaded Airplane Weight (lbs) 500 250 (1850 lbs, 46.4 inches) 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 8 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172B (+36.45) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.4) to (+46.4) at 2200 lb. 8.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are changed in Center of Gravity from the Type Certificate Data Sheet. FEB - 9 2015 Date: FAA Approved .50 50 51 52 52 Page 9 of 80 DOCUMENT AE00-1FM Revision C 4250 4000 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2200 lbs, 40.4 inches) (2200 lbs, 46.4 inches) 2750 2500 (1850 lbs, 46.4 inches) 2250 Loaded Airplane Weight (lbs) 2000 1750 1500 1250 1000 750 500 250 0- 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 9 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172B (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.4) to (+46.4) at 2200 lb. 7.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES 50 50 51 52 CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2200 lbs, 40.4 inches) (2200 lbs, 46.4 inches) 2750 2500 2250 2000 1750 1500 Loaded Airplane Weight (lbs) (1850 lbs, 46.4 inches): 1250 1000 750 500 250 °- 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 10 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172B (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.4) to (+46.4) at 2200 lb. 6.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. Date: FEB - 9 2015 FAA Approved 52 62 Page 10 of 80 DOCUMENT AE00-1FM Revision C 4250 4000 3750 3500 3250 (1850 lbs, 36.45 inches) 3000 (2200 lbs, 40.4 inches) (2200 lbs, 46.4 inches) 2750 2500 (1850 lbs, 46.4 inches) Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 250 0- 32 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 11 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172B (+36.45) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.4) to (+46.4) at 2200 lb. 7.00 X 6 NOSE TIRE 50 50 51 52 8.00 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are changed in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2200 lbs, 40.4 inches) (2200 lbs, 46.4 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 250 0 32 22 33 (1850 lbs, 46.4 inches) 44 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 12 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172B (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.4) to (+46.4) at 2200 lb. 6.00 X 6 NOSE TIRE 550 50 51 52 FEB - 9 2015 7.00 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. Date: FAA Approved Page 11 of 80 DOCUMENT AE00-1FM Revision C 4250 4000 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2250 lbs, 40.5 inches) (2250 lbs, 46.4 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 (1850 lbs, 46.4 inches) 250 0+ 32 33 -3 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 13 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSE FORK 172C (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.5) to (+46.4) at 2250 lb. ALL 3 TIRES SAME SIZE CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1850 lbs, 36.45 inches) 3000 (2250 lbs, 40.5 inches) (2250 lbs, 46.4 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 250 ~(1850 lbs, 46.4 inches) 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 14 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSE FORK 172C (+36.45) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.5) to (+46.4) at 2250 lb. 8.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are changed in Center of Gravity from the Type Certificate Data Sheet. FEB - 9 2015 Date: FAA Approved Page 12 of 80 DOCUMENT AE00-1FM Revision C ... 4250 4000 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2250 lbs, 40.5 inches) (2250 lbs, 46.4 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 (1850 lbs, 46.4 inches) 250 0 - 32 33 34 35 36 37 38 39 40 41 42 43 44 45 Airplane C.G. Location, Inches Aft of Datum 46 47 48 C.G. points 49 19 TABLE 15 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSE FORK 172C (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.5) to (+46.4) at 2250 lb. 7.00 X 6 NOSE TIRE 50 51 52 8.50 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2250 lbs, 40.5 inches) (2250 lbs, 46.4 inches) 2750 2500 2250 (1850 lbs, 46.4 inches) 2000 1750 1500 1250 1000 750 500 250 0- · 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 -8 50 51 52 Airplane C.G. Location, Inches Aft of Datum C.G. points Loaded Airplane Weight (lbs) TABLE 16 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSE FORK 172C (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.5) to (+46.4) at 2250 lb. 6.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. Date: FEB-9 2015 FAA Approved Page 13 of 80 DOCUMENT AE00-1FM Revision C 4250 4000 3750 3500 3250 (1850 lbs, 36.45 inches) 3000 (2250 lbs, 40.5 inches) (2250 lbs, 46.4 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 (1850 lbs, 46.4 inches) 250 ° 32 33 34 35 36 37 38 39 40 41 42 43 44 45 Airplane C.G. Location, Inches Aft of Datum 46 47 C.G. points 48 49 50 51 52 TABLE 17 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSE FORK 172C (+36.45) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.5) to (+46.4) at 2250 lb. 7.00 X 6 NOSE TIRE 8.00 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft not listed are changed in Center of Gravity from the Type Certificate Data Sheet. 4250 4000 3750 3500 3250 (1850 lbs, 36.4 inches) 3000 (2250 lbs, 40.5 inches) (2250 lbs, 46.4 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 250 0- 32 3 33 34 35 36 37 38 39 40 41 (1850 lbs, 46.4 inches) 42 43 44 45 46 47 48 49 50 51 C.G. points Airplane C.G. Location, Inches Aft of Datum TABLE 18 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSE FORK 172C (+36.4) to (+46.4) at 1850 lb. or less NORMAL CATEGORY (+40.5) to (+46.4) at 2250 lb. 6.00 X 6 NOSE TIRE 7.00 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. Date: FEB - 9 2015 FAA Approved 52 22 Page 14 of 80 DOCUMENT AE00-1FM Revision C 4250 4000 3750 3500 3250 (1950 lbs, 35.0 inches) 3000 (2300 lbs, 38.5 inches) (2300 lbs, 47.3 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 (1950 lbs, 47.3 inches) 250 0- 72 32 33 34 35 36 37 38 39 40 41 42 43 Airplane C.G. Location, Inches Aft of Datum 44 45 46 47 C.G. points 48 49 TABLE 19 4250 4000- APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172D,E,F,G,H (+35.0) to (+47.3) at 1950 lb. or less NORMAL CATEGORY (+38.5) to (+47.3) at 2300 lb. ALL 3 TIRES 150 50 51 52 52 SAME SIZE CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are unchanged in Center of Gravity from the Type Certificate Data Sheet. 3750 3500 3250 (1950 lbs, 35.05 inches) 3000 (2300 lbs, 38.5 inches) (2300 lbs, 47.3 inches) 2750 2500 Loaded Airplane Weight (lbs) 2250 2000 1750 1500 1250 1000 750 500 (1950 lbs, 47.3 inches) 250 0 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 Airplane C.G. Location, Inches Aft of Datum C.G. points TABLE 20 APPROVED C.G. WITH AIRGLAS PA32-206LA NOSEFORK 172D,E,F,G,H (+35.05) to (+47.3) at 1950 lb. or less NORMAL CATEGORY (+38.5) to (+47.3) at 2300 lb. 8.00 X 6 NOSE TIRE 8.50 X 6 MAIN TIRES CENTER OF GRAVITY ENVELOPE FOR CESSNA 172 (SPECIFIC MODELS LISTED ABOVE) EQUIPPED WITH AN AIRGLAS, INC. PA32-206LA NOSE FORK. NOTE: Aircraft listed are changed in Center of Gravity from the Type Certificate Data Sheet. FEB - 9 2015 Date: FAA Approved Page 15 of 80