Weight & Balance for Cessna 210
CESSNA 210 · Weight And Balance
Overview
This document provides essential weight and balance information for the Cessna 210 aircraft. It is designed for pilots and aviation personnel who need to understand the loading limits and weight distribution for safe flight operations. The document outlines the maximum weight capacities, center of gravity limits, and procedures for calculating weight and balance before flight. Proper weight and balance calculations are critical for ensuring the aircraft's performance and safety during operations.
- Maximum takeoff weight: 3,600 lbs
- Maximum landing weight: 3,600 lbs
- CG limits: 34.0 to 40.0 inches from datum
- Weight calculation must include aircraft, passengers, cargo, and fuel
- Proper weight and balance are critical for flight safety.
Document
Source
Originally published by flighttech.com.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 10
- File size
- 4.9 MB
- Publisher
- flighttech.com.au
Specifications & performance
Extracted from this document.
Specifications
- Max takeoff weight (lb)
- 3,600
Weight & balance
- Max landing weight (lb)
- 3,600
- Max takeoff weight (lb)
- 3,600
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In this document
Weight Limits
The Cessna 210 has a maximum takeoff weight of 3,600 lbs and a maximum landing weight of 3,600 lbs. It is crucial to adhere to these limits to ensure safe flight operations.
Center of Gravity (CG) Limits
The CG limits for the Cessna 210 are specified as 34.0 inches to 40.0 inches from the datum. Maintaining the CG within these limits is essential for stable flight.
Weight Calculation Procedures
Pilots must calculate the total weight by adding the weights of the aircraft, passengers, cargo, and fuel. The document provides a sample calculation to assist pilots in ensuring compliance with weight limits.
Safety notes
- Ensure that the total weight does not exceed the maximum takeoff or landing weight.
- Always check that the CG is within the specified limits before flight.
Full document text
Part A Weight & Balance Maintenance Data D. J. MACARTHUR 11 PARADISE COURT 4019 WEIGHT AND BALANCE RECORD (to be completed by a Weight and Balance Control Officer (WBCO)} Weight and Balance Report Ref: WB-3917 Centre of Gravity Position (CG) is LONGITUDINAL Configuration: CLONTARF AUSTRALIA PHONE: (07) 3283 3817 FAX: (07) 3319 6171 measured AFT of datum SIX SEATS TOTAL UNUSABLE FUEL & FULL ENGINE OIL AVA Aircraft Longitudinal Datum Fwd Face on Engine Firewall WEIGHT CONTROL AUTHORITY No. AQ45 Date 05-Jul-07 Part B Record of Empty Weight and Balance Date Description of Alteration 05-Jul-07 Revision and Re-issue Required INDEFINITE SUBJECT TO C.A.O. 100.7 Empty Weight and Empty Weight CG Reweigh Dated Weight (kg) Arm (mm) 1039.5 05-Jul-07 Index 1050 1091115 Maximum & Minimum Empty Weight & Empty Weight CG Revision and Reissue by WBCO is required when calculated running totals are Weight (kg) Arm (mm) MORE THAN or LESS THAN 1049.5 1029.5 1058 1042 (the person co-ordinating maintenance shall ensure that Part B is calculated and recorded in accordance with CAO 100.7) Running Total of Empty Weight and Empty Weight C of G Arm (mm) Moment Arm Weight and Balance Change from Datum Added (+) (mm) Weight (kg) Index Removed (-) Weight (kg) Index Weight (kg) 1039.5 1050 Index 1091115 Organisation Aircraft Type Registration Page D. MacArthur & Associates VH-TQC 1 of 1 Cessna 210N WEIGHT AND BALANCE RECORD D. MacArthur & Associates ABN 69 317 590 696 11 Paradise Court, Clontarf. QLD. 4019 Phone (07) 3283 3817 Fax (07) 3319 6171 Mobile 0439 328 338 AIRCRAFT WEIGHING SUMMARY REASON FOR REPORT C of A No. of Report Pages 9 These "Owners Copies" are supplied to ensure compliance with CAO 100.7 para 5.2 which requires that, "The owner or operator shall keep in a safe place on the ground, duplicate copies of all current approved loading data applicable to his aircraft." Aircraft Type Aircraft Registration Aircraft Serial No. Owner or Operator Cessna 210N VH-TQC 21063325 OWNERS COPY Fwd Face on Engine Firewall Archerfield EFM 136-457 D. MacArthur & Associates Aircraft Datum Place Scales Number Organisation Authority No. AQ-45 Work Order No. WB-3917 Date 05-Jul-07 LOAD DATA SHEET Issue No. ONE 3917-63325 Date of Expiry INDEFINITE Empty Weight Arm 1039.5 kg 1050 mm Index Units 1091115 kg.mm Page 1 of 9 Determination of Empty Weight Note 1: Note 2: The difference between the two gross weights must not exceed 0.2% or 10kg (whichever is the greater) otherwise further weighings must be carried out until two consecutive weighings agree within this tolerance. Readings should be made to the nearest 1kg. First Weighing Second Weighing Jack Point Cell Colour Scale Reading Zero Set Correction Actual Weight Cell Colour Scale Zero Reading Set Actual Average Correction Weight Weight PORT 356 356 Red 356 356 356.0 STBD Yellow 355 355 Yellow 354 354 354.5 NOSE Blue 326 326 Blue 326 326 326.0 TAIL First Weighing - Gross Total 1037 kg Second Weighing - Gross Total 1036 kg - Average Both Weighings 1036.5 kg Deductions kg Moment Arm kg kg kg + or - kg Total Deductions kg Additions Drainable unusable fuel 584 Moment Arm + or - 3.0 kg kg kg kg kg Total Additions 3.0 kg Gross Total (average of both weighings) 1036.5 kg Net Adjustment +/- 3.0 kg Empty Weight of Aircraft 1039.5 kg Configuration at time of weighing (refer also to equipment list) UNUSABLE FUEL & FULL ENGINE OIL Remarks Aircraft stripped, repainted, radio upgrade. Supervised by: Weight Control Officer The Colcha Date 05-Jul-07 AQ45 Page 2 of 9 Datum (Firewall, Front Face, Lower Portion) Sta. 0.0 C.G. N L & R -Level on Leveling Screws (Left Side of Tailcone) Centre of Gravity Determination Aircraft weighed on wheels using platforms Horizontal distance from datum to jack point Horizontal distance from datum to nose or tail jack point Note: First Weighing 1625 -200 mm mm Second Weighing 1625 mm -200 mm Distances measured aft of the datum are positive (+). Distances measured forward of the datum are negative (-). Moment Arm Average 1625 mm -200 mm Weight PORT STBD NOSE TAIL Weight kg + +/- mm 356.0 1625 354.5 1625 326.0 -200 Index Moment (kg.mm) + 578500 576063 Drainable unusable fuel 3.0 584 1752 65200 Moment Totals Aircraft Empty Moment Index 1156315 (1) 1091115 ((1)-(2)) 65200 (2) Aircraft Empty Weight (from page 2) 1039.5 kg Aircraft Empty Weight C of G (empty moment index) 1050 mm AFT of datum empty weight Prepared by: Date Supervised by: Weight Control Officer D. MacArthur & Associates 05-Jul-07 уже Date 05-Jul-07 AQ45 Page 3 of 9 List of items included in the empty weight of aircraft Aircraft Registration VH-TQC Details of Configuration Type Cessna 210N SIX SEATS TOTAL Issue No. ONE Date 05-Jul-07 Work Order WB-3917 Continental IO-520 1 INDICAT Airspeed Cabin Rate of Climb Compressor RPM Hartzel 3 Blade 1 Directional Gyro 2 Exhaust Gas Analyser Flight Hour 1 Magnetic Remote Indicating 1 Fuel Flow Duplex 1 0 Gyro Horizon 1 Stall Warning 1 Tachometer Non-recording Tachometer Recording Trim Indicator 1 1 Altimeters Ammeters Clocks Propeller Synchroniser ---0 1 Turn & Bank 1 Turn Co-ordinator 2 1 Undercarriage Position Lights Vertical Speed (rate of climb) 1 Voltmeters 0 Wing Flap Position 1 Brake Pressure Engine Oil Pressure Fuel Contents Fuel Pressure Hydraulic Oil Pressure Oil Contents Manifold Pressure Oxygen Pressure Duplex Suction Pressure Torque Meter OrNoo-oo-o Anti-Collision Instrument 1 A/R 1 Landing 1 2 0 Map reading Navigation 1 3 Signal 1 Taxi 1 0 Under Wing 2 1 -OONO----o--ONE---5--00-8 Carburettor Air Temp. Engine Temp. Oil Temp. Outside Air Temp. Turbine Temp. Exhaust Gas Temp. Digital Engine Monitoring C.H.T & E.G.T C.H.T. O---o- Insight 1 Fuel, Main Fuel, Auxiliary Fuel, Wing Tip Fuel, Other Cargo Restraint Cordage/Webbing Freight Restraint Nets Inertia Reels Lap-sash Assemblies Lap Assemblies 2000 OONO Page 4 of 9 4 A.D.F. Auto pilot Cabin Speakers D.M.E. Glide Slope Rec. S-Tec Part of Navs Head Phones H.F VAR V.H.F. GNS 480/GNC 250XL V.H.F. Nav. Rec.
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E.L.T. GNS 480 ACK-E01 Transponder Garmin GTX 330 GPS Garmin GNS480/GNC 250XL OF-ONOOONN--~---- Audio/Mkr Garmin GMA 340 Display Garmin MX20 Storm Scope BFG Hand Mike NEOUS EQUIPMENT Dual Controls De-icer Boots Fire Ext. (engine) Fire Ext. (portable) Fixed Ballast Hydraulic Pumps L/G Warning Horn Oxygen Equipment Combustion Heater Vacuum Pumps Landing Gear Mirrors Fuel, Main Liters 3.8 Fuel, Auxiliary 0 Fuel, Other 0 Oil, Hydraulic Full Oil, Lubricating Full Alternators Batteries Generators Starters External Power 1 24 Volt 1 Weight Control Officer Signature DISPOSA Crash Axe Flight Control Locks First Aid Outfits Disposable Ballast Signalling Apparatus Torch FAA Flight Manual Head Rests 1 1 --0-- 300-0--00-- SPECIAL PURPOSE EQUIP ymal уж AQ45 Date 00000004 05-Jul-07 Page 5 of 9 Aircraft Registration VH-TQC DETERMINE BASIC WEIGHT ITEM EMPTY WEIGHT ΔΙΑ Work Order WB-3917 WEIGHT ARM INDEX MOMENT 1039.50 1050 1091115 BASIC WEIGHT 1039.5 1050 1091115 BASIC WEIGHT: DETERMINE INDEX 7 DETERMINE MAX & MINIMUM EMPTY C of G AND ARM FOR REWEIGH 0.5% or 10kg which ever is greater Max Take Off weight kg = 1723 = 0.5% MTOW 9.00 2% or 5mm which ever is the greater Max C of G range mm = +/- empty weight 10 kg = 2% C of G +/- mm C of G 406.4 8.00 8 mm We Me weight Date 05-Jul-07 Control Officer AQ45 Page 6 of 9 11 PARADISE COURT CLONTARF QLD. AUSTRALIA 4019 Phone: (07) 3283 3817 Fax: Mobile (07) 3319 6171 0439 328 338 Aircraft Type Cessna 210N LOAD DATA SHEET D. MacArthur & Associates (NAME OF ORGANISATION) S/N 21063325 Aircraft Reg VH-TQC Approved Loading System Cessna 210N Pilots Operating Handbook Section 6 AUTHORISED DATE DATE OF EXPIRY INDEFINITE ISSUE D. J. MacArthur 05-Jul-07 ONE SUBJECT TO C.A.O. 100.7 APPROVED D.J. Ph Riha WEIGHT CONTROL AUTHORITY No. AQ45 DATE 05-Jul-07 ITEM WEIGHT ARM Kg MOMENT mm INDEX * (IU) CONFIGURATION (ALSO SEE EQUIPMENT LIST) EMPTY WEIGHT 1039.5 1050 1091115 EMPTY WEIGHT IMPERIAL SIX SEATS TOTAL |WEIGHT Lbs ARM Inches MOMENT SIX SEATS TOTAL 2291.7 41.3 94705 THE ABOVE WEIGHTS INCLUDE: EMPTY WEIGHT: UNUSABLE FUEL & FULL ENGINE OIL LOAD SYSTEM 1) REFER TO FLIGHT MANUAL & SUPPLEMENTS FOR LOAD LIMITATIONS. 3917-63325 WORK ORDER DATUM WB-3917 Fwd Face on Engine Firewall FORM DMA001LDS Page 7 of 9 Aircraft Registration VH-TQC ΔΙΑ Work Order WB-3917 LOADING CHECK A/C Weight Arm Moment Moment Arm Weight PLOT # 1 FWD AFT 1039.5 1091115 1050 1039.5 OK OK Pilot 86 940 80840 1171955 1041 1125.5 OK OK Pax Front 86 940 80840 1252795 1034 1211.5 OK OK Row 2 172 1803 310116 1562911 1130 1383.5 OK OK Row 3 120 2565 307800 1870711 1244 1503.5 OK OK Wheelwell 30 2972 89160 1959871 1278 1533.5 OK OK Aft Bag 30 3505 105150 2065021 1321 1563.5 OK OK Fuel 236Kg 159.0 1092 173628 2238649 1300 1722.5 OK OK 2238649 1300 1722.5 OK OK TAUW 1722.5 MTOW 1723 A/C Weight Arm Moment Moment Arm Weight PLOT #2 FWD AFT 1039.5 1091115 1050 1039.5 OK OK Pilot 86 940 80840 1171955 1041 1125.5 OK OK Pax Front 86 940 80840 1252795 1034 1211.5 OK OK Row 2 172 1803 310116 1562911 1130 1383.5 OK OK Row 3 2565 1562911 1130 1383.5 OK OK Wheelwell 68 2972 202096 1765007 1216 1451.5 OK OK Aft Bag 56 3505 196280 1961287 1301 1507.5 OK OK Fuel 215.0 1092 234780 2196067 1275 1722.5 OK OK TAUW 1722.5 MTOW 1723 A/C Weight Arm Moment Moment Arm Weight PLOT #3 FWD AFT 1039.5 1091115 1050 1039.5 OK OK Pilot 86 940 80840 1171955 1041 1125.5 OK OK Pax Front 940 1171955 1041 1125.5 OK OK Row 2 1803 1171955 1041 1125.5 OK OK Row 3 2565 1171955 1041 1125.5 OK OK Wheelwell 2972 1171955 1041 1125.5 OK OK Aft Bag 3505 1171955 1041 1125.5 OK OK Fuel 236.0 1092 257712 1429667 1050 1361.5 OK OK TAUW 1361.5 MTOW 1723 Date 05-Jul-07 Weight Control Officer AQ45 Page 8 of 9 Weight Kg 1800 1700 ΔΙΑ Cessna 210N Work Order WB-3917 1600 FWD LIMIT 1500 1080 VH-TQC 1400 1130 1130 940 PLOT #50 1300 1034 1034 1200 1041 1041 1100 1000 900 1000 1050 1050 1275 # 43004346 PLOT # 1 1278 > 121301 a 1216 PLOT #2 1321 AFT LIMIT 1346 1100 1200 1300 1400 C of G mm PLOT #1 FULL OCCUPANTS 4 @ 86Kg EACH, ROW 3 60Kg EACH, 60Kg BAGGAGE FUEL TO ALL UP WEIGHT. PLOT #2 FOUR OCCUPANTS @ 86Kg EACH, NIL PAXS ROW 3, BAGGAGE 68Kg (wheelwell) 56Kg (Rear) FUEL TO ALL UP WEIGHT PLOT #3 PILOT ONLY @ 86Kg, FULL FUEL Date 05-Jul-07 Weigh Control Officer AQ45 Page 9 of 9
What's in the CESSNA 210 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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