C206H-POH.pdf - Sydney Aviators
CESSNA TURBO 210L · Weight And Balance
Overview
The Cessna 206H Stationair Pilot's Operating Handbook (POH) provides essential information for pilots operating this aircraft model. It covers various aspects of the aircraft's operation, including performance data, operating limitations, and emergency procedures. The handbook is designed to assist pilots in understanding the aircraft's systems and ensuring safe operation. Key sections include preflight checks, normal and emergency procedures, and performance specifications, which are crucial for both new and experienced pilots. This document serves as a vital reference for flight planning and in-flight decision-making.
- Maximum Takeoff Weight (MTOW): 3,600 lbs
- Stall Speed (Landing Configuration): 61 knots
- Takeoff Distance Over 50 ft Obstacle: Approximately 1,600 ft
- Climb Rate: 730 ft/min at sea level
- Seating Capacity: Up to 6 occupants
Document
Source
Originally published by sydneyaviators.com.au. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Weight And Balance
- Pages
- 563
- File size
- 15 MB
- Publisher
- sydneyaviators.com.au
Specifications & performance
Extracted from this document.
Specifications
- Range (nm)
- 605
- Engine (hp)
- 300
- Propeller
- 3-Bladed, Constant Speed
- Wingspan (ft)
- 79
- Engine model
- IO-540-AC1A5
- Max speed (kt)
- 151
- Cruise speed (kt)
- 142
- Empty weight (lb)
- 3,614
- Fuel capacity (gal)
- 92
- Rate of climb (fpm)
- 988
- Service ceiling (ft)
- 15,700
- Max takeoff weight (lb)
- 3,600
Performance
- Landing over 50ft
- 735
- Takeoff over 50ft
- 910
- Landing distance (ft)
- 1,860
- Takeoff distance (ft)
- 988
V-speeds
- VS1
- 62
- VSO
- 54
Weight & balance
- Useful load (lb)
- 2,210
- Max ramp weight (lb)
- 3,614
- Baggage allowance (lb)
- 180
- Basic empty weight (lb)
- 3,600
- Max landing weight (lb)
- 3,600
- Max takeoff weight (lb)
- 3,600
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In this document
General Information
This section provides an overview of the Cessna 206H, including its specifications, dimensions, and general characteristics. The aircraft features a high-wing design, a seating capacity for up to six occupants, and is powered by a Lycoming IO-540-U4A5 engine, producing 300 horsepower.
Operating Limitations
The operating limitations section outlines critical parameters such as maximum takeoff weight (MTOW) of 3,600 lbs, maximum landing weight of 3,600 lbs, and a stall speed of 61 knots in landing configuration. These limitations are essential for safe flight operations.
Performance Data
This section details the aircraft's performance capabilities, including takeoff and landing distances, climb rates, and cruise speeds. For example, the takeoff distance over a 50-foot obstacle is approximately 1,600 feet at sea level on a standard day.
Emergency Procedures
Emergency procedures are outlined for various scenarios, including engine failure, electrical failure, and emergency landings. Pilots are instructed on the appropriate actions to take in these situations to ensure safety.
Weight and Balance
This section provides guidance on calculating weight and balance for the Cessna 206H. It includes charts and formulas to determine the center of gravity (CG) and ensure that the aircraft is within safe operating limits.
Safety notes
- Always adhere to the operating limitations specified in the POH.
- Perform thorough preflight checks to ensure aircraft readiness.
- In case of engine failure, follow the emergency procedures outlined in the handbook.
Full document text
6/04 NOTICE AT THE TIME OF ISSUANCE, THIS INFORMATION MANUAL WAS AN EXACT DUPLICATE OF THE OFFICIAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL AND IS TO BE USED FOR GENERAL PURPOSES ONLY. IT WILL NOT BE KEPT CURRENT AND, THEREFORE, CANNOT BE USED AS A SUBSTITUTE FOR THE OFFICIAL PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL INTENDED FOR OPERATION OF THE AIRPLANE. CESSNA AIRCRAFT COMPANY ORIGINAL ISSUE - 5 OCTOBER 1998 i ==: PERFORMANCE- SPECIFICATIONS CESSNA MODEL 206H PERFORMANCE - SPECIFICATIONS * SPEED Maximum at Sea Level Cruise, 75% Power at 6200 Ft CRUISE: 151 KTS .. 142 KTS Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve. 75% Power at 6200 Ft 88 Gallons Usable Fuel Max Range at 6500 Ft 88 Gallons Usable Fuel RATE OF CLIMB AT SEA LEVEL SERVICE CEILING TAKEOFF PERFORMANCE: Range 605 NM Time 4.3 HRS Range 730 NM Time 6.8 HRS 988 FPM Ground Roll .... Total Distance Over 50 Ft. Obstacle LANDING PERFORMANCE: Ground Roll Total Distance Over 50 Ft. Obstacle STALL SPEED (KCAS): Flaps Up, Power Off • Flaps Down, Power Off MAXIMUM WEIGHT: Ramp Takeoff Landing STANDARD EMPTY WEIGHT MAXIMUM USEFUL LOAD BAGGAGE ALLOWANCE • 15,700 FT 910 FT 1860 FT 735 FT 1395 FT 62 KCAS 54 KCAS 3614 LBS 3600 LBS 3600 LBS 2210 LBS " • • 1404 LBS 180 LBS 6/04 CESSNA MODEL 206H PERFORMANCE- SPECIFICATIONS PERFORMANCE-SPECIFICATIONS (Continued) WING LOADING: Lbs/Sq Ft POWER LOADING Lbs/HP FUEL CAPACITY OIL CAPACITY .. ENGINE: Textron Lycoming 300 BHP at 2700 RPM ... . PROPELLER: 3-Bladed, Constant Speed, Diameter " 20.7 12.0 92 GAL 11 QTS IO-540-AC1A5 79 IN The above performance figures are based on the indicated weights, standard atmospheric conditions, level, hard-surface dry runways and no wind. They are calculated values derived from flight tests conducted by The Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes and numerous factors affecting flight performance. 6/04 iii/(iv blank) Information Manual ☑ Member of GAMA Cessna A Textron Company The Cessna Aircraft Company Model 206H COPYRIGHT © 1998 The Cessna Aircraft Company Wichita, Kansas USA CESSNA MODEL 206H TABLE OF CONTENTS TABLE OF CONTENTS GENERAL " LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES PERFORMANCE WEIGHT & BALANCE/EQUIPMENT LIST AIRPLANE & SYSTEMS DESCRIPTION HANDLING, SERVICE & MAINTENANCE SUPPLEMENTS 6/04 SECTION 1 2 3 4 5 6 7 8 0 vii/(viii blank) CESSNA MODEL 206H SECTION 1 GENERAL TABLE OF CONTENTS SECTION 1 GENERAL Page Three View - Normal Ground Attitude Introduction 1-2 1-4 Descriptive Data Engine Propeller Fuel Oil 1-4 1-4 1-4 1-4 1-6 ... Maximum Certificated Weights Standard Airplane Weights Cabin And Entry Dimensions Baggage Space and Entry Dimensions Specific Loadings Symbols, Abbreviations and Terminology General Airspeed Terminology And Symbols Meteorological Terminology Engine Power Terminology Airplane Performance And Flight Planning Terminology Weight And Balance Terminology Metric / Imperial / U.S. Conversion Charts 1-7 1-7 1-7 1-7 1-7 1-8 1-8 1-9 1-9 1-10 .. 1-11 1-13 Weight Conversions 1-14 Length Conversions 1-16 Distance Conversions 1-20 Volume Conversions 1-21 Temperature Conversions 1-24 Volume to Weight Conversions 1-25 Quick Conversions 1-26 Revision 4 1-1 SECTION 1 GENERAL 1-2 79" MAX -13'-0" * * ° -36'-0" -8'-1" CESSNA MODEL 206H 1210T1002 1210T1002 Figure 1-1. Three View - Normal Ground Attitude (Sheet 1 of 2) May 30/01 CESSNA MODEL 206H 9'-3 1/2" MAX. NOTE 1: −28'-3” · SECTION 1 GENERAL WING SPAN SHOWN WITH STROBE LIGHTS INSTALLED. WHEEL BASE LENGTH IS 69 1/4". NOTE 2: NOTE 3: PROPELLER GROUND CLEARANCE IS 12”. NOTE 4: WING AREA IS 174 SQUARE FEET. NOTE 5: MINIMUM TURNING RADIUS (* PIVOT POINT TO OUTBOARD WING TIP) IS 26'-3". NOTE 6: NORMAL GROUND ATTITUDE IS SHOWN WITH NOSE STRUT SHOWING APPROXIMATELY 2" OF STRUT, AND WINGS LEVEL. 1210T1002 Figure 1-1. Three View - Normal Ground Attitude (Sheet 2 of 2) May 30/01 1-3 SECTION 1 GENERAL INTRODUCTION CESSNA MODEL 206H This handbook contains 9 sections, and includes the material required to be furnished to the pilot by FAR Part 23. It also contains supplemental data supplied by The Cessna Aircraft Company. Section 1 provides basic data and information of general interest. It also contains definitions or explanations of symbols, abbreviations, and terminology commonly used. DESCRIPTIVE DATA ENGINE Number of Engines: 1. Engine Manufacturer: Textron Lycoming. Engine Model Number: 10-540-AC1A5. Engine Type: Normally aspirated, direct drive, air-cooled, horizontally opposed, fuel injected, six cylinder engine with 541.5 cu. in. displacement. Horsepower Rating and Engine Speed: 300 rated BHP at 2700 RPM. PROPELLER Propeller Manufacturer: McCauley Propeller Systems. Propeller Model Number: B3D36C432/80VSA-1. Number of Blades: 3. Propeller Diameter: 79 inches. Propeller Type: Constant speed. | FUEL 1-4 A WARNING USE OF UNAPPROVED FUELS MAY RESULT IN DAMAGE TO THE ENGINE AND FUEL SYSTEM COMPONENTS, RESULTING IN POSSIBLE ENGINE FAILURE. (Continued Next Page) Revision 4 CESSNA MODEL 206H SECTION 1 GENERAL DESCRIPTIVE DATA (Continued) FUEL (Continued) Approved Fuel Grades (and Colors): 100LL Grade Aviation Fuel (Blue). 100 Grade Aviation Fuel (Green). NOTE Isopropyl alcohol or diethylene glycol monomethyl ether (DiEGME) may be added to the fuel supply. Additive concentrations shall not exceed 1% for isopropyl alcohol or 0.10% to 0.15% for DiEGME. Refer to Section 8 for additional information. Fuel Capacity Serials 20608001 thru 20608173: Total Capacity: 92.0 U.S. gallons. Total Usable: 88.0 U.S. gallons. Total Capacity Each Tank: 46.0 U.S. gallons. Total Usable Each Tank: 44.0 U.S. gallons. Serials 20608174 and on: Total Capacity: 92.0 U.S. gallons. Total Usable: 87.0 U.S. gallons. Total Capacity Each Tank: Total Usable Each Tank: 46.0 U.S. gallons. 43.5 U.S. gallons. NOTE
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To ensure maximum fuel capacity and minimize cross- feeding when refueling, always park the airplane in a wings- level, normal ground attitude and place the fuel selector in the Left or Right position. Refer to Figure 1-1 for normal ground attitude dimensions. Revision 4 (Continued Next Page) 1-5 SECTION 1 GENERAL CESSNA MODEL 206H OIL Oil Specification: MIL-L-6082 or SAE J1966 Aviation Grade Straight Mineral Oil: Used when the airplane was delivered from the factory and should be used to replenish the supply during the first 25 hours. This oil should be drained and the filter changed after the first 25 hours of operation. Refill the engine with MIL-L-6082 or SAE J1966 Aviation Grade Straight Mineral Oil and continue to use until a total of 50 hours has accumulated or oil consumption has stabilized. MIL-L-22851 or SAE J1899 Aviation Grade Ashless Dispersant Oil: Oil conforming to Textron Lycoming Service Instruction No. 1014, and all revisions and supplements thereto, must be used after first 50 hours or oil consumption has stabilized. Recommended Viscosity for Temperature Range: Above 16°C (60°F) Temperature Above 27°C (80°F) MIL-L-6082 or SAE J1966 Straight Mineral Oil SAE Grade MIL-L-22851 or SAE J1899 Ashless Dispersant Oil SAE Grade 60 40 or 50 60 50 -1°C (30°F) to 32°C (90°F) 40 40 |-18°C (0°F) to 21°C (70°F) 30 30, 40 or 20W-40 Below -12°C (10°F) 20 30 or 20W-30 -18°C (0°F) to 32°C (90°F) 20W-50 20W-50 or 15W-50 All Temperatures 15W-50 or 20W-50 NOTE When operating temperatures overlap, use the lighter grade oil. Oil Capacity: Sump: 11 U.S. Quarts ☐ Total: 12 U.S. Quarts 1-6 Jan 18/02 CESSNA MODEL 206H DESCRIPTIVE DATA (Continued) MAXIMUM CERTIFICATED WEIGHTS Ramp Weight: 3614 lbs. Takeoff Weight: 3600 lbs. Landing Weight: 3600 lbs. SECTION 1 GENERAL Weight in Baggage Compartment (Station 109 to 145): 180 lbs. maximum. NOTE Refer to Section 6 of this handbook for loading arrangements with one or more seats removed for cargo accommodations. STANDARD AIRPLANE WEIGHTS Serials 20608001 thru 20608173: Standard Empty Weight: 2204 lbs. Maximum Useful Load, Normal Category: 1410 lbs. Serials 20608174 and On: Standard Empty Weight: 2182 lbs. Maximum Useful Load, Normal Category: 1432 lbs. CABIN AND ENTRY DIMENSIONS Detailed dimensions of the cabin interior and entry door openings are illustrated in Section 6. BAGGAGE SPACE AND ENTRY DIMENSIONS Dimensions of the baggage area and baggage door opening are illustrated in detail in Section 6. SPECIFIC LOADINGS Wing Loading: Power Loading: 20.7 lbs./sq. ft. 12.0 lbs./hp Revision 5 1-7
What's in the CESSNA TURBO 210L 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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