Cessna Skylane 182T Operating Handbook
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Cessna Skylane 182T, CESSNA MODEL 182T NAV Ill SECTION 4 NORMAL PROCEDURES CRUISE (Continued) FUEL VAPOR PROCEDURES The engine fuel system can cause fuel vapor formation on tht ground during warm weather. This will generally occur when tht outside ambient air temperature is above 80°F. Vapor formatior may increase when the engine fuel flows are lower at idle and tax engine speeds. The following procedures are recommended wher engine idle speed and fuel flow fluctuations show that fuel vapo may be prese
Cessna Skylane 182T, CESSNA MODEL 182T NAV I I I SECTION 5 PERFORMANCE SAMPLE PROBLEM (Continued) With an expected 10 knot headwind, the ground speed for cruise is predicted to be: 130 -1 0 1% Knots Therefore, the time required for the cruise portion of the trip is: 429 Nautical Miles = 3.6 Hours 120 Knots The fuel required for cruise is: 3.6 hours X 10.7 gallons/hour = 38.5 Gallons A 45-minute reserve requires: 45 - 60 X 10.7 gallons 1 hour = 8.0 Gallons The total estimated fuel required is as follows: Engine start, taxi, and takeoff 1.7 Climb 3.2 Cruise 38.5 Reserve
Cessna Skylane 182T, CESSNA MODEL 182T NAV I I I SECTION 5 PERFORMANCE ALTIMETER CORREC'TION ALTERNATE STATIC SOURCE NOTE Add correction to desired altitude to obtain indicated altitude to fly. Windows closed, ventilators closed, cabin heater, cabin air, and defroster on maximum. CONDITIONS: Power required for level flight or maximum power descent cruise configuration. Altimeter corrections for the takeoff configuration are less than 50 feet. CONDITION FLAPS UP S.L. 2000 FT 4000 FT 6000 FT 8000 FT 10,000 FT 12,000 FT 14,000 FT Figure 5-2 1 82TPHAUS-00 CONDITION FLAPS FULL S.L. 2000 FT 4000 FT 6000 FT 8000 FT 10,000 F
Cessna Skylane 182T, CESSNA MODEL 182T NAV Ill SECTION 5 PERFORMANCE CRUISE PERFORMANCE PRESSURE ALTITUDE 4000 FEET CONDITIONS: 31 00 Pounds Recommended Lean Mixture Cowl Flaps Closed NOTE RPM 2400 2300 2200 1. Maximum cruise power is 8O0lO MCP. Those powers above that value in the table are for interpolation purposes only. 2. For best economy, operate at peak EGT. Figure 5-9 (Sheet 5) MP 25 24 23 22 21 20 25 24 23 22 21 20 25 24 23 22 21 20 U.S. 5-25 20°C BELOW STANDARD TEMP BOhP --- 84 79 74 70 65 --- 81 76 72 67 62 82 78 73 69 65 60 STANDARD TEMPERATURE -13°C KTAS --- 140 138
Cessna Skylane 182T, SECTION 3 EMERGENCY PROCEDURES CESSNA MODEL 182T NAV Ill ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS (Continued) INSUFFICIENT RATE-OF-CHARGE When the over-voltage sensor circuit, or other fault, opens the alternator (ALT FIELD) circuit breaker and de-energizes the alternator, a discharge (-) current will be shown on the main battery ammeter and the low voltage annunciator (LOW VOLTS) will come on. The ACU can de-energize the alternator due to minor disturbances in the electrical system, resulting in a "nuisance" opening of the ALT FIELD circuit breaker. If t
Cessna Skylane 182T, CESSNA SECTlOlV 7 MODEL 182T NAV Ill AIRPLANE AND SYSTEMS DESCRIP-I-ION ENGINE (Continued) IGNITION AND STARTER SYSTEM Engine ignition is provided by two engine-driven magnetos, and two spark plugs in each cylinder. 'The right magneto fires the lower right and upper left spark plugs, and the left magneto fires the lower left and upper right spark plugs. Normal operation is conducted with both magnetos due to the more complete burning of the fuellair mixture with dual ignition. Ignition and starter o
Cessna Skylane 182T, SECTION 8 CESSNA HANDLING, SERVICE AhlD MAINTENANCE MODEL 182T NAV Ill AIRPLANE FILE There are miscellaneous data, information and licenses that are a part of the airplane file. The following is a checklist for that file. In addition, a periodic check should be made of the latest Federal Aviation Regulations to ensure that all data requirements are met. To be displayed in the airplane at all times: 1. Aircraft Airworthiness Certificate (FAA Form 81 00-2). 2. Aircraft Registration Certificate (FAA
SECTION 6 CESSIVA WEIGHT AND BALANCEIEQUIPMENT LIST MODEL 182T NAV Ill 84065 AIRPLANE WEIGHING FORM Locating CG with Airplane on Landing Gear X (Inches Aft of Datum) =A - Nosewheel Weight x [ Total Weight* 1 Locating Percent MAC *(Nose + L + R Wheel Weights) (CG Arm of Airplane) - 25.98 CG Percent MAC = 0.5880 Levelina Provisions Longitu
Cessna Skylane 182T, SECTION 8 CESSNA HANDLING, SERVICE AND MAINTENANCE MODEL 182T NAV Ill CESSNA CUSTOMER CARE PROGRAM Specific benefits and provisions of the Cessna Warranty plus other important benefits for you are contained in your Customer Care Program Handbook supplied with your airplane. The Customer Care Program Handbook should be thoroughly reviewed and kept in the airplane at all times. You will also want to return to your Cessna Service Station either at 50 hours for your first Progressive Care Operation, or at 100 hours for your first 100 hour inspection depending on which program you
SECTION 7 CESSN A AIRPLANE AND SYSTEMS DESCRIPTION MODEL 182T NAV Ill ELECTRICAL SYSTEM (Continued) EXTERNAL POWER RECEPTACLE (Continued) NOTE Set the AVIONICS switches BUS 1 and BUS 2 to OFF if no avionics are required. If maintenance on the avionics equipment is required, a 28 VDC regulated and filtered external power source must be provided
Cessna Skylane 182T, SECTION 7 CESSNA AIRPLANE AND SYSTEMS DESCRIPTION MODEL 182T NAV Ill CABIN HEATING, VENTILATING AND DEFROSTING SYSTEM (Continued) Separate adjustable ventilators supply additional air; one near each I upper corner of the windshield supplies air for the pilot and front passenger, and two ventilators are available for the rear cabin area to supply air to the rear seat passengers. There are additional ventilators located in various positions in the cockpit. PITOT-STATIC SYSTEM AND INSTRUMENTS The pitot-static system uses a heated total pressure (pitot) head mounted on the lower surface of the left wing, external static
Cessna Skylane 182T, CESSNA MODEL 182T NAV Ill SECTlOlV 1 GENERAL INTRODUCTION 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 Cessna Aircraft Company. Section 1 provides basic data and information of general interest. It also contains definitions and explanations of symbols, abbreviations, and terminology commonly used. DESCRIPTIVE DATA ENGINE Number of Engines: 1. Engine Manufacturer: Textron Lycoming. Engine Model Number: 10-540-AB1 A5. Engine Type: Normally aspirated, direct drive, air-cooled, horizontally opposed, fuel i
Cessna Skylane 182T, SECTION 5 PERFORMANCE CESSNA MODEL 182T NAV I I I TIME, FUEL AND DISTANCE TO CLIMB AT 3100 POUNDS NORMAL CLIMB - 90 KlAS CONDITIONS: Flaps Up 2400 RPM, 23 in. Hg. or full throttle (whichever is less), mixture 15 GPH or full rich (whichever is less). Cowl flaps as required. Standard Temperature NOTE 1. Add 1.7 gallons of fuel for engine start, taxi and takeoff al- lowance. 2. Mixture leaned to Maximum Power Fuel Flow placard value for smooth engine operation and increased power. 3. Increase time, fuel and distance by 10% for each 10°C above standard temperature. 4. Distances shown are based on zero wind. Press Alt - Feet S.L. 2000
Cessna Skylane 182T, CESSNA MODEL 182T NAV Ill SECTION 3 ENIERGENCY PROCEDURES ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS (Continued) IF LOW VOLTS ANNUNCIATOR REMAINS ON (Continued) 9. Land as soon as practical. NOTE Make sure a successful landing is possible before extending flaps. The flap motor is a large electrical load during operation. AIR DATA SYSTEM FAILURE RED X - PFD AIRSPEED INDICATOR 1. ADCIAHRS Circuit Breakers - CHECK IN (ESS BUS and AVN BUS 1). If open, reset (close) circuit breaker. If circuit breaker opens again, do not reset. 2. Standby
Cessna Skylane 182T, SECTION 7 CESSNA AIRPLANE AND SYSTEMS DESCRIPTION MODEL 182T NAV Ill ELECTRICAL SYSTEM (Continued) 81524 r-~.-------...--------...-----.-...-----.--~ , Power To LOW VOLT Battery ++- Circuit Breaker External Power 077011519 It Figure 7-7 (Sheet 1 of 3) 7-48 U.S.
Cessna Skylane 182T, CESSNA MODEL 182T NAV Ill SECTION 5 PERFORMANCE STALL SPEEDS AT 31 00 POUNDS CONDITIONS: Power OFF MOST REARWARD CENTER OF GRAVITY MOST FORWARD CENTER OF GRAVITY FLAP SETTING UP 20" FULL NOTE ANGLE OF BANK FLAP SETUNG UP 20" FULL 1. Altitude loss during a stall recovery may be as much as 250 feet. 2. KlAS values are approximate. Figure 5-4 0" ANGLE OF BANK U.S. 5-13 KlAS 50 43 40 KCAS 54 50 49 30" 0" KlAS 54 46 43 KlAS 51 44 41 KCAS 58 54 53 45" KCAS 56 52 50 30" KlAS 59 51 48 60" KlAS 55 47 44 KC
Cessna Skylane 182T, CESSNA MODEL 182T NAV Ill SECTION 5 PERFORMANCE CRUISE PERFORMANCE PRESSURE ALTITUDE 14,000 FEET CONDITIONS: 31 00 Pounds Recommended Lean Mixture Cowl Fla~s Closed NOTE RPM 2400 2300 2200 2100 1. Maximum cruise power is 80% MCP. Those powers above that value in the table are for interpolation purposes only. 2. For best economy, operate at peak EGT. Figure 5-9 (Sheet 1 1 ) MP 16 15 16 16 16 U.S. 5-31 20°C BELOW STANDARD TEMP -33°C BEP 56 50 53 51 49 STANDARD TEMPERATURE -13°C KTAS 126 118 123 120 116 BEp 53 48 51 20°C ABOVE STANDARD TEMP 7°C GPH 10.1 9.4 9.8
Cessna Skylane 182T, CESSNA SECTION 6 MODEL 182T NAV Ill WEIGHT AND BALANCEIEQLIIPMENT LIST SAMPLE LOADING PROBLEM WEIGHT AND MOMENT TABULATION ITEM DESCRIPTION providing that flight time is allowed for fuel burn-off to a maximum of 2950 pounds before landing. The maximum allowable combined weight capacity for baggage in areas A, B and C is 200 pounds. The maximum allowable combined weight capacity in areas B and C is 80 pounds. R Figure 6-3 (Sheet 1 of 2) I I 1 82TPHAUS-02 U.S. 6-11
CESSNA MODEL 182T NAV Ill SECTION 2 OPERATING LIMITATIONS MANEUVER LIMITS This airplane is certificated in the normal category. The normal category is applicable to aircraft intended for non aerobatic operations. These include any maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights, chandelles, and turns in which
Cessna Skylane 182T, CESSNA MODEL 182T NAV Ill SECTION 3 EMERGENCY PROCEDURES VACUUM SYSTEM FAILURE LOW VACUUM ANNLINCIATOR COMES ON 1. Vacuum Indicator (VAC) - CHECK EIS SYSTEM page to make sure vacuum pointer is in green arc limits. CAUTION IF VACUUM POINTER IS OUT OF THE GREEN ARC DURING FLIGHT OR THE GYRO FLAG IS SHOWN ON THE STANDBY ATTITUDE INDICATOR, THE STANDBY ATTITUDE INDICATOR MUST NOT BE - -USED FOR ATTITUDE INFORMATION. HlGH CARBON MONOXIDE ANNUNCIATOR (if installed) LEVELl CO LVL HlGH ANNUNCIATOR COMES ON I 1. CABIN HT Knob - OFF (push full in) 2. CABIN AIR Knob - ON (pu
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