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Cessna skylance tc T182T Information Manual

Cessna skylance tc T182T Manual Online:

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Cessna skylance tc T182T User Manual
Cessna skylance tc T182T User Guide
Cessna skylance tc T182T Online Manual

Text of Cessna skylance tc T182T User Guide:

  • Cessna skylance tc T182T, SECTION 5 CESSNA PERFORMANCE MODEL T182T NAV III GFC 700 AFCS U.S. SAMPLE PROBLEM The following sample flight problem utilizes information from the various charts to determine the predicted performance data for a typical flight. Assume the following information has already been determined: (Continued Next Page) AIRPLANE CONFIGURATION: Takeoff weight 3100 Pounds Usable fuel 87.0 Gallons TAKEOFF CONDITIONS: Field pressure altitude 3500 Feet Temperature 24°C (16°C Above Standard) Wind component along runway 12 Knot Headwind Field length 3500 Feet CRUISE CONDITIONS: Total distance 450 Nautical Miles Pressure altitude 11,500 Feet Temperature 8°C Expected wind enroute 10 Knot Headwind LANDIN

  • Cessna skylance tc T182T, CESSNA SECTION 4 MODEL T182T NAV III NORMAL PROCEDURES GFC 700 AFCS U.S. BEFORE STARTING ENGINE 1. Preflight Inspection - COMPLETE 2. Passenger Briefing - COMPLETE 3. Seats and Seat Belts - ADJUST and LOCK (verify inertia reel locking) 4. Brakes - TEST and SET 5. Circuit Breakers - CHECK IN 6. Electrical Equipment - OFF 7. AVIONICS Switch (BUS 1 and BUS 2) - OFF CAUTION THE AVIONICS SWITCH (BUS 1 AND BUS 2) MUST BE OFF DURING ENGINE START TO PREVENT POSSIBLE DAMAGE TO AVIONICS. 8. Cowl Flaps - OPEN 9. FUEL SELECTOR Valve - BOTH T182TPHBUS-00 4-11

  • Cessna skylance tc T182T, CESSNA SECTION 9 - SUPPLEMENTS MODEL T182T NAV III SUPPLEMENT 1 GFC 700 AFCS U.S. FAA APPROVED SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement. This list contains only those Service Bulletins that are currently active. Number Title Airplane Serial Effectivity Revision Incorporated Incorporated in Airplane T182TPHBUS-S1-00 S1-3

  • SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL T182T NAV III GFC 700 AFCS U.S. ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS Malfunctions in the electrical power supply system can be detected through regular monitoring of the main battery ammeter (M BATT AMPS) and the main electrical bus voltmeter (M BUS VOLTS); however, the cause of these malfunctions is usually difficult

  • Cessna skylance tc T182T, CESSNA SECTION 9 - SUPPLEMENTS MODEL T182T NAV III SUPPLEMENT 4 GFC 700 AFCS U.S. FAA APPROVED NORMAL PROCEDURES (Continued) ADF TEST (PREFLIGHT or IN FLIGHT): 1. ADF Button - SELECT ANT mode and note pointer moves to 90° position. 2. ADF Button - SELECT ADF mode and note the pointer moves without hesitation to the station bearing. Excessive pointer sluggishness, wavering or reversals indicate a signal that is too weak or a system malfunction. TO OPERATE BFO: 1. OFF/VOL Control - ON 2. BFO Button

  • Cessna skylance tc T182T, CESSNA SECTION 7 MODEL T182T NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCS U.S. INTRODUCTION This section provides description and operation of the airplane and its systems. Some equipment described herein is optional and may not be installed in the airplane. Refer to Section 9, Supplements, for details of other optional systems and equipment. AIRFRAME The airplane is an all metal, four-place, high wing, single-engine airplane equipped with tricycle landing gear and is designed for general utility purposes. The construction of the fuselage is a conventional formed sheet metal bulkhead,

  • Cessna skylance tc T182T, SECTION 7 CESSNA AIRPLANE AND SYSTEM DESCRIPTION MODEL T182T NAV III GFC 700 AFCS U.S. ELECTRICAL SYSTEM (Continued) EXTERNAL POWER RECEPTACLE A external power receptacle is integral to the power distribution module and allows the use of an external power source for cold weather starting or for lengthy maintenance work on electrical and avionics equipment. The receptacle is located on the left side of the cowl near the firewall. Access to the receptacle is gained by opening the receptacle door. NOTE Set the AVIONICS switches BUS 1 and BUS 2 to OFF if no avionics are required. If maintenance on the avionic

  • Cessna skylance tc T182T, CESSNA SECTION 5 MODEL T182T NAV III PERFORMANCE GFC 700 AFCS U.S. TIME, FUEL AND DISTANCE TO CLIMB AT 3100 POUNDS NORMAL CLIMB - 95 KIAS CONDITIONS: Flaps UP 2400 RPM, 25 in.hg. or mixture set at 16 GPH Cowl Flaps OPEN Standard Temperature NOTE • Add 2.0 gallons of fuel for engine start, taxi and takeoff allowance. • Increase time, fuel and distance by 10% for each 8°C above standard temperature. • Distances shown are based on zero wind. Figure 5-8 (Sheet 2) Pressure Altitude Feet Climb Speed KIAS Rate of Climb FPM From Sea Level Time Minutes Fuel Used Gallons Distance NM Sea Level 95 560 0 0.0 0 2000 95 545 4 1.0 6 4000 95 530 7 2.0 12 6000

  • Cessna skylance tc T182T, CESSNA SECTION 7 MODEL T182T NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCS U.S. ELECTRICAL SYSTEM (Continued) CIRCUIT BREAKERS AND FUSES Individual system circuit breakers are found on the circuit breaker panel below the pilot's control wheel. All circuit breakers on ESSENTIAL BUS, AVIONICS BUS 1 and AVIONICS BUS 2 are capable of being opened or disengaged from the electrical system by pulling straight out on the outer ring for emergency electrical load management. Using a circuit breaker as a switch is discouraged since the practice will decrease the life of the circuit breaker. All circuit bre

  • Cessna skylance tc T182T, CESSNA SECTION 7 MODEL T182T NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCS U.S. STANDARD AVIONICS The Garmin G1000 Avionics System is an integrated flight control and navigation system. The system combines primary flight instruments, communications, airplane system information and navigational information all displayed on two color displays. The G1000 system consists of the following pieces of equipment: GARMIN DISPLAY UNITS (GDU) Two identical units are mounted on the instrument panel. One, located in front of the pilot, is configured as a

  • Cessna skylance tc T182T, CESSNA SECTION 4 MODEL T182T NAV III NORMAL PROCEDURES GFC 700 AFCS U.S. STARTING ENGINE (Continued) RECOMMENDED STARTER DUTY CYCLE Operate the starter motor for 10 seconds followed by a 20 second cool down period. This cycle can be repeated two additional times, followed by a ten minute cool down period before resuming cranking. After cool down, operate the starter motor again, three cycles of 10 seconds followed by 20 seconds of cool down. If the engine still does not start, try to find the cause. LEANING FOR GROUND OPERATIONS For all ground operations, after starting the engine and when the engine is running smoothly: 1. Set the th

  • Cessna skylance tc T182T, SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL T182T NAV III GFC 700 AFCS U.S. AUTOPILOT OR ELECTRIC TRIM FAILURE AP OR PTRM ANNUNCIATOR(S) COME ON 1. Control Wheel - GRASP FIRMLY (regain control of airplane) 2. A/P TRIM DISC Button - PRESS and HOLD (throughout recovery) 3. Elevator and Rudder Trim Controls - ADJUST MANUALLY (as necessary) 4. AUTO PILOT Circuit Breaker - OPEN (pull out) 5. A/P TRIM DISC Button - RELEASE WARNING FOLLOWING AN AUTOPILOT, AUTOTRIM OR MANUAL ELECTRIC TRIM SYSTEM MALFUNCTION, DO NOT E

  • Cessna skylance tc T182T, SECTION 5 CESSNA PERFORMANCE MODEL T182T NAV III GFC 700 AFCS U.S. SAMPLE PROBLEM (Continued) FUEL REQUIRED (Continued) With an expected 10 knot headwind, the ground speed for cruise is predicted to be: Therefore, the time required for the cruise portion of the trip is: The fuel required for cruise is: A 45-minute reserve requires: The total estimated fuel required is as follows: Once the flight is underway, ground speed checks will provide a more accurate basis for estimating the time enroute and the corresponding fuel required to c

  • Cessna skylance tc T182T, SECTION 7 CESSNA AIRPLANE AND SYSTEM DESCRIPTION MODEL T182T NAV III GFC 700 AFCS U.S. FLIGHT INSTRUMENTS The G1000 Integrated Cockpit System primary flight instrument indications are shown on the PFD. The primary flight instruments are arranged on the PFD in the basic T configuration. The Attitude Indicator (AI) and Horizontal Situation Indicator (HSI) are centered vertically on the PFD and are conventional in appearance and operation. Vertical tape-style (scrolling scale) indicators with fixed p

  • Cessna skylance tc T182T, SECTION 8 CESSNA AIRPLANE HANDLING, SERVICE MODEL T182T NAV III AND MAINTENANCE GFC 700 AFCS U.S. LANDING GEAR Consult the following table for servicing information on the landing gear. * Keep strut filled with MIL-H-5606 hydraulic fluid per filling instructions placard, and with no load on the strut, inflate with air to 55.0-60.0 PSI. Do not over inflate. COMPONENT SERVICING CRITERIA Nose Wheel (5.00-5, 6-Ply Rated Tire) 49.0 PSI Main Wheel (6.00-6, 6-Ply Rated Tire) 42.0 PSI Brakes MIL-H-5606 Nose Gear Shock Strut MIL-H-5606; 55.0-60.0 PSI * T182TPHBUS-00 8-22

  • Cessna skylance tc T182T, CESSNA SECTION 8 MODEL T182T NAV III AIRPLANE HANDLING, SERVICE GFC 700 AFCS AND MAINTENANCE U.S. CLEANING AND CARE (Continued) PROPELLER CARE Preflight inspection of propeller blades for nicks, and wiping them occasionally with an oily cloth to clean off grass and bug stains will assure long blade life. Small nicks on the propeller, particularly near the tips and on the leading edges, should be dressed out as soon as possible since these nicks produce stress concentrations, and if ignored, may result in cracks or failure of the propeller blade. Never use an alkaline cleaner on the blades; remove grease and dirt with Stoddard solvent.

  • Cessna skylance tc T182T, SECTION 2 CESSNA OPERATING LIMITATIONS MODEL T182T NAV III GFC 700 AFCS U.S. FAA APPROVED AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown in Figure 2-1. AIRSPEED LIMITATIONS SYMBOL SPEED KCAS KIAS REMARKS V NE Never Exceed Speed 170 175 Do not exceed this speed in any operation. V NO Maximum Structural Cruising Speed 137 140 Do not exceed this speed except in smooth air, and then only with caution. V A Maneuvering Speed: 3100 Pounds 2600 Pounds 2100 Pounds 110 101 92 110 101 91 Do not make full or abrupt cont

  • Cessna skylance tc T182T, CESSNA SECTION 7 MODEL T182T NAV III AIRPLANE AND SYSTEM DESCRIPTION GFC 700 AFCS U.S. FLIGHT INSTRUMENTS (Continued) HORIZONTAL SITUATION INDICATOR The Horizontal Situation Indicator (HSI) is found along the lower center area of the PFD. The heading indication data is provided by the AHRS and magnetometer units. The HSI combines a stabilized magnetic direction indicator (compass card) with selectable navigation deviation indicators for GPS or VHF navigation. The HSI is conventional in appearance and operation. Magnetic heading is shown numeri

  • CESSNA SECTION 9 - SUPPLEMENTS MODEL T182T NAV III SUPPLEMENT 4 GFC 700 AFCS U.S. FAA APPROVED SERVICE BULLETIN CONFIGURATION LIST The following is a list of Service Bulletins that are applicable to the operation of the airplane, and have been incorporated into this supplement. This list contains only those Service Bulletins that are currently active. Number Title Airplane Serial

  • CESSNA SECTION 3 MODEL T182T NAV III EMERGENCY PROCEDURES GFC 700 AFCS U.S. ENGINE FAILURES (Continued) ENGINE FAILURE DURING FLIGHT (Restart Procedures) 1. Airspeed - 75 KIAS (best glide speed) 2. FUEL SELECTOR Valve - BOTH 3. FUEL PUMP Switch - ON 4. Mixture Control - RICH (if restart has not occurred) 5. MAGNETOS Switch - BOTH (or START if propeller is stopped) NOT

  • Cessna skylance tc T182T, CESSNA SECTION 1 MODEL T182T NAV III GENERAL GFC 700 AFCS U.S. INTRODUCTION This POH contains 9 sections, and includes the material required to be furnished to the pilot by 14 CFR 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 or explanations of symbols, abbreviations, and terminology commonly used. DESCRIPTIVE DATA ENGINE Number of Engines: 1 Engine Manufacturer: Textron Lycoming Engine Model Number: TIO-540-AK1A Engine Type: Turbocharged, direct drive, air-cooled, horizontally opposed, fuel injected, six

  • Cessna skylance tc T182T, CESSNA SECTION 4 MODEL T182T NAV III NORMAL PROCEDURES GFC 700 AFCS U.S. TAXIING (Continued) TAXIING DIAGRAM NOTE Strong quartering tail winds require caution. Avoid sudden bursts of the throttle and sharp braking when the airplane is in this attitude. Use the steerable nosewheel and rudder to maintain direction. Figure 4-2 T182TPHBUS-00 4-29

  • SECTION 3 CESSNA EMERGENCY PROCEDURES MODEL T182T NAV III GFC 700 AFCS U.S. EMERGENCY PROCEDURES Procedures in the Emergency Procedures Checklist portion of this section shown in bold faced type are immediate action items which should be committed to memory. ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF ROLL 1. Throttle Control - IDLE (pull full out) 2. Brakes - APPLY 3. Wing Flaps - RET

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