Cessna 177 Cardinal Скачать руководство пользователя страница 54 | Manualshive

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LOSS OF INDIVIDUAL DISPLAY ELEMENT

1. Continue normal engine operation by referring to the remaining parameters displayed.

1. Avoid high engine power settings and rapid power changes;
2. Enrichen Mixture to maintain smooth engine operation;
3. Arrange to terminate the flight safely and as soon as practicable.
4. Refer to your origional airplane AFM for possible additional engine instrument
failure information

EDM-900 EMERGENCY PROCEDURES

LOSS OF ALL DISPLAYS (Electrical Failure).

The RAL will indicate limits even if the display fails

and the rest of the unit is functional.

NOTE

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Содержание 177 Cardinal

Страница 1: ... MODEL 177 AND CARDINAL OWNER S MANUAL MORE PEOPLE BUY AND FLY CESSNA AIRPLANES THAN ANY OTHER MAKE WORLD S LARGEST PRODUCER OF GENERAL AVIATION AIRCRAFT SINCE 1956 Cessna N35031 As of 1 28 20 As of 1 30 20 ...

Страница 2: ...PERFORMANCE SPECIFICATIONS N35031 1 426 lbs 1 073 lbs N35031 ...

Страница 3: ...imum Flap Extension 10 Vfo2 130 Maximum Flap Extension 10 Va 117 Maneuvering Speed Gross Weight Vno 153 Maximum Structural Cruising Speed Vne 186 Never Exceed Speed 65 Lift Nose Wheel 92 Normal Climb Out 69 Short Field Takeoff Flaps 15 As of 1 15 20 C 177B Cardinal 2 500 lbs Take Off Speed Approach Speed Horton 47 mph Horton 50 mph Normal Operation 57 mph Normal Operation 55 mph Normal Cessna 65 m...

Страница 4: ...seful Load 773 lbs Payload with Full Fuel 11 gph Approximate Fuel Flow 50 gal Total Fuel Capacity 49 gal Total Useable Fuel 100LL Blue Fuel Octane Rating 8 qts Oil Sump Capacity 6 qts Minimum Usual Oil Quantity 180 HP Lycoming O 360 A1F6 12 v Battery 104 02 Empty C G 148 344 61 Empty C G Moment As of 1 15 20 ...

Страница 5: ...CONGRATULATIONS ...

Страница 6: ......

Страница 7: ...ERATING CHECKLIST DESCRIPTION AND OPERATING DETAILS EMERGENCY PROCEDURES OPERATING LIMITATIONS CARE OF THE AIRPLANE OPERATIONAL DATA OPTIONAL SYSTEMS SECTION I SECTION II SECTION III SECTION IV SECTION V SECTION VI SECTION VII ...

Страница 8: ...BY SMALL HOLES INSIDE FILLER NECK 22 Gallons N O T E To ensure desired fuel capacity when refueling place the fuel selector valve in either LEFT or RIGHT position to prevent cross feeding L A N D I N G G E A R NOSE WHEEL TIRE PRESSURE 35 PSI on 5 00 5 4 Ply Rated Tire 35 PSI on 6 00 6 4 Ply Rated Tire MAIN WHEEL TIRE PRESSURE 30 PSI on 6 00 6 6 Ply Rated Tires N O S E G E A R S H O C K S T R U T K...

Страница 9: ...ill to 8quarts These quantities refer to oil dipstick level readings During oil and oil filter changes one addi tional quart is required when the filter element is changed O I L A N D O I L F I L T E R C H A N G E After the first 25 hours of operation drain engine oil sump and oil cooler clean the oil suction strainer and change the oil filter element Refill sump with straight mineral oil non dete...

Страница 10: ...OPERATING CHECKLIST See APPENDIX 86 19 11 Preflight Fuel System Check ...

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Страница 13: ...SAMPLE 13 Main Wheel Tire CHECK 14 Fuel Vent Opening CHECK CLEAR PREFLIGHT EMPENNAGE 1 Antennas CHECK 2 Baggage Door CHECK SECURE 3 Stabilator CHECK 4 Trim Taps CHECK 5 Tail Tie Down DISCONNECT 6 Rudder CHECK PREFLIGHT RIGHT WING 1 Fuel Vent Opening CHECK CLEAR 2 Main Wheel Tire CHECK 3 Fuel Tank Sump SAMPLE 4 Flap Connection CHECK 5 Flap Guides CHECK 6 Aileron CHECK FREE 7 Aileron CHECK PUSH BAR ...

Страница 14: ...Mixture LEAN FOR TAXI 8 Parking Brake RELEASE 9 Brakes TEST 10 Flight Controls POSITIONED FOR WIND BEFORE TAKE OFF 1 Nose Wheel STRAIGHT 2 Parking Brake SET 3 Flight Controls FREE CORRECT 4 Fuel Shutoff Valve IN WIRED 5 Fuel Selector Valve ON BOTH 6 Mixture RICH below 3 000 7 Stabilator Trim TAKE OFF 8 Rudder Trim TAKE OFF 9 Primer IN LOCKED 10 Oil Temperature IN GREEN 11 Throttle Setting 1800 RPM...

Страница 15: ...nditions 2 Seatbelt Operations WEAR AT ALL TIMES 3 Headset Operation 4 What NOT TO TOUCH 5 Sterile Cockpit until after Takeoff 6 Sick Sacks 7 Ventilation 8 How to Radio for Help PTT Button on panel 9 Emergency Situations 10 Foreflight Passenger App on iPhone As of 1 15 20 ...

Страница 16: ... ANGLE 69 10 Flaps RETRACT 11 Power Prop 2500 RPM 25 12 Climb Speed BEST RATE 92 ENROUTE CLIMB 1 Landing Light OFF 2 Airspeed 90 to 100 3 Power 24 2500 2700 RPM 4 Mixture LEAN ABOVE 3 000 5 Cowl Flaps OPEN AS REQUIRED CRUISE 1 Power 75 OR LESS 2 Stabilator Trim ADJUST 3 Rudder Trim ADJUST 4 Mixture LEAN 5 Cowl Flaps ADJUST FOR 350 OR LESS DECENT 1 Fuel Selector Valve BOTH 2 Mixture RICH 3 Power AS...

Страница 17: ... LANDING 1 Wing Flaps UP 2 Carburetor Heat COLD CLEAR OF RUNWAY 1 Transponder STANDBY 2 Strobe Nav Landing Lights OFF PRIOR TO PARKING 1 Fuel TOP OFF 2 Purchase RECORD SECURING AIRCRAFT 1 Parking Brake SET 2 Tach Time RECORD FROM JPI 3 Radios Electrical Equipment OFF 4 Ignition Switch GROUND CHECK 5 Mixture IDLE CUT OFF 6 Ignition Switch OFF 7 Master Battery Switch s OFF 8 Control Lock INSTALL 9 F...

Страница 18: ... 100 ELECTRICAL FIRE DURING FLIGHT 1 Master Switch OFF 2 All other Switches except Ignition OFF 3 Vents Cabin Air Heat CLOSED 4 Fire Extinguisher ACTIVATE if fire appears out a Master Switch ON b Circuit Breakers CHECK Do NOT reset faulty circuit c Electrical Radios ON One at a time with delay after each EMERGENCY LANDING 1 Mixture IDLE CUT OFF 2 Fuel Selector Valve OFF 3 Fuel Shutoff Valve OUT Br...

Страница 19: ......

Страница 20: ...G DETAILS NOTE With full cabin loading with either standard or long range tanks it will be necessary to reduce the fuel load to keep the aircraft within approved weight limits Refer to Section IV for weight and balance control procedures ...

Страница 21: ......

Страница 22: ...ng the selector valve handle to the fuel tank in the heavy wing The recommended cruise fuel management procedure for extended flight is to use the left and right tank alternately With low fuel 1 16th tank or less a prolonged powered steep descent 1 000 or more should be avoided with more than 10 flaps to prevent the possibility of fuel starvation resulting from uncovering the fuel tank outlets If ...

Страница 23: ...ELECTRICAL SYSTEM MASTER SWITCH AMMETER OVER VOLTAGE SENSOR AND WARNING LIGHT ...

Страница 24: ...ELECTRICAL SYSTEM ...

Страница 25: ...LIGHTING EQUIPMENT CIRCUIT BREAKERS AND FUSES EXTERIOR LIGHTING ...

Страница 26: ...INTERIOR LIGHTING ...

Страница 27: ...CABIN HEATING VENTILATING AND DEFROSTING SYSTEM ...

Страница 28: ...SHOULDER HARNESSES ...

Страница 29: ...ximum shoulder harness comfort and safe retention of the seat occupants This location requires that the shoulder harnesses cross near the top so that the right hand inertia reel serves the pilot and the left hand reel serves the front passenger When fastening the harness check to ensure the proper harness is being used ...

Страница 30: ...TAXIING BEFORE TAKE OFF NOTE WARM UP Additional details concerning cold weather starting and operation may be found under Cold Weather Operation paragraphs in this seciton ...

Страница 31: ...TAXIING DIAGRAM ...

Страница 32: ...TAKE OFF MAGNETO CHECK ALTERNATOR CHECK POWER CHECK ...

Страница 33: ...WING FLAP SETTINGS PERFORMANCE CHARTS CROSSWIND TAKE OFFS ...

Страница 34: ... Operational D a t a i n S e c t i o n V I The Cruise Performance table shown on the following page iliustrates the time airspeed and miles per gallon during cruise for various altitudes and percent powers This table should be used as aguide along with the available winds aloft information to determine the most favorable altitude and power setting for agiven trip TJie selection of cruise altitude ...

Страница 35: ...CRUISE PERFORMANCE ...

Страница 36: ...LEANING WITH A CESSNA ECONOMY MIXTURE INDICATOR EGT ...

Страница 37: ...SPINS STALLS LANDING SHORT FIELD LANDINGS ...

Страница 38: ...N NOTE CROSSWIND LANDINGS BALKED LANDING STARTING When pulling the propeller through by hand treat it as if the ignition switch is turned on A loose or broken ground wire on either magneto could cause the engine to fire 2 1 ...

Страница 39: ...TE Use heavy strokes of primer for best atomization of fuel After priming push primer all the way in and turn to the locked position to avoid the possibility of the engine drawing fuel through the primer ...

Страница 40: ...his occurs maintain a cranking action to suck the flames the engine An outside attendant with a fire extinguisher is advised for cold starts without preheat If the engine does not start during the first few attempts or if engine firing diminishes in strength it is probable that the spark plugs have frosted over Preheat must be used before another start is attempted ...

Страница 41: ...nded procedures do not apply where they would conflict with Air Traffic Control clearances or instructions or where in the pilot s judgement an altitude of less than 2 000 feet is necessary for him ti adequately exercise his duty to see and avoid other aircraft ...

Страница 42: ...EMERGENCY PROCEDURES ENGINE FAILURE ENGINE FAILURE AFTER TAKE OFF ENGINE FAILURE AFTER DURING FLIGHT ...

Страница 43: ...FORCED LANDINGS PRECAUTIONARY LANDING WITH ENGINE POWER EMERGENCY LANDING WITHOUT POWER ...

Страница 44: ...FIRES DITCHING ENGINE FIRE DURING START ON GROUND ...

Страница 45: ...ENGINE FIRE IN FLIGHT ELECTRICAL FIRE IN FLIGHT ...

Страница 46: ...EXECUTING A 180 TURN IN CLOUDS EMERGENCY LET DOWNS THROUGH CLOUDS DISORIENTATION IN CLOUDS ...

Страница 47: ...he turn by using coordinated aileron and rudder control to align the symbolic airplane in the turn coordinator with the horizon r e f e r e n c e l i n e 3 Cautiously apply control wheel back pressure to slowly reduce the indicated airspeed to 90 MPH 4 Adjust the stabilator trim control to maintain a90 MPH glide 5 Keep hands off the control wheel using rudder control to hole astraight heading Adju...

Страница 48: ...ROUGH ENGINE OR LOSS OF POWER CARBURETOR ICING SPARK PLUG FOULING ...

Страница 49: ...ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS MAGNETO MALFUNCTION LOW OIL PRESSURE ...

Страница 50: ...INSUFFICIENT RATE OF CHARGE EXCESSIVE RATE OF CHARGE ...

Страница 51: ... 100 ELECTRICAL FIRE DURING FLIGHT 1 Master Switch OFF 2 All other Switches except Ignition OFF 3 Vents Cabin Air Heat CLOSED 4 Fire Extinguisher ACTIVATE if fire appears out a Master Switch ON b Circuit Breakers CHECK Do NOT reset faulty circuit c Electrical Radios ON One at a time with delay after each EMERGENCY LANDING 1 Mixture IDLE CUT OFF 2 Fuel Selector Valve OFF 3 Fuel Shutoff Valve OUT Br...

Страница 52: ... 100 ELECTRICAL FIRE DURING FLIGHT 1 Master Switch OFF 2 All other Switches except Ignition OFF 3 Vents Cabin Air Heat CLOSED 4 Fire Extinguisher ACTIVATE if fire appears out a Master Switch ON b Circuit Breakers CHECK Do NOT reset faulty circuit c Electrical Radios ON One at a time with delay after each EMERGENCY LANDING 1 Mixture IDLE CUT OFF 2 Fuel Selector Valve OFF 3 Fuel Shutoff Valve OUT Br...

Страница 53: ...H 4 Mixture RICH 5 Ignition Switch BOTH or START 6 Primer IN LOCKED 7 Airspeed 80 MPH EMERGENCY LANDING 1 Mixture IDLE CUT OFF 2 Fuel Selector Valve OFF 3 Select Field SUITABLE 4 Electrical Switches OFF 5 Wing Flaps on final 30 6 Airspeed 75 MPH 7 Master Battery Switch OFF 8 Doors UNLATCH PRIOR TO TOUCHDOWN 9 Touchdown SLIGHT TAIL LOW 10 Ignition OFF 11 Brakes APPLY HEAVILY PRECAUTIONARY LANDING 1...

Страница 54: ...ichen Mixture to maintain smooth engine operation 3 Arrange to terminate the flight safely and as soon as practicable 4 Refer to your origional airplane AFM for possible additional engine instrument failure information EDM 900 EMERGENCY PROCEDURES LOSS OF ALL DISPLAYS Electrical Failure The RAL will indicate limits even if the display fails and the rest of the unit is functional NOTE ...

Страница 55: ...ht side of the fuselage To gain access to the unit grasp the edge of the baggage wall and pull The ELT is operated by acontrol panel at the forward facing end of the unit see figure 3 1 E L T O P E R A T I O N 1 NORMAL OPERATION As long as the function selector switch remains in the ARM position the ELT automatically activates fol lowing an impact of 5gor more over ashort time period 2 ELT FAILURE...

Страница 56: ......

Страница 57: ...OPERATIONS AUTHORIZED MANEUVERS NORMAL CATEGORY OPERATING LIMITATIONS ...

Страница 58: ...MANEUVERS UTILITY CATEGORY ...

Страница 59: ...AIRSPEED LIMITATIONS CAS AIRSPEED INDICATOR MARKINGS ENGINE OPERATION LIMITATIONS ENGINE INSTRUMENT MARKINGS OIL TEMPERATURE GAGE CYLINDER HEAD TEMPERATURE GAGE ...

Страница 60: ...RESSURE GAGE FUEL QUANTITY INDICATORS TACHOMETER MANIFOLD PRESSURE GAGE CARBURETOR AIR TEMPERATURE GAGE optional The licensed empty weight and moment are recorded on the Weight and Balancer and Installed Equipment Data sheet or on revised weight and ...

Страница 61: ...d on the actual weight and c g arm fuselage station of the item being loaded must be made if the position of the load is different from that shown on the Loading Graph A reduced fuel weight may be measured for use with heavy cabin loadings by filling both tanks to the 22 gallon marker for 43 gallons 258 pounds usable Both tanks may be filled for maximum range provided gross weight is not exceeded ...

Страница 62: ...ny existing RPM MAP EGT CHG CDT TIT O T O P F P FF and Fuel Quantity indicators required by the aircraft type design B The EDM 930 cannot be used as primary if the RAD is not working C This Pilots Guide must be available to the pilot for all flight operations ...

Страница 63: ...LOADING ARRANGEMENTS STANDARD SEATING 2ND ROW SEAT REMOVED ...

Страница 64: ...1 426 148 3 33 0 294 0 450 0 41 7 10 0 2 0 2197 225 8 SAMPLE LOADING PROBLEM N35031 17 0 8 Weight lbs Moment lb ins 1000 ...

Страница 65: ... LOADING GRAPH ...

Страница 66: ... CENTER OF GRAVITY MOMENT ENVELOPE ...

Страница 67: ...GROUND HANDLING MOORING YOUR AIRPLANE CARE OF THE AIRPLANE ...

Страница 68: ...RFACES NOTE Never use gasoline benzine alcohol acetone carbon tetrachloride fire extinguisher or anti ice fluid lacquer thinner or glass cleaner to clean the plastic These materials will attack the plastic and may cause it to craze ...

Страница 69: ...ALUMINUM SURFACES PROPELLER CARE ...

Страница 70: ...INTERIOR CARE ...

Страница 71: ...MAA PLATE FINISH AND TRIM PLATE AIRCRAFT FILE ...

Страница 72: ...afety check that the ignition switch is OFF the throttle is closed the mixture control is in the idle cut off position and the airplane is secured before rotating the propeller by hand Do not stand within the arc of the propeller blades while turning the propeller ...

Страница 73: ...CESSNA PROGRESSIVE CARE CESSNA CUSTOMER CARE PROGRAM ...

Страница 74: ...SERVICING REQUIREMENTS ...

Страница 75: ...OWNER FOLLOW UP SYSTEM PUBLICATIONS ...

Страница 76: ...OPERATIONAL DATA ...

Страница 77: ......

Страница 78: ...2500 2200 1900 2500 2200 1900 ...

Страница 79: ... 2500 2400 2300 2200 2100 2 500 FEET ...

Страница 80: ... 2500 2400 2300 2200 2100 5 000 FEET ...

Страница 81: ... 2500 2400 2300 2200 2100 7 500 FEET ...

Страница 82: ... 2500 2400 2300 2200 2100 2600 2700 10 000 FEET ...

Страница 83: ... 2500 2400 2300 2200 2100 2600 2700 12 500 FEET ...

Страница 84: ...2500 Horton 540 Horton 50 ...

Страница 85: ...CLE OPTIONAL SYSTEMS COLD WEATHER EQUIPMENT Electrical power for the aircraft electrical circuits is provided through a split bus bar having all electronic circuits on one side of the bus and the other electrical circuits on the other side of NOTE ...

Страница 86: ...tomatically opens the circuit to the electronic portion of the split bus bar as a protection against damage to the transistors in the electronic equipment by transient voltages from the power source Therefore the external power source can not be used as a source of power when checking electronic components ...

Страница 87: ...should not be open when using the alternate static source M I C R O P H O N E H E A D S E T Amicrophone headset combination is offered as optional equipment Using the microphone headset and amicrophone keying switch on the left side of the pilot s control wheel the pilot can conduct radio communica tions without interrupting other control operations to handle ahand held microphone Also passengers ...

Страница 88: ...N35031 17702167 ...

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Страница 90: ......

Страница 91: ......

Страница 92: ......

Страница 93: ......

Страница 94: ...N35031 17702167 Cessna 177B ...

Страница 95: ...rt Murray ODA STC Unit Administrator Garmin International Inc ODA 240087 CE Date 05 01 2013 2 03 08 2016 All New supplement format with GTX 3X5 added Michael Warren Michael Warren ODA STC Unit Administrator Garmin International Inc ODA 240087 CE Date 03 08 2016 3 12 07 2017 All Updated SW versions and removed section 3 2 3 Updated section 2 2 Corrected PED FAR reference and additional minor correc...

Страница 96: ...ay with User Navigation Angle 12 2 4 Applicable System Software 13 2 5 Pressure Altitude Broadcast Inhibit PABI 13 2 6 Datalinked Weather Display GTX 345 Only 13 2 7 Portable Electronic Devices 13 Section 3 EMERGENCY PROCEDURES 14 3 1 Emergency Procedures 14 3 2 Abnormal Procedures 14 Section 4 NORMAL PROCEDURES 15 4 1 Unit Power On 15 4 2 Before Takeoff 16 Section 5 PERFORMANCE 16 Section 6 WEIGH...

Страница 97: ...ar or TCAS interrogations at 1030 MHz and transmitting a coded response of pulses to ground based radar on a frequency of 1090 MHz Each unit is equipped with IDENT capability to initiate the SPI special position identification pulse for 18 seconds and will reply to ATCRBS Mode A Mode C and Mode S All Call interrogation Interfaces to the GTX 33X are shown in the following block diagrams GTX 330 or ...

Страница 98: ...n of ADS B out data on 1090 extended squitter 1090 MHz o Integration of data from internal and external sources to transmit the following data per 14 CFR 91 227 GPS Position Altitude and Position Integrity Ground Track and or Heading Ground Speed and Velocity Integrity Air Ground Status Flight ID Call Sign ICAO Registration Number Capability and Status Information Transponder Squawk Codes between ...

Страница 99: ... x x x x FIS B x x x x Internal GPS x x x x Bluetooth x x x x Optional Garmin Altitude Encoder x x x x x x x x Table 1 GTX 3X5 Unit Configurations Interfaces to the GTX 3X5 are shown in Figure 3 TAS TCAS I Traffic Sensor ADS B Traffic FIS B Display Bluetooth Device GTX 3X5 GPS Antenna External GPS Source Audio Panel Bottom Antenna GTX 3X5 with GPS only OR GTX 335R 345R Control Power Ground Altitud...

Страница 100: ... Pressure Altitude Broadcast Inhibit The GTX 335 performs the following additional functions x Reception of TIS A traffic data from a ground station x Provide TIS A traffic alerting to the pilot via interfaced display and audio output The GTX 345 performs the following additional functions x Reception of ADS B In data on 1090 MHz o ADS B Data directly from another transmitting aircraft o ADS R Reb...

Страница 101: ... Graphical and textual weather products NEXRAD PIREPs AIRMET SIGMETs METARs TAFs Winds Aloft o Aviation Data TFRs NOTAMs 1 3 Capabilities The Garmin GTX 33X and GTX 3X5 as installed in this aircraft have been shown to meet the equipment requirements of 14 CFR 91 227 when operating in accordance with sections 2 1 and 2 2 of this supplement 1 4 Installation Configuration This aircraft is equipped wi...

Страница 102: ...TX 335R GTX 345 GTX 345R Interfaced GPS SBAS Position Source s GPS 1 GPS 2 if installed Internal Internal GTN 6XX 7XX Series GTN 6XX 7XX Series GNS 400W 500W Series GNS 400W 500W Series GNS 480 GNS 480 GIA 63W GDL 88 GTX 330 only GIA 63W GDL 88 GTX 330 only Interfaced Pressure Altitude Source Pressure Altitude Source 1 _____________________ Garmin Altitude Encoder Pressure Altitude Source 2 if ins...

Страница 103: ...ontroller Transponder 2 Remote Control Display if installed GTN 6XX 7XX GNS 480 G950 1000 Display Gables 7534 Controller Interfaced Active Traffic System None TCAD TAS TCAS NOTE If the system includes all of the following components x GTX 345R x G950 1000 Display and x TCAD or TAS TCAS Then the aircraft is no longer equipped with a TSO compliant active TCAD TAS or TCAS system Any operational requi...

Страница 104: ...adar Beacon System CFR Code of Federal Regulations ES Extended Squitter GNSS Global Navigation Satellite System GNS Garmin Navigation System GPS Global Positioning System GTX Garmin Transponder GTN Garmin Touchscreen Navigator ICAO International Civil Aviation Organization LRU Line Replaceable Unit PABI Pressure Altitude Broadcast Inhibit POH Pilot Operating Handbook SBAS Satellite Based Augmentat...

Страница 105: ... 2 Required Equipment 2 2 ADS B Out The GTX 33X and GTX 3X5 only comply with 14 CFR 91 227 for ADS B Out when all required functions are operational When the system is not operational ADS B Out transmit failure messages will be present on the remote control display interface or the GTX 330 or GTX 3X5 panel display If a Gables 7534 controller is being used the ADS B equipment failure condition will...

Страница 106: ...mpliant transmitter PABI is enabled by selecting the GTX to ON mode 2 6 Datalinked Weather Display GTX 345 Only Do not use datalink weather information for maneuvering in near or around areas of hazardous weather Information provided by datalink weather products may not accurately depict current weather conditions Do not use the indicated datalink weather product age to determine the age of the we...

Страница 107: ...ed aircraft for loss of power generation 3 2 2 LOSS OF GPS SBAS POSITION DATA When the GPS SBAS receiver is inoperative or GPS position information is not available or invalid the GTX will no longer be transmitting ADS B Out data For GTX 330 installations NO ADSB annunciator illuminated Interfaced GPS position sources VERIFY VALID POSITION For GTX 3X5 installations NO 1090ES TX annunciator illumin...

Страница 108: ...transponders thereby providing a single point of entry for Mode 3 A code Flight ID IDENT functionality and activating or deactivating emergency status for both transponder and ADS B Out functions Details on performing these procedures are located in the GTX 330 330D P G GTX 3X5 S T P G 4 1 Unit Power On For GTX 330 installations GTX Mode VERIFY ALT NO ADSB CONSIDERED For GTX 3X5 installations GTX ...

Страница 109: ...X EXTINGUISHED NOTE The ADS B TX or 1090ES TX CTL must be turned on and the NO ADS B or NO 1090ES TX Annunciation or associated display annunciations must be EXTINGUISHED for the system to meet the requirements specified in 14 CFR 91 227 This system must be operational in certain airspaces after January 1 2020 as specified by 14 CFR 91 225 Section 5 PERFORMANCE No change Section 6 WEIGHT AND BALAN...

Страница 110: ...3X5R Title Part Number Revision Garmin GTN 725 750 P G 190 01007 03 Rev E or later Garmin GTN 625 635 650 P G 190 01004 03 Rev E or later GNS 480 P G 190 00502 00 Rev D or later GTX 3X5 Series T G1000 P Guide 190 01499 01 Rev A or later 7 1 GTX TIS Behavior The TIS Standby Operate controls for GTX 33 330 and GTX 335 units only function when the aircraft is airborne 7 2 GTX 345R and G950 1000 No Be...

Страница 111: ......

Страница 112: ...w 3 Repeat Steps 1 and 2 on each wing tank quick drain 4 If the airplane has been exposed to rain sleet or snow or if the wing fuel tanks or fuel strainer drains produce water the fuel reservoir s must be checked for the presence of water by operating the fuel reservoir quick drains The airplane fuel system must be purged to the extent necessary to insure that there is no water ice or other fuel c...

Страница 113: ... data 2 15 enroute 1 5 2 15 maximum performance 1 6 m a x i m u m r a t e o f c l i m b data chart 6 3 normal 1 5 speeds 2 15 Cold Weather Equipment 7 1 ground service plug receptacle 7 1 static pressure alternate source valve 7 2 winterization kit 7 1 Cold Weather Operation 2 20 flight operations 2 22 starting 2 20 Correction Table Airspeed 6 2 Crosswind Landings 2 19 Crosswind Take Off 2 14 Crui...

Страница 114: ...imb 2 15 maximum performance 1 6 n o r m a l 1 5 Equipment Cold Weather 7 1 E x c e s s i v e R a t e o f E l e c t r i c a l Charge 3 9 Executing 180 Turn in Clouds E 3 5 Economy Mixture Indicator 7 7 operating instructions 2 17 Electrical Power Supply System Malfunctions 3 8 excessive rate of charge 3 9 insufficient rate of charge 3 9 Electrical System 2 4 a m m e t e r 2 4 circuit breakers and ...

Страница 115: ...ghting 2 6 interior lighting 2 7 Limitations Airspeed 4 3 Limitations Engine Operation G Graph Loading 4 9 Gross Weight inside front cover Ground Handling 5 1 Ground Service Plug Receptacle 7 1 H Handling Airplane on Ground 5 1 rnesses Shoulder 2 9 jadset Microphone 7 3 Heating Ventilating and Defrosting System Cabin 2 8 Hot Weather Operation 2 22 4 3 I Loading Arrangements Diagram 4 7 Indicator E...

Страница 116: ...ooring Your Airplane 5 1 N Noise Abatement 2 22 Normal Category Maneuvers 4 1 Normal Climb 1 5 Normal Landing 1 7 Normal Take OH 1 5 Nose Gear Shock Strut inside back Q Quick Drain Valve Oil 7 7 Quick Drain Valves Fuel 2 3 c r o R Oil System capacity inside back cover oil filter change inside back c o v e r oil grade inside back cover pressure gage 4 4 quick drain valve 7 7 temperature gage 4 3 Op...

Страница 117: ...Reel 2 10 Spark Plug Fouling 3 7 Speaker Phone Switches 7 5 Spins 2 18 Stalls 2 18 speed chart 6 2 Starting Engine 1 4 2 10 2 20 Static Pressure Alternate Source Valve 7 2 Storage Flyable 5 6 Surfaces aluminum 5 3 painted 5 2 True Airspeed Indicator 7 6 u utility Category Maneuvers 4 2 w Warm Up 2 11 Weight empty inside front cover gross inside front cover Weight and Balance 4 4 baggage and cargo ...

Страница 118: ...CESSNA AIRCRAFT COMPANY WICHITA KANSAS TAKE YOUR CESSNA HOME FOR SERVICE AT THE SIGN OF THE CESSNA SHIELD ...

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