Cessna 1980 172RG Cutlass Скачать руководство пользователя страница 64 | Manualshive

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CESSNA

SECTION 6

MODEL 172RG

WEIGHT & BALANCE/

EQUIPMENT LIST

EQUIPMENT LIST

The following equipment list is a comprehensive list of all Cessna equipment

available for this airplane. A separate equipment list of items installed in your
specific airplane is provided in your aircraft file. The following list and the specific

list for your airplane have a similar order of listing.

This equipment list provides the following information:

An

item number

gives the identification number for the item. Each number is

prefixed with a letter which identifies the

descriptive

grouping (exam-

ple:

A. Powerplant & Accessories) under which it is listed. Suffix letters

identify the equipment as a required item, a standard item or an optional
item. Suffix letters are as follows:

-R = required items of equipment for FAA certification

-S = standard equipment items
-

0= optional equipment items replacing required or standard

items

- A = optional equipment items which are in addition to

required or standard items

A reference drawing

column provides the drawing number for the item.

NOTE

If additional equipment is to be installed, it must be done in
accordance with the reference drawing, accessory kit instruc-
tions, or a separate FAA approval.

Columns showing

weight (in pounds)

and

arm (in inches)

provide the weight

and center of gravity location for the equipment.

NOTE

Unless otherwise indicated, true values (not net change

values) for the weight and arm are shown. Positive arms are
distances aft of the airplane datum; negative arms are distan-
ces forward of the datum.

NOTE

Asterisks (*) after the item weight and arm indicate complete

11

assembly installations. Some major components of the assem-
bly are listed on the lines immediately following. The summa-
tion of these major components does not necessarily equal the

complete assembly installation.

1 July 1979

6-15

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Содержание 1980 172RG Cutlass

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Страница 5: ...alers worldwide Specific benefits and provisions of warranty plus other important benefits for you are contained in your Customer Care Program book supplied with your airplane Warranty service is avai...

Страница 6: ...e examined immediately upon receipt and incorporated in this handbook NOTE It is the responsibility of the owner to maintain this handbook in a current status when it is being used for operational pur...

Страница 7: ...ENERAL 1 LI MITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT BALANCE EQUIPMENT LIST 6 AIRPLANE SYSTEMS DESCRIPTIONS 7 AIRPLANE HANDLING SERVICE MAINTENANCE 8 SUPPLEMENTS Opt...

Страница 8: ...ed Weights 1 4 Standard Airplane Weights 1 5 Cabin And Entry Dimensions 1 5 Baggage Space And Entry Dimensions 1 5 Specific Loadings 1 5 Symbols Abbreviations And Terminology 1 6 General Airspeed Term...

Страница 9: ...equipped four cylinder engine with 361 cu in displacement Horsepower Rating and Engine Speed 180 rated BHP at 2700 RPM PROPELLER Propeller Manufacturer McCauley Accessory Division Propeller Model Numb...

Страница 10: ...SAE 40 18 C 0 F to 21 C 70 F use SAE 30 Below 12 C 10 F use SAE 20 MIL L 22851 Ashless Dispersant Oil All temperatures use SAE 20W 50 or Above 16 C 60 F use SAE 40 or SAE 50 1 C 30 F to 32 C 90 F use...

Страница 11: ...nding configu ration at the most forward center of gravity CESSNA SECTION 1 MODEL 172RG GENERAL Vx Best Angle of Climb Speed is the speed which results in the greatest gain of altitude in a given hori...

Страница 12: ...C G Center of Gravity Arm is the arm obtained by adding the Arm airplane s individual moments and dividing the sum by the total weight C G Center of Gravity Limits are the extreme center of gravity L...

Страница 13: ...4 Airspeed Indicator Markings 2 4 Power Plant Limitations 2 5 Power Plant Instrument Markings 2 6 Weight Limits 2 6 Center Of Gravity Limits 2 7 Maneuver Limits 2 7 Flight Load Factor Limits 2 7 Kinds...

Страница 14: ...tandard equipment The limitations included in this section and in Section 9 have been approved by the Federal Aviation Administration Observance of these operating limitations is required by Federal A...

Страница 15: ...ance are shown in figure 2 2 2 4 1 July 1979 CESSNA SECTION 2 MODEL 172RG LIMITATIONS MARKING KIAS VALUE OR RANGE SIGNIFICANCE White Arc 42 100 Full Flap Operating Range Lower limit is maximum weight...

Страница 16: ...ECTION 2 MODEL 172RG LIMITATIONS Baggage Area 2 Station 108 to 124 50 lbs See note below NOTE The maximum combined weight capacity for baggage areas 1 and 2 is 200 lbs CENTER OF GRAVITY LIMITS Center...

Страница 17: ...empty red line cannot be safely used in flight Approved Fuel Grades and Colors 100LL Grade Aviation Fuel Blue 100 Formerly 100 130 Grade Aviation Fuel Green OTHER LIMITATIONS FLAP LIMITATIONS Approve...

Страница 18: ...so me chanical detent at 10 10 to 30 White color code and 100 kt callout also mechanical detent at 10 and 20 7 Forward of fuel tank filler cap FUEL 100LL 100 MIN GRADE AVIATION GASOLINE CAP 33 0 U S G...

Страница 19: ...Engine Fire In Flight 3 6 Electrical Fire In Flight 3 6 Cabin Fire 3 7 Wing Fire 3 7 Icing 3 7 Inadvertent Icing Encounter 3 7 Static Source Blockage Erroneous Instrument Reading Suspected 3 8 Landing...

Страница 20: ...dures for coping with emergencies that may occur Emergencies caused by airplane or engine malfunctions are extremely rare if proper preflight inspections and maintenance are practiced Enroute weather...

Страница 21: ...rrain is rough or soft 6 Wing Flaps 30 on final approach 7 Airspeed 65 KIAS 3 4 1 July 1979 CESSNA SECTION 3 MODEL 172RG EMERGENCY PROCEDURES 8 Doors UNLATCH PRIOR TO TOUCHDOWN 9 Avionics Power and Ma...

Страница 22: ...cs Power Switch ON 10 Radio Electrical Switches ON one at a time with delay after each until short circuit is localized 3 6 1 July 1979 CESSNA SECTION 3 MODEL 172RG EMERGENCY PROCEDURES 11 Vents Cabin...

Страница 23: ...ver DOWN 3 Landing Gear and Gear Pump Circuit Breakers IN 4 Emergency Hand Pump EXTEND HANDLE and PUMP perpen dicular to handle until resistance becomes heavy about 35 cycles 5 Gear Down Light ON 6 Pu...

Страница 24: ...ator OFF 8 Nonessential Radio and Electrical Equipment OFF 9 Flight TERMINATE as soon as practical 3 10 1 July 1979 CESSNA SECTION 3 MODEL 172RG EMERGENCY PROCEDURES AMPLIFIED PROCEDURES ENGINE FAILUR...

Страница 25: ...procedure execute a forced landing Do not attempt to restart the engine 3 12 1 July 1979 CESSNA SECTION 3 MODEL 172RG EMERGENCY PROCEDURES The initial indication of an electrical fire is usually the...

Страница 26: ...cape icing conditions 3 14 1 July 1979 CESSNA SECTION 3 MODEL 172RG EMERGENCY PROCEDURES STATIC SOURCE BLOCKED If erroneous readings of the static source instruments airspeed altimeter and vertical sp...

Страница 27: ...SECTION 3 MODEL 172RG EMERGENCY PROCEDURES LOW OIL PRESSURE If low oil pressure is accompanied by normal oil temperature there is a possibility the oil pressure gage or relief valve is malfunctioning...

Страница 28: ...TE OF CHARGE After engine starting and heavy electrical usage at low engine speeds such as extended taxiing the battery condition will be low enough to accept above normal charging during the initial...

Страница 29: ...Wing 4 5 Nose 4 6 Left Wing 4 6 Left Wing Leading Edge 4 6 Left Wing Trailing Edge 4 6 Before Starting Engine 4 7 Starting Engine 4 7 Before Takeoff 4 7 Takeoff 4 8 Normal Takeoff 4 8 Short Field Take...

Страница 30: ...optional systems can be found in Section 9 SPEEDS FOR NORMAL OPERATION Unless otherwise noted the following speeds are based on a maximum weight of 2650 pounds and may be used for any lesser weight Ho...

Страница 31: ...OVE 4 Ignition Switch OFF 5 Avionics Power Switch OFF 6 Master Switch ON WARNINGI When turning on the master switch using an external power source or pulling the propeller through by hand treat the pr...

Страница 32: ...uel grade 3 Fuel Quantity CHECK VISUALLY for desired level 4 Fuel Filler Cap SECURE 7 LEFT WING Leading Edge 1 Pitot Tube Cover REMOVE and check opening for stoppage 2 Fuel Tank Vent Opening CHECK for...

Страница 33: ...2 seconds to restore hydraulic pressure 5 Climb Speed 70 80 KIAS 6 Brakes APPLY momentarily when airborne 7 Landing Gear RETRACT in climb out 4 8 1 July 1979 CESSNA SECTION 4 MODEL 172RG NORMAL PROCED...

Страница 34: ...wn MAIN WHEELS FIRST 6 Landing Roll LOWER NOSE WHEEL GENTLY 7 Braking MINIMUM REQUIRED SHORT FIELD LANDING 1 Airspeed 65 75 KIAS flaps UP 2 Wing Flaps 30 below 100 KIAS 3 Airspeed MAINTAIN 63 KIAS 4 T...

Страница 35: ...crank the engine through several revolutions with the starter Repeat the starting proce dure without any additional priming If the engine is underprimed most likely in cold weather with a cold engine...

Страница 36: ...ion RPM drop should not exceed 150 RPM on either magneto or show greater than 50 RPM differen tial between magnetos If there is a doubt concerning operation of the ignition system RPM checks at higher...

Страница 37: ...landing gear swings downward approximately two feet as it starts the retraction cycle damage can result by retracting it before obtaining at least that much ground clearance 4 16 1 July 1979 CESSNA SE...

Страница 38: ...6 127 14 6 116 15 3 9000 140 14 0 130 14 9 118 15 6 Standard Conditions Zero Wind Figure 4 3 Cruise Performance Table 4 18 1 July 1979 CESSNA SECTION 4 MODEL 172RG NORMAL PROCEDURES For best fuel econ...

Страница 39: ...n 63 KIAS and flare to land on the main wheels first Immediately after touchdown lower the nose gear to the ground and apply heavy braking as required For maximum brake 4 20 1 July 1979 CESSNA SECTION...

Страница 40: ...ause raw fuel to accumulate in the intake manifold creating a fire hazard in the event of a backfire If this occurs maintain a cranking action to suck flames into the engine An outside attendant with...

Страница 41: ...permitting even though flight at a lower level may be consistent with the provisions of government regulations 2 During departure from or approach to an airport climb after takeoff and descent for lan...

Страница 42: ...lanning of flights in detail and with reasonable accuracy The data in the charts has been computed from actual flight tests with the airplane and engine in good condition and using average piloting te...

Страница 43: ...the cruise perfor mance characteristics presented in figure 5 7 the range profile chart presented in figure 5 8 and the endurance profile chart presented in figure 5 9 The relationship between power a...

Страница 44: ...nd the corresponding fuel required to complete the trip with ample reserve 5 6 1 July 1979 CESSNA SECTION 5 MODEL 172RG PERFORMANCE LANDING A procedure similar to takeoff should be used for estimating...

Страница 45: ...d for level flight or maximum power during descent CESSNA SECTION 5 MODEL 172RG PERFORMANCE AIRSPEED CALIBRATION ALTERNATE STATIC SOURCE HEATER AND DEFROSTER FULL ON AND WINDOWS CLOSED Figure 5 1 Airs...

Страница 46: ...1 July 1979 CESSNA SECTION 5 MODEL 172RG PERFORMANCE STALL SPEEDS CONDITIONS Power Off Gear Up or Down NOTES Maximum altitude loss during a stall recovery may be as much as 230 feet KIAS values are a...

Страница 47: ...ixture should be leaned to give maximum power in a full throttle static runup 3 Decrease distances 10 for each 9 knots headwind For operation with tailwinds up to 10 knots increase distances by 10 for...

Страница 48: ...F CLIMB CONDITIONS Flaps Up Gear Up 2700 RPM Full Throttle Mixture Leaned above 3000 Feet Cowl Flaps Open Standard Temperature NOTES 1 Add 1 4 gallons of fuel for engine start taxi and takeoff allowan...

Страница 49: ...distance by 10 for each 10 C above standard temperature 3 Distances shown are based on zero wind Figure 5 6 Time Fuel and Distance to Climb Sheet 2 of 2 5 16 1 July 1979 CESSNA SECTION 5 MODEL 172RG P...

Страница 50: ...economy operate at the leanest mixture that results in smooth en g ine operation or at peak EGT if an EGT indicator is installed CONDITIONS 2650 Pounds Recommended Lean Mixture Cowl Flaps Closed NOTE...

Страница 51: ...G PERFORMANCE CRUISE PERFORMANCE PRESSURE ALTITUDE 10 000 FEET NOTE For best fuel economy operate at the leanest mixture that results in smooth engine operation or at peak EGT if an EGT indicator is i...

Страница 52: ...chart allows for the fuel used for engine start taxi takeoff and climb and the distance during a normal climb up to 8000 feet and maximum climb above 8000 feet NOTE For best fuel economy operate at th...

Страница 53: ...limb up to 8000 feet and maximum climb above 8000 feet CESSNA SECTION 5 DEL 172RG PERFORMANCE ENDURANCE PROFILE 45 MINUTES RESERVE 44 GALLONS USABLE FUEL CONDITIONS i0 Pounds Recommended Lean Mixture...

Страница 54: ...NOTES 1 Short field technique as specified in Section 4 2 Decrease distances 10 for each 9 knots headwind For operation with tailwinds up to 10 knots increase distances by 10 for each 2 knots 3 For op...

Страница 55: ...IGHT BALANCE EQUIPMENT LIST SECTION 6 WEIGHT BALANCE EQUIPMENT LIST TABLE OF CONTENTS Page Introduction 6 3 Airplane Weighing Procedures 6 3 Weight And Balance 6 6 Baggage Tie Down 6 6 Equipment List...

Страница 56: ...il sump drain plug to drain all oil d Move sliding seats to the most forward position e Raise flaps to the fully retracted position f Place all control surfaces in neutral position 2 Leveling a Place...

Страница 57: ...heel R Nose Wheel N Sum of Net Weights As Weighed W Item Moment 1000 Weight Lbs X C G Arm In Lbs In Airplane Weight From Item 5 Page 6 3 Airplane Oil 9 Qts at 7 5 Lbs Gal 16 9 16 1 0 3 Add Unusable Fu...

Страница 58: ......

Страница 59: ...list these on the loading problem NOTE Loading Graph information for the pilot passengers and baggage is based on seats positioned for average occu pants and baggage loaded in the center of the baggag...

Страница 60: ...low the aft window near each sidewall approxi mately at station 108 When the cabin floor baggage area 1 only is utilized for baggage the two floor mounted eyebolts and the two eyebolts on the forward...

Страница 61: ...eses indicate forward and aft limits of occupant center of gravity range Arm measured to the center of the areas shown NOTES 1 The usable fuel C G arm is located at station 48 0 2 The rear cabin wall...

Страница 62: ...epresenting adjustable seats shows the pilot or passenger center of gravity on adjustable seats positioned for an average occupant Refer to the Loading Arrangements diagram for forward and aft limits...

Страница 63: ...Figure 6 7 Center of Gravity Moment Envelope Figure 6 8 Center of Gravity Limits...

Страница 64: ...ndard equipment items 0 optional equipment items replacing required or standard items A optional equipment items which are in addition to required or standard items A reference drawing column provides...

Страница 65: ...4 1 2 12 99 15 588 King NAV COM KX 155 5 5 13 2 72 6 King NAV Indicator KI 204 1 7 14 0 23 8 Antenna Coupler 0 15 10 1 1 52 SCHALLDAEMPFER LIESE FLIGHT 3 93 6 9 BASIC EMPTY WEIGHT 1623 51 38 46 62452...

Страница 66: ...61 HEATING SYSTEM STALL WARNING PITOT EXCH 6 24 4 15 INDICATOR TRUE AIRSPEED EXCH 1 18 1 2 LIGHT BEACON OMNI FLASH 1 4 204 7 287 LIGHTS COURTESY 5 61 0 31 LOCATOR BEACON 3 5 116 5 408 STATIC SOURCE AL...

Страница 67: ...C07 A GROUND SERVICE PLUG RECEPTACLE 2401005 2 7 126 0 C16 0 HEATED PITOT SYSTEM NET CHANGE 0422355 7 0 6 24 4 622 A LIGHTS INSTRUMENT POST REQUIRES E34 D 2413120 0 5 17 3 C25 A LIGHT INSTALLATION CO...

Страница 68: ...2 0 82 0 23 S BELT SHOULDER HARNESS ASSY CO PILOT S 2215 3 1 6 37 0 E21 S SEAT BELT ASSEMBLY REAR SET OF TWO S 1146 13 2 0 10 0 E27 0 BELT SHOULDER HARNESS ASSY 2ND ROW 2 S 2215 8 3 2 10 0 E33 0 CARPE...

Страница 69: ...SCRIPTION REF DRAWING WT LBS ARM INS REMOTE RECEIVER SHELF INSTALLATION 3940266 1 1 0 134 6 H08 A 1 AUTO RADIAL CENTERING INDICATOR ARC LOC EXCHANGE FOR VOR LOC INDICATOR IN ITEM H22 A AND H25 A WT NE...

Страница 70: ...VO IS 3 9 LBS AT SHOWN SPLITTER 68 9 INCHES PA 495 MISC WIRING A HARDWARE ITEMS BASIC AVIONICS KIT INSTALLATION RADIO COOLING NOISE FILTER INSTALLATION COM ANTENNA CABLE LH VHF OMNI ANTENNA CABLE OMNI...

Страница 71: ...Hand Pump 7 12 Landing Gear Warning System 7 13 Baggage Compartment 7 13 Seats 7 13 Seat Belts And Shoulder Harnesses 7 14 Seat Belts 7 14 Shoulder Harnesses 7 15 Integrated Seat Belt Shoulder Harnes...

Страница 72: ...and rear carry through spars to which the wings are attached a bulkhead with attaching plates at the base of the forward doorposts for the lower attachment of the wing struts and the orgings and stru...

Страница 73: ...ESSNA SECTION 7 MODEL 172RG AIRPLANE SYSTEMS DESCRIPTIONS AILERON CONTROL SYSTEM RUDDER AND RUDDER TRIM CONTROL SYSTEMS Figure 7 1 Flight Control and Trim Systems Sheet 1 of 2 7 4 1 July 1979 Figure 7...

Страница 74: ...ir Temperature Gage 21 Suction Gage 22 Flight Hour Recorder 23 ADF Radio 24 Map Compartment 25 Cabin Heat Control 26 Cabin Air Control 27 Cigar Lighter 28 Wing Flap Switch and Position Indicator 29 Mi...

Страница 75: ...ltimeter are located to the left and right of the gyros respectively The remaining flight instruments are located around the basic T The fuel pressure gage clock fuel quantity indicators ammeter oil p...

Страница 76: ...gear shock strut Each main gear wheel is equipped with a hydraulically actuated single disc brake on the inboard side of each wheel The landing gear extension retraction and main gear down lock releas...

Страница 77: ...th the hand pump To utilize the pump extend the handle forward and pump vertically For complete emergency procedures refer to Section 3 7 12 1 July 1979 CESSNA SECTION 7 MODEL 172RG AIRPLANE SYSTEMS D...

Страница 78: ...d right sides of the seat bottom and the buckles at the center of the seat bottom 7 14 1 July 1979 CESSNA SECTION 7 MODEL 172RG AIRPLANE SYSTEMS DESCRIPTIONS To use the seat belts for the front seats...

Страница 79: ...est The inside door handle has three positions and a placard at its base which reads OPEN CLOSE and LOCK The handle is spring loaded to the CLOSE up position When the door has been pulled shut and lat...

Страница 80: ...mference and is equipped with a lock 7 18 1 July 1979 CESSNA SECTION 7 MODEL 172RG AIRPLANE SYSTEMS DESCRIPTIONS button in the end of the knob The rich position is full forward and full aft is the idl...

Страница 81: ...to various engine parts for lubrication Residual oil is returned to the sump by gravity flow An oil filler cap oil dipstick is located at the rear of the engine on the 7 20 1 July 1979 CESSNA SECTION...

Страница 82: ...f the cowling The cowl flaps are mechanically operated from the cabin by means of a cowl flap lever on the right side of the control pedestal The pedestal is labeled OPEN COWL FLAPS CLOSED Before star...

Страница 83: ...line equipped with a check valve which protrudes from the bottom surface of the left wing near the wing strut The right fuel tank filler cap is also vented Fuel quantity is measured by two float type...

Страница 84: ...r drain under an access panel on the right side of the engine cowling The fuel tanks should be filled after each flight to prevent condensation HYDRAULIC SYSTEM Hydraulic power see figure 7 7 is suppl...

Страница 85: ...brakes with heavy pressure If the brakes become spongy or pedal travel increases pumping the pedals should build braking pressure If one brake becomes weak or fails use the other brake sparingly whil...

Страница 86: ...ion With the switch in the OFF position no electrical power will be applied to the avionics equipment regardless of the position of the master switch or the individual equipment switches The avionics...

Страница 87: ...are not protected by circuit breakers are the battery contactor closing external power circuit clock circuit and flight hour recorder circuit These circuits are protected by fuses mounted adjacent to...

Страница 88: ...re is a burned out bulb however in the event any of the lighting systems fail to illuminate when turned on check the appropriate circuit breaker If the circuit breaker has opened white button popped o...

Страница 89: ...ure line going to the standard external static pressure source the alternate static source valve should be pulled on Pressures within the cabin will vary with heater vents opened or closed and windows...

Страница 90: ...attitude indicator is available and gives a visual indication of flight attitude Bank attitude is presented by a pointer at the top of the indicator relative to the bank scale which has index marks at...

Страница 91: ...nd sensor unit in the wing leading edge is equipped with a heating element The heated part of the system is operated by the PITOT HT switch and is protected by the PITOT HT circuit breaker The stall w...

Страница 92: ...from the navigation receivers of the 7 42 1 July 1979 CESSNA SECTION 7 MODEL 172RG AIRPLANE SYSTEMS DESCRIPTIONS NAV COM radios only Communication receiver audio is selected by the switches labeled C...

Страница 93: ...transmitting 7 44 1 July 1979 CESSNA SECTION 7 MODEL 172RG AIRPLANE SYSTEMS DESCRIPTIONS When the airplane has one or two transmitters sidetone is provided in both the speaker and headset anytime the...

Страница 94: ...sult in loss of usable radio signals on all communications and navigation radio equipment Usually the ADF is first to be affected and VHF communication equipment is the last to be affected Installatio...

Страница 95: ...Cessna Dealer and take advantage of his knowledge and experience He knows your airplane and how to maintain it He will remind you when lubrications and oil changes are necessary and about other season...

Страница 96: ...A SECTION 8 MODEL 172RG HANDLING SERVICE MAINTENANCE A To be displayed in the airplane at all times 1 Aircraft Airworthiness Certificate FAA Form 8100 2 2 Aircraft Registration Certificate FAA Form 80...

Страница 97: ...NTY plus other important benefits for you are contained in your CUSTOMER CARE P ROGRAM book supplied with your airplane You will want to thoroughly review your Customer Care Program book and keep it i...

Страница 98: ...ssing down on a tailcone bulkhead just forward of the horizontal stabilizer and allowing the tail to rest on the tail tie down ring h 8 8 1 July 1979 CESSNA SECTION 8 MODEL 172RG HANDLING SERVICE MAIN...

Страница 99: ...CESSNA SECTION 8 HANDLING SERVICE MAINTENANCE 1 C 30 F to 32 C 90 F use SAE 40 18 C 0 F to 21 C 70 F use SAE 30 Below 12 C 10 F use SAE 20 MIL L 22851 Ashless Dispersant Oil This oil must be used afte...

Страница 100: ...in areas of the world and consequently must be dealt with when encountered Therefore to alleviate the possibility of fuel icing occurring under these unusual conditions it is permissible to add isopro...

Страница 101: ...rub with moderate pressure until all dirt oil scum and bug stains are removed Allow the cleaner to dry then wipe it off with soft flannel cloths If a windshield cleaner is not available the plastic ca...

Страница 102: ...ear ENGINE CARE The engine may be cleaned with Stoddard solvent or equivalent then dried thoroughly CAUTION Particular care should be given to electrical equipment 8 16 1 July 1979 CESSNA SECTION 8 MO...

Страница 103: ...s 9 HF Transceiver Type PT10 A 4 pages 10 SSB HF Transceiver Type ASB 125 4 pages 11 200A Navomatic Autopilot Type AF 295B 6 pages 12 300 ADF Type R 546E 6 pages 13 300 Nav Com Type RT 385A 8 pages 14...

Страница 104: ...n Section 7 Limitations contained in the following supplements are FAA approved Observance of these operating limitations is required by Federal Aviation Regulations 9 2 1 July 1979 1 PILOT S OPERATIN...

Страница 105: ...ch will display to the pilot the time of day the calendar date and the elapsed time interval between a series of selected events such as in flight check points or legs of a cross country flight etc Th...

Страница 106: ...by changing the position of an internal slide switch accessible through a small hole on the bottom of the instrument case Notice that in the 24 hour format the clock mode indicator does not appear 2 1...

Страница 107: ...lon blinks off for one second each ten seconds To stop timing the event press the RH button once again and the time shown by the display is frozen Successive pushes of the RH button will alternately r...

Страница 108: ...ARNING I When turning on the master switch using an external power source or pulling the propeller through by hand treat the propeller as if the ignition switch were on Do not stand nor allow anyone e...

Страница 109: ...l power supplies a rocker switch labeled STROBE LT and a 5 amp push to reset circuit breaker The rocker switch and circuit breaker are located on the left side of the switch and control panel SECTION...

Страница 110: ...the oil cooler insulation for the engine crankcase breather line and a placard to be installed on the instrument panel This equipment should be installed for operations in temperatures consistently be...

Страница 111: ...to station or ground speed readouts The DME is designed to operate at altitudes up to a maximum of 50 000 feet at ground speeds up to 250 knots and has a maximum slant range of 199 9 nautical miles Th...

Страница 112: ...YPE 190 8 IDENT KNOB Rotation of this control increases or decreases the volume of the received station s Ident signal An erratic display accompanied by the presence of two Ident signals can result if...

Страница 113: ...DBOOK EMERGENCY LOCATOR SUPPLEMENT TRANSMITTER ELT SUPPLEMENT EMERGENCY LOCATOR TRANSMITTER ELT SECTION 1 GENERAL The ELT consists of a self contained dual frequency radio transmitter and battery powe...

Страница 114: ...onserve airplane battery Do not activate radio transceiver 3 AFTER SIGHTING RESCUE AIRCRAFT Place ELT function selector switch in the OFF position preventing radio interference Attempt contact with re...

Страница 115: ...aft to the waypoint repeatedly to provide continual informa tion on WHICH WAY and HOW FAR to the waypoint The pilot can monitor BEARING and RANGE on RNAV 511 to fly straight line paths to waypoints up...

Страница 116: ...gitally displays the magnetic bearing from the airplane to the waypoint While VOR DME pushbutton 5 is pressed the digital display reads RADIAL from the VOR station on which the airplane is presently p...

Страница 117: ...NAVIGATION OPERATING NOTES 1 Proper RNAV operation requires valid VOR and DME inputs to the RNAV system In certain areas the ground station antenna patterns and transmitter power may be inadequate to...

Страница 118: ...d DISTANCE Typically the first waypoint is set into the left side set of thumbwheels 8 RADIAL and DISTANCE Thumbwheels SET to second waypoint RADIAL and DISTANCE Typically the second waypoint is set i...

Страница 119: ...the airplane performance when this avionic equipment is installed 8 1 July 1979 9 PILOT S OPERATING HANDBOOK HF TRANSCEIVER SUPPLEMENT TYPE PT10 A SUPPLEMENT HF TRANSCEIVER TYPE PT 0 A SECTION GENERAL...

Страница 120: ...change to the airplane emergency procedures when this avionic equipment is installed SECTION 4 NORMAL PROCEDURES COMMUNICATIONS TRANSCEIVER OPERATION 1 XMTR SEL Switch on audio control panel SELECT tr...

Страница 121: ...er exciter a remote mounted power amplifier power supply an antenna coupler and an externally mounted fixed wire medium high frequency antenna A channel selector knob determines the operating frequenc...

Страница 122: ...g Controls 2 1 July 1979 0 PILOT S OPERATING HANDBOOK SSB HF TRANSCEIVER SUPPLEMENT TYPE ASB 125 SECTION 2 LIMITATIONS There is no change to the airplane limitations when this avionic equipment is ins...

Страница 123: ...Cessna 200A Navomatic is an all electric single axis aileron control autopilot system that provides added lateral and directional stability Components are a computer amplifier a turn coordinator an a...

Страница 124: ...signal to provide more precise operation during localizer approach In low sensitivity position push button out response to NAV signal is dampened for smoother tracking of enroute VOR radials it also...

Страница 125: ...or 2 PULL TURN Knob CENTER and PULL out 3 A P ON OFF Switch ON 4 Autopilot TRIM Control ADJUST for zero turn rate wings level indication on Turn Coordinator NOTE For optimum performance in airplanes e...

Страница 126: ...performance when this avionic equipment is installed 6 1 July 1979 2 PILOT S OPERATING HANDBOOK CESSNA 300 ADF SUPPLEMENT TYPE R 546E SUPPLEMENT CESSNA 300 ADF Type R 546E SECTION GENERAL The Cessna...

Страница 127: ...illator to permit coded identifier of stations transmitting keyed CW signals Morse Code to be heard REC Selects operation as standard communication receiver using only sense antenna ADF Set operates a...

Страница 128: ...FINDER 1 Function Selector Knob ADF position and note relative bearing on indicator 2 Function Selector Knob TEST position and observe that pointer moves away from relative bearing at least 10 to 20...

Страница 129: ...ting frequencies are digitally displayed by incandescent readouts on the front panel of the Nav Com A DME receiver transmitter or a glide slope receiver or both may be interconnected with the Nav Com...

Страница 130: ...ween 108 and 117 MHz simultaneously selects paired glide slope frequency and DME channel 8 COMMUNICATION RECEIVER TRANSMITTER FRACTIONAL MEGAHERTZ SELECTOR Depending on position of 5 0 switch selects...

Страница 131: ...00 Nav Com incorporates a variable threshold automatic squelch With this squelch system you set the threshold level for auto matic operation the further clockwise the lower the threshold or the more s...

Страница 132: ...with the windshield mounted glide slope antenna pilots should avoid use of 2700 100 RPM on airplanes equipped with a two bladed propeller or 1800 100 RPM on airplanes equipped with a three bladed pro...

Страница 133: ...LIND SECTION GENERAL The Cessna 300 Transponder Type RT 359A shown in Figure 1 is the airborne component of an Air Traffic Control Radar Beacon System ATCRBS The transponder enables the ATC ground con...

Страница 134: ...Altitude Encoder Blind Sheet 1 of 2 2 1 July 1979 4 PILOT S OPERATING HANDBOOK CESSNA 300 TRANSPONDER SUPPLEMENT AND ALTITUDE ENCODER BLIND 3 IDENT ID SWITCH When depressed selects special pulse iden...

Страница 135: ...TUDE ENCODER BLIND 2 Function Switch ON 3 DIM Control ADJUST light brilliance of reply lamp NOTE During normal operation with function switch in ON position reply lamp flashes indicating transponder r...

Страница 136: ...n the control center s radarscope more readily The Cessna 300 Transponder consists of a panel mounted unit and an externally mounted antenna The transponder receives interrogating pulse signals on 103...

Страница 137: ...provide a check of transponder operation Reply Lamp will glow steadily to verify self test operation 6 REPLY CODE SELECTOR KNOBS 4 Select assigned Mode A reply code 7 REPLY CODE INDICATORS 4 Display...

Страница 138: ...NT operation TO TRANSMIT MODE C ALTITUDE REPORTING CODES IN FLIGHT 1 Off Indicator Warning Flag VERIFY that flag is out of view on encoding altimeter 2 Altitude Encoder Altimeter Setting Knob SET IN a...

Страница 139: ...heading are sensed by the direction al gyro The computer amplifier electronically computes the necessary correction and signals the actuator to move the ailerons to maintain the airplane in the comman...

Страница 140: ...T or NAV TRK operation this high sensitivity setting increases autopilot response to NAV signal to provide more precise operation during localizer approach In low sensitivity position push button out...

Страница 141: ...Coordinator 2 PULL TURN Knob CENTER and PULL out 3 A P ON OFF Switch ON 4 Autopilot TRIM Control ADJUST for zero turn rate wings level indication on Turn Coordinator NOTE For optimum performance in a...

Страница 142: ...S OPERATING HANDBOOK CESSNA 400 GLIDE SLOPE SUPPLEMENT TYPE R 443B SUPPLEMENT CESSNA 400 GLIDE SLOPE Type R 443 B SECTION GENERAL The Cessna 400 Glide Slope is an airborne navigation receiver which r...

Страница 143: ...443B SECTION 3 EMERGENCY PROCEDURES There is no change to the airplane emergency procedures when this avionic equipment is installed SECTION 4 NORMAL PROCEDURES TO RECEIVE GLIDE SLOPE SIGNALS NOTE The...

Страница 144: ...e switch is labeled HIGH LO MUTE and provides the pilot with HIGH LO sensitivity selection and marker beacon audio muting for approximately 30 seconds to enable voice communica tion to be heard withou...

Страница 145: ...H ONE OR TWO TRANSMITTERS 1 MARKER BEACON ANNUNCIATOR LIGHTS OUTER Light illuminates blue to indicate passage of outer marker beacon MIDDLE Light illuminates amber to indicate passage of middle marker...

Страница 146: ...ger knob increases light intensity Figure 2 Cessna 400 Marker Beacon Operating Controls and Indicator Lights Supplied With Three Transmitters 4 1 July 1979 18 PILOT S OPERATING HANDBOOK CESSNA 400 MAR...

Страница 147: ...TUDE ENCODER BLIND SECTION 1 GENERAL The Cessna 400 Transponder Type RT 459A shown in Figure 1 is the airborne component of an Air Traffic Control Radar Beacon System ATCRBS The transponder enables th...

Страница 148: ...TUDE ENCODER BLIND SECTION 1 GENERAL The Cessna 400 Transponder Type RT 459A shown in Figure 1 is the airborne component of an Air Traffic Control Radar Beacon System ATCRBS The transponder enables th...

Страница 149: ...play selected Mode A reply code 8 REMOTE MOUNTED DIGITIZER Provides an altitude reporting code range of 1000 feet up to the airplane s maximum service ceiling FUNCTION SWITCH Controls application of p...

Страница 150: ...D ALTITUDE ENCODER BLIND 2 Function Switch ON 3 DIM Control ADJUST light brilliance of reply lamp NOTE During normal operation with function switch in ON position reply lamp flashes indicating transpo...

Страница 151: ...in flight on the control center s radarscope more readily The 400 Transponder consists of a panel mounted unit and an exter nally mounted antenna The transponder receives interrogating pulse signals o...

Страница 152: ...OL Allows pilot to control brilliance of Reply Lamp 5 SELF TEST TEST SWITCH When depressed causes transponder to generate a self interrogating signal to provide a check of transponder operation Reply...

Страница 153: ...reply lamp NOTE During normal operation with function switch in ON position REPLY lamp flashes indicating transponder replies to interrogations 4 ID Button DEPRESS momentarily when instructed by grou...

Страница 154: ...Airplane Flight Manual must be carried in the airplane when the Secondary Seat Stop modification is installed in accordance with Cessna Single Engine Service Bulletin SEB89 2 The information contained...

Страница 155: ...e desired flight position Regardless of where the seat is positioned rearward seat travel will be restricted in the event the seat occupant fails to lock the seat in position by normal means When rear...

Страница 156: ...rotate to an unlatched position to allow the passage of each stop plate tab and the aft seat roller housing The pilot should demonstrate the operation of all seats to the passengers before flight SEC...

Страница 157: ...e desired flight position Regardless of where the seat is positioned rearward seat travel will be restricted in the event the seat occupant fails to lock the seat in position by normal means When rear...

Страница 158: ...nt of the seat will be stopped when the aft roller housing on the seat contacts the secondary seat stop Then momentarily unlatch the secondary seat stop and move the seat farther aft to test that each...

Страница 159: ...nhang zum Flughandbuch D 82008 UNTERHACHING Cessna 172 RG Tel FAX 089 6113249 Ausgabe 22 7 96 Dieser Anhang zum Flughandbuch enth lt alle erg nzenden Informationen die f r den Betrieb des Flugzeuges C...

Страница 160: ...uf einen Wert innerhalb des gr nen Bereichs des Drehzahlmessers zu reduzieren Die ge nderten Steigleistungen sind zu beachten Siehe Abschnitt V dieses Anhanges zum Flughandbuch 3 4 Hermann LIESE FLUGT...

Страница 161: ...perating Handbook or Pilot s Operating Handbook and FAA Approved Airplane Flight Manual when Century Flight Systems Inc Century 2000 Autopilot Model AK1002 is installed in accordance with STC SA3495SW...

Страница 162: ......

Страница 163: ...applicable revision must be available to the pilot at all times in the aircraft when the autopilot is enabled SECTION 3 EMERGENCY OPERATING PROCEDURES 3 1 AUTOPILOT In the event of an autopilot malfu...

Страница 164: ...rim system circuit circuit breaker After failed system has been identified leave system circuit breaker open and do not operate until the system failure has been identified and corrected 3 Altitude Lo...

Страница 165: ...Pilot s Operating Manual for procedures not contained herein 4 1 COMMAND TRIM SYSTEM To be performed before the first flight of each day 1 Using the control wheel trim switch verify normal trim up and...

Страница 166: ...dition Both trim annunciators continuously extinguished is a properly trimmed condition 1 When the autopilot is engaged and a flashing trim annunciators is noted the pilot should manually move the air...

Страница 167: ...ng the final approach fix FAF reduce the power for approximately 65 70 KIAS on the final approach segment Adjust power as necessary during remainder of approach to maintain correct airspeed Monitor co...

Страница 168: ...ontrol the aircraft 2 Add take off power or power as desired 3 Check that correct attitude and a positive rate of climb is indicated then raise the flaps 4 Set the heading bug to the desired missed ap...

Страница 169: ...ed by Supplement SECTION 7 REQUIRED OPERATING EQUIPMENT Text of this Section not affected by Supplement SECTION 8 WEIGHT AND BALANCE Text of this Section not affected by Supplement i CENTURY FLIGHT SY...

Страница 170: ...k and basic Airplane Flight Manual when the optional Bendix King KLN 89B GPS system is installed in the Aircraft under Swiss FOCA Major Alteration No MOD 01 089 gig and according to Bendix King Inst M...

Страница 171: ...AVIONITEC Ltd General Aviation Center P O Box 1351 8058 Zurich Airport Switzerland Log of Revisions AFM Supplement Cessna 172RG King GPS KLN 89B...

Страница 172: ...of contents Page 1 General 4 2 Limitations 5 3 Emergency Procedures Abnormal Procedures 5 4 Normal Procedures 5 5 Performance 6 6 Weight and Balance 6 7 Airplane System Descriptions 6 Original Issue...

Страница 173: ...European Airspace system North Atlantic Minimum Navigation Performance Specifications MNPS Airspace and latitudes bounded by 74 North and 60 South using the WGS 84 or NAD 83 coordinate reference datu...

Страница 174: ...ndices B and C for appropriate pilot actions to be accomplished in response to annunciated messages Section 4 NORMAL PROCEDURES A OPERATION Normal operating procedures are outlined in the KLN 89B GPS...

Страница 175: ...s HSI course pointer is required to provide course datum to the autopilot E ALTITUDE ALERT AUDIO SIGNAL 1000 feet prior to reaching the selected altitude three short signals Upon reaching the selected...

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