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Cessna 150 COMMUTER 1976, Руководство по эксплуатации для пилотов

Книга "Pilot Operating Handbook" для Cessna 150 COMMUTER 1976 доступна для загрузки совершенно бесплатно на manualshive.com. Этот руководство поможет вам максимально эффективно использовать ваш самолет, обеспечивая безопасные и комфортные полеты. Будьте уверены в своих действиях, имея этот удобный ресурс под рукой.

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Содержание 150 COMMUTER 1976

Страница 1: ......

Страница 2: ...Down Power Off MAXIMUM WEIGHT STANDARD EMPTY WEIGHT Commuter Commuter II MAXIMUM USEFUL LOAD Commuter Commuter II BAGGAGE ALLOWANCE WING LOADING Pounds Sq Ft POWER LOADING Pounds HP FUEL CAPACITY Tota...

Страница 3: ...ervice FACTORY APPROVED SERVICE EQUIPMENT to provide you with the most efficient and accurate workmanship possible A STOCK OF GENUINE CESSNA SERVICE PARTS on hand when you need them THE LATEST AUTHORI...

Страница 4: ...n and Entry Dimensions Baggage Space Dimensions Specific Loadings Symbols Abbreviations and Terminology General Airspeed Terminology and Symbols Meteorological Terminology Engine Power Terminology Air...

Страница 5: ...ations and terminology commonly used DESC RIPTIVE DATA ENG INE Number of Engines 1 Engine Manufacturer Teledyne Continental Engine Model Number 0 200 A Engine Type Normally aspirated direct drive air...

Страница 6: ...ti viscosity oil with a range of SAE 10W30 is recom mended for improved starting in cold weather Oil Capacity Sump 6 Quarts Total 7 Quarts if oil filter installed 1 4 CESSNA MODEL 150M SECTION 1 GENER...

Страница 7: ...barometric subscale has been set to 29 92 inches of mercury 1013 mb CESSNA MODEL 150M SECTION 1 GENERAL ENGINE POWER TERMINOLO G Y BHP RPM Static RPM Brake Horsepower is the power developed by the eng...

Страница 8: ...t Useful Load Gross Loaded Weight Maximum Takeoff Weight Maximum Landing Weight Tare 1 8 Useful Load is the difference between takeoff weight and the basic empty weight Gross Loaded Weight is t he loa...

Страница 9: ...e No 3A1 9 as Cessna Model No 150M AIR SPEED LIMIT AT I ONS Airspeed limitations and their oper ational significance are shown in figure 2 1 SPEED KCAS KI AS REMARKS VNE Never Exceed Speed 141 141 Do...

Страница 10: ...116 C 240 F Oil Pressure Minimum 10 psi Maximum 100 psi Propeller Manufacturer McCauley Accessory Division Propeller Model Number 1A102 0CM6948 Propeller Diameter Maximum 69 inches Minimum 67 5 inches...

Страница 11: ...design load factors are 150 of the above and in all cases the structure meets or exceeds design loads KI N DS O F OP ERA TION LI MITS The airplane is equipped for day VFR and may be equipped for nigh...

Страница 12: ...alls Slow Deceleration 2 8 Abrupt use of controls prohibited above 97 knots Spin Recovery opposite rudder forward elevator neutralize controls Intentional spins with flaps extended are prohibited Flig...

Страница 13: ...ower Precautionary Landing With Engine Power Ditching Fires Engine Fire During Start On Ground Engine Fire in Flight Electrical Fire In Flight Cabin Fir e Wing Fire Icing Inadvertent Icing Encounter L...

Страница 14: ...nance are practiced Enr Alte weather emergencies can be minimized or eliminated by careful flight planning and good judgement when unexpect ed weather is encountered However should an emergency arise...

Страница 15: ...A MODEL 150M SECTION 3 EMERGENCY PROCEDURES and intentions 2 Heavy Objects in baggage area SECURE or JETTISON 3 Approa ch High Winds Heavy Seas INTO THE WIND Light Winds Heavy Swells PARALLEL TO SWELL...

Страница 16: ...oon as pOSSible with flaps retracted INADVERTENT ICING ENCOUNTER 1 Turn pitot heat switch ON 2 Turn back or change altitude to obtain an outside air temperature that is less conducive to icing 3 Pull...

Страница 17: ...o maintain airspeed and establish a glide attitude is the first response to an engine failure after takeoff In most cases the landing should be planned straight ahead with only small changes in direct...

Страница 18: ...abled and the pilot will have to rely on the turn coordinator or the turn and bank indicator if he inadvertently flies into clouds The following instructions assume that only the electrically powered...

Страница 19: ...f the control inputs may extend the recovery 6 AS ROTATION STOPS NEUTRALIZE RUDDER AND MAKE A SMOOTH RECOVERY FROM THE RESULTING DIVE NOTE If disorientation precludes a visual determination of the dir...

Страница 20: ...describe the recommended remedy for each situation EXCESSI V E RATE OF CHARGE After engine starting and heavy electrical usage at low engine speeds such as extended taxiing the battery condition will...

Страница 21: ...Nose Left Wing Left Wing Leading Edge Left Wing Trailing Edge Before Starting Engine Starting Engine Before Takeoff Takeoff Normal Takeoff Maximum Performance Takeoff Enroute Climb Cruise Before Land...

Страница 22: ...ration Normal procedures associated with Optional Sys tems can be found in Section 9 SPEEDS FOR SAFE OPERATION Unless otherwise noted the following speeds are based on a maxi mum weight of 1600 pounds...

Страница 23: ...Control Surfaces CHECK freedom of movement and security o RIGHT WING Trailing Edge 1 Aileron CHECK freedom of movement and security o RI G HT WING 1 Wing Tie Down DISCONNECT 2 Main Wheel Tire CHE CK...

Страница 24: ...ling Edge 1 Aileron CHECK freedom of movement and security BEFORE STARTING ENGIN E 4 6 1 Preflight Inspection COMPLETE 2 Seats Belts Shoulder Harnesses ADJUST and LOCK 3 Fuel Shutoff Valve ON 4 Radios...

Страница 25: ...1 Seats Belts Harnesses ADJUST and LOCK 2 Mixture RICH 3 Carburetor Heat ON apply full heat before closing throttle 4 Airspeed 60 70 KIAS flaps UP 5 Wing Flaps AS DESIRED O clOw 85 KIAS 6 Airspeed 50...

Страница 26: ...As soon as the cylinders begin to fire open the throttle slightly to keep it running After starting if the oil gage does not begin to show pressure within 30 seconds in the summertime and about twice...

Страница 27: ...itch first to R position and note RPM Next move switch back to BOTH to clear the other set of plugs Then move switch to the L posi tion note RPM and return the swit ch to the BOTH position RPM drop sh...

Страница 28: ...e climb would be marginal with flaps 10 Flap deflections greater than 10 are not approved for takeoff MAXIMUM PERFORMANCE TAKEOFF If an obstruction dictates the use of a steep climb angle after liftof...

Страница 29: ...eat is to be used continuously in cruise flight The use of full carburetor heat is recommended during flight in very heavy rain to avoid the possibility of engine stoppage due to excessive water inges...

Страница 30: ...ull down elevator may be required at aft center of gravity loadings to assure optimum recoveries 4 HOLD THESE CONTROL INPUTS UNTIL ROTATION STOPS Premature relaxation of the control inputs may extend...

Страница 31: ...gine four to ten strokes as the propeller is being turned over by hand NOTE Use heavy strokes of primer for best atomization of fuel After priming push primer all the way in and CESSNA MODEL 150M SECT...

Страница 32: ...make every effort to fly not less t han 2000 feet above the surface weather permitting even though flight at a lower level may be consistent with the provisions of government regulations 2 During dep...

Страница 33: ...ler con dition and air turbulence may account for variations of 10 or more in range and endurance Therefore it is important to utilize all available information to estimate the fuel required for the p...

Страница 34: ...ng altitude and winds aloft information have been given for this fl ight However the power setting selection for cruise must be de termined based on several considerations These include the cruise per...

Страница 35: ...adwind the ground speed for cruise is pre dicted to be 94 10 84 Knots Therefore the time required for the cruise portion of the trip is 5 6 327 Nautical Miles 84 Knots 3 9 Hours CESSNA MODEL 150M SECT...

Страница 36: ...98 108 50 60 70 80 85 50 60 69 78 82 50 60 70 80 85 50 61 72 83 89 Figure 5 1 Airspeed Calibration 120 118 CESSNA MODEL 150M 130 140 129 140 II I CESSNA MODEL 150M SECTION 5 PERFORMANCE TEMPERATURE CO...

Страница 37: ...c ru nup 3 Decrease distances 10 for each 9 knots headwind For operation with tailwinds up to 10 knots increase distances by 10 for each 2 knots 4 Where distance value has been deleted climb performan...

Страница 38: ...re NOTES 1 Add 0 8 of a gallon of fuel for engine start taxi and takeoff allowance 2 Increase time fuel and distance by 10 for each 8 C above standard temperature 3 Distances shown are based on zero w...

Страница 39: ...87 3 4 I Figure 5 7 Cruise Performance I I 5 14 CESSNA MODEL 150M 20 C ABOVE STANDARD TEMP KTAS GPH BHP 72 102 5 4 68 100 5 1 60 95 4 6 53 91 4 1 47 86 3 7 42 81 3 3 72 104 5 4 64 99 4 8 57 95 4 3 50...

Страница 40: ...Q Q Q to to to 0 to t 100 KTAS 94 KTAS 88 KTAS 600 640 680 720 RANGE NAUTICAL MI LES 87 KTAS 84 KTAS 81 KTAS 760 Figure 5 8 Range Profile Sheet 2 of 2 800 CESSNA MODEL 150M CONDITIONS 1600 Pounds ENDU...

Страница 41: ...se 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 operation on a dry grass runway increase distances by 45 of the gr...

Страница 42: ...50M SECTION 6 WEIGHT BALANCE EQUIPMENT LIST SECTION 6 WEIGHT BALANCE EQUIPMENT LIST TABLE OF CONTEN TS Introduction Airplane Weighing Procedures Weight and Balance Equipment List Page 6 3 6 3 6 5 6 13...

Страница 43: ...lug to drain all fuel c Remove oil sump drain plug to drain all oil d Move sliding seats to the most forward position e Raise flaps to the fully retracted position 2 Leveling a Place scales under each...

Страница 44: ...our airplane and enter them in the column titled YOUR AIRPLANE on the Sample Loading Problem NOTE In addition to the basic empty weight and moment noted on these records the c g arm fuselage station i...

Страница 45: ...used 84 AREA 2 as a convenient interior refer ence point for determining the location of baggage area fuselage stations 94 STANDARD SEATING 84 94 Figure 6 3 Loading Arrangements AREA 2 J OPTIONAL SEAT...

Страница 46: ...full oil 1100 35 9 Usable Fuel At 6 Lbs Gal Standard Tanks 22 5 Gal Maximum 135 5 7 Long Range Tanks 35 Gal Maximum Reduced Fuel As limited by maxi mum weight Pilot and Passenger Station 33 to 41 340...

Страница 47: ...20 22 5 MAX I I I 120 1 100 50 I 0 I 0 1 1600 j 1500 8 1450 1400 1350 1300 1250 1200 1150 1100 1 I 1 I I 10 I 10 m I I I I 2 3 4 5 6 7 8 9 10 11 12 13 14 LOAD MOMENT 1000 POUND INCHES NOTES Line repr...

Страница 48: ...sted 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...

Страница 49: ...ONE RESISTER MEMCOR LIGHT INSTALLATION WING TIP STROBE STROBE LIGHTS IN WING TIP SET OF 2 FLASHER POWER SUPPLIES IN TIPS SET OF 2 LIGHT INSTALLATION COWL MOUNTEO LANDING LIGHT INSTALLATION COWL MOUNTE...

Страница 50: ...ING OPERATIONAL LIMITATIONS PLACARD VFR 1FR DAY ND NIGHT INDICATOR STALL WARNING AuDIBLE G AUXIL I t RY EQUIPME NT HOOK TOW I NST AUED I STOWEDI HOISTING RINGS AIRCRAFT CABIN TOP CORROS ON PROOF IN G...

Страница 51: ...31 AI H25 A 3 CESSNA 300 NAV COM 360 CH SECOND UNI T WITH VOR LOC EXPORT ONLY RECEIVER TRAN SMI TTf R RT 5 28E 1 VOR LOC INDI CATOR IN 51 413 1 AVIO ICS OPTIO N Bl I TEM H37 AI H28 A 1 EMERGENCY LOCAT...

Страница 52: ...l Vl 0 UJ Z 0 Z Vl0 o o z U Ja o o Cl OVlU Er w z Ou lW I I u o vUct r I _Olo Z UJ J z Z ex 002 Z UJ l W OO wrOVl u r Q Z u o o UJ I z lUZ 0Z Z0 l O J a VlV1 c OWOOUJVl O UJ Z ElJJUJ Z 0 l lJJUUOO Z c...

Страница 53: ...s containing the fuel tanks are construc ed of a front and rear spar with formed sheet metal ribs doublers and stringers The entire structure is covered with aluminum skin The front spars are equipped...

Страница 54: ...CONTROL SYSTEM CESSNA MODEL 150M Figure 7 1 Flight Control and Trim Systems Sheet 1 of 2 7 4 CESSNA MODEL 150M SECTION 7 AIRP LANE SYSTEMS DESCRIPTIONS ELEVATOR CONTROL SYSTEM E LEVATOR T RIM CONTROL...

Страница 55: ...Altimeter 30 Throttle With Friction Lock l Ul 10 Marker Beacon Indicator Lights 31 Microphone i and Switches 32 Elevator Trim Control Wheel 11 Omni Course Indicator 33 Carburetor Heat Control Knob l...

Страница 56: ...which these items are related 7 8 CESSNA MODEL 150M SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS GROUND CONTROL Effective ground control while taxiing is accomplished through nose wheel steering by using...

Страница 57: ...seat back pull forward on the knob under the center of the seat and apply pres sur e to the back To re turn the seat back to the upright position pull forward on the exposed portion of the seat back...

Страница 58: ...eration Also the pilot will want the freedom to reach all controls easily Removing the shoulder harness is accomplished by pulling upward on the narrow release strap and removing the harness stud from...

Страница 59: ...e of the fixed type and cannot be opened Two additional fixed windows may be installed in the 7 14 CESSNA MODEL 150M cabin top CO N TROL LOCKS SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS A control lock is...

Страница 60: ...nstalled and is then circulated to the left and right oil galleries The engine parts are then lubricated under pres sure from the galleries Oil pressure to the galleries is regulated by a pressure rel...

Страница 61: ...t and injects it into the in take manifold when the plunger is pushed back in The plunger knob on the instrument panel is equipped with a lock and after being pushed full in must be rotated either lef...

Страница 62: ...approximately 1 75 gallons remains in a standard tank and 1 5 gallons remains in a long range tank as unusable fuel The indi cators cannot be relied upon for accurate readings during skids slips or u...

Страница 63: ...r switch is a split rocker type switch labeled MASTER and and is ON in the up position and OFF in the down position The right half of the switch labeled BAT controls all electrical power to the airpla...

Страница 64: ...d during lengthy maintenance work on the electrical and electronic equipment The recep tacle is located behind a door on the left side of the fuselage near the aft 7 24 CESSNA MODEL 150M dge of the co...

Страница 65: ...ck the appropriate circuit breaker If the circuit breaker has opened white button popped out and there is no obviOUS indication of a short circuit smoke or odor turn off the light switch of the affect...

Страница 66: ...s actuated by an atmospheric pressure 7 28 CESSNA MODEL 150M SECTION 7 AIRPLANE SYSTEMS DESCRIPTIONS change supplied by the static source AL TIM ETER Airplane altitude is depicted by a barometric type...

Страница 67: ...draws air through the warning horn resulting in an audible warning at 5 to 10 knots above stall in all flight conditions The stall warning system should be checked during the preflight in spection by...

Страница 68: ...nt IFR flights are planned installation of wick type static dischargers is recommended to improve radio communications during flight through dust or various forms of precipitation rain freezing rain s...

Страница 69: ...e Identification Plate located on the cabin floor below the left rear cor ner of the pilot s seat The plate is accessible by sliding the seat for ward and lifting the carpet in this area Located adjac...

Страница 70: ...f other nations may require other documents and data owners of airplanes not registered in the United States should check with their own aviation officials to determine their in dividual requirements...

Страница 71: ...rformed allowing the Dealer to make any minor adjustments which may be necessary You will also want to return to your Dealer either at 50 hours for your first Progressive Care Operation or at 100 hour...

Страница 72: ...in raising and holding the nose wheel off the ground weight down the tail by placing sand bags or suitable weight on each side of the 8 8 CESSNA MODEL 150M SECTION 8 HANDLING SERVICE MAINTENANCE hori...

Страница 73: ...breather fill to 5 quart level for normal flights of less than 3 hours For extended flight fill to 6 quarts These quantities refer to oil dipstick level readings During oil and oil filter changes one...

Страница 74: ...soaps or detergents which cause corrosion or scratches should never be used Remove stubborn oil and grease with a cloth moistened with Stoddard solvent 8 12 CESSNA MODEL 150M SECTI N 8 HA NDLING RVIe...

Страница 75: ...fabric keep the foam as dryas possible and remove it with a vacuum cleaner The plastic trim headliner instrument panel and control knobs need only be wiped off with a damp cloth Oil and grease on the...

Страница 76: ...he ELT emits an omni dir ec tional signal on the international distress frequencies of 121 5 and 243 0 MHz Some ELT units in export aircraft t ransmit only on 121 5 MHz General aviation and commercial...

Страница 77: ...LOCATOR TRANSMITTER ELT 2 PRIOR TO SIGHTING RESCUE AIRCRAFT Conserve airplane battery Do not activate radio transceiver 3 AFTER SIGHTING RESCUE AIRCRAFT Place ELT function selector switch in the OFF...

Страница 78: ...ver transmitter a spike antenna and interconnecting cables The system utilizes the airplane microphone headphone and speaker All of the required operating controls are mounted on the front panel of th...

Страница 79: ...d noise decreases squelch action counterclockwise rotation decreases background noise Figure 1 Cessna 300 Transceiver Controls PILOT S OPERATING HANDBOOK SUPPLEMENT CESSNA 300 TRANSCEIVER TYPE RT 524A...

Страница 80: ...ived the navigation receiver does not include the circuits required to actuate the course deviation needle However the audio portion of the localizer is audible so that flight information such as that...

Страница 81: ...ncy in 0 05 MHz steps between 0 00 and 0 95 MHz 7 NAVIGATION RECEIVER MEGAHERTZ SELE CTOR Selects navigation receiver fr equency in 1 MHz steps between 108 and 117 MHz 8 NAVIGATION RECEIVER VOLUME CON...

Страница 82: ...nd transmits sig nals between 118 00 and 135 95 MHz in 50 kHz steps The navigation re ceiver receives and interprets VOR and localizer signals between 108 00 and 117 95 MHz in 50 kHz steps The communi...

Страница 83: ...equency in O 05 MHz steps between O 00 and O 95 MHz 10 COMBINED INDENTIFIER SIGNAL SELECTOR AND VOR SEL F TEST SELECTOR SWITCH When VOR station is selected in ID position station identifier is audible...

Страница 84: ...istening level OFF VOL knob must be ON 5 SQ Control ROTATE counterclockwise t o decrease background noise TO OPERATE IDENT FILTER 4 1 ID T Switch CENTER unmarked to include filter in audio circuit of...

Страница 85: ...transmitter or a glide slope r eceiver or both may be interconnected with the Cessna 300 Nav Com set for automatic selec tion of the associated DME or GS frequency When a VOR frequency is selected on...

Страница 86: ...ope frequency or DME channel 9 NA VIGATION RECEIVER VOLUME CONTROL Controls volume of audio from navigation receiver only Clockwise rotation increases audio level 10 NAVIGATION RECEIVER FRACTIONAL MEG...

Страница 87: ...ELECT operating frequency not selected for navigational frequencies 5 VOL Control ADJUST to listening level OFF VOL knob must be ON 6 SQ Control ROTATE counterclockwise to decrease background noise PI...

Страница 88: ...l reception of amplitude modulated AM signals With the function selector knob at ADF the Cessna ADF provides a visual indication on the bear ing indicator of the bearing to the trans mitting station r...

Страница 89: ...receiver using only sense antenna NOTE In this position an automatic pointer stow feature will alert the pilot to non ADF operation by positioning and retaining the pointer at the 3 00 o clock positi...

Страница 90: ...ADJUST to desired listening level NOTE When switching stations place function selector knob in REC position Then after station has been selected PILOT S OPERATING HANDBOOK SUPPLEMENT return selector...

Страница 91: ...e signals on 1030 MHz and transmits coded pulse train r eply signals on 1090 MHz It is capable of r eplying to Mode A aircraft position identification and Mode C altitude information interrogations on...

Страница 92: ...mmediate identification of aircraft on ground con troller s display Reply Lamp will glow steadily during duration of IDENT pulse transmission 4 DIMME R CONTROL Allows pilot to control brilliance of re...

Страница 93: ...ECT assigned code 4 PILOT S OPERA TING HANDBOOK SUPPLEMENT CESSNA 300 TRANSPONDER AND ALTITUDE ENCODER 2 Function Switch ON 3 DIM Control ADJUST light brilliance of r eply lamp NOTE During normal oper...

Страница 94: ...odels a HI LO sensitivity selector switch and a press to test button are provided On all 172 177 177RG 180 and 185 series models a single three position switch is provided for HI LO sensitivity select...

Страница 95: ...l clock wise fully on n order to view the marker beacon lights during te st 4 LO HI SENS SWITCH 150 182 206 207 210 337 Model Series Only In the LO position Up receiver sensi tivity is positioned tor...

Страница 96: ...d SECTION 4 NORMAL PROCEDURES TO OPERATE 1 OFF VOL Control VOL position and adjust to desired listening level 2 LO HI SENS Switch SELECT HI position for airway flying or LO position for ILS approaches...

Страница 97: ...Ce a It TAKE YOUR CESSNA HOME FO R SERVICE AT THE SIGN OF THE CESS NA SHIELD CESSNA AIRCRAFT COMPANY WICHITA KANSAS...

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