Pilot s Operating Handbook - Wayman Flight Training

1 Pilot s Operating HandbookAndFAA Approved Airplane Flight Manual(abridged for KCN Aero Club)N49696 For complete information, consult Pilot s Operating ManualThis abbreviated Pilot s Handbook contains excerpts of the Cessna 152 Pilot sOperating Temperature Chart added January 2, 2003 Performance - SpecificationsSpeed *Maximum at Sea Level ..110 knotsCruise, 75% Power at 8,000 ft ..107 knotsCRUISE: Recommended lean mixture with fuel allowance forengine start, taxi, takeoff, climb and 45 minutes reserve at 45%power75% Power at 8,000 ft .. Range350 NM Gallons usable fuel .. hours75% Power at 8,000 ft .. Range580 NM Gallons usable fuel .. hoursMaximum Range at 10,000 ft .. Range415 NM Gallons usable fuel .. hoursMaximum Range at 10,000 ft .. Range690 NM Gallons usable fuel .. hoursRATE OF CLIMB AT SEA LEVEL ..715 FPMSERVICE CEILING ..14,700 FTTAKEOFF PERFORMANCE Ground Roll.

2 725 ft Total Distance over 50 ft obstacle ..1340 ftLANDING PERFORMANCE Ground roll ..475 ft Total Distance over 51 ft obstacle ..1200 ftSTALL SPEED (CAS) Flaps up, power off ..48 knots Flaps down, power off ..43 knotsMAXIMUM WEIGHT Ramp ..1675 lbs Takeoff or landing ..1670 lbsSTANDARD EMPTY WEIGHT 152 ..1101 lbs 152 II ..1133 lbsMAXIMUM USEFUL LOAD 152 ..574 lbs 152 II ..542 BAGGAGE ALLOWANCE ..120 LBSWING LOADING (Pounds / ) .. LOADING (Pounds / HP) .. CAPACITY26 galOIL CAPACITY ..6 qtsENGINE: Avco Lycoming O235-L2C 110 bhp at 255o rpmPROPELLER: Fixed Pitch, diameter ..69 in Speed performance is shown for an airplane equipped with optional speed fairings which increasethe speeds by approximately 2 kts. There is a corresponding difference in range while all otherperformance figures are unchanged when speed fairings are installed. Page 1-2 AIRSPEED LIMITATIONSSPEEDKCASKIASREMARKSVNEN ever Exceed Speed145149Do not exceed thisspeed in any operationVNOM aximum StructuralCruising Sped108111Do not exceed thisspeed except in smoothair, and then only withcautionVAManeuvering Speed:1670 not make full orabrupt controlmovements above thisspeedVFEM aximum Flap ExtendedSpeed8785 Maximum Window OpenSpeed145149 AIRSPEED INDICATOR MARKINGSMARKINGKIASSIGNIFICANCEW hite arc35 - 85 Full flap Operating range.

3 Lower limit is maximum weightV-so in landing configuration. Upper limit is maximumspeed permissible with flaps extendedGreen arc40 111 Normal operation range. Lover limit is maximum weightVs at most forward with flaps retracted. Upper limitis maximum structural cruising speedYellow arc111 149 Operations must be conducted with caution and only insmooth airRed Line149 Maximum speed for all operationsPower Plant Limitations and MarkingsEngine Operating Limits for Takeoff and Continuous OperationsMaximum Power 110 BHPM aximum Engine speed 2550 RPMM aximum Oil Temperature 245 F (118 C)Oil PressureMinimum 25 psiMaximum 100 psiManeuver limitsThis airplane is certificated in the utility category and is designed for limited aerobatic the acquisition of various certificates such as commercial Pilot and Flight instructor, certainmaneuvers are required. All of these maneuvers are permitted in this airplanePage 1-3No aerobatic maneuvers are approved except those listed belowManeuverRecommended Entry SpeedChandelles95 Lazy Eights95 Steep Turns95 SpinsSlow DecelerationStalls (except whip stalls)Slow DecelerationHigher speeds can be used if abrupt use of controls if avoidedThe baggage compartment and / or child s seat must not be occupied during aerobaticsAerobatics that may impose high loads should not be attempted.

4 The important thing to bearin mind in Flight maneuvers is that the airplane is that the airplane is clean in aerodynamicdesign and will build up speed quickly with the nose down. Proper speed control is anessential requirement for execution of any maneuver and care should always be exercised toavoid excessive speed which, in turn, can impose excessive loads. In the execution of allmaneuvers, avoid abrupt of Load Factor LimitsFlaps Up + g to gFlaps Down+ gFuel LimitationsTotal fuel capacity 26 gal (13 gal each tank)Usable fuel, all conditions galApproved Fuel Grades100 LL Grade Aviation100 Grade AviationAutomotive (91 octane minimum)Mixed fuel (automotive and aviati on)Section 2- Placards Not IncludedPage 1-4 SECTION 3 EMERGENCY PROCEDUREST able of ContentsPageIntroduction .. 3-3 Airspeeds for Emergency 3-3 OPERATIONAL CHECKLISTS Engine 3-3 Engine Failure During Takeoff Run.

5 3-3 Engine Failure Immediately After Takeoff.. 3-3 Engine Failure during 3-3 Forced Landings .. 3-4 Emergency Landing Without Engine 3-4 Precautionary Landing With Engine 3-4 Ditching .. 3-4 3-5 During Start On Ground .. 3-5 Engine Fire In 3-5 Electrical Fire In 3-5 Cabin Fire .. 3-6 Wing 3-6 3-6 Inadvertent Icing 3-6 Landing With A Flat Main Tire .. 3-7 Electrical Power Supply System 3-7 Ammeter Shows Excessive Rate Of Charge (Full Scale Deflection).. 3-7 Low-Voltage Light Illuminates During Flight (Ammeter Indicates Discharge)3-7 AMPLIFIED PROCEDURES Engine 3-8 Forced Landings .. 3-8 Landing without elevator 3-9 3-9 Emergency Operation In Clouds (Vacuum System Failure).. 3-9 Executing A 1800 Turn In Clouds .. 3-9 Emergency Descent Through Clouds .. 3-10 Recovery From A Spiral Dive .. 3-10 Inadvertent Flight Into Icing 3-10 Spins .. 3-11 Page 3-1 Rough Engine Operation Or Loss Of Power.

6 3-11 Carburetor 3-11 Spark Plug Fouling .. 3-11 Magneto Malfunction .. 3-11 Low Oil Pressure .. 3-12 Electrical Power Supply System Malfunctions .. 3-12 Excessive Rate of Charge .. 3-12 Insufficient Rate of Charge .. 3-12 Page 3-2 INTRODUCTIONS ection 3 provides checklist and amplified procedures for coping with emergenciesthat may occur. Emergencies caused by airplane or engine malfunctions are extremely rare ifproper preflight inspections and maintenance are practiced. Enroute weather emergencies canbe minimized or eliminated by careful Flight planning and good judgment when unexpectedweather is encountered. However, should an emergency arise, the basic guidelines describedin this section should be considered and applied as necessary to correct the FOR EMERGENCY OPERATIONE ngine Failure After 60 KIASM aneuvering Speed:1670 Lbs ..104 KIAS1500 Lbs .. 98 KIAS1350 Lbs .. 93 KIASM aximum 60 KIASP recautionary Landing With Engine 55 KIASL anding Without Engine Power:Wing Flaps 65 KIASWing Flaps 60 KIASOPERATIONAL CHECKLISTSENGINE FAILURESENGINE FAILURE DURING TAKEOFF RUN1.

7 Throttle -- Brakes -- Wing Flaps -- Mixture -- IDLE Ignition Switch -- Master Switch -- FAILURE IMMEDIATELY AFTER TAKEOFF1. Airspeed -- 60 Mixture -- IDLE Fuel Shutoff Valve -- Ignition Switch -- Wing Flaps -- AS Master Switch -- 3-4 ENGINE FAILURE DURING FLIGHT1. Airspeed -- 60 Carburetor Heat -- Primer -- IN and Fuel Shutoff Valve -- Mixture -- Ignition Switch -- BOTH (or START if propeller is stopped).FORCED LANDINGSEMERGENCY LANDING WITHOUT ENGINE POWER1. Airspeed 65 KIAS (flaps up60 KIAS (flaps DOWN).2. Mixture -- IDLE Fuel Shutoff Valve -- Ignition Switch -- Wing Flaps -- AS REQUIRED (30 recommended).6. Master Switch -- Doors -- UNLATCH PRIOR TO Touchdown -- SLIGHTLY TAIL Brakes -- APPLY LANDING WITH ENGINE POWER1. Airspeed -- 60 Wing Flaps -- 20 .3. Selected Field -- FLY OVER, noting terrain and obstructions, then retract flaps uponreaching a safe altitude and Radio and Electrical Switches -- Wing Flaps -- 30 (on final approach).)

8 6. Airspeed -- 55 Master Switch -- Doors -- UNLATCH PRIOR TO Touchdown -- SLIGHTLY TAIL Ignition Switch -- Brakes -- APPLY Radio - - TRANSMIT MAYDAY on MHz, giving location and intentions andSQUAWK 7700 if transponder is Heavy Objects (in baggage area) -- SECURE OR Approach -- High Winds, Heavy Seas -- INTO THE WIND.; Light Winds, Heavy Swells -- PARALLEL TO 3-54. Wing Flaps -- 30 .5. Power -- ESTABLISH 300 FT/MIN DESCENT AT 55 Cabin Doors -- Touchdown -- LEVEL ATTITUDE AT 300 FT/MIN Face -- CUSHION at touchdown with folded Airplane -- EVACUATE through cabin doors. If necessary, open windows and floodcabin to equalize pressure so doors can be Life Vests and Raft -- START ON GROUND1. Cranking CONTINUE ,to get a start which would suck the flames and accumulated fuelthrough the carburetor and into the engine starts:2. Power -- 1700 RPM for a few Engine -- SHUTDOWN and inspect for engine fails to start:4.

9 Cranking -- CONTINUE in an effort to obtain a Fire Extinguisher - - OBTAIN (have ground attendants obtain if not installed).6. Engine -- Master Switch -- Ignition Switch -- Fuel Shutoff Valve -- Fire EXTINGUISH using fire extinguisher ,wool blanket ,or Fire Damage -- INSPECT, repair damage or replace damaged components or wiringbefore conducting another FIRE IN FLIGHT1. Mixture -- IDLE Fuel Shutoff Valve -- Master Switch -- Cabin Heat and Air -- OFF (except wing root vents).5. Airspeed -- 85 KIAS (If fire is not extinguished, increase glide speed to find an airspeedwhich will provide an incombustible mixture).6. Forced Landing -- EXECUTE (as described in Emergency Landing Without EnginePower).Page 3-6 ELECTRICAL FIRE IN FLIGHT1. Master Switch -- All Other Switches (except ignition switch) -- Vents/Cabin Air/Heat -- Fire Extinguisher -- ACTIVATE (if available)WARNINGA fter discharging an extinguisher within a closed cabin,ventilate the If fire appears out and electrical power is necessary for continuance of Flight :6.

10 Master Switch -- Circuit Breakers -- CHECK for faulty circuit, do not Radio/Electrical Switches -- ON one at a time, with delay after each until short circuit Vents/ Cabin Air/ Heat -- OPEN when it is ascertained that fire is FIRE1. Master Switch -- Vents/Cabin Air/Heat -- CLOSED (to avoid drafts).3. Fire Extinguisher -- ACTIVATE (if available).WARNINGA fter discharging an extinguisher within a closed cabin,ventilate the Land the airplane as soon as possible to inspect for damage,WING FIRE1. Navigation Light Switch -- Strobe Light Switch (if installed) -- Pitot Heat Switch (if installed) -- a sideslip to keep the flames away from the fuel tank and cabin, and land as soon aspossible, with flaps 3-7 ICINGINADVERTENT ICING ENCOUNTER1. Turn pitot heat switch ON (if installed).2. Turn back or change altitude to obtain an outside air temperature that is less conducive Pull cabin heat control full out to obtain maximum defroster air temperature.