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.

2 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 ..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.

3 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.

4 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.

5 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)

6 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.

7 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.

8 3-3 Airspeeds for Emergency 3-3 OPERATIONAL CHECKLISTS Engine 3-3 Engine Failure During Takeoff Run .. 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).

9 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 .. 3-11 Carburetor 3-11 Spark Plug Fouling .. 3-11 Magneto Malfunction.

10 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.