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PILOT'S OPERATING MAFdDBOOEi
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CONGRATULATIONS . . .
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LIST OF EFFECTIVE PAGES
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LIST OF EFFECTIVE PAGES CONTINUED -
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PILOT'S OPERATING HANDBOOK ~ r n
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TABLE 06 COlTEWTS
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TABLE OF CONTENTS
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FIGURE 1-1 THREE VIEW
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5. 125 i n ,
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STANDARD AIRPLANE WEIGHTS
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Maneuvering Speed is the maximum speed at
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Outside Air Temperature is the free air
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Revo%utions Per -u Mirrute i s engine speed,
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The extreme center of gravity locations within
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SECTION II .
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AIRSPEED DWBDCATOR MAWKlNGS
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POWER PLANT LlMITATIONS
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POWER PLANT INSTRUMENT MARKINGS
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Maximum Positive Load Factor,
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DECALS & PLACARDS
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On Lower Center
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On Fuel Selector Valve
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The following placards must be installed on the
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Qn Lrhoasrd End oa" Right Flap
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T A B L E OF CONTENTS
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, il '
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EWGlME FIRE- GROUND
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ENGlNE FAILURE DURBNG GROUND ROLL
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AIR START PROCEDURE
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POWER OFF LANDlNG
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FADLURE OF LANBlNG GEAR
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UNLATCHED DOOR IN FLIGHT
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ing to reset the breaker not more than one time
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FAlbURE OF LANDING GEAR TO
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SECTION I V .
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FIGURE 4- I. PREFLIGHT WALK AROUND DUGRAM
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Flap and Attach Points--CHECK.
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Fuel Tank--CHECK QUANTITY.
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Propeller Contr 01- -FORWARD/~GH RPM.
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6. Annunciator Lights & Gear Horn--CHECK WITH
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Move the controls slowly and smoothly. En
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TAKEOFF (Obstacle Clearance)
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CLIMB (Best Rate)
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Enrich until engine suns sn~oothly and power i s
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Trim - ADJUST, a s necessary.
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Throttle--IDLE at 1000 to 1200 RPM until cy-
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SECTION V .
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ALf lTUDE CONVERSION
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DEGREES CELSIUS (CENTIGRADE)
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KNOTS - KT§.
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NORMAL STATIC SYSTEM - FLAPS AND GEAR UP, POWER ON
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NORMAL STATIC SYbwI'EM - FLAPS AND GEAR D W M
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A L T E R N I A E STATIC SOURCE
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Gross Weight = 2'940 EBS.
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TAKEOFF DISTANCES (Maximum Performance)
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800 1000 1200 1400
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TIME, FUEL AND DISTANCE TO CLIMB
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TIME, FUEL AND DISTANCE "$ CLIMB
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CRUISE & RANGE DATA CONDlTlONS
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CRUISE 8, RANGE AT ECONOMY CRUISE
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CRUISE 8 RANGE AT ECONOPAY CRUBISE
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CRUISE & RANGE AT ECONOMY CRUISE
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CRUISE & RANGE AT ECQNOMV CRUISE
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CRUBSE L RANGE AT ECONOMY CRUISE
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CRUISE L RANGE AT 66QN6MY CRUlSE
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CRUISE L RANGE AT ECGNOMY CRUiSE
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CRUlSE % RANGE AT ECONOMY CRUISE
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CRUlSE L RANGE AT BEST POWER
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CRU19E & RANGE AT BEST PQWEW
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CRUISE L RANGE ANBEST POWER
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14,QQO FT, -13"~
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NORMAL LANDING DiSTANCES
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WEIGHT & BALAWCE
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Measure the horizontal distance from the reference
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s 5 5
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FAA REGISTRATION NO.
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AIRCRAFT CG LOCATION(LY)
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Once more proceed a s in Step 2 to account for
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8 2 0 2 3 0 - 5 0 1
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SECTION VII .
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ELECTRIC GEAR WCTRACFIBN SYSTEM . .
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FIGURE 7-1 ENGINE AIR IND&TG'FION SYSTEM
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'$he engine tlas a full-pressure we&--~ilmp
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FLIGHWPANE h B CONTROLS FAMlLlARlZATlON
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Airplane altitude is depicted by a barometric type
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3 FLAP SWTCIT
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LANDING LIGHT WITCH/CBZCUIT BREAKER
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ENGIPJE YNSTRUMEN'YS ANB CONTROLS
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: @ COWL FLAP CONTROL
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@ RADIO MICROPHONE (If Installed)
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En~ergency Locator Transmitter section for proper
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PREP4It%?Y FLIGHT CONTROLS
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ELECTRIC GEAR RETRACTION SYSTEM
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EMERGENCY GEAR- EXTENSION SY$TEM
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IGNITION & CIG LTR (OPT)
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Push--{ o--r:?st?t, piisll-pull,
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Rotating the knob above the pilot seat extends or
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SECTION VII& .
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Individual wheels may be raised with-
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Your Mooney Service Center has approved brands of
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P% Bonaldson D-1408 Filter Cleaner is
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1.295. A recharge is necessary when the specific
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