Engineering and Research Corporation Ercoupe 415-C Скачать руководство пользователя страница 8

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density found at sea level when the barometer reads 29.92 inches 
of mercury and the temperature is 59⁰ F. 

The true air speed may be found with satisfactory accuracy by 
adding to the indicated air speed, 1 percent of itself for every 10⁰ 
above 59⁰ (or subtracting likewise for below) 

For example, if the temperature is 89⁰ and the indicated air speed 
is 95 MPH, 1 per cent of it is .95 MPH and for 3 percent add 2.85 
MPH, making the true air speed 97.85 MPH 

For altitudes up to 10,000 feet, at 59⁰, add 1 per cent for every 500 

ft.   At 6000 feet add to this indicated air speed of 95 MPH, 12 x

 .

95 

or 11.40 MPH, making 106.40 MPH.  Since the temperature at 6000 
feet is 89⁰ the 2.85 MPH correction should also be added, making 

109.25 MPH 

There is also a correction for a change in barometric pressure.  If 
the barometer at sea level is down 0.6” below the normal 29.92, 

another 1 percent is added. Therefore, if the barometer reads 29.62 
at sea level, add .5 x 

.

95 or .47 MPH to the 109.25 MPH, making 

109.72 MPH the true airspeed. 

The carburetor mixture control is operated by means of a push-pull 

knob on the instrument panel near the throttle.  At altitudes above 
5000 ft, the decreased density of the air may cause the mixture to 
become too rich for best power. This may be investigated by 

moving the mixture control from the full-rich position while 
checking the constant load RPM.   If the RPM does not increase as 
the mixture is made leaner, the control should be returned to the 

full-rich position. For average operation below 5000 feet altitude, 
the carburetor should be left in the full-rich position. When at part 
throttle, the fuel consumption may be improved by leaning the 
mixture, but in no case should the control be moved far enough to 

decrease the engine RPM.   The control should always be moved 
back to full-rich before any change in throttle setting 

While cruising, the carburetor air heater is controlled by a 

push-pull knob on the instrument panel near the throttle.  The 
engine should be operated with cold air at all times, except when 

Содержание Ercoupe 415-C

Страница 1: ...Ercoupe 415 C Pilot Operating Handbook...

Страница 2: ...em 7 Fuel System 8 Exhaust System 5 Appendix January 2013 This version of the Ercoupe POH was derived from the original 1946 Ercoupe 415 C Instructional Manual that was scanned to a PDF file and is po...

Страница 3: ...nd aft controls the elevator The ERCOUPE is certified by the Civil Aeronautics Administration as characteristically incapable of spinning OPERATING LIMITATIONS Required Information For 75 H P Model 41...

Страница 4: ...ther The ignition switch can then be turned to BOTH the throttle opened slightly about 1 8 and the starter engaged If the engine fails to start the operation should be repeated If the engine loads up...

Страница 5: ...if desired and using greater engine power for taxiing Finally warmed up the engine will turn approximately 2000 RPM standing still TAKING OFF For the take off there s a trim tab adjustment handle on t...

Страница 6: ...aves the ground completely Neutralize the control wheel after the airplane breaks contact The nose will normally swing and point upwind just about right to offset drift The main thing is not to have t...

Страница 7: ...energy is available to overcome the effects of gusty air or misjudgment If the control wheel is eased back gradually with power full on the airplane will reach an uncomfortable nose high altitude In...

Страница 8: ...29 62 at sea level add 5 x 95 or 47 MPH to the 109 25 MPH making 109 72 MPH the true airspeed The carburetor mixture control is operated by means of a push pull knob on the instrument panel near the t...

Страница 9: ...one between 60 and 70 MPH As the ground is approached the flight path is leveled off so as to reduce the vertical velocity At the same time the airplane is flared in the conventional manner until it...

Страница 10: ...had been reached Also if the approach has been made at too high an altitude the flight path can be steepened by rolling the airplane from side to side dipping each wing 20 or 30 degrees If the altitud...

Страница 11: ...and land at a somewhat higher speed than in still air and to have the airplane at all times either definitely in the air or definitely on the ground After landing the brakes may be used as desired In...

Страница 12: ...to the air and a straight course of travel is maintained without difficulty The pilot should not hesitate to make slight turns near the ground in order to maintain the desired path and avoid being dr...

Страница 13: ...round Immediately thereafter ease the control wheel forward slowly and roll down the runway Prompt application of the brakes or setting the brake on about half way during the glide approach brings the...

Страница 14: ...1 Carburetor Air Heat Off use full heat in icing conditions 2 Oil temperature 90 F min 3 Oil pressure 35 lb sq inch above 1900 RPM 4 Full throttle 2000 RPM approximately 5 Ignition Check maximum 75 RP...

Страница 15: ...nges or modifications in his airplane be recommended The serial number on the nameplate fastened on the deck behind the baggage compartments should be included in all correspondence requesting informa...

Страница 16: ...Remove axle nut 4 Pry bead of tire loose 5 Remove outer wheel half and tire Leave inner wheel half remaining on axle TO INSTALL TIRE REVERSE REMOVAL PROCEDURE TIRE NOSE WHEEL In removing tire proceed...

Страница 17: ...Continue bleeding until brake has a solid feel when applied Note Do not allow hydraulic brake fluid to get on linings Wash clean with carbon tetrachloride or naphtha CONTROL SYSTEM To Check Control Sy...

Страница 18: ...ipped shop Watch for signs of wear and dents on the leading edges or scratches which expose the wood and permit the absorption of moisture Bare spots should be sanded and sealed with spar varnish Mois...

Страница 19: ...k to the wing tanks Fuel is gravity feed from the header tank to the engine carburetor In case of fuel pump failure the engine will continue to function until the six gallon header tank is empty The M...

Страница 20: ...he floor on the pilots side of the cockpit The header tank gauge located forward of the windshield is a visual check of the remaining fuel in the header tank When the gauge is fully up there are six g...

Страница 21: ...be understood and periodically checked by the pilot during flight operation Excessive charging at a high rate will boil the battery and cause serious damage During all operation the master switch sho...

Страница 22: ...22 Electrical System...

Страница 23: ...acks that would allow the exhaust gases from the engine to enter the carburetor or cabin heater Any crack permitting exhaust leakage should be repaired immediately APPENDIX 1 Ercoupe Inspection Report...

Страница 24: ...ks 1 Drain Oil 2 Exhaust System 3 Ignition Wiring 4 Fuel Lines 5 Fuel Sediment Bowl 6 Carburetor and Air Intake 7 Bolts and Nuts 8 Engine Mount Fittings 9 Check Compression LANDING GEAR 1 Brakes 2 Tir...

Страница 25: ...Exhaust System Heaters 3 Spark Plugs 4 Magnetos 5 Fuel Tank Finger Strainers 6 Oil System Screen 7 Carburetor and Air System LANDING GEAR 1 Wheels 2 Shock Absorber Units 3 Brake Lines 4 Bolts and Fit...

Страница 26: ...26 CRUISE CONTROL TABLES...

Страница 27: ...ERCOUPE LUBRICATION CHART...

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