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RETURN TO FLIGHT TRAINING INFO-PRESS HERE
N3907F s/n 36807
The 1958 model 4-place is renowned for its visibility. It’s cowling slopes down like a modern ag aircraft allowing an unparalleled view among aircraft of its type. It is configured with a straight tail with no rear window. Already excellent maneuverability and comfort at low speeds is enhanced by a full Horton STOL kit; it lands at a "slow walk!" For training purposes, students like its ample power and performance at our 3400' elevation airport.
ENGINE
The power plant is a Continental 0300 six cylinder producing 145 very smooth horsepower. OK for flight instruction any time of the day at Quincy's mountain airport.
EQUIPMENT
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P E R F O R M A N C E
| PAYLOAD, | BEST | |||||
| FULL FUEL | RANGE | Vx | Vy | GLIDE | Va | Vne |
| 663 lbs. | 4.6 hrs. | 60 | 72 | 65 | 115 | 160 |
FOR TRAINING PURPOSES WE HAVE ADDED THE INFORMATION BELOW
Cessna 3907F Checklist
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BEFORE STARTING
CONTROL LOCK -------------------------- REMOVED SEAT BELTS ---------------------------------- LOCKED FUEL SELECTOR ------------------------------- BOTH ELECTRIC & AVIONICS ------------------------- OFF MASTER ------------------------------------------------ ON TIME ----------------------------------------------- NOTED
STARTING
MIXTURE -------------------------------------------- RICH CARB HEAT ----------------------------------------- OFF THROTTLE ---------------------------------- CRACKED PRIME ----------------------------------------- AS REQD MAGNETOS --------------------------------------- BOTH PROPELLER ----------------------------------- CLEAR! BRAKES --------------------------------------- APPLIED STARTER ----------------------------------- ENGAGED
AFTER STARTING
OIL PRESSURE -------------------------------------- UP MIXTURE --------------------------- LEAN AS REQD AVIONICS & LIGHTS ------------------- ON AS REQD
BEFORE TAKEOFF
CONTROLS ---------------------------------------- FREE TRIM -------------------------------------------------- SET FLAPS ----------------------------------------- AS REQD INSTMNTS & AVIONICS ------- CHECKED & SET FUEL GAUGES ---------------------------- CHECKED RUNUP 1700 RPM: MIXTURE --------------------------- LEAN AS REQD CARB HEAT ------------------------------- CHECKED MAGNETOS ------------------------------- CHECKED AMPS --------------------------------------- CHARGING
DOORS & WINDOWS ---------------------- LOCKED
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CLIMB FLAPS ------------------------------------ RETRACTED BEST ANGLE OF CLIMB ------------------- 57 KTS BEST RATE OF CLIMB ------------------- 65 KTS
CRUISE
MIXTURE ------------------------------- LEAN AS REQD FUEL SELECTOR ---------------- AS PER PLACARD
2500 2400 RPM 8.1 GPH 98 KTS 5000 2400 RPM 7.6 GPH 98 KTS 7500 2400 RPM 7.2 GPH 96 KTS 10000 2500 RPM 7.5 GPH 104 KTS
BEFORE LANDING
FUEL SELECTOR ------------------------------- BOTH MIXTURE ---------------------------- RICH AS REQD CARB HEAT ------------------------------------------- ON
AFTER LANDING
CARB HEAT ----------------------------------------- OFF FLAPS ------------------------------------ RETRACTED
STOPPING ENGINE
ELECTRIC & AVIONICS ------------------------- OFF MIXTURE ------------------------------- IDLE CUTOFF MAGNETOS ----------------------------------------- OFF TIME ----------------------------------------------- NOTED MASTER ---------------------------------------------- OFF CONTROL LOCK ------------------------ INSTALLED EFIS ------------------------ INSURE POWER-DOWN
· close flight plan 1-800-992-7433 · Sugarpine Aviators 530-283-2600
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· Maximum allowable gross weight 2200 lbs.
· Empty weight of airplane 1311 lbs
· Useful load (gross weight less empty weight) 889 lbs
· Payload (allowable weight after fuel is topped off. Pilot, passengers & cargo) 663 lbs
· Maximum weight allowed in baggage compartment 120 lbs
· Limit load factor, normal category, flaps up, 3.8, -1.52
· Limit Load factor, utility category, flaps down 3.5
MPH KTS
· Never exceed speed (Vne), red line . . . 160 138
· Caution range (yellow arc on airspeed indicator) ... .. 140-160 122-140
· Normal operating range (Vno) Green arc on airspeed indicator 59-140 51-122
· Maneuvering speed (Va) 115 100
· Flaps operating speed (Vfe) ... ..55-100 48-87
· Best rate of climb speed (Vy) ... 75 65
Best angle of climb speed (Vx) .............. 60 57
· Best glide speed, flaps up . 64 56
· Stall speed power off, flaps up, wings level (VS1) ... ... 58 51
· Stall speed, power off, flaps down, wings level VSO) .... 52 45
· Takeoff distance to clear 50 foot obstacle at 5000 feet MSL: 2455 feet.
· Best rate of climb at sea level: 660 FPM.
· Best rate of climb at 10,000 feet: 240 FPM.
· Service ceiling: 15,000 feet.
· Total usable fuel 37 gallons.
· Recommended fuel octane rating 80/87 or higher.
· For planning: average fuel consumption at cruise power, 8 GPH. 4.6 hours endurance.
· Owners Manual data: 2500 rpm @ 5000 feet MSL = 60% power = 7.6 GPH, 113 MPH, 98 KTS.
· Average no wind ground speed 105 MPH, 91 KTS.
· Oil capacity 8 quarts. Add below 6 quarts. Preferred brand: Aeroshell 15-w 50 or 40w.
· Tire pressures: mains 23 PSI nose wheel 26 PSI.
· Battery 14 VOLTS, type G25. Generator, 35 AMPS. Red generator warning light.
· Engine: Continental 0-300. 145 horsepower. 6 cylinders. Carburetor.
· Magnetos; dual. Brand: Slick.
DYNON EFIS 10-A
ELECTRONIC FLIGHT INFORMATION SYSTEM
CHEAT SHEET
q POWER on/off The unit powers up when master switch is turned on. It automatically powers down within 28 seconds. It can be turned off any time by pressing the left button for 2 seconds. Insure that the unit is off before leaving the airplane.
q BAROMETRIC PRESSURE Press left button to the UNITS toggle. Reset BARO with DEC and INC buttons.
q BUGS Heading: Choose BUGS menu, push SYNC for current heading or TOGGLE then SEL, DEC or INC for another heading.
q VOLTS M = Aircraft battery, E = EFIS external backup battery, I = EFIS internal battery.
q TIMER Left button to TIMER. For elapsed time select UP. To reset press UP/DN button twice.
q DIM Change screen brightness: Press DIM, then BRITR or DARKR.
For more information go to this link:
http://www.dynonavionics.com/docs/D10A_intro.html