Cessna 152

                           Cessna Model 152  aircraft is high-wing monoplanes of all-metal semimonocoque construction and are equipped with fixed tubular spring-steel main gear struts and a steerable nose gear. The nose gear has an air/hydraulic fluidshook strut. Two-place seating is standard, and a double-width, fold-up auxiliary rear seat is optional. Also featured is a “wrap-around” rear window and a sweptback fin and rudder. Powering these aircraft is a four-cylinder. horizontally-opposed air cooled Lycoming “Blue Streak” engine, driving an all-metal fixed-pitch propeller.

GROSS WEIGHT (Takeoff or Landing) …………………….1670 Lbs.

FUEL CAPACITY  Standard Wing (Total) ………………….22.6 Gal

Standard Wing (Usable) …………………………………….. …245 Gal.

Long Range Wing (Total) ……………………………………. ..39 Gal

Long Range Wing (Usable) ……………………………… .. ..37.5 Gal

OIL CAPACITY          Without External Filter ………….. 6 Qt.

                                      With External Filter …………….. 7 Qt.

ENGINE MODEL …………………………………………………. .Lycoming 0-235 Series

PROPELLER (Fixed Pitch) ………………………………. …… 69″ McCauley

MAIN WHEEL TIRES (Optional) ………………………   ….. 6.00 x 6, 4-Ply Rating

                                       Pressure ……………………….    …21 Psi

MAIN WHEEL TIRES (Standard) ……………………..15 x 600 x 6, 4-Ply Rating

                                          Pressure ……… …… ………   …29 Psi

NOSE WHEEL Tire (Standard) …………………………5.00 x 5, 4-Ply Rating

                                               Pressure ………………… …  30 Psi

NOSE GEAR STRUT PRESSURE (Strut Extended)……  20 Psi

WHEEL ALIGNMENT  Camber ………………… ………………. 3 to +5 °

                                           Toe-in ………………………. ….   0″ to + .16″

AILERON TRAVEL       Up …………………………………   20° + 2° – 0

                                            Down …………………….. : ….   15° + 2° – 0

                                          Droop ….. ……………………. + 11°/2 ° Down from streamline

WING FLAP TRAVEL …………………………………… ………….30° 2° Down

RUDDER TRAVEL (Parallel to Water Line)

                                         Right …………………………. 20° 30′ +0 -2°

                                         Left ……. ……………………..20 30′ +0° -2 °

RUDDER TRAVEL (Perpendicular to Hinge Line)

                                         Right ……………………………  23, +00 -20′

                                         Left ……………………………… 23°, +0 -2

ELEVATOR TRAVEL         Up ………..25° 1°       Down … 18° + 1°

ELEVATOR TRIM TAB Up……………. 10 ° 1     Down ….. 20° 1°

PRINCIPAL DIMENSIONS

Wing Span ……….. …………………………………………… 400.00″

Length ………………………………. …………………………… 284.84″

Fin Height (Maximum With Nose Gear Depressed And

Flashing Beacon Installed on Fin) …………………. 102.00″

Track Width ………………………………………………………. 91.28″

Tail Span …………………………………………………………… 120.00″

BATTERY LOCATION …………………………….  FIREWALL Right Side

Author: spsingh

Aircraft Engineer, 39 years aviation experience. Working as Quality Manager. Reading & Writing is my hobby.

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