Manual cessna 150 (para pilotos)
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For Flight Training Reference OnlyNOTICE
AT THE TIME OF ISSUANCE, THIS INFOR
MATION MANUAL WAS AN EXACT DUPLI CATE OF THE OFFICIAL PILOT'S OPERAT
ING
HANDBOOK AND
FAA APPROVED
AIRPLANE FLIGHT MANUAL AND IS TO BE
USED FOR GENERAL PURPOSES ONLY.
IT WILL
NOT
BE
KEPT
CURRENT AND, BE USED AS A
THEREFORE,
CANNOT
SUBSTITUTE FOR THE OFFICIAL PILOT'S OPERATING HANDBOOK AND FAA
APPROVED AIRPLANE
FLIGHT MANUAL
INTENDED FOR OPERATION OF THE AIR
PLANE.
CESSNA AIRCRAFT COMPANY
1 JULY 1979
For Flight Training Reference Only
INFORMATION MANUAL
CESSNA AIRCRAFT COMPANY
1980 MODEL 152
CESSNA AIRCRAFT COMPANY
M.mb.r of GAMA
1 July 1979
WICHITA, KANSAS, USA iii D1170-13-RPC-1OOOO-12/79
For Flight Training Reference Only
PERFORMANCESPECIFICATIONS
CESSNA MODEL 152
PERFORMANCE - SPECIFICATIONS
*SPEED: Maximum at Sea Level Cruise, 75% Power at 8000 Ft CRUISE: Recommended lean mixture with fuel allowance for engine start, taxi, takeoff, climb and 45 minutes reserve. 110 KNOTS
107 KNOTS
75% Power at 8000 Ft
Range
320 NM
75% Power at 8000 Ft
24.5 Gallons Usable Fuel
. '
Time
Time
Range
3.1 HRS 545 NM 5.2 HRS
415 NM
r
37.5 Gallons Usable Fuel Maximum Range at 10,000 Ft
Range
24.5 Gallons Usable Fuel
Maximum Range at 10,000 Ft 37.5 Gallons Usable Fuel RATE OF CLIMB AT SEA LEVEL
Time
Range Time
5.2 HRS 690 NM
8.7 HRS 715 FPM
14,700 FT
SERVICE CEILING TAKEOFF PERFORMANCE: Ground Roll
Total Distance Over 50-Ft Obstacle LANDING PERFORMANCE: Ground Roll Total Distance Over 50-Ft Obstacle
725 FT
1340 FT
475 FT 1200 FT
n n —
STALL SPEED (CAS):
Flaps Up, Power Off
Flaps Down, Power Off MAXIMUM WEIGHT:
Ramp
48 KNOTS 43 KNOTS
1675 LBS 1670 LBS 1109 LBS 1142 LBS
Takeoff or Landing STANDARD EMPTY WEIGHT:
152 152 II
MAXIMUM USEFUL LOAD:
152
566 LBS 533 LBS
152 II
BAGGAGE ALLOWANCE WING LOADING: Pounds/Sq