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1075 (L. Flaps Up Power Off. 55 mph. Flaps Down
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION
28 mar. 2008 Cessna Aircraft Company. P.O. Box 7704. Wichita Kansas 67277. I - Model 150
On Centerline Aviation
This C-150L is a wonderful example of the Cessna line. This aircraft is reliable inexpensive to operate and a great way to build hours.
Airworthiness Directive Schedule - Aeroplanes Cessna 150 and 152
29 sept. 2011 This AD schedule is applicable to Cessna aircraft manufactured under the ... 150L. FAA TC No. 3A19. 150M. FAA TC No. 3A19. A150K. FAA TC No.
CESSNA_150_POH.pdf
Cessna. 150 COMMUTER. 1977 MODEL 150M. Serial No. Registration No. MIL-L-6082 Aviation Grade Straight Mineral Oil: Use to replenish.
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION
Cessna Aircraft Company. P.O. Box 7704. Wichita Kansas 67277. I - Model 150
Type Acceptance Report - Cessna 150/152 Series
New Zealand Type Acceptance has been granted to the Cessna 150/152 and Structural Materials Summary – Revision L (Includes Memo 80M2/7-4 which lists.
P691-12
1 mar. 1996 Cessna. A Textron Company. Illustrated Parts Catalog. 1970 ... 150L. 15073659. 15074850. 150 COMMUTER II. 1974. 150L. 15074851. 15075781.
“CESSNA 150 L” CC-SAC “CLUB AÉREO DE ANGOL”
“CESSNA 150 L”. CC-SAC. “CLUB AÉREO DE ANGOL”. NOMBRE : FIRMA: ______. FECHA. : A.- Limitaciones de Operación. 1.- Limitaciones (Velocidades).
“CESSNA C-150L”
DEPARTAMENTO “SEGURIDAD OPERACIONAL”. SUBDEPARTAMENTO “LICENCIAS”. SECCIÓN EVALUACIONES. “CESSNA C-150L”. A.- Limitaciones de Operación.
DEPARTAMENTO "SEGURIDAD OPERACIONAL"
SUBDEPARTAMENTO "LICENCIAS"
SECCIÓN EVALUACIONES
"CESSNA C-150L"A.- Limitaciones de Operación
1.- Limitaciones (Velocidades)
MPHVa 109
Vne 162
Vno 120
Vfe 100
Vs 55Vso 48
Vx 70 Vy 76 Vr 55Vapp (Flap DN) 60 - 70
Vplaneo 70 - 80
Max Cross Wind 15
2.- Combustible (U.S. GAL)
Tipo a Utilizar 100/130
Capacidad Total 26
Combustible Usable 22,5
Presión de Combustible (PSI)
Mínima Red line
Máxima Red line
3.- Pesos (LBS)
Máximo TAKE-OFF 1.600
Máximo Equipaje 120
4.- Motor (Potencia Máxima Continua)
Limitaciones Operativas de Motor
Razón HP o BHP 100
Máximas RPM 2.750
RPM estáticas
Máximas 2.550
Mínimas 2.000
Temperatura de aceite (°F)
Máxima 240
Mínima Red line
Presión de aceite (PSI)
Máxima 100
Mínima 10
5.- Limites de maniobras (Cat. Normal)
MANIOBRA MPH
Spin (Flaps UP) Show Deceleration
Escarpados 109
Ocho Flojo 109
Chandela 109
2B.- Emergency Procedure
1.- ENGINE POWER LOSS DURING TAKEOFF (Not Airborne)
a.- Sufficient runaway remaining:Throttle CLOSE IMMEDIATELY
Brakes APPLY AS REQUIRED
Stop STRAIGHT AHEAD
b.- Insufficient runaway remaining:Throttle CLOSE IMMEDIATELY
Brakes APPLY AS REQUIRED
Mixture IDLE CUT-OFF
Fuel selector OFF
Master switch OFF
Magnetos OFF
Directional Control MAINTAIN - Maneuver to avoid obstacles. 32. - ENGINE POWER LOSS DURING TAKEOFF (if Airborne)
a.- Sufficient runaway remaining:Airspeed MAINTAIN ABOVE STALL (70 MPH)
Directional control MAINTAIN
Land STRAIGHT AHEAD
b.- Insufficient runaway remaining:Airspeed MAINTAIN ABOVE STALL (70 MPH)
Throttle CLOSE
Mixture IDLE CUT-OFF
Fuel selector OFF
Flaps AS REQUIRED
Master Switch OFF
Magnetos OFF
Directional Control MAINTAIN - Make only shallow turns to avoid obstacles.3. ENGINE FAILURE IN FLIGHT
Speed 70 MPH
Fuel selector BOTH
Mixture FULL RICH
Primer SECURE
Magnetos CHECK
44. ENGINE FIRE DURING START ON GROUND
Starter CONTINUE CRANKING
a.- If the start is successful:Engine 1700 RPM FOR A FEW MINUTES
Before shutting it down to inspect damage.
b.- If engine start is unsuccessful:Continue CRANKING FOR TWO OR THREE MINUTES
Throttle FULL OPEN
When ready to extinguish fire,
Starter RELEASE
Master switch OFF
Ignition switch OFF
Fuel shutoff valve OFF
Fire Damage INSPECT
5. ENGINE FIRE IN FLIGHT
Mixture control IDLE CUT-OFF
Fuel shutoff valve OFF
Master switch OFF
Establish a glide 100 MPH
Cabin heat control CLOSE
Select a field FORCED LANDING
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