DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES
“BEECHCRAFT SUPER KING AIR B200/B200C”
NOMBRE : ______FIRMA: ______
FECHA : ______
A.- Limitaciones de Operación
1.- Limitaciones (KIAS) 2.- Combustible (U.S. GAL) Va Tipo a Utilizar Vb Capacidad Total Vmo Mmo (Mach) Vfe Approach 40% 3.- Pesos (LBS) Vfe Full Down 100% Máximo TAKE-OFF Vmca (Hartzell) Máximo LANDING Vs MAX ZFW Vso Vx Vy 4.- Starter Limitations Vyse V1 Vapp Max Cross Wind
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B.- Emergencies Procedures
1-. ENGINE FAILURE IN FLIGHT OR FIRE IN FLIGHT
a.- Affected engine: Condition Lever ______Prop Lever ______Firewall Shutoff Valve ______Fire Extinguisher (if installed) (if fire warning persists) ______
2-. ENGINE FIRE ON GROUND
a.- Affected engine: Condition Lever ______Firewall Shutoff Valve ______Ignition and Engine Start ______
b.- If Fire Warning Persists: Fire Extinguisher (if installed) ______
3-. ENGINE SHUTDOWN ON THE GROUND
Condition Levers ______Prop Levers ______Firewall Shutoff Valves ______Master Switch (gang bar) ______
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4-. ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) TAKEOFF ABORTED
Power levers ______Brakes ______Operative engine ______
a.- If insufficient runway remains for stopping: Condition Levers ______Firewall Shutoff Valves ______Master switch ______
5-. ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) TAKEOFF CONTINUED
Power ______Airspeed ______Landing Gear ______Prop Lever (inoperative engine) ______(or verify FEATHERED if autofeather is installed) Airspeed (After obstacle clearance altitude is reached) ______
6-. ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (VMCA)
Power ______Nose ______
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7-. ENGINE FLAMEOUT (2ND ENGINE)
Power Lever ______Prop Lever ______Condition Lever ______Conduct Air Start Procedures in ABNORMAL PROCEDURES
8-. FUEL PRESSURE LOW (L or R FUEL PRESS ANNUNCIATOR)
Standby Pump (failed side) ______
9-. ELECTRICAL SMOKE OR FIRE
Oxygen System Ready ______Crew (Diluter Demand Masks) ______Mask Selector Switch ______Mic Selector ______Audio Speaker ______
10-. ENVIRONMENTAL SYSTEM SMOKE OR FUMES Oxygen System Ready ______Crew (Diluter Demand Masks) ______Mask Selector Switch ______Mic Selector ______Audio Speaker ______
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11-. CABIN OR CARGO DOOR UNLOCKED (DOOR UNLOCKED Annunciator)
All Occupants ______
12-. EMERGENCY DESCENT
Oxygen ______(Passengers as required) Oxygen System Ready ______Crew (Diluter Demand Masks) ______Mic Selector ______Audio Speaker ______Passenger Manual Drop Out ______Passengers ______Power Levers ______Prop Levers ______Flaps ______Landing Gear ______Airspeed ______
13-. GLIDE Landing Gear ______Flaps ______Props ______Airspeed ______
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14-. INVERTER INOPERATIVE (INVERTER Annunciator)
Select ______
15-. DUAL GENERATOR FAILURE
Generators ______
a.- If Either Generator Will Reset: Operating Generator Loadmeter ______
16-. UNSCHEDULED ELECTRIC ELEVATOR TRIM
Airplane Attitude ______) Control Wheel Disconnect Switch ______2nd level, ELECT TRIM OFF Annunciator ______
17-. UNSCHEDULED RUDDER BOOST ACTIVATION
Directional control ______Rudder boost ______
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18-. USE OF OXYGEN
Cabin Pressure Altitude ______Oxygen System Ready ______Crew (Diluter Demand Masks) ______Mic Selector ______Audio Speaker ______Passenger Manual Drop Out ______Passengers ______
19-. PRESSURIZATION LOSS (ALT WARN Annunciator)
Oxygen Oxygen System Ready ______Crew (Diluter Demand Masks) ______Mic Selector ______Audio Speaker ______Passenger Manual Drop Out ______Passengers ______Descend ______
20-. AUTO - DEPLOYMENT OXYGEN SYSTEM FAILURE (ALT WARN Annunciator Illuminated y PASS OXY ON Annunciator Not Illuminated)
Passenger Manual Drop Out ______
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21-. HIGH DIFFERENTIAL PRESSURE (Cabin Differential Pressure Exceeds 6.6 psi)
Bleed Air Valves ______Oxygen (Crew and Passengers) ______Descend ______
22-. BLEED AIR LINE FAILURE (L or R BL AIR FAIL Annunciator)
Bleed Air Valve (Affected Engine) ______[L BL AIR OFF] or [R BL AIR OFF]-ILLUMINATED
23-. SPINS
Control Column ______Full Rudder ______Power Levers ______Rudder ______Execute a Smooth Pullout
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