BEECHCRAFT SUPER KING AIR B200/B200C
Beechcraft King Air 200 · Checklist
Overview
This document serves as a checklist for the Beechcraft Super King Air B200 and B200C models. It outlines operational limitations, emergency procedures, and critical operational data necessary for pilots to safely operate the aircraft. The checklist is designed for use during various phases of flight, including takeoff, in-flight emergencies, and landing. It provides essential information on airspeeds, weights, and emergency protocols, ensuring that pilots are well-prepared for both normal and abnormal situations. The document is crucial for maintaining safety and efficiency in flight operations.
- Va (Maneuvering Speed): 181 KIAS
- Maximum Takeoff Weight: 12,500 lbs
- Fuel Capacity: 544 U.S. gallons
- Vmo (Maximum Operating Speed): 259 KIAS
- Emergency procedures for engine failure include setting condition levers to fuel cutoff and feathering the prop lever.
Document
Source
Originally published by www.dgac.gob.cl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Checklist
- Pages
- 8
- File size
- 29 KB
- Publisher
- www.dgac.gob.cl
Common. Rarer than 17% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft King Air 200.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Operational Limitations
This section details the operational limitations for the Beechcraft Super King Air B200/B200C, including airspeeds (KIAS) and fuel capacity. Key values include: Va (Maneuvering Speed) at 181 KIAS, Vb (Design Maneuvering Speed) at 170 KIAS, Vmo (Maximum Operating Speed) at 259 KIAS, and Mmo (Maximum Mach) at 0.52. The total fuel capacity is 544 U.S. gallons.
Emergency Procedures
This section outlines critical emergency procedures for various scenarios, including engine failure and fire. For an engine failure in flight, the affected engine's condition lever should be set to fuel cutoff, and the prop lever should be feathered. In case of an engine fire on the ground, the same initial steps apply, with the addition of using the starter only for ignition. The document provides detailed steps for handling emergencies effectively.
Weights and Balances
The maximum takeoff weight for the Beechcraft Super King Air B200/B200C is 12,500 lbs, with a maximum landing weight also at 12,500 lbs. The maximum zero fuel weight is 11,000 lbs. These weights are critical for ensuring safe flight operations and compliance with regulatory requirements.
Safety notes
- Always ensure that all occupants are seated with seat belts securely fastened during flight.
- In case of an engine failure during takeoff at or below V1, abort the takeoff immediately.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “BEECHCRAFT SUPER KING AIR B200/B200C” A.- Limitaciones de Operación 1.- Limitaciones (KIAS) 2.- Combustible (U.S. GAL) Va 181 Tipo a Utilizar JET A-1 Vb 170 Capacidad Total 544 Vmo 259 Mmo (Mach) 0.52 Vfe Approach 40% 200 3.- Pesos (LBS) Vfe Full Down 100% 157 Máximo TAKE-OFF 12500 Vmca (Hartzell) 86 Máximo LANDING 12500 Vs 99 MAX ZFW 11000 Vso 75 Vx 100 Vy 125 4.- Starter Limitations Vyse 121 40 SEC ON 60 SEC OFF 60 SEC V1 95 40 SEC ON 60 SEC OFF 60 SEC Vapp 103 40 SEC ON 30 MIN OFF 30 MIN Max Cross Wind 25 2 B.- Emergencies Procedures 1-. ENGINE FAILURE IN FLIGHT OR FIRE IN FLIGHT a.- Affected engine: Condition Lever FUEL CUTOFF Prop Lever FEATHER Firewall Shutoff Valve CLOSE Fire Extinguisher (if installed) (if fire warning persists) ACTUATE 2-. ENGINE FIRE ON GROUND a.- Affected engine: Condition Lever FUEL CUTOFF Firewall Shutoff Valve CLOSE Ignition and Engine Start STARTER ONLY b.- If Fire Warning Persists: Fire Extinguisher (if installed) ACTUATE 3-. ENGINE SHUTDOWN ON THE GROUND Condition Levers FUEL CUTOFF Prop Levers FEATHER Firewall Shutoff Valves CLOSE Master Switch (gang bar) OFF 3 4-. ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) TAKEOFF ABORTED Power levers GROUND FINE Brakes AS REQUIRED TO ACHIEVE STOPPING DISTANCE Operative engine MAXIMUM REVERSE a.- If insufficient runway remains for stopping: Condition Levers FUEL CUTOFF Firewall Shutoff Valves CLOSE Master switch OFF (Gang bar down) 5-. ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) TAKEOFF CONTINUED Power MAXIMUM ALLOWABLE Airspeed MAINTAIN (take-off speed or above) Landing Gear UP Prop Lever (inoperative engine) FEATHER (or verify FEATHERED if autofeather is installed) Airspeed (After obstacle clearance altitude is reached) Vyse 6-. ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (VMCA) Power REDUCE AS REQUIRED TO MAINTAIN CONTROL Nose LOWER TO ACCELERATE ABOVE VMCA 4 7-. ENGINE FLAMEOUT (2ND ENGINE) Power Lever IDLE Prop Lever DO NOT FEATHER Condition Lever FUEL CUTOFF Conduct Air Start Procedures in ABNORMAL PROCEDURES 8-. FUEL PRESSURE LOW (L or R FUEL PRESS ANNUNCIATOR) Standby Pump (failed side) ON 9-. ELECTRICAL SMOKE OR FIRE Oxygen System Ready CONFIRM ON Crew (Diluter Demand Masks) DON MASKS Mask Selector Switch EMERGENCY Position Mic Selector OXYGEN MASK Audio Speaker ON 10-. ENVIRONMENTAL SYSTEM SMOKE OR FUMES Oxygen System Ready CONFIRM ON Crew (Diluter Demand Masks) DON MASKS Mask Selector Switch EMERGENCY Position Mic Selector OXYGEN MASK Audio Speaker ON 5 11-. CABIN OR CARGO DOOR UNLOCKED (DOOR UNLOCKED Annunciator) All Occupants SEATED WITH SEAT BELTS SECURELY FASTENED 12-. EMERGENCY DESCENT Oxygen CREW REQUIRED (Passengers as required) Oxygen System Ready CONFIRM ON Crew (Diluter Demand Masks) DON MASKS Mic Selector OXYGEN MASK Audio Speaker ON Passenger Manual Drop Out PULL ON Passengers PULL LANYARD PIN, DON MASK Power Levers IDLE Prop Levers FULL FORWARD Flaps APPROACH Landing Gear DOWN Airspeed 181 KNOTS MAXIMUM 13-. GLIDE Landing Gear UP Flaps UP Props FEATHERED Airspeed 135 KNOTS 6 14-. INVERTER INOPERATIVE (INVERTER Annunciator) Select THE OTHER INVERTER. 15-. DUAL GENERATOR FAILURE Generators RESET, THEN ON a.- If Either Generator Will Reset: Operating Generator Loadmeter DO NOT EXCEED 100% (88% above 31,000 feet) 16-. UNSCHEDULED ELECTRIC ELEVATOR TRIM Airplane Attitude MAINTAIN (Using elevator control) Control Wheel Disconnect Switch FULLY DEPRESS 2nd level, ELECT TRIM OFF Annunciator ILLUMINATED 17-. UNSCHEDULED RUDDER BOOST ACTIVATION Directional control MAINTAIN USING RUDDER PEDALS Rudder boost OFF 7 18-. USE OF OXYGEN Cabin Pressure Altitude TUC Oxygen System Ready CONFIRM ON Crew (Diluter Demand Masks) DON MASKS Mic Selector OXYGEN MASK Audio Speaker ON Passenger Manual Drop Out PULL ON Passengers PULL LANYARD PIN, DON MASK 19-. PRESSURIZATION LOSS (ALT WARN Annunciator) Oxygen Oxygen System Ready CONFIRM ON Crew (Diluter Demand Masks) DON MASKS Mic Selector OXYGEN MASK Audio Speaker ON Passenger Manual Drop Out PULL ON Passengers PULL LANYARD PIN, DON MASK Descend AS REQUIRED 20-. AUTO - DEPLOYMENT OXYGEN SYSTEM FAILURE (ALT WARN Annunciator Illuminated y PASS OXY ON Annunciator Not Illuminated) Passenger Manual Drop Out PULL ON 8 21-. HIGH DIFFERENTIAL PRESSURE (Cabin Differential Pressure Exceeds 6.6 psi) Bleed Air Valves ENVIRONMENT OFF Oxygen (Crew and Passengers) AS REQUIRED Descend AS REQUIRED 22-. BLEED AIR LINE FAILURE (L or R BL AIR FAIL Annunciator) Bleed Air Valve (Affected Engine) INST & ENVIRONMENT OFF [L BL AIR OFF] or [R BL AIR OFF]-ILLUMINATED 23-. SPINS Control Column FULL FORWARD AILERONS NEUTRAL Full Rudder OPPOSITE THE DIRECTION OF SPIN Power Levers IDLE Rudder NEUTRALIZE WHEN ROTATION STOPS Execute a Smooth Pullout