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BEECHCRAFT KING AIR B-250 (B-200GT)

Beechcraft King Air 250 · Checklist

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Overview

This document serves as a checklist for the Beechcraft King Air B-250 and B-200GT aircraft. It provides essential operational limitations, emergency procedures, and performance data crucial for pilots operating these aircraft. The checklist is designed to enhance safety and efficiency during flight operations, ensuring that pilots have quick access to critical information. It includes limitations on airspeed, fuel capacity, weights, and specific emergency procedures to follow in various scenarios. This document is intended for pilots and flight crews to ensure compliance with operational standards and to facilitate safe flight operations.

  • Va (Maneuvering Speed): 181 KIAS
  • Maximum Takeoff Weight: 12,500 lbs
  • Usable Fuel Capacity: 3,645 lbs
  • Emergency Descent Airspeed: 181 KIAS
  • Glide Airspeed: 135 KIAS
  • Maximum Cross Wind: 25 KIAS
  • Turbulent Air Penetration Speed: 170 KIAS

Document

Source

Originally published by www.dgac.gob.cl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at www.dgac.gob.cl

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Document details

Type
Checklist
Pages
7
File size
73 KB
Publisher
www.dgac.gob.cl
Documentation completeness
4/7

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In this document

Operational Limitations

This section outlines critical operational limitations for the Beechcraft King Air B-250, including airspeeds (KIAS) such as Va 181, Vmo 259, and Vfe approach 200. It also specifies fuel types (JET-A/JET-A1/JET B) and usable fuel capacity of 3,645 lbs. Weight limitations include maximum ramp weight of 12,590 lbs, maximum takeoff weight of 12,500 lbs, and zero fuel weight of 11,000 lbs.

Emergency Procedures

The emergency procedures section details actions to take in various emergency scenarios. For engine shutdown, the condition lever should be set to FUEL CUTOFF, and the prop lever to FEATHER. In the event of an engine fire on the ground, the same initial steps apply, followed by starting the engine with the starter only. Specific procedures for engine failure during takeoff are also included, with instructions for aborting or continuing the takeoff based on the situation.

Cruise Climb Performance

This section provides cruise climb performance data, indicating KIAS for different altitude ranges. For instance, at sea level to 10,000 feet, the cruise climb speed is 160 KIAS, decreasing to 120 KIAS at 25,000 feet to 30,000 feet.

Emergency Descent and Glide Procedures

Emergency descent procedures require power levers to be set to IDLE, prop levers full forward, and landing gear down, maintaining a maximum airspeed of 181 knots. For glide procedures, the landing gear and flaps should be up, with props feathered and maintaining an airspeed of 135 knots.

Safety notes

  • Always follow emergency procedures as outlined in the checklist.
  • Ensure all weights and balances are within limits before flight.
  • Monitor fuel levels and pressures closely during flight.

Full document text

1 DEPARTAMENTO DE SEGURIDAD OPERACIONAL SUBDEPARTAMENTO “LICENCIAS” “BEECHCRAFT KING AIR B-250 (B-200GT)” MATRÍCULA CC-AFO A.- Limitaciones de Operación 1.- Limitaciones (KIAS) 2.- Combustible (LBS) Va 181 Tipo a Utilizar JET-A/JET-A1/JET B Vmo 259 Capacidad Usable 3.645 Mmo 0.58 Vfe aproach 200 3.- Pesos (LBS) Vfe down 157 Maximum Ramp 12.590 Vlo extension 181 Maximum take off 12.500 Vlo retraction 162 Maximum landing 12.500 Vle 181 Zero fuel wight 11.000 Vmca 92 Max Rear Baggage 510 Vx 100 Vy 125 4.- Starter Limitations Vxse 105 40 SEG ON 60 SEG OFF Vyse 116 40 SEG ON 60 SEG OFF Emergency Descent 181 40 SEG ON 30 MIN OFF Max. range glide 135 Max Cross Wind 25 5.- Cruise Clim (KIAS) Turbulent air penetration 170 SL - 10.000’ 160 10.000 - 20.000’ 140 20.000 - 25.000’ 130 25.000’ - 30.000’ 120 2 1-. EMERGENCY ENGINE SHUTDOWN a.- Affected engine: Condition Lever FUEL CUTOFF Prop Lever FEATHER Firewall Shutoff Valve CLOSE 2-. ENGINE FIRE ON GROUND a.- Affected engine: Condition Lever FUEL CUTOFF Firewall Shutoff Valve CLOSE Ignition and Engine Start STARTER ONLY 3-. ENGINE SHUTDOWN ON THE GROUND Condition Levers FUEL CUTOFF Prop Levers FEATHER Firewall Shutoff Valves CLOSE Master Switch (gang bar) OFF ESIS Power 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 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) VERIFY FEATHER 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 Oxigen Mask (s) DON Mask Selector Switch EMERGENCY Position Mic Swich (s) OXY 10-. ENVIRONMENTAL SYSTEM SMOKE OR FUMES Oxigen Mask (s) DON Mask Selector Switch EMERGENCY Position Mic Swich (s) OXY 11-. AIRSTAIR DOOR OR CARGO DOOR UNLOCKED (DOOR UNLOCKED Annunciator) All Occupants SEATED WITH SEAT BELTS SECURELY FASTENED 5 12-. EMERGENCY DESCENT 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 14-. DUAL GENERATOR FAILURE Generators RESET, THEN ON 15-. USE OF OXYGEN Crew: Oxigen Mask (s) DON Mic Selector Swich (es) OXY 6 16-. PRESSURIZATION LOSS Oxigen Mask (s) DON Mask Selector Switch EMERGENCY Position Mic Swich (s) OXY Passenger Manual Drop Out PULL ON (Pax Oxy On Illuminated) Descend AS REQUIRED 17-. HIGH DIFFERENTIAL PRESSURE (Cabin Differential Pressure Exceeds 6.6 psi) Bleed Air Valves ENVIRONMENT OFF Oxygen (Crew and Passengers) AS REQUIRED Descend AS REQUIRED 18-. AUTO - DEPLOYMENT OXYGEN SYSTEM FAILURE Passenger Manual Drop Out PULL ON 19-. BLEED AIR FAIL Bleed Air Valve (affected engine) PNEU & ENVIR OFF 7 20-. 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 21-. UNSCHEDULED ELECTRIC ELEVATOR TRIM Airplane Attitude MAINTAIN (USING ELEVATOR CONTROL) Control Wheel Disconnect Switch DEPRESS FULLY & HOLD 22-. UNSCHEDULED RUDDER BOOST ACTIVATION Directional control MAINTAIN USING RUDDER PEDALS Rudder boost OFF If condition persist Rudder Bust Circuit Braker Pull

All Beechcraft King Air 250 checklist