BEECHCRAFT KING AIR A-100
Beechcraft King Air 100 · Emergency Procedures
Overview
This document serves as the Emergency Procedures manual for the Beechcraft King Air A-100, published in 1990. It is designed for pilots operating this aircraft model, providing critical information on handling emergencies that may arise during flight operations. The manual outlines various emergency scenarios, including engine failures, fires, and emergency descent procedures, along with specific actions to take in each situation. Pilots should familiarize themselves with these procedures to ensure safety and effective response in emergencies.
- Maximum Take-Off Weight: 11,500 lbs
- Maximum Cross Wind: 25 knots
- Fuel Capacity: 470 U.S. gallons
- Emergency Descent Airspeed: 156 knots
- Engine Failure Below Take-Off Speed: Power IDLE, Brakes AS REQUIRED
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
- Emergency Procedures
- Year
- 1990
- Pages
- 4
- File size
- 17 KB
- Publisher
- www.dgac.gob.cl
Common. Rarer than 12% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft King Air 100.
- 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
Limitations of Operation
This section details operational limitations for the Beechcraft King Air A-100, including speed limitations such as Va (170 KCAS), Vmo (226 KCAS), and Vne. It also specifies fuel capacity (470 U.S. gallons), usable fuel, and weight limitations, including a maximum take-off weight of 11,500 lbs.
Engine Failure During Take-Off
In the event of an engine failure during take-off, if below take-off speed, pilots should reduce power to idle, apply brakes as required, and use maximum reverse thrust on the operative engine. If airborne, maintain maximum allowable power and feather the propeller of the inoperative engine.
Engine Failure or Fire in Flight
For an engine failure or fire in flight, the affected engine's power lever should be reduced to idle, and the propeller feathered. The condition lever should be set to cut-off, and the fuel firewall valve closed. If a fire extinguisher is installed, it should be actuated.
Emergency Descent Procedure
In an emergency descent, pilots should reduce power to idle, set the propeller to full increase RPM, extend the landing gear, and maintain a maximum airspeed of 156 knots.
Safety notes
- Always confirm the inoperative engine before feathering the propeller.
- Actuate the fire extinguisher if a fire is detected in flight.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “BEECHCRAFT KING AIR A-100” (1990) A.- Limitaciones de Operación 1.- Limitaciones de Velocidad KCAS Va 170 Vb 170 Vne Vmo 226 Vfe 10° Vfo 75 – 140 Vle 156 Vlo 130 Vmca 10° 85 Vs 90 Vso 75 Vx 100 Vy 120 Vsse Vxse 113 Vyse 120 Vr Vplaneo Vapp (Full Flaps) 99 Max Cross Wind 25 2.- Combustible (U.S. GAL) Tipo a Utilizar JP-1 Capacidad Total 470 Combustible Usable Presión de Combustible (PSI) Mínima Máxima 3.- Pesos (LBS) Máximo TAKE-OFF 11.500 Baggaje FWD Baggaje AFT 410 4.- Starter Limitations 40 Seconds ON 60 Seconds OFF 40 Seconds ON 60 Seconds OFF 40 Seconds ON 30 Minutes OFF 2 B.- Emergencies Procedures 1.- ENGINE FAILURE DURING TAKE-OFF a. - Below Take-off Speed: Power IDLE Brakes AS REQUIRED Operative Engine MAXIMUM REVERSE If Insufficient Runway remains for stopping: Condition Lever CUT-OFF Fuel Firewall Valves CLOSED Electrical Power OFF b. - If aircraft is airborne and conditions preclude an immediate landing: Power MAXIMUM ALLOWABLE. Propeller RPM FULL INCREASE Airspeed MAINTAIN Landing Gear UP Confirm INOPERATIVE ENGINE Propeller (Inoperative Engine) FEATHERED Airspeed BEST ANGLE OF CLIMB SPEED Flaps UP Airspeed BEST RATE OD CLIMB SPEED 3 2. - ENGINE FAILURE OR FIRE IN FLIGHT a. - Affected Engine: Power lever IDLE Propeller FEATHER Condition lever CUT-OFF Fuel Firewall Valve CLOSED Bleed Air Valve AS REQUIRED Fire Extinguisher ACTUATE (if installed) 3. - ENGINE FLAME OUT (2ND Engine) a. - Affected Engine: Power lever IDLE Propeller DO NOT FEATHER Condition lever CUT-OFF Conduct AIR START PROCEDURES 4. - ENGINE FAILURE IN FLIGHT BELOW VMCA Reduce Power OPERATIVE ENGINE AS REQUIRED TO MAINTAIN CONTROL Lower Nose TO ACCELERATE ABOVE VMCA Power AS REQUIRED Power lever IDLE (INOPERATIVE ENGINE) Propeller FEATHER Condition lever CUT-OFF 4 5. - ENGINE FIRE ON GROUND a. - Affected Engine: Condition lever CUT-OFF Fuel Firewall Valve CLOSED Starter Switch STARTER ONLY Fire Extinguisher ACTUATE (if installed) 6. – EMERGENCY DESCENT PROCEDURE Power lever IDLE Propeller FULL INCREASE RPM Wing Flaps APPROACH Landing Gear EXTEND Airspeed 156 KNOTS, MAXIMUM