BEECHCRAFT KING AIR B100
Beechcraft King Air 100 · Checklist
Overview
This document serves as a checklist for the Beechcraft King Air B100, providing essential operational limitations, emergency procedures, and performance data. It is intended for pilots operating this aircraft model, ensuring they have quick access to critical information necessary for safe flight operations. The checklist includes speed limits, weight specifications, fuel requirements, and emergency procedures for various scenarios, such as engine failure and fire. This structured approach helps pilots maintain compliance with operational standards and enhances safety during flight.
- Max Takeoff Weight (MTOW): 11,800 lbs
- Max Ramp Weight: 11,875 lbs
- Vmo: 223 KIAS, Va: 167 KIAS, Vs: 93 KIAS
- Total Usable Fuel Capacity: 430 U.S. gallons
- Max Demo Cross Wind: 25 knots
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
- 5
- File size
- 157 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
Operational Limitations
This section outlines critical operational limitations for the Beechcraft King Air B100, including speeds in knots indicated airspeed (KIAS) for various phases of flight, temperature limits, and weight specifications. Key speeds include Vmo at 223 KIAS, Va at 167 KIAS, and Vs at 93 KIAS. The maximum ramp weight is 11,875 lbs, with a maximum takeoff weight (MTOW) of 11,800 lbs.
Fuel Requirements
The document specifies fuel types and capacities for the King Air B100. The total usable fuel capacity is 430 U.S. gallons, with Jet A being the recommended fuel type. Emergency fuel options include AVGAS 100 LL and AVGAS 80/87.
Power Limitations
This section details power limitations during various flight conditions, including takeoff, maximum continuous, and cruise settings. For takeoff, the torque is limited to 1,878 lbs-PSI, with ITT at 923 °C and engine speed at 101%. Oil pressure must be maintained between 70-120 PSIG.
Emergency Procedures
Emergency procedures are outlined for scenarios such as hot starts, engine fires, and engine failures during takeoff. For a hot start, pilots must stop the engine if ITT approaches redline and follow specific steps to cool the engine. In case of an engine fire, the checklist provides a sequence of actions to ensure safety, including shutting down fuel and activating fire extinguishers.
Engine Failure Procedures
Procedures for handling engine failure during takeoff and in-flight are detailed. If an engine fails during takeoff, pilots are instructed to abort the takeoff if possible, or to continue with specific power and speed settings if the takeoff is continued. The checklist emphasizes identifying the inoperative engine and managing power accordingly.
Safety notes
- Ensure compliance with speed limits during all phases of flight.
- Follow emergency procedures promptly to ensure safety in critical situations.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” “BEECHCRAFT KING AIR B100” CC-AVS NOMBRE : _____________________________________ FIRMA: _________ FECHA : ____________________ A.- Limitaciones de Operación 1.- Velocidades (KIAS) 3.- Límites de Temperatura Va 167 Temperatura Ambiental (°C) Vmo 223 Mínima a la Partida -40 Vfe - Flaps APP 179 Máxima de Operación ISA +37 - Flaps FULL 153 Mínima de Operación -54 Vle/Vlo 153 Vs 93 4.- Pesos (Libras) Vso 83 Max.Ramp Weight 11.875 Vy 130 MTOW 11.800 Vx 115 MLW 11.210 Vyse 125 MZFW 9.600 Vxse 111 Max. Rear Baggage 410 Vsse 100 Vapp 112 5.- Límites del Starter Max Demo Cross Wind 25 Tiempo ON Tiempo OFF 30 SEGS 1 MIN. 30 SEGS 1 MIN. 30 SEGS 30 MIN 2.- Combustible (U.S. GAL) 6.- Límites de Generadores Tipo a emplear Jet A Engine RPM Loadmeter Capacidad Total Util 430 Ground - 65% 0.80% Combustible de Emergencia Ground - 70% 0.86% AVGAS 100 LL Flight 96-100% 1.00% AVGAS 80/87 2 7.- LIMITACIONES DE POTENCIA COND TORQUE (Lbs-PSI) ITT (°C) ENG SPEED (%) OIL P° (PSIG) OIL T° (°C) Takeoff 1878 923 101 70-120 55-110 Max Cont 1878 923 100.5 70-120 55-110 Cruise 1878 905 96-100 70-120 55-110 Flight Idle 96-100 70-120 55-110 Ground Idle 64-97.5 40-120 -40 Max Rev 923 93 70-120 55-110 Starting 1149 -40 B.- Procedimientos de Emergencias 1.- HOT START ON GROUND (ITT rapidly approaching redline) Engine Start/Stop Switch STOP If ITT not immediately decrease: Fuel Cutoff/Feather Lever FUEL CUTOFF & FEATHER Allow the engine to windmill to a stop. Then, to continue cooling the engine: Start Select Switch CRANK Engine Start/Stop Switch MONETARILY TO START After the RPM reaches 15% or 15 seconds have passed, whichever occurs first: Engine Start/ Stop Switch STOP 3 2. – NACELLE FIRE ON GROUND (ENGINE FIRE WARNING ANNUNCIATOR ILLUMINATED COMBINED WITH VISIBLE SMOKE OR FLAMES, OR ABNORMALLY HOGH FUEL FLOW) Engine Start/ Stop Switches (2) STOP Fuel Cutoff/Feather Levers (2) FUEL CUTOFF & FEATHER Fuel Firewall Valves (2) CLOSED Standby Pumps OFF Battery and Generator Switches OFF Engine Fire Extinguisher ACTUATE Airplane EVACUATE Handheld Fire Extinguisher ACTUATE (as required) 3. - ENGINE FAILURE DURING TAKEOFF- TAKEOFF ABORTED NOTE: This procedure may also be used for an aborted takeoff caused by reasons other than engine failure. Power Levers REVERSE Brakes AS REQUIRED If Insufficient runway remains for stopping: Engine Start/ Stop Switches STOP Battery and Generator Switches OFF Fuel Firewall Valves CLOSED Standby Pumps OFF 4 4. – ENGINE FAILURE DURING TAKEOOF- TAKEOFF CONTINUED CAUTION: For some combinations of airports elevation, OAT, and aircraft weight, a continued takeoff with an engine failure may be impossible. Then only option will be to land straight ahead. Power MAXIMUM (Speed Levers FULL FORWARD) Landing Gear UP Airspeed MAINTAIN TAKEOOF SPEED Inoperative Engine IDENTIFY. (Do not retard power lever) Fuel Cutoff/Feather Lever FUEL CUTOFF & FEATHER Airspeed (at 400´ AGL, minimum) ACCELERATE TO 111 KIAS OR HIGHER Flaps UP Clean-up inoperative engine after reaching at least 1.000 feet AGL 5. – CONFIRMED ENGINE FIRE IN FLIGHT Fuel Cutoff/ Feather Lever FUEL CUTOFF & FEATHER Fuel Firewall Valve CLOSED Fire Extinguisher ACTUATE AS REQUIRED Continue with ENGINE FAILURE IN FLIGHT 5 6. – ENGINE FAILURE IN FLIGHT Power AS REQUIRED Yaw Damp OFF Speed Levers FULL FORWARD Flaps CONSIDERED (UP, if in doubt) Gear CONSIDERED (UP, if in doubt) Inoperative Engine IDENTIFY (Do not retard power lever.) For the inoperative engine: Fuel Cutoff/ Feather Lever FUEL CUTOFF &FEATHER 7. – EMERGENCY DESCENT Oxygen AS REQUIRED Power Levers FLIGHT IDLE Speed Levers FULL FORWARD Flaps APPROACH (179 KTS MAX) Landing Gear DOWN (153 KTS MAX) Airspeed 153 kts.