Emergency Procedures for Beechcraft King Air E-90
Beechcraft King Air 90 · Emergency Procedures
Overview
This document outlines the emergency procedures for the Beechcraft King Air E-90. It is intended for pilots and crew members operating this aircraft model, providing critical information on how to handle various emergency situations. The procedures include responses to engine failures during take-off, in-flight engine failures, engine fires, and emergency descent protocols. Each section details specific actions to take, ensuring safety and effective management of emergencies. The document serves as a vital reference for maintaining operational safety and efficiency in critical situations.
- Va (Maneuvering Speed): 175 KCAS
- Maximum Take-Off Weight: 10,100 lbs
- Usable Fuel Capacity: 392 US gallons (main), 82 US gallons (auxiliary)
- Emergency Descent Airspeed: 159 KIAS maximum
- Max 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
- Emergency Procedures
- Pages
- 4
- File size
- 17 KB
- Publisher
- www.dgac.gob.cl
Common. Rarer than 8% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Beechcraft King Air 90.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the King Air 90 to your watchlist and track it in one place.
More Beechcraft King Air 90manuals & documents
- King Air MagazinePerformance Data
- AIRCRAFT SERIOUS INCIDENT SHORT REPORTOther Documents
- Garmin G1000Systems Description
- BE90 (C90A) Checklist V 1.4Checklist
- Airworthiness Directive AD/BEECH 90/99 Main Landing Gear Torque KneeOther Documents
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- The Use of an Airborne Air Sampling Platform for Regional Air Quality StudiesOther Documents
If you fly the Beechcraft King Air 90, you may also be researching these.
In this document
Limitations de Operación
This section provides operational limitations for the Beechcraft King Air E-90, including speed limitations such as Va 175 KCAS, Vne 226 KCAS, and Vmo 226 KCAS. It also details fuel capacities, with 392 US gallons usable in the main tanks and 82 gallons in the auxiliary tanks. Maximum take-off weight is specified as 10,100 lbs, with baggage limits of 350 lbs for both forward and aft compartments.
Engine Failure During Take-Off
In the event of an engine failure during take-off, if below take-off speed, the procedure involves reducing power to idle and applying brakes as required. If there is insufficient runway to stop, the condition lever should be cut off, fuel firewall valves closed, and electrical power turned off. If airborne, the power should be set to take-off, landing gear retracted, and the inoperative engine confirmed and feathered.
Engine Failure or Fire in Flight
For an engine failure or fire in flight, the affected engine's power lever should be set to idle, and the propeller lever feathered. The condition lever should be cut off, and the fuel firewall valve closed. If installed, the fire extinguisher should be actuated. The procedure emphasizes maintaining control and executing clean-up for the inoperative engine.
Emergency Descent Procedure
In an emergency descent, power levers should be set to idle, propeller levers to high RPM, and wing flaps set to approach. The landing gear should be extended, and the maximum airspeed for the descent is 159 KIAS.
Safety notes
- Always confirm the inoperative engine before executing clean-up procedures.
- Actuate fire extinguishers only if installed and necessary.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “BEECHCRAFT KING AIR E-90” A.- Limitaciones de Operación 1.- Limitaciones de Velocidad KCAS Va 175 Vb 176 Vne 226 Vmo 226 Vfe 35% 174 Vfo 140 Vle 156 Vlo 156-146 Vmca 10° 88 Vs 88 Vso 76 Vx 102 Vy 112 Vxse 99 Vyse 110 Vloff 97 Vapp (Full Flaps) 140 Max Cross Wind 25 2.- Combustible (U.S. GAL) Tipo a Utilizar JP-1 Principales Usable 392 Auxiliares Usable 82 3.- Pesos (LBS) Máximo TAKE-OFF 10.100 Baggaje FWD 350 Baggaje AFT 350 4.- Starter Limitations 40 Seconds ON 60 Seconds OFF 40 Seconds ON 60 Seconds OFF 40 Seconds ON 30 Minutes OFF 5.- Cruise Clima (KIAS) SL – 10.000 ft 150 10.000 – 20.000 ft 130 20.000 – 25.000 ft 120 25.000 – 31.000 ft 110 2 B.- Emergencies Procedures 1.- ENGINE FAILURE DURING TAKE-OFF a. - Below Take-off Speed: Power IDLE Brakes AS REQUIRED 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 TAKE OFF Propeller RPM HIGH RPM Airspeed MAINTAIN Landing Gear UP Confirm INOPERATIVE ENGINE Propeller Lever (Inoperative Engine) FEATHERED Airspeed BEST RATE OD CLIMB SPEED Clean UP (inoperative engine) EXECUTE 3 2. - ENGINE FAILURE OR FIRE IN FLIGHT a. - Affected Engine: Power lever IDLE Propeller lever FEATHER Condition lever CUT-OFF Fuel Firewall Valve CLOSED Pressurization Bleed Air Valve AS REQUIRED Fire Extinguisher ACTUATE (if installed) Clean UP (inoperative engine) EXECUTE 3. - ENGINE FLAME OUT (2ND 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 Clean UP (inoperative engine) EXECUTE 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 levers IDLE Propeller levers HIGH RPM Wing Flaps APPROACH Landing Gear EXTEND Airspeed 159 KIAS, MAXIMUM