BEECHCRAFT SUPER KING AIR B-350
Beechcraft King Air 350 · Checklist
Overview
This document serves as a checklist for the Beechcraft Super King Air B-350, providing essential operational limitations, emergency procedures, and performance data for pilots. It is designed to assist flight crews in managing the aircraft safely and effectively during various phases of flight, including normal operations and emergencies. The checklist includes critical speeds, weights, and emergency procedures that are vital for safe operation. Pilots and aviation enthusiasts will find this document useful for understanding the operational capabilities and emergency protocols of the Beechcraft Super King Air B-350.
- Va (Maneuvering Speed): 184 KIAS
- Vmo (Maximum Operating Speed): 263 KIAS
- Maximum Takeoff Weight: 15,000 lbs
- Total Usable Fuel Capacity: 3,611 lbs
- Emergency Descent Airspeed: 184 KIAS
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
- 10
- File size
- 63 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 350.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)Not on file
- Systems & Wiring
- Service BulletinsNot on file
- Type Certificate (TCDS)Not on file
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In this document
Operational Limitations
This section outlines key operational limitations for the Beechcraft Super King Air B-350, including speeds such as Va (184 KIAS), Vmo (263 KIAS), and Vfe (202 KIAS for approach, 158 KIAS for full down). Fuel capacity is detailed, with a total usable fuel of 3,611 lbs, and maximum weight limits including ramp weight (15,100 lbs), takeoff weight (15,000 lbs), and landing weight (15,000 lbs).
Emergency Procedures
This section provides detailed emergency procedures for various scenarios, including engine fire or failure in flight, on the ground, and during takeoff. For an engine fire in flight, the checklist includes steps such as moving the condition lever to fuel cutoff and actuating the fire extinguisher if necessary. Each emergency procedure is clearly outlined to ensure pilots can respond quickly and effectively.
Starter Limitations
The checklist specifies starter limitations for the Beechcraft Super King Air B-350, indicating that the starter can be operated for 30 seconds with a 5-minute cooldown period, or 30 seconds with a 30-minute cooldown period for emergency situations.
Engine Failure Procedures
Procedures for handling engine failures during takeoff and in flight are detailed, including actions to take at or below V1, and maintaining control above Vmc. The checklist emphasizes the importance of maintaining airspeed and verifying propeller feathering for the inoperative engine.
Glide and Emergency Descent
The glide procedure specifies maintaining an airspeed of 135 KIAS with landing gear and flaps up, while the emergency descent procedure outlines steps to take, including reducing power levers to idle and configuring flaps for approach.
Safety notes
- Always follow checklist procedures for emergency situations to ensure safety.
- Maintain awareness of operational limitations to prevent exceeding aircraft capabilities.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “BEECHCRAFT SUPER KING AIR B-350” SERVICIOS AEREOS Y TERRESTRES “AVIASUR” A.- Limitaciones de Operación 1.- Limitaciones (KIAS) 2.- Combustible (LBS) Va 184 Tipo a Utilizar JET A-1 Vmo 263 Capacidad Total Usable 3.611 Mmo (Mach) 0.58 Each Main Fuel Tank System 1.273 llbslbs Vle 184 Each AUX Fuel tank 533 Vlo extensión 184 Max Fuel imbalance 300 Vlo retraction 166 Vfe Approach 202 Vfe Full Down 158 3.- Pesos (LBS) Vmca Flaps Up 94 Máximo RAMP 15.100 Vmca Flaps Approach 93 Máximo TAKE-OFF 15.000 Vso 81 Máximo LANDING 15.000 Vs1 Max W. Flaps 89 Máximo Zero Fuel Weight 12.500 Vs1 Max W. Flaps Up 96 Vx 125 Vy 140 4.- Starter Limitations Vxse 125 30 SEC ON 05 MIN OFF Vyse 125 30 SEC ON 05 MIN OFF Venr 125 30 SEC ON 30 MIN OFF Emergency Descent 184 Max Range Glide 135 Max.Demo.Crosswind 20 2 B.- Emergency Procedures 1. ENGINE FIRE OR FAILURE IN FLIGHT Affected Engine: 1. Condition Lever............................................................................FUEL CUTOFF 2. Prop Lever.....................................................................................FEATHER 3. Firewall Fuel Valve.......................................................................CLOSE 4. Fire Extinguisher (if fire warning persists)................................ACTUATE 5. Checklist 2. ENGINE FIRE ON GROUND Affected Engine: 1. Condition Lever...........................................................................FUEL CUTOFF 2. Firewall Fuel Valve......................................................................CLOSE 3. Starter Switch..............................................................................STARTER ONLY 4. Fire Extinguisher (If Fire Warning Persists)............................ACTUATE 3 3. EMERGENCY ENGINE SHUTDOWN ON THE GROUND 1. Condition Levers…………………………………………………….FUEL CUTOFF 2. Prop Levers………………………………………………………..…FEATHER 3. Firewall Fuel Valves……………………….………………………..CLOSE 4. Master Switch (gang bar)…………………………………………...OFF 5. Battery Bus……………………………………………….…………..EMERG OFF 6. ESIS Power…………………………………………………………...OFF 4. ENGINE FAILURE DURING TAKEOFF (AT OR BELOW V1) - TAKE OFF ABORTED 1. Power levers................................................................................GROUND FINE 2. Brakes..........................................................................................MAXIMUM 5. ENGINE FAILURE DURING TAKEOFF (AT OR ABOVE V1) - TAKEOFF CONTINUED 1. VR Speed.......................ROTATE TO APPROXIMATELY 10º PITCH ATTITUDE 2. Landing Gear (when positive climb established).........................................UP 3. Airspeed...............................................................MAINTAIN V2 TO 400 FT AGL 4. Propeller (inoperative engine).........................................VERIFY FEATHERED 5. Checklist 4 6. ENGINE FAILURE IN FLIGHT BELOW AIR MINIMUM CONTROL SPEED (Vmca) 1. Power.................................REDUCE AS REQUIRED TO MAINTAIN CONTROL 2. Nose....................................LOWER TO ACCELERATE ABOVE Vmca 3. Checklist 7. ELECTRICAL SMOKE OR FIRE 1. Oxygen Mask(s)………………….……………………………. DON 2. Mask Selector Switch…………………………………………..EMERG 3. Mic Switch (es)………………………………………………….OXY 4. Checklist 8. ENVIRONMENTAL SYSTEM SMOKE OR FUMES 1. Oxygen Mask(s)………………….……………………………. DON 2. Mask Selector Switch…………………………………………..EMERG 3. Mic Switch (es)………………………………………………….OXY 4. Checklist 5 9. AIRSTAIR DOOR/CARGO DOOR UNLOCKED If the [DOOR UNLOCKED] Illuminates, Or if An Unlatched Airstair Door/Cargo Door Is Suspected: 1. All occupants...............SEATED WITH SEAT BELTS SECURELY FASTENED 2. Checklist 10. EMERGENCY DESCENT 1. Power Levers...........................................................................IDLE 3. Prop Levers.............................................................................FULL FORWARD 4. Flaps (202 Knots maximum)..................................................APPROACH 5. Landing Gear (184 Knots maximum)....................................DOWN 6. Airspeed...................................................................................184 KNOTS MAXIMUM 11. GLIDE 1. Landing Gear...................................................................................UP 2. Flaps..................................................................................................UP 3. Prop Levers…..................................................................................FEATHERED 4. Airspeed............................................................................................135 KNOTS 5. Checklist 6 12. DUAL GENERATOR FAILURE 1. Instrument Emergency Lights (if required)……….……… ON 2. Generators…………..……………………………………………RESET, THEN ON If Either Generator Will Reset: 3. Operating Generator Loadmeter………………….……………………MONITOR If Neither Generator Will Reset: 4. ECS Mode…………………………………………………..………………… OFF 5. Cockpit/Cabin Blower…………………………………………………………AUTO 6. Non-essential equipment…………………………………………………….OFF 7. Checklist 13. USE OF OXYGEN Crew 1. Oxygen Mask (s)……………………………………………………………DON 2. Mic Switch (es)......................................................................................OXY 3. Checklist 14. RESSURIZATION LOSS 1. Oxygen Mask (s)…………………………………………………… DON 2. Mic Switch (es)..............................................................................OXY 3. Passenger Manual Drop-Out........................................................PULL ON 4. Descend…………………………………………..……………………AS REQUIRED 5. Checklist 7 15. HIGH DIFFERENTIAL PRESSURE 1. Bleed Air Valves…………………………………………………..ENVIR OFF 2. Oxygen (crew and passengers)……………………………… AS REQUIRED 3. Descend…………………………………………………………….AS REQUIRED 16. AUTO-DEPLOYMENT OXYGEN SYSTEM FAILURE 1. Passenger Manual Drop-Out................................................................PULL ON 2. Checklist 17. BLEED AIR FAIL
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1. Bleed Air valve (Affected engine)......................................PNEU & ENVIR OFF 2. Checklist 18. SPINS 1. Control Column.................................FULL FORWARD, AILERONS NEUTRAL 2. Full Rudder........................................OPPOSITE THE DIRECTION OF SPIN 3. Power Levers......................................IDLE 4. Rudder................................................NEUTRALIZE WHEN ROTATION STOPS 5. Execute a smooth pullout 8 19. UNSCHEDULED ELECTRIC PITCH TRIM ACTIVATION 1. Airplane Attitude…..........................MAINTAIN USING ELEVATOR CONTROL 2. AP / Trim Disconnect…...................DEPRESS FULLY & HOLD 3. Checklist 20. UNSCHEDULED RUDDER BOOST ACTIVATION 1. AP / Trim Disconnect…..........................DEPRESS TO 1ST LEVEL AND HOLD 2. Rudder Boost….......................................OFF If Condition Persists: 3. YD / AP DISC (on Flight Guidance Panel)……………………….…PULL DOWN 4. Checklist 21. AUTOPILOTS FAILURES 1. Flight Controls…..........................................................................HOLD FIRMLY (control forces may exceed 25 pounds) 2. AP…..................................................................................................DISENGAGE 3. Checklist 9 22. AUTOPILOTS TRIM FAIL (TRIM) 1. Flight Controls…..........................................................................HOLD FIRMLY 2. AP…...............................................................................................DISENGAGE 3. Checklist 23. AUTOPILOTS AUTOMATIC DISENGAGEMENT If An Automatic Disengagement Occurs: 1. Maintain Airplane Controls. 2. AP / TRIM Disconnect…............DEPRESS TO 1ST LEVEL TO CANCEL HORN 3. Checklist 10 24. ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) GPWS WARNING (Red [GPWS] on PFD and Continuous “PULL UP, PULL UP” Voice Warning) Or EGPWS TERRAIN WARNING (Red [GPWS] on PFD and “TERRAIN,TERRAIN, PULL UP” or “OBSTACLE, OBSTACLE, PULL UP” Voice Warning) In IMC or at Night: 1. Wings………………………………………………………..LEVEL 2. Power…..........................................................................MAX ALLOWABLE 3. Pitch…………………………………………………………INCREASE Promptly and smoothly increase pitch towards an initial pitch attitude of 20º - 25º. Adjust as required to avoid continuous buffeting and /or stall warning. Adjust to maintain 125 KIAS. 4. Gear and Flaps…………………………………………….UP 5. Checklist