Emergency Procedures for Cessna 402C
CESSNA 402C · Emergency Procedures
Overview
This document outlines the emergency procedures for the Cessna 402C aircraft. It is intended for pilots operating this aircraft, providing critical information on handling various emergency situations. The procedures cover engine failures during takeoff and flight, as well as responses to in-flight fires and emergency descents. Each procedure is designed to ensure the safety of the aircraft and its occupants, detailing specific actions to take under different circumstances.
- Maximum take-off weight: 6850 lbs
- Va: 150 KIAS, Vne: 235 KIAS, Vfe: 180 KIAS
- Engine failure during takeoff requires immediate throttle closure and braking as needed
- In-flight engine fire requires shutting off auxiliary fuel pumps and securing the engine
- Emergency descent involves throttles idle, propellers full forward, and mixtures adjusted for smooth operation
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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
Document
Source
Copy found at www.dgac.gob.cl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Emergency Procedures
- Pages ·
- 5
- File size ·
- 199 KB
- Copy found at ·
- www.dgac.gob.cl
What is the Emergency Procedures for Cessna 402C?
The Emergency Procedures for Cessna 402C is a emergency procedures for the CESSNA 402C.
How many pages is the Emergency Procedures for Cessna 402C?
The copy of the Emergency Procedures for Cessna 402C on file runs 5 pages.
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In this document
Operating Limitations
This section provides essential operating limitations for the Cessna 402C, including airspeeds in knots (KIAS) for various maneuvers such as Va (150 KIAS), Vne (235 KIAS), and Vfe (180 KIAS). It also lists weight limitations, with a maximum take-off weight of 6850 lbs and a maximum baggage weight of 350 lbs. Engine operating limitations include a maximum continuous power of 325 HP and a maximum RPM of 2700.
Engine Securing Procedure
In the event of an engine failure, the procedure begins with closing the throttle, setting the mixture to idle cut-off, and feathering the propeller. This is crucial for securing the inoperative engine and ensuring the safety of the flight.
Engine Failure During Takeoff
If an engine failure occurs during takeoff with speed below 95 KIAS or with the gear down, the pilot must close the throttles immediately and apply brakes or land as required. This quick response is vital for maintaining control of the aircraft.
Engine Failure After Takeoff
For engine failure after takeoff with speed above 91 KIAS, the procedure involves setting the mixtures to full rich, propellers full forward, and throttles full forward, while checking that the landing gear is up. This ensures optimal performance from the operative engine.
In-Flight Engine Fire
In case of an in-flight engine fire, the procedures include turning off both auxiliary fuel pumps, securing the appropriate engine, and feathering the propeller. These steps are critical to managing the emergency and preventing further escalation.
Emergency Descent
The emergency descent procedure involves reducing throttle to idle, setting propellers full forward, and adjusting mixtures for smooth engine operation. The landing gear should be up, and a moderate bank should be initiated to facilitate a controlled descent.
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Safety notes
- Always verify fuel quantity and oil pressure before securing an inoperative engine.
- In case of engine failure, maintain control of the aircraft by adjusting power and pitch as necessary.
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Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” “CESSNA C – 402 C” “CC–COV y CC–CLV” A.- OPERATING LIMITATIONS 1.- Limitations (KIAS) 3.- Weights (LBS) Va 150 Maximum TAKE-OFF 6850 Vne 235 Maximum Baggaje FWD 350 Vfe (Approch 15°) 180 Vle 180 4.- Engine (Maximum Continuous Power) Vno 205 Engine Operating Limitations Vmca 80 Reason HP o BHP 325 Vx 84 Maximum RPM 2700 Vy 109 Vsse 95 Cylinder Head Temperature (°F) Vxse 95 Maximum 460 Vyse 104 Nonmal 200-460 Emergency Descent 149/230 Vapp (Flap DN) 95 Oil Temperature (°F) Max Cross Wind 15 Maximum 240 Normal 75-240 2.- Fuel (U.S. GAL) Type to Use 100-0/100ll Oil Pressure (PSI) Total Capacity 213,4 Maximum 100 Usable Fuel 204,0 Minimum 10 Fuel Pressure (PSI) Maximum 18,5 Minimum 3 2 B.- EMERGENCIES PROCEDURES 1.- ENGINE SECURING PROCEDURE Throttle CLOSE Mixture IDLE CUT–OFF Propeller FEATHER 2.- ENGINE FAILURE DURING TAKEOFF(Speed Below 95 KIAS or Gear Down) Throttles CLOSE INMEDIATELY Brake or Land and Brake AS REQUIRED 3.- ENGINE FAILURE AFTER TAKEOFF (Speed Above 91 KIAS or Up) Mixtures FULL RICH Propellers FULL FORWARD Throttles FULL FORWARD Landing Gear CHECK UP Inoperative Engine: Throttle CLOSE Mixture IDLE CUT–OFF Propeller FEATHER 3 4.- ENGINE FAILURE DURING FLIGHT (Speed Above Vmca) Inoperative Engine DETERMINE Operative Engine ADJUST AS REQUIRED Before Securing Inoperative Engine: Fuel Flow CHECK Fuel Selector MAIN TANKS Fuel Quantity CHECK Oil Pressure and Oil Temperature CHECK Magneto Switch CHECK ON Mixture ADJUST 5.- ENGINE FAILURE DURING FLIGHT (Speed Below Vmca) Rudder APPLY Power REDUCE TO STOP TURN Pitch Attitude LOWER NOSE TO ACELERATE ABOVE Vmca Inoperative Engine Propeller FEATHER Operative Engine INCREASE POWER 4 6.- FIRE ON THE GROUND (Engine Start, Taxi and Takeoff With Sufficient Distance Remaining To Stop) Throttles CLOSE Brakes AS REQUIRED Mixtures IDLE CUT–OFF Battery OFF Magnetos Switch OFF 7.- INFLIGHT WING OR ENGINE FIRE Both Auxiliary Fuel Pumps OFF Operative Engine Fuel Selector MAIN TANK Emergency Crossfeed Shutoff OFF (PULL UP) Appropriate Engine SECURE Throttle CLOSE Mixture IDLE CUT–OFF Propeller FEATHER Fuel Selector OFF 5 8.- EMERGENCY DESCENT a.- Preference Procedure Throttles IDLE Propellers FULL FORWARD Mixtures ADJUST FOR SMOOTH ENGINE OP Wing Flaps UP Landing Gear UP Moderate Bank INITIATE b.- In Turbulence Atmospheric Conditions Throttles IDLE Propellers FULL FORWARD Mixtures ADJUST Wing Flaps DOWN 45º Landing Gear DOWN Moderate Bank INITIATE