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Cessna 340 – RAM VII

Cessna 340 · Checklist

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Overview

This document serves as a checklist for the Cessna 340, specifically the RAM VII variant. It outlines operational limitations, emergency procedures, and critical performance data necessary for pilots operating this aircraft. The checklist is designed to assist pilots in ensuring safety and compliance during flight operations, providing essential information on speeds, weights, engine performance, and emergency protocols. It is crucial for pilots to familiarize themselves with these procedures to enhance safety and efficiency during flight.

  • Va (Maneuvering Speed): 159 KIAS
  • Max Takeoff Weight: 6390 lbs
  • Max Landing Weight: 6075 lbs
  • Max Engine RPM: 2700
  • Max Cylinder Head Temperature: 460 °F
  • Emergency Descent Procedure: Throttles Idle, Flaps Down, Moderate Bank 35º-45º
  • Max Crosswind Component: 23 knots

Document

Source

Originally published by www.dgac.gob.cl. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Checklist
Pages
6
File size
28 KB
Publisher
www.dgac.gob.cl
How rare is it?
206Cessna 340 registered worldwide · 182 active

Common. Rarer than 1% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the Cessna 340.

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In this document

Operational Limitations

This section details the operational limitations for the Cessna 340, including critical airspeeds such as Va (159 KIAS), Vne (234 KIAS), and Vno (200 KIAS). It also specifies maximum weights for takeoff (6390 lbs) and landing (6075 lbs), along with engine performance limits such as maximum continuous horsepower (335 HP) and RPM (2700). Fuel specifications and pressure limits are also included.

Emergency Procedures

The emergency procedures section outlines critical actions to take in various scenarios, such as engine failure during takeoff and in-flight emergencies. For instance, in the event of an engine failure during takeoff with speed below 91 KIAS, pilots are instructed to close the throttles immediately and land as required. The procedures also cover actions for both engines failing during cruise flight and in-flight fires.

Engine Performance Limits

This section provides detailed engine performance limits, including maximum cylinder head temperature (460 °F), oil temperature limits (maximum 240 °F, minimum 75 °F), and oil pressure limits (maximum 100 PSI, minimum 10 PSI). It also specifies the type of fuel to be used (100/130) and the total fuel capacity (203 U.S. gallons, with 199 gallons usable).

Safety notes

  • Spin (Flaps UP) Prohibited
  • Ensure proper fuel flow before securing inoperative engine
  • Monitor oil pressure and temperature during flight

Full document text

1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “CESSNA 340 – RAM VII” A.- Limitaciones de Operación 1.- Limitaciones (KIAS) 3.- Pesos (LBS) 4.- Motor (Potencia Máxima Continua) 2.- Combustible (U.S. AL) 5.- Límites de maniobras (Cat. Normal) Va 159 Vne 234 Vno 200 Vfe 15° 160 Vle (extended) 140 Vmca 72 Vs 81 Vso 71 Vx 93 Vy 108 Vsse 93 Vxse 95 Vyse 105 Emergency Descent 234/140 V. balked landing 95 V. app (Flap DN) 95 Max Cross Wind 23 Max TAKE-OFF 6390 Max LANDING 6075 Max Nos eBay + Wing lockers 350 +120 Limitaciones Operativas de Motor Razón HP o BHP 335 Máximas RPM 2700 Temperatura Cabeza de Cilindros (°F) Máxima 460 Mínima 200 Temperatura de aceite (°F) Máxima 240 Mínima 75 Tipo a utilizar 100/130 Capacidad Total STD 203 Combustible Usable STD 199 Presión de aceite (PSI) Máxima 100 Mínima 10 Presión de Combustible (PSI) Máxima 21.7 Mínima 3.0 Escarpados 159 Spin (Flaps UP) Prohibit 2 B.- EMERGENCIES PROCEDURES 1.- ENGINE SECURING PROCEDURE Throttle CLOSED Mixture IDDLE CUT-OFF Propeller FEATHER 2.- ENGINE FAILURE DURING TAKEOFF (Speed Below 91 KIAS or Gear Down) Throttles CLOSE INMEDIATELY Brakes or Land and Brake AS REQUIRED 3.- ENGINE FAILURE DURING TAKEOFF (Speed Above 91 KIAS with Gear Up or In Transit) Mixtures FULL RICH Propellers FULL FORWARD Throttles FULL FORWARD Landing Gear CHECK UP Inoperative Engine : Throttle CLOSE Mixture IDDLE CUT-OFF Propeller FEATHER 3 4.- ENGINE FAILURE DURING FLIGHT (Speed above Vmca) Inoperative Engine DETERMINE Operative Engine ADJUST POWER a.- Before Securing Inoperative Engine : Fuel Flow CHECK, IF DEFICIENT, POS Booster ON Fuel Selector MAIN TANK Fuel Quantity CHECK Oil Pressure and Oil Temperature CHECK Magneto Sw CHECK ON Mixtures ADJUST 5.- ENGINE FAILURE DURING FLIGHT (Speed below Vmca) Rudder APPLY TOWARD OP. ENGINE Power REDUCE TO STOP TURN Pitch Attitude LOWER NOSE Inop. Engine Propeller FEATHER Op Engine INCREASE POWER 4 6.- ENGINE INOPERATIVE GO-AROUND (Speed above 95 KIAS) Throttle FULL FORWARD Mixture RICH Positive Rate-of-climb ESTABLISH Landing Gear UP Wing Flaps UP 7.- BOTH ENGINES FAILURE DURING CRUISE FLIGHT Wing Flaps UP Landing Gear UP Propellers FEATHER 8.- FIRE IN THE GROUND Engine Start, Taxi and Takeoff with sufficient distance and remaining to stop. Throttle CLOSED Brake AS REQUIRED Mixture CUT – OFF Battery OFF (USE GANG BAR) Magneto Sw OFF (USE GANG BAR) 5 9.- IN FLIGHT WING OR ENGINE FIRE Boosters OFF Appropriate Engine SECURE Throttle CLOSE Mixture IDDIE CUT-OFF Propeller FEATHER Fuel Selector OFF Fire Extinguisher ON 10.- EMERGENCY DESCENT PROCEDURES a.- Preference Procedure Throttles IDDIE Propellers FULL FORWARD Mixture RICH Wing Flaps DOWN Landing Gear DOWN Moderate Bank 35º - 45º 6 b.- In Turbulence Atmospheric Conditions Throttles IDDLE Propellers FULL FORWARD Mixture ADJUST Landing Gear DOWN Flaps FULL Moderate Bank INITIATE 11.- AIR INLET OR FILTER ICING EMERGENCY PROCEDURES Alternate Air Control (s) PULL OUT Power INCREASE Mixture (s) LEAN (AS REQUIRED)

Type certificate, explained

What's in the Cessna 340 TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS 3A25Rev 25· Issued 1994
Read the full TCDS

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