Cessna C-404 Checklist
Cessna 404 Titan · Checklist
Overview
This document serves as a checklist for the Cessna 404 Titan, detailing operational limitations, emergency procedures, and performance specifications. It is intended for pilots operating the Cessna 404, providing essential information for safe flight operations. The checklist includes critical speed limitations, weight capacities, fuel specifications, and engine operational limits, as well as emergency procedures for various in-flight scenarios. This resource is crucial for ensuring compliance with safety protocols and enhancing pilot preparedness during flight.
- Va (Maneuvering Speed): 160 KIAS
- Maximum Take-Off Weight: 8,400 lbs
- Maximum Landing Weight: 8,100 lbs
- Fuel Capacity: Total 348 U.S. gallons, Usable 344 U.S. gallons
- Maximum Continuous Engine Power: 375 HP at 2,235 RPM
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
- 38 KB
- Publisher
- www.dgac.gob.cl
Common. Rarer than 5% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 404 Titan.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the 404 Titan to your watchlist and track it in one place.
More Cessna 404 Titanmanuals & documents
See all 24 →- TDS GTNXi Flight Simulator User’s Manual for Flight Simulator 2020 and 2024Checklist
- Fumes event involving Cessna 404, VH-LADOther Documents
- Controlled flight into terrain involving Cessna 404, VH-OZOOther Documents
- AHAC-INCID-01-2019, CESSNA 404 TITAN MATRICULA HR-AYDAirworthiness Directives
- Type Acceptance Report TAR 8/21B/8 – Cessna 404Other Documents
- Notice of Proposed Amendment 2017-03Supplemental Type Certificate
- Cessna Flyer May 2016Other Documents
- Auxiliary Aircraft Facility Maintenance StandardsType Certificate
- Cessna 404 Systems DescriptionSystems Description
- Engine-driven fuel pump – material substitutionOther Documents
- Airworthiness Directive Schedule Aeroplanes Cessna 404 SeriesAirworthiness Directives
- AAIB Bulletin: 6/2007 G-OOSI EW/A2006/12/02Other Documents
If you fly the Cessna 404 Titan, you may also be researching these.
In this document
Operational Limitations
This section outlines the operational limitations for the Cessna 404, including critical speeds such as Va (160 KIAS), Vne (241 KIAS), and Vso (70 KIAS). It also specifies maximum take-off weight (8,400 lbs) and landing weight (8,100 lbs), along with fuel capacity details (total 348 U.S. gallons, usable 344 U.S. gallons).
Engine Specifications
The engine specifications detail the maximum continuous power output of 375 HP, with maximum RPM set at 2,235. It also provides temperature limits for cylinder head (460°F max, 200°F min) and oil (240°F max, 100°F min), as well as oil pressure limits (100 PSI max, 10 PSI min).
Emergency Procedures
This section includes critical emergency procedures such as engine securing, engine failure during takeoff, and in-flight engine failure. Specific actions are outlined for various scenarios, including throttle management, mixture adjustments, and propeller settings. For instance, in the event of an engine failure immediately after takeoff, the pilot should reduce power and manage manifold pressure and RPM accordingly.
Fire Procedures
Fire procedures on the ground and in-flight are detailed, including steps to take in the event of a fire. On the ground, pilots should close the throttle, apply brakes, and cut off the mixture. In-flight, the checklist advises shutting off auxiliary fuel pumps and securing the affected engine.
Emergency Descent Procedures
Emergency descent procedures are provided for both preferred conditions and turbulence. The checklist specifies actions such as reducing throttle, adjusting propellers, and managing flaps and landing gear during descent.
Safety notes
- Ensure compliance with maximum weight limits during takeoff and landing.
- Monitor engine temperatures and pressures closely to avoid damage.
- Follow emergency procedures promptly to ensure safety during in-flight failures.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “CESSNA C-404” A.- Limitaciones de Operación 1.- Limitaciones (Velocidades) KIAS Va 3.600 lbs 160 Vne 241 Vno 212 Vfe T.O. & APPR 182 Vle 182 Vlo 182 Vmca 78 Vs 83 Vso 70 Vx (SL) 96 Vy (SL) 109 Vsse 102 Vxse 105 Vyse 109 Vr 91/102 Vapp (Flap DN) 91 Max Cross Wind 20 3.- Pesos (LBS) Máximo Take-Off 8.400 Máximo Landing 8.100 2.- Combustible (U.S. GAL) Tipo a Utilizar 100/130 Capacidad Total 348 Capacidad Usable 344 Presión de Combustible (PSI) Mínima 3,6 Máxima 19,2 4.- Motor (Potencia Máxima Continua) Limitaciones Operativas de Motor Razón HP o BHP 375 Máximas RPM 2.235 Cylinder Head Temperatura (°F) Máximas 460 Mínimas 200 Temperatura de aceite (°F) Máxima 240 Mínima 100 Presión de aceite (PSI) Máxima 100 Mínima 10 5.- Limites de maniobras (Cat. Normal) MANIOBRA KIAS Spin (Flaps UP) Prohibit Escarpados 160 Ocho Flojo 160 Chandela 160 2 B.- Emergencies Procedures 1.- ENGINE SECURING PROCEDURE Throttle CLOSE Mixture IDLE CUT-OFF Propeller FEATHER 2.- ENGINE FAILURE DURING TAKEOFF (Speed above recommended Safe Single-Engine Speed) Throttle CLOSE IMMEDIATELY Brakes AS REQUIRED 3.- ENGINE FAILURE AFTER TAKEOFF (Speed above recommended Safe Single-Engine Speed with Gear Up or in Transit) Mixture FULL RICH Propeller FULL FORWARD Throttle FULL FORWARD (40,0 INCHES HG.) Landing Gear CHECK UP Inoperative engine: Throttle CLOSE Mixture IDLE CUT-OFF Propeller FEATHER 3 4.- ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF Power REDUCE IMMEDIATELY Manifold Pressure 33,5 IN HG. MAXIMUM RPM 1.900 MAXIMUM (1.800 recommended) Propeller synchronizer OFF Rough Engine DETERMINE Problem ANALYZE Rough engine SECURE (if roughness cannot be cleared) 5.- ENGINE FAILURE DURING FLIGHT (Speed above Vmca or Buffet Speed) Inoperative Engine DETERMINE Operative Engine ADJUST AS REQUIRED a.- Before securing inoperative engine: Fuel Flow CHECK, if deficient, POSITION AUXILIARY FUEL PUMP TO ON. Fuel Selector MAIN TANK Fuel Quantity CHECK Oil Pressure and Oil Temperature CHECK Magneto Switches CHECK ON Mixture ADJUST Lean until manifold pressure begins to increase then enrichen as power increase 4 6.- ENGINE FAILURE DURING FLIGHT (Speed below Vmca or Buffet Speed) Rudder APPLY Power REDUCE Pitch attitude LOWER NOSE TO ACCELERATE Inoperative engine propeller FEATHER Operative engine INCREASE POWER as airspeed increase above Vmca or buffet speed. 7.- ENGINE INOPERATIVE GO-AROUND (Speed above 109 KIAS) Throttle FULL FORWARD (40,0 INCHES HG.) Wing Flaps T.O. & APPR (if extended) Positive Rate Of Climb ESTABILSH AT 102 KIAS Landing Gear UP 8.- FIRE ON THE GROUND Throttle CLOSE Brakes AS REQUIRED Mixture IDLE CUT-OFF Battery OFF Magnetos OFF 5 9.- INFLIGHT WING OR ENGINE FIRE Both Auxiliary Fuel Pumps OFF Operative Engine Fuel Selector MAIN TANK Emergency Crossfeed OFF Appropriate Engine SECURE Throttle CLOSE Mixture IDLE CUT-OFF Propeller FEATHER Fuel Selector OFF 10.- EMERGENCY DESCENT PROCEDURE PREFERRED PROCEDURE Throttle IDLE Propellers FULL FORWARD Mixture ADJUST Wing Flaps UP Landing Gear UP Moderate Bank INITIATE 11.- EMERGENCY DESCENT PROCEDURE IN TURBULENCE CONDITIONS Throttle IDLE Propellers FULL FORWARD Mixture ADJUST Wing Flaps LAND Landing Gear DOWN Moderate Bank INITIATE