Cessna C-T303
Cessna 303 Crusader · Specifications
Overview
This document serves as a checklist for the Cessna 303 Crusader, detailing operational limitations, emergency procedures, and performance specifications. It is intended for pilots operating the Cessna 303, providing critical information for safe flight operations. The checklist includes essential speeds, weights, fuel capacities, engine limitations, and emergency protocols to follow in various scenarios. This reference is crucial for ensuring compliance with operational standards and enhancing safety during flight.
- Va (Maneuvering Speed): 148 KIAS
- Maximum Take-Off Weight: 5,150 lbs
- Total Fuel Capacity: 155 U.S. gallons
- Maximum RPM: 2,400
- Vmca (Minimum Control Speed): 65 KIAS
- Emergency airspeed for single-engine go-around: 97 KIAS
- Maximum Cross Wind: 20 knots
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
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 ·
- Specifications
- Year ·
- 1983
- Pages ·
- 5
- File size ·
- 22 KB
- Copy found at ·
- www.dgac.gob.cl
What is the Cessna C-T303?
The Cessna C-T303 is a specifications for the Cessna 303 Crusader, dated 1983.
How many pages is the Cessna C-T303?
The copy of the Cessna C-T303 on file runs 5 pages.
What year was the Cessna C-T303 published?
The Cessna C-T303 — the Cessna 303 Crusader specifications on file — is dated 1983.
Common. More common than 78% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 303 Crusader.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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- Cessna 303 CrusaderFlight Manual
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In this document
Operational Limitations
The operational limitations section outlines critical speeds for the Cessna 303 Crusader, including Va (148 KIAS), Vne (210 KIAS), and Vso (58 KIAS). It also specifies maximum take-off weight at 5,150 lbs and fuel capacities, including a total capacity of 155 U.S. gallons, with 153 gallons usable. Engine limitations include a maximum continuous power of 250 HP and maximum RPM of 2,400.
Emergency Procedures
This section provides detailed emergency procedures for various scenarios, such as engine failure during takeoff and flight. For instance, if an engine fails during takeoff below 80 KIAS, the throttle should be closed immediately. In the event of a dual engine failure during cruise, both engines must be secured. Specific airspeeds are provided for actions during emergencies, such as maintaining 97 KIAS for a single-engine go-around.
Weight and Balance
The weight and balance section specifies the maximum take-off weight of 5,150 lbs, with limits on forward and aft baggage of 150 lbs and 200 lbs, respectively. This information is crucial for ensuring the aircraft is within safe operating limits before flight.
Engine Limitations
Engine limitations include maximum cylinder head temperature of 460 °F and oil temperature limits of 100 °F to 240 °F. Oil pressure must be maintained between 10 PSI and 100 PSI. These parameters are essential for maintaining engine health and performance during flight.
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Safety notes
- Throttle must be closed immediately in case of engine failure during takeoff below 80 KIAS.
- Maintain airspeed below 110 KIAS if cabin entry door open warning is activated.
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Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “CESSNA C-T303” “1983” A.- Limitaciones de Operación 1.- Limitaciones (Velocidades) KIAS Va 5.150 lbs 148 Vne 210 Vno 175 Vfe 10° Flaps 175 Vle 210 Vlo 175 Vmca 65 Vs 66 Vso 58 Vx (SL) 77 Vy (SL) 103 Vsse 80 Vxse 93 Vyse 97 Vr 80 Vapp (Flap DN) 80-90 Max Cross Wind 20 3.- Pesos (LBS) Máximo Take-Off 5.150 Máximo Equipaje FWD 150 W/AC Máximo Equipaje AFT 200 2.- Combustible (U.S. GAL) Tipo a Utilizar 100/130 Capacidad Total 155 Capacidad Usable 153 Presión de Combustible (PSI) Mínima 3 Máxima 16,1 4.- Motor (Potencia Máxima Continua) Limitaciones Operativas de Motor Razón HP o BHP 250 Máximas RPM 2.400 Temperatura Cabeza Cilindros (°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 148 Ocho Flojo 148 Chandela 148 2 B.- Emergencies Procedures 1.- ENGINE FAILURE DURING TAKEOFF (Speed below 80 Kias) Throttle CLOSE IMMEDIATELY Brakes AS REQUIRED 2.- CONTINUED TAKEOFF WITH ENGINE OUT (Speed above 80 Kias) Throttle FULL FORWARD Propeller Controls FULL FORWARD Mixture Controls FULL FORWARD Wing Flaps UP Landing Gear UP Inoperative engine IDENTIFY Windmilling Propeller FEATHER PROMPTLY Establish Bank 5° TOWARD OPERATING ENGINE Airspeed 97 KIAS (93 KIAS with obstacles ahead) 3.- ENGINE FAILURE DURING FLIGHT (Speed below Vmca) Throttles RETARD AS NECESSARY Aileron and Rudder AS REQUIRED Elevator LOWER NOSE to accelerate to above Vmca 4.- ENGINE FAILURE DURING FLIGHT (Speed above Vmca) Power INCREASE 5.- DUAL ENGINE FAILURE DURING CRUISE FLIGHT Both Engine SECURE 3 6.- SECURE INOPERATIVE ENGINE Inoperative Engine IDENTIFY Throttle IDLE Propeller Control FEATHER Mixture Control IDLE CUT-OFF 7.- SINGLE ENGINE GO-AROUND Operative Engine Power 32,5 INCHES HG and 2.400 RPM Wing Flaps RETRACT TO 10° Landing Gear UP (if climb established) Wing Flaps UP Airspeed 97 KIAS (or 93 KIAS with obstacles ahead) 8.- ENGINE FIRE DURING START ON GROUND (RED ENG FIRE ANNUNCIATOR LIGHT ON OR OFF) Auxiliary Fuel Pumps OFF Mixture Controls IDLE CUT-OFF Battery and Alternator Switches OFF Magneto Switches OFF Parking Brake OFF Fire Extinguisher OBTAIN (if installed) 9.- CABIN FIRE DURING GROUND OPERATIONS Throttles CLOSE Brakes AS REQUIRED Mixture Controls IDLE CUT-OFF Battery Switch OFF Magneto Switches OFF Airplane EVACUATE 4 10.- ENGINE FIRE IN FLIGHT (RED ENG FIRE ANNUNCIATOR LIGHT ON) Auxiliary Fuel Pumps OFF Affected Engine: Throttles IDLE Propeller Control FEATHER Mixture Controls IDLE CUT-OFF Fuel Selector OFF Cowl Flaps OPEN 11.- ELECTRICAL FIRE IN FLIGHT Battery and Alternator Switches OFF Vents CLOSED (to avoid drafts) Cabin Heater OFF Fire Extinguisher ACTIVATE 12.- CABIN FIRE Battery and Alternator Switches OFF Vents CLOSED (to avoid drafts) Cabin Heater OFF Fire Extinguisher ACTIVATE 13.- WING FIRE Pitot Heat Switch OFF Strobe Light Switch (if installed) OFF Navigation Light Switch OFF Landing Light Switch OFF 5 14.- CABIN ENTRY DOOR OPEN (RED DOOR OPEN ANNUNCIATOR LIGHT ON) Airspeed MAINTAIN LESS THAN 110 KIAS Flight Controls MANEUVER for return for landing Before landing Checklist COMPLETE Landing MAKE NORMAL APPROACH AND LANDING