CESSNA CITATION CJ4 / C25C CC-AOR
Cessna Citation CJ4 · Checklist
Overview
This document serves as a checklist for the Cessna Citation CJ4, providing essential limitations, emergency procedures, and abnormal event responses. It is designed for pilots operating the CJ4, ensuring they are aware of critical operational limits and emergency protocols. The checklist includes weight limits, airspeed limitations, and electrical power system specifications, as well as detailed steps for handling various emergency situations during flight. This resource is crucial for maintaining safety and efficiency during operations of the Cessna Citation CJ4.
- Maximum takeoff weight (MTOW): 17,110 lbs
- Maximum landing weight (MLW): 15,660 lbs
- VMO (between 8,000 and 27,884 feet): 305 KIAS
- Vlo and Vle: 200 KIAS
- Maximum tire ground speed: 160 KIAS
- Emergency descent: initiate maximum rate of descent to a safe altitude
- Battery start limit: three engine starts per hour
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
- 3
- File size
- 157 KB
- Publisher
- www.dgac.gob.cl
Common. Rarer than 2% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation CJ4.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Limitations
This section outlines critical operational limits for the Cessna Citation CJ4, including weight limits such as a maximum takeoff weight (MTOW) of 17,110 lbs and a maximum landing weight (MLW) of 15,660 lbs. Airspeed limitations are also specified, with VMO values of 305 KIAS between 8,000 and 27,884 feet, and 260 KIAS below 8,000 feet. Other important limits include maximum tire ground speed of 160 KIAS and maximum autopilot operation speed of 305 KIAS or Mach 0.77.
Emergencies / Abnormal Procedures
This section details procedures for various emergencies and abnormal events during flight. For instance, in the event of an engine failure during takeoff below V1, pilots are instructed to apply brakes, idle throttles, and extend ground spoilers. If an engine failure occurs above V1, the checklist outlines steps for climbing to a safe altitude, retracting landing gear, and maintaining minimum airspeed of V2. Additional emergency scenarios, such as engine fires and electrical fires, are also addressed with specific actions to take.
Safety notes
- Maximum tailwind component: 10 knots
- If engine fire light remains on after 15 seconds, push the illuminated ENG FIRE button.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “CESSNA CITATION CJ4 / C25C CC-AOR” NOMBRE : _____________________________________ FIRMA: _________ FECHA : ____________________ A.- Limitations 3.- Weight (lbs) 2.- Takeoff and landing limits 1.- Airspeed limitations KIAS/Mach MMO (Above 27.884 feet) Mach 0.77 (indicated) VMO (Between 8000 and 27.884 feet) 305 KIAS VMO (below 8000 feet) 260 KIAS Vlo 200 KIAS Vle 200 KIAS Vsb (maximum speed brake operation speed) No limit Maximum tire ground speed 160 KIAS Maximum autopilot operation speed 305 KIAS or Mach 0.77 Maximum design ramp weight 17.230 Pounds Maximum design takeoff weight (MTOW) 17.110 Pounds Maximum design landing weight (MLW) 15.660 Pounds Maximum design zero fuel weight (MZFW) 12.500 Pounds 4.- Electrical power system Ground 240 Amps Air < FL250 300 Amps >FL250 and <FL450 Linear decrease from 300 amps to 170 amps Battery start limit Three (3) engine starts per hour Maximum altitude limit 14.000 feet Maximum tailwind component 10 Knots 2 B.- EMERGENCIES / ABNORMAL PROCEDURES 1.- ENGINE FAILURE or OTHER EMERGENCY/ABNORMAL EVENT DURING TAKEOFF SPEED BELOW V1 – TAKEOFF REJECTED 1. Takeoff Abort a. Brakes Apply b. THROTTLES Idle c. Ground Spoilers Extend 2.- ENGINE FAILURE or OTHER EMERGENCY/ABNORMAL EVENT DURING TAKEOFF SPEED ABOVE V1 – TAKEOFF CONTINUED 1. Climb to safe altitude a. Accelerate to Vr Rotate b. Landing Gear (positive climb) Up c. Airspeed V2 Minimum d. Flaps (clear of obstacles and V2+10) 0º e. Airspeed Vern 2. WING XFLOW Button On 3.- ENGINE FIRE L or R 1. THROTTLE (affected engine) IDLE * If Light Remains On After 15 Seconds 2. Illuminated ENG FIRE Button Push * If Light Remains On After Additional 15 Seconds 3. Illuminated BOTTLE ARMED Button Push 4.- WINDSHEAR 1. THROTTLES TO 2. Pitch Attitude Smoothly Rotate to an initial pitch attitude of 7.5º (FD Go Around pitch command) 3. Speed brakes 0% 5.- ELECTRICAL FIRE OR SMOKE 1. Oxygen Mask(s)/Goggles Don and EMER 2. OXYGEN MASK MIC Button(s) On 3 6.- ENVIROMENTAL SYSTEM SMOKE OR ODOR 1. Oxygen Mask(s)/Goggles Don and EMER 2. OXYGEN MASK MIC Button(s) On 7.- SMOKE REMOVAL 1. Oxygen Mask(s)/Goggles Don and EMER 2. OXYGEN MASK MIC Button(s) On 8.- AILERON TRIM RUNAWAY 1. AP TRIM DISC Button Push and Hold 9.- PRIMARY PITCH TRIM RUNAWAY 1. AP TRIM DISC Button Push and Hold 10.- AUTOPILOT MALFUNCTION 1. AP TRIM DISC Button Push 11.- EMERGENCY DESCENT 1. Initiate maximum rate of descent to a safe altitude 12.- WHEEL BRAKE FAILURE 1. Brake Pedals Remove Feet 2. GROUND SPOILERS (after nose wheel touchdown) EXTEND 3. EMER BRAKE Handle Pull as required 4. Directional control Maintain with Nose wheel Steering 13.- DUAL ENGINE RESTART 1. ENGINE RUN/STOP Buttons (both) STOP 2. THROTTLES IDLE 3. BATTERY Switch (if descent to FL250 will take longer than 5 min) EMER 4. Altitude Below FL250 5. BATTERY Switch ON 6. ANTI – ICE Buttons (all) Off 7. HYDRAULIC SHUTOFF Buttons (both) Push (light on) 8. Airspeed 250 KIAS Minimum (altitude permitting) 9. ENGINE RUN/STOP Buttons RUN
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