CESSNA CITATION LATITUDE / C680A CC-AXC
Cessna Citation Latitude · Checklist
Overview
This document serves as a checklist for the Cessna Citation Latitude (C680A), providing essential limitations, emergency procedures, and operational guidelines for pilots. It outlines critical airspeed limitations, weight specifications, and electrical power system details necessary for safe operation. The checklist is designed for use during various flight phases, including takeoff, landing, and emergency situations, ensuring pilots have quick access to vital information. The document is intended for pilots operating the Cessna Citation Latitude, enhancing safety and efficiency in flight operations.
- Maximum takeoff weight (MTOW): 30,800 lbs
- Maximum landing weight (MLW): 27,575 lbs
- VMO (between 8,000 and 29,833 feet): 305 KIAS
- Maximum tire ground speed: 182 knots
- Emergency descent requires oxygen masks and maximum rate of descent.
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
- 4
- File size
- 207 KB
- Publisher
- www.dgac.gob.cl
Common. Rarer than 24% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation Latitude.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Cessna Citation Latitude for sale now
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- ENGINEERING REVIEW OF DATA FROM 680A-0010 ON AUGUST 15, 2019Flight Manual
- Cessna Citation LatitudeChecklist
- 2018 Cessna Citation Latitude / N68HASystems Description
- 2017 Cessna Citation LatitudeSystems Description
- Cessna Citation Latitude SpecificationsSpecifications
- C ITATION LATITUDESystems Description
- Flammability Testing & Certification ServicesSupplemental Type Certificate
- Emergency ProceduresEmergency Procedures
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In this document
Limitations
This section details the operational limitations of the Cessna Citation Latitude. Key figures include a maximum takeoff weight (MTOW) of 30,800 lbs, a maximum landing weight (MLW) of 27,575 lbs, and a maximum design zero fuel weight (MZFW) of 21,200 lbs. Airspeed limitations include VMO of 305 KIAS between 8,000 and 29,833 feet, and 270 KIAS below 8,000 feet. The maximum tire ground speed is 182 knots, and the maximum autopilot operation speed is 305 KIAS or Mach 0.80.
Emergencies / Abnormal Procedures
This section outlines critical emergency procedures for various scenarios, such as APU fire, engine fire, and cabin altitude issues. For an APU fire, the APU FIRE button must be pushed. In the event of an engine fire during takeoff above V1, the autothrottle should be disengaged, and the affected engine throttle should be set to idle. For cabin altitude issues, oxygen masks should be donned and a maximum rate of descent initiated.
Safety notes
- Ensure to don oxygen masks during cabin altitude emergencies.
- Abort takeoff if engine fire is detected below V1.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “CESSNA CITATION LATITUDE / C680A CC-AXC” NOMBRE : _____________________________________ FIRMA: _________ FECHA : ____________________ A.- Limitations 3.- Weigth (lbs) 2.- Take off and landing limits 1.- Airspeed limitations KIAS/Mach MMO (Above 29.833 feet) Mach 0.80 (indicated) VMO (Between 8000 and 29.833 feet) 305 KIAS VMO (below 8000 feet) 270 KIAS Vlo 210 KIAS Vle 210 KIAS Vsb (maximum speed brake operation speed) No limit Maximum tire ground speed 182 Knots Maximum autopilot operation speed 305 KIAS or Mach 0.80 Maximum design ramp weight 31.050 Pounds Maximum design take off weight (MTOW) 30.800 Pounds Maximum design landing weigt (MLW) 27.575 Pounds Maximum design zero fuel weight (MZFW) 21.200 Pounds 4.- Electrical power system Ground 300 Amps Air < FL350 300 Amps >FL350 and <FL450 275 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 APU FIRE 1. APU FIRE Button....................................................................................................Push AT HOLD FAIL 1. Takeoff..................................................................................................................Abort BATTERY O’TEMP L and/or R 1. BATT Button (affected side).....................................................................................OFF CABIN ALTITUDE 1. Oxygen Masks...............................................................................................Don and 100% 2. MIC SEL Buttons (Both)...............................................................................................MASK 3. Initiate maximum rate of descent to a safe altitude. EMERGENCY DESCENT and EDM 1. Oxygen Masks...............................................................................................Don and 100% 2. MIC SEL Buttons (Both)...............................................................................................MASK 3. Initiate maximum rate of descent to a safe altitude. ENGINE FIRE L or R • Takeoff Above V1 or In Flight 1. Autothrottle.....................................................................................................Disengage 2. Throttle (affected engine)..........................................................................................IDLE 3. WING XFLOW ANTI-ICE Button (if bleed air anti-ice systems are on).........................................................................XFLOW If ENG FIRE Light Still Illuminated After 15 Seconds (Probable Fire) 4. ENG FIRE Button (illuminated Side)....................................................................Push 5. BOTTLE ARMED Button (either illuminated side)...............................................Push • Takeoff Below V1 or On Ground 1. Takeoff..................................................................................................................Abort NO TAKEOFF 1. Takeoff..................................................................................................................Abort T/R DEPLOY L or R 1. T/R EMER STOW Button (flashing button)....................................................................Push 2. Throttle (affected engine)...............................................................................................IDLE 3. Airspeed...........................................................................Decrease to 150 KIAS Maximum 3 WINDSHEAR 1. Autothrottle...........................................................................................................Disengage 2. Autopilot...............................................................................................................Disengage 3. Throttles............................................................................................................................TO 4. Pitch Attitude..............................................................................Go-Around Attitude (7.5o) 5. SPEEDBRAKE Handle...................................................................................................RET Engine Failure or Other Emergency/During Takeoff • Speed Below V1 1. Takeoff....................................................................................................................Abort • If Speed at or Above V1 1. Takeoff....................................................................................Continue to a safe altitude 2. WING XFLOW ANTI-ICE Button (if bleed air anti-ice systems are on).........................................................................XFLOW Engine Failure During Final Approach 1. FLAP Selector......................................................................................................................2 2. Airspeed.......................................................................................................................VAPP Dual Engine Flameout - Cruise 1. Crew Oxygen Masks (if required)...............................................................Don and 100% Dual Engine Flameout - Low Altitude 1. Fuel................................................................................................Check Tanks/Quantity 2. FUEL BOOST PUMP Buttons (both)...............................................................................ON 3. ENGINE RUN/STOP Buttons (both).......................................................................................STOP Uncommanded Engine Thrust • During Takeoff Below V1 1. Takeoff....................................................................................................................Abort 2. ENG FIRE Button (affected side)..............................................................................Push • During Takeoff Above V1, Climb, Cruise, or Descent 1. Climb to safe altitude • During Approach
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1. TO/GA Button (either throttle)...................................................................................Push 2. Throttles.......................................................................................................................TO 3. Airplane Pitch Attitude...................................................................................7.5o Initially • During Landing Roll 1. Directional Control (rudder, NWS, differential braking).......................................Maintain 2. ENG FIRE Button (affected side)..............................................................................Push Electrical System Smoke or Fire 1. Oxygen Masks/Goggles............................................................................Don and EMER Environmental System Smoke or Odor 1. Oxygen Masks/Goggles............................................................................Don and EMER 4 Smoke Removal 1. Oxygen Masks/Goggles............................................................................Don and EMER Hydraulic Wheel Brake Failure 1. Brake Pedals.................................................................................................Remove Feet 2. EMERGENCY BRAKE Handle..............................................Pull and Hold Until Stopped Aileron Trim Runaway 1. AP/TRIM/NWS DISC Button......................................................................Push and Hold Uncommanded Roll 1. AP/TRIM/NWS DISC Button......................................................................................Push Primary Pitch Trim Runaway 1. AP/TRIM/NWS DISC Button......................................................................Push and Hold Secondary Pitch Trim Runaway 1. SECONDARY TRIM Button........................................................................................OFF Rudder Trim Runaway 1. AP/TRIM/NSW DISC Button......................................................................Push and Hold Jammed Pitch or Roll Control System 1. Stabilizer Trim Switch.........................................Actuate to establish desired pitch attitude 2. Control Wheel............................................................................................Relax Pressure 3. PITCH/ROLL Disconnect Handle...........................................................Pull Until Latched 4. Operative Control Wheel............................................Identify, Recover Airplane Attitude Nosewheel Steering Malfunction 1. AP/TRIM/NSW DISC Button........................................................................Push and Hold Total Loss of or Unreliable Airspeed Indication (Pilot, Copilot, and Standby) 1. Autothrottle........................................................................................................Disengage 2. Autopilot.............................................................................................................Disengage 3. Yaw Damper......................................................................................................Disengage 4. PITOT/STATIC ANTI-ICE Buttons (both).......................................................OFF, then ON Inadvertant Stall (Stick Shaker, Buffet, and/or Roll-Off) 1. AP/TRIM/NWS DISC Button.......................................................................................Push 2. Pitch Attitude........................................................................................................Decrease 3. Roll Attitude.....................................................................................................Wings Level 4. Autothrottle........................................................................................................Disengage 5.Throttles..........................................................................................................................TO




