Emergency Procedures
Cessna Citation Latitude · Emergency Procedures
Overview
This document provides emergency procedures for the Cessna Citation Latitude (C680A). It is intended for pilots and crew members to ensure safety during abnormal situations and emergencies. The procedures outlined include responses to various emergencies such as APU fire, engine fire, cabin altitude issues, and more. Each section details specific actions to take, ensuring that crew members can respond effectively to maintain control of the aircraft and ensure passenger safety.
- Maximum Takeoff Weight (MTOW): Specific value not provided in the text.
- Maximum Landing Weight (MLW): Specific value not provided in the text.
- APU Fire response includes activating the APU FIRE Button.
- Engine Fire procedures vary for takeoff and in-flight scenarios.
- Emergency descent procedures require oxygen masks and maximum rate of descent initiation.
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
- Emergency Procedures
- Pages
- 4
- File size
- 202 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)
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More Cessna Citation Latitudemanuals & documents
- CITATION LATITUDE OPTIONAL EQUIPMENT SELECTION GUIDEMaintenance Manual
- Service Advisory 2186Normal Procedures
- 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
- CESSNA CITATION LATITUDE / C680A CC-AXCChecklist
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In this document
Limitations
This section outlines critical limitations for the Cessna Citation Latitude, including weight limits, airspeed limitations, and electrical power system constraints. Key values include maximum takeoff weight (MTOW), maximum landing weight (MLW), and maximum zero fuel weight (MZFW). Specific airspeed limitations are provided for various flight conditions.
APU Fire
In the event of an APU fire, the procedure involves activating the APU FIRE Button and following specific steps depending on whether the aircraft is on the ground or in flight. Immediate actions are crucial to mitigate risks and ensure safety.
Engine Fire
The procedures for handling an engine fire differ based on whether the incident occurs during takeoff or in flight. Key actions include managing throttle settings and activating fire suppression systems. The document specifies steps for both scenarios to ensure a safe response.
Emergency Descent
In case of cabin altitude issues, the document instructs crew members to don oxygen masks, select the appropriate MIC SEL buttons, and initiate a maximum rate of descent to a safe altitude.
Uncommanded Engine Thrust
This section details the response to uncommanded engine thrust during various phases of flight, including takeoff and approach. It emphasizes the importance of maintaining control and executing specific throttle and autopilot commands.
Safety notes
- Immediate action is required for APU and engine fire situations.
- Proper use of oxygen masks is critical during cabin altitude emergencies.
- Follow specific procedures for uncommanded engine thrust to maintain control.
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) VMO (Between 8000 and 29.833 feet) VMO (below 8000 feet) Vlo Vle Vsb (maximum speed brake operation speed) Maximum tire ground speed Maximum autopilot operation speed Maximum design ramp weight Maximum design take off weight (MTOW) Maximum design landing weigt (MLW) Maximum design zero fuel weight (MZFW) 4.- Electrical power system Ground Air < FL350 >FL350 and <FL450 Battery start limit Maximum altitude limit Maximum tailwind component 2 B.- EMERGENCIES / ABNORMAL PROCEDURES APU FIRE 1. APU FIRE Button.................................................................................................... AT HOLD FAIL 1. Takeoff.................................................................................................................. BATTERY O’TEMP L and/or R 1. BATT Button (affected side)..................................................................................... CABIN ALTITUDE 1. Oxygen Masks............................................................................................... 2. MIC SEL Buttons (Both)............................................................................................... 3. Initiate maximum rate of descent to a safe altitude. EMERGENCY DESCENT and EDM 1. Oxygen Masks............................................................................................... 2. MIC SEL Buttons (Both)............................................................................................... 3. Initiate maximum rate of descent to a safe altitude. ENGINE FIRE L or R • Takeoff Above V1 or In Flight 1. Autothrottle..................................................................................................... 2. Throttle (affected engine).......................................................................................... 3. WING XFLOW ANTI-ICE Button (if bleed air anti-ice systems are on)......................................................................... If ENG FIRE Light Still Illuminated After 15 Seconds (Probable Fire) 4. ENG FIRE Button (illuminated Side).................................................................... 5. BOTTLE ARMED Button (either illuminated side)............................................... • Takeoff Below V1 or On Ground 1. Takeoff.................................................................................................................. NO TAKEOFF 1. Takeoff.................................................................................................................. T/R DEPLOY L or R 1. T/R EMER STOW Button (flashing button).................................................................... 2. Throttle (affected engine)............................................................................................... 3. Airspeed........................................................................... 3 WINDSHEAR 1. Autothrottle........................................................................................................... 2. Autopilot............................................................................................................... 3. Throttles............................................................................................................................ 4. Pitch Attitude.............................................................................. 5. SPEEDBRAKE Handle................................................................................................... Engine Failure or Other Emergency/During Takeoff • Speed Below V1 1. Takeoff.................................................................................................................... • If Speed at or Above V1 1. Takeoff.................................................................................... 2. WING XFLOW ANTI-ICE Button (if bleed air anti-ice systems are on)......................................................................... Engine Failure During Final Approach 1. FLAP Selector...................................................................................................................... 2. Airspeed....................................................................................................................... Dual Engine Flameout - Cruise 1. Crew Oxygen Masks (if required)............................................................... Dual Engine Flameout - Low Altitude 1. Fuel................................................................................................ 2. FUEL BOOST PUMP Buttons (both)............................................................................... 3. ENGINE RUN/STOP Buttons (both)....................................................................................... Uncommanded Engine Thrust • During Takeoff Below V1 1. Takeoff.................................................................................................................... 2. ENG FIRE Button (affected side).............................................................................. • During Takeoff Above V1, Climb, Cruise, or Descent 1. Climb to safe altitude • During Approach 1. TO/GA Button (either throttle)................................................................................... 2. Throttles....................................................................................................................... 3. Airplane Pitch Attitude................................................................................... • During Landing Roll 1. Directional Control (rudder, NWS, differential braking).......................................
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2. ENG FIRE Button (affected side).............................................................................. Electrical System Smoke or Fire 1. Oxygen Masks/Goggles............................................................................ Environmental System Smoke or Odor 1. Oxygen Masks/Goggles............................................................................ 4 Smoke Removal 1. Oxygen Masks/Goggles............................................................................ Hydraulic Wheel Brake Failure 1. Brake Pedals................................................................................................. 2. EMERGENCY BRAKE Handle.............................................. Aileron Trim Runaway 1. AP/TRIM/NWS DISC Button...................................................................... Uncommanded Roll 1. AP/TRIM/NWS DISC Button...................................................................................... Primary Pitch Trim Runaway 1. AP/TRIM/NWS DISC Button...................................................................... Secondary Pitch Trim Runaway 1. SECONDARY TRIM Button........................................................................................ Rudder Trim Runaway 1. AP/TRIM/NSW DISC Button...................................................................... Jammed Pitch or Roll Control System 1. Stabilizer Trim Switch......................................... 2. Control Wheel............................................................................................ 3. PITCH/ROLL Disconnect Handle........................................................... 4. Operative Control Wheel............................................ Nosewheel Steering Malfunction 1. AP/TRIM/NSW DISC Button........................................................................ Total Loss of or Unreliable Airspeed Indication (Pilot, Copilot, and Standby) 1. Autothrottle........................................................................................................ 2. Autopilot............................................................................................................. 3. Yaw Damper...................................................................................................... 4. PITOT/STATIC ANTI-ICE Buttons (both)....................................................... Inadvertant Stall (Stick Shaker, Buffet, and/or Roll-Off) 1. AP/TRIM/NWS DISC Button....................................................................................... 2. Pitch Attitude........................................................................................................ 3. Roll Attitude..................................................................................................... 4. Autothrottle........................................................................................................ 5.Throttles..........................................................................................................................




