Emergency Procedures for Cessna Citation CJ3
Cessna Citation CJ3+ · Emergency Procedures
Overview
This document outlines the emergency procedures for the Cessna Citation CJ3. It serves as a critical reference for pilots operating this aircraft, detailing specific actions to take in various emergency situations. The procedures include responses to engine failures, environmental system issues, and emergency descents, among others. Each section provides clear instructions to ensure safety and effective management of emergencies during flight operations.
- Maximum ramp weight: 14,070 lbs
- Max takeoff weight: 13,870 lbs
- Max landing weight: 12,750 lbs
- V1 speed: critical for engine failure decisions
- Emergency descent pitch attitude: 7.5° nose down
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
- 21 KB
- Publisher
- www.dgac.gob.cl
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation CJ3+.
- 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
Operating Limits
This section provides essential operating limits for the Cessna Citation CJ3, including maximum speeds (VA 200 KIAS, VMO 278 KIAS, MMO 0.737), fuel capacities (max usable fuel quantity 4,710 lbs), and weight limitations (maximum ramp weight 14,070 lbs, max takeoff weight 13,870 lbs). It also lists various speed configurations for different flight phases.
Engine Failure During Takeoff
The procedures for engine failure during takeoff are divided into two scenarios: below and above V1. If failure occurs below V1, pilots should apply brakes as required, throttle to idle, and extend speed brakes. If above V1, maintain directional control, accelerate to VR, rotate at VR, and climb at V2.
Engine Fire Procedures
In the event of an engine fire indicated by a warning light, the affected engine's throttle should be set to idle. If the warning light remains illuminated, the engine fire button should be activated to discharge the fire suppression system.
Emergency Descent Procedures
For an emergency descent, pilots should disengage the autopilot, set throttles to idle, extend speed brakes, and initially target a pitch attitude of 7.5° nose down to expedite descent.
Emergency Evacuation Procedures
In case of an emergency evacuation, the parking brake should be set, throttles turned off, and both engine fire buttons pressed. The battery switch should be turned off, and the emergency locator transmitter (ELT) activated. Pilots must assess the best escape route and open the cabin door or emergency exit as necessary.
Safety notes
- Always maintain directional control during engine failure above V1.
- Ensure oxygen masks are donned in case of cabin altitude issues.
- Follow emergency evacuation procedures carefully to ensure safety.
Full document text
1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “CESSNA CITATION CJ3 C-525” SR. HERNÁN BRIONES A.- OPERATING LIMITS 1.- Limitations (KIAS) 2.- Fuel (U.S. GAL) VA (maximum) 200 Type to Utilize JET-A1 VMO (8000 TO 29.300) 278 Main Fuel System 4.710 lbs MMO (Above 30.500’) 0,737 Max Imbalance 200 VFE (up to 15°) 200 Max Usable Fuel Quantity 4.710 Lbs VFE (Full Down) 35ª 161 Max Emergency Imbalance 600 VFE (Ground 55°) 140 VLE 200 3.- Weight (LBS) VLO 200 Maximum Ramp Weight 14.070 VSB NO LIMIT Maximum TOW 13.870 VTIRE 165 MAX Landing Weight 12.750 VMCA 88 MAX ZFW 10.510 VMCG 89 VS (CLEAN, MTOW) 102 VSO (Flaps 35°, Gear Down) 86 VX (flaps 15) 110 4.- Starter Limitations VY (flaps 15) 160 VAPP (Full Flaps) 130 Max Cross Wind 21 3 Starts in 30 Min with 60 sec rest between starter. Max Tail Wind 10 2 B.- EMERGENCIES PROCEDURES 1.- ENGINE FAILURE DURING TAKEOFF SPEED BELOW V1 Brakes AS REQUIRED Throttles IDLE Speed Brakes EXTEND 2.- ENGINE FAILURE DURING TAKEOFF SPEED ABOVE V1 Maintain Directional Control Airspeed Accelerate to VR Rotate at VR, CLIMB AT V2 Landing Gear UP (after positive rate-of-climb) Flaps RETRACT (1500¨ AGL V2 + 10 or VENR) 3.- ENGINE FAILURE DURING FINAL APPROACH Thrust (Operating Engine) INCREASE Airspeed Vapp Flaps TAKEOFF AND APPROACH 15° 4.- ENGINE FIRE (LH OR RH ENGINE FIRE WARNING LIGHT/SWITCH ILLUMINATED) Throttle (Affected Engine) IDLE a.- If Light Remains Illuminated: Engine Fire Button LIFT COVER and PUSH Either Illuminated Bottle Armed Light PUSH 3 5.- EMERGENCY RESTART – TWO ENGINES L/R boost pump BOTH ON Throttles OFF, THEN IDLE (24% N2 MAX) If altitude Allows INCREASE AIRSPEED TO 230 KIAS 6.- ENVIRONMENTAL SYSTEM SMOKE, ODOR, SMOKE REMOVAL, ELECTRICAL FIRE OR SMOKE Oxygen Masks DON and EMER Microphone Select Sw MIC OXY MASK 7.- CABIN ALT (Cabin decompression, cabin altitude above normal limits) Oxygen Masks DON and 100% OXYGEN Microphone Select Sw MIC OXY MASK Emergency Descent AS REQUIRED Passenger Oxygen MAKE SURE PASSENGER ARE RECEIVING OXYGEN 8.- EMERGENCY DESCENT Autopilot/Trim Disengage Button PRESS AND RELEASE Throttles IDLE Speed Brakes EXTEND Airplane Pitch Attitude INITIALLY TARGET 7.5° NOSE DOWN 4 9.- BATTERY OVERHEAT Volt/Amp NOTE Battery Switch EMER Volt/Amp NOTE DECREASE 10.- AUTOPILOT MALFUNCTION Autopilot/Trim Disengage Button PRESS AND RELEASE 11.- EMERGENCY EVACUATION Parking Brake SET Throttles BOTH OFF LH/LR Engine Fire Buttons BOTH PRESS Illuminated Bottle armed Buttons BOTH PRESS Battery Switch OFF Elt ACTIVATE Airplane And immediate area CHECK FOR BEST ESCAPE ROUTE a.- If Thru Cabin Door: Cabin Door OPEN Move Away From Airplane b.- If Thru Emergency Exit: Emergency Exit Door REMOVE AND THROW EXIT DOOR OUT OF AIRPLANE. Move away from airplane.
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