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Cessna Citation CE-525A – CJ2 Note Taking Guide

Cessna Citation CJ2+ · Wiring Diagram

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Overview

This document serves as a note-taking guide for the Cessna Citation CE-525A CJ2, providing essential information for pilots and crew members. It includes memory items, operational procedures, and limitations relevant to the aircraft. The guide is structured to assist in training and evaluation, ensuring that users can memorize critical information without errors. It covers various systems such as fuel, electrical, hydraulics, and environmental controls, along with emergency procedures and performance data. This guide is particularly useful for pilots preparing for evaluations or seeking to enhance their operational knowledge of the CJ2.

  • Ramp weight: 12,500 lbs
  • Takeoff weight: 12,375 lbs
  • Landing weight: 11,500 lbs
  • Maximum altitude: FL 450
  • V1, V2, and other critical speeds must be memorized for safe operation.

Document

Source

Originally published by aeromania.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Wiring Diagram
Year
2019
Pages
15
File size
4.8 MB
Publisher
aeromania.net
How rare is it?
97Cessna Citation CJ2+ registered worldwide · 0 active

Common. Rarer than 1% of the aircraft models we track.

Documentation completeness
4/7

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In this document

Memory Items

This section outlines critical memory items for emergency situations, such as engine failure or fire during takeoff. It emphasizes the importance of knowing when to abort a takeoff based on speed relative to V1, and the necessary actions to take in various emergency scenarios.

Takeoff Briefing

The takeoff briefing section provides a structured approach for pilots to prepare for takeoff. It includes key speeds (V1, V2), runway requirements, and communication protocols during the takeoff phase.

Weights and Speeds

This section lists important weight and speed specifications for the CJ2, including ramp weight (12,500 lbs), takeoff weight (12,375 lbs), and landing weight (11,500 lbs). It also details various operational speeds such as VMO, MMO, and stall speeds.

Limitations

The limitations section outlines operational constraints for the CJ2, including maximum altitude (FL 450), temperature limits, and generator load specifications. It is crucial for pilots to understand these limitations to ensure safe operation.

Environmental Systems

This section describes the environmental control systems of the CJ2, including cabin altitude limits and emergency procedures for smoke or odor in the cabin. It provides guidelines for maintaining passenger comfort and safety.

Safety notes

  • Engine failure or fire during takeoff requires immediate action based on V1 speed.
  • Emergency descent procedures must be understood and practiced.

Full document text

Cessna Citation CE-525A – CJ2 Note Taking Guide +1.307.388.0026 ` Document Version 1.2 16 Jan 2019 © Aeromania, LLC 2019 ™ 2 Aeromania LLC CE 525A CJ-2 Note Taking Guide Ver. 1.0 1.1 1.2 Original New cover Edit limits 1/15/2016 6/10/2017 1/16/2019 Table of Contents Memory Items ………………………………………………………………………………3 Takeoff Briefing ………………………………………………………………………………5 Stall / Missed Approach ………………………………………………………………5 Fuel ……………………………………………………………………..………6 Electrical …………………………………………………………………………..…7 Hydraulics ……………………………………………………………………………..8 Environmental ……………………………………………………………………………..9 Ice Protection ……………………………………………………………………………10 PRACTICE ……………………………………………………………………………11 Limitations ……………………………………………………………………………12 You are not ready for the evaluation until you can fill in the blank PRACTICE pages from memory without any errors. The systems schematics are to be used for taking notes in class. 3 Memory Items Engine Failure or Fire or Master Warning During Takeoff Speed below V1 – takeoff should be aborted. Engine Failure or Fire During Takeoff Speed above V1 – takeoff should be continued. Engine Failure During Coupled Approach Engine FIRE (L or R Engine FIRE WARNING switch/light illuminated) Emergency Restart – Two Engines 4 Electrical Fire or Smoke, Environmental Smoke or Odor, Smoke Removal CABIN ALT (CABIN ALTITUDE) Emergency Descent BATT O’TEMP (Battery Over temperature) Autopilot Malfunction Electric Elevator Trim Runaway 5 EMERGENCY EVACUATION Takeoff Briefing Memorize this briefing: V1 is ___, V2 is ___, VENR is___, we need ___ feet of dry/wet RWY If you see a need to abort prior to V1, say “ABORT” and we’ll stop straight ahead. After V1, say “CONTINUE” and tell me what you see. We’ll (remain VFR and land, continue the SID and hold, etc) Calls will be “Power’s set, airspeed alive, cross-checked at 60, V1-Rotate, Positive Rate – I’ll command GEAR UP, V2+10, I’ll command FLAPS UP, YAW DAMPER ON, and we’ll delay the after takeoff checks until we’re talking to departure. Stall / Missed Approach Say the following words out loud and do each step in order for a single engine missed approach, a normal missed approach, or to recover from any stall. Memorize the following: MAX POWER, Flaps – APPROACH Positive Rate – GEAR UP Climb at V2 V2 plus 10 – FLAPS UP 6 Fuel 7 Electrical 8 Hydraulics 9 Environmental 10 Ice Protection 11 Practice Memory Items Engine Failure or Fire or Master Warning During Takeoff Speed below V1 – takeoff should be aborted. Engine Failure or Fire During Takeoff Speed above V1 – takeoff should be continued. Engine Failure During Coupled Approach Engine FIRE (L or R Engine FIRE WARNING switch/light illuminated) Emergency Restart – Two Engines 12 Electrical Fire or Smoke, Environmental Smoke or Odor, Smoke Removal CABIN ALT (CABIN ALTITUDE) Emergency Descent BATT O’TEMP (Battery Over temperature) Autopilot Malfunction Electric Elevator Trim Runaway 13 EMERGENCY EVACUATION Practice Takeoff Briefing ________________________________________________________ ________________________________________________________ ________________________________________________________ __________________________________ ________________________________________________________ ________________________________________________________ ________________________________________________________ _____________________ Practice Stall / Missed Approach _____________________, _____________________ _____________________ _____________________ _____________________ CE-525A CJ-2 Weights – in pounds Ramp 12,500 Takeoff 12,375 Landing 11,500 Zero Fuel 9,300 Baggage, Nose 400 Baggage, Aft Cabin 100 Baggage, Tail 600 BEW, Typical 7,700 Speeds – in knots VMO to 8,000 260 VMO 8 to FL293 275 MMO 0.72 Va 8500 lbs @ SL 165 12375 lbs @ FL310 214 Turbulent Air 180 Flaps 15 (TO & APR) 200 Flaps 35 (Land) 161 Flaps failed to Ground 140 Gear (ALL) 200 VMCG 89 VMCA (Flaps 0) 81 VMCA (Flaps 15) 89 Autopilot 275/0.72 Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.75” Max Temp (SL) +54 C Min Temp -33 C Max Tailwind 10 kts Starter 3 Starts in 30 min Battery 3 starts/hr Max Generator Load Ground 250 amps Tire groundspeed 165 Tire pressure Nose 120+/-5 Mains 114+/-5 P/S heat on ground 2 min Limitations, SN 1-299 Enroute Max Altitude FL 450 Max Temp ISA +39 C Max Generator Load Up to FL410 300 amps Above FL410 250 amps Min A/P takeoff 240’ AGL Min A/P cruise 1000’ AGL Min A/P on ILS GS 70’ AGL Min A/P non-precision 240’ Powerplant FJ44-2C N1 105.2 % N2 98.8 % N2 Icing 75 % ITT (Start) 1000 C ITT Take-Off (5 min) 820 C ITT Continuous 805 C ITT Idle 580 C Thrust-ISA, TO, 5 min 2400# Bypass Ratio 3.3 to 1 TBO 4000 hrs Fuel Quantity 3960# LO FUEL LEVEL 220# LO FUEL PRESS 5 psi Imbalance 200/600# Environmental Max Design Cabin Alt. 8000’ CAB ALT 10,000’ or 14,500’ Altitude Limiters 14,500’ (+/-500) Masks Auto-Drop 14,500’ (+/-500) Max Cabin Differential 9.0 15 CE-525A CJ-2+ Weights – in pounds Ramp 12,625 Takeoff 12,500 Landing 11,525 Zero Fuel 9,700 Baggage, Nose 400 Baggage, Aft Cabin 100 Baggage, Tail 600 BEW, Typical 7,700 Speeds – in knots VMO to 8,000 260 VMO 8 to FL293 278 MMO 0.737 Va 8500 lbs @ SL 164 12375 lbs @ FL310 214 Turbulent Air 180 Flaps 15 (TO & APR) 200 Flaps 35 (Land) 161 Flaps failed to Ground 140 Gear (ALL) 200 VMCG 79 VMCA (Flaps 0) 83 VMCA (Flaps 15) 89 Autopilot 275/0.72 Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.75” Max Temp (SL) +54 C Min Temp -33 C Max Tailwind 10 kts Starter 3 Starts in 30 min Battery 3 starts/hr Max Generator Load Ground 200 amps Tire groundspeed 165 Tire pressure Nose 120+/-5 Mains 119+/-5 P/S heat on ground 2 min Limitations, SN 300 on Enroute Max Altitude FL 450 Max Temp ISA +39 C Max Generator Load Up to FL410 300 amps Above FL410 250 amps Min A/P takeoff 240’ AGL Min A/P cruise 1000’ AGL Min A/P on ILS GS 70’ AGL Min A/P non-precision 240’

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Powerplant FJ44-3A-24 N1 105.2 % N2 98.8 % N2 Icing 75 % ITT (Start) 1000 C ITT Take-Off (5 min) 820 C ITT Continuous 805 C Thrust-ISA, TO, 5 min 2490# Bypass Ratio 2.2 to 1 TBO 4000 hrs Fuel Quantity 3960# LO FUEL LEVEL 220# LO FUEL PRESS 5 psi Imbalance 200/600# Environmental Max Design Cabin Alt. 8000’ CAB ALT 10,000’ or 14,500’ Altitude Limiters 14,500’ (+/-500) Masks Auto-Drop 14,500’ (+/-500) Max Cabin Differential 9.0

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