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Cessna Citation CE-525 Note Taking Guide

CESSNA CITATION JET · Checklist

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Overview

This document is a Note Taking Guide for the Cessna Citation CE-525, aimed at pilots and students preparing for evaluations. It includes critical memory items, takeoff briefings, and emergency procedures. The guide emphasizes the importance of memorizing specific procedures and limitations associated with the aircraft. It serves as a practical tool for understanding the aircraft's systems and operational protocols, ensuring that pilots are well-prepared for various flight scenarios.

  • Maximum Takeoff Weight: 10,400 lbs
  • Maximum Altitude: 41,000 feet
  • VMO: 263 knots, MMO: 0.71
  • Emergency descent initiated at CABIN ALT warning
  • Battery over temperature warning requires immediate attention

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
Checklist
Year
2017
Pages
16
File size
7.2 MB
Publisher
aeromania.net
Documentation completeness
4/7

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In this document

Memory Items

The Memory Items section outlines critical emergency procedures such as actions during engine failure or fire during takeoff. It specifies that if an engine failure occurs below V1, the takeoff should be aborted, while if it occurs above V1, the takeoff should continue.

Takeoff Briefing

This section provides a structured takeoff briefing that pilots must memorize. It includes key speeds such as V1, V2, and required runway length. The briefing emphasizes communication between the pilot and co-pilot during takeoff.

Limitations

The Limitations section details the aircraft's operational limits, including maximum weights, speeds, and environmental conditions. For instance, the maximum takeoff weight is 10,400 lbs, and the maximum altitude is 41,000 feet.

Weights and Speeds

This section lists important weights and speeds for the CE-525, including ramp weight (10,500 lbs), takeoff weight (10,400 lbs), and landing weight (9,700 lbs). It also specifies various speeds such as VMO (263 knots) and MMO (0.71).

Emergency Procedures

Emergency procedures are outlined for various scenarios, including engine failure, electrical fire, and cabin altitude warnings. Pilots are instructed on the appropriate actions to take in these situations.

Safety notes

  • Speed below V1 requires takeoff to be aborted.
  • Engine failure above V1 requires continuation of takeoff.

Full document text

Note Taking Guide +1.307.388.0026 Cessna Citation CE-525 Note Taking Guide +1.307.388.0026 Document Version 1.1 10 June 2017 © Aeromania, LLC 2017 ™ 2 Aeromania LLC CE 525 CJ Note Taking Guide Ver. 1.0 1.1 Original New cover & edits 1/15/2016 6/10/2017 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-525 thru SN 359 Weights – in pounds Ramp 10,500 Takeoff 10,400 Landing 9,700 Zero Fuel 8,400 Baggage, Nose 400 Baggage, Aft Cabin 100 Baggage, Tail 300 BEW, Typical 6,500 Speeds – in knots VMO to FL305 263 MMO 0.71 Va 7000 lbs @ SL 154 10400 lbs @ FL380 217 Turbulent Air 180 Flaps 15 (TO & APR) 200 Flaps 35 (Land) 161 Gear (ALL) 186 VMCG 95 VMCA 92 Autopilot 263/0.71 Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.75” Max Temp (SL) ISA+ 39 C Min Temp -53 C Max Tailwind 10 kts Starter 3 Starts in 30 min Battery 3 starts/hr Max Generator Load Ground 300 amps >15 Minute 250 amps Tire groundspeed 165 Tire pressure Nose 120+/-5 Mains 98+/-5 P/S heat on ground 2 min Limitations Enroute Max Altitude FL 410 Max Temp 7C @ FL360, 62C SL Max Generator Load 300 amps Powerplant FJ44-1A N1 104.4 % N2 99.3 % ITT (Start) 1000 C ITT Take-Off (5 min) 820 C ITT Continuous 796 C ITT Idle 620 C Thrust-ISA, TO, 5 min 1900# Bypass Ratio 3.3 to 1 Fuel Quantity 3200# LO FUEL LEVEL 170# LO FUEL PRESS 5 psi Imbalance 200# Prist Required Environmental Max Design Cabin Alt. 8000’ CAB ALT 10,000’ Altitude Limiters 13,000’ (+/-1500) Masks Auto-Drop 13,500’ (+/-600) Max Cabin Differential 8.5 15 CJ1 SN 360-599 Weights – in pounds Ramp 10,700 Takeoff 10,600 Landing 9,700 Zero Fuel 8,400 Baggage, Nose 400 Baggage, Aft Cabin 100 Baggage, Tail 300 BEW, Typical 6,600 Speeds – in knots VMO to FL305 263 MMO 0.71 Va 7000 lbs @ SL 154 10400 lbs @ FL380 217 Turbulent Air 180 Flaps 15 (TO & APR) 200 Flaps 35 (Land) 161 Gear (ALL) 186 VMCG 95 VMCA 92 Autopilot 263/0.71 Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.75” Max Temp (SL) ISA+ 39 C Min Temp -53 C Max Tailwind 10 kts Starter 3 Starts in 30 min Battery 3 starts/hr Max Generator Load Ground 300 amps >15 Minute 250 amps Tire groundspeed 165 Tire pressure Nose 120+/-5 Mains 98+/-5 P/S heat on ground 2 min Limitations Enroute Max Altitude FL 410 Max Temp 7C @ FL360, 62C SL Max Generator Load 300 amps Powerplant FJ44-1A N1 104.4 % N2 99.3 % ITT (Start) 1000 C ITT Take-Off (5 min) 820 C ITT Continuous 796 C ITT Idle 620 C Thrust-ISA, TO, 5 min 1900# Bypass Ratio 3.3 to 1 Fuel Quantity 3200# LO FUEL LEVEL 170# LO FUEL PRESS 5 psi Imbalance 200# Prist Required Environmental Max Design Cabin Alt. 8000’ CAB ALT 10,000’ Altitude Limiters 13,000’ (+/-1500) Masks Auto-Drop 13,500’ (+/-600)

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Max Cabin Differential 8.5 16 CJ1+ SN 600 on Weights – in pounds Ramp 10,800 Takeoff 10,700 Landing 9,900 Zero Fuel 8,400 Baggage, Nose 400 Baggage, Aft Cabin 100 Baggage, Tail 300 BEW, Typical 6,800 Speeds – in knots VMO to FL305 263 MMO 0.71 Va 7000 lbs @ SL 154 10400 lbs @ FL380 217 Turbulent Air 180 Flaps 15 (TO & APR) 200 Flaps 35 (Land) 161 Gear (ALL) 186 VMCG 95 VMCA 92 Autopilot 263/0.71 Takeoff, Landing, Ground Max Altitude 10,000 Water or Slush 0.75” Max Temp (SL) ISA+ 39 C Min Temp -53 C Max Tailwind 10 kts Starter 3 Starts in 30 min Battery 3 starts/hr Max Generator Load Ground 300 amps >15 Minute 250 amps Tire groundspeed 165 Tire pressure Nose 120+/-5 Mains 103+/-5 P/S heat on ground 2 min Limitations Enroute Max Altitude FL 410 Max Temp 7C @ FL360, 62C SL Max Generator Load To FL 350 300 amps Above FL 3 250 amps Powerplant FJ44-1AP N1 102.6 % N2 100.0 % ITT (Start) 1000 C ITT Take-Off (5 min) 855 C ITT Continuous 835 C ITT Idle 620 C Thrust-ISA, TO, 5 min 1960# Bypass Ratio 3.3 to 1 Fuel Quantity 3200# LO FUEL LEVEL 170# LO FUEL PRESS 5 psi Imbalance 200# Environmental Max Design Cabin Alt. 8000’ CAB ALT 10,000’ Altitude Limiters 13,000’ (+/-1500) Masks Auto-Drop 13,500’ (+/-600) Max Cabin Differential 8.5