Cessna Citation CE-525A – CJ2 Note Taking Guide
Cessna Citation CJ2+ · Pilot's Operating Handbook
Overview
This document is a Note Taking Guide for the Cessna Citation CE-525A CJ2, designed to assist pilots in memorizing critical operational procedures and limitations. It covers essential memory items, takeoff briefing protocols, and emergency procedures, as well as detailed specifications regarding fuel, electrical systems, hydraulics, environmental controls, and ice protection. The guide emphasizes the importance of practice and memorization for safe operation, particularly in emergency scenarios. It serves as a supplementary resource for pilots preparing for evaluations and familiarization with the aircraft's systems and operational limits.
- Ramp weight: 12,500 lbs
- Takeoff weight: 12,375 lbs
- Maximum altitude: FL 450
- Fuel capacity: 3960 lbs
- ITT Take-Off limit: 820°C
Document
Source
Originally published by aeromania.net. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Year
- 2017
- Pages
- 14
- File size
- 7.2 MB
- Publisher
- aeromania.net
Specifications & performance
Extracted from this document.
Specifications
- Engine model
- FJ44-2C
- Max speed (kt)
- 275
- Empty weight (lb)
- 7,700
- Service ceiling (ft)
- 45,000
- Max takeoff weight (lb)
- 12,375
Performance
- Max crosswind (kt)
- 10
- Stall speed clean (kt)
- 180
- Stall speed landing (kt)
- 161
V-speeds
- VA
- 165
- VFE
- 200
Weight & balance
- Useful load (lb)
- 5,300
- Max ramp weight (lb)
- 12,500
- Baggage allowance (lb)
- 1,100
- Basic empty weight (lb)
- 7,700
- Max landing weight (lb)
- 11,500
- Max takeoff weight (lb)
- 12,375
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Most owners only have the POH. Here's the essential set for the Cessna Citation CJ2+.
- 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
Memory Items
This section outlines critical memory items for emergency situations, including procedures for engine failure or fire during takeoff. Key points include aborting takeoff if below V1 and continuing if above V1. It also covers emergency descent protocols and responses to electrical fires or smoke.
Takeoff Briefing
The takeoff briefing section provides a structured approach for pilots to memorize essential takeoff parameters such as V1, V2, and required runway lengths. It emphasizes communication during takeoff and outlines the sequence of calls and actions to be taken.
Weights and Speeds
This section lists important weight limits for the CJ2, including ramp weight (12,500 lbs), takeoff weight (12,375 lbs), landing weight (11,500 lbs), and zero fuel weight (9,300 lbs). It also details critical airspeeds, such as VMO and MMO, as well as flap and gear operation speeds.
Limitations
The limitations section specifies operational constraints, including maximum altitude (FL 450), maximum temperature (ISA +39°C), and generator load limits at various flight levels. It also outlines autopilot minimum altitudes for takeoff and cruise.
Powerplant Specifications
This section provides technical specifications for the CJ2's powerplant, the FJ44-2C, including thrust ratings, ITT limits for various phases of operation, and TBO (4000 hours). It also includes fuel quantity and pressure limits.
Safety notes
- Abort takeoff if speed is below V1 during engine failure.
- Emergency descent procedures must be memorized.
Full document text
Cessna Citation CE-525A – CJ2 Note Taking Guide +1.307.388.0026 ` Document Version 1.1 10 June 2017 © Aeromania, LLC 2017 ™ 2 Aeromania LLC CE 525A CJ-2 Note Taking Guide Ver. 1.0 1.1 Original New cover 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-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 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
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