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Cessna Citation CE-550 JT-15 Note Taking Guide

CESSNA 550 Citation II · Checklist

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Overview

This document serves as a Note Taking Guide for the Cessna 550 Citation II, providing essential memory items, limitations, and operational procedures for pilots. It includes critical information on engine failure, electrical issues, and emergency procedures, as well as detailed weight and speed limitations. The guide is designed to assist pilots in memorizing key procedures and preparing for evaluations, ensuring they can respond effectively to various in-flight scenarios. It also contains practice sections for takeoff briefings and stall recovery, making it a comprehensive resource for both training and operational use.

  • Ramp weight: 13,500 lbs
  • Takeoff weight: 13,300 lbs
  • Landing weight: 12,700 lbs
  • Maximum altitude: FL 430
  • VMO to 14,000 ft: 262 knots

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
20
File size
4.5 MB
Publisher
aeromania.net
How rare is it?
4CESSNA 550 Citation II registered worldwide · 0 active

Common. Rarer than 12% of the aircraft models we track.

Documentation completeness
6/7

Most owners only have the POH. Here's the essential set for the CESSNA 550 Citation II.

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In this document

Memory Items

This section outlines critical memory items for emergency situations, including engine failure or fire during takeoff, electrical fires, and cabin decompression. Pilots are instructed on the appropriate actions to take based on the aircraft's speed relative to V1.

Takeoff Briefing

The takeoff briefing section emphasizes the importance of memorizing key speeds (V1, V2, VENR) and runway requirements. It details the communication protocol for aborting or continuing takeoff based on engine performance.

Limitations

This section provides detailed weight and speed limitations for the Cessna 550 Citation II, including ramp weight (13,500 lbs), takeoff weight (13,300 lbs), and landing weight (12,700 lbs). It also specifies maximum altitude, temperature limits, and generator load.

Weights and Speeds

The guide lists various weights and speeds relevant to the Cessna 550 Citation II, including VMO, MMO, and turbulent air speeds. It also details baggage weight limits and typical empty weight.

Environmental and Fuel Limitations

This section outlines environmental limitations such as maximum cabin altitude and temperature limits, as well as fuel quantity and low fuel pressure thresholds.

Safety notes

  • Speed below V1 – takeoff should normally be aborted.
  • Speed above V1 – takeoff should normally be continued.
  • Emergency descent procedures must be memorized.

Full document text

Cessna Citation CE-550 JT-15 Note Taking Guide Document Version 1.1 20 April 2017 © Aeromania, LLC 2017 +1.307.388.0026 ™ 2 Aeromania LLC CE 550 Note Taking Guide Ver. 1.0 Ver 1.1 Original Cover & edits 3/15/2016 4/20/2017 Table of Contents Memory Items ………………………………………………………………………………3 Takeoff Briefing ………………………………………………………………………………6 Stall / Missed Approach ………………………………………………………………6 Fuel ……………………………………………………………………..………7 Electrical ……………………………………………………………………………..8 Hydraulics ……………………………………………………………………………..9 Environmental ……………………………………………………………………………10 Ice Protection ……………………………………………………………………………11 Annunciator Panel ……………………………………………………………12 PRACTICE ……………………………………………………………………………13 Limitations ………………………………………………………………………17-20 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 normally be aborted. Engine Failure or Fire During Takeoff Speed above V1 – takeoff should normally be continued. Engine Failure During Coupled Approach Engine FIRE (Engine FIRE switch illuminated) Emergency Restart – Two Engines 4 Electrical Fire or Smoke Cabin Decompression Emergency Descent Battery Overheat Autopilot Malfunction TAWS WARNING (PULL UP) 5 Inadvertent Stall or Buffet Inadvertent Thrust Reverser Deployment During Takeoff SPEED BELOW V1 - ABORT Inadvertent Thrust Reverser Deployment During Takeoff SPEED ABOVE V1 – CONTINUE TAKEOFF Thrust Reverser Inadvertent In-Flight Deployment Thrust Reverser UNLOCK Light ON In Flight 6 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-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 7 Fuel 8 Electrical 9 Hydraulics 10 Environmental 11 Ice Protection 12 ANNUNCIATOR PANEL 13 Practice Memory Items Engine Failure or Fire or Master Warning During Takeoff Speed below V1 – takeoff should normally be aborted. Engine Failure or Fire During Takeoff Speed above V1 – takeoff should normally be continued. Engine Failure During Coupled Approach Speed above V1 – takeoff should normally be continued. Engine FIRE (Engine FIRE switch illuminated) Emergency Restart – Two Engines 14 Electrical Fire or Smoke Cabin Decompression Emergency Descent Battery Overheat Autopilot Malfunction TAWS WARNING (PULL UP) 15 Inadvertent Stall or Buffet Inadvertent Thrust Reverser Deployment During Takeoff SPEED BELOW V1 - ABORT Inadvertent Thrust Reverser Deployment During Takeoff SPEED ABOVE V1 – CONTINUE TAKEOFF Thrust Reverser Inadvertent In-Flight Deployment Thrust Reverser UNLOCK Light ON In Flight 16 Practice Takeoff Briefing ________________________________________________________ ________________________________________________________ _____________________ ________________________________________________________ __________________________________ ________________________________________________________ ________________________________________________________ ________________________________________________________ _____________________ Practice Stall / Missed Approach _____________________ _____________________ _____________________ _____________________ _____________________ 17 CE-550 Weights – in pounds Ramp 13,500 Takeoff 13,300 Landing 12,700 Zero Fuel 9,500 Opt. ZFW 11,000 Baggage, Nose 350 Baggage, Aft 650 Baggage, Tail 500 BEW, Typical 8,000 Speeds – in knots VMO to 14,000 262 VMO 14 to FL280 277 VMO heavy ZFW <FL305 262 MMO .705 Va 8500 lbs @ SL 150 12500 lbs @ FL310 255 Turbulent Air 180 Flaps 15 (TO & APR) 202 Flaps 40 (Land) 176 Gear (ALL) 176 VMCG 62 VMCA 77 Tire Ground (Mains) 165 Autopilot VMO/MMO Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.4” Max Temp ISA +39 C Min Temp -54 C Max Tailwind 10 kts Starter 3 Starts in 30 min Generator Load 325 amps Battery-NICAD 3 starts/hr Tire pressure Nose 120+/-5 Mains 108+/-5 P/S heat on ground 2 min Limitations <SN 505 Enroute Max Altitude FL 430 Max Temp ISA +39 C Max Generator Load Up to FL350 400 amps Above FL350 325 amps Min Autopilot on GS 95’ AGL Powerplant JT15D-4 N1 104.0 % N2 95.0 % ITT (Normal Start) 500 C ITT Take-Off (5 min) 700 C ITT Climb 680 C ITT Cruise 670 C ITT Idle 580 C Thrust-ISA, TO, 5 min 2500# Bypass Ratio 2.5 to 1 TBO 3500 hrs Fuel Quantity 5000# LO FUEL LEVEL 170-280# LO FUEL PRESS 5 psi Imbalance 600# Environmental Max Design Cabin Alt. 8000’ CAB ALT 10K FT 10,000’ Altitude Limiters 13,000’ (+/-1500) Masks Auto-Drop 13,500’ (+/-600) Max Cabin Differential 8.9 18 Heavy CE-550 Weights – in pounds Ramp 14,300 Takeoff 14,300 Landing 12,700 Zero Fuel 9,500 Opt. ZFW 11,000 Baggage, Nose 350 Baggage, Aft 650 Baggage, Tail 500 BEW, Typical 8,300 Speeds – in knots VMO to 14,000 262 VMO 14 to FL280 277 VMO heavy ZFW <FL305 262 MMO .705 VA 8500 lbs @ SL 150 12500 lbs @ FL310 255 Turbulent Air 180 Flaps 15 (TO & APR) 202 Flaps 40 (Land) 176 Gear VLO-extend 250 VLO-retract 200 VLE-extended VMO/MMO VMCG 62 VMCA 77 Tire Ground (Mains) 165 Autopilot VMO/MMO Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.4” Max Temp ISA +39 C Min Temp -54 C

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Max Tailwind 10 kts Starter 3 Starts in 30 min Generator Load 325 amps Battery-NICAD 3 starts/hr Tire pressure Nose 120+/-5 Mains 108+/-5 P/S heat on ground 2 min Limitations >SN 505 Enroute Max Altitude FL 430 Max Temp ISA +39 C Max Generator Load Up to FL350 400 amps Above FL350 325 amps Min Autopilot on GS 95’ AGL Powerplant JT15D-4 N1 104.0 % N2 95.0 % ITT (Normal Start) 500 C ITT Take-Off (5 min) 700 C ITT Climb 680 C ITT Cruise 670 C ITT Idle 580 C Thrust-ISA, TO, 5 min 2500# Bypass Ratio 2.5 to 1 TBO 3500 hrs Fuel Quantity 5000# LO FUEL LEVEL 170-280# LO FUEL PRESS 5 psi Imbalance 600# Environmental Max Design Cabin Alt. 8000’ CAB ALT 10K FT 10,000’ Altitude Limiters 13,000’ (+/-1500) Masks Auto-Drop 13,500’ (+/-600) Max Cabin Differential 8.9 19 CE-550 Bravo Weights – in pounds Ramp 15,000 Takeoff 14,800 Landing 13,500 Zero Fuel 11,300 Opt. ZFW None Baggage, Nose 350 Baggage, Aft Left Side 650 Baggage, Tail Fwd area 300 Baggage, Tail Aft area 200 BEW, Typical 9,000 Speeds – in knots VMO to 8,000 260 VMO 8,000 to FL279 275 MMO <FL279 .700 VA 8600 lbs @ SL 140 14800 lbs @ FL370 220 Turbulent Air 180 Flaps 15 (TO & APR) 200 Flaps 40 (Land) 174 Gear VLO-extend 250 VLO-retract 200 VLE-extended 260 VMCG 78 VMCA 89 Tire Ground (Mains) 165 Autopilot VMO/MMO Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.4” Max Temp ISA +39 C Min Temp -54 C Max Tailwind 10 kts Starter 3 Starts in 30 min Generator Load 315 amps Battery-NICAD 3 starts/hr Tire pressure Nose 120+/-5 Mains 135+/-5 P/S heat on ground 2 min Limitations Enroute Max Altitude FL 450 Max Temp ISA +54 C Min Temp ISA -54 C Max Generator Load Up to FL350 400 amps Above FL350 315 amps Min Autopilot 500’ AGL Powerplant PW530A N1 100.0 % N2 100.0 % ITT (Start Limit) 740 C ITT (Normal Start) 550 C ITT Take-Off (5 min) 700 C ITT Idle 580 C Thrust-ISA, TO, 5 min 2887# Bypass Ratio 3.2 to 1 TBO 4000 hrs Oil Capacity 5 qts LO OIL PRESS 20 psi Fuel Quantity 4860# LO FUEL LEVEL 170-280# LO FUEL PRESS 5 psi Imbalance 600# Environmental Max Design Cabin Alt. 8000’ CAB ALT 10K FT 10,000’ Altitude Limiters 13,000’ (+/-1500) Masks Auto-Drop 13,500’ (+/-600) Max Cabin Differential 8.9 20 CE-551 Weights – in pounds Ramp 12,700 Takeoff 12,500 Landing 12,700 Zero Fuel 9,500 Opt. ZFW 11,000 Baggage, Nose 350 Baggage, Aft 650 Baggage, Tail NA BEW, Typical 8,000 Speeds – in knots VMO to 14,000 262 VMO 14 to FL280 277 VMO heavy ZFW <FL305 262 MMO .705 VA 8500 lbs @ SL 150 12500 lbs @ FL310 255 Turbulent Air 180 Flaps 15 (TO & APR) 202 Flaps 40 (Land) 176 Gear (ALL) 176 VMCG 62 VMCA 77 Tire Ground (Mains) 165 Autopilot VMO/MMO Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.4” Max Temp ISA +39 C Min Temp -54 C Max Tailwind 10 kts Starter 3 Starts in 30 min Generator Load 325 amps Battery-NICAD 3 starts/hr Tire pressure Nose 120+/-5 Mains 100+/-5 P/S heat on ground 2 min Limitations Enroute Max Altitude FL 430 Max Temp ISA +39 C Max Generator Load Up to FL350 400 amps Above FL350 325 amps Min Autopilot on GS 95’ AGL Powerplant JT15D-4 N1 104.0 % N2 95.0 % ITT (Normal Start) 500 C ITT Take-Off (5 min) 700 C ITT Climb 680 C ITT Cruise 670 C ITT Idle 580 C Thrust-ISA, TO, 5 min 2500# Bypass Ratio 2.5 to 1 TBO 3500 hrs Fuel Quantity 5000# LO FUEL LEVEL 170-280# LO FUEL PRESS 5 psi Imbalance 600# Environmental Max Design Cabin Alt. 8000’ CAB ALT 10K FT 10,000’ Altitude Limiters 13,000’ (+/-1500) Masks Auto-Drop 13,500’ (+/-600) Max Cabin Differential 8.9