Cessna Citation CE-550 JT-15
Note Taking Guide
+1.307.388.0026
Document Version 1.1 20 April 2017 © Aeromania, LLC 2017
™ 2
Aeromania LLC CE 550 Note Taking Guide Ver. 1.0 Original 3/15/2016 Ver 1.1 Cover & edits 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
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Practice Stall / Missed Approach
______
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______17
CE-550 Limitations Weights – in pounds Enroute Ramp 13,500 Max Altitude FL 430 Takeoff 13,300 Max Temp ISA +39 C Landing 12,700 Max Generator Load Zero Fuel 9,500 Up to FL350 400 amps Opt. ZFW 11,000 Above FL350 325 amps Baggage, Nose 350 Min Autopilot on GS 95’ AGL Baggage, Aft 650 Baggage, Tail 500 BEW, Typical 8,000 Powerplant JT15D-4 N1 104.0 % N2 95.0 % Speeds – in knots ITT (Normal Start) 500 C VMO to 14,000 262 ITT Take-Off (5 min) 700 C VMO 14 to FL280 277 ITT Climb 680 C VMO heavy ZFW Takeoff, Landing, Ground Max Altitude 14,000 Environmental Water or Slush 0.4” Max Design Cabin Alt. 8000’ Max Temp ISA +39 C CAB ALT 10K FT 10,000’ Min Temp -54 C Altitude Limiters 13,000’ Max Tailwind 10 kts (+/-1500) Starter 3 Starts in 30 min Masks Auto-Drop 13,500’ Generator Load 325 amps (+/-600) Battery-NICAD 3 starts/hr Max Cabin Differential 8.9 Tire pressure Nose 120+/-5 Mains 108+/-5 P/S heat on ground 2 min 18 Heavy CE-550 Limitations >SN 505 Weights – in pounds Enroute Ramp 14,300 Max Altitude FL 430 Takeoff 14,300 Max Temp ISA +39 C Landing 12,700 Max Generator Load Zero Fuel 9,500 Up to FL350 400 amps Opt. ZFW 11,000 Above FL350 325 amps Baggage, Nose 350 Min Autopilot on GS 95’ AGL Baggage, Aft 650 Baggage, Tail 500 BEW, Typical 8,300 Powerplant JT15D-4 N1 104.0 % Speeds – in knots N2 95.0 % VMO to 14,000 262 ITT (Normal Start) 500 C VMO 14 to FL280 277 ITT Take-Off (5 min) 700 C VMO heavy ZFW Takeoff, Landing, Ground Environmental Max Altitude 14,000 Max Design Cabin Alt. 8000’ Water or Slush 0.4” CAB ALT 10K FT 10,000’ Max Temp ISA +39 C Altitude Limiters 13,000’ Min Temp -54 C (+/-1500) Max Tailwind 10 kts Masks Auto-Drop 13,500’ Starter 3 Starts in 30 min (+/-600) Generator Load 325 amps Max Cabin Differential 8.9 Battery-NICAD 3 starts/hr Tire pressure Nose 120+/-5 Mains 108+/-5 P/S heat on ground 2 min 19 CE-550 Bravo Limitations Weights – in pounds Enroute Ramp 15,000 Max Altitude FL 450 Takeoff 14,800 Max Temp ISA +54 C Landing 13,500 Min Temp ISA -54 C Zero Fuel 11,300 Max Generator Load Opt. ZFW None Up to FL350 400 amps Baggage, Nose 350 Above FL350 315 amps Baggage, Aft Left Side 650 Min Autopilot 500’ AGL Baggage, Tail Fwd area 300 Baggage, Tail Aft area 200 BEW, Typical 9,000 Powerplant PW530A N1 100.0 % Speeds – in knots N2 100.0 % VMO to 8,000 260 ITT (Start Limit) 740 C VMO 8,000 to FL279 275 ITT (Normal Start) 550 C MMO Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.4” Environmental Max Temp ISA +39 C Max Design Cabin Alt. 8000’ Min Temp -54 C CAB ALT 10K FT 10,000’ Max Tailwind 10 kts Altitude Limiters 13,000’ Starter 3 Starts in 30 min (+/-1500) Generator Load 315 amps Masks Auto-Drop 13,500’ Battery-NICAD 3 starts/hr (+/-600) Tire pressure Nose 120+/-5 Max Cabin Differential 8.9 Mains 135+/-5 P/S heat on ground 2 min 20 CE-551 Limitations Weights – in pounds Enroute Ramp 12,700 Max Altitude FL 430 Takeoff 12,500 Max Temp ISA +39 C Landing 12,700 Max Generator Load Zero Fuel 9,500 Up to FL350 400 amps Opt. ZFW 11,000 Above FL350 325 amps Baggage, Nose 350 Min Autopilot on GS 95’ AGL Baggage, Aft 650 Baggage, Tail NA BEW, Typical 8,000 Powerplant JT15D-4 N1 104.0 % Speeds – in knots N2 95.0 % ITT (Normal Start) 500 C VMO to 14,000 262 ITT Take-Off (5 min) 700 C VMO 14 to FL280 277 ITT Climb 680 C VMO heavy ZFW Flaps 40 (Land) 176 Gear (ALL) 176 Fuel VMCG 62 Quantity 5000# VMCA 77 LO FUEL LEVEL 170-280# Tire Ground (Mains) 165 LO FUEL PRESS 5 psi Autopilot VMO/MMO Imbalance 600# Takeoff, Landing, Ground Max Altitude 14,000 Environmental Water or Slush 0.4” Max Design Cabin Alt. 8000’ Max Temp ISA +39 C CAB ALT 10K FT 10,000’ Min Temp -54 C Altitude Limiters 13,000’ Max Tailwind 10 kts (+/-1500) Starter 3 Starts in 30 min Masks Auto-Drop 13,500’ Generator Load 325 amps (+/-600) Battery-NICAD 3 starts/hr Max Cabin Differential 8.9 Tire pressure Nose 120+/-5 Mains 100+/-5 P/S heat on ground 2 min