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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.
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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
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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
_____________________
_____________________
_____________________
_____________________
_____________________
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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<SN505
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
HeavyCE-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 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>SN505
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
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CE-550Bravo
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
LimitationsEnroute 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
LimitationsEnroute 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
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