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Cessna Citation Mustang CE-510 Note Taking Guide

CESSNA 510 Citation Mustang · Wiring Diagram

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Overview

This document is a Note Taking Guide for the Cessna 510 Citation Mustang, designed to assist pilots in memorizing critical procedures and limitations. It includes memory items for emergency situations, takeoff briefings, and various system overviews such as fuel, electrical, hydraulics, and environmental systems. The guide emphasizes the importance of memorization for safety and operational efficiency, providing structured practice pages for pilots to fill out from memory. It also outlines key performance limitations and operational parameters essential for safe flight operations.

  • Ramp weight: 8,730 lbs
  • Takeoff weight: 8,645 lbs
  • Maximum altitude: FL 410
  • VMO: 250 knots, MMO: 0.63
  • Minimum battery voltage for NiCad: 22V

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
Wiring Diagram
Year
2021
Pages
19
File size
6.9 MB
Publisher
aeromania.net
How rare is it?
12CESSNA 510 Citation Mustang registered worldwide · 0 active

Common. Rarer than 6% of the aircraft models we track.

Documentation completeness
5/7

Most owners only have the POH. Here's the essential set for the CESSNA 510 Citation Mustang.

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In this document

Memory Items

This section outlines critical memory items for emergency situations during takeoff and approach. It specifies actions to take in case of engine failure, fire, or other non-normal events, including aborting takeoff below V1 and continuing above V1. Emergency restart procedures and responses to various failure scenarios are also detailed.

Takeoff Briefing

The takeoff briefing section provides a structured approach for pilots to memorize essential takeoff parameters, including V1, V2, and required runway lengths. It emphasizes the importance of communication during takeoff and outlines the sequence of calls and actions to ensure a safe departure.

Weights and Speeds

This section lists critical weight limits for the Cessna 510, including ramp weight (8,730 lbs), takeoff weight (8,645 lbs), and landing weight (8,000 lbs). It also details various speeds such as VMO (250 knots) and MMO (0.63), along with specific speeds for different configurations and conditions.

Limitations

The limitations section provides operational limits for the aircraft, including starting conditions, maximum altitude (FL 410), and temperature limits. It specifies battery voltage requirements for starting and generator load limits at different altitudes.

Environmental Systems

This section describes the environmental control systems of the Cessna 510, including cabin altitude limits and pressure differentials. It outlines the maximum design cabin altitude of 8,000 feet and the conditions under which cabin altitude warnings are activated.

Safety notes

  • Engine failure or fire during takeoff requires immediate action based on speed relative to V1.
  • Emergency descent procedures must be memorized and practiced regularly.

Full document text

Cessna Citation Mustang CE-510 Note Taking Guide +1.307.388.0026 ` Document Version 1.0 1 September 2021 © Aeromania, LLC 2021 ™ 2 Aeromania LLC CE510 Mustang Note Taking Guide Ver. 1.0 Original 9/1/2021 Table of Contents Memory Items ………………………………………………………………………………3 Takeoff Briefing ………………………………………………………………………………7 Stall / Missed Approach ………………………………………………………………7 Fuel ……………………………………………………………………..………8 Electrical …………………………………………………………………………..…9 Hydraulics …………………………………………………………………………….10 Environmental …………………………………………………………………………….11 Ice Protection …………………………………………………………………………….12 PRACTICE ………………………………………………………………………….…13 Limitations ………………………………………………………………………….…18 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 or Any Other Non-Normal Event During Takeoff Speed below V1 – takeoff should be aborted. Engine Failure or Fire or Master Warning or Any Other Non-Normal Event During Takeoff Speed above V1 – takeoff should be continued. Engine Failure During Approach (Possible ENGINE FAIL L-R CAS Message) Engine FIRE L or R (ENGINE FIRE Light Illuminated) Emergency Restart – Two Engines Starter Assist 20,000’ or lower 4 Engine Surges or Unstable Operation Electrical Fire or Smoke UNKNOWN SOURCE Electrical Fire or Smoke KNOWN SOURCE Smoke Removal, Environmental System Smoke or Odor Loss of Cabin Pressure (Red CABIN ALT CAS Message) 5 Emergency Descent Battery Over temperature (Red BATTERY O’TEMP CAS Message) Dual Generator Failure (Red GEN OFF L-R CAS Message) Hydraulic Wheel Brake Failure Autopilot Malfunction Aileron Trim Runaway 6 Rudder Trim Runaway Pitch Trim Runaway Inadvertent Stall (Buffet, and/or Roll-Off) Emergency Evacuation 7 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 8 Fuel LP LP T S 9 Electrical 10 Hydraulics 11 Environmental 12 Ice Protection 13 Practice Memory Items Engine Failure or Fire or Master Warning or Any Other Non-Normal Event During Takeoff Speed below V1 – takeoff should be aborted. Engine Failure or Fire or Master Warning or Any Other Non-Normal Event During Takeoff Speed above V1 – takeoff should be continued. Engine Failure During Approach (Possible ENGINE FAIL L-R CAS Message) Engine FIRE L or R (ENGINE FIRE Light Illuminated) Emergency Restart – Two Engines Starter Assist 20,000’ or lower 14 Engine Surges or Unstable Operation Electrical Fire or Smoke UNKNOWN SOURCE Electrical Fire or Smoke KNOWN SOURCE Smoke Removal, Environmental System Smoke or Odor Loss of Cabin Pressure (Red CABIN ALT CAS Message) 15 Emergency Descent Battery Over temperature (Red BATTERY O’TEMP CAS Message) Dual Generator Failure (Red GEN OFF L-R CAS Message) Hydraulic Wheel Brake Failure Autopilot Malfunction Aileron Trim Runaway 16 Rudder Trim Runaway Pitch Trim Runaway Inadvertent Stall (Buffet, and/or Roll-Off) Emergency Evacuation 17 Practice Takeoff Briefing ________________________________________________________ ________________________________________________________ ________________________________________________________ __________________________________ ________________________________________________________ ________________________________________________________ ________________________________________________________ _____________________ Practice Stall / Missed Approach _____________________, _____________________ _____________________, _____________________ _____________________ _____________________, _____________________ 18 CE-510 Mustang Weights – in pounds Ramp 8,730 Takeoff 8,645 Landing 8,000 Zero Fuel 6,750 Opt. ZFW 6,300 Baggage, Nose 320 Baggage, Tail 300 BEW, Typical 5,350 Speeds – in knots VMO SL to 27,120 250 MMO 0.63 VA 6000# @ SL 135 8645# @ FL410 170 Turbulent Air 160 Flaps 15 (TO & APR) 185 Flaps 30 (Land) 150 Gear VLO EXT & VLE 250 Gear VLO RET 185 VMCG 73 VMCA Flaps 0 92 VMCA Flaps 15 81 VMCA Flaps 30 74 Tire Ground (Mains) 160 Autopilot VMO/MMO Takeoff, Landing, Ground Max Altitude 14,000 Water or Slush 0.75” Max Temp ISA +50°C Min Temp -40°C Max Tailwind 10 kts Starter 3 Starts in 30 min Generator Lo Idle 150 amps Generator Hi Idle 300 amps Battery-NICAD 3 starts/hr Tire pressure Nose 125+/-5 Mains 88+/-5 P/S heat on ground 2 min Limitations Starting Minimum Battery Voltage NiCad 22 Lead Acid 24 Max Start Alt Batt 10,000’ Max Start Alt GPU 14,000’ GPU Max 29V & 1,100 amps Enroute Max Altitude FL 410 Max Temp +50°C @ SL Max Generator Load Up to FL300 300 amps Above FL300 280 amps Min Autopilot on GS 200’AGL Powerplant PW615F N1 & N2 100 % ITT (Normal Start) 500°C ITT Take-Off (5 min) 830°C ITT Climb & Cruise 830°C Thrust ISA, TO, 5 min 1460# Bypass Ratio 2.8 to 1 Oil Use 1 qt / 13.5 hrs Fuel Quantity 2580# FUEL LEVEL LO 170# FUEL PRESS LO 5 psi Imbalance Normal 200# Imbalance Demonstrated 600# Min fuel for Takeoff 400# Environmental Max Design Cabin Alt. 8000’ CABIN ALT amber CAS 8,500’ CABIN ALT red CAS 10,000’ Altitude Limiters 14,300’ Masks Auto-Drop 14,800’ Max Cabin Differential 8.6

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