CAE SimuFlite Citation Bravo Installation guide

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Pilot Training Manual
Pilot Training Manual
Citation Bravo
Citation XLS
Revision 2
Revision 0

Printed in the United States of America.
Excerpted Materials used in this Publication
have been reproduced with permission of
the Cessna Aircraft Company.
Copyright 2013, CAE, Inc.
All Rights Reserved
NOTICE: This Citation Bravo Initial Pilot Training Manual is
to be used for Aircraft familiarization and training purposes
only. It is not to be used as, nor considered a substitute for,
the manufacturer’s Pilot or Maintenance Manual.

Introduction
Citation Bravo Developed for Training Purposes 1-1
March 2009
Welcome to
CAE
SimuFlite
Welcome to CAE SimuFlite!
Our goal is a basic one: to enhance your safety, proficiency and
professionalism within the aviation community. All of us at
CAE SimuFlite know that the success of our company depends
upon our commitment to your needs. We strive for excellence
by focusing on our service to you.
We urge you to participate actively in all training activities.
Through your involvement, interaction, and practice, the full
value of your training will be transferred to the operational
environment. As you apply the techniques presented through
CAE SimuFlite training, they will become “second nature” to
you.
Thank you for choosing CAE SimuFlite. We recognize that
you have a choice of training sources. We trust you will find us
committed to providing responsive, service-oriented training
of the highest quality.
Our best wishes are with you for a most successful and
rewarding training experience.
The Staff of CAE SimuFlite

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Introduction
Citation Bravo Developed for Training Purposes 1-3
March 2009
Using this
Manual
This manual is a stand-alone document appropriate for various
levels of training. Its purpose is to serve as an informational
resource and study aid.
The Quick Reference chapter provides limitations and other data
for quick review.
The Operating Procedures section contains chapters that pro-
vide a pictorial preflight inspection of the aircraft, normal proce-
dures in an expanded format, standard operating procedures,
maneuvers, and other information for day-to-day operations.
The Flight Planning chapter covers weight and balance and per-
formance; a sample problem is included.
The Systems section is subdivided by aircraft system. Each sys-
tem chapter contains a discussion of components, preflight and
servicing procedures, and abnormal and emergency procedures.
At the beginning of the Systems section, a list of systems is cross-
referenced to ATA codes to facilitate further self-study, if desired,
with the manufacturer’s manuals.
The graphics (right) in this manual direct your attention to a spe-
cific location in the cockpit. A shaded area locates various instru-
ments or switches shown in the adjacent photographs.

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Quick Reference
Citation Bravo Developed for Training Purposes 2-1
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Quick
Reference
This chapter contains the aircraft’s operating limits and require-
ments as well as system by system charts summarizing compo-
nents, power sources, distribution, monitors, and specific
limitations. All limitations are printed in bold italic.
It also contains sections on supplement-directed limitations and
operations, instrument markings, and operations in the United
Kingdom.
This chapter is intended to serve as a convenient reference.

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Quick Reference
Citation Bravo Developed for Training Purposes 2-3
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Table of
Contents
General Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5
Authorized Operations . . . . . . . . . . . . . . . . . . . . . . . . 2-5
Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5
Certification Status . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5
Emergency Exit Door Pin . . . . . . . . . . . . . . . . . . . . . . 2-5
Maneuvers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5
Minimum Crew . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5
Noise Levels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-6
Passenger Seat Position . . . . . . . . . . . . . . . . . . . . . . . 2-6
Operational Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-7
Maximum Design Weights . . . . . . . . . . . . . . . . . . . . . 2-7
Center of Gravity Moment Envelope . . . . . . . . . . . . . . 2-7
Center of Gravity Limits . . . . . . . . . . . . . . . . . . . . . . . . 2-8
Speed Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-9
Takeoff and Landing Operational Limits . . . . . . . . . . 2-11
Enroute Operational Limits . . . . . . . . . . . . . . . . . . . . 2-12
Load Factors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-12
Icing Factors
(Airworthiness Directive 98-04038) . . . . . . . . . . . . . . 2-13
System Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-15
Avionics and Communications . . . . . . . . . . . . . . . . . 2-15
Electrical and Lighting Systems . . . . . . . . . . . . . . . . 2-17
Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-18
Hydraulic Fluid . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-19
Ice and Rain Protection . . . . . . . . . . . . . . . . . . . . . . . 2-20
Landing Gear and Brakes . . . . . . . . . . . . . . . . . . . . . 2-21
Miscellaneous Systems . . . . . . . . . . . . . . . . . . . . . . . 2-21
Pneumatic and Pressurization Systems . . . . . . . . . . 2-22
Powerplant – Pratt and Whitney . . . . . . . . . . . . . . . . 2-23
Instrument Markings . . . . . . . . . . . . . . . . . . . . . . . . . . 2-29
System Data Summaries . . . . . . . . . . . . . . . . . . . . . . . 2-31
Electrical Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-31
Fire Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-32
Flight Controls Systems . . . . . . . . . . . . . . . . . . . . . . 2-33

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Fuel System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-35
Hydraulic System . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-36
Ice and Rain Protection . . . . . . . . . . . . . . . . . . . . . . 2-37
Landing Gear and Brakes . . . . . . . . . . . . . . . . . . . . 2-40
Oxygen Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-42
Pneumatic Systems . . . . . . . . . . . . . . . . . . . . . . . . . 2-43
Thrust Reverser System . . . . . . . . . . . . . . . . . . . . . . 2-46
AFM Supplements . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-47
EROS Oxygen Mask . . . . . . . . . . . . . . . . . . . . . . . . 2-47
Flood Cooling System . . . . . . . . . . . . . . . . . . . . . . . 2-47
Global GNS-XLS Flight Management System
(Single or Dual) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-48
Gravel Runway Modification . . . . . . . . . . . . . . . . . . 2-49
Honeywell Primus-1000 Flight Guidance System . . 2-50
Honeywell LSZ-850 Lightning Sensor System . . . . . 2-51
UNS-1Csp (Single) or UNS-1K (Single or Dual)
Flight Management System
(with or without Unilink) . . . . . . . . . . . . . . . . . . . . . . . . . .2-