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10. Flight Compartment, Instrumentation and Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
10.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
10.2 Instrument and Control Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
10.3 Flight Compartment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
10.4 Avionics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14
11. Interior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
11.1 General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
11.2 Standard Interior Configuration . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
11.3 Baggage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
12. Exterior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
13. Additional Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
14. Emergency Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20
15. Documentation and Technical Publications . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
16. Computerized Maintenance Record Service (CESCOM) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
17. Limited Warranties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
17.1 Cessna Citation Mustang Limited Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
17.2 Pratt & Whitney Canada Corp. New Engine Warranty . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22
18. Citation Mustang Crew Training Agreement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23
FIGURE I — CITATION MUSTANG EXTERIOR DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
FIGURE II — CITATION MUSTANG INTERIOR DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5
FIGURE III — CITATION MUSTANG INSTRUMENT PANEL AND PEDESTAL LAYOUT . . . . . . . . . . . . . . . . . . . . . 13
FIGURE IV — CITATION MUSTANG STANDARD FLOORPLAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
September 2006
3
MANUFACTURER CESSNA AIRCRAFT COMPANY
MODEL 510
1. GENERAL DESCRIPTION
The Cessna Citation Mustang is a low-wing aircraft with
retractable tricycle landing gear and a T-tail. A pressurized
cabin accommodates a crew of two and up to four
passengers in a spacious club seating arrangement.
Two FADEC controlled Pratt & Whitney Canada (P&WC)
PW615F turbofan engines are pylon-mounted on the
rear fuselage. Fuel stored in the wings offers generous
range for missions typical of this class aircraft. Space for
baggage is provided in the nose and tailcone with additional
storage space available in the cabin.
Multiple structural load paths and system redundancies
have been built into the aluminum airframe. Metal
bonding techniques have been used in many areas for
added strength and reduced weight. The nose radome
and bullet fairings are made of composite materials to
save weight. The airframe design incorporates anti-corrosion
applications and lightning protection.
Cessna offers a third-party training package for one pilot
and one mechanic, and various warranties as described
in this book. Cessna's worldwide network of companyowned
and authorized service centers provides a complete
source for all servicing needs.
1.1 Certification
The Model 510 is certified to the requirements of U.S. 14
CFR Part 23 including day, night, VFR, IFR, and flight
into known icing conditions. It is also certified for single
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Specification & Description(2)
