Cessna CITATION MUSTANG User Manual (English)

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INTRODUCTION

This manual provides a description of the major airframe and engine systems in the Cessna

Citation Mustang (Figure 1-1). This material does not supersede, nor is it meant to sub-

stitute for, any of the manufacturer’s maintenance or flight manuals. The material pre-

sented has been prepared from current design data. Chapter 1 covers the structural makeup

of the airplane and gives an overview of the systems.

CITATION MUSTANG OPERATING MANUAL

510OM-00

1-1

GENERAL

The Citation Mustang is certified in accor-

dance with Title 14 of the Code of Federal

Regulations (14CFR23) Part 23, including

day, night, visual flight rules (VFR), instru-

ment flight rules (IFR), single pilot, and flight

into known icing conditions. Takeoff and land-

ing performance and other special condition

certification requirements are similar to

14CFR Part 25. The Mustang meets 14CFR

Part 36 noise standards, and meets 14CFR

Part 34 fuel venting and exhaust emission

standards. It combines systems simplicity with

ease of access to reduce maintenance require-

ments. Low takeoff and landing speeds permit

operation at small airports. Medium bypass tur-

bofan engines contribute to overall operating

efficiency and performance.

CHAPTER 1

AIRCRAFT GENERAL

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Cessna CITATION MUSTANG Specifications

General

Manufacturer	Cessna
Model	Citation Mustang
Type	Very Light Jet
Crew	2
Passenger Capacity	4-5
Engines	2 × Pratt & Whitney Canada PW615F turbofans
Length	40 ft 7 in
Wingspan	43 ft 2 in (13.16 m)
Height	13 ft 5 in
Thrust	1, 460 lbf each
Cruise Speed	391 mph
Service Ceiling	41, 000 ft (12, 500 m)
Rate of Climb	3, 010 ft/min