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.
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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