Table of Contents
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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.
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
510OM-00
CITATION MUSTANG OPERATING MANUAL
AIRCRAFT GENERAL
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
1-1
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Table of Contents
Related Manuals for Cessna CITATION MUSTANG
Summary of Contents for Cessna CITATION MUSTANG
- Page 1 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.
- Page 2 The Citation Mustang is equipped with a STRUCTURES Garmin G-1000 integrated avionics system. This three-panel display system integrates flight The Citation Mustang (Figure 1-1) is an all- instruments, flight guidance, navigation, and metal, pressurized, low-wing monoplane with communication systems. Also integrated into a swept T-tail.
- Page 3 CITATION MUSTANG OPERATING MANUAL 43.17 FT (13.0 M) 11.79 FT (3.6 M) 13.10 FT (3.99 M) 14.35 FT (4.37 M) 40.56 FT (12.36 M) Figure 1-2. Exterior Three-View Drawing 510OM-00...
- Page 4 CITATION MUSTANG OPERATING MANUAL WING-TIP LIGHT TO CURB TO CURB WING TIP LIGHT 27.32 FEET 54.97 FEET (8.33 M) (16.75 M) 15.53 FEET (4.734 M) 11.79 FEET (3.59 M) Figure 1-3. Braking Taxi Turning Distance 27 FEET (8 M) 18 FEET (5.50 M)
- Page 5 CITATION MUSTANG OPERATING MANUAL ENTRANCE DOOR CAUTION The cabin entrance door is on the forward left The locking pins will contact and side of the fuselage (Figure 1-5). The entrance damage the painted surface of the door opens outboard and forward. It is se-...
- Page 6 CITATION MUSTANG OPERATING MANUAL Figure 1-6. Hinged Panel NOTE The water barrier is installed at the main cabin door threshold. Crew Figure 1-7. Door Pin Indicator members should be familiar with its location and operation; and passen- gers should be briefed prior to flights EMERGENCY EXIT over water.
- Page 7 CITATION MUSTANG OPERATING MANUAL measures approximately 14 feet in length, 4.7 feet in width, and 4.5 feet in height. Figure 1- 9 shows the interior arrangements. Refer to Figure 1-10 for interior dimensions. The standard interior arrangement consists of two aft-facing and two forward-facing passen- ger seats.
- Page 8 CITATION MUSTANG OPERATING MANUAL FORWARD 144.00 IN. 202.76 IN. 321.00 IN. PRESSURE (3,658 MM) (8,153 MM) (5,150 MM) BULKHEAD 24.00 IN. (610 MM) AFT PRESSURE BULKHEAD 46.00 IN. 54.00 IN. (1,168 MM) (1,372 MM) FORWARD DIVIDER (0.53 IN. THICK) (13 MM THICK)
- Page 9 CITATION MUSTANG OPERATING MANUAL This door opens the tail cone baggage compart- ment (Figure 1-11), which holds 300 pounds. Figure 1-12. Wing Trailing Edge Figure 1-11. Tail Cone Baggage Door The tail cone compartment door is secured at the aft side by mechanical latches and a key lock and is hinged at the left forward edge.
- Page 10 CITATION MUSTANG OPERATING MANUAL NOSE SECTION The nose section is an unpressurized storage area. Various hydraulics components, pneu- matic bottles, oxygen bottle, fresh-air duct, and radar antenna are located in this com- partment (Figure 1-15). The nose storage compartment holds up to 20-cubic feet (320- pounds) of baggage.
- Page 11 CITATION MUSTANG OPERATING MANUAL each produces approximately 1,460 pounds aileron, elevator, and rudder tabs. The eleva- of thrust (sea level ISA + 10°C). tor trim is both mechanically and electrically actuated. Aileron and rudder trim are electri- To improve automation and efficiency, the en- cally activated.
- Page 12 CITATION MUSTANG OPERATING MANUAL and navigation systems. The navigation sys- SINGLE-PILOT tem includes GPS, ground-based navigation, OPERATION and is WAAS-capable. An integrated engine indicating and crew alerting system (EICAS) is included. The Garmin G1000 system man- The following are required when the airplane...