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30,000
34,000
40,000
197
258
350
492
77 48 35 27
Table 17-1. OXYGEN SUPPLY DURATION
CAS message WOW MISCOMPARE warns of
the difference.
Malfunctions of the squat switches
and their associated circuits may
cause abnormal functioning of any or
all of the aircraft systems that use
squat switch information.
Dependent Systems
The following systems require squat switch information
for normal functioning:
• External doors
• Engine/FADEC
• Pneumatics
• Windshield anti-ice
• Air conditioning
• Pressurization
• Landing gear
• Brakes (antiskid)
• Avionics
• Stall warning
CONTROLS AND INDICATIONS
L and R SQUAT SWITCH Circuit
Breakers
Each squat switch (left and right) is powered
through the corresponding L or R SQUAT
SWITCH circuit breaker in the ENGINE SYSTEMS
section of the corresponding CB panel
(left or right).
WOW MISCOMPARE Message
The amber CAS message WOW MISCOMPARE
indicates that the squat switch system is indicating
different status (miscompare) of the two
switches. One squat switch appears to indicate
weight-on-wheels while the other appears to
indicate weight-off-wheels. The message does
not display until the miscompare has continued
for 2 seconds. This allows for momentary differences
during takeoff and landing.
The miscompare may be caused by:
• Different wheel positions
• Stuck squat switch
• Electrical short or open circuit
• Problems with the multi-function PCB
• Popped L or R SQUAT SWITCH circuit
breaker
• Loss of power to a squat switch
EMERGENCY/ABNORMAL
For specific information on emergency/abnormal
procedures, refer to the appropriate abbreviated
checklists or the FAA-approved AFM.
CAUTION
17-12 510OM-00
CITATION MUSTANG OPERATING MANUAL
CHAPTER 18
MANEUVERS AND PROCEDURES
CONTENTS
INTRODUCTION................................................................................................................. 18-1
GENERAL ............................................................................................................................ 18-1
PERFORMANCE.................................................................................................................. 18-2
Takeoff and Landing Speeds ......................................................................................... 18-2
Weights .......................................................................................................................... 18-2
FLIGHT OPERATIONS ....................................................................................................... 18-3
Preflight and Taxi........................................................................................................... 18-3
Takeoff ........................................................................................................................... 18-5
AIRWORK MANEUVERS .................................................................................................. 18-6
Steep Turns .................................................................................................................... 18-6
Approach to Stalls ......................................................................................................... 18-6
Unusual Attitude Recoveries ......................................................................................... 18-7
Miscellaneous ................................................................................................................ 18-7
CITATION MUSTANG OPERATING MANUAL
510OM-00 18-i
CITATION MUSTANG OPERATING MANUAL
18-ii 510OM-00
INTENTIONALLY LEFT BLANK
ILLUSTRATIONS
Figure Title Page
18-1 Takeoff and Landing Data Card............................................................................. 18-3
18-2 Takeoff—Normal ................................................................................................... 18-9
18-3 Takeoff—Engine Failure (Speed Below V1) ....................................................... 18-10
18-4 Takeoff—Engine Failure (At or Above V1)......................................................... 18-11
18-5 VFR Approach—Normal..................................................................................... 18-12
18-6 VFR Approach—Single Engine .......................................................................... 18-13
18-7 ILS Approach—Normal....................................................................................... 18-14
　
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