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aircraft systems relying on WOW signals may be inoperative
or operate incorrectly.
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS messages listed here display L-R for example.
INHIBITS
Table 4-4. AMBER CAS MESSAGES (Cont)
CITATION MUSTANG OPERATING MANUAL
510OM-00 4-15
Table 4-5. WHITE CAS MESSAGES
ESI
TOPI
AIR
LOPI
ESDI
EMER
GND
MESSAGE DESCRIPTION
CABIN ALT High-altitude mode only—In flight, the white CABIN ALT ¸ ¸ ¸
message appears any time the cabin altitude is between
10,000 and 15,000 feet for less than 30 minutes.
ENG A/I COLD L-R* Indicates that the engine inlet temperature is below safe level ¸ ¸
for satisfactory ice protection. This message will post in white for
up to two minutes after engine anti-ice is turned on while the inlet
warms up to the normal operating temperature.
FUEL BOOST L-R* Appears when the pilot commands the fuel boost pump on ¸
(by selecting the FUEL TRANSFER knob to L TANK or R
TANK, or by selecting a FUEL BOOST L-R switch to ON, or
during an engine start.
FUEL LO INOP L-R* Indicates the amber FUEL LVL LO L-R message is not ¸ ¸
operational and cannot provide reliable indication of fuel level.
FUEL TRANSFER Indicates the fuel transfer valve is open. ¸
NO TIRE SPINDOWN Indicates the antiskid control spindown function is not working. ¸ ¸
PRESS CTRL Indicates failure of the ARINC 429 data link from the G1000 ¸ ¸ ¸
system, indicating that the controller may no longer have
valid data on outside air pressure, actual aircraft altitude,
or destination elevation.
PRESS OFF Appears when the crew selects the AIR SOURCE SELECT ¸ ¸
knob to either OFF or FRESH AIR. This alerts the crew there
is no bleed-air inflow to pressurize the cockpit or cabin. All
pressurization leaks out of the pressure vessel, which causes
it to depressurize.
SPD BRK EXTEND Indicates the speedbrakes are extended on either side. ¸
STALL WARN HI Indicates the stall warning system is operating on the ¸ ¸
ice-contaminated schedule.
SURFACE DE-ICE AUTO mode—Indicates when all pressure switches for the ¸
inflation sequence (lower wing/left tail or upper wing/right
and vertical tail) are indicating deice boot inflation. The pilot
must verify the appearance of the white SURFACE DE-ICE
message following activation of the surface deice system
to protect against failures of the WING/STAB switch.
MANUAL mode—Displays if all pressure switches indicate
deice boot inflation.
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS messages listed here display L-R for example.
INHIBITS
CITATION MUSTANG OPERATING MANUAL
4-16 510OM-00
Table 4-5. White CAS Messages (Cont)
ESI
TOPI
AIR
LOPI
ESDI
EMER
GND
MESSAGE DESCRIPTION
W/S A/I FAIL L-R* Normal indication after windshield heat is turned on. ¸
Turns amber if condition exists for more than 5 seconds.
W/S O’HEAT L-R* Normal indication after windshield heat is turned on. ¸
Turns amber if condition exists for more than 5 seconds.
*Only affected side displayed (L, R, or L-R) in a CAS message; applicable CAS messages listed here display L-R for example.
INHIBITS
CHAPTER 5
FUEL SYSTEM
CONTENTS
Page
INTRODUCTION ................................................................................................................... 5-1
GENERAL.............................................................................................................................. 5-1
FUEL STORAGE.................................................................................................................... 5-3
Description ....................................................................................................................... 5-3
Components ..................................................................................................................... 5-3
Controls and Indications .................................................................................................. 5-4
Operation......................................................................................................................... 5-4
FUEL DISTRIBUTION .......................................................................................................... 5-5
Description ....................................................................................................................... 5-5
Components ..................................................................................................................... 5-5
　
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