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PROCEDURE COMPLETED
• ON GROUND
1. Pitot-Static Switch . . . . . . . . . . . . . . . . PITOT-STATIC, verify message clears then OFF
CAUTION
Pitot probes may be damaged if the pitot/static heat is operated for more than
2 minutes on the ground.
PROCEDURE COMPLETED
510FM-07 AA 3-85
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
SEVERE ICING ENCOUNTER
Severe icing may be encountered at temperatures as cold as -18°C. Increased vigilance is
required at temperatures around 0°C ambient air temperature with visible moisture present.
NOTE
The following weather conditions may be conducive to severe in-flight icing:
• Visible rain at temperatures colder than 0°C ambient air temperature.
• Droplets that splash or splatter at temperatures colder than 0°C ambient air
temperature.
IF SEVERE ICING IS PRESENT
One or more of the following visual cues indicates severe icing conditions:
• Unusually extensive ice accumulations on the airframe and windshield in areas not normally
observed to collect ice.
• Accumulation of ice on the upper surface of the wing aft of the protected area.
1. Immediately report weather conditions and request priority handling from Air Traffic Control
to facilitate a route or altitude change to exit the severe icing conditions.
2. Flaps. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LEAVE IN CURRENT POSITION
(Do not extend or retract until airframe is clear of ice)
NOTE
Operation with flaps extended can result in a reduced wing angle-of-attack with the
possibility of ice forming on the upper surface further aft on the wing than normal,
possibly aft of the protected area.
3. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Hold control wheel firmly and DISENGAGE
CAUTION
Exert control wheel force as required to maintain desired flight path.
4. Avoid abrupt and excessive maneuvering that may aggravate control problems.
5. If unusual or uncommanded roll is encountered. . . . . . . . . REDUCE ANGLE OF ATTACK
PROCEDURE COMPLETED
3-86 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
STALL WARN HTR
(STALL WARNING VANE HEATER FAILURE)
Indicates that no power is being supplied to the stall warning vane.
1. PITOT-STATIC Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PITOT-STATIC
2. STALL WARN HEAT Circuit Breaker (R circuit breaker panel). . . . . . . . . . . . . . . . . CHECK
• IF IN ICING CONDITIONS AND MESSAGE DOES NOT CLEAR
3. Exit icing environment.
4. Airspeed (except approach and landing) . . . . . . . . . . . . . . . . . . . . 160 KIAS MINIMUM
5. Airspeed (approach and landing) . . . . . . . . . . . . . . . . . . . . . VAPP/VREF MINIMUM from
STALL WARNING-HIGH performance charts for approach and landing
WARNING
If the Stall Warning Vane becomes iced, the following systems may
provide invalid data:
• Stall Warning Horn with automatic autopilot disconnect.
• Low-speed awareness range on Airspeed Indicator.
• On-speed circle.
PROCEDURE COMPLETED
• IF NOT IN ICING CONDITIONS OR MESSAGE CLEARS
PROCEDURE COMPLETED
T2 HTR FAIL (ENGINE T2 HEATER FAILURE)
Indicates that there is no current to the T2 heater on the affected side when ENGINE ANTI-ICE
Switch has been selected ON for that side.
• ON GROUND
1. Correct prior to flight.
PROCEDURE COMPLETED
• IN FLIGHT
1. Exit icing environment.
PROCEDURE COMPLETED
510FM-07 AA 3-87
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
TAIL DE-ICE FAIL
Indicates that one or more segments of the horizontal or vertical tail deice boot system did not
reach the required pressure when commanded or that pressure is present when not
commanded.
• IF WING/STAB DEICE SWITCH AUTO OR MANUAL
1. Throttles . . . . . . . . . . . . . . . . . . . . . . INCREASE POWER (as required above 70% N2)
2. WING/STAB Deice Switch . . . . . . . . . OFF (Verify TAIL DE-ICE FAIL message clears)
3. WING/STAB Deice Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HOLD IN MANUAL
(SURFACE DE-ICE message should display within 6 seconds)
4. WING/STAB Deice Switch . . . . . . . . . . . . . . . . . . . . . . . . . AUTO for at least 2 minutes
IF TAIL DE-ICE FAIL MESSAGE REMAINS DISPLAYED OR
DISPLAYS AGAIN
5. Exit icing environment.
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Citation Mustang airplane flight manual 1(68)
