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WARNING
If the ADG fails to deliver the required electrical power after
the GEN 1 and GEN 2 switches are set to OFF, the GEN 1
and GEN 2 switches must be reset immediately to ON, and
normal supply to the essential busses restored, by
pressing the PWR TXFR OVERRIDE switch, after
confirming that the ADG manual deploy handle is stowed.
(18) GEN 1 .................................................................................................................. OFF
• Check that GEN 1 OFF caution message comes on.
(19) GEN 2 .................................................................................................................. OFF
• Check that GEN 2 OFF caution message comes on.
IN-FLIGHT CHECKS
Air-Driven Generator Checks
Vol. 1 09−02−3
REV 73, May 14/08
▼
CL−604 Operating Manual
PSP 604−6
2. MANUAL DEPLOYMENT OPERATIONAL CHECK (CONT'D)
B. In-Flight Procedures (Cont’d)
(20) Primary display ................................................................................................. Check
• That EMER PWR ONLY warning message comes on,
• MACH TRIM caution message comes on, and
• All other indications are normal, except VIB = 0.0 .
(21) Pilot’s and copilot’s intercoms........................................................................... Check
(22) STAB TRIM, CH 2 switch/light........................................................... Check engaged
• STAB CH 1 INOP status message on.
(23) YAW DAMPER, YD 1 switch/light...................................................... Check engaged
• YD 1 INOP status message out.
(24) Pitch trim.........................................................................................................Operate
• To check that stabilizer trim operates normally.
IN-FLIGHT CHECKS
Air-Driven Generator Checks
Vol. 1 09−02−4
REV 73, May 14/08
▼
CL−604 Operating Manual
PSP 604−6
2. MANUAL DEPLOYMENT OPERATIONAL CHECK (CONT'D)
B. In-Flight Procedures (Cont’d)
(25) AC and DC essential busses ............................................................................ Check
• Verify that power is available on each bus. It is sufficient to confirm the normal
operation of one of the services powered by the bus. The following is a list of the
essential busses and the services appropriate for this check:
A. DC Essential Bus:
• VHF Nav 1 operational.
• ADF 1 operational.
• Transponder 1 operational.
• Pilot’s MFD and PFD with complete displays.
• Wing anti-ice, STBY (Check for ITT variation).
B. AC Essential Bus:
• ICE DETECTOR 1 FAIL status message out.
• ICE DET TEST: Select to DET and verify that L AOA HEAT, L PITOT BASE
HEAT, L PITOT TUBE HEAT, STBY PITOT HEAT, L STATIC HEAT and L
WINDOW HEAT caution messages out; then
LH WHSLD switch ....................................RESET
NOTE
L AOA HEAT, L PITOT BASE HEAT, L PITOT TUBE
HEAT, and STBY PITOT HEAT caution messages
may come on during ADG deployment. If this
occurs, reset circuit breaker 4A11.
C. Battery Bus:
• RAM AIR SOV operational.
• Copilot’s clock operational.
• Standby attitude indicator and altimeter/indicated airspeed indicators
operational.
• INTEG instruments panel lights operational.
(26) Hydraulic system No. 3 pressure.................................... Stabilized at 3,000 ±200 psi
(27) Landing gear lever ........................................................................ Cycle; UP then DN
• Check that hydraulic No. 3 system pressure does not go below 2,150 psi.
(28) Airspeed.......................................................................................................... Reduce
• Slow down to 130 KIAS or slowest practical safe speed and confirm the ADG output:
• ADG voltage ..................................................... 115 ±5 VAC
• Frequency..................................................340 Hz minimum
IN-FLIGHT CHECKS
Air-Driven Generator Checks
Vol. 1 09−02−5
REV 75, Feb 17/09
▼
CL−604 Operating Manual
PSP 604−6
2. MANUAL DEPLOYMENT OPERATIONAL CHECK (CONT'D)
B. In-Flight Procedures (Cont’d)
(29) Airspeed.................................................................................................... As required
• Resume normal airspeed for phase of flight, in accordance with the operating
limitations as established in Chapter 2.
(30) GEN 1 and GEN 2 ................................................................................................. ON
　
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