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NOTE: Start valve should close by 44.5% HP RPM. On SPZ-8000
equipped airplanes, the SVO mnemonic changes from blue to amber
above 42% (44.5% on SPZ-8400 equipped airplanes) and starts flashing.
Check at ground idle HP RPM, and if not closed (SVO still illuminated),
execute Start Valve Failure checklist, page EC-17.
15. TGT .........................................................MONITOR (700° C MAX)
NOTE: During starting, TGT should not exceed 700°C. If there is any
evidence of rapid rising TGT and it is anticipated that 700°C will be
exceeded, select HP fuel cock to SHUT immediately. If TGT has not
exceeded 700°C, a second start may be attempted. If, under normal
starting conditions, TGT exceeds 650°C, this will indicate a fault in the
engine or starting systems.
NOTE: Hot Start checklist, if needed, is on page EC-18.
16. Engine RPM ..................................CHECK (46.6% HP MINIMUM)
17. Oil Pressure and Temperature............................................CHECK
18. EVM.....................................................................................CHECK
NOTE: The EVM system is designed to monitor engine vibrations
at idle and above. During start, the EVM system may occasionally
display momentary EVM values above the ALERT level (0.60)
which in turn causes EVM digits to an amber display momentarily
on CAS (SPZ-8400 equipped airplanes). This normally occurs on
the first start of the day.
19. SNGL RUDDER LIMIT Message (right engine only running).....ON
20. Hydraulic Pressure ........................ CHECKED (0 / 3000 / 3000 / 0)
21. Flight Data Recorder Fail Message............................ CHECK OUT
22. Second Engine Start........................ REPEAT STEPS 10 THRU 18
23. SNGL RUDDER LIMIT Message (both engines running) ........OUT
24. Hydraulic Pressure ........................ CHECKED (3000 / 3000 / 0 / 0)
END
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page NC - 8 May 30/02
Notes
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page ND - 1
After Starting Engines AFM 2-04-10
1. START MASTER...................................................................... OFF
2. Electrical Power..........................................................................ON
3. External Electrical Power / Air ................OFF / CARTS REMOVED
4. Auxiliary Electrical Power / Air / Engine Bleed Air ......AS DESIRED
NOTE: Only one source of bleed air, either APU or engines, should be
selected after engines are started. This is to prevent thermal transients
on the APU or possible damage to the APU when the power levers are
moved from idle. With engines as source of bleed air, ensure the
isolation valve is CLOSED.
5. Battery Ammeters................................................................CHECK
6. ESS DC Bus Power Source ....AUTO / LEFT MAIN ILLUMINATED
CAUTION: DO NOT DISPATCH WITH ESS DC BUS POWERED BY
THE BATTERIES.
7. Emergency Power ....................................................................ARM
8. Doors................................................................................... CLOSE
NOTE: Check that the orange dot position indicators on each of the six
locking pins is visible.
9. Anti-Ice Heaters..........................................................................ON
SN 1096 and subs. (5); SN 1000 through 1095 (4).
10. Cowl / Wing Anti-Ice................................ CHECK / AS REQUIRED
NOTE: To prevent excessive APU EGT, check or select cowl anti-ice /
wing anti-ice ON using engine bleed air only.
11. Pressurization Control ................................. AUTO / FLIGHT / SET
12. Fuel Boost Pumps / Crossflow Valve ....................... ON / CLOSED
13. Nose Wheel Steering ............................................................... OFF
14. Ground Spoilers (Sys. Check: Pg. NH-7) ............................CHECK
NOTE: Check on first flight of the day.
15. Stall Barrier (Sys. Check: Pg. NH-9) ...................................... TEST
NOTE: Check on first flight of the day. If flight time for the day exceeds
eight (8) hours, a second stall barrier check is required prior to the
second flight of the day.
16. Flight Controls / Rudder Torque Limiter ..............................CHECK
17. Yaw Damper...............................................................................ON
18. Nose Wheel Steering .................................................................ON
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page ND - 2 May 30/02
19. Pedal Steering Disconnect Switch .....................ON / LIGHTS OUT
20. Auxiliary Hydraulic Pump ....................................................ARMED
　
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