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45. Non Essential Static Source (if installed) ................................... ON
46. Emergency Flap Handle..................................................NEUTRAL
47. Emergency Flap Switch............................... NORMAL / GUARDED
48. Smoke Detector ..................................................................... TEST
49. RH R / R Fan Indicator (SN 1156 and subs)..........................AUTO
Quick Reference Handbook
REVISION 7 NORMAL PROCEDURES
May 30/02 Page NC - 3
Instrument Panel:
50. Clocks..................................................................................CHECK
51. Display Controllers ..............................................................CHECK
52. EFIS........................................................................................ TEST
53. EICAS ..................................................................................... TEST
54. IRSs..............................................................................NAV / TEST
55. ELWS (APU) Loadmeter ..............................................TEST / OFF
NOTE: For airplanes SN 1156 through 1429, and SN 1000 through
1155 with APU loadmeter not having ASC 420: If the ELWS (APU
loadmeter) is used for dispatch, see Operational Procedures With
Converter / Alternator Inoperative - ELWS Installed, page EA-10.
Selecting ELWS loadmeter ON causes spurious readings unless the
EPMP is properly configured for ELWS use.
56. Standby Engine Instruments ................................................. AUTO
NOTE: Compare static indications with EICAS on first flight of day.
57. Guidance Controller.............................................................CHECK
58. Thrust Reverser Lights ........................................................CHECK
A. REV ARM ..............................................................................ON
B. REV Unlock / Deploy ...........................................................OUT
NOTE: If either or both UNLOCK or DEPLOY lights are ON,
maintenance is required before flight.
59. Standby Attitude Indicator ............................................. UNCAGED
60. Standby Warning Lights Panel (SPZ-8000 Only) .......AS DESIRED
NOTE: The standby warning lights panel is not installed on SPZ-8400
equipped airplanes.
61. Fuel Quantity (Normal and Standby) ...................................... TEST
62. DBDIs ..................................................................................... TEST
NOTE: The DBDI will return to standby after TEST unless the
corresponding IRS is in NAV.
63. Cabin Pressurization Controller................................................ SET
64. Flap Indicator.......................................................................CHECK
65. Gear Handle .........................................................................DOWN
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page NC - 4 May 30/02
Center Pedestal:
66. Fire Handles................................................................................. IN
67. Power Levers ...........................................................................IDLE
68. Gust Lock ................................................................AS REQUIRED
69. Ground Spoiler Flap Override Switch........................................OFF
70. Speed Brake Handle .......................................................RETRACT
71. Elevator Trim (Sys. Check: Pg. NH-6) ...................... CHECK / SET
See next page for recommended elevator trim tab settings.
72. Stall Barrier................................................................................. ON
73. Anti-Skid..................................................................................... ON
74. Ground Spoilers ........................................................................OFF
75. T/REV EMER STOW Switch.....................................................OFF
76. Nutcracker Test Switch ..........................................GUARD DOWN
CAUTION: DO NOT DEPRESS THE NUTCRACKER TEST SWITCH
WHILE THE AIRPLANE IS ON THE GROUND. DEPRESSING THE
TEST SWITCH SIMULATES THE IN-FLIGHT CONDITION, WHICH
AFFECTS MANY AIRPLANE SYSTEMS, INCLUDING MOMENTARILY
UNLOCKING THE LANDING GEAR HANDLE DOWNLOCK SOLENOID.
77. Parking Brake............................................................................. ON
78. Brake Accumulator Pressure ............................................ 3000 PSI
79. Flight Power Shutoff Handle ................................................DOWN
80. Radios .......................................................................................SET
81. TCAS / TCAS MODE / SET UP ................ TEST / TA-RA / ABOVE
　
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