(b)
FLIGHT RECORDER AC

(2)
Close the following circuit breakers on the P6 circuit breaker panel:

(a)
ENGINE NO. 1 THRUST REV DC

(b)
ENGINE NO. 2 THRUST REV DC

(c)
INDICATOR (3 places)

(d)
LANDING GEAR LIGHTS

(e)
AURAL WARN

(f)
EPR WARN

(g)
ENG 1 EPR & LG WARN

(h)
ENG 2 EPR & LG WARN

(i)
LEVER LATCH & PRESS WARN

(3)
Position landing gear selector lever to OFF.

(4)
Check that standby hydraulic system is not pressurized.

(5)
Move engine No. 1 thrust reverser override switch to OVERRIDE.

(a) The ISOLATION VALVE light shall illuminate.

(6)
Return engine No. 1 thrust reverser override switch to NORMAL.

(a) The ISOLATION VALVE light shall extinguish.

(7)
Repeat steps (5) and (6) using engine No. 2 thrust reverser override switch.

(8)
With landing gear selector lever in OFF position, pressurize standby hydraulic system.

(9)  
Lift engine No. 1 reverse thrust lever to limit of travel.

(a)  
The engine No. 1 thrust reverser shall not deploy.

(b)  
All lights shall remain extinguished.

(10)
Return No. 1 reverse thrust lever to stow position.

(11)
Repeat steps (9) and (10) using No. 2 reverse thrust lever.

(12)
Depressurize standby hydraulic system.

(13)
Position stabilizer so that stabilizer position indicator pointer is within one unit of center of green band.

(14)
Place speed brake lever in zero degree detent (STOWED) position.

(15)
Check that thrust levers are at idle position.

(16)
Fully retract flaps and place flap lever in zero degree detent position.

(17)
Check that landing gear ground lockpins are installed in all landing gear.

(18)
Start engine No. 1 (Ref 71-09-100).

(a)  Check that flight recorder starts operating during start of engine No. 1

(19)
Start engine No. 2 (Ref 71-09-100).

(20)
Slowly advance engine No. 1 thrust lever.

(a) The takeoff warning horn shall sound before the EPR indicator reads 1.48 maximum.

(21)
Slowly retard the No. 1 thrust lever.

(a)  The warning horn shall cease sounding before the EPR indicator reads 1.32 minimum.

(22)
Return thrust lever to idle stop.

NOTE:  Below approximately -20 degrees F (-29 degrees C), an indicated EPR of 1.48 may be commanded before the throttle lever reaches 13.5 degrees from the idle stop, depending on engine model installed. Under these conditions, the horn will start sounding at 13.5 degrees maximum thrust lever travel from idle, and the indicated EPR may exceed 1.48.

(23)
Repeat steps (20) thru (22) for engine No. 2.

(24)
Extend trailing edge flaps to 15 units.

(25)
Simulate a landing gear-not-down-and-locked condition by placing a copper shield 

(1.5 x 2.5 x 0.06 inches) between any landing gear downlock sensor and its activating bar.
(a)  The continuous warning horn shall sound.

(26)
Press the horn cutout switch on the aisle stand.

(a)  The horn will continue to sound.

(27)
Slowly advance engine No. 1 thrust lever.

(a)  The warning horn shall cease at or before 1.71 EPR is attained.

(28)
Retard No. 1 thrust lever to idle.

(a)  The warning horn shall sound.

(29)
Press the horn cutout switch on the aisle stand.

(a)  The horn shall continue to sound.

(30)
Repeat steps (27), (28) and (29) with No. 2 engine.

(31)
Remove copper shield from downlock sensor.

(a)  The horn shall cease sounding.

(32)
Deploy and stow both thrust reversers at minimum necessary power.

(a)  Check that REVERSER UNLOCKED lights illuminate when deflector doors are out-of-stow, extinguish when the doors are stowed and that the ISOLATION VALVE light does not illuminate.

(33)
Shut down engine No. 1 using procedure for normal shutdown (Ref 71-09-100).

(a)  Check that flight recorder continues to operate.

(34)
Shut down engine No. 2 using procedure for normal shutdown (Ref 71-09-100).

(a)  Check that flight recorder ceases to operate.

(35)
Restore all systems to precheck configuration.

(36)
AIRPLANES WITH THE CENTER TANK FUEL SCAVENGE SYSTEM; do the Fuel Scavenge System Test, AMM 28-15-0/501.

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Feb 20/86  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  78-34-91 Page 401 

580 
78-34-91 Page 402  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Feb 20/86 
　
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