corrosion.
(d)
Apply BMS 3-23 Type II, Corrosion Preventive Compound to the engine dry bays and center wing cavity. 1) This will remove the moisture that collects.
(e)
Refuel the airplane (fill all serviceable fuel tanks to full) (AMM 12-11-01).
NOTE: When it is possible, do not operate the airplane for 24
____ hours. After 24 hours, examine it for external fuel leaks.
H. Electrical/Electronics Systems
S 632-031
(1) To make sure the Electrical/Electronic systems are serviceable, do the steps that follow:
(a)
Make sure the electrical ground is installed on the airplane.
(b)
Make sure the Electrical/Electronic systems circuit breakers are open or closed when it is necessary.
(c)
Make sure the Electrical/Electronic systems switches are in the OFF position.
(d)
Make sure the equipment racks are clean, dry, and have no corrosion.
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(e) Install all of the rack-mounted electronic packages when it is necessary. 1) These were the components that were removed in the
Electrical/Electronic System procedures for Long Term storage.
S 712-032
(2)
Do an operational test of the Electrical/Electronic components that are installed.
S 422-033
(3)
Install all of the batteries that were removed for storage.
S 762-034
(4)
Make sure the batteries that follow are fully charged:
(a)
The main battery (AMM 24-31-01/401).
(b)
The APU battery (AMM 24-31-03/401).
S 722-035
(5) Do a functional test of the batteries that follow:
(a)
The main battery (AMM 24-31-01/401).
(b)
The APU battery (AMM 24-31-03/401).
S 862-036
(6) If the batteries were not removed at the start of the storage, close all circuit breakers.
I. Control Cabin Equipment
S 632-037
(1) To make the flight compartment equipment serviceable, do the steps that follow:
WARNING: FAILURE TO REMOVE COVERS FROM PITOT PROBES BEFORE FLIGHT
_______ MAY CAUSE LARGE ERRORS IN AIRSPEED-SENSING AND ALTITUDE-SENSING SIGNALS WHICH MAY LEAD TO LOSS OF SAFE FLIGHT.
CAUTION:_______REMOVE ALL COVERS. ENGINES SHOULD NOT BE OPERATED WITH COVERS IN PLACE BECAUSE THE COVERS CAN COME OFF AND DAMAGE THE ENGINES.
CAUTION: MAKE SURE THE PITOT PROBE COVERS ARE IN GOOD WORKING CONDITION
_______ WITH NO EVIDENCE OF DAMAGE, ESPECIALLY FRAYING AROUND THE COVER OPENING. FRAYED FIBERS FROM THE COVER COMBINED WITH OTHER SUBSTANCES SUCH AS DIRT, GREASE AND FLUIDS CAN CAUSE OBSTRUCTION IN THE PROBE.
(a) Remove the covers from the Pitot Probes and tubes.
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(b)
Remove the "PITOT PROBES COVERED" tag from the left control wheel in the flight deck.
(c)
Do the steps that follow if it is necessary: 1) Replace the quick-opening drain valve assembly to the pitot and static drain tubes (AMM 34-11-00/501).
2) Replace the drain plug to the pitot and static drain tubes. (AMM 34-11-00/501).
(d)
Remove the tape or covers from the items that follow: 1) The temperature probes 2) The angle of attack sensors 3) The ice detector (when installed)
WARNING: FAILURE TO REMOVE BARRICADE TAPE AND VINYL ADHESIVE TAPE
_______ FROM THE STATIC PORTS BEFORE FLIGHT MAY CAUSE LARGE ERRORS IN AIRSPEED-SENSING AND ALTITUDE-SENSING SIGNALS, WHICH MAY LEAD TO LOSS OF SAFE FLIGHT.
CAUTION: REMOVE ALL BARRICADE TAPE AND VINYL ADHESIVE TAPE.
_______ ENGINES SHOULD NOT BE OPERATED WITH COVERINGS IN PLACE BECAUSE THE COVERS CAN COME OFF AND DAMAGE THE ENGINES.
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