TM 55-1520-240-23-7
8-26
PURGE PITOT-STATIC AND SIDESLIP SENSE SYSTEMS
(Continued)
8-26
34.
Connect pitot (7), static (8), and sideslip lines (9
and 10) to No. 2 AFCS computer (11).
35.
Connect pitot (2), static (3), and sideslip lines (4
and 5) to No. 1 AFCS computer (6).
36.
Install two radio compartment drain caps (1).
37.
Install two nose compartment drain caps (1).
38.
Install seven bottom fuselage drain caps (1).
FOLLOW-ON MAINTENANCE:
Pitot static system leak check (TM 55-1520-240-T).
Sideslip sensing system leak check (TM
55-1520-240-T).
Install TSEC/KY28 (TM 11-1520-240-23).
Install electronic compartment acoustical blanket
(Task 2-210).
Install pilots AIMS altimeter, copilots barometric
altimeter (Task 8-91).
Install pilots and copilots vertical speed and airspeed
indicators (Task 8-91).
Close nose enclosure door (Task 2-2).
TSEC/KY28 operational check (TM 11-1520-240-23).
END OF TASK
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