a. Set MODE SELECTOR to CAL. Conduct four-
heading electrical swing by rotating HEADING SE-
LECTOR to 0, 90, 180, and 270 degrees. Enter
errors in table F1 of swing data sheet.
b. Repeat electrical swing to obtain errors while
O degrees equals error at 180 degrees (N-S) and
error at 90 degrees equals error at 270 degrees
(E-W) within 12 minute 3.
4-55. SYSTEM ERROR COMPENSATION.
a. Set MODE SELECTOR to MON. Disconnect
adapter cable W1 and connect adapter cable W2 as
follows :
End W2P1 to J8 of KE28 compensator.
End W2J1 to cable P8 of A-6A aircraft.
End W2P2 to MC-2 Adapter Box.
b. Connect adapter cable W3 as follows:
End W3P1 to J9 of KE28 compensator.
End W3J1 to cable P9 of A-6A aircraft.
End W3P2 to connector 1J4 of Console.
c. Apply power to aircraft compass system and
d. Set MODE SELECTOR to COMP, READOUT SE-
LECT to EXT CX, and rotate HEADING SELECTOR
in 15-degree increments. Synchronize MA-1 com-
h. Change controls and switches of Console as
pass system with its controller and adjust KE28
follows :
compensator to obtain zero error on Console readout.
Allow sufficient time for slaving signal to reach a
null. Record final system readout errors in table
E1-E2 CHECK to E1 CHECK.
F2 of swing data sheet.
READOUT SELECT to 90.
e. After compass system is fully compensated, re-
i. Adjust E1 voltage controls to null NULL INDI-
move all adapter cables and return compass system
CATOR. Record voltage value on line F-7 of swing
to its original configuration.
data sheet. Set E1-E2 CHECK switch to E2 CHECK
and adjust E2 voltage controls to null NULL INDI-
4-56. FORMS. NAVAIR Form 13910/1, Magnetic
CATOR. Record value of E2 voltage on line F-8 of
Compass Calibrator Set Type MC-2 Area Magnetic
swing data sheet. Set E1-E2 CHECK switch to OFF.
Survey Data, and NAVA IR Form 13910/2, Magnetic
Compass Calibrator Set Type MC-2 Swing Data, are
4-54. ONE-CYCLE ERROR COMPENSATION. (For
stocked in the Forms anc Publications Segment of the
A-6A aircraft. See applicable manual for compen -
Navy Supply System and may be requisitioned in
sation in other types of aircraft.)
accordance with NAVSUF Publication 2002.
4-25