(2)
HSI indicates for each setting of AUTO/MAN/RMT switch:
AUTO/MAN/RMT SWITCH SETTING
HSI
INDICATIONS AUTO MAN RMT
DSR TK 50.1` 59.6` 354.1`
XTK R7.5 N.M. R3.7 N.M. L3.7 N.M.
TKE L27.6` L37.1` R28.4`
HDG 11.25` 11.25` 11.25`
TK 22.5` 22.5` 22.5`
DA 11.25` 11.25` 11.25`
MILES 888 888 888
EFFECTIVITY AIRPLANES WITH LTN-72 INS
CONFIG 01 A Page 111 Aug 25/87
34-41-00
When at STS 80 or lower (3 minutes after turn on), position ATTITUDE switch to transfer information from INS undergoing test to the ADI. (Refer to Flight Instrument Switching - Description and Operation) - Check that attitude sphere in ADI will level with airplane symbol and that ADI GYRO and RMI HEADING flags are withdrawn. (HSI HEADING and NAVIGATION warning or barber pole flags should be withdrawn before status 40. Do not wait for status 40 before continuing but monitor flags and note that they withdraw from view).
IF -
EFFECTIVITY AIRPLANES WITH LTN-72 INS
CONFIG 01 A Page 112 Aug 25/87
34-41-00
Set display selector switch to DSR TK/STS and select ALIGN position of mode selec-tor switch on MSU -
Check that warn annunciator does not flash and check mode sequencing as follows:
(1)
Right-hand data display is 80 at 3 minutes after MSU mode selector switch set to ALIGN (if ambient temp is less than 70`F, this time could exceed 3 minutes. If temp is greater than 70`F and time exceeds 3 minutes, check 115-volt ac circuit breakers on P7 panel).
(2)
Right-hand data display is 70 at 2 minutes after status 80 is attained, and present position entered.
(3)
If no flashing WARN is encountered in alignment status 60, the system attains alignment status 50 within 75 seconds.
IF -
When at status 50, set display selector switch to TK/GS - Check left-hand display indicates true heading (magnetic | variation) and right-hand display is all zeros. (At ground speeds below 10 knots, true heading is displayed in place of inertial track angle.) IF -
EFFECTIVITY AIRPLANES WITH LTN-72 INS
CONFIG 01 A Page 113 Aug 25/87
34-41-00
AUTO/MAN/RMT switch to MAN. Insert waypoint positions determined as follows: ____ Data cannot be entered in WPT 0 using data keyboard.
NOTE:
(1)
WPT 1; for latitude, subtract 4.0' (mins) from present position latitude; for longitude, subtract 1` from present position longitude.
(2)
WPT 2; latitude as determined above; for longitude, add 1` to present position longitude.
(3)
WPT 3; coordinates of present position.
(4)
WPT 4; for latitude, add 10` to present position latitude; for longitude, use present position longitude.
(5)
WPT 5; coordinates of present position.
(6)
WPT 6, WPT 7, WPT 8, WPT 9; for latitude, use 1.0' S latitude; for longitude, use present position longitude.
IF -
EFFECTIVITY AIRPLANES WITH LTN-72 INS
CONFIG 01 A Page 114 Aug 25/87
34-41-00
Enter track 2-1. Set data selector switch to DIS/TIME, AUTO/MAN/RMT switch to RMT, and initiate track 3-4 using TK CHG key and data keyboard - Check that CDU and HSI displays are as follows:
(1)
Left-hand data display on CDU - 600 nautical miles
(2)
Right-hand data display on CDU - 070.3 minutes
(3)
HSI TO/FROM pointer indicates TO IF -
Set data selector switch to WIND - Check that displays are blank at ground speed less than 170 knots TAS (left display indicates wind direction (true) from 0 to 359`, right display wind speed from 0 to 799 knots, both in increments of 1). IF -
EFFECTIVITY AIRPLANES WITH LTN-72 INS
CONFIG 01 A Page 115 Aug 25/87
34-41-00
OK
Set data selector switch to DSR TK/STS and set AUTO/MAN/RMT switch to MAN. Using TK CHG key and data keyboard, initiate track 3-4 followed by track 4-3. Press data keyboard 0 key. Enter a 45.0` track in left-hand display using data keyboard and press INSERT key - Check that CDU displays are as follows:
(1)
Left-hand data display indicates 000.0` for track 3-4 selection.
(2)
Left-hand data display indicates 180.0` for track 4-3 selection.
(3)
Right display shows present system status.
(4)
FROM/TO display indicates 9-9 and left-hand data display indicates 45.0` when this track is inserted in computer.
IF -
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