ILS Procedures
E2-C2 BIFP-06 & IUT BIFP-05
Sg 2, fr 7 p2
Sg 2, fr 7 p1
IABC
IABC
110.1
110.1
33
3
9.3
360
RANGE
COURSE
N
32 -33 -34 -35 -
-1- 2- 3- 4
N-
-
BC LOC
BC LOC
3
33
CRS
HDG
REVERSE SENSING
REVERSE SENSING
Sg 2, fr 8
Sg 2, fr 9
CAUTION: FALSE GLIDESLOPE SIGNALS MAY
CAUTION: DO NOT USE BACK COURSE
EXIST IN THE AREA OF THE LOCALIZER BC
SIGNALS FOR APPROACH UNLESS A BACK
APPROACH WHICH CAN CAUSE THE GS
COURSE APPROACH PROCEDURE IS
WARNING FLAG TO DISAPPEAR AND PRESENT
PUBLISHED FOR THAT PARTICULAR RUNWAY
UNRELIABLE GS INFORMATION. DISREGARD
AND THE APPROACH IS AUTHORIZED BY ATC.
ALL GS SIGNAL INDICATIONS WHEN MAKING A
LOCALIZER BC APPROACH.
C.
Back course LOC approach 22.9.4.6.2
NOTE: The T-45A is not equipped with automatic
reverse sensing equipment which would provide a normal
sensing display on the HSI and ADI when executing a
back course LOC. When flying a back course LOC in
this aircraft, the pilot will always experience reverse
sensing on the ADI and on HSI displays when the back
course inbound course to the field is selected. In this
situation, to correct to course, the pilot will have to "fly
away" from the ADI azimuth deviation bar and HSI CDI.
An alternate procedure is to set the front course into the
HSI. This will induce a normal sensing display in the
HSI. Caution should be taken because the azimuth
deviation bar on the ADI will continue to display reverse
sensing.
(03-97) Original
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