Airplane Flight Manual Supplement
UPS Aviation Technologies
i-linc MFD
2345 Turner Rd. SE
February 10, 2003
Salem, OR 97302
Part #:560-1045-02 Rev A
FAA Approved
Date:
February 26, 2003
Page 5 of 11
2.2
U
SER
M
ANUAL
The manual or the information contained in the manual listed below(or later appropriate revisions),
must be immediately available to the flight crew.
·
i-linc MFD Multi-Function Display Pilot’s Guide……P/N 0040-19001-01 Rev D
2.3
S
YSTEM
S
OFTWARE
The system software resides on the front loading datacard. The front loading datacard must be
inserted into the unit for operational use and not removed during flight. The system must utilize
the software version listed below (or later FAA approved versions). The software version can be
displayed in the system mode on the i-linc display under the INFO smart key.
·
i-linc Software ........................................... Ver 4.1 (138-0448-041)
·
i-linc Software (with ChartView ®).......... Ver 4.1 (138-0456-041)
2.4
M
AGNETIC
V
ARIATION
The automatic magnetic variation (MagVar) correction is not available in the i-linc MFD above
73
°
North or below 73
°
South latitude. All bearing and track information is computed and
displayed relative to true north in these polar regions.
2.5
P
OWER ON
S
ELF
T
EST
(POST)
The i-linc MFD performs a self test when power is applied. The pilot is responsible for verifying
all tests pass. If any of the i-linc MFD tests fail, power off the i-linc MFD.
2.6
P
LACARD
Aircraft will have a placard identifying the MFD circuit breaker. The placard will be placed
directly adjacent to the respective breaker.
3.
EMERGENCY / ABNORMAL PROCEDURES
3.1
E
MERGENCY
P
ROCEDURES
No change. Refer to approved Airplane Flight Manual.
3.2
A
BNORMAL
P
ROCEDURES
No change. Refer to approved Airplane Flight Manual.
