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Check -- To the Line”
NOTE: All speeds are recommended
procedural speeds, NOT
minimum maneuvering speeds.
Nominally 1,500 feet AGL
PF:
G “Gear DN”
Prior to 500 feet AGL:
G “Flaps 45” --
Speed VREF + factor
G “Before Landing Check --
Below the Line”
Turning Final:
PF: PNF:
G Select FLT CT
Synoptic page
PF:
G Maintain nominal 3_
glideslope to landing
G “Descent Check”
Prior to 400 feet AGL:
G “AP Off, FD Off”
PF:
After Touchdown
G Set Flaps 20, reset Trim
PNF:
G Thrust Levers to 70%
G Verify GLDs down
G Thrust levers to TOGA detent
G At VREF , “Rotate”
PNF:
PF:
G Rotate
PNF:
G “Positive Rate”
PF:
G “Gear Up”
PF:
G Climb at 170 KIAS
G “Climb Check”
PNF:
G Select
Status Page
OPERATOR'S
MANUAL
COPYRIGHT © UNIVERSAL AVIONICS SYSTEMS CORPORATION 1997, 1998.
ALL RIGHTS RESERVED
NOTICE
When the FMS is configured for the Advanced Performance Option, a
Performance Supplement is provided for insertion at the end of the FUEL
AND PERFORMANCE Section.
3260 E. Lerdo Rd.
Tucson, AZ 85706 U.S.A.
(520) 295-2300 (800) 321-5253
Report No. 2423sv602
Change 1, January 5, 1998
UNS-1B
UNS-1C
UNS-1Csp
UNS-1D
UNS-1K
FLIGHT MANAGEMENT SYSTEM
SCN 602
Application
2423sv602
Change 1
APPLICATION
This Operator’s Manual
Report No. 2423sv602
is applicable to
UNS-1B
UNS-1C
UNS-1Csp
UNS-1K
UNS-1D
FLIGHT
MANAGEMENT SYSTEM
possessing software program
Version 602.X
Refer to approved
Airplane Flight Manual Supplement
for certified version.
The software program version
is found on the
Initialization Page
and the S/W Versions page.
2423sv602
Change 1
CONTENTS
SUBJECT SECTION
Systems Description I
Control & Display II
Quick References III
Data Base IV
Navigation
Pilot/Company
Operations V
Predeparture
Enroute
Arrival
Fuel & Performance
Abnormal Procedures
Special Missions VI
Sensors and Interfaces VII
UniLink VIII
Appendices A
Supplements
Messages
Glossary
Index
 
 
2423sv602 LOEP-1
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