Esterline CMA-9000 - Waypoint Time Constraints (RTA; Vertical Profile Verification; TAKEOFF REF Page

OPERATOR’S MANUAL
CMA-9000 FLIGHT MANAGEMENT SYSTEM
1.4.4 Waypoint Time Constraints (RTA)
r Descent waypoint [1L] using the RTA PROGRESS
TA.
An RTA ca chievable:
will permit the aircraft to respect the waypoint time constraint are
• An RTA UNACHIEVABLE message will be raised if the entered RTA cannot be met.
NOTE: Refer to the Required Time of Arrival in Cruise sub-section for additional details.
• st are consistent with the takeoff gross weight.
t with the V
1
, V
2
symbols displayed on the PFD. For
V
R
, refer to the Note below. The PFD display is illustrated below.
• The reduced takeoff thrust (De-rate or Flex) displayed on the primary field of view is consistent with the
entered value
NOTE: V
2
, the reduced takeoff thrust, the departure runway elevation and the thrust reduction height
impact the computed vertical profile. The FMS assumes that a speed of V
2
+10kts will be flown
up to the Acceleration Altitude.
V
R
is displayed on the PFD only during the takeoff ground run.
ACT RTA PROGRESS 3/4
RTA WPT RTA
MLN 2055.0z
RTA CRZ SPD DIS
.575 406nm
REC TO UTC
1942.7z 1930.9z
ETA TO MLN
2043.1z
FIRST -TO WINDOW- LAST
1934.3z 1951.1z
A time constraint [1R] can be assigned to a single Cruise o
3/4 page:
• Only the planned Cruise speed schedule [2L] is adjusted to meet the R
• n be entered while on-ground or while airborne. If the RTA is a
• While on ground, a recommended takeoff time is displayed at [3L].
• The earliest and latest times that
displayed at [5L] and [5R].
1.4.5 Vertical Profile Verification
1.4.5.1 TAKEOFF REF page
Before takeoff, go to the TAKEOFF REF page to ensure that:
he entered takeoff speeds and the T reduced takeoff thru
• The V
1
, V
2
speeds entered on the MCDU are consisten
Page F-16
August 17, 2010
DRAFT