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T-45A/C TS, E2-C2, ADV & IUT Aero-06/07
NATOPS Performance Charts / Charts and Exam Review
I.
Dive Recovery
Sg 3, fr 19
Dive Recovery
1.
This chart is used to compute the altitude loss during
a dive recovery
2.
Altitude loss based on a dive recovery with a 2 g per
second buildup to a sustained 4-g’s or maximum
usable lift
3.
Dive recovery computation
a.
Enter chart at altitude at start of dive recovery
Overlay 1
Overlay 2
b.
Extend horizontal line from altitude at start of
dive recovery to the Mach number or airspeed
Overlay 3
at start of dive recovery reference line
Overlay 4
c.
From the intersection of the altitude line and
Mach number or airspeed reference line extend
Overlay 5
a vertical line down to the initial dive-angle
reference line
Overlay 6
d.
From the intersection of the vertical line and the
initial dive angle reference line extend a line
Sg 3, fr 20
horizontally to the left to determine altitude lost
Dive Recovery
in the pullout
4.
Subtract altitude lost during pullout from the altitude
the pullout was initiated at to find the minimum
altitude after pullout
J.
Operating Envelope
1.
T-45 operating Envelope is a graphic representation
Sg 2, fr 21
of the airspeed and altitude limits
Operating Envelope
2.
Portions of the envelope impose additional
restrictions on throttle movement and position
(9-99) Original
Page 6-13


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