737 Flight Crew Operations Manual
7.23
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-4Q8-SJA
7.23
3 Thrust lever
(affected engine) . . . . Confirm. . . . . . . . . Close
4 Engine start lever
(affected engine) . . . . Confirm. . . . . . . CUTOFF
5 Engines can accelerate to idle very slowly,
especially at high altitudes or in heavy
precipitation. If N2 is steadily increasing and EGT
stays within limits, do not interrupt the start.
▼
Continued on next page
▼
▼Engine In-Flight Start continued▼
IN-FLIGHT START ENVELOPE
(FLT)
WINDMILL
(GRD)
ASSIST
260
20
15
240150
STARTER
PRESSURE ALTITUDE - 1000 FT
0
24
340
I
N
D
I
C
A
T
E
D
A
I
R
S
P
E
E
D
-
K
N
O
T
S
March 18, 2016
To Next Page
Loading...
