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Page Access
Access to these pages is by selection of the N1 LIMIT mode
select key on the CDU or the N1 LIMIT prompt on the PERF INIT
or TAKEOFF REF pages.
N1 Limits Page (On Ground)
Line 1L shows the SEL/OAT prompt. This data field lets the flight
crew enter the outside air temperature (OAT). An assumed
temperature (SEL) can also be entered for reduced thrust
takeoffs.
Line 2L shows the TO prompt. This selects full takeoff thrust.
SHZ 001-003 (POST SB 737-34-1650 AND PRE SB 737-34A1801)
OR PRE SB 737-34-1918; SHZ 009-999 PRE SB 737-34-1918 OR
(POST SB 737-34-1650 AND PRE SB 737-34A1801)
Line 3L shows The TO-1 prompt. This selects the first reduced
takeoff thrust.
Line 4L shows the TO-2 prompt. This selects the second
reduced takeoff thrust.
SHZ ALL
When a specific takeoff thrust is selected, the <ACT> prompt
shows adjacent to the selected thrust. The FMCS always selects
the highest possible climb thrust which would not result in a
thrust increase when a takeoff thrust is selected. This prevents
a throttle push at transition from takeoff thrust to climb thrust.
Line 6L shows the PERF INIT prompt. This selects the PERF INIT
page.
Line 1R shows the TAKEOFF N1 prompt. This data field shows
the active takeoff thrust calculated by the FMCS.
Line 2R shows the CLB prompt. This enables and shows the
maximum climb thrust for the autothrottle and the N1 bugs after
transition from the takeoff mode.
Line 3R shows the CLB-1 prompt. This selects the first derate
climb thrust to be used after transition from takeoff mode.
Line 4R shows the CLB-2 prompt. This selects the second
derate climb thrust to be used after transition from takeoff
mode.
FMCS - DISPLAYS - CDU - N1 LIMIT PAGE
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.39
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-043
The selected climb thrust shows by the <SEL> prompt in large
font adjacent to the selected thrust data field.
Line 6R shows the TAKEOFF prompt. This selects the TAKEOFF
REF page.
N1 Limits Page (In Air)
The N1 limit page lets the flight crew select an N1 limit for these
thrust limit modes:
* Go-around (GA)
* Continuous (CON)
* Climb (CLB)
* Cruise (CRZ)
* Climb - 1
* Climb - 2.
Line 1L shows the AUTO prompt. This selection lets the FMCS
calculate N1 limit values. AUTO is the default selection.
Line 2L and 2R show the GA (go-around) N1 limit.
Line 3L and 3R show the CON (continuous) N1 limit.
Line 4L and 4R show the CLB (climb) N1 limit.
Line 5L and 5R show the CRZ (cruise) N1 limit.
Line 6L and 6R show the CLB-1 and CLB-2 prompts. Selection
will show the reduced climb N1 limit.
FMCS - DISPLAYS - CDU - N1 LIMIT PAGE
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.40
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-043
FMCS - DISPLAYS - CDU - N1 LIMIT PAGE
FMCS - DISPLAYS - CDU - N1 LIMIT PAGE
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.41
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-043
Purpose
The takeoff reference pages show this data for takeoff:
* Temperature
* Takeoff thrust
* V speed data
* Runway data.
Page Access
You get access to this page from one of these pages:
* INIT/REF INDEX
* PERF INIT
* RTE.
Page 1 Information
This page lets the flight crew see FMC calculated takeoff
thrusts, crew entered takeoff data, and V speed data.
Line 1L shows the FLAPS prompt. This lets the flight crew enter
the takeoff flap setting. Box prompts show before there is a valid
entry. Allowable entries are flaps 1, 5, 10, 15, and 25. This data
field may also be uplinked in an ACARS takeoff data message.
Line 2L shows the active N1 takeoff thrust calculated by the
FMCS. The data field header line changes to show whether it is
one of these:
* Full rated thrust
* Reduced thrust from a SEL (assumed) temperature entry
* First takeoff derate thrust
* Second takeoff derate thrust.
If the takeoff N1 value is calculated from ACARS uplinked data,
the N1 values show in small font until the flight crew accepts the
data.
Line 3L shows the prompts for center of gravity (CG) and TRIM.
This lets the flight crew enter CG. If gross weight is entered, the
　
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