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@ G/A – Go-around.
A CON – Continuous.
B - - - FMC is not computing thrust limit.
C A/T LIM – Autothrottle limit. Indicates that A/T computer is calculating a
degraded N1 thrust limit for the affected engine or engines.
AUTO FLIGHT
737 Sec. 6.4 Page 59
Flight Manual Continental Rev. 11/15/02 #41
BCD Thrust Mode Display (As Installed)
< Thrust Mode Display
N1 limit reference is the active N1 limit for autothrottle and manual thrust
control.
N1 limit reference is also displayed by N1 reference bugs with N1 SET
control in AUTO position.
N1 limit reference is normally calculated by the FMC.
Thrust mode display annunciations are:
· R-TO – Reduced takeoff.
· R-CLB – Reduced climb.
· TO – Takeoff.
· CLB – Climb.
· CRZ – Cruise.
· G/A – Go-around.
· CON – Continuous.
· - - - FMC is not computing thrust limit.
= Autothrottle Limit (A/T LIM) Indication
Illuminated (white) – The FMC is not providing the A/T system with N1
limit values. The A/T is using a degraded N1 thrust limit from the related
EEC.
AUTO FLIGHT
Sec. 6.4 Page 60 737
Rev. 11/15/02 #41 Continental Flight Manual
> Flight Mode Annunciator Panels
A mode annunciator is on each pilot instrument panel. The annunciator panels
are identical and display mode status of the AFDS, A/T and N1 limit.
The individual annunciators are three-sided prisms which mechanically rotate to
the appropriate display and are externally illuminated.
The A/P and A/T disengage lights and FMC alert light are internally illuminated
light caps.
When the test switch is held at the 1 and 2 positions, the following displays are
annunciated.
A white horizontal line on a black background indicates a spare annunciator and
is displayed only during test.
AUTO FLIGHT
737 Sec. 6.4 Page 61
Flight Manual Continental Rev. 11/15/02 #41
> Flight Mode Annunciators
AUTO FLIGHT
Sec. 6.4 Page 62 737
Rev. 11/15/02 #41 Continental Flight Manual
< CWS / ROLL
= CWS / PITCH – (black on amber)
Indicates axis in CWS mode.
> SINGLE CHANNEL (black on amber)
Annunciated in APP mode from LOC capture until the APP mode is
disengaged.
? A/P OFF (black on white)
Neither autopilot engaged and at least one F/D is ON.
AUTO FLIGHT
737 Sec. 6.4 Page 63
Flight Manual Continental Rev. 11/15/02 #41
>@ Flight Mode Annunciations (As Installed)
R
P
EADI
PITCH ARMED MODE ROLL ARMED MODE
seconds after each engagement.
PITCH ENGAGED MODE ROLL ENGAGED MODE
(rectangle) is drawn around each
SINGLE CHANNEL
CWS P (Y)
CWS PITCH ENGAGED
CWS ROLL ENGAGED
FLARE (W)
VOR/LOC (W)
G/S V/S (W)
(Y) - Yellow
(W) - White
(G) - Green
A mode change highlight symbol
mode annunciation for a period of 10
pitch, roll, CWS, and thrust engaged
MODE CHANGE HIGHLIGHT SYMBOL
L NA V
CMD (G)
A/P STATUS
HDG SEL (G)
G/S (G)
TO/GA (G)
ARM (W)
N1 (G)
MCP SPD (G)
THR HLD (G)
FMC SPD (G)
A/T ENGAGED MODE
G/S VOR/LOC
CWS
CWS
THR HLD V NA V P T H F D
CAPT INST PANEL
F/O INST PANEL
37371292
AUTO FLIGHT
Sec. 6.4 Page 64 737
Rev. 11/15/02 #41 Continental Flight Manual
BCD Flight Mode Annunciations (FMA’s) (As Installed)
AUTO FLIGHT
737 Sec. 6.4 LEP-1
Flight Manual Continental Rev. 11/15/02 #41
LIST OF EFFECTIVE PAGES
PAGE DATE PAGE DATE PAGE DATE
* Asterisk indicates page(s) revised or added by the current revision.
* TOC-1 11/15/02
* TOC-2 11/15/02
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