diff --git a/Models/Instruments/PFD/PFD.nas b/Models/Instruments/PFD/PFD.nas
index a75723d9..e456251d 100644
--- a/Models/Instruments/PFD/PFD.nas
+++ b/Models/Instruments/PFD/PFD.nas
@@ -210,7 +210,7 @@ var canvas_PFD_base = {
wow2 = getprop("/gear/gear[2]/wow");
# FMA MAN TOGA MCT FLX THR
- if (athr == 1 and (state1 == "TOGA" or state1 == "MCT" or state1 == "MAN THR" or state2 == "TOGA" or state2 == "MCT" or state2 == "MAN THR")) {
+ if (athr == 1 and (state1 == "TOGA" or state1 == "MCT" or state1 == "MAN THR" or state2 == "TOGA" or state2 == "MCT" or state2 == "MAN THR") and getprop("/systems/thrust/eng-out") != 1) {
me["FMA_man"].show();
me["FMA_manmode"].show();
if (state1 == "TOGA" or state2 == "TOGA") {
@@ -245,6 +245,30 @@ var canvas_PFD_base = {
me["FMA_manmode"].setText("THR");
me["FMA_man_box"].setColor(0.7333,0.3803,0);
}
+ } else if (athr == 1 and (state1 == "TOGA" or (state1 == "MCT" and getprop("/controls/engines/thrust-limit") == "FLX") or (state1 == "MAN THR" and thr1 >= 0.83) or state2 == "TOGA" or (state2 == "MCT" and
+ getprop("/controls/engines/thrust-limit") == "FLX") or (state2 == "MAN THR" and thr2 >= 0.83)) and getprop("/systems/thrust/eng-out") == 1) {
+ me["FMA_man"].show();
+ me["FMA_manmode"].show();
+ if (state1 == "TOGA" or state2 == "TOGA") {
+ me["FMA_flx_box"].hide();
+ me["FMA_flxtemp"].hide();
+ me["FMA_man_box"].show();
+ me["FMA_manmode"].setText("TOGA");
+ me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
+ } else if ((state1 == "MAN THR" and thr1 >= 0.83) or (state2 == "MAN THR" and thr2 >= 0.83)) {
+ me["FMA_flx_box"].hide();
+ me["FMA_flxtemp"].hide();
+ me["FMA_man_box"].show();
+ me["FMA_manmode"].setText("THR");
+ me["FMA_man_box"].setColor(0.7333,0.3803,0);
+ } else if ((state1 == "MCT" or state2 == "MCT") and getprop("/controls/engines/thrust-limit") == "FLX") {
+ me["FMA_flxtemp"].setText(sprintf("%s", "+" ~ getprop("/FMGC/internal/flex")));
+ me["FMA_man_box"].hide();
+ me["FMA_flx_box"].show();
+ me["FMA_flxtemp"].show();
+ me["FMA_manmode"].setText("FLX ");
+ me["FMA_man_box"].setColor(0.8078,0.8039,0.8078);
+ }
} else {
me["FMA_man"].hide();
me["FMA_manmode"].hide();
@@ -253,6 +277,12 @@ var canvas_PFD_base = {
me["FMA_flxtemp"].hide();
}
+ if (getprop("/systems/thrust/eng-out") == 1) {
+ me["FMA_lvrclb"].setText("LVR MCT");
+ } else {
+ me["FMA_lvrclb"].setText("LVR CLB");
+ }
+
if (athr == 1 and getprop("/systems/thrust/lvrclb") == 1) {
me["FMA_lvrclb"].show();
} else {
@@ -260,7 +290,15 @@ var canvas_PFD_base = {
}
# FMA A/THR
- if (athr == 1 and ((state1 == "MAN" or state1 == "CL") and (state2 == "MAN" or state2 == "CL"))) {
+ if (athr == 1 and getprop("/systems/thrust/eng-out") != 1 and (state1 == "MAN" or state1 == "CL") and (state2 == "MAN" or state2 == "CL")) {
+ me["FMA_thrust"].show();
+ if (getprop("/modes/pfd/fma/throttle-mode-box") == 1 and throttle_mode != " ") {
+ me["FMA_thrust_box"].show();
+ } else {
+ me["FMA_thrust_box"].hide();
+ }
+ } else if (athr == 1 and getprop("/systems/thrust/eng-out") == 1 and (state1 == "MAN" or state1 == "CL" or (state1 == "MAN THR" and thr1 < 0.83) or (state1 == "MCT" and getprop("/controls/engines/thrust-limit") != "FLX")) and
+ (state2 == "MAN" or state2 == "CL" or (state2 == "MAN THR" and thr2 < 0.83) or (state2 == "MCT" and getprop("/controls/engines/thrust-limit") != "FLX"))) {
me["FMA_thrust"].show();
if (getprop("/modes/pfd/fma/throttle-mode-box") == 1 and throttle_mode != " ") {
me["FMA_thrust_box"].show();
@@ -390,7 +428,7 @@ var canvas_PFD_base = {
me["FMA_fd"].setText(sprintf("%s", getprop("/modes/pfd/fma/fd-mode")));
me["FMA_athr"].setText(sprintf("%s", getprop("/modes/pfd/fma/at-mode")));
- if ((state1 == "MAN" or state1 == "CL") and (state2 == "MAN" or state2 == "CL")) {
+ if (getprop("/modes/pfd/fma/athr-armed") != 1) {
me["FMA_athr"].setColor(0.8078,0.8039,0.8078);
} else {
me["FMA_athr"].setColor(0.0862,0.5176,0.6470);
diff --git a/Nasal/FMGC-c.nas b/Nasal/FMGC-c.nas
index 2b1faa02..ba2214e4 100644
--- a/Nasal/FMGC-c.nas
+++ b/Nasal/FMGC-c.nas
@@ -46,17 +46,23 @@ var loopFMA = maketimer(0.05, func {
var state1 = getprop("/systems/thrust/state1");
var state2 = getprop("/systems/thrust/state2");
var newthr = getprop("/modes/pfd/fma/throttle-mode");
+ var thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
+ var thr2 = getprop("/controls/engines/engine[1]/throttle-pos");
if (state1 == "TOGA" or state2 == "TOGA") {
- if (newthr != " ") {
- setprop("/modes/pfd/fma/throttle-mode", " ");
+ if (newthr != " ") {
+ setprop("/modes/pfd/fma/throttle-mode", " ");
}
- } else if (state1 == "MCT" or state2 == "MCT") {
+ } else if ((state1 == "MAN THR" and thr1 >= 0.83) or (state2 == "MAN THR" and thr2 >= 0.83)) {
+ if (newthr != " ") {
+ setprop("/modes/pfd/fma/throttle-mode", " ");
+ }
+ } else if ((state1 == "MCT" or state2 == "MCT") and getprop("/systems/thrust/eng-out") != 1) {
if (newthr != " ") {
setprop("/modes/pfd/fma/throttle-mode", " ");
}
- } else if (state1 == "MAN THR" or state2 == "MAN THR") {
- if (newthr != " ") {
- setprop("/modes/pfd/fma/throttle-mode", " ");
+ } else if (((state1 == "MAN THR" and thr1 < 0.83) or (state2 == "MAN THR" and thr2 < 0.83)) and getprop("/systems/thrust/eng-out") != 1) {
+ if (newthr != " ") {
+ setprop("/modes/pfd/fma/throttle-mode", " ");
}
} else {
if ((getprop("/it-autoflight/output/vert") == 4) or (getprop("/it-autoflight/output/vert") == 6) or (getprop("/it-autoflight/output/vert") == 7) or (getprop("/it-autoflight/output/vert") == 8)) {
@@ -71,7 +77,11 @@ var loopFMA = maketimer(0.05, func {
setprop("/modes/pfd/fma/throttle-mode", "THR IDLE");
}
} else if (thr == 2) {
- if (state1 == "CL" or state2 == "CL") {
+ if (state1 == "MCT" or state2 == "MCT" and getprop("/systems/thrust/eng-out") == 1) {
+ if (newthr != "THR MCT") {
+ setprop("/modes/pfd/fma/throttle-mode", "THR MCT");
+ }
+ } else if (state1 == "CL" or state2 == "CL") {
if (newthr != "THR CLB") {
setprop("/modes/pfd/fma/throttle-mode", "THR CLB");
}
@@ -88,7 +98,12 @@ var loopFMA = maketimer(0.05, func {
}
# A/THR Armed/Active
- if (getprop("/it-autoflight/output/athr") == 1 and (state1 == "MAN THR" or state2 == "MAN THR" or state1 == "MCT" or state2 == "MCT" or state1 == "TOGA" or state2 == "TOGA")) {
+ if (getprop("/it-autoflight/output/athr") == 1 and (state1 == "MAN THR" or state2 == "MAN THR" or state1 == "MCT" or state2 == "MCT" or state1 == "TOGA" or state2 == "TOGA") and getprop("/systems/thrust/eng-out") != 1) {
+ if (getprop("/modes/pfd/fma/athr-armed") != 1) {
+ setprop("/modes/pfd/fma/athr-armed", 1);
+ }
+ } else if (getprop("/it-autoflight/output/athr") == 1 and ((state1 == "MAN THR" and thr1 >= 0.83) or (state2 == "MAN THR" and thr2 >= 0.83) or (state1 == "MCT" and getprop("/controls/engines/thrust-limit") == "FLX") or
+ (state2 == "MCT" and getprop("/controls/engines/thrust-limit") == "FLX") or state1 == "TOGA" or state2 == "TOGA") and getprop("/systems/thrust/eng-out") == 1) {
if (getprop("/modes/pfd/fma/athr-armed") != 1) {
setprop("/modes/pfd/fma/athr-armed", 1);
}
@@ -612,8 +627,13 @@ setlistener("/modes/pfd/fma/athr-armed", func {
setlistener("/modes/pfd/fma/throttle-mode", func {
var state1 = getprop("/systems/thrust/state1");
var state2 = getprop("/systems/thrust/state2");
- if (getprop("/it-autoflight/output/athr") == 1 and state1 != "MCT" and state2 != "MCT" and state1 != "MAN THR" and state2 != "MAN THR" and state1 != "TOGA" and state2 != "TOGA" and state1 != "IDLE" and state2 != "IDLE") {
+ if (getprop("/it-autoflight/output/athr") == 1 and state1 != "MCT" and state2 != "MCT" and state1 != "MAN THR" and state2 != "MAN THR" and state1 != "TOGA" and state2 != "TOGA" and state1 != "IDLE" and state2 != "IDLE" and
+ getprop("/systems/thrust/eng-out") != 1) {
setprop("/modes/pfd/fma/throttle-mode-time", getprop("/sim/time/elapsed-sec"));
+ } else if (getprop("/it-autoflight/output/athr") == 1 and state1 != "TOGA" and state2 != "TOGA" and state1 != "IDLE" and state2 != "IDLE" and getprop("/systems/thrust/eng-out") == 1) {
+ if (getprop("/controls/engines/engine[0]/throttle-pos") < 0.83 and getprop("/controls/engines/engine[1]/throttle-pos") < 0.83) {
+ setprop("/modes/pfd/fma/throttle-mode-time", getprop("/sim/time/elapsed-sec"));
+ }
}
});
diff --git a/Nasal/fadec-common.nas b/Nasal/fadec-common.nas
index cbab9e7f..7ceaff98 100644
--- a/Nasal/fadec-common.nas
+++ b/Nasal/fadec-common.nas
@@ -28,6 +28,7 @@ setprop("/systems/thrust/mct-lim", 0.0);
setprop("/systems/thrust/clb-lim", 0.0);
setprop("/systems/thrust/lim-flex", 0);
setprop("/engines/flex-derate", 0);
+setprop("/systems/thrust/eng-out", 0);
setlistener("/sim/signals/fdm-initialized", func {
var thr1 = getprop("/controls/engines/engine[0]/throttle-pos");
@@ -70,13 +71,15 @@ setlistener("/controls/engines/engine[0]/throttle-pos", func {
setprop("/systems/thrust/state1", "MAN THR");
unflex();
} else if (thr1 >= 0.78 and thr1 < 0.83) {
- if (getprop("/controls/engines/thrust-limit") == "FLX") {
- if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) {
- setprop("/it-autoflight/input/athr", 1);
+ if (getprop("/systems/thrust/eng-out") != 1) {
+ if (getprop("/controls/engines/thrust-limit") == "FLX") {
+ if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) {
+ setprop("/it-autoflight/input/athr", 1);
+ }
+ setprop("/controls/engines/engine[0]/throttle-fdm", 0.99);
+ } else {
+ setprop("/controls/engines/engine[0]/throttle-fdm", 0.95);
}
- setprop("/controls/engines/engine[0]/throttle-fdm", 0.99);
- } else {
- setprop("/controls/engines/engine[0]/throttle-fdm", 0.95);
}
setprop("/systems/thrust/state1", "MCT");
} else if (thr1 >= 0.83 and thr1 < 0.95) {
@@ -129,13 +132,15 @@ setlistener("/controls/engines/engine[1]/throttle-pos", func {
setprop("/systems/thrust/state2", "MAN THR");
unflex();
} else if (thr2 >= 0.78 and thr2 < 0.83) {
- if (getprop("/controls/engines/thrust-limit") == "FLX") {
- if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) {
- setprop("/it-autoflight/input/athr", 1);
+ if (getprop("/systems/thrust/eng-out") != 1) {
+ if (getprop("/controls/engines/thrust-limit") == "FLX") {
+ if (getprop("/gear/gear[0]/wow") == 1 and (engstate1 == 3 or engstate2 == 3)) {
+ setprop("/it-autoflight/input/athr", 1);
+ }
+ setprop("/controls/engines/engine[1]/throttle-fdm", 0.99);
+ } else {
+ setprop("/controls/engines/engine[1]/throttle-fdm", 0.95);
}
- setprop("/controls/engines/engine[1]/throttle-fdm", 0.99);
- } else {
- setprop("/controls/engines/engine[1]/throttle-fdm", 0.95);
}
setprop("/systems/thrust/state2", "MCT");
} else if (thr2 >= 0.83 and thr2 < 0.95) {
@@ -187,14 +192,6 @@ var atoff_request = func {
}
}
-setlistener("/systems/thrust/state1", func {
- thrust_lim();
-});
-
-setlistener("/systems/thrust/state2", func {
- thrust_lim();
-});
-
var thrust_lim = func {
state1 = getprop("/systems/thrust/state1");
state2 = getprop("/systems/thrust/state2");
@@ -266,7 +263,18 @@ var unflex = func {
var thrust_loop = func {
state1 = getprop("/systems/thrust/state1");
state2 = getprop("/systems/thrust/state2");
- if ((state1 == "CL") and (state2 == "CL")) {
+
+ thrust_lim();
+
+ if (getprop("/gear/gear[1]/wow") == 0 and getprop("/gear/gear[2]/wow") == 0 and (getprop("/engines/engine[0]/state") != 3 or getprop("/engines/engine[1]/state") != 3)) {
+ setprop("/systems/thrust/eng-out", 1);
+ } else {
+ setprop("/systems/thrust/eng-out", 0);
+ }
+
+ if (state1 == "CL" and state2 == "CL" and getprop("/systems/thrust/eng-out") != 1) {
+ setprop("/systems/thrust/lvrclb", "0");
+ } else if (state1 == "MCT" and state2 == "MCT" and getprop("/systems/thrust/lim-flex") != 1 and getprop("/systems/thrust/eng-out") == 1) {
setprop("/systems/thrust/lvrclb", "0");
} else {
var status = getprop("/systems/thrust/lvrclb");
@@ -286,7 +294,7 @@ var thrust_loop = func {
setprop("/systems/thrust/lvrclb", "0");
}
}
-
+
# ias = getprop("/instrumentation/airspeed-indicator/indicated-speed-kt");
# flaps = getprop("/controls/flight/flap-pos");
# alphaProtSpd = getprop("/FMGC/internal/alpha-prot-speed");
diff --git a/Systems/fadec-cfm.xml b/Systems/fadec-cfm.xml
index 856ba3ae..79fb501d 100644
--- a/Systems/fadec-cfm.xml
+++ b/Systems/fadec-cfm.xml
@@ -279,6 +279,20 @@
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state1
+ MCT
+
+
/systems/thrust/state1
MAN THR
@@ -302,16 +316,60 @@
-
- /systems/thrust/state1
- MAN THR
-
+
+
+ /systems/thrust/eng-out
+ 0
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
/it-autoflight/output/athr
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state1
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
/systems/thrust/state1
CL
@@ -338,6 +396,34 @@
1
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state1
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
/systems/thrust/state1
CL
@@ -373,6 +459,20 @@
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state2
+ MCT
+
+
/systems/thrust/state2
MAN THR
@@ -396,16 +496,60 @@
-
- /systems/thrust/state2
- MAN THR
-
+
+
+ /systems/thrust/eng-out
+ 0
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
/it-autoflight/output/athr
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
/systems/thrust/state2
CL
@@ -432,6 +576,34 @@
1
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
/systems/thrust/state2
CL
diff --git a/Systems/fadec-iae.xml b/Systems/fadec-iae.xml
index b68b0d17..7305caff 100644
--- a/Systems/fadec-iae.xml
+++ b/Systems/fadec-iae.xml
@@ -618,6 +618,20 @@
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state1
+ MCT
+
+
/systems/thrust/state1
MAN THR
@@ -641,16 +655,60 @@
-
- /systems/thrust/state1
- MAN THR
-
+
+
+ /systems/thrust/eng-out
+ 0
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
/it-autoflight/output/athr
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state1
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
/systems/thrust/state1
CL
@@ -677,6 +735,34 @@
1
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state1
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
/systems/thrust/state1
CL
@@ -712,6 +798,20 @@
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state2
+ MCT
+
+
/systems/thrust/state2
MAN THR
@@ -735,16 +835,60 @@
-
- /systems/thrust/state2
- MAN THR
-
+
+
+ /systems/thrust/eng-out
+ 0
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
/it-autoflight/output/athr
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
/systems/thrust/state2
CL
@@ -771,6 +915,34 @@
1
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
/systems/thrust/state2
CL
diff --git a/Systems/fmgc-thrust.xml b/Systems/fmgc-thrust.xml
index d0e68f94..d50d6806 100644
--- a/Systems/fmgc-thrust.xml
+++ b/Systems/fmgc-thrust.xml
@@ -192,6 +192,54 @@
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+
+ /systems/thrust/state1
+ MCT
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
+
+
/systems/thrust/state1
MAN
@@ -276,6 +324,54 @@
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+
+ /systems/thrust/state1
+ MCT
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
+
+
/systems/thrust/state1
MAN
@@ -358,6 +454,54 @@
1
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+
+ /systems/thrust/state1
+ MCT
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
+
+
/systems/thrust/state1
MAN
@@ -430,6 +574,54 @@
2
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+
+ /systems/thrust/state1
+ MCT
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
+
+
/systems/thrust/state1
MAN
@@ -471,6 +663,54 @@
0
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+ /systems/thrust/lim-flex
+ 0
+
+
+
+ /systems/thrust/state1
+ MCT
+
+
+ /systems/thrust/state2
+ MCT
+
+
+
+
+
+ /systems/thrust/eng-out
+ 1
+
+
+
+
+ /controls/engines/engine[0]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state1
+ MAN THR
+
+
+
+
+ /controls/engines/engine[1]/throttle-pos
+ 0.83
+
+
+ /systems/thrust/state2
+ MAN THR
+
+
+
+
/systems/thrust/state1
MAN
diff --git a/revision.txt b/revision.txt
index fefa68a8..8e0f03b2 100644
--- a/revision.txt
+++ b/revision.txt
@@ -1 +1 @@
-4062
\ No newline at end of file
+4063
\ No newline at end of file