diff --git a/Luminary099/P32-P35_P72-P75.agc b/Luminary099/P32-P35_P72-P75.agc
index d6a6626..a5a580a 100644
--- a/Luminary099/P32-P35_P72-P75.agc
+++ b/Luminary099/P32-P35_P72-P75.agc
@@ -79,39 +79,39 @@
 #		PARALLEL TO THE PLANE OF THE CSM ORBIT.  HOWEVER CREW
 # Page 619
 #		MODIFICATION OF DELTA V (LV) COMPONENTS MAY RESULT IN AN
-#		OUT-OF-PLANE CSI MANEUVER
-
+#		OUT-OF-PLANE CSI MANEUVER.
+#
 #	(8)	STATE VECTOR UPDATES BY P27 ARE DISALLOWED DURING AUTOMATIC
 #		STATE VECTOR UPDATING INITIATED BY P20 (SEE ASSUMPTION 10).
-
+#
 #	(9)	COMPUTED VARIABLES MAY BE STORED FOR LATER VERIFICATION BY
 #		THE GROUND.  THESE STORAGE CAPABILITIES ARE NORMALLY LIMITED
 #		ONLY TO THE PARAMETERS FOR ONE THRUSTING MANEUVER AT A TIME
 #		EXCEPT FOR CONCENTRIC FLIGHT PLAN MANEUVER SEQUENCES.
-
+#
 #	(10)	THE RENDEZVOUS RADAR MAY OR MAY NOT BE USED TO UPDATE THE LM
 #		OR CSM STATE VECTORS FOR THIS PROGRAM.  IF RADAR USE IS
-#		DESIRED THE RADAR WAS TURNED ON AND LOCKED BY THE CSM BY
+#		DESIRED THE RADAR WAS TURNED ON AND LOCKED ON THE CSM BY
 #		PREVIOUS SELECTION OF P20.  RADAR SIGHTING MARKS WILL BE MADE
 #		AUTOMATICALLY APPROXIMATELY ONCE A MINUTE WHEN ENABLED BY THE
 #		TRACK AND UPDATE FLAGS (SEE P20).  THE RENDEZVOUS TRACKING
 #		MARK COUNTER IS ZEROED BY THE SELECTION OF P20 AND AFTER EACH
 #		THRUSTING MANEUVER.
-
-#	(11)	THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM.
-
-#	(12)	THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS --
 #
-#			ACTIVE VEHICLE FLAG -- DESIGNATES THE VEHICLE WHICH IS
+#	(11)	THE ISS NEED NOT BE ON TO COMPLETE THIS PROGRAM.
+#
+#	(12)	THE OPERATION OF THE PROGRAM UTILIZES THE FOLLOWING FLAGS -
+#
+#			ACTIVE VEHICLE FLAG - DESIGNATES THE VEHICLE WHICH IS
 #			DOING RENDEZVOUS THRUSTING MANEUVERS TO THE PROGRAM WHICH
 #			CALCULATES THE MANEUVER PARAMETERS.  SET AT THE START OF
 #			EACH RENDEZVOUS PRE-THRUSTING PROGRAM.
 #
-#			FINAL FLAG -- SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
+#			FINAL FLAG - SELECTS FINAL PROGRAM DISPLAYS AFTER CREW HAS
 #			COMPLETED THE FINAL MANEUVER COMPUTATION AND DISPLAY
 #			CYCLE.
 #
-#			EXTERNAL DELTA V STEERING FLAG -- DESIGNATES THE TYPE OF
+#			EXTERNAL DELTA V STEERING FLAG - DESIGNATES THE TYPE OF
 #			STEERING REQUIRED FOR EXECUTION OF THIS MANEUVER BY THE
 #			THRUSTING PROGRAM SELECTED AFTER COMPLETION OF THIS
 #			PROGRAM.
@@ -119,16 +119,15 @@
 #	(13)	IT IS NORMALLY REQUIRED THAT THE ISS BE ON FOR 1 HOUR PRIOR TO
 #		A THRUSTING MANEUVER.
 #
-#	(14)	THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY
+#	(14)	THIS PROGRAM IS SELECTED BY THE ASTRONAUT BY DSKY ENTRY -
 #
 #			P32 IF THIS VEHICLE IS ACTIVE VEHICLE.
 #
-#			P72 IF THIS VEHICLE IS THE PASSIVE VEHICLE.
+#			P72 IF THIS VEHICLE IS PASSIVE VEHICLE.
 #
 # INPUT
-
+#
 #	(1)	TCSI		TIME OF THE CSI MANEUVER
-
 # Page 620
 #	(2)	NN		NUMBER OF APSIDAL CROSSINGS THRU WHICH THE ACTIVE
 #				VEHICLE ORBIT CAN BE ADVANCED TO OBTAIN THE CDH