diff --git a/Luminary099/P51-P53.agc b/Luminary099/P51-P53.agc
index c0a738d..1653b9e 100644
--- a/Luminary099/P51-P53.agc
+++ b/Luminary099/P51-P53.agc
@@ -197,7 +197,7 @@ P52D		CALL			# READ VEHICLE ATTITUDE AND
 		TC	BANKCALL	# DISPLAY GIMBAL ANGLES
 		CADR	GOFLASH
 		TC	GOTOPOOH
-		TCF	COARSTYP	# V33 -- PROCEED, SEE IF GYRO TORQUE COARSE
+		TCF	COARSTYP	# V33-PROCEED, SEE IF GYRO TORQUE COARSE
 P52H		TC	INTPRET
 		GOTO
 			P52D
@@ -215,14 +215,14 @@ VB05N09		=	V05N09
 V06N34*		VN	634
 
 # Page 931
-# CHECK FOR GYRO TORQUE COARSE ALIGNMENT
+# CHECK FOR GRRO TORQUE COARSE ALIGNMENT
 
 COARSTYP	CAF	OCT13
 		TC	BANKCALL	# DISPLAY V 50N25 WITH COARSE ALIGN OPTION
 		CADR	GOPERF1
-		TCF	GOTOPOOH	# V34 -- TERMIN&OE
-		TCF	REGCOARS	# V33 -- NORMAL COARSE
-		TC	INTPRET		# V32 -- GYRO TORQUE COARSE
+		TCF	GOTOPOOH	# V34-TERMIN&OE
+		TCF	REGCOARS	# V33-NORMAL COARSE
+		TC	INTPRET		# V32-GYRO TORQUE COARSE
 		VLOAD	MXV
 			XSMD		# GET SM(DESIRED) WRT SM(PRESENT)
 			REFSMMAT
@@ -264,7 +264,7 @@ P52LS		SET	CLEAR		# GET LANDING SITE ORIENTATION
 		STCALL	XSMD
 			LSORIENT
 		GOTO
-			P52D		# NOW GO COMPUTE GIMBAL ANGLES.
+			P52D		# NOW GO COMPUTE GIMBAL ANGLES
 
 # Page 933
 # SUBROUTINE TO CALCULATE AND DISPLAY THE LUNAR LANDING SITE
@@ -289,9 +289,9 @@ N89DISP		STQ
 LSDISP		CAF	V06N89*		# DISPLAY LAT,LONG/2,ALT
 		TC	BANKCALL
 		CADR	GOFLASH
-		TCF	GOTOPOOH	# V34 -- TERMINATE -- EXIT P57
-		TCF	+2		# V33 -- PROCEED -- ACCEPT LS DATA
-		TCF	LSDISP		# V32 OR E -- LOOK AGAIN AND/OR LOAD NEW LS
+		TCF	GOTOPOOH	# V34-TERMINATE-EXIT P57
+		TCF	+2		# V33-PROCEED- ACCEPT LS DATA
+		TCF	LSDISP		# V32 OR E- LOOK AGAIN AND/OR LOAD NEW LS
 
 		TC	INTPRET
 		DLOAD	SL1
@@ -309,57 +309,53 @@ LSDISP		CAF	V06N89*		# DISPLAY LAT,LONG/2,ALT
 V06N89*		VN	689
 
 # Page 934
-# NAME -- S50 ALIAS LOCSAM
+# NAME -S50 ALIAS LOCSAM
 # BY
 # VINCENT
-#
-# FUNCTION -- COMPUTE INPUTS FOR PICAPAR AND PLANET
+# FUNCTION - COMPUTE INPUTS FOR PICAPAR  AND PLANET
 #
 #	DEFINE
 #
-#	U   = UNIT( SUN WRT EARTH )
+#	U   = UNIT( SUN WRT EARTH)
 #	 ES
 #
-#	U   = UNIT( MOON WRT EARTH )
+#	U   =UNIT( MOON WRT EARTH)
 #	 EM
 #
-#	R   = POSITION VECTOR OF LEM
+#	R   =POSITION VECTOR OF LEM
 #	 L
 #
-#	R   = MEAN DISTANCE (384402KM) BETWEEN EARTH AND MOON
+#	R   =MEAN DISTANCE (384402KM) BETWEEN EARTH AND MOON
 #	 EM
 #
-#	P   = RATIO R  /(DISTANCE SUN TO EARTH) > .00257125
-#	             EM
+#	P   =RATIO   R  /(DISTANCE SUN TO EARTH)       >.00257125
+#	              EM
 #
-#	R   = EQUATORIAL RADIUS (6378.166KM) OF EARTH
+#	R   =EQUATORIAL RADIUSS (6378.166KM) OF EARTH
 #	 E
 #
 #	LOCSAM COMPUTES IN EARTH INFLUENCE
 #
-#	VSUN = U
-#	        ES
+#	 VSUN  = U
+#	          ES
 #
 #	VEARTH = -UNIT( R  )
 #	                 L
 #
-#	VMOON = UNIT(R  .U   - R  )
-#	              EM  EM    L
+#	VMOON  = UNIT(R  .U   - R  )
+#	               EM  EM    L
 #
-#	CSUN = COS 90
+#	CSUN   = COS 90
 #
 #	CEARTH = COS(5 + ARCSIN(R /MAG(R )))
 #	                         E      L
 #
-#	CMOON	= COS 5
+#	CMOON  = COS 5
 #
-# INPUT -- TIME IN MPAC
-#
-# OUTPUT -- LISTED ABOVE
-#
-# SUBROUTINES -- LSPOS, LEMPREC
-#
-# DEBRIS -- VAC AREA, TSIGHT
+# INPUT -  TIME IN MPAC
+# OUTPUT - LISTED ABOVE
+# SUBROUTINES -LSPOS,LEMPREC
+# DEBRIS - VAC AREA ,TSIGHT
 
 # Page 935
 		COUNT*	$$/LOSAM