diff --git a/Luminary099/AOSTASK_AND_AOSJOB.agc b/Luminary099/AOSTASK_AND_AOSJOB.agc
index 51a8d0c..4e3cda9 100644
--- a/Luminary099/AOSTASK_AND_AOSJOB.agc
+++ b/Luminary099/AOSTASK_AND_AOSJOB.agc
@@ -31,23 +31,23 @@
 # Page 1485
 # PROGRAM NAME:		1/ACCS
 # PROGRAM WRITTEN BY: 	BOB COVELLI AND MIKE HOUSTON
-# LAST MODIFICATION:	FEB. 14, 1969 BY G. KALAN
+# *LAST MODIFICATION:	FEB. 14, 1969 BY G. KALAN
 #
 # PROGRAM DESCRIPTION:
-#	1/ACCS PROVIDES THE INTERFACE BETWEEN THE GUIDANCE PROGRAMS AND THE DIGITAL AUTOPILOT.  WHENEVER THERE IS A
+#		1/ACCS PROVIDES THE INTERFACE BETWEEN THE GUIDANCE PROGRAMS AND THE DIGITAL AUTOPILOT.  WHENEVER THERE IS A
 # 	CHANGE IN THE MASS OF THE VEHICLE, IN THE DEADBAND SELECTED, IN THE VEHICLE CONFIGURATION (ASCENT-DESCENT-
 #	DOCKED), AND DURING A FRESH START OR A RESTART, 1/ACCS IS CALLED TO COMMUNICATE THE DATA CHANGES TO THE DAP.
 #
-# 	THE INPUTS TO 1/ACCS ARE MASS, ACCELERATION (ABDELV), DEADBAND (DB), OFFSET ACCELERATIONS (AOSQ AND AOSR),
+# 		THE INPUTS TO 1/ACCS ARE MASS, ACCELERATION (ABDELV), DEADBAND (DB), OFFSET ACCELERATIONS (AOSQ AND AOSR),
 # 	STAGE VERIFY BIT (CHAN30, BIT2), DOCKED BIT (DAPBOOLS, BIT13), DRIFT BIT (DAPBOOLS, BIT8), USEQRJTS (DAPBOOLS,
-# 	BIT14), AND SURFACE FLAG (FLAGWRDB, BIT8), AND CH5MASK.
+# 	BIT14), AND SURFACE FLAG (FLAGWRD8, BIT8), AND CH5MASK.
 #
-#	1/ACCS COMPUTES THE JET ACCELERATIONS (1JACC, 1JACCQ, 1JACCR) AS FUNCTIONS OF MASS.  1JACCU AND 1JACCV ARE
+#		1/ACCS COMPUTES THE JET ACCELERATIONS (1JACC, 1JACCQ, 1JACCR) AS FUNCTIONS OF MASS.  1JACCU AND 1JACCV ARE
 #	FORMED BY RESOLVING 1JACCQ AND 1JACCR.  IN THE DESCENT CASE, THE DESCENT ENGINE MOMENT ARM (L, PVT-CG) IS ALSO
 # 	COMPUTED AS A FUNCTION OF MASS.  THE RATE OF CHANGE OF ACCELERATION DUE TO ROTATION OF THE GIMBAL (ACCDOTQ,
 #	ACCDOTR) IS ALSO COMPUTED IN THE DESCENT CASE.
 #
-#	AFTER THE ABOVE COMPUTATIONS, THE PROGRAM 1/ACCONT COMPUTES THE RECIPROCAL NET ACCELERATIONS ABOUT THE P, U,
+#		AFTER THE ABOVE COMPUTATIONS, THE PROGRAM 1/ACCONT COMPUTES THE RECIPROCAL NET ACCELERATIONS ABOUT THE P, U,
 # 	AND V AXES (2 JETS FOR P-AXIS, BOTH 1 AND 2 JETS FOR U AND V AXES), AND THE RECIPROCAL COAST ACCELERATIONS ABOUT
 # 	THE P, U, AND V AXES.  THE ACCELERATION FUNCTIONS (ACCFCTZ1 AND ACCFCTZ5) ARE ALSO COMPUTED FOR THESE AXES.  THE
 # 	FIRE AND COAST DEADBANDS AND AXISDIST ARE COMPUTED FOR EACH AXIS.  FLAT AND ZONE3LIM, THE WIDTH AND HEIGHT OF THE
@@ -65,9 +65,9 @@
 #
 # NORMAL EXIT:	VIA BANKJUMP
 #
-# ALARM AND EXIT MODES:  NONE
+# ALARM AND EXIT MODES:  NONE.
 #
-# INPUT/OUTPUT:  SEE PROGRAM DESCRIPTION.
+# INPUT/OUTPUT:  SEE PROGRAM DESCRIPTION
 #
 # DEBRIS:
 #	ALL OF THE EXECUTIVE TEMPORARY REGISTERS, EXCEPT FIXLOC AND OVFIND, AND THE CORE SET AREA FROM MPAC TO BANKSET.
@@ -108,7 +108,7 @@
 
 # DETERMINE MASS OF THE LEM.
 
-		CA	DAPBOOLS	# IS THE CSM DOCKED
+		CA	DAPBOOLS	# IS CSM DOCKED
 		MASK	CSMDOCKD
 		TS	DOCKTEMP	# STORE RECORD OF STATE IN TEMP (MPAC +3).
 		CCS	A
@@ -117,7 +117,7 @@
 		TS	LEMMASS
 
 # ON THE BASIS OF APSFLAG:
-#	SET THE P-AXIS RATE COMMAND LIMIT FOR 2-JET/2-JET CONTROL
+#	SET THE P-AXIS RATE COMMAND LIMIT FOR 2-JET/4-JET CONTROL
 #	SET MPAC, WHICH INDICATES THE PROPER SET OF COEFFICIENTS FOR THE LEM-ALONE F(MASS) CALCULATIONS
 #	ENSURE THAT THE LEM MASS VALUE IS WITHIN THE ACCEPTABLE RANGE