Cory Hamasaki's DC Y2K Weather Report V2, # 9
            "February 24, 1998 -  675 days to go."  WRP65
                          FINAL
    (c) 1997, 1998 Cory Hamasaki - I grant permission to distribute and
reproduce this article as long as this entire document is reproduced in
its entirety including this notice.  I do not grant permission to
a commercial publisher to reprint this in print media.

As seen in
   USENET:comp.software.year-2000
   http://www.elmbronze.demon.co.uk/year2000/
   http://www.kiyoinc.com/HHResCo.html

Please fax or email copies of this to your geek pals, especially those
idiots who keep sending you lightbulb, blonde, or Bill Gates jokes,
and urban legends like the Arizona rocket car story.

If you have a Y2K webpage, feel free to host the Weather Reports.

Don't forget- April 2, 3 1998, Geek Out.
Project Dumbass needs you.

In this issue:

1. Old GPS News
2. Feb DC Y2K Meeting Embeddeds
   ICBM Launch Controls and Rick Cowles.
3. ALC 10 JCL, Assembly Listing
4. Quarter Million Dollars offered for Y2K idea
5. CCCC

--------------- Old GPS News? ------------------

<GCN is a DC area tabloid that reports on... the government and computers.  I 
invoke fair use as an Y2K commentator and educator and offer this digital 
clipping to my students as part of our Y2K studies.>

"Government Computer News" 17 April 1997

Gregory Slabodkin

DOD Computing
What's to be done with GPS?

Paige says the vital system will be readied and waiting for the year
2000. Of the Defense Department's myriad systems, the Global Positioning
System is most vulnerable to malfunction and most likely to suffer
devastating consequences due to year 2000 code problems, DOD officials
have concluded. "People are depending on this system far beyond
anybody's expectations," said Lt. Col. Rick Reaser, chief engineer for
the Navstar GPS Joint Program Office at Los Angeles Air Force Base,
Calif. "People's lives depend on this system, and we take that very
seriously.
          
No play toy 

DOD plans for all military aircraft to use GPS for navigation by 2000
and the military's growing dependence on GPS-guided smart bombs have
heightened Pentagon concerns about the vulnerability of the navigation
system to year 2000 glitches. First showcased during Operation Desert
Storm, GPS has become the source for precise and accurate targeting
information for the Tomahawk cruise missile, Joint Direct Attack
Munition, Army Tactical Missile System and Joint Standoff Weapon. 

"The most significant system today that is not [year 2000] compliant is
GPS, which would have more impact than anything else," Emmett Paige Jr.,
assistant secretary of Defense for command, control, communications and
intelligence, recently told the House Government Reform and Oversight
Subcommittee on Government Management, Information and Technology. "Yet
I have no doubt that GPS will be ready along with all the other weapon
systems and command and control systems in the Department of Defense." 

The GPS year 2000 problem is threefold and reflects the three components
of the navigation system: the space segment, the ground control segment
and the user segment. GPS consists of 24 operational Navstar satellites
mounted on six orbital planes that continuously broadcast navigation
signals to ground stations. Specialized computers built into
inexpensive, portable GPS receivers in turn derive highly accurate
position and velocity information by correlating data uploaded to the
satellites from ground stations. 

Ground gaffes 

According to documents provided to Congress earlier this month by
Paige's office, the year 2000 problems within the space segment can be
found in two pieces of ground equipment: the Bus Ground Support
Equipment vehicle checkout stations and the Boeing Mission Operation
Support Center (MOSC). 

Software to correct the year 2000 problem in the Bus Ground Support
Equipment vehicle checkout stations already exists, and DOD will install
it during the normal systems maintenance lifecycle. But the MOSC date
code problem lies in its underlying commercial products. So DOD will
replace MOSC with the Integrated Mission Operation Support Center
(IMOSC), which it expects to finish in December 1999. 

But GPS JPO is working to push the completion date up at least six
months to June 1999. The IMOSC project is part of a $1.3 billion GPS
Block IIF satellite contract that DOD awarded to Boeing Co. last April.

The GPS ground control segment consists of six monitor stations, four
ground antennas and a master control station. The software needing date
code fixes generates the uplink code to the satellites. It was written
in the 1970s and uses only two-digit date fields. 

The original plan was to replace the old code as part of a modernization
of the ground control segment, or Architecture Evolutionary Plan (AEP).
But schedule delays have pushed AEP's operational beginning to mid-2000. 

"It looks like that schedule is slipping out," Reaser said. "The
replacement system may or may not be there in time for year 2000
rollover. So what we're going to do is upgrade the current system to be
Y2K-tolerant as sort of the backup plan which may become our primary
plan." 
              
Plan B 

GPS JPO officials have decided to rewrite some of the existing legacy
code for the ground control segment at a cost of $7.6 million. Lockheed
Martin Federal Systems has been assessing the code and will rewrite it
under an existing maintenance contract. Until then, GPS JPO will
incrementally integrate modifications as part of its normal software
maintenance releases. Though the GPS user segment does not have a year
2000 problem per se, it does have a clock overflow problem, the Z-count
rollover. This rollover occurs every 1,024 weeks; the first one comes in
August 1999. 

GPS' user segment consists of the antennas and receiver-processors that
provide positioning, velocity and precise timing to the users, such as
the Army handheld GPS receivers and Navy shipboard receivers. Although
GPS JPO established specifications for GPS receivers, some manufacturers
did not account for the Z-count rollover in the satellites' atomic
clocks, which synchronize the navigational signals. 

To date, the only GPS receivers that GPS JPO has identified as having
the Z-count rollover problem are older Rockwell-Collins 3A airborne
receivers and 3S shipboard receivers with Link 40 software. 

As part of scheduled depot maintenance, users must manually reset
affected receivers. Those with flash memory or removable programmable
read-only memory can be reset easily to accommodate the rollover. Users
will have to replace altogether any receivers that cannot be reset.

<Your homework assignment is to analyze this report and for the space segment,
decide whether Boeing will complete the 1.3 billion dollar Block IIF/IMOSC
project on December 1999 or June 1999 or ?????. The final exam will be in 675
days.  This will count as 50% of your grade.>

<Your term project is an analysis on the AEP ground segment, scheduled for
completion some time after 2000. Will it or the $7.6 million quick patch
succeed or will both fail?  Hint to the student: Lockheed Martin is the same
company that is doing the superb job on the FAA's computers.>

<I looked for more recent info than April 17, 1997 but couldn't find anything.
In Y2K, no news is a sure sign of a coverup.  Everyone's been focused on 
Z-count, not the MOSC or AEP.  Similarly in banking, we're all looking at our 
credit cards and have no information on check processing, loan reconciliation,
savings account processing, money markets, CD's, or electronic funds 
transfers.>

------------- Feb DC Y2K Meeting --------------------
------------- ICBM Launch Controls ------------------
While we're in butt-pucker mode, here's my record copy of the February DC 
Y2K meeting:

DC Y2K User's group meeting - Embeddeds - Fannie Mae - February 17, 1998, This
is a public, unclassified meeting held monthly in Washington DC.  5:30-9:00PM. 
There were 200+ attendees.

There were five speakers:

1. Diane Shields - VP CACI - Submarine Fire Control Systems, ICBM Launch
Controls.

6 months ago, CACI discovered "a major, catastrophic problem" in ICBM launch
controls.  The launch control system will fail because of a Y2K date and time
flaw. The failure was fail-safe, as it's supposed to be.  The ICBMs will be
unlaunchable. Of course, that presents another problem.

Diane gave a failure time and date which is in the future. Certainly the
software will be fixed by then, if it is not already fixed.  She would not 
have reported to a user's forum like DC Y2K unless it had already been 
fixed and the fix tested by an IV&V team.

She detailed the bit level anomaly that initiates the problem.  It has to do 
with characteristics of binary counters and made sense.  It is analogous
to but not related to the GPS roll over problem.

Diane enumerated several problems with working with legacy embedded
systems, a major one was: Subsystem vendors go out of business.

She explained Black Box v. White Box testing; in White box testing, you can 
open the box and test the components and analyze the machine states.

She offered some guidance: Use Qualified Personnel; Start in 1997 <oops>;
Have accurate documentation; Keep records; Too late for large systems.

2. Pete Himmelburger - GTE - Phones

License latch; ambiguity; horizontal tests; unit v. system tests; test
platforms unavailable at any cost; only fix absolutely critical; plan, plan,
plan; document. Horizontal tests are full systems tests. 

3. Rick Cowles - DEC/Compaq - Utilities

Nukes provide 20% of US Power; 60% in NJ; no easy fixes; Industry late; cited 
failures discovered in testing.

4. Hernando Quintero - BRI - Power generation

Based on technical assessment of hundreds of systems in 12 generating
facilities including Gas, Oil, and Coal but not Nuclear, 400 person days per 
site; expert engineers.

15% of systems are not Y2K compliant and have problems ranging from minor 
inconveniance to loss of life.  He didn't say but I'm guessing he's talking 
about boiler explosions and fires.  There are 200 major control and monitoring
systems in a power plant.

They found problems found in systems responsible for boilers, water
treatment, programmable sequence controls, area control systems, cc20 boiler
management, turbine management, smart sensor data freeze, etc.

5. Tom Shope - FDA - Medical systems.

Pacemakers OK (except perhaps one obsolete model) but pacemaker monitoring 
systems and external control systems may have problems.  Imaging systems and 
radiation therapy systems suspected to have problems.  FDA sent out a request 
for information from medical equipment suppliers <bandaids, crutches OK> but 
they are concerned about complex computer controlled system.  Responses due in
March, monitor http://www.fda.gov/cdrh click down to Y2K info.

--- more inflamatory comments from the king of cluelessness ---

Last year we had a c.s.y2k squabble about nuclear missile controls; a 
denial-head who said his wife had been a launch officer ran his keyboard,
called us stupid for worrying about launch controls.  Well guess what, CACI 
has run tests and has found date problems in nuclear missile launch controls.

Just because his wife knew the combo to the safe and how to key the
system, doesn't mean she has any understanding about what's under the hood. 
A-ha-ha, I'm laughing at YOU.

And the GPS problem has three parts, space, ground control, not just the
receivers, so you pilots and air traffic controllers, it's sextant and 
binocular time.  Note also that even the part that they say is fixed has yet
to be installed and run in production.

Last year we had a c.s.y2k squabble about planes, air traffic control, and the
FAA.  Turns out that KLM is canceling flights, the FAA is hosed, and <reported
at DC Y2K> there are 170 date sensitive systems in a jetliner.

Power? Rick managed to keep those denial heads in check but, surprise, 
Hernando has run tests and checks on 12 generating facilities and they have
big problems to include the possibility of loss of life.

Got it, denial-heads, Y2K is real; don't attempt to reason it out; don't 
extrapolate from what you know.  That's like going into a chemical 
manufacturing plant and declaring that you know that turning knobs won't cause
a problem... because you saw a chemistry set in a toy store once.

------------- ALC 10 -------------------

The ALC lessons are not intended to make a COBOL'er into an assembler 
gear-head.  The lessons show you what to look for so that you can read dumps 
and debug the little utility subroutines that infest production systems.  Your
management may not know that they exist but I've seen them, there're there, 
and they can take down production.  Dump reading will help you debug certain 
kinds of COBOL and CICS problems.

IT and MIS shops used to have several assembler mechanics; not any more, now 
you're on your own.  Corporate America has right-sized itself into a lobotomy.

I ran the job on the MVS mainframe in my living room, copied it to a 1.44 and 
clipped the sysout into this file.

If you had clipped and run ALC-9, you'd have something that looks like this:

                                                J E S 2   J O B   L O G


05.03.04 JOB    4  IEF677I WARNING MESSAGE(S) FOR JOB ASM      ISSUED
05.03.04 JOB    4  $HASP373 ASM      STARTED - INIT  A - CLASS A - SYS H155
05.03.18 JOB    4  IEF450I ASM GO - ABEND S0C1 U0000
05.03.18 JOB    4  $HASP395 ASM      ENDED


.------ JES2 JOB STATISTICS ------      


. 16 FEB 98 JOB EXECUTION DATE          


.        47 CARDS READ                  


.     1,085 SYSOUT PRINT RECORDS        


.         5 SYSOUT PUNCH RECORDS        


.      0.24 MINUTES EXECUTION TIME      

    1     //ASM    JOB (1234,5678),'C.S.Y2K',CLASS=A,MSGLEVEL=(1,1)               JOB    4
    2     //       EXEC  ASMFCLG  
    3     XXASMFCLG  PROC MAC='SYS1.MACLIB',MAC1='SYS1.MACLIB'                    00050000
    4     XXASM      EXEC PGM=IFOX00,PARM=OBJ,REGION=128K                         00100000
    5     XXSYSLIB   DD   DSN=&MAC,DISP=SHR                                       00150000
    6     XX         DD   DSN=&MAC1,DISP=SHR                                      00200000
    7     XXSYSUT1   DD   DSN=&&SYSUT1,UNIT=SYSDA,SPACE=(1700,(600,100)),         00250000
          XX             SEP=(SYSLIB)                                             00300000
    8     XXSYSUT2   DD   DSN=&&SYSUT2,UNIT=SYSDA,SPACE=(1700,(300,50)),          00350000
          XX             SEP=(SYSLIB,SYSUT1)                                      00400000
    9     XXSYSUT3   DD   DSN=&&SYSUT3,UNIT=SYSDA,SPACE=(1700,(300,50))           00450000
   10     XXSYSPRINT DD   SYSOUT=A,DCB=BLKSIZE=1089                               00500000
   11     XXSYSPUNCH DD   SYSOUT=B                                                00550000
   12     XXSYSGO    DD   DSN=&&OBJSET,UNIT=SYSDA,SPACE=(80,(200,50)),            00600000
          XX             DISP=(MOD,PASS)                                          00650000
   13     //ASM.SYSIN  DD *       
   14     XXLKED     EXEC PGM=IEWL,PARM=(XREF,LET,LIST,NCAL),REGION=128K,         00700000
          XX             COND=(8,LT,ASM)                                          00750000
   15     XXSYSLIN   DD   DSN=&&OBJSET,DISP=(OLD,DELETE)                          00800000
   16     XX         DD   DDNAME=SYSIN                                            00850000
   17     XXSYSLMOD  DD   DSN=&&GOSET(GO),UNIT=SYSDA,SPACE=(1024,(50,20,1)),      00900000
          XX             DISP=(MOD,PASS)                                          00950000
   18     XXSYSUT1   DD   DSN=&&SYSUT1,UNIT=(SYSDA,SEP=(SYSLIN,SYSLMOD)),         01000000
          XX             SPACE=(1024,(50,20))                                     01050000
   19     XXSYSPRINT DD   SYSOUT=A                                                01100000
   20     XXGO       EXEC PGM=*.LKED.SYSLMOD,COND=((8,LT,ASM),(4,LT,LKED))        01150000
   21     //GO.SYSUDUMP DD SYSOUT=A       
 STMT NO. MESSAGE
-  
    5     IEF653I SUBSTITUTION JCL - DSN=SYS1.MACLIB,DISP=SHR  
    6     IEF653I SUBSTITUTION JCL - DSN=SYS1.MACLIB,DISP=SHR  
   20     IEF686I DDNAME REFERRED TO ON DDNAME KEYWORD IN PRIOR STEP WAS NOT RESOLVED 
IEF236I ALLOC. FOR ASM ASM
IEF237I 149  ALLOCATED TO SYSLIB
IEF237I 149  ALLOCATED TO
IEF237I 149  ALLOCATED TO SYSUT1
IEF237I 149  ALLOCATED TO SYSUT2
IEF237I 149  ALLOCATED TO SYSUT3
IEF237I JES2 ALLOCATED TO SYSPRINT
IEF237I JES2 ALLOCATED TO SYSPUNCH
IEF237I 149  ALLOCATED TO SYSGO
IEF237I JES2 ALLOCATED TO SYSIN
IEF142I ASM ASM - STEP WAS EXECUTED - COND CODE 0008
IEF285I   SYS1.MACLIB                                  KEPT
IEF285I   VOL SER NOS= RES538.
IEF285I   SYS1.MACLIB                                  KEPT
IEF285I   VOL SER NOS= RES538.
IEF285I   SYS98047.T050304.RA000.ASM.SYSUT1            DELETED
IEF285I   VOL SER NOS= RES538.
IEF285I   SYS98047.T050304.RA000.ASM.SYSUT2            DELETED
IEF285I   VOL SER NOS= RES538.
IEF285I   SYS98047.T050304.RA000.ASM.SYSUT3            DELETED
IEF285I   VOL SER NOS= RES538.
IEF285I   JES2.JOB00004.SO0102                         SYSOUT
IEF285I   JES2.JOB00004.SO0103                         SYSOUT
IEF285I   SYS98047.T050304.RA000.ASM.OBJSET            PASSED
IEF285I   VOL SER NOS= RES538.
IEF285I   JES2.JOB00004.SI0101                         SYSIN
IEF373I STEP /ASM     / START 98047.0503
IEF374I STEP /ASM     / STOP  98047.0503 CPU    0MIN 04.48SEC SRB    0MIN 00.12SEC VIRT   128K SYS   204K
IEF236I ALLOC. FOR ASM LKED
IEF237I 149  ALLOCATED TO SYSLIN
IEF237I DMY  ALLOCATED TO
IEF237I 149  ALLOCATED TO SYSLMOD
IEF237I 149  ALLOCATED TO SYSUT1
IEF237I JES2 ALLOCATED TO SYSPRINT
IEF142I ASM LKED - STEP WAS EXECUTED - COND CODE 0000
IEF285I   SYS98047.T050304.RA000.ASM.OBJSET            DELETED
IEF285I   VOL SER NOS= RES538.
IEF285I   SYS98047.T050304.RA000.ASM.GOSET             PASSED
IEF285I   VOL SER NOS= RES538.
IEF285I   SYS98047.T050304.RA000.ASM.SYSUT1            DELETED
IEF285I   VOL SER NOS= RES538.
IEF285I   JES2.JOB00004.SO0104                         SYSOUT
IEF373I STEP /LKED    / START 98047.0503
IEF374I STEP /LKED    / STOP  98047.0503 CPU    0MIN 00.84SEC SRB    0MIN 00.14SEC VIRT   128K SYS   204K
IEF236I ALLOC. FOR ASM GO
IEF237I 149  ALLOCATED TO PGM=*.DD
IEF237I JES2 ALLOCATED TO SYSUDUMP
IEF472I ASM GO - COMPLETION CODE - SYSTEM=0C1 USER=0000
IEF285I   SYS98047.T050304.RA000.ASM.GOSET             KEPT
IEF285I   VOL SER NOS= RES538.
IEF285I   JES2.JOB00004.SO0105                         SYSOUT
IEF373I STEP /GO      / START 98047.0503
IEF374I STEP /GO      / STOP  98047.0503 CPU    0MIN 01.15SEC SRB    0MIN 00.06SEC VIRT    40K SYS   228K
IEF237I 149  ALLOCATED TO SYS00001
IEF285I   SYS98047.T050318.RA000.ASM.R0000001          KEPT
IEF285I   VOL SER NOS= RES538.
IEF285I   SYS98047.T050304.RA000.ASM.GOSET             DELETED
IEF285I   VOL SER NOS= RES538.
IEF375I  JOB /ASM     / START 98047.0503
IEF376I  JOB /ASM     / STOP  98047.0503 CPU    0MIN 06.47SEC SRB    0MIN 00.32SEC

As a mainframe COBOL'er you should recognize the JES log, the JCL, and the 
SMB's, System Message Blocks. Note 12 lines up, the 0C1.  Pull out your IBM
card, Program Interruption Codes, 0001 Operation exception.

Sigh, IBM documentation.  0C1, so you look for 0001 on the reference card.

In the JES log, the IEF450I ABEND S0C1 is the same as the IEF472I SYSTEM=0C1

Here's your homework for the week:

  LOC  OBJECT CODE    ADDR1 ADDR2  STMT   SOURCE STATEMENT                                       ASM 0201 05.03 02/16/98

                            0000A     1 R10      EQU   10      
                            0000B     2 R11      EQU   11      
                            0000C     3 R12      EQU   12      
                            0000D     4 R13      EQU   13      
                            0000E     5 R14      EQU   14      
                            0000F     6 R15      EQU   15      
                            00000     7 R0       EQU   0       
                            00001     8 R1       EQU   1       
                            00002     9 R2       EQU   2       
                            00003    10 R3       EQU   3       
                            00004    11 R4       EQU   4       
                            00005    12 R5       EQU   5       
000000                               13 STCK     CSECT 
                                     14          SAVE  (14,12),,STCK..&SYSDATC 
000000                               15+         DS    0H                                                       01650000
000000 90EC D00C      0000C          16+         STM   14,12,12(13)                      SAVE REGISTERS         02950000
000004 05C0                          17          BALR  R12,0               INIT BASE   
                            00006    18          USING *,R12               ADDRESS     
000006 50D0 C04A      00050          19          ST    R13,SAVE+4          SAVE OLD SAVE       
00000A 41D0 C046      0004C          20          LA    R13,SAVE            COPY IN NEW SAVE    
                                     21 *...   
00000E 1744                          22          XR    R4,R4   
000010 5840 C08E      00094          23          L     R4,COUNT
000014 8840 0004      00004          24          SRL   R4,4               SHIFT OUT THE SIGN   
                                     25 *...   
000018 4130 0003      00003          26          LA    R3,3               R3 = 3       
00001C 4150 C092      00098          27          LA    R5,SLOTS           R5 = &SLOTS  
000020                               28 DOLOOP   DS    0H      
000020 4140 4001      00001          29          LA    R4,1(,R4)          INCREMENT YEAR BY ONE
000024 1824                          30          LR    R2,R4              R2 = R4      
000026 8920 0004      00004          31          SLL   R2,4               MAKE ROOM FOR THE SIGN       
                                     32 *...   
00002A 5020 5000      00000          33          ST    R2,0(,R5)          *SLOT = R2   
00002E 960F 5003      00003          34          OI    3(R5),X'0F'        TURN ON THE SIGN     
000032 4150 5004      00004          35          LA    R5,4(,R5)          SLOT++       
000036 4630 C01A      00020          36          BCT   R3,DOLOOP          R3--; IF R3 > 0 GOTO DOLOOP; 
00003A                               37 EXIT     DS 0H 
00003A 58D0 C04A      00050          38          L     R13,SAVE+4         RELOAD OLD SAVE      
00003E 0000                          39          DC    XL2'0000'          ABEND.       
                                     40          RETURN (14,12),RC=0   
000040 98EC D00C      0000C          41+         LM    14,12,12(13)                      RESTORE THE REGISTERS  00650000
000044 41F0 0000      00000          42+         LA    15,0(0,0)                         LOAD RETURN CODE       01750000
000048 07FE                          43+         BR    14                                RETURN                 02000000
                                                                                                                PAGE    3


  LOC  OBJECT CODE    ADDR1 ADDR2  STMT   SOURCE STATEMENT                                       ASM 0201 05.03 02/16/98

00004C                               45 SAVE     DS 18F
000094 0001978C                      46 COUNT    DC PL4'1978'          
000098                               47 SLOTS    DS 4F 
000000                               48          END     STCK  

                                                  CROSS-REFERENCE                                              PAGE    4

Using your S/390 reference card, look up the machine instructions and match 
the opcodes to the object code.  For example, the last instruction, BR 14, 
assembles to 07FE,  07 is branch on condition register.  F is the mask and 
means always. E is register 14.

The point of this exercise is to become familiar with the opcodes and machine 
formats.  Remember 90ECD00C, 98ECD00C, and 07FE are important clues in dumps.

Extra credit, go the other way with 05EF.

And as usual, any denial-heads who are still reading, please feel free to jump
in.  Just because you clicked on a word processor or read a couple Jerry 
Pontificate articles in Byle Magazine, that doesn't mean you know anything
about enterprise scale computing.

I'm guessing that there are only two types who are reading this far, real 
assembler gear-heads for whom this is like reading a third grade book on a 
visit to the zoo and S/390 non-assembler programmers who are breaking a sweat 
but on every lesson say, a-ha, I've always wondered how that worked, who are 
starting to feel the power of the force.

----------- Quarter Million Dollars offered for Y2K Idea ----

http://www.worldbank.org/infodev/y2k.html

Proposal form is in http://www.worldbank.org/infodev/formword.doc

The Information for Development Program (infoDev) is concerned that developing
countries are slow to begin the work necessary to convert information systems
to avoid the Year 2000 problem (Y2K), will have difficulty allocating the 
large amounts of resources appropriate to the problem, and may face serious
disruption in many sectors in the next five years due to Y2K computer 
failures. 

infoDev therefore proposes to make a grant of up to $250,000 to the proponent
providing the best proposal on how to assist and stimulate developing 
countries to take a more proactive approach in dealing with the Y2K problem.

                    Carlos Braga
                    Program Manager
                    infoDev Program
                    World Bank
                    1818 H St.NW
                    Washington DC 20433
                    USA
                    Room No. F3K-266
                    Tel: (202) 458-5153
                    Fax: (202) 522-3186
                    E-mail: infodev@worldbank.org

A big DC Y2K WRP thanks to Mr. A. for the tip.
---------------- CCCC ---------------------

Cory's Clueless Closing Comments.

What about a print version of the DC Y2K report? Is there enough interest that
I could publish this as a monthly magazine.  I've seen a couple attempts at a 
Y2K magazine and believe that with a little hired help, I could do better.

Couple things, print magazines have a better reach than ezines.  They also 
have more credibility, although I don't know why.

I have more to say, but it's so clueless that I better wait a week....

cory hamasaki   675 days.