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Subject: How Not to Conduct a Training Class
Jim,
I just attended a workshop on GD&T taught by a team of our in-house
“experts”. They would read a passage out of the Y14.5 standard, and
then ask for our opinions on what it meant. Since most of the people
in the class were new to this stuff, we might as well have had
cardboard question marks hanging over our heads. After we displayed
a lot of shoulder shrugging and head shaking, they would say, “Ok
then, let’s move on to the next section.
After a while, some of us got the gist of what was going on and
decided to ask them what the passage meant. They said, “It’s open to
interpretation.” We said, “Okay, what’s your interpretation?” Then
they huddled up (a team of five “instructors”) and when the huddle
broke, they said, “You mean you don’t know?” And I was the one who
said, “Of course we don’t know. We’re here to learn.” And then they
huddled up again. When they came out of their mini-conference, one
said, “Well, I guess we hired the wrong people.” And I said,
“Someone definitely hired the wrong people to teach this workshop.”
I was told, in chorus, to “Just shut up.”
Many of the people in the class were so intimidated after that, that
they refused to speak for the rest of the day. I was asked not to
return for the next day of “training” and a letter rebuking my
conduct was added to my personnel file.
Some of those who attended the second day said, the
“instructor/experts” changed their tact. When they read a passage
from the standard and asked the “students” what they thought it
meant, if no one knew or asked a question, they said, “What’s wrong
with you that don’t know?” Or, “What’s wrong with you that you’d ask
a question like that? Are you stupid?” When one guy responded that
he “must be stupid for showing up to a second day of this class”, he
was asked to leave.
By the third day, they were down to one guy and he showed up just so
he wouldn’t have to go back to work. It was Friday and he said he
just wanted to sleep through the day and get to the weekend.
I don’t have a question for you. I just wanted to “whine and gripe”
(a quote from my letter of misconduct).
John (The Whiner with a Gripe)
John,
What can I say? You obviously signed up for the deluxe training
package.
Jim
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Figure 25-11 from my newest GD&T textbook
Subject: Question on Book-Minimum Wall Thickness Calculations Using
Tolerance Stack-Up Analysis
Jim,
I’ve been working my way through your book Geometric Dimensioning
and Tolerancing and had a question regarding one of your examples.
In Step 1 of the solution for Figure 25-11 on page 496, I understand
all of the calculations except that I would also expect there to be
some inclusion of the datum shift allowed for Maximum Material
Boundary on datum B for the central hole. Am I correct that this
would add another .040 to the diameter of the Outer Boundary of the
holes?
I’ve really enjoyed and learned a lot from the book so far.
Best regards,
Michael
From Page 497
Step 1:
.375 = LMC Hole
+ .035 = Geo. Tol. at LMC
Ř.410 = Outer Boundary Hole
+ .400 = Datum Feature Shift
Ř.810 = Outer Boundary Hole with Pattern Shift
+ .400 = Position Tol. of D
Ř1.210 = Outer Boundary Holes with all Facets
R.605
Step 2:
4.990 = LMC Outside Diameter
- .040 = Geo. Tol. at LMC Ř 4.950 = R2.475
Ř4.950 = Inner Boundary of Outside Diameter 2
Step 3:
1.600 Basic Distance between Holes
x 2 (1.4142)
Ř 2.263 Bolt Circle Diameter
R1.1315
FIGURE 25-12 [Circuit Graphed]
Michael,
The tolerance on datum feature B can either be used as
perpendicularity tolerance on the O.D., or it can be used as datum
feature shift for datum feature D. Since it was used as
perpendicularity tolerance on B, it would negate any shift of datum
feature D from datum B being referenced at MMB. Notice step 2 where
the perpendicularity tolerance is listed as .040. If it’s there, it
locks up the B feature. One way to understand this is to picture the
functional gage that inspects datum feature D. In this gage, datum
feature B would be simulated by a gage hole that is a diameter of
5.030. If you look at step 2 and add the .040 to the 4.990 (instead
of subtracting it as the step does), it shows that the O.D. would
(at 5.030) lock itself up inside the gage hole which is that size.
Hope this helps.
Jim
Subject: Mistake on Page 42 and 47 of your Workbook? Variables Data
Analysis
Hello, Mr. Meadows,
I purchased your book "Workbook and Answers for GDT" and going over
problems. I realize that space is limited and sometimes detailed
answers cannot be given. I so far cannot explain responses to some
questions:
Question 16 on Page 42;
0.04 straightness at RFS of surface elements. The part has a taper
as manufactured ranging from 100.1 to 99.9. If I were to look at
surface elements, draw two parallel lines (.04 apart) to axis of
part from 100.1, straightness is violated. 0.1 is greater than 0.04.
Am I missing something?
16. Circularity, Straightness & Total Runout

Regarding the last part of Question 21 on Page 47
I don't understand the question and answer regarding the .003
out-of-straightness. There is no mention of straightness on the
drawing and why would an inspector look at derived median. If the
part is made within the limits of size.....I don't understand?
Paul
The Problem as stated for page 47:
Part 12135 – Bushing: Using the following variables data, assess the
part on the following page and make assessments pertaining to its
compliance to the tolerances depicted.
Available collected measurement data:
•Outside diameter measures .525 at its largest and .519 at its
smallest.
•Part outside diameter is round to within .0002.
•FIM of I.D. while centered on and rotating about datum axis D is
.002 at each cross section.
•Inside diameter is .2550 at its largest and .2549 at its smallest.
•Part thickness (shown in the left side view) varies between .196
and .195. It is rigid.
•Part thickness (shown in the left side view) has a slight uniform
bow. Its derived median plane is out of straightness .003.

Paul,
Regarding page 42, in order for surface elements to be out of
straightness, the surface would have to have pits, bumps or curves.
None are shown. Taper has nothing to do with straightness.
On page 47, Rule #1 in ASME Y14.5 states that, unless otherwise
specified, rigid parts must have perfect form at MMC. In gaging
terms, the part must be able to fit the GO gage (which checks the
MMC) to meet size requirements. That part’s MMC in that view is
.197. The statement of the produced part’s condition is as follows:
•Part thickness (shown in the left side view) varies between .196
and .195. It is rigid.
•Part thickness (shown in the left side view) has a slight uniform
bow. Its derived median plane is out of straightness .003.
When you add .003 to either .195 or .196, one can see that the part
would not fit between two parallel planes that are .197 (the MMC
envelope-simulated by a GO gage) and would fail to comply with Rule
#1. In other words, it fails the size requirements.
Hope this helps.
James Meadows
Subject: Question on Composite Profile
Mr. Meadows,
I am hoping you can help me to understand the profile feature call
out on this drawing. I explain my thoughts in RED next to the RED
highlighted feature control frame.
Thanks in advance,
Mark

Mark,
Yes that’s correct. You must hold angle and location to the datum
structure to within 4mm and shape/form to within 3mm. The 3mm shape
control only applies to size if the features being controlled are
closed loop features (such as oddly configured holes and shafts). In
other words, it only applies if the controlled features have a size.
I can’t tell if they do from the illustration you sent, but the note
3 DUCT OPENINGS would seem to indicate that they do.
Profile isn’t required to reference datums. Composite profile
controls often don’t reference datums in the lower level (tighter
toleranced) control. The tightest tolerance controls form and if it
is an all-around or all-over control, it also controls size. If
datums are referenced in the lower level of a composite profile (or
position) control, they don’t control location, but can only control
orientation (angle).
Jim Meadows
Subject: Basic Dimension Question
Hi Jim,
A question came up that we would appreciate your opinion on: can you
have a “0.000” Basic dimension. The example would be when a datum is
in the same plane as the holes that are being dimensioned
David,
A zero basic dimension applies where axes, center planes or surfaces
are shown coincident (in the same place) on a drawing and geometric
tolerances establish the relationship between the features.
[Although this concept is not new to previous Y14.5 standards, this
statement explicitly states the concept for the Y14.5-2009
standard.]
In other words, it is implied, so there’s no reason to put it on the
drawing.
Jim
Subject: Positional Boundary
Jim,
I am a prior student of yours. Would you confirm or correct
following interpretation to attached drawing requirement stating
ASME Y14.100 applies.
The right and bottom sides of rectangular cutout must meet position
.005 callout with respect to datums B & C. The left and top sides of
cutout must conform to size tolerancing. Also, would any of the
fillet radii 4 places need to meet position .005 as well?
Regards,
Michael

Michael,
The widths must meet the size requirements of 1.500-1.510 and
.500-.510, and the positional boundary control states that the
surface of those widths may not violate a virtual condition boundary
that measures MMC minus .005 positional tolerance if the widths are
holes/slots or if they are shafts/tabs the inviolate boundary would
be the MMC plus .005. These boundaries are located at the true
position (perfect location and orientation) from the datums E and C.
The problem, as I see it, is that they located the surfaces of the
widths (with basic dimensions), whereas they should have located the
centerplane of the widths (with basic dimensions-one of which is
implied to be zero). They think they are locating the individual
surfaces, but should be locating the centerplanes. The position
tolerance zones are in the middle of the widths (two parallel planes
that are .005 apart at MMC). The local notes (BOUNDARY) just mean
they want you to simulate the effect of the position tolerances on
the surfaces of the width by simulating a gauge. These functional
gauges make sure that no portion of the width violates its virtual
condition boundary as calculated in the first paragraph of this
response. If these widths are slots, then picture the gage pin as
.495 X 1.495 and located right at true position (which is not
currently defined correctly). The surface of the widths must fit
over the gage pin to comply with the position control.
I don’t think that they know that position isn’t used to locate
planar surfaces with basic dimensions. It is used to locate the
middle of the feature (in this case the centerplanes). Usually the
features can be measured to determine if either 1) the centerplanes
have violated the tolerance zones which are two sets of parallel
planes .005 apart at MMC or 2) the surfaces of the controlled
features have violated the virtual condition boundary (as the gauge
I described would do). However, the local note BOUNDARY says do the
second thing.
I hope this helps.
Jim
Subject: Total Runout Question
Hi Jim,
You recently taught a class at NASA which my branch attended. We
have been holding group drawing “reviews” within the branch to help
sharpen what we learned in your class. The most recent one we did a
question surfaced that I thought you might clarify.
Attached is a copy of a total runout scheme along a compound datum
axis where both datums have total runout applied. This differs from
the approach of initially applying cylindricity then using total
runout and referencing the compound datum axis (I attached the
example from your book). Are these the same situation? Are both
schemes then correct?
Your input on this would be appreciated.
David
Illustration from Y14.5-2009:

David and All Interested Parties,
Yes, even though the illustration you sent from my textbook is the
more linear progressive way to define the part, the use of Runout or
Total Runout on all of the diameters, including the datum features
that will construct the compound axis they are measured from is, in
some ways, more logical. The premise is that since each diameter
alone doesn’t generate enough surface area to stabilize the part to
measure other diameters from, each doesn’t create enough stability
to measure the other datum feature from.
Illustration from my textbook:

Since each diameter generates an axis that is different from the
compound axis, you can say that each must be coaxial (using Runout,
Total Runout, Concentricity or Position) to the common axis formed
simultaneously from both together. I explain this when going over
the example you sent from my textbook and I have a worksheet in the
workbook on page 114 that analyzes the four controls when used that
way. In the worksheet, each possibility is explained as an option,
and only one would be selected.
Illustration from my workbook (Pick One of These Options-Position
vs. Runout vs. Total Runout vs. Concentricity):

Some feel uncomfortable in saying each datum feature diameter is
controlled to their compound axis, in that if we were to “chuck-up”
on both, they would be obscured and not measurable. The way around
that is to not “chuck-up” on both, but rather probe them with a CMM
and analyze the collected data, or put both in Vee-blocks which
leaves them exposed to measure, or center drill the part and put it
between centers, then measure every diameter to see how far off they
are from each other. If everything is measured from the same axis,
whether that axis is the proper datum axis or not, then every
diameter is related to each other to within the sum of their
tolerances to that common axis. In other words, if the part measures
within the tolerance, it is good. If not, another measurement tactic
can be used.
At any rate, the result of using either the linear progressive
method in my textbook, or the “one-fell-swoop” method on page 114 in
my workbook (and in the example you sent me from another source) can
reap the same or similar results.
I hope this helps.
Jim Meadows
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