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Thread Engagement Calculator —
How Deep to Tap, and the Tap Drill for Any Percent of Thread

By C&W Engineering Team
Two questions every tapped hole raises: what drill gives the percent of thread you want, and how many threads deep does the hole need to be so the bolt breaks before the threads strip? Pick a thread, the bolt material, and the material being tapped. The calculator gives the tap drill for any percent of thread with the nearest standard drill, and the minimum engagement length by the Machinery's Handbook shear-area method, including the correction for a soft tapped material like aluminum.[1][2]
Tap drill and engagement calculator
Threads and material strengths come from the tables further down this page. Percent of thread is the share of full thread height cut by the tap; 75% is the shop default. The engagement result is the depth of full thread, not the drilled depth.

Tap Drill for Any Percent of Thread

A tap does not have to cut the full thread height. The tap drill sets how much of the theoretical sharp-V height the tap engages, and the standard shop practice is about 75%, which gives nearly the full strength of a 100% thread at roughly half the tapping torque. Going below 60% is common in tough materials like Inconel and titanium to save taps; going above 80% rarely adds strength and breaks taps.[1]

Formulas
Inch: tap drill = major diameter − (0.0130 × percent of thread) / TPI. Metric: tap drill = major diameter − 1.299 × pitch × percent / 100. At 75% these reduce to the familiar major − 0.974/TPI and major − 0.974 × pitch, which is where the tap drill chart values come from.

The calculator then picks the closest standard drill from the drill size chart and reports the percent of thread that drill actually gives, so you can see whether it landed slightly above or below your target.

How Deep to Tap: Length of Engagement

A bolt in a tapped hole can fail three ways: the bolt breaks in tension, the bolt's external threads shear off, or the internal threads in the hole strip out. Good design makes the bolt break first, because a broken bolt is obvious and replaceable while stripped threads in a housing are neither. The engagement length that guarantees it comes from comparing the thread shear areas with the bolt's tensile stress area.[2]

QuantityFormula (basic dimensions, 60° threads)
Tensile stress area of the boltAt = 0.7854 (D − 0.9743 / n)² inch, or 0.7854 (D − 0.9382 P)² metric
External thread shear area per unit lengthAs = π n Kn [1 / (2n) + 0.57735 (Es − Kn)], with Kn = D − 1.0825 P and Es = D − 0.6495 P
Internal thread shear area per unit lengthAn = π n Ds [1 / (2n) + 0.57735 (Ds − En)], with Ds = D and En = D − 0.6495 P
Engagement, equal materialsLe = 2 At / As (external thread shear area equal to twice the tensile area)
Correction for a weaker tapped materialJ = (As × Ss,bolt) / (An × Ss,hole); if J > 1, multiply Le by J

Shear strength is taken as 0.6 times tensile strength for every material in the tables, a common engineering approximation. The calculator uses basic thread dimensions; class 2A/2B allowances make the real shear areas a few percent smaller, so treat the result as a design minimum and round up to the next practical depth. It also assumes uniform load sharing along the engaged threads and does not cover thread inserts, fatigue, or fine-pitch threads in soft materials, which strip more easily than the areas suggest.

Worked Example: 1/4-20 Grade 5 Bolt in 6061-T6

StepValue
Tap drill at 75%: 0.250 − 0.0130 × 75 / 200.2013 in → #7 drill (0.2010)
Tensile stress area At0.7854 × (0.250 − 0.0487)² = 0.0318 in²
Kn, Es0.1959 in, 0.2175 in
External shear area per inch Asπ × 20 × 0.1959 × [0.025 + 0.57735 × 0.0217] = 0.462 in² per inch
Engagement for equal materials, 2 At / As0.0636 / 0.462 = 0.138 in (0.55 D)
Internal shear area per inch Anπ × 20 × 0.250 × [0.025 + 0.57735 × 0.0325] = 0.687 in² per inch
J with Grade 5 (120 ksi) in 6061-T6 (45 ksi)(0.462 × 72) / (0.687 × 27) = 1.79
Minimum engagement in aluminum0.138 × 1.79 = 0.247 in, about 1.0 × D

The result lands on the rule of thumb machinists already use, one diameter of engagement for a steel bolt in aluminum, and shows where it comes from. The same bolt in a 4140 pre-hard housing needs only the 0.14 in equal-material value, and in Delrin the multiplier climbs past 8, which is why plastic parts get threaded inserts.

Threads in the Calculator

Basic major diameters and pitches per ASME B1.1 (unified inch) and ISO 261 / ASME B1.13M (metric). The calculator reads this table when the page loads.[3]

SeriesSizeTPI (inch) or pitch (mm)Major diameter (in or mm)
UNC#1-64640.0730
UNC#2-56560.0860
UNC#3-48480.0990
UNC#4-40400.1120
UNC#5-40400.1250
UNC#6-32320.1380
UNC#8-32320.1640
UNC#10-24240.1900
UNC#12-24240.2160
UNC1/4-20200.2500
UNC5/16-18180.3125
UNC3/8-16160.3750
UNC7/16-14140.4375
UNC1/2-13130.5000
UNC9/16-12120.5625
UNC5/8-11110.6250
UNC3/4-10100.7500
UNC7/8-990.8750
UNC1-881.0000
UNC1-1/8-771.1250
UNC1-1/4-771.2500
UNC1-1/2-661.5000
UNF#0-80800.0600
UNF#2-64640.0860
UNF#4-48480.1120
UNF#6-40400.1380
UNF#8-36360.1640
UNF#10-32320.1900
UNF#12-28280.2160
UNF1/4-28280.2500
UNF5/16-24240.3125
UNF3/8-24240.3750
UNF7/16-20200.4375
UNF1/2-20200.5000
UNF9/16-18180.5625
UNF5/8-18180.6250
UNF3/4-16160.7500
UNF7/8-14140.8750
UNF1-12121.0000
Metric coarseM2 × 0.40.42.0
Metric coarseM2.5 × 0.450.452.5
Metric coarseM3 × 0.50.53.0
Metric coarseM4 × 0.70.74.0
Metric coarseM5 × 0.80.85.0
Metric coarseM6 × 1.01.06.0
Metric coarseM8 × 1.251.258.0
Metric coarseM10 × 1.51.510.0
Metric coarseM12 × 1.751.7512.0
Metric coarseM14 × 2.02.014.0
Metric coarseM16 × 2.02.016.0
Metric coarseM20 × 2.52.520.0
Metric coarseM24 × 3.03.024.0
Metric fineM8 × 1.01.08.0
Metric fineM10 × 1.251.2510.0
Metric fineM12 × 1.251.2512.0
Metric fineM16 × 1.51.516.0
Metric fineM20 × 1.51.520.0

Material Strengths Used

Fastener strengths are the specification minimum tensile strengths; tapped-material strengths are the typical values stated in this library's material guides, so the calculator agrees with the articles. Shear strength is taken as 0.6 × tensile throughout.[4]

Bolt / external threadTensile strength (ksi)Basis
SAE Grade 2 steel74SAE J429, sizes to 3/4 in
SAE Grade 5 steel120SAE J429, sizes to 1 in
SAE Grade 8 steel150SAE J429
Alloy steel socket head cap screw170ASTM A574, sizes over 1/2 in (180 ksi up to 1/2 in)
18-8 / 304 stainless fastener100ASTM F593 condition CW, sizes to 5/8 in
Ti-6Al-4V fastener130Typical, see the titanium guide
Tapped / internal materialTensile strength (ksi)From
6061-T6 aluminum456061 vs 7075 vs 2024
7075-T7351 aluminum736061 vs 7075 vs 2024
2024-T351 aluminum706061 vs 7075 vs 2024
A36 steel58A36 vs 1018
1018 cold drawn steel64A36 vs 1018
1045 steel911018 vs 1045
4140 pre-hard (28–32 HRC)1304140 vs 4340 vs 4130
303 stainless90Stainless grades
304 stainless84Stainless grades
316 stainless84Stainless grades
17-4 PH H900190Stainless grades
Ti-6Al-4V130Titanium grades
CP titanium Grade 250Titanium grades
Delrin (acetal)10UHMW vs Delrin
UHMW polyethylene5.8UHMW vs Delrin
In plain terms
Drill for 75% thread unless the material argues otherwise, and tap deep enough that the bolt is the weak link. In steel that is about half a diameter of full thread; in aluminum, one diameter; in plastic, use an insert.

Tapped holes gaged, not guessed

C&W taps to the percent of thread the material wants, checks every tapped hole with go/no-go gages, and will flag a drawing whose thread depth cannot carry the fastener.

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Sources & References
[1]Machinery's Handbook, 31st ed., Tapping and Thread Cutting: tap drill formulas for a given percentage of thread (inch: major − 0.0130 × % / TPI) and the strength-versus-torque discussion behind the 75% default.
[2]Machinery's Handbook, 31st ed., Strength of Screw Threads: tensile stress area, shear areas of external and internal threads, length of engagement for equal and dissimilar materials (the J factor); FED-STD-H28/2B.
[3]ASME B1.1 Unified Inch Screw Threads (basic major diameters and pitches, thread height 0.6495 P and 1.0825 P relationships); ASME B1.13M / ISO 261 metric screw threads.
[4]SAE J429 (Grades 2, 5, 8 minimum tensile), ASTM A574 (alloy steel socket head cap screws), ASTM F593 (stainless steel fasteners). Tapped-material tensile values are the typical figures stated in the linked C&W material guides.