AMSC N/A FSC 5920
INCH-POUND
MIL-PRF-23419/12E
17 April 2012
SUPERSEDING
MIL-PRF-23419/12D
30 March 2006
PERFORMANCE SPECIFICATION SHEET
FUSES, INSTRUMENT TYPE, STYLE FM12
(SUBMINIATURE - HIGH PERFO RMANC E)
This specification is approved for use by all Departments
and Agencies of the Department of Defense.
The requirements for acquiring the product described herein
shall consist of this specification sheet and MIL-PRF-23419.
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for general information only.
3. Unless otherwise specified, tolerance is ±.01 (0.3 mm).
FIGURE 1. Style FM12 fuse (.026 inch diameter leads).
Inches
mm
.002
0.05
.010
0.25
.020
0.51
.025
0.64
.026
0.66
.050
1.27
.070
1.78
.145
3.68
.160
4.06
.270
6.86
.280
7.11
1.50
38.1
MIL-PRF-23419/12E
2
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for general information only.
3. Unless otherwise specified, tolerance is ±.01 (0.3 mm).
FIGURE 2. Style FM12 fuse (.051 inch diameter leads).
Inches
mm
.002
0.05
.010
0.25
.020
0.51
.032
0.81
.051
1.30
.083
2.11
.100
2.54
.200
5.08
.210
5.33
.380
9.65
.410
10.41
2.00
50.8
MIL-PRF-23419/12E
3
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for general information only.
3. Unless otherwise specified, tolerance is ±.01 (0.3 mm).
FIGURE 3. Style FM12 fuse (.064 inch diameter leads).
Inches
mm
.002
0.05
.010
0.25
.020
0.51
.032
0.81
.064
1.63
.085
2.16
.100
2.54
.200
5.08
.210
5.33
.380
9.65
.410
10.41
2.00
50.8
MIL-PRF-23419/12E
4
NOTES:
1. Dimensions are in inches.
2. The figures referenced indicate figure 1, 2, and 3 of the straight lead fuse.
3. “F” option fuses will be supplied with solder coated leads. Solder coating shall extend up the
leads to a point between the fuse stand-off and the lead egress point.
FIGURE 4. Style FM12 fuse (“F” option formed leads).
MIL-PRF-
23419/12
A
B
C
D
E
F
G
Figure
Min.
Max.
Min.
Max.
Min.
Max.
Min.
Max.
Min.
Max.
Min.
Max.
Min.
Max.
1
.145
.175
.024
.028
.120
.135
.480
.540
.260
.280
.255
.275
.130
.145
2
.190
.210
.049
.054
.120
.135
.610
.685
.360
.380
.395
.410
.190
.210
3
.190
.210
.063
.067
.120
.135
.610
.685
.360
.380
.395
.410
.190
.210
MIL-PRF-23419/12E
5
REQUIREMENTS:
Interface and physical dimensions: See table I and figures 1, 2, 3, or 4.
Case material: Polyphenylene sulfide (PPS) or equivalent.
Internal construction: The fuse element shall be a thick film material printed on a thermally insulated
substrate and sealed with a thick film arc suppressive glass.
Terminals:
Material: CDA-102 Copper.
Finish: Gold plate in accordance with SAE-AMS2422 and ASTM B488 ( Exc epti on to SAE-AMS2422:
The gold underplate shall consist of a minimum of 50 microinches of nickel). The Knoop Hardness
range shall be an ASTM code C.
Strength: Five pounds applying force axially to each fuse, and one pound of force applying three
bends to each terminal.
Outgassing: Material shall meet the outgassing requirements specified in MIL-PRF-23419.
Current rating: See table I.
Voltage rating: See table I.
Current carr ying capac it y: 100 percent at +25°C;110 percent at -55°C; 80 percent at +125°C. Current
carryi ng capacity is independent of vacuum conditions. The temperature of the case or terminals shall,
at no point, rise more than +85°C above the ambient air temperature. The maximum temperature rise
for 6.0, 7.5, 10, 15, and 20 ampere fuses shall be +120°C.
Resistance: See table I.
Overload interrupt: Interrupt time from -55°C through +125°C shall be as specified in table I. The
following exception shall apply for interrupt times at -55°C and 250 percent overload current:
a. Fuse ratings of 1.0 ampere and less shall open in 10 seconds maximum.
b. Fuse rating greater than 1.0 ampere shall open in 5 seconds maximum.
c. Fuse ratings less than 3/8 ampere shall open in 60 seconds maximum.
For group B, group C, and qualificati on insp ec tio ns, the power supp ly shall have an open-circuit voltage
of not less than that of the specified voltage rating of the fuse under test. Opening times (the interval
measured from the application of current to the time the current drops below the rating of the fuse) shall
be made with an oscillogram for periods shorter than 1 second.
Short circuit interrupt: 1,000 amperes at maximum voltage dc.
Maximum current clearing I2t: The maximu m current clearing I2t shall be in accordance with
MIL-PRF-23419 and shall be as specified in table I.
MIL-PRF-23419/12E
6
Vibration, high frequency: Fuses shall be tested in accordance with method 20 4 of MIL-STD-202. The
following details and exceptions shall apply:
a. Mounting: Fuses shall be mounted with their bodies restrained from movement, on an
appropriate mounting fixture.
b. Test level: Sinusoidal vibration from 5 to 3,000 hertz, 0.4 inch double amplitude or 30 g’s peak,
whichever is less. (Method 201 of MIL-STD-202 is not applicable).
c. Sweep rate: Approximately one-half octave per minute.
d. Test duration: 12 hours total (4 hours in each of three major axis).
e. Loading during testing: Rated dc current on 50 percent of fuse samples tested.
f. Measurements: DC resistance measurements shall be taken before and after the vibration
exposure.
Shock: In accordance with method I of MIL-PRF-23419, except test condition F. Fuses shall be
mounted by their normal mounting means, with their bodies restrained from movement, on an
appropriate mounting fixture.
Thermal shock: In accordance with MIL-PRF-23419, except test condition B shall apply.
Burn-in (168 hours): Fuses shall be mounted by their terminals in sockets. Spacing between each fuse
shall not be less than .250 inch (6.35 mm) or greater than 1.00 inch (25.4 mm). Fuses shall be
electrically connected to a constant dc source supplying rated current to each fuse. Initial voltage drop
measurements shall be taken after current has been applied for a minimum of 2 hours but not longer
than 4 hours. Current shall be applied for 168 +4, -0 hours while at room ambient conditions. Forced
air shall not flow over the fuses during the burn-in period. The voltage drop of each fuse shall be
measured after the burn-in period with the voltage drop change determined from measurements taken
before the thermal shock test. The voltage drop change for each fuse shall be less than ±10 percent.
Terminal strength: M eth od 211 of MIL-STD-202, test condition A (5 pounds pull) applying the force
axially to each wire individually, then test condition C (1 pound force) applying three bends to each wire
terminal. The DC resistance of each fuse shall be measured before and after testing in accordance
with MIL-PRF-23419. The change in resistance shall not exceed ±10 percent from the initial value.
Resistance to soldering heat: Method 210 of MIL-STD-202, test condition B. Depth of immersion to be
between .020 and .050 inch (0.51 and 1.27 mm) from the base for the fuse case. The DC resistance of
each fuse shall be measured before and after testing in accordance with MIL-PRF-23419. The change
in resistance shall not exceed ±10 percent from the initial value. The formation of solder balls in the
lead egress area shall not be considered reason for rejection.
MIL-PRF-23419/12E
7
Low temperature operation: Fuses shall be mounted by their terminals in sockets and placed in a low
temperature chamber. The chamber temperature shall be lowered gradually to -55°C +0°C, -3°C withi n
a period of 1 hour. After stabilizing at the low temperature for 1 hour, rated dc current shall be applied
to the fuses for a period of 4 +1, -0 hours while at the low temperature. The chamber shall then be
gradually raised to room temperature over a 4 hour period and maintained at room temperature for a
period of 8 hours minimum. After this time, the dc current shall be removed from the fuses and the
fuses removed from the chamber. The DC resistance of each fuse shall be measured before and after
testing in accordance with MIL-PRF-23419. The change in resistance shall not exceed ±10 percent
from the initial value.
Life (2,000 hours): Fuses shall be mounted by their terminals in sockets and mounted in a chamber at
+125°C +3 °C, -0°C ambient. The fuses shall be electrically connected to a dc source supply ing each
fuse with 64 percent of the +25°C rated value of current. The fuses shall remain in the chamber at
specified current for 2,000 ±8 hours. The electrical circuit shall provide a suitable indicator, which shall
be monitored daily during the length of the life test, to identify failure (blowing) of any fuse. The time of
failure shall be recorded to the nearest ±12 hours and the blown fuse replaced with a short circuit for
the remainder of the test. The DC resistance of each fuse shall be measured before and after testing
as specified in MIL-PRF-23419 and shall not have changed by more than ±10 percent.
Solderability: Fuses shall be tested in accordance with method 208 of MIL-STD-202. Gold plated leads
shall have the gold removed by single or double dipping into a flowing or nonflowing hot solder of
sufficient volume to assure complete gold removal.
Moisture resistance: Fuses shall be tested as specified in MIL-PRF-23419. The DC resistance of each
fuse shall be measured before and after testing and shall not have changed by more than ±15 percent.
Dielectric withs ta ndi ng volt age: Fuses shal l be tested in accor d anc e with method 301 of MIL-STD-202.
Fuses shall be mounted in a test fixture capable of exposing all major surfaces of the fuse body and the
leads to the test voltage. The test voltage shall be applied to the terminals electrically tied together and
to the test fixture. The following details shall apply:
a. Test voltage: 500 V rms.
b. Duration: 5 seconds for group A inspections.
60 seconds for qualification inspections.
c. Leakage current: 1 milliampere maximum.
d. Measurements: DC resistance of the fuse after the dielectric withstanding exposure in
accordanc e with MIL-PRF-23419.
This test shall become part of the group I test under qualification and group A inspections.
MIL-PRF-23419/12E
8
Thermal vacuum: Fuses shall be mounted in suitable mount sockets. The fuses shall then be placed in
a vacuum chamber and the chamber evacuated to a pressure of 5 x 10-5 torr maximum. The
temperature of the fuse mount shall be controlled such that the temperature of the fuses, as measured
with a thermocouple mounted on the fuse body, is maintained at +125°C ±3°C for a period of 48 +4, -0
hours, while 90 percent of the 25°C rated current is flowing through each fuse. At the end of the 48
hour exposure and while the fuses are at the test temperature and pressure, one-half of the samples
shall be given an overload interrupt test at 400 percent of their rated current. The fuses shall then be
removed from the chamber and the remaining fuses (not blown) measured for DC res ist ance as
specif ied in MIL-PRF-23419. The change in resistance shall not exceed ±10 percent of the initial value.
Quality conformance: With the exception of the overload characterization test and dielectric
withstanding voltage test, the following tests shall be conducted on 100 percent of the units, in the order
shown, and shall replace the group A tests referenced in MIL-PRF-23419. Nonconforming units shall
be removed from the lot. The lot shall be considered rejected if it exceeds the allowable PDA of 5
percent for the thermal shock and burn-in tests combined.
a. Precap inspection performed at 10X magnification as specified herein.
b. Visual and mechanical inspection; screen for the following defects:
(1) Cracks in the plastic molded housing (critical at lead egress area).
(2) Insufficient plastic fill (critical at lead egress area).
(3) Excessive plastic flash (part out of dimensional tolerance).
c. Thermal shock as specified herein.
d. Burn-in: 168 hours at rated current and ambient air at +25°C +3°C, -0°C.
e. DC resistance in accordance with MIL-PRF-23419.
f. Overload characterization: Each fuse lot shall be sampled to assure that overload interrupt
times shall fall within the limits as specified in table I. Each lot shall be truncated to form an
inspection lot based upon the final voltage drop as measured after the completion of burn-in.
The manufacturer shall subject samples selected from the extremes of the truncated population
to overload interrupt testing to ensure that overload interrupt times are as specified in table I. A
minimum of 20 fuses shall be selected from the extremes of the population and subjected to 250
percent, 400 percent, and 600 percent overload interrupt testing.
g. Radiogr a phic inspec t io n in acc ordanc e with method 209, MIL-STD-202, two views (0° and 90°).
Inspection criteria shall be as specified herein.
h. Visual and mechanical inspection in accordance with MIL-PRF-23419 at 10X magnification.
i. Dielectric withstanding voltage shall be performed as specified herein. A sample of fuses shall
be randomly selected in accordance with the zero defect sampling plan of MIL-PRF-23419
(group B column). If one or more defects are found, the lot shall be rejected.
Part or Identifying Number (PIN): The PIN shall be derived from table I. An example of a complete
PIN designation: FM12A72V1/2A.
MIL-PRF-23419/12E
9
Marking: Fuses shall be marked with the PIN desig nat ion in ac cor danc e wit h MIL-PRF-23419,
manufacturer’s name or logo, date code, and serialized label. Manufacturer’s lot may be marked
optionally. Marking ink color shall be white.
Current derating limits: The recommended derating limits for fuses covered in this specification sheet
are listed on figure 4 below. This figure relates current to case temperature, regardless of vacuum
conditions.
Precap inspection: Prior to molding, all fuses shall be visually inspected at 10X magnification for the
following def ec ts :
a. Obvious foreign inclusions or pits greater than .005 inch (0.13 mm) diameter in the arc
suppress ant glass sha ll be caus e for rej ect ion if they fall with in the dashe d lin e as indic at ed on
figure 5.
b. Parts shall be visually free of flux or other foreign material after cleaning.
c. Solder must make a continuous fillet between the silver termination pad and lead.
d. Voids, or the sum of voids in the solder fillet shall not exceed .015 inch (0.38 mm) in diameter.
e. A sample of five fuses shall be subjected to lead peel strength testing. Minimum acceptable
force as meas ur ed at lead pullou t sha ll be 250 grams.
FIGURE 5. Current derating limits.
MIL-PRF-23419/12E
10
FIGURE 6. Precap inspect ion.
MIL-PRF-23419/12E
11
Radiographic inspection: The radiographic examination shall include, but not be limited to, inspection
for loose or foreign particles, solder splash, excessive solder on leads, voids in molded material >.020
inch (0.51 mm) in diameter, any void at lead egress, adequate clearance between the alumina
substrate and the molded body and fractures or cracks in the alumina substrate or arc suppressant
glass. Figures 7 and 8 define accept and reject criteria.
a. Two views are required. View 1 shall show the plan view of the part. View 2 shall show a side
view of the part on an edge that does not contain external leads.
b. The sensitivity of the radiograph must be such that a lead particle .004 inch (0.10 mm) in
diameter shall be visible. Use of double emulsion film is optional.
NOTES:
1. Voids less than or equal to .020 inch (0.51 mm) diameter are acceptable provided th ey are not adjacent to
the arc suppressant glass.
2. Voids in the lead egress area which are less than or equal to 50 percent of the distance between
case bottom and the bottom of the alumina substrate are acceptable.
3. Scribe mark at the perimeter of the alumi na substrate are acceptable.
4. Pin holes less than or equal to .010 inch (0.25 mm) diameter in the arc suppressant gl ass are acceptable.
5. Foreign material less than or equal to .015 inch (0.38 mm) diameter between the terminals or bordering
edge of the alumina substrate are acce ptab le.
6. Solder fillets are defi ned as th at area along t he side of each t ermi nal and is not inclusive of the the sold ered
area immediately under the terminal. The "Solder Fillet Voids <= .015 Dia." shall apply to that portion of the
solder void that can be viewed in an area extending beyond the side of the terminal.
7. Solder voids found under the terminal shall not be cause for rejection if the s um of voids is less than 50% of
the solderable area under the terminal
FIGURE 7. Accept criteria (radiographic inspection).
MIL-PRF-23419/12E
12
NOTES:
1. Voids greater than .020 in ch (0.51 mm) dia met er are rejecta ble.
2. Voids in the lead egress area, which are greater than 50 percent of the distance between the case bottom
and the botto m of the alumin a sub strate, are rejectable.
3. Voids extending the full length between the terminals are rejectable.
4. Pin holes greater than .010 inch (0.25 mm) diameter in the arc suppressant glass are rejectable.
5. Foreign materi al gr eat er than .015 inch (0.38 mm) diameter between terminals or bordering edge of the
alumina substrate are rejectable.
6. Cracks in the alumina substrate are rejectable.
7. Cracks in the molded case are rejectable.
8. Solder fillets are defi ned as th at area along t he side of each t ermi nal and is not inclusive of the the sold ered
area immediately under the terminal. The "Solder Fillet Voids > .015 Dia." shall apply to that portion of the
solder void that can be viewed in an area extending beyond the side of the terminal.
9. Solder voids found under the terminal shall be cause for rejection if the sum of voids is exceeds 50% of the
solderable area under the terminal.
FIGURE 8. Reject criteria (radiographic inspection).
MIL-PRF-23419/12E
13
TABLE I. PIN designation identification.
PIN designation 1/ DC resistance
(ohms) 2/ Figure
(1, 2,
or 3)
Overload interrupt tim e
(seconds ) 3/ Maximum current cleari ng I
2
t
(ampere2 seconds) 4/
Style Charac-
teristic Maximum
voltage
(V dc)
Current
rating
(A)
Minimum Maximum 250%
nominal
rating
400%
nominal
rating
600%
nominal
rating
250%
nominal
rating
400%
nominal
rating
600%
nominal
rating
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
FM12
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
72V
72V
72V
72V
72V
72V
72V
72V
72V
72V
72V
72V
72V
72V
72V
125V
125V
125V
125V
125V
125V
125V
125V
125V
125V
125V
50V
1/8A
1/4A
3/8A
1/2A
3/4A
1A
1.5A
2.0A
3.0A
4.0A
5.0A
6.0A
7.5A
10A
15A
1/8A
1/4A
3/8A
1/2A
3/4A
1A
1.5A
2.0A
3.0A
4.0A
5.0A
20A
6.375
1.875
1.125
0.675
0.225
0.135
0.097
0.045
0.0262
0.0195
0.0135
0.0112
0.0082
0.0063
0.0038
6.375
1.875
1.125
0.675
0.225
0.090
0.0850
0.0450
0.0350
0.0300
0.0220
0.0025
10.625
3.125
1.875
1.125
0.375
0.225
0.163
0.075
0.0438
0.0325
0.0225
0.0188
0.0138
0.0107
0.0070
10.625
3.125
1.875
1.125
0.375
0.270
0.2250
0.1350
0.1050
0.0900
0.0680
0.0050
1
1
1
1
1
1
1
1
1
1
1
1
1
2
2
1
1
1
2
2
2
2
2
2
2
2
3
0-30.0
0-30.0
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
0-30.0
0-30.0
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
.01-.300
0-.015
0-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
.001-.015
0-.015
0-.015
.0005-.015
.0005-.015
.0005-.015
.0005-.015
.0005-.015
.0005-.015
.0005-.015
.0005-.015
.0005-.015
.001-.015
0-.003
0-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
.00015-.003
0-.003
0-.003
.00005-.003
.00005-.003
.00005-.003
.00005-.003
.00005-.003
.00005-.003
.00005-.003
.00005-.003
.00005-.003
.00015-.003
2.930
11.719
0.264
0.469
1.055
1.875
4.219
7.500
16.875
30.000
46.875
67.500
105.469
187.500
421.875
2.930
11.719
0.264
0.469
1.055
1.875
4.219
7.500
16.875
30.000
46.875
750.000
0.004
0.015
0.034
0.060
0.135
0.240
0.540
0.960
2.160
3.840
6.000
8.640
13.500
24.000
54.000
0.004
0.015
0.034
0.060
0.135
0.240
0.540
0.960
2.160
3.840
6.000
96.000
0.002
0.007
0.015
0.027
0.061
0.108
0.243
0.432
0.972
1.728
2.700
3.888
6.075
10.800
24.300
0.002
0.007
0.015
0.027
0.061
0.108
0.243
0.432
0.972
1.728
2.700
43.200
1/ Add “T” suffix to PIN designati on if optional sol der coated leads are required. Solder coating shall extend up the leads to a point between the fuse stand-off and the
lead egress point. Add “F” suffix to PIN designation if optional formed leads are required (see figure 4). Formed lead “F” suffix fuses are only supplied with solder
coated leads, theref ore “T” suffix should never be used with this “F” suffi x.
2/ DC resistance is measured with a test current of 0.1 to 10 milliamperes.
3/ Overloads interrupt times at -55°C and 250 percent overload current shall be as follows:
a. Fuse ratings of 1.0 ampere and less shall open in 10 seconds maximum.
b. Fuse ratings greater than 1. 0 ampere shall open in 5 seconds maximum .
c. Fuse ratings less than 3/8 ampere shall open in 60 seconds maximum.
4/ Maximum current clearing I2t at -55°C and 250 percent overload current m ay be greater than indic ated. To calculate maximum I2t at case temperat ure of -55°C and
250 percent overload current multiply the I2 product by the maximum blow times indicated in note 2/ above.
MIL-PRF-23419/12E
14
Group B inspection:
Inspection routine: Group B inspection shall be in accordance with MIL-PRF-23419, except the number
of samples shall be 20 and the inspections shall be as shown in table II. If the inspection lot exceeds
1,200 fuses, the zero defect sampling plan of MIL-PRF-23419 shall apply. Additional Group B testing
for option F fuses shall be performed after the standard Group A and Group B testing is completed, and
it shall be the same as Group B cited above, except that solderability testing will be conducted prior to
terminal strength testing and overload interrupt testing.
TABLE II Group B samples.
Inspection
Number of sample
fuses
Terminal strength
Overload int err upt at +25 °C
250% overload current
400% overload current
600% overload current
Solderability
ALL
12 of 20
4 of 20
4 of 20
ALL
Qualification inspection: Qualification inspection shall be in accordance with MIL-PRF-23419, except
the group II and group III inspections shall be as follows:
Group II inspection routine: Six samples shall be subjected to the group II inspection routine as
specified in table III. Maximum clearing I2t shall be measured when group II samples are subjected to
600 percent over lo ad int err upt tes ting.
TABLE III Group II samples.
Inspection
Number of sample
fuses
Group II
Terminal strength
Overload int err upt
250% at -55°C
250% at +125°C
400% at -55°C
400% at +125°C
600% at -55°C
600% at +125°C
Solderability
ALL
1 of 6
1 of 6
1 of 6
1 of 6
1 of 6
1 of 6
ALL
Group III inspection routine: Fourteen samples shall be subjected to the group III inspection routine as
specified in table IV. Group III samples shall be taken as indicated. DC resistance measurements shall
be taken before and after each test. DC resistance values for each fuse shall not change by more than
±10 percent.
MIL-PRF-23419/12E
15
TABLE IV. Group III samples.
Inspection Sample number. ‘X’ indicates test to be performed.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
Group III
Low temp. operation
Life (2,000 hours)
Overload int err upt
250% at +25°C
400% at +25°C
600% at +25°C
Thermal vacuum
Overload int err upt at 400%
Short circuit
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
Group C inspection: Group C inspection shall be in accordance with MIL-PRF-23419, except 16
samples shall be subjected to the subgroup I inspections as specified in table V. Maximum clearing I2t
for subgroups II and IV shall be performed at 600 percent of the +25°C rated current.
TABLE V. Subgroup I samples.
Inspection Sample number. ‘X’ indicates test to be performed.
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
Group I
Low temp. operation
Life (2,000 hours)
Overload interrupt
250% at +25°C
400% at +25°C
600% at +25°C
Short circuit
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
X
Referenced documents. In addition to MIL-PRF-23419, this document references the following:
MIL-STD-202 SAE-AMS2422 ASTM B488
The margins of this specification are marked with vertical lines to indicate where changes from the
previous issue were made. This was done as a convenience only and the Government assumes no
liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to
evaluate the requirements of this document based on the entire content irrespective of the marginal
notations and relationship to the last previous issue.
MIL-PRF-23419/12E
16
Custodians: Preparing activity:
Navy - EC DLA - CC
Air Force - 85
DLA - CC (Project 5920-2011-080)
NOTE: The activities listed above were interested in this document as of the date of this document.
Since organizations and responsibilities can change, you should verify the currency of the information
above using the ASSIST Online database at https://assist.daps.dla.mil.
