Technical_Specifications_Amendment_0001.pdf
PDF 75 KB Posted
- Attached to
- Reamers Federal contract opportunity
- Solicitation number
- FA8126-15-Q-0106
About this file
Updated Technical Specifications for changed delivery date.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| FA8126-15-Q-0106-0001.doc | DOC document | |
| FA8126-15-Q-0106.doc | DOC document | |
| Technical_Specifications.pdf | ||
| Draft_Item_Description_FA8126-15-Q-0106.pdf | ||
| Draft_Technical_Criteria.pdf |
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Technical Specifications
To be technically acceptable the reamers and core drills, must meet these requirements:
1. Chucking reamers must have straight 6 flute with approximate ¼” pilot
2. Core drills must have twisted 4 flute with approximate ¼” to ½” pilot
3. Threaded reamers must be ¼” 28 thread
4. Flute hardness must be within of 65.5 – 67.5 RC
5. Shank hardness must be with 45 – 67.5 RC with the last 1 ½ inch 30 – 45 RC
6. All reamers and core drills with a chucking end/shank that measures over .500 will be turned down to .500 and have tri-flats added to accommodate mechanics drills
7. Must be delivered within 45 days or less after the contract is awarded
8. All reamers and core drills shall be made and manufactured in the USA and be made of cobalt steel material
All reamers and core drills shall be of the following requirements and sizes:
Piloted Threaded Reamers:
1. Reamers must be made of cobalt steel
2. Reamers must have ¼-28 threaded end
3. Overall length shall be approximately 2 1/8th inch
4. Pilots on all threaded reamers shall be approximately ¼ in length
5. Reamers must meet the following sizes and quantities:
Piloted Threaded Reamers CLIN FINAL CUT X PILOT Quantities
0001‐AA .153 X .140 150
0002‐AA .168 X .153 150
0003‐AA .184 X .168 150
0004‐AA .199 X .184 1000
0005‐AA .215 X .200 300
0006‐AA .247 X .231 300
0007‐AA .262 X .247 1000
0008‐AA .278 X .262 300
0009‐AA .325 X .309 500
0010‐AA .340 X .325 100
0011‐AA .387 X .372 150
0012‐AA .450 X .434 50
0013‐AA .512 X .497 50
Piloted Core Drills:
1. All piloted core drills must be made of cobalt steel
2. Any piloted core drill with the chucking end that measures over .500 inch diameter will have the chucking end turned down to .500 inch and have tri-flats added to accommodate mechanics drills.
3. Pilot lengths shall be between .250 inch on smaller core drills to .500 inch on larger core drills except where noted on chart below for special 2 inch long pilots
4. Overall lengths may vary between 5 inches on smaller core drills to 10 inches on larger core drills
Piloted Core Drills
CLIN FINAL CUT X PILOT Quantities
0014‐AA .156 X .127 100
0015‐AA .157 X .127 100
0016‐AA .168 X .098 100
0017‐AA .185 X .098 100
0018‐AA .187 X .098 250
0019‐AA .187 X .125 250
0020‐AA .187 X .156 200
0021‐AA .247 X .187 300
0022‐AA
.247 X .187 100
2" pilot
THIS CORE DRILL REQUIRES
A 2" LONG PILOT
0023‐AA .250 X .187 300
0024‐AA
.309 x .247 300
2" pilot
THIS CORE DRILL REQUIRES
A 2" LONG PILOT
0025‐AA .312 X .187 200
0026‐AA .312 X .250 200
0027‐AA .363 X .246 100
0028‐AA .372 X .309 100
0029‐AA .375 X .187 150
0030‐AA .375 X .250 200
0031‐AA .437 X .187 100
0032‐AA .437 X .250 100
0033‐AA .437 X .312 75
0034‐AA .437 X .375 75
0035‐AA .480 X .437 75
0036‐AA .500 X .187 200
0037‐AA .500 X .250 150
0038‐AA .500 X .312 150
0039‐AA .500 X .375 100
0040‐AA .562 X .250 50
0041‐AA .606 X .500 25
0042‐AA .750 X .500 25
0043‐AA .850 X .750 15
Chucking Reamers, Piloted/Non-Piloted:
1. All chucking reamers will be made of cobalt steel
2. Any chucking reamer with the chucking end diameter over .500 inch will have the chucking end turned down to .500 inch and have tri-flats added to accommodate mechanics drills
3. Overall lengths may vary from approximately 4 ½ inch to 7 inches
4. Pilot lengths may vary from approximately 3/16 inch to 5/16 inch
5. Cutting lengths may vary from approximately 1 ¼ inch to 2 ¼ inch.
6. All chucking reamers shall be piloted except as noted on the chart below
Chucking Reamers
CLIN FINAL CUT X PILOT Quantities
0044‐AA .153 X .140 100
0045‐AA .190 X .187 100
0046‐AA .199 X .184 1000
0047‐AA .203 X .187 100
0048‐AA .215 X .200 200
0049‐AA .231 X .215 100
0050‐AA .247 X .231 200
0051‐AA .250 X .247 100
0052‐AA .262 X .247 500
0053‐AA .266 X .247 100
0054‐AA .278 X .262 100
0055‐AA .309 X .293 100
0056‐AA .312 X .309 100
0057‐AA .325 X .309 500
0058‐AA .329 X .309 75
0059‐AA .421 X .406 75
0060‐AA .437 X .421 50
0061‐AA .450 X .434 50
0062‐AA .451 X .437 75
0063‐AA .453 X .437 100
0064‐AA .465 X .450 50
0065‐AA .500 X .484 50
0066‐AA .512 x .497 50
0067‐AA .514 x .493 50
0068‐AA .516 X .497 25
0069‐AA .518 X .512 25
0070‐AA .545 X .528 25
0071‐AA .563 X .559 25
0072‐AA .579 X .560 25
0073‐AA .593 X .578 25
0074‐AA .597 X .579 25
0075‐AA .606 X .590 25
0076‐AA .6094 X .5938 25
0077‐AA .622 X .606 25
0078‐AA .625 X .622 10
0079‐AA .636 X .622 25
0080‐AA .6406 X .625 25
0081‐AA .6562 X .6406 10
0082‐AA .6718 X .6562 10
0083‐AA .6875 X .6718 10
0084‐AA .7031 X .6875 10
0085‐AA .7188 X .7031 5
0086‐AA .7500 X .7344 10
0087‐AA .760 X .741 10
0088‐AA .762 X .747 10
0089‐AA .7656 X .7500 15
0090‐AA .787 X .775 5
0091‐AA .776 X .758 10
0092‐AA .787 X .775 5
0093‐AA .805 X .790 10
0094‐AA .820 X .809 10
0095‐AA .822 X .805 10
0096‐AA .8281 X .8125 10
0097‐AA .837 X .821 10
0098‐AA .854 X .837 10
0099‐AA .856 X .840 10
0100‐AA .8594 X .8438 10
0101‐AA .872 X .856 10
0102‐AA .874 X .858 10
0103‐AA .885 X .867 10
0104‐AA .887 X .872 10
0105‐AA .8906 X .8875 5
0106‐AA .894 X .858 20
0107‐AA .9062 X .8906 10
0108‐AA .921 X .912 5
0109‐AA .9218 X .9062 10
0110‐AA .9375 X .9218 5
0111‐AA 1.2656 5 NOT PILOTED
0112‐AA .3300 X .3144 20
0113‐AA 11/32 X .3281 20
0114‐AA .3460 X .3304 20
0115‐AA .3594 X .3437 20
0116‐AA .3610 X .3454 20
0117‐AA .3730 X .3574 20
0118‐AA .3895 X .3739 20
0119‐AA 25/64 X .3750 20
0120‐AA .3930 X .3774 20
0121‐AA .4045 X .3889 20
0122‐AA 13/32 X .3906 20
0123‐AA .4080 X .3924 20
0124‐AA .4200 X .4044 20
0125‐AA .4219 X .4062 10
0126‐AA .4240 X .4084 10
0127‐AA 7/16 X .4219 10
0128‐AA .4400 X .4244 10
0129‐AA .4515 X .4359 10
0130‐AA .4555 X .4399 10
0131‐AA 15/32 X .4531 10
0132‐AA .4715 X .4559 10
0133‐AA .4830 X .4674 10
0134‐AA 31/64 X .4687 10
0135‐AA .4865 X .4709 10
0136‐AA .4980 X .4824 10
0137‐AA 1/2 X .4843 10
0138‐AA .5025 X .4869 30
0139‐AA 17/32 X .5156 10
0140‐AA .5335 x .5156 10
0141‐AA .5450 X .5294 10
0142‐AA .5469 X .5312 10
0143‐AA .5495 X .5339 10
0144‐AA 1.2656 X 1.258 5
0145‐AA 1.020 12 NOT PILOTED
0146‐AA 1.2350 X 1.220 12
0147‐AA 1.2425 X 1.2350 12
0148‐AA 1.2495 X 1.2425 12
0149‐AA 1.2651 12 NOT PILOTED
0150‐AA 1.2812 12 NOT PILOTED
0151‐AA 1.2891 X 1.2807 12
0152‐AA 1.2969 X 1.2891 12
0153‐AA 1.3047 X 1.2969 12
0154‐AA 1.3157 X 1.3047 12
0155‐AA 1.3610 X 1.3460 12
0156‐AA 1.3680 X 1.3610 12
0157‐AA 1.3745 X 1.3680 12
0158‐AA 1.3828 X 1.3750 12
0159‐AA 1.3901 X 1.3828 12
0160‐AA 1.3906 12 NOT PILOTED
0161‐AA 1.4062 12 NOT PILOTED
0162‐AA 1.4140 X 1.4057 12
0163‐AA 1.4219 X 1.4140 12
0164‐AA 1.4297 X 1.4219 12
0165‐AA 1.4407 X 1.4297 12
0166‐AA 1.5630 6 NOT PILOTED
0167‐AA 1.5700 6 NOT PILOTED
0168‐AA 1.5800 6 NOT PILOTED
0169‐AA 1.5880 6 NOT PILOTED
0170‐AA 1.6000 6 NOT PILOTED
0171‐AA 1.6100 6 NOT PILOTED
0172‐AA 1.6170 6 NOT PILOTED
File details come from the government source that posted it. Updated .