Mfg Part Number: I18-1908
Alternate P/N: I181908
NSN : 2805-00-737-3513
NIIN : 007373513
CAGE Code : 71772
Manufacturer: Stanadyne Chicago Div
Item Name : Push Rod Engine Pop
Here at Internet For Aviation, we have I18-1908 Push Rod Engine Pop from Stanadyne Chicago Div, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific I18-1908 to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
Note : We Will Not Share Your Information To Any Third Parties.
We pride ourselves in our abilities to deliver quality superior grade aviation parts in a timely schedule. Thanks to the various supply chain locations that we have across the United States. We can execute fast shipping times that outpace our competitors. Unlike other competitors, we can promise same day shipping and delivery right to the very place you need. We’re leaders in our industry thanks to our parts streamlining process which includes quick stock and acquisition of the certified product and fast shipping. For whatever needs you have, be they Push Rod Engine Pop and I18-1908 parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2805-00-737-3513 Item Description: Push Rod Engine Pop | 2805 | 007373513 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | U | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| I18-1908 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AAZP | CHAMFER LENGTH | 0.281 INCHES NOMINAL SECOND END |
| ABHP | OVERALL LENGTH | 12.688 INCHES NOMINAL |
| ABPA | UNDERCUT DIAMETER | 0.370 INCHES MAXIMUM SECOND END |
| AJGE | BODY TYPE | TUBULAR |
| BNKG | END LARGEST DIAMETER | 0.382 INCHES MINIMUM AND 0.386 INCHES MAXIMUM FIRST END |
| BQSY | END HARDNESS RATING | 57.0 ROCKWELL C MINIMUM AND 63.0 ROCKWELL C MAXIMUM |
| BQTC | FLAT DIAMETER | 0.125 INCHES NOMINAL FIRST END |
| STYL | STYLE DESIGNATOR | CUP W/SHOULDER AND CHAMFER SECOND END |
| AATE | CHAMFER ANGLE IN DEG | 77.5 SECOND END |
| AAVK | SHOULDER LENGTH | 0.062 INCHES NOMINAL SECOND END |
| ABPC | UNDERCUT WIDTH | 0.109 INCHES MINIMUM FIRST END |
| ADAR | BODY OUTSIDE DIAMETER | 0.375 INCHES NOMINAL |
| AXMB | END LENGTH | 0.3085 INCHES MINIMUM AND 0.3165 INCHES MAXIMUM FIRST END |
| BQSZ | END CASEHARDENING INDICATOR | CASEHARDENED |
| BQTD | END SPHERICAL RADIUS | 0.1865 INCHES MINIMUM AND 0.1885 INCHES MAXIMUM SECOND END |
| BQTF | SPHERICAL RADIUS DEPTH | 0.209 INCHES NOMINAL SECOND END |
| MATL | MATERIAL | STEEL |
| MATT | MATERIAL | STEEL |
| ZZZV | FSC APPLICATION DATA | GASOLINE ENGINE,NONAIRCRAFT |
Semiconductor's Certifications and Memberships
 |
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”. |
We Hope that You'll Choose Buy Aviation Parts as Your Quick and Convenient Parts Distributor In the Future.
Request for Quote
