Mfg Part Number: 709353
NSN : 2805-00-927-3322
NIIN : 009273322
CAGE Code : 34623
Manufacturer: Am General Llc
Item Name : Connecting Rod Pist
Here at Internet For Aviation, we have 709353 Connecting Rod Pist from Am General Llc, 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 709353 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 Connecting Rod Pist and 709353 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 |
---|---|---|---|---|---|---|
2805-00-927-3322 Item Description: Connecting Rod Pist | 2805 | 009273322 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
709353 | 5 | 9 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | FORGED AND MACHINED |
AETC | METALLIC HARDNESS RATING | 241.0 MINIMUM BRINELL TUNGSTEN CARBIDE AND 269.0 MAXIMUM BRINELL TUNGSTEN CARBIDE |
AXPW | END THICKNESS | 1.060 INCHES MINIMUM AND 1.070 INCHES MAXIMUM |
BQBP | END HOLE INSIDE DIAMETER | 0.860 INCHES NOMINAL |
BQBW | BEARING REPLACEABILITY | REPLACEABLE |
BQBZ | PISTON CONNECTING END LUBRICATION METHOD | SPLASH |
BQCB | SHAFT CONNECTING END BEARING | NOT INCLUDED |
BQCG | SHAFT CONNECTING END WIDTH | 3.252 INCHES MINIMUM AND 3.255 INCHES MAXIMUM |
BQCZ | SHAFT CONNECTING END LUBRICATION DRILL FEATURE | INCLUDED |
BRNG | CENTER TO CENTER EFFECTIVE LENGTH | 6.998 INCHES MINIMUM AND 7.002 INCHES MAXIMUM |
BRNJ | BODY WIDTH AT SHAFT CONNECTING END | 0.910 INCHES NOMINAL |
BRNK | BODY THICKNESS AT PISTON CONNECTING END | 0.562 INCHES NOMINAL |
FEAT | SPECIAL FEATURES | U/O CYLINDER NO. 2,4,AND 6 |
MATL | MATERIAL | STEEL FED-STD-66 AISI 1141 |
MATT | MATERIAL | STEEL FED-STD-66 AISI 1141 |
ZZZV | FSC APPLICATION DATA | ENGINE,GASOLINE,VEHICULAR |
AAGR | CROSS-SECTIONAL SHAPE STYLE | I-SECTION TYPE |
AKEU | SHAFT CONNECTING END STYLE | AUTOMOTIVE STANDARD SPLIT BEARING 2 BOLT |
BQBN | EDGE RADIUS | 0.670 INCHES NOMINAL |
BQBT | PISTON CONNECTING END BEARING | INCLUDED |
BQBY | PISTON CONNECTING END LUBRICATION DRILL FEATURE | INCLUDED |
BQCC | SHAFT CONNECTING END HOLE INSIDE DIAMETER | 2.187 INCHES NOMINAL |
BQCF | SHAFT CONNECTING END EDGE RADIUS | 1.688 INCHES NOMINAL |
BQCH | SHAFT CONNECTING END THICKNESS | 1.304 INCHES MINIMUM AND 1.306 INCHES MAXIMUM |
BQDB | SHAFT CONNECTING END LUBRICATION METHOD | SPLASH |
BRNH | BODY WIDTH AT PISTON CONNECTING END | 0.780 INCHES NOMINAL |
BRNL | BODY THICKNESS AT SHAFT CONNECTING END | 0.780 INCHES NOMINAL |
BXYS | PISTON END CONNECTION STYLE | SMALL ENGINE AND AUTOMOTIVE STANDARD |
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