Mfg Part Number: AMS-QQ-A-200 5
Alternate P/N: AMSQQA2005
NSN : 9540-00-542-2691
NIIN : 005422691
CAGE Code : 81343
Manufacturer: Society Of Automotive Engineers Inc
Item Name : Beam Structural
Here at Internet For Aviation, we have AMS-QQ-A-200 5 Beam Structural from Society Of Automotive Engineers Inc, 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 AMS-QQ-A-200 5 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 Beam Structural and AMS-QQ-A-200 5 parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!
MRC | Criteria | Characteristic |
---|---|---|
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.312 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.312 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
BQJK | LEFT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
ZZZT | NONDEFINITIVE SPEC/STD DATA | H111 TEMPER |
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.312 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.250 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.250 INCHES NOMINAL |
BQJM | RIGHT SIDE TOP FLANGE TIP THICKNESS | 0.250 INCHES NOMINAL |
BQKH | ERR DEFAULT | ERR DEFAULT |
BQKH | LEG TIP THICKNESS | 0.250 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 1.290 POUNDS PER LINEAR FOOT |
HEAT | HEAT TREATMENT | H-111 STRAIN HARDENED |
MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/5, ALLOY 5086 |
MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/5, ALLOY 5086 |
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