Mfg Part Number: S122
NSN : 9540-00-146-0726
NIIN : 001460726
CAGE Code : 71379
Manufacturer: Cessna Aircraft Co
Item Name : Angle Structural
Here at Internet For Aviation, we have S122 Angle Structural from Cessna Aircraft Co, 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 S122 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.
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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 Angle Structural and S122 parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!
MRC | Criteria | Characteristic |
---|---|---|
STRUCTURAL | AARN | FABRICATION METHODEXTRUDED |
STRUCTURAL | ABKW | OVERALL HEIGHT0 625 INCHES NOMINAL |
STRUCTURAL | ABMK | OVERALL WIDTH1 000 INCHES NOMINAL |
STRUCTURAL | ABRY | LENGTH10 000 FEET MINIMUM AND 12 000 FEET MAXIMUM |
STRUCTURAL | ADXL | LEFT SIDE FLANGE THICKNESS0 062 INCHES NOMINAL |
STRUCTURAL | AGTA | BASIC SHAPE STYLEANGLE |
STRUCTURAL | AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0 031 INCHES NOMINAL |
STRUCTURAL | AJGP | BASE FLANGE THICKNESS0 062 INCHES NOMINAL |
STRUCTURAL | BRFD | WEIGHT PER UNIT MEASURE0 120 POUNDS PER LINEAR FOOT |
STRUCTURAL | CMZY | FIRST TIP STYLESQUARE END |
STRUCTURAL | CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL |
STRUCTURAL | CQHP | LEFT INSIDE ANGLE90 0 DEGREES NOMINAL |
STRUCTURAL | HEAT | HEAT TREATMENTT-3511 SOLUTION HEAT TREATED |
STRUCTURAL | MATT | MATERIALALUMINUM ALLOY 2024 |
STRUCTURAL | MDCL | MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-2003 FED SPEC 1ST MATERIAL RESPONSE |
STRUCTURAL | ZZZT | NONDEFINITIVE SPECSTD DATAT3511 TEMPER |
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