AMS QQ A 250 4 O 0 050X12X48 by Sae Inc with NSN 9535-01-531-7060 Available Quote Now!

Mfg Part Number: AMS QQ A 250 4 O 0 050X12X48

Alternate P/N: AMSQQA2504O0050X12X48

CAGE Code : 0U583

Manufacturer: Sae Inc

FSC : FSC 9535 Plate Sheet Strip and Foil Nonferrous Base Metal

Here at Internet For Aviation, we have AMS QQ A 250 4 O 0 050X12X48 Sheet Metal from Sae 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 250 4 O 0 050X12X48 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 Sheet Metal and AMS QQ A 250 4 O 0 050X12X48 parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!

Cross Reference Parts List for NSN 9535015317060

AMS-QQ-A-250 4

AMS-QQ-A-250 4-CD0-0 05X12X48

Characteristics Data of NSN 9535-01-531-7060, 9535015317060

MRC	Criteria	Characteristic
ALBY	USAGE DESIGN	AIRCRAFT
MATL	MATERIAL	ALUMINUM ALLOY, QQ-A-250/4
AGTA	BASIC SHAPE STYLE	SOLID
AARN	FABRICATION METHOD	ROLLED
ABRY	LENGTH	48.000 INCHES NOMINAL
HEAT	HEAT TREATMENT	O-ANNEALED
ABGL	WIDTH	12.000 INCHES NOMINAL
ADVM	CROSS-SECTIONAL THICKNESS	0.0500 INCHES NOMINAL
AGAV	END ITEM IDENTIFICATION	FUSELAGE F4F JET AIRCRAFT
FEAT	SPECIAL FEATURES	MAXIMUM TENSILE STRENGTH 32000 POUNDS PER SQUARE INCH; MAXIMUM YIELD STRENGTH 14000 POUNDS PER SQUARE INCH
MATT	MATERIAL	ALUMINUM ALLOY 2024
MDCL	MATERIAL DOCUMENT AND CLASSIFICATION	QQ-A-250/4 FED SPEC 1ST MATERIAL RESPONSE

Corresponding National Stock Number to AMS QQ A 250 4 O 0 050X12X48

AMS-0	AMS-04	AMS-04	AMS-04
AMS-1	AMS-1-23053 3	AMS 1 23053 3	AMS 1 7444
AMS-1-7444	AMS-1000	AMS-1005	AMS 10133-2402
AMS 10134 0601	AMS 10134-0601	AMS 10134-1202	AMS 10134 1602
AMS 10134 1602	AMS 10134-1602	AMS 10134-1602	AMS 10134-1602
AMS 10134-1602	AMS 10134-2007	AMS 10134-2007	AMS 10134-2008