bug

Doing Business with Boeing
Approved Process Sources D1-4426
Revision: LM   Effective: 3/May/2021

 
Doing Business with Boeing Homespc
Closespc
Approved Process Sources D1-4426

d1-4426 Left Navigation
 

Document D1-4426 - Processes for BE10363421






Detail Information for Processor Code number: BE10363421
Supplier Name: AIRTECH SUPPLY INC
Address:3058 HWY 290,
City/town:HOT SPRINGS
Province/state:AR 71913-8610
Country:UNITED STATES
Area:AR
Contact Name:Mark Sorrell
Title: QA Mgr
Phone: 5015257707x102
Fax:

* An acronym in the "Nadcap Commodity" column only indicates that Nadcap accreditation may be required for this Process Code. It does not provide any indication of this company's actual Nadcap accreditation status.

Process Code *Nadcap
Commodity
Limitation Codes Doc Notes Nomenclature Specification
Number
002 AQS None . Boeing approved QMS as defined in D1-4426 Processor Requirements Sec 6.16.2 Quality System
111 HT None Does not include castings, forgings or rivets Heat Treat of Aluminum Alloys BAC 5602
113 HT None Limited to Solution (870-995 degrees F) and Age (225-375 degrees F) only. Heat Treat of Wrought Aluminum Alloys AMS 2770
151 HT H5 Limited to Hot Brake Forming Heat Treat of Titanium and Titanium Alloys BAC 5613
806 HT None . Temper Inspection of Non-ferrous Alloys (Conductivity Method including BAC 5651) BAC 5946
806A HT A3 None Hardness Testing BAC 5650
806B HT A3 None Hardness and Conductivity Inspection of Wrought Aluminum Alloy Parts (Hardness Testing) AMS 2658
806C HT A3 None Hardness and Conductivity Inspection of Wrought Aluminum Alloy Parts (Conductivity Testing) AMS 2658
L151 HT H5 Limited to Hot Brake Forming HT Titanium DPS6.33
L806A HT A3 None Eddy Current Conductivity Testing - Equipment & Procedures DPS1.05-8
L806B HT A3 None Hardness Testing of Metals DPS1.05
S111 HT None Limited to Solution (870-995 degrees F) and Age (225-375 degrees F) only. Heat Treating for Aluminum Alloys PS15500
S151 HT H5 Limited to Hot Brake Forming HT Titanium PS15800
S151A No Nadcap Commodity Code None None Stress Relief Procedure - Titanium Alloys PS15807
S806A HT A3 None Eddy Current Determination of Electrical Conductivity for Aluminum Alloys PS21207
S806B HT A3 None Hardness Testing of Parts and Materials PS21203
T111A HT None Limited to Solution (870-995 degrees F) and Age (225-375 degrees F) only. Aluminum Heat Treatment Procedures C17 DPS7.00-1-17
Untitled Document

Copyright ©2010 The Boeing Company - All rights reserved Security Agreement