EDR.pdf
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- Attached to
- C-5 Brake Hydraulic
- Solicitation number
- SPRHA1-27-R-0031
- Issued by
-
Defense Logistics Agency Aviation
About this file
This document is Engineering Data Requirements/Instructions (Attachment 'A') for the manufacture of a Brake Hydraulic component for C-5 Aircraft. The part number is 42252E220 with National Stock Number 1620-00-122-0474. The document was prepared by Joshua Auger of the 417 SCMS/GUEA office on 6 August 2014. Prior to contract award, contractors must certify in writing full compliance with all applicable manuals, specifications, and standards required for manufacturing this landing gear component. OO-ALC Landing Gear Engineering retains all rights to review and accept Material Review Board dispositions for discrepant items, with all major deviations (Class I changes) requiring procuring activity approval prior to shipment and minor deviations (Class II) requiring courtesy notification at shipment.
Marking and Unique Identification requirements mandate that each part receive a UID applied per MIL-STD-130 containing both human-readable information (HRI) and machine-readable information (MRI). The HRI must be applied via electro-chemical etching, dot peen, vibro peen, or micro-mill with mark depth between .003 and .005 inches and character height not exceeding .125 inches. The serial number format includes the vendor CAGE code, manufacture date in MMYY format, and a unique 4-digit sequential number beginning with 0001. A TESA tape label containing MRI per drawing 200827953 must be applied to the part, followed by two topcoats of polyurethane per MIL-PRF-85285, Type I, clear per FED-STD-595. Military specifications and standards will not be furnished in the bid set.
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Other files
| File | Type | Posted |
|---|---|---|
| SPRHA127R0031.pdf | ||
| SOW.pdf | ||
| EDL.pdf |
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Text version
REV:
ENGINEERING DATA REQUIREMENTS/INSTRUCTIONS
(ATTACHMENT ‘A’)
NOTE: MILITARY SPECIFICATIONS / STANDARDS WILL NOT BE FURNISHED IN THE BID SET.
1. THE FOLLOWING INSTRUCTIONS ARE FURNISHED FOR THE MANUFACTURE OF:
BRAKE HYDRAULIC (C-5 AIRCRAFT)
2. PART NUMBER:
42252E220
3. NATIONAL STOCK NUMBER:
1620-00-122-0474
PREPARED BY:
JOSHUA AUGER
OFFICE SYMBOL:
417 SCMS/GUEA
DATE:
6 AUGUST 2014
HILL AFB FORM 462 Page 1 of 1
4. THE FOLLOWING SPECIFICATIONS/STANDARDS, ETC. WILL BE USED IN LIEU OF THE DATA INDICATED. THE
SUPERSEEDED DATA WILL NOT BE FURNISHED UNLESS SO INDICATED.
5. MATERIAL REVIEW BOARD:
A. OO-ALC LANDING GEAR ENGINEERING RETAINS ALL RIGHTS TO REVIEW AND ACCEPT MATERIAL REVIEW BOARD (MRB’S) DISPOSITIONS OF DISCREPANT ITEMS. ALL DEVIATIONS, MINOR (CLASS II) AND MAJOR (CLASS I), FROM THE ENGINEERING DRAWING PACKAGE SHALL BE SUBMITTED TO THE PROCURING ACTIVITY. ALL MAJOR CHANGES SHALL REQUIRE APPROVAL OF THE PROCURING ACTIVITY PRIOR TO SHIPMENT. ALL MINOR CHANGES SHALL REQUIRE COURTESY COPY TO THE PROCURING ACTIVITY AT THE TIME OF SHIPMENT. THE PROCURING ACTIVITY SHALL HAVE FINAL AUTHORITY TO DETERMINE CHANGE CLASSIFICATIONS AS MAJOR/MINOR IF THERE IS A DISAGREEMENT WITH THE SUPPLIER ASSIGNED CLASSIFICATION. A MAJOR CHANGE IS DEFINED AS ANY CHANGE THAT MAY AFFECT THE FORM, FIT, OR FUNCTION OF THE COMPONENT OR ASSEMBLY. IF THE SUPPLIER OR DCMA INSPECTORS ARE UNSURE IF THE CHANGE SHOULD BE CLASSIFIED AS MAJOR/MINOR, THE
DEVIATION/WAIVER SHALL BE SUBMITTED TO THE PROCURING ACTIVITY FOR DISPOSITION.
B. PRIOR TO CONTRACT AWARD, THE CONTRACTOR SHALL CERTIFY TO THE GOVERNMENT IN WRITING FULL
COMPLIANCE WITH MANUALS, SPECIFICATIONS AND STANDARDS CALLED OUT AND REQUIRED FOR THE MANUFACTURE OF THIS CONTRACTED LANDING GEAR COMPONENT/ASSEMBLY. CONTRACTOR IS RESPONSIBLE TO COMPLETELY SEARCH THESE MANUALS, SPECIFICATIONS AND STANDARDS AND FULLY UNDERSTAND THE REQUIREMENTS NECESSARY TO MANUFACTURE LANDING GEAR COMPONENTS. ANY QUESTIONS CAN BE
FORWARDED TO OO-ALC LANDING GEAR ENGINEERING.
6. MARKING AND UNIQUE IDENTIFICATION (UID) TO MEET DRAWING REQUIREMENTS PER MIL-STD-130 IN LIEU OF
CONTRACTOR SPECIFICATION.
A. TESA TAPE LABEL APPLIED DIRECTLY TO PART AND HRI ETCHED DIRECTLY ON PART: UNIQUE IDENTIFICATION (UID) SHALL BE APPLIED TO EACH PART PER MIL-STD-130. THE UID SHALL CONTAIN HUMAN-READABLE INFORMATION (HRI) AND MACHINE-READABLE INFORMATION (MRI) MARKINGS. QUALITY AND TECHNICAL REQUIREMENTS FOR BOTH THE MRI AND HRI SHALL BE IN ACCORDANCE WITH SAE AS9132. THE METHOD OF MARKING FOR THE HRI SHALL BE LIMITED TO ELECTRO-CHEMICAL ETCHING, DOT PEEN, VIBRO PEEN, OR MICRO- MILL. THE DEPTH OF EACH MARK SHALL BE FROM .003 - .005 INCHES. THE HRI MARK SHALL INCLUDE BOTH THE PART NUMBER AND THE SERIAL NUMBER. THE SERIAL NUMBER WILL BE LIMITED TO 16 ALPHANUMERIC CHARACTERS INCLUDING THE VENDOR CAGE (FSCM) OF THE CONTRACTOR NAMED ON THE CONTRACT, DATE OF MANUFACTURE IN THE FORMAT MMYY, AND A UNIQUE 4-DIGIT NUMBER STARTING WITH 0001 IN NUMERICAL ORDER OF MANUFACTURE. THE HRI SHALL APPEAR AS “SN 9874701040001”. THE HEIGHT OF EACH ALPHANUMERIC CHARACTER IN THE HRI SHALL BE A MAXIMUM OF .125 INCHES. THE METHOD OF MARKING FOR THE MRI SHALL BE IN ACCORDANCE WITH DRAWING 200827953 (DASH NUMBER SHALL BE CHOSEN ACCORDING TO THE LARGEST LABEL THAT CAN BE APPLIED TO THE PART). APPLY TWO TOPCOATS POLYURETHANE OVER LABEL PER MIL-PRF-85285, TYPE I, CLEAR PER FED-STD-595.THE LOCATION OF THE UID SHALL BE CHOSEN AT THE DIGRESSION OF THE MANUFACTURER. TESA TAPE LABEL SHALL ONLY BE PLACED ON THE TOP COAT OF THE
PAINTED COMPONENTS.
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