EDL.pdf

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Attached to
PISTON, LANDING GEAR (26-R-0103)
Solicitation number
SPRHA1-26-R-0103
Issued by

About this file

This is an Engineering Data List (EDL) for the C-130 Landing Gear piston assembly, dated November 21, 2023, and issued by the Ogden Air Logistics Center (CAGE Code 98747) under Air Force organization 429 SCMS/GUMACB. The document provides the engineering drawing requirements and reference materials necessary for the manufacture and procurement of the shock strut piston assembly for the main landing gear (MLG) of C-130 aircraft, identified by NSN 1620016766364LE and reference number 201612109-01.

The EDL specifies 11 engineering documents and drawings required for the component, including the primary shock strut piston assembly drawing (201612109), engineering orders, coating and grinding specifications for tungsten carbide application on high-strength steel, qualification requirements for high-velocity oxygen/fuel spraying, shock strut piston forging specifications (201612115), unique identification labeling requirements, and the landing gear requirements document with engineering notes (drawing 201416605). All documents are furnished with the solicitation (code "S"), with distribution codes ranging from "D" (initial distribution) to "A" (data not available). A critical note directs all supply chain personnel to reference Air Force drawing 201416605 for engineering notes, as the previously used Hill AFB Form 462 (Engineering Instructions) has been superseded and will not be provided for landing gear manufacture. Release of this technical data to foreign-owned, controlled, or influenced companies requires approval from the Foreign Disclosure Office.

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Text version

ENGINEERING DATA LIST

DATE:

21 NOV 2023

REVISION: 1 *HISTORY*

CAGE:

98747

PAGE:

NSN:

1620016766364LE

DATA TECH:

Williamson, Tiffany

END ITEM:

C-130 LANDING GEAR

ORGANIZATION/OFFICE SYMBOL:

429 SCMS GUMACB/

MANUFACTURER NAME:

OGDEN AIR LOGISTICS CENTER

REFERENCE NUMBER:

201612109-01

NOUN:

PISTON,LANDING GEAR

LINE/

SUB CAGE

ENG DRAWING NUM/ ACCOMP

DOC NUM REV

NR

SHEETS

FURN

CODE

DIST

CODE NOUN REMARKS

L 98747 201612109 S D SHOCK STRUT PISTON ASSY,

MLG

S 98747 2602 S D ENGINEERING ORDER

L 98747 200310641 H S A COATINGS, TUNGSTEN

CARBIDE ON HIGH STRENGTH

STEEL

L 98747 200310642 B S A GRINDING, HIGH VELOCITY

OXYGEN/FUEL SPRAYED

TUNGST

S 98747 10A0193-H S A ENGINEERING ORDER

S 98747 15A7106-H S A ENGINEERING ORDER

L 98747 200925098 N S A QUALIFICATION

REQUIREMENTS FOR HIGH

VELOCITY OXYGE

L 98747 201612115 S D SHOCK STRUT PISTON

FORGING, MLG

S 98747 2602 S D ENGINEERING ORDER

L 98747 200827953 A S D LABEL, UNIQUE

IDENTIFICATION (UID),

LANDING GEAR

L 98747 201416605 E S D LANDING GEAR

REQUIREMENTS DOC.

(ENGINEERING NOTES)

STANDARD ENGINEERING TEXT

Williamson, Tiffany 21 NOV 2023

RELEASE OF THIS DATA TO A FOREIGN OWNED, CONTROLLED OR INFLUENCED COMPANY IS DEPENDENT UPON THE APPROVAL OF THE FOREIGN DISCLOSURE OFFICE.

NOTE TO ALL SUPPLY CHAIN PERSONNEL: THE ENGINEERING NOTES ARE PROVIDED ON AIR FORCE DRAWING 201416605, CAGE CODE 98747. THE ENGINEERING INSTRUCTIONS (HILL AFB FORM 462) ARE NO LONGER UTILIZED FOR LANDING GEAR AND WILL NOT BE PROVIDED. ALL PREVIOUS LANDING GEAR VERSIONS OF THE ENGINEERING INSTRUCTIONS (HILL AFB FORM 462) FOR THIS NATIONAL STOCK NUMBER (NSN) HAVE BEEN SUPERSEDED AND WILL NOT BE UTILIZED FOR THE MANUFACTURE OF THIS COMPONENT/ASSEMBLY.

NAME: DATE:

C - CLASSIFIED DOCUMENT.

S - FURNISHED WITH SOLICITATION.

M - STABLE BASE DRAWING REQUIRED; FURNISHED WITH

CONTRACT AWARD.

X - DATA SUPPLIED (NOT IN JEDMICS).

R - FURNISHED BY PCO UPON REQUEST.

P - PARTIAL DOCUMENT FURNISHED.

V - VENDOR DRAWING; (NOT PROVIDED).

G - GOV'T DOCUMENT.

O - OTHERS, CONTRACTOR MUST ACQUIRE.

A- DATA NOT AVAILABLE.

FURNISHED METHOD CODE LEGEND:

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