Attachment 0012_MEO_B3315.pdf

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Solicitation for the Overhaul of the Rotor, Turbine Aircraft
Solicitation number
W58RGZ-20-R-0074
Issued by

About this file

This document contains a federal contract opportunity solicitation for the overhaul of aircraft rotor turbines. The Army Materiel Command Contracting Command Redstone Arsenal is soliciting proposals for an indefinite delivery indefinite quantity contract with a minimum quantity of 5 turbines and maximum of 414 turbines over 5 years. The solicitation seeks overhaul of the Rotor, Turbine, Aircraft identified by national stock number 2840-01-515-3538. Offerors must be approved sources according to DFARS 209.270-3 and overhaul can only be performed according to technical data in Depot Maintenance Work Requirement 1-2840-248-1/-2/-3/-4 dated September 2014, Change #2 and applicable Maintenance Engineering Orders. Proposals are due by the estimated closing date in the solicitation, though the date may be adjusted. Award will be withheld pending receipt of sufficient funds.

The second document provides a Maintenance Engineering Order clarifying the depot life limit and reasons for scrapping gas generator blades for turbine aircraft that have operated on aged dampers due to excessive excitation force. It requests publication changes to reflect this information.

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Text version

MAINTENANCE ENGINEERING ORDER

(AMCOM Reg. 750-2)

MEO NO.

DATE PAGE 1 of

TITLE Tolerances Unless otherwise noted, dimensions are in inches and tolerances are:

Fractional ………………… ± 1/32 Decimal ………………... ± 0.010 Angular ………………… ± ½°

APPLICABILITY CSI Critical Characteristic Affected?

Impact Statement Attached?

REFERENCES FOR RDECOM USE ONLY

DOCUMENT(S) AFFECTED

PURPOSE OR PROBLEM

PROJECT ENGINEER ENGINEERING REVIEW ENGINEERING RELEASE

MED FORM 5-DEC-09 1401-R-E

AR 70-62 •11 May 2016 B 3315

Sep 5, 2018 1

GG Blades Depot Life Limit Clarification (T700, T401, T401C, T701C, T701D)

Technical

INTERIM USE OF THIS MEO IS AUTHORIZED

UNTIL AFFECTED DOCUMENT IS UPDATED.

MEO CHANGE TYPE

4) Normal - Can be implemented with normal priorityPRIORITY IMPLEMENTATION CATEGORY

T700 DAX

DMWR 1-2840-248-1 Dated 30 Sept 14 TTS 187877

DOCUMENT CHANGE IS REQUIRED Verification: Hands-On Table-Top None

To clarify DMWR information regarding Depot Life Limit for GG blades, and provide reason for the DLL. Blades that have operated on aged dampers are suspect of having had excessive excitation force, and so are to be scrapped.

PELTIER.JARED.

RYAN.152335277

Digitally signed by

PELTIER.JARED.RYAN.1523

352772 Date: 2018.08.28 12:05:00 -05'00'

BONHAM.ROBI

N.L.1229254100

Digitally signed by

BONHAM.ROBIN.L.12292541

Date: 2018.08.23 11:39:57 -05'00'

Robin Bonham

HORN.REINHOL

D.J.1087783495

Digitally signed by

HORN.REINHOLD.J.1087783

Date: 2018.08.31 08:49:39 -05'00'

Jared Peltier Reinhold Horn PUBLICATION CHANGE REQUEST: REQUEST THAT THE FOLLOWING DATA BE INCLUDED IN THE NEXT

CHANGE OR REVISION TO THE PUBLICATION IDENTIFIED ABOVE.

WP NO. PAGE

NO.

PARA-

GRAPH

FIGURE/

TABLE

NO.

CHANGES

(EXACT WORDING OF CHANGES MUST BE GIVEN)

3-376 3-4 CHANGE Note at bottom of the table to the following:

"****Gas generator blades are not time tracked. The Depot Life Limit for these is for the time since last overhaul of the gas generator rotor disk. Or, if the disk has not been overhauled yet, it is the time since new. Aged dampers are suspect of not providing adequate dampening, which then subjects the blades to excessive excitation force. The intention of the Depot Life Limit on the blades is to ensure that blades that have operated on aged dampers are scrapped."

Distribution Statement D:- Distribution authorized to Department of Defense and U.S. DoD contractors only to protect critical technology effective as of 26 June 2014. Other requests for this document must be referred to U.S. Army Aviation and Missile Research, Development and Engineering Center, ATTN: RDMR -AEM , Corpus Christi, TX 78419-5211

MED FORM 13 JAN 2017

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