Attachment 0013_MEO_B3390A.pdf

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Solicitation for the Overhaul of the Rotor, Turbine Aircraft
Solicitation number
W58RGZ-20-R-0074
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About this file

This document contains a solicitation for the overhaul of rotor turbine aircraft. The contractor shall provide all labor, facilities, parts, materials, equipment, tools and data to overhaul rotor turbine aircraft assemblies. The assemblies include rotor turbine aircraft with national stock numbers 2840-01-515-3538 as both input and output. Estimated quantities to overhaul range from a minimum of five to a maximum of 414, including 69 for foreign military sales. The proposed contract is a five-year firm fixed price indefinite delivery indefinite quantity contract. Delivery is FOB origin. Overhaul must be performed by an approved source in accordance with defense regulations for aviation critical safety items, and currently the only approved source is GE Engine Services. Electronic proposals are authorized and should be submitted to the specified government email addresses by the estimated closing date. Award is subject to receipt of sufficient funding.

This document contains a solicitation for an overhaul contractor of rotor turbine aircraft assemblies. The contractor shall provide all resources to overhaul a minimum of five to a maximum of 414 rotor turbine aircraft assemblies, including 69 for foreign military sales, over five years using a firm fixed price IDIQ contract. Overhaul can only be performed by the currently approved source, GE Engine Services, in accordance with defense regulations for aviation critical safety items. Electronic proposals are due by the estimated closing date, with award contingent on funding.

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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 3390A

Apr 2, 2019 2

Blast Cleaning for Gas Generator Blades and Vanes, Clarification (T700, T401, T401C, T701C, T701D)

Administrative

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 1-2840-248-2 dtd 30 Sept 2014 TN 198733

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

Rev A: Clarify wording to Basic and correct formatting. Basic: To call out correct paragraph for GG blade grit blast, which includes requirement for heat tint inspection; To clarify that flow check of GG blades and vanes is needed after blasting, to ensure cooling holes are clear.

BONHAM.ROBI

N.L.1229254100

Digitally signed by

BONHAM.ROBIN.L.12292541

Date: 2019.04.01 16:18:42 -05'00'

SCHNEIDER.EMI

LY.DON.1502474

Digitally signed by

SCHNEIDER.EMILY.DON.150

2474282 Date: 2019.04.01 14:55:44 -05'00'

Emily Schneider

VELAZQUEZ.MA

RK.A.1254578424

Digitally signed by

VELAZQUEZ.MARK.A.125457

Date: 2019.04.01 17:15:07 -05'00'

Robin L. Bonham Mark A. Velazquez 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)

3-705

3-705

3-813

3-237.d

Table 3-8

Table 3-8

DELETE the following for "Blades, Gas Generator Turbine Rotor ...

Rene 125, Rene 108", in the Cleaning Paragraphs column: "3-199"

ADD the following for "Blades, Gas Generator Turbine Rotor ... Rene 125, Rene 108", in the Cleaning Paragraphs column: "3-238"

ADD the following to the end of step:

"For gas generator nozzle segments, check for plugged trailing edge cooling holes (Fig. 3-275) using water flow."

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 17 JAN 2019

CSI CC Affected? NO

MAINTENANCE ENGINEERING ORDER

(AMCOM Reg. 750-2) Continuation Sheet

MEO NO.

PAGE of

WP NO. PAGE

NO.

PARA-

GRAPH

FIGURE/

TABLE

NO.

CHANGES

(EXACT WORDING OF CHANGES MUST BE GIVEN)

MED FORM 15-DEC-09 1401-R-E

3-238.f ADD new step as follows:

"f. For gas generator nozzle segments, check for plugged cooling holes using water flow. For gas generator blades, check for plugged cooling-air holes using water-flow check (para 3-221). Clean holes if necessary using a suitable size wire or pin, and repeat flow check."

MED FORM 17 JAN 2019

AR 70-62 •11 May 2016

3-813

B 3390A

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