Attachment 0016_MEO_P7003.pdf
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- Solicitation number
- W58RGZ-20-R-0074
About this file
This solicitation requests offers for the overhaul of rotor turbines for aircraft. The five-year IDIQ contract seeks a minimum of five and maximum of 414 overhauls annually, including 69 for foreign military sales. Offerors must overhaul at an approved source in accordance with DFARS 209.270-3 and Public Law 108-136. Currently, the only approved source is GE Engine Services. The solicitation will remain open until the closing date stated or receipt of sufficient funding and is issued by the Department of the Army Materiel Command Contracting Command at Redstone Arsenal. Products required include rotor turbines (NSN 2840-01-515-3538) with overhaul technical data in DMWR 1-2840-248-1/-2/-3/-4 and applicable MEOs. Delivery is FOB origin and pricing shall be firm fixed price.
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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 P 7003
Jun 6, 2019 2
Gas Generator Nozzle Segments, Cracks, Discoloration (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 1-2840-248-2 dtd 30 Sept 2014 TN 198622
MEC-P350210
DOCUMENT CHANGE IS REQUIRED Verification: Hands-On Table-Top None
To specify that no material fallout is allowed; To clarify crack inspection limits for ease of inspection;
To clarify allowance for deposits and discoloration.
BONHAM.ROBI
N.L.1229254100
Digitally signed by
BONHAM.ROBIN.L.12292541
Date: 2019.05.31 12:38:22 -05'00'
SCHNEIDER.EMI
LY.DON.1502474
Digitally signed by
SCHNEIDER.EMILY.DON.150
2474282 Date: 2019.05.31 12:36:22 -05'00'
Emily Schneider
VELAZQUEZ.MA
RK.A.1254578424
Digitally signed by
VELAZQUEZ.MARK.A.125457
Date: 2019.06.04 15:58:41 -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)
3-968
3-968, -969
3-973
3-980
3-310.a.
3-310
3-310.o.
(1), (2)
3-312.g.
CHANGE Usable Limits as follows: "Cracks which intersect are not allowed. Material in danger of fallling out (or has fallen out) is not allowed. Total cumulative length of all cracks will not exceed 1 inch."
REPLACE steps a(2) through d(3) as shown on page 2 of this MEO.
CHANGE Usable Limits for both to be "Not allowed."
ADD Note prior to step as follows:
"NOTE. Discoloration that is due to metal buildup or deposits, or hot gas corrosion, does not indicate coating loss. It is acceptable provided inspection limits (para 3-310 or 3-317) are met."
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
MED FORM 15-DEC-09 1401-R-E
AR 70-62 •11 May 2016 2
Inspect Usable Limits Max Repairable Limits Corrective Action .
a. Cracks in all areas: Cracks which intersect are not Not repairable. (1) Stage 1: Replace allowed. Material fallout, or in segment (para 3-621).
danger of falling out is not allowed.
Total cumulative length of all (2) Stage 2: Replace cracks will not exceed 1 inch. segment.
(1) Stage 1 vane Any number of cracks less Not repairable. Replace segment showerhead holes than 1/8 inch long. Each (para 3-621).
(fig. 3-276). crack must be contained within the showerhead holes.
(2) Stage 1 vanes One crack per vane between Not repairable. (1) Stage 1: Replace (except 3/8 and 1/4 inch long. Any segment (para 3-621).
showerhead holes) number less than 1/4 inch long and stage 2 vanes. provided total cumulative length of all (2) Stage 2: Replace cracks in all areas does not exceed 1 inch. segment.
(3) Areas other than Any number less than 1/4 inch long, Not repairable. (1) Stage 1: Replace vanes. provided total cumulative length of all segment (para 3-621).
cracks in all areas do not exceed 1 inch. (2) Stage 2: Replace segment
b. (6068T85G20 and Any amount allowed. Crazed. Same as usable Not applicable.
6068T85G21) Stage 1 coating cracks may intersect. limits.
vane convex surface, inner band, and outer band crazed coating cracks.
NOTE
Missing top coating may appear as discoloration, but there is still a diffusion layer that continues to provide protection.
c. Metal buildup, Clean to remove (table 3-8). Any amount if parent Blend to smooth deposits or After cleaning, any amount metal is undamaged. (para 3-503). Avoid discoloration. on vane is allowed provided it removing CODEP cannot be felt with a scriber having a 0.040 coating when blending.
inch tip radius and contour is not affected. Any amount on inner and outer bands provided it can be assembled normally with its mating parts.
NOTE
• Hot gas corrosion may appear as an area with blisters and blue or black discoloration.
It is not an indication of missing coating.
• There is a diffusion layer under the aluminide coating that continues to provide protection
d. Hot gas corrosion on aluminide coated flowpath surfaces:
(1) Discoloration. Any amount. Not applicable. Not applicable.
(2) Surface Any amount that does not Any amount, provided Repair aluminide roughness or penetrate into parent parent metal is not pitted coating (para 3-515).
blisters. metal. beyond 0.020 inch deep.
(3) Inner and outer Any amount of pits that do Any amount, provided Repair aluminide bands: not penetrate parent metal parent metal is not pitted coating (para 3-515).
more than 0.015 inch deep beyond 0.020 inch deep.
Through holes are not allowed.
MED FORM 17 JAN 2019
P 7003
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