SPE4A219R0055 A0002 (issued 7Feb20).pdf

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Attached to
F108 Workload Augmentation Federal contract opportunity
Solicitation number
SPE4A219R0055
Issued by
Defense Logistics Agency Aviation

About this file

This amendment to the solicitation modifies requirements for a federal contract to provide workload augmentation for F108 engine remanufacturing. Key changes include extending the proposal due date from February 21, 2020 to April 10, 2020. The FOB point is revised from Destination to Origin. Additional technical orders are added to the scope, and some are removed. The Defense Logistics Agency Aviation is seeking these services to support its engine remanufacturing work.

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Appendix F - CEMS Input Forms.xls XLS spreadsheet
SPE4A219R0055 A0003 (issued 16Mar20).pdf PDF
SPE4A219R0055 (issued 22Nov19).pdf PDF

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Offers must acknowledge receipt of this amendment prior to the hour and date specified in the solicitation or as amended, by one of the following methods:

(a) By completing items 8 and 15, and returning or (c) By separate letter or electronic communication which includes a reference to the solicitation and amendment numbers. FAILURE OF YOUR ACKNOWLEDGMENT TO BE RECEIVED AT THE PLACE DESIGNATED FOR THE RECEIPT OF OFFERS PRIOR TO THE HOUR AND DATE SPECIFIED MAY RESULT IN REJECTION OF YOUR OFFER. If by virtue of this amendment you desire to change an offer already submitted, such change may be made by letter or electronic communication, provided each letter or electronic communication makes reference to the solicitation and this amendment, and is received prior to the opening hour and date specified.

E. IMPORTANT: Contractor is not is required to sign this document and return copies to the issuing office.

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT 1. CONTRACT ID CODE

2. AMENDMENT/MODIFICATION NUMBER 3. EFFECTIVE DATE 4. REQUISITION/PURCHASE REQUISITION NUMBER 5. PROJECT NUMBER (If applicable)

7. ADMINISTERED BY (If other than Item 6) CODE

STANDARD FORM 30 (REV. 11/2016)

Prescribed by GSA FAR (48 CFR) 53.243

FACILITY CODE

9A. AMENDMENT OF SOLICITATION NUMBER

9B. DATED (SEE ITEM 11)

10A. MODIFICATION OF CONTRACT/ORDER NUMBER

10B. DATED (SEE ITEM 13)

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

The above numbered solicitation is amended as set forth in Item 14. The hour and date specified for receipt of Offers is extended. is not extended.

12. ACCOUNTING AND APPROPRIATION DATA (If required) copies of the amendment; (b) By acknowledging receipt of this amendment on each copy of the offer submitted;

13. THIS ITEM APPLIES ONLY TO MODIFICATIONS OF CONTRACTS/ORDERS.

IT MODIFIES THE CONTRACT/ORDER NUMBER AS DESCRIBED IN ITEM 14.

CHECK ONE A. THIS CHANGE ORDER IS ISSUED PURSUANT TO: (Specify authority) THE CHANGES SET FORTH IN ITEM 14 ARE MADE IN THE CONTRACT ORDER

NUMBER IN ITEM 10A.

B. THE ABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (such as changes in paying office, appropriation data, etc.) SET FORTH IN ITEM 14, PURSUANT TO THE AUTHORITY OF FAR 43.103(b).

C. THIS SUPPLEMENTAL AGREEMENT IS ENTERED INTO PURSUANT TO AUTHORITY OF:

D. OTHER (Specify type of modification and authority)

Except as provided herein, all terms and conditions of the document referenced in Item 9A or 10A, as heretofore changed, remains unchanged and in full force and effect.

15C. DATE SIGNED

15A. NAME AND TITLE OF SIGNER (Type or print)

16C. DATE SIGNED

16A. NAME AND TITLE OF CONTRACTING OFFICER (Type or print)

14. DESCRIPTION OF AMENDMENT/MODIFICATION (Organized by UCF section headings, including solicitation/contract subject matter where feasible.)

PAGE OF PAGES

6. ISSUED BY CODE

8. NAME AND ADDRESS OF CONTRACTOR (Number, street, county, State and ZIP Code) (X)

CODE

15B. CONTRACTOR/OFFEROR

(Signature of person authorized to sign)

16B. UNITED STATES OF AMERICA

(Signature of Contracting Officer)

Previous edition unusable

A0002

SPE4A2

DLA AVIATION RICHMOND

8000 JEFFERSON DAVID HIGHWAY

RICHMOND, VA 23297

INITIATOR: INGRID SMITH, INGRID.SMITH@DLA.MIL

F108 Workload Augmentation

SPE4A219R0055

1 10

02/07/2020

11/22/2019

CONTINUATION SHEET REFERENCE NO. OF DOCUMENT BEING CONTINUED

SPE4A2-19-R-0055 Amendment 0002

Page

NAME OF OFFEROR OR CONTRACTOR

50336-101 NSN 7540-01-152-8067

US GOVERNMENT PRINTING OFFICE 1990-262-081

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

Amendment 0002 is issued to clarify, change or add the subject RFP requirements, summarized as follows:

Extends the proposal due date at Section 9 of the RFP SF-33

Section A

A.3: Changes the FOB point from Destination to Origin.

Section I

Deletes FAR 52.247-48 Adds FAR 52.247-29

Section L

L.7.1: Corrects the number of volumes subject to proposal submission.

Appendix B

Corrects reference from Main Fuel Control to Main Engine Control (MEC) Removes the following Technical Orders from the requirement as no longer applicable or included in error at RFP:

o 00-20-5 o 00-20K-1 o 00-25-254-2 o 35E20-3-1-103

Adds the following TOs to the requirement that were omitted in error at time of RFP issuance:

o 2J-F108-534 o 2J-F108-537 o 2J-F108-539C o 2J-F108-540 o 2J-F108-550 o 2J-F108-552 o 2J-F108-554 o 2J-F108-567E

The aforementioned RFP section paragraphs and Appendix B are replaced as shown on pages 3 – 10 herein.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

Block 9 of the RFP SF-33 is hereby amended to reflect an extended proposal response date, FROM: 1500 local time 2/21/2020 TO: 1500 local time 4/10/2020.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

Section A

A.3 FOB Point

Ready for issue remanufactured engines shall be subject to FOB Origin terms.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

Section I

Deletes:

FAR 52.247-48 FOB DESTINATION – EVIDENCE OF SHIPMENT (FEB 1999)

Adds:

FAR 52.247-29 FOB ORIGIN (FEB 2006)

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

Section L

L.7.1 Written proposals shall be submitted in three (3) volumes in loose-leaf binders as outlined below. Offerors shall attach a binder cover sheet to the outer cover of each volume, which clearly identifies each volume by number, name, and copy number (i.e., Volume 1, Past Performance, copy 2 of 3), solicitation number, date of submission, and the offeror's name. This information shall also be placed on the edge of the binder where it can be seen when placed in a vertical position in a storage cabinet.

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

Appendix B

Applicable Technical Orders

NOTE

Basic T.O. dates in this APPENDIX are current as of the date of this SOW and in accordance with Amendment 0002 herein. The SOR at the facility where work under provision of this specification is accomplished shall control and maintain all technical orders and other technical directives, manuals and associated documents applicable to the work requirements, in an updated and current status. The SOR shall accomplish a timely review of revisions and directives applicable to the work requirements for this specification. The review shall consider the impact on work requirements, cost, schedules and any other pertinent factors. Written evaluation, along with specific back-up data for those changes which impact the performance of the specification shall be provided to PCO within ten working days after receipt. The SOR shall incorporate all authorized technical orders and subsequently negotiate impact on cost or schedules with PCO.

NUMBER SECTIONS/CHAPTERS/PAGE TITLE

00‐5‐1 15‐Feb‐19 Air Force T.O. System

00‐5‐3 15‐Feb‐19 T.O. Distribution System

00‐5‐15 29‐Sep‐17 TCTO Process

00‐20‐1 1‐Jun‐18 Preventative Maintenance Program

00‐20‐2 15‐Mar‐16 Maintenance Data Collection

00‐20‐3 10‐Jul‐17 Maintenance Procedures of Reparable Property

00‐25‐113 15‐Dec‐16 Conservation and Segregation of Critical Alloy and Precious Metal Bearing Parts and Scrap

00‐25‐113‐F108 15‐Dec‐16 Critical Material Parts

00‐25‐195 1‐Oct‐12 Source, Maint, and Recover Coding

00‐25‐254‐1 15‐Aug‐18 D042 User Manual CEMS

00‐25‐257 15‐Oct‐07 Engine Trending and Diagnostics User's Manual

00‐25‐257‐7‐CD‐

1 15‐Apr‐16

Engine Trending and Analysis User's Manual for Turbofan Engine Model F108‐100/201

00‐35D‐54 1‐Sep‐15 Deficiency Reporting

00‐85‐20 1‐Feb‐18 Engine Shipping Inst

1C‐135(K)R‐1‐1 30‐May‐85 Flight Manual

1C‐135(K)R‐10 1‐Jul‐17 Buildup Instruction Aircraft Power Package

1C‐135‐6 15‐Jun‐15 Aircraft Maintenance Work Unit Code Manual

2‐‐1‐‐11 31‐Oct‐84 Corrosion Control of Engine Parts During Overhaul

2‐‐1‐‐16 30‐Aug‐03 Reident by S/N of Acft Engines

2J‐1‐13 15‐Jun‐30 Cleaning of Gas Turb Acft Engs & Parts

2J‐1‐18 15‐Oct‐18 Preparation for Shipment and Storage of Gas Turbine Engs

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

2J‐1‐19 1‐Jul‐03 Insp& Disposition of Gas Turb Eng After Accident or Engine Dropped During Handling

2J‐1‐24 15‐Jan‐18 Comprising Complete Basic Gas Turbine Engine

2J‐1‐F108 15‐Dec‐16 Warranty Implementation Manual TurboFan Engine F108‐CF‐100

2J‐F108‐05‐11 24‐May‐94 F108CF100 Engine Life Limits

2J‐F108‐1 1‐Jan‐17 Specific Operating Instructions

2J‐F108‐2‐1 15‐Oct‐18 Maintenance Manual

2J‐F108‐2‐2 1‐Feb‐19 Standard Practices Manual

2J‐F108‐2‐3 1‐Jan‐17 Consumable Products Manual

2J‐F108‐13‐1 1‐Jan‐17 Engine Shop Manual

2J‐F108‐13‐2 1‐Jan‐17 Service Bulletin List

2J‐F108‐13‐2‐1 1‐Jan‐17 Service Bulletin, Depot

2J‐F108‐13‐05‐11 1‐Jan‐17 Engine Time Limits

2J‐F108‐13‐72‐00 1‐Apr‐18 Engine Assembly

2J‐F108‐13‐72‐09 1‐Jan‐17 General Procedures

2J‐F108‐13‐72‐21 1‐Feb‐17 Fan and Booster Assembly

2J‐F108‐13‐72‐22 1‐Mar‐18 Number 1 and 2 Bearing

2J‐F108‐13‐72‐23 1‐Apr‐18 Fan Frame Assembly

2J‐F108‐13‐72‐31 1‐May‐19 Compressor Rotor Assembly

2J‐F108‐13‐72‐32 1‐Aug‐18 Compressor Front Stator Assembly

2J‐F108‐13‐72‐33 1‐Jan‐17 Compressor Rear Stator Assembly

2J‐F108‐13‐72‐41 15‐Aug‐18 Combustion Case Assembly

2J‐F108‐13‐72‐42 1‐Jan‐17 Combustion Chamber

2J‐F108‐13‐72‐51 1‐Jan‐17 High Pressure Turbine Assembly

2J‐F108‐13‐72‐52 1‐Jan‐17 High Pressure Turbine Rotor Assembly

2J‐F108‐13‐72‐53 15‐Mar‐17 High Pressure Turbine Shroud and Stage one Low Pressure Turbine Nozzle Assy

2J‐F108‐13‐72‐54 1‐Jan‐17 Low Pressure Turbine Rotor

2J‐F108‐13‐72‐55 1‐Jan‐17 Low Pressure Turbine Shaft Assembly

2J‐F108‐13‐72‐56 1‐Jan‐17 Turbine Frame Assembly

2J‐F108‐13‐72‐61 1‐Jan‐17 Inlet Gearbox and No. 3 Bearing Assembly

2J‐F108‐13‐72‐62 1‐Jan‐17 Transfer Gearbox Assembly

2F‐F108‐13‐72‐ 63 1‐Jan‐17 Accessory Gearbox Assembly

2J‐F108‐14 15‐Nov‐18 Illustrated Parts Catalog

2J‐F108‐19 1‐Jan‐17 Non‐Destructive Test Manual

2J‐F108‐534 15‐Sep‐93 Modification of Combustor Assembly

2J‐F108‐537 27‐Oct‐99 Removal of Stage One Compressor Blades which Experienced Operational Instability

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

2J‐F108‐539C 15‐Apr‐20

Recalibration of IGV Rigging ‐ 3 Degree Closure (Note: Supplement 539E changed this TCTO to a depot level TCTO)

2J‐F108‐540 8‐Mar‐93 No. 3 Bearing Improvement Program

2J‐F108‐550 1‐Oct‐97 Inspection of Fan Disk

2J‐F108‐552 1‐Oct‐97 Immersion Ultra‐Sonic/Eddy Current Inspection of Fan Disk

2J‐F108‐554 1‐Jun‐98 Replacement of Combustion Chamber Assemblies with Small Tip Fuel Nozzles and Swirlers

2J‐F108‐567E 1‐Jul‐15 Inspection of Variable Bleed Valve Actuators for F108‐CF‐100 Series Engines

2JA3‐63‐4 15‐Aug‐18 Engine Starter 36E153‐6E

2JA11‐5‐3‐WA‐1 15‐Oct‐14 Alternator Electrical Lead Assembly

2JA11‐6‐3‐WA‐1 15‐Oct‐14 T495 Wiring Harness

2JA11‐7‐3‐WA‐1 15‐Oct‐14 Control Parameter Wiring Harness

2JA12‐12‐13 1‐Dec‐04 Turbine Clearance Control Valve

5E6‐3‐116‐3‐1 15 Feb 16 (Section 1‐10008) CIT Sensor

5E6‐3‐124‐2‐WA‐

1 15‐Oct‐14

Component Maint Manual, T12 Temperature Sensor P/N 154BY (301‐771‐601‐0) 73‐21‐41

5E6‐3‐125‐2‐WA‐

1 15‐Oct‐14

Component Maint Manual, T12 Temperature Sensor P/N RP211‐00 (301‐798‐601‐0) (CFMI‐TP‐

CM 421)

6J3‐4‐113‐3‐WA‐

1 15 Nov 16 (Section 1‐8) Main Engine Control

6J3‐4‐113‐4‐WA‐

1 1‐Jan‐17 Main Engine Control, IPB

6J3‐8‐20‐23‐WA‐

1 1‐Aug‐16 Bleed Valve Fuel Gear Motor

6J8‐37‐13 01 Apr 18 (Section 1‐10058) Fuel Nozzle (Parker)

6J8‐47‐3 1‐May‐18 Fuel Nozzle (Woodward FST)

6J10‐4‐89‐13 1‐Dec‐16 Fuel Pump

6J15‐20‐5‐13 30‐Nov‐96 Bleed Valve Stop Mechanism

6J24‐10‐13 1‐Aug‐18 Servo‐Fuel Heater

7J1‐85‐13 31‐Aug‐86 Oil/Fuel Heat Exchanger

7J4‐2‐59‐13 28‐Feb‐81 Lubrication Unit

7J10‐21‐13 30‐Sep‐16 Oil Tank

7J11‐3‐3 29‐Feb‐96 Oil Indicator Cap

8A6‐2‐8‐3‐WA‐1 01 Jun 18 (Section 1‐16002) Permanent Magnet Alternator

8D21‐6‐13‐WA‐1 1‐Jun‐18 N1 Speed Sensor

8D21‐10‐3 31 Oct 97 (Section 1‐1004) No. 1 Bearing Vibe Sensor Endevco

8D21‐11‐3 01 Jun 09 (Section 1‐1008) No. 1 Bearing Vibe Sensor Vibro‐Meter

OPTIONAL FORM 336 (4-86)

Sponsored by GSA

FAR (48 CFR) 53.110

8E1‐7‐14‐3 31 May 14 (Section 1‐1006) Ignition Lead Assemblies

8E1‐8‐31‐13 31 Jul 14 (Section 1‐16002) Ignition Exciter, Unison

9H2‐7‐39‐13 15 Jun 17 (Section 1‐1006) Variable Stator Actuator

9H2‐7‐51‐3 15‐Jun‐17 Ballscrew Actuator

16R1‐2‐27‐3 10‐Jun‐05 Variable Stator Feedback Cable

16R1‐2‐33‐3 30‐Nov‐87 Variable Bleed Valve Feedback Cable

33‐1‐37‐1 15‐Sep‐14 Joint Oil Analysis Program Laboratory Manual

33‐1‐37‐2 1‐Jun‐15 Joint Oil Analysis Program Laboratory Manual

33‐1‐37‐3 30‐Apr‐18 Joint Oil Analysis Program Laboratory Manual

33‐1‐37‐4 30‐Aug‐13 Joint Oil Analysis Program

33B‐1‐1 15‐Oct‐16 Nondestructive Inspection Methods

35D3‐7‐6‐1 21‐Nov‐18 ETU‐111/E Trailer, Aircraft Engine‐Multi‐Purpose

42E1‐1‐1 1‐Dec‐17 Aircraft Hose

42E2‐1‐2 15‐Dec‐02 Packing Gaskets

44B‐1‐15 28‐Feb‐92

Jet Engine Antifriction Bearing Handling, Removal, Cleaning, Inspection, and Installation at Jet Engine Base Maintenance Facilities

44B‐1‐102 1‐Jun‐17 Antifriction Bearings

44H3‐1‐3 15‐Mar‐12 Use of Boss, Cap & Tube Seals

SF30 pg1 A0002
SPE4A219R0055 A00002 pgs 2-10 for combo

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