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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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Appendix F - CEMS Input Forms.xls | XLS spreadsheet | |
| SPE4A219R0055 A0003 (issued 16Mar20).pdf | ||
| SPE4A219R0055 (issued 22Nov19).pdf |
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Text version
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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