Loadmaster Crashworthy Seats (LCWS)

Award Notice Posted Apr 15, 2010

Solicitation number: FD2060-10-21507
Agency: AFLCMC Robins AFB Lifecycle Management Center, Department of Defense
Awarded: Sep 30, 2010 to Mississippi Aerospace Corp
Set-aside: HUBZone

Opportunity facts

Contract number: FA8509-10-C-0026 Federal contract award
NAICS code: 336411 Aircraft Manufacturing
PSC: Not on record
Place of performance: Wralc 235 Byron St., Suite 19A Robins AFB, Georgia 31098, United States

Notice details come from SAM.gov. Updated Oct 1, 2010.

Notice text

5 versions

Update #5 · Latest · Jul 26, 2010

Added: Jul 26, 2010 1:35 pm Note: As of 26 July 2010, the response due date has been extended to 19 Aug 2010 at 4:30pm EST.

Update #4 · Jul 2, 2010

Added: Apr 15, 2010 10:43 am Modified: Jul 02, 2010 5:19 pmTrack Changes The following requirement is intended to be a Hubzone, small business set-aside competition. The solicitation will be uploaded to FBO. ESTIMATED Request for Proposal release date: 2 July 2010. ESTIMATED response date: 5 Aug 2010. ESTIMATED award date: NLT 30 Sep 2010, with options to be awarded 1-365 days after award of the basic contract.

The Air Force Special Operations Command (AFSOC) MC-130W, MC-130H, EC-130J and HC-130P aircraft fleet requires crashworthy scanner seats to facilitate optimal mission effectiveness and survivability. For the purpose of this task, the potential contractor shall utilize a previously developed technical data package for the loadmaster/scanner crashworthy seat (LCWS) frame and seat assembly for all aircraft configurations. The potential contractor will update the drawing package to include a designed tie-down strap to secure the seat and frame in the stowed position. The LCWS kit includes two seats, associated mounting mechanisms and hardware. The contractor shall provide the following for each aircraft configuration:

MC-130W
The potential contractor shall manufacture 11 LCWS group A kits and 10 LCWS group B kits. The contractor shall install using contract field team (CFT). The first production kit shall be used to validate installation by a CFT and finalize drawing and Tech Order data package. Installation of the kits will be IAW with the drawing (Seat Mounting Installation). The potential contractor shall be supplied with a LCWS group B kit to be installed as one of the post kit proof production kits. The potential contractor shall be responsible for production of the group A kit for the Government furnished LCWS group B kit and installation of kit.

For the MC-130W MDS the CLIN structure will include:
Kit Proof Kit to include installation labor (FFP) 1ea.
Data (FFP) 1 Lo for each ELIN
Production Kits (FFP) 10 ea.
Production Kits installation labor (FFP) 1 Lo
ODC-Production Kit Storage (FFP) 1 Lo.
ODC-Kit Transportation (CPFF) 1 Lo.
Travel/Per Diem (CR-no fee) 1 Lo.

MC-130H
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the MC-130H. The potential contractor shall develop a Time Compliance Technical Order (TCTO) for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, one Trial Installation and one Kitproof LCWS kit. The potential contractor shall manufacture and install, using CFT, 20 each production kits.

For the MC-130H MDS the CLIN structure will include:
NRE (FFP) 1 Lo.
Trial Install Kit to include installation labor (FFP) 1 ea.
Kit Proof Kit to include installation labor (FFP) 1ea.
Data (FFP) 1 Lo for each ELIN
Production Kits (FFP) 20 ea.
Production Kits installation labor (FFP) 1 Lo
ODC-Production Kit Storage (FFP) 1 Lo.
ODC-Kit Transportation (CPFF) 1 Lo.
Travel/Per Diem (CR-no fee) 1 Lo.

EC-130J
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the EC-130J. The potential contractor shall develop a TCTO for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, one Trial Installation and one Kitproof LCWS kit. The potential contractor shall manufacture and install, using CFT, 2 production kits.

For the EC-130J MDS the CLIN structure will include:
NRE (FFP) 1 Lo.
Trial Install Kit to include installation labor (FFP) 1 ea.
Kit Proof Kit to include installation labor (FFP) 1ea.
Data (FFP) 1 Lo for each ELIN
Production Kits (FFP) 2 ea.
Production Kits installation labor (FFP) 1 Lo
ODC-Production Kit Storage (FFP) 1 Lo.
ODC-Kit Transportation (CPFF) 1 Lo.
Travel/Per Diem (CR-no fee) 1 Lo.

HC-130P (OPTION)
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the HC-130P. The potential contractor shall develop a TCTO for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, one Trial Installation and one Kitproof LCWS kit. The potential contractor shall manufacture and install, using CFT, 6 each production kits.

For the HC-130P (OPTION) MDS the CLIN structure will include:
NRE (FFP) 1 Lo.
Trial Install Kit to include installation labor (FFP) 1 ea.
Kit Proof Kit to include installation labor (FFP) 1ea.
Data (FFP) 1 Lo for each ELIN
Production Kits (FFP) 6 ea.
Production Kits installation labor (FFP) 1 Lo
ODC-Production Kit Storage (FFP) 1 Lo.
ODC-Kit Transportation (CPFF) 1 Lo.
Travel/Per Diem (CR-no fee) 1 Lo.

HC-130P (AF Reserve) (OPTION)
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the HC-130P. The potential contractor shall develop a TCTO for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, one Trial Installation and one Kitproof LCWS kit. The potential contractor shall manufacture and install, using CFT, 5 each production kits.

For the HC-130P (AR Reserve) (OPTION) MDS the CLIN structure will include:
Production Kits (FFP) 5 ea.
Production Kits installation labor (FFP) 1 Lo
ODC-Production Kit Storage (FFP) 1 Lo.
ODC-Kit Transportation (CPFF) 1 Lo.
Travel/Per Diem (CR-no fee) 1 Lo.

The potential contractor shall be responsible for the completion of all tasks identified in the Performance Work Statement (PWS). The LCWS seat- frame assembly and seat-frame-aircraft interface for the MC-130W were designed under a separate contract. Drawing and technical order packages were verified during trial installation on the MC-130W aircraft, 13-19 Jul 09. The Government will provide the awardee copies of the data packages for use in designing and installing the LCWS on the MC-130W. The contractor shall finalize the data packages for delivery IAW CDRL. The potential contractor shall use the MC-130W design for the seat-frame assembly on all aircraft configurations listed in this PWS.

Added: May 18, 2010 8:21 am Modified: Jul 02, 2010 5:19 pmTrack Changes NOTE: REVISED estimated Request For Proposal release date is: 1 June 2010.

NOTE: As of 2 July 2010, the Request for Proposal and its attachments have been posted via FBO. All responses are due no later than 5 Aug 2010 at 3:30pm EST.

Qustions concerning the drawing attachments can be directed to the Government Engineer via email) to Charles.Ruckle@robins.af.mil and copy Benjamin.wilton@robins.af.mil

Update #3 · Jul 2, 2010

Added: Apr 15, 2010 10:43 am Modified: Jul 02, 2010 8:46 amTrack Changes The following requirement is intended to be a Hubzone, small business set-aside competition. The solicitation will be uploaded to FBO. ESTIMATED Request for Proposal release date: 6 July 2010. ESTIMATED response date: 5 Aug 2010. ESTIMATED award date: NLT 30 Sep 2010, with options to be awarded 1-365 days after award of the basic contract.

The Air Force Special Operations Command (AFSOC) MC-130W, MC-130H, EC-130J and HC-130P aircraft fleet requires crashworthy scanner seats to facilitate optimal mission effectiveness and survivability. For the purpose of this task, the potential contractor shall utilize a previously developed technical data package for the loadmaster/scanner crashworthy seat (LCWS) frame and seat assembly for all aircraft configurations. The potential contractor will update the drawing package to include a designed tie-down strap to secure the seat and frame in the stowed position. The LCWS kit includes two seats, associated mounting mechanisms and hardware. The contractor shall provide the following for each aircraft configuration:

Added: May 18, 2010 8:21 am Modified: Jul 02, 2010 8:46 amTrack Changes NOTE: REVISED estimated Request For Proposal release date is: 1 June 2010.

NOTE: As of 2 July 2010, the new ESTIMATED RFP release date is: 6 July 2010.

Update #2 · May 18, 2010

Added: May 18, 2010 8:21 am NOTE: REVISED estimated Request For Proposal release date is: 1 June 2010.

Update #1 · Apr 15, 2010

Added: Apr 15, 2010 10:43 am The following requirement is intended to be a Hubzone, small business set-aside competition. The solicitation will be uploaded to FBO. ESTIMATED Request for Proposal release date: 18 May 2010. ESTIMATED response date: 22 June 2010. ESTIMATED award date: 16 Aug 2010, with options to be awarded 1-365 days after award of the basic contract.
The Air Force Special Operations Command (AFSOC) MC-130, EC-130J and HC-130 aircraft fleet requires crashworthy scanner seats to facilitate optimal mission effectiveness and survivability. For the purpose of this task, the potential contractor shall utilize a previously developed technical data package for the loadmaster/scanner crashworthy seat (LCWS) frame and seat assembly for all aircraft configurations. The potential contractor will update the drawing package to include a designed tie-down strap to secure the seat and frame in the stowed position. The LCWS kit includes two seats, associated mounting mechanisms and hardware. The contractor shall provide the following for each aircraft configuration:

MC-130P
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the MC-130P. The potential contractor shall develop a TCTO for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, one Trial Installation and one Kitproof LCWS kit. The potential contractor shall manufacture and install, using CFT, 9 each production kits.

EC-130J
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the EC-130J. The potential contractor shall develop a TCTO for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, one Trial Installation and one Kitproof LCWS kit. The potential contractor shall manufacture and install, using CFT, 2 production kits.

HC-130P
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the HC-130P. The potential contractor shall develop a TCTO for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, one Trial Installation and one Kitproof LCWS kit. The potential contractor shall manufacture and install, using CFT, 10 each production kits.

HC-130N
The potential contractor shall develop engineering drawings of the seat-aircraft interface for the HC-130N. The potential contractor shall develop a TCTO for aircraft modifications and a Commodity Technical Order for the seat and mounting mechanism. The potential contractor shall fabricate and install, using CFT, a combined Trial Installation/Kitproof LCWS kit. There will be no additional production kits.
The potential contractor shall be responsible for the completion of all tasks identified in the Performance Work Statement (PWS). The LCWS seat- frame assembly and seat-frame-aircraft interface for the MC-130W were designed under a separate contract. Drawing and technical order packages were verified during trial installation on the MC-130W aircraft, 13-19 Jul 09. The Government will provide the awardee copies of the data packages for use in designing and installing the LCWS on the MC-130W. The contractor shall finalize the data packages for delivery IAW CDRL. The potential contractor shall use the MC-130W design for the seat-frame assembly on all aircraft configurations listed in this PWS.

Files

File	Type	Posted
Q A for RFP FA8509-10-R-21507	—	Aug 17, 2010
Q A for RFP FA8509-10-R-21507	—	Aug 12, 2010
FA850910R21507_0005 RFP amd dtd 12 Aug 2010.pdf	PDF	Aug 12, 2010
Q A for RFP FA8509-10-R-21507 dtd 11 Aug 2010.pdf	PDF	Aug 11, 2010
FA850910R21507_0004 RFP amd dtd 11 Aug 2010.pdf	PDF	Aug 11, 2010
Q A for RFP FA8509-10-R-21507 dtd 3 Aug 2010.pdf	PDF	Aug 3, 2010
Q A for FA8509-10-R-21507 dated 29 July 2010.pdf	PDF	Jul 29, 2010
FA850910R21507_0003 RFP amd dtd 29 July 2010.pdf	PDF	Jul 29, 2010
PWS_revA_dated22July2010.pdf	PDF	Jul 27, 2010
FA850910R21507_0002 RFP amd dtd 27 July 2010.pdf	PDF	Jul 27, 2010
Performance_Plan_12Jul10.pdf	PDF	Jul 26, 2010
PWS_LCWS_12Jul10Rev12.pdf	PDF	Jul 26, 2010
FA850910R21507_0001 RFP amd dtd 26 July 2010.pdf	PDF	Jul 26, 2010
Q A Addtl Info for RFP .docx	DOCX document	Jul 23, 2010
Performance_Plan.pdf	PDF	Jul 20, 2010
PWS_LCWS_1July10Rev11.pdf	PDF	Jul 20, 2010
packaging_reqmts10_21507.pdf	PDF	Jul 20, 2010
AT1_FACTS_sheet_21May.doc	DOC document	Jul 20, 2010
AT5_PastPerformanceQuestionnaire21May.doc	DOC document	Jul 20, 2010
FA850910R21507 RFP dtd 2July10.pdf	PDF	Jul 20, 2010
CDRLS_A001_thru_A015.pdf	PDF	Jul 20, 2010
AT2_ClientAuthorizationLetter.doc	DOC document	Jul 20, 2010
APPXC_1021507_00_2_.pdf	PDF	Jul 20, 2010
AT3_PastPerformanceQuestionnaireTrackingRecord.doc	DOC document	Jul 20, 2010
AT4_TransmittalLetter.doc	DOC document	Jul 20, 2010
Q A for RFP FA8509-10-R-21507.pdf	PDF	Jul 19, 2010
Q A for Pre Solicitation FD2060-10-21507.pdf	PDF	May 4, 2010