L-6_Vol_4_Non-Prime_Entity_CS.xlsx

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N00019-15-R-0090
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DRAFT L-6 Volume 4 Non-Prime entity CS

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Amendment_0003.pdf PDF
Attachment_13_-_Government_Furnished_Property_List.pdf PDF
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Site_Visit_Q As.pdf PDF
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CDRL_A003_-_Program_Plans_-_Ground_Operations.PDF PDF
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CDRL_A005_-_Program_Plans_-_Aviation_Safety.PDF PDF
L-5_Vol_4_CSDR.xls XLS spreadsheet
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CDRL_A00Q_-_Parts_and_Material_Summary_Report.PDF PDF
Attachment_13_-_Government_Furnished_Property_List.pdf PDF
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Instructions

FIRM FIXED PRICE
FFP EXAMPLE

Effective Work Year (Hours): 1920 NOTE: The Productive Work Year (in labor hours) shall be calculated by the Offeror. DO NOT USE the example's "1920 hours" as it is provided for illustrative purposes ONLY.

Option Period: EXAMPLELabor RateDirect LaborIndirect LaborDirect + Indirect Labor CostCOM $Direct + Indirect + COM CostOther Direct CostsMaterialNon-Prime Entity Cost $Non-Prime Entity Handling FeeFixed Fee $Total Sell Price
Cost ElementsShiftSourceCompanyCategory TitleFTEsHoursRateDirect Labor CostOverhead $Fringe Benefits $G&A $Other (as req'd)Indirect Labor Cost
Prime Contractor Labor Cost
Prime Contractor Direct Labor
CLIN 0001 - HFH Bulletin Suites (includes AFB-657, as required)
0001-A001, CBR+ and Nacelle Mods / Replacements NINC (Lot 7)
AFB-605, High Flight Hour (HFH) Forward Fuselage and Center Fuselage Structure, Inspection of
Schedule Maintenance Mechanic I1FPRAPrime Contractor XXMechanic I52400$ 25.82$ 61,968$ 1.00$ 3.00$ 4.00$ 61,972.00$ 1.00$ 61,973.00$ 3,098.65$ 65,071.65
Inspection Manager1FPRAPrime Contractor XXManager1480$ 30.00$ 14,400$ 1.00$ 3.00$ 4.00$ 14,404.00$ 1.00$ 14,405.00$ 720.25$ 15,125.25
Jr Support Equipment Mechanic1FPRAPrime Contractor XXMechanic I2960$ 25.82$ 24,787$ 1.00$ 3.00$ 4.00$ 24,791.20$ 1.00$ 24,792.20$ 1,239.61$ 26,031.81
Sr Support Equipment Mechanic1FPRAPrime Contractor XXMechanic II1480$ 27.62$ 13,258$ 1.00$ 3.00$ 4.00$ 13,261.60$ 1.00$ 13,262.60$ 663.13$ 13,925.73
Note AEtc.
Note BEtc.
Note CEtc.
Note DCLIN 0001 Total94320$ 114,412.80$ 4.00$ - 0$ 12.00$ - 0$ 16.00$ 114,428.80$ 4.00$ 114,432.80$ 5,721.64$ 120,154.44
CLIN 0002 - Discrete Technical Directives
0002-A001, ACC-695 Single Seat, Navy Aircrew Common Ejection Seat (NACES) Joint Helmet Mounted Cueing System (JHMCS), Incorporation of
Maintenance Mechanic I1FPRAPrime Contractor XXMechanic I2960$ 25.82$ 24,787$ 1.00$ 3.00$ 4.00$ 24,791.20$ 1.00$ 24,792.20$ 1,239.61$ 26,031.81
Note EMaintenance Mechanic II2FPRANon-Prime Entity XXMechanic II1480$ 27.62$ 13,258$ 1.00$ 3.00$ 4.00$ 13,261.60$ 1.00$ 13,262.60$ 7,287.28$ 1,027.49$ 21,577.37
Note AEtc.
Note FEtc.
Note DCLIN 0002 Total31440$ 38,044.80$ 2.00$ - 0$ 6.00$ 8.00$ 38,052.80$ 2.00$ 38,054.80$ 7,287.28$ 2,267.10$ 47,609.18
FFP CLIN Additional Instructions:
- Pre-populated formulae may need to be altered by the Offeror
- Gray shading indicates cells where no data or formulae is expected.
- Include information to the lowest level appropriate for each CLIN (i.e. detail down to CLIN level or Task level).
- If the Offeror's fiscal calendar does not line up with the Government's fiscal calendar please provide additional documentation describing the methodology to determine rates, etc. within the Government's fiscal year
- Indirect Labor categories shall include at a minimum Overhead, Fringe Benefits and G&A. Additional columns can be added to include additional indirect categories at the discretion
of the Offeror. All indirect labor costs shall be accounted for within the Overhead, Fringe Benefit, G&A and other Offeror-proposed categories. Indirect labor costs shall be included
at the Total Task level; however, it is at the discretion of the Offeror to include indirect costs at a more detailed level (e.g. labor category level).
- If there is no Prime Offeror, such as a Joint Venture with two non-Primes, both entities should fill out a Price Attachment L-6 (Non-Prime Entity CS) and Price Attachment L-5 will remain blank.
Note A: Insert rows as necessary to accommodate all labor categories that fall under the specified Technical Directive.
Note B: Insert rows as necessary to accommodate all Technical Directives that fall under the specified Task
Note C: Insert rows as necessary to accommodate all Tasks that fall under the specified CLIN
* The "Source" column should reflect the source of the labor rate (e.g. CBA, AWD, FPRA, etc).
* The "Company" column should reflect the name of the company, union, etc. to which the labor rate is associated.
* The "Category Title" column should reflect the labor category title associated with the Source of the labor rate.
Note D (yellow highlight): The "Total Sell Price" for each Task should match the proposed price submitted in Price Attachment L-4, "Unit Price Matrix". Any differences need to be
explained and justified.
Note E (yellow highlight): Labor categories that are being manned/fulfilled by Non-Prime Entities should be included in Price Attachment L-6 "Non-Prime Entity CS".
The "Total Sell Price" for the Non-Prime Entity labor in Price Attachment L-6 should match inputs in the "Non-Prime Entity Cost $" column in this attachment.
Each subsequent sub-contractor to the Non-Prime Entity should fill out a Prime Attachment L-6. The sub-contractor's "Total Sell Price" in Price Attachment L-6 should
match inputs in the "Non-Prime Entity Cost $" column in the Non-Prime Entity's Price Attachment L-6.
Note F: Insert rows as necessary to accommodate all Tasks that fall under the specified CLIN
Labor Hour
LH EXAMPLE

Effective Work Year (Hours): 1920 NOTE: The Productive Work Year (in labor hours) shall be calculated by the Offeror. DO NOT USE the example's "1920 hours" as it is provided for illustrative purposes ONLY.

Option Period: EXAMPLELabor RateDirect LaborIndirect LaborDirect + Indirect Labor CostCOM $Direct + Indirect + COM CostOther Direct CostsMaterialNon-Prime Entity Cost $Non-Prime Entity Handling FeeFixed Fee $Total Sell PriceTotal Sell Rate
Cost ElementsShiftSourceCompanyCategory TitleFTEsHoursRateDirect Labor CostOverhead $Fringe Benefits $G&A $Other (as req'd)Indirect Labor Cost
Prime Contractor Labor Cost
Prime Contractor Direct Labor
CLIN 0003 - O&A: Engineering Services
Engineer I1FPRAPrime Contractor XXEngineer I1150$ 27.62$ 4,143$ 1.00$ 3.00$ 4.00$ 4,147.00$ 1.00$ 4,148.00$ 207.40$ 4,355.40
Note EEngineer III1FPRANon-Prime Entity XXEngineer III1100$ 39.00$ 3,900$ 1.00$ 3.00$ 4.00$ 3,904.00$ 1.00$ 3,905.00$ 6,557.20$ 523.11$ 10,985.31
Note AEtc.
CLIN 0003 Total2250$ 8,043.00$ 2.00$ 6.00$ 8.00$ 8,051.00$ 2.00$ 8,053.00$ 6,557.20$ 730.51$ 15,340.71
Note DCLIN 0003 Fixed Rate$ 58.44
LH CLIN Additional Instructions:
- Pre-populated formulae may need to be altered by the Offeror
- Gray shading indicates cells where no data or formulae is expected.
- Include information to the lowest level appropriate for each CLIN (i.e. detail down to CLIN level or Task level).
- If the Offeror's fiscal calendar does not line up with the Government's fiscal calendar please provide additional documentation describing the methodology to determine rates, etc. within the Government's fiscal year
- Indirect Labor categories shall include at a minimum Overhead, Fringe Benefits and G&A. Additional columns can be added to include additional indirect categories at the discretion
of the Offeror. All indirect labor costs shall be accounted for within the Overhead, Fringe Benefit, G&A and other Offeror-proposed categories. Indirect labor costs shall be included
at the Total CLIN level; however, it is at the discretion of the Offeror to include indirect costs at a more detailed level (e.g. labor category level).
- If there is no Prime Offeror, such as a Joint Venture with two non-Primes, both entities should fill out a Price Attachment L-6 (Non-Prime Entity CS) and Price Attachment L-5 will remain blank.
Note A: Insert rows as necessary to accommodate all labor categories that fall under the specified CLIN.
* The "Source" column should reflect the source of the labor rate (e.g. CBA, AWD, FPRA, etc).
* The "Company" column should reflect the name of the company, union, etc. to which the labor rate is associated.
* The "Category Title" column should reflect the labor category title associated with the Source of the labor rate.
Note D (yellow highlight): The "Total Rate" for each Task should match the proposed prices submitted in Price Attachment L-4, "Unit Price Matrix". Any differences need to be
explained and justified.
Note E (yellow highlight): Labor categories that are being manned/fulfilled by Non-Prime Entities should be included in Price Attachment L-6 "Non-Prime Entity CS".
The "Total Sell Price/Rate" for the Non-Prime Entity labor in Price Attachment L-6 should match inputs in the "Non-Prime Entity Cost $" in this attachment.
Each subsequent sub-contractor to the Non-Prime Entity should fill out a Prime Attachment L-6. The sub-contractor's "Total Sell Price" in Price Attachment L-6 should
match inputs in the "Non-Prime Entity Cost $" column in the Non-Prime Entity's Price Attachment L-6.
ROLL-UP Tab Additional Instructions:
- Gray shading indicates cells where no data or formulae is expected.
- The Firm Fixed Price (FFP) Roll-Up and Cost Plus Fixed Fee (CPFF) Roll-Up tabs shall include the total FTEs, total hours, and the Sell Price/Rate by Task. The FTEs, total hours, and
Sell Price/Rate shall match the FTEs, total hours, and Sell Price/Rate that is shown on the Base Period or appropriate Option Period tab within this workbook. In addition,
the Sell Price/Rate shall match the proposed Price/Rate submitted in Price Exhibit L-4, "Unit Price Matrix".
Non-Prime Entity Dollar Value as a percentage (%) of Offeror's Total Evaluated Price (TEP)
EXAMPLE
Non-Prime EntityNon-Prime Entity Total PriceOfferor (Prime Contractor) Total Proposed PriceNon-Prime Entity Price % (Entity % of Offeror's Total Proposed Price)
Non-Prime Entity "A" (Name)$50,000$2,000,0002.50%
Non-Prime Entity "B" (Name)$300,000$2,000,00015.00%
Non-Prime Entity "C" (Name)$75,000$2,000,0003.75%
Etc. (Name)
- The Offeror (Prime Contractor) shall provide a Total Price for each Non-Prime Entity to be utilized by the Offeror.
- The Total Price for each Non-Prime Entity shall be reported at a summary level with a single dollar amount that includes prices for all work
to be performed by that particular Non-Prime Entity for the Base Period and all Option Periods.
- Additionally, the Offeror shall provide the percentage (%) of the Offeror's Total Proposed Price that corresponds to each Non-Prime Entity's
Total Price dollar amount.
- The Offeror shall provide this information for all Non-Prime Entities with the exception of those Non-Prime Entities that choose to submit
its rates directly to the Government for proprietary reasons.
- Insert rows as necessary to accommodate all Non-Prime Entities, one entity per row.
- The Non-Prime Entity Total Prices and associated Total Price percentage (as a % of the Offeror's Total Proposed Price) should match
those reported in Volume 1 (Executive Summary), Table ES-1 "Offeror Summary". Any differences need to be expalined and justified.

Attachment L-6 Prime Contractor Cost Summary N00019-15-R-0090

DRAFT

Firm Fixed Price (FFP) Roll-Up

FIRM FIXED PRICE LABOR & SUPPORT

Prime Offeror Name:
DCAA Point of Contact Information:
Effective Work Year (Hours):
Totals & Unit Price
for Base Ordering PeriodTotals & Unit Price
for Option 1 Ordering PeriodTotals & Unit Price

for Option 2 Ordering Period

Firm Fixed Price (FFP) Roll-upTotals & Unit Price
for Base Ordering Period-FY16Totals & Unit Price
for Base Ordering Period-FY17Totals & Unit Price
for Base Ordering Period-FY18Totals & Unit Price
for Base Ordering PeriodTotals & Unit Price
for Option 1 Ordering Period-FY17Totals & Unit Price
for Option 1 Ordering Period-FY18Totals & Unit Price
for Option 1 Ordering Period-FY19Totals & Unit Price
for Option 1 Ordering PeriodTotals & Unit Price
for Option 2 Ordering Period-FY18Totals & Unit Price
for Option 2 Ordering Period-FY19Totals & Unit Price
for Option 2 Ordering Period-FY20Totals & Unit Price

for Option 2 Ordering Period

Cost ElementsFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPriceFTEsHoursPrice
Non-Prime Contractor Labor Cost
Non-Prime Contractor Direct Labor
CLIN 0X01 - HFH Bulletin Suites (includes AFB-657, as required)
0X01-A001, CBR+ and Nacelle Mods / Replacements NINC (Lot 7)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A002, CBR+ and Nacelle Mods / Replacements NINC (Lot 8 thru 21)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A003, CBR+ and Nacelle Mods INC (Lot 7)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A004, CBR+ and Nacelle Mods INC (Lot 8 thru 21)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A005, CBR+ INC; Nacelle Mod NINC (Lot 7)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A006, CBR+ INC; Nacelle Mod NINC (Lot 8 thru 21)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A007, Two (2) IWPs within the 7,000 to 8,000 FH Compliance window- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A008, Two (2) OWPs within the 7,000 to 8,000 FH Compliance window- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A009, One (1) IWP within the 7,000 to 8,000 FH Compliance window- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A00A, One (1) OWP within the 7,000 to 8,000 FH Compliance window- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A00B, HFH Recurring Inspections (200 FH)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A00C, HFH Recurring Inspections (1000 FH)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X01-A00D, Launch & Recovery- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
CLIN 0X02 - Discrete Technical Directives
0X02-A001, ACC-695 Single Seat, Navy Aircrew Common Ejection Seat (NACES) Joint Helmet Mounted Cueing System (JHMCS), Incorporation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A002, ACC-695 FWD and AFT Seat, Navy Aircrew Common Ejection Seat (NACES) Joint Helmet Mounted Cueing System (JHMCS), Incorporation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A003, AFC-400 (F/A-18C), Joint Helmet Mounted Cueing System (JHMCS) Retrofit for F/A-18C, Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A004, AFC-400 "O/C" Kit, Joint Helmet Mounted Cueing System (JHMCS) Retrofit for F/A-18C, Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A005, AFC-444, Joint Helmet Mounted Cueing System (JHMCS) F/A-18 FWD/AFT Cockpit, Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A006, AFC-444 "O/C" Kit, Joint Helmet Mounted Cueing System (JHMCS) F/A-18 FWD/AFT Cockpit, Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A007, AFC-483 (F/A-18C/D)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A008, AYC-1321 (F/A-18C), Joint Helmet Mounted Cueing System Canopy Provisions, Incorporation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A009, AYC-1321 (F/A-18D), Joint Helmet Mounted Cueing System Canopy Provisions, Incorporation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00A, AYC-1321 "O/C" Kit, Joint Helmet Mounted Cueing System Canopy Provisions, Incorporation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00B, Launch & Recovery- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00C, AFC-207 Single Seat, Cockpit Video Recording System (CVRS) Retrofit Installation- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00D, AFC-207 FWD & AFT Seat, Cockpit Video Recording System (CVRS) Retrofit Installation- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00E, AFC-446 PT3 (F/A-18C), Cockpit Pressure Warning System (CPWS), Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00F, AFC-446 PT3 (F/A-18D), Cockpit Pressure Warning System (CPWS), Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00G, AFC-446 PT4 (F/A-18A), Cockpit Pressure Warning System (CPWS), Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00H, AFC-446 PT4 (F/A-18B), Cockpit Pressure Warning System (CPWS), Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00J, AFC-446 PT5 (F/A-18A+), Cockpit Pressure Warning System (CPWS), Installation of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00K, AFC-494 (F/A-18A/B/C/D), NR 2 and NR 3 Cavity Center and Side Decks, Retrofit of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00L, AFC-494 "O/C" Kit (4 & 5); One Side - A/B/C/D, NR 2 and NR 3 Cavity Center and Side Decks, Retrofit of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00M, AFC-494 "O/C" Kit (4 & 5); Both Sides - A/B/C/D, NR 2 and NR 3 Cavity Center and Side Decks, Retrofit of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00N, AFC-494 "O/C" Kit (6 & 7); One Side - A/B, NR 2 and NR 3 Cavity Center and Side Decks, Retrofit of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00P, AFC-494 "O/C" Kit (6 & 7); Both Sides - A/B, NR 2 and NR 3 Cavity Center and Side Decks, Retrofit of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00Q, AVC-5312 F/A-18A/B (Kit A2), Caution Light Indicator Panel, Modification of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00R, AVC-5312 F/A-18A+/C (Kit A1), Caution Light Indicator Panel, Modification of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00S, AVC-5312 F/A-18D (Kit A3), Caution Light Indicator Panel, Modification of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00T, AYC-1363- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00U, ECP-1022 / AYC-1420 One (1) Inner Wing Structure- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00V, ECP-1022 / AYC-1420 Two (2) Inner Wing Structures- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00W, ECP-1022 / AYC-1420 One (1) IWP "O/C" Kit,- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00X, ECP-1022 / AYC-1420 Two (2) IWPs "O/C" Kit,- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00Y, ECP-1034 / AYC-1460 One (1) IWP (TEF Hinge Half Assembly Shim)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A00Z, ECP-1034 / AYC-1460 Two (2) IWPs (TEF Hinge Half Assembly Shims)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A010, ECP-1034 / AYC-1481 One (1) OWP (Aileron Hinge Half Assembly Shim)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A011, ECP-1034 / AYC-1481 Two (2) OWPs (Aileron Hinge Half Assembly Shims)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A012, ECP-974 / AFC-548 One (1) Side, Modification to Y488 Bulkhead and Y497 Former- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A013, ECP-974 / AFC-548 Two (2) Sides, Modification to Y488 Bulkhead and Y497 Former- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A014, ECP-6321 / AFC-554 "O/C" Kit Installation- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A015, ECP-1102 / AFC-578 (F/A-18A/B/C/D), Y508 Former Shear Tie Fastener Holes Retrofit, Modification of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A016, ECP-1102 / AFC-578 "O/C" Kit One (1) Side, Y508 Former Shear Tie Fastener Holes Retrofit, Modification of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A017, ECP-1102 / AFC-578 "O/C" Kit Two (2) Sides, Y508 Former Shear Tie Fastener Holes Retrofit, Modification of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A018, ECP-1100 / AFC-580 (F/A-18A/B/C/D), Y557.5 to Y574.5 Right Hand Side Keel Beam Wen Doubler, Retrofit of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A019, ECP-1100 / AFC-580 "O/C" Kit, Y557.5 to Y574.5 Right Hand Side Keel Beam Wen Doubler, Retrofit of- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01A, ECP-1098 / AFC-591 One (1) Side- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01B, ECP-1098 / AFC-591 Two (2) Sides- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01C, ECP-1118 / AFC-604 One (1) Former,- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01D, ECP-1118 / AFC-604 Two (2) Formers,- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01E, ECP-1142 / AFC-605 One (1) Side- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01F, ECP-1142 / AFC-605 Both Sides- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01G, ECP-1148 / AFC-609- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01H, ECP-1120 / AFC-615 One (1) Side- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01J, ECP-1120 / AFC-615 Two (2) Sides- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01K, ECP-1120 / AFC-615 PT 2 "O/C" Replace the L/H 74A324702 Skin- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01L, ECP-1120 / AFC-615 PT 3 "O/C" Replace the R/H 74A324702 Skin- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01M, ECP-1142 / AFC-618 One (1) Side- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01N, ECP-1142 / AFC-618 Both Sides- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01P, ECP-1159 / AFC-643- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01Q, ECP-1101 / AYC-1536 One (1) IWP (Aft Closure Rib)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01R, ECP-1101 / AYC-1536 Two (2) IWPs (Aft Closure Rib),- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01S, ECP-1125 / AYC-1606 One (1) IWP (Y470 Lower Wing Lug)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01T, ECP-1125 / AYC-1606 Two (2) IWPs (Y470 Lower Wing Lug)- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01U, ECP-XXX / Future 11-84 Technical Derivatives- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0
0X02-A01V, ECP-XXX / Future 11-99 Technical Derivatives- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0- 0- 0$ - 0

Attachment L-6 Prime Contractor Cost Summary N00019-15-R-0090

FFP - Base Ordering Period-FY16

FIRM FIXED PRICE LABOR & SUPPORT

Prime Offeror Name:
DCAA Point of Contact Information:
Effective Work Year (Hours):
Option Period: BaseLabor RateDirect LaborIndirect LaborDirect + Indirect Labor CostCOM $Direct + Indirect + COM CostOther Direct CostsMaterialNon-Prime Entity Cost $Non-Prime Entity Handling FeeFixed Fee $Total Sell Price
Cost ElementsShiftSourceCompanyFunctional AreaCategory TitleFTEsHoursRateDirect Labor CostOverhead $Fringe Benefits $G&A $Other (as req'd)Indirect Labor Cost
Non-Prime Contractor Labor Cost
Non-Prime Contractor Direct Labor
CLIN 0001 - HFH Bulletin Suites (includes AFB-657, as required)
0001-A001, CBR+ and Nacelle Mods / Replacements NINC (Lot 7)
AFB-605, High Flight Hour (HFH) Forward Fuselage and Center Fuselage Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-605 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-606, High Flight Hour (HFH) Center Fuselage Areas, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-606 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-607, High Flight Hour (HFH) Aft Fuselage Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-607 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-618, High Flight Hour (HFH) Vertical Stabilizer Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-618 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-688, High Flight Hour (HFH) Center Fuselage Nacelle Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-688 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-689, High Flight Hour (HFH) Center Fuselage Dorsal Areas, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-689 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-657, Y488 Bulkhead and Y497 Former MLG Uplock Mechanism Support Holes, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-657 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A001 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A002, CBR+ and Nacelle Mods / Replacements NINC (Lot 8 thru 21)
AFB-605, High Flight Hour (HFH) Forward Fuselage and Center Fuselage Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-605 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-606, High Flight Hour (HFH) Center Fuselage Areas, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-606 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-607, High Flight Hour (HFH) Aft Fuselae Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-607 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-618, High Flight Hour (HFH) Vertical Stabilizer Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-618 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-688, High Flight Hour (HFH) Center Fuselage Nacelle Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-688 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-689, High Flight Hour (HFH) Center Fuselage Dorsal Areas, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-689 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-657, Y488 Bulkhead and Y497 Former MLG Uplock Mechanism Support Holes, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-657 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A002 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A003, CBR+ and Nacelle Mods INC (Lot 7)
AFB-605, High Flight Hour (HFH) Forward Fuselage and Center Fuselage Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-605 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-607, High Flight Hour (HFH) Aft Fuselae Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-607 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-618, High Flight Hour (HFH) Vertical Stabilizer Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-618 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A003 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A004, CBR+ and Nacelle Mods INC (Lot 8 thru 21)
AFB-605, High Flight Hour (HFH) Forward Fuselage and Center Fuselage Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-605 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-607, High Flight Hour (HFH) Aft Fuselae Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-607 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-618, High Flight Hour (HFH) Vertical Stabilizer Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-618 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A004 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A005, CBR+ INC; Nacelle Mod NINC (Lot 7)
AFB-605, High Flight Hour (HFH) Forward Fuselage and Center Fuselage Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-605 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-607, High Flight Hour (HFH) Aft Fuselae Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-607 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-618, High Flight Hour (HFH) Vertical Stabilizer Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-618 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-688, High Flight Hour (HFH) Center Fuselage Nacelle Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-688 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A005 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A006, CBR+ INC; Nacelle Mod NINC (Lot 8 thru 21)
AFB-605, High Flight Hour (HFH) Forward Fuselage and Center Fuselage Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-605 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-607, High Flight Hour (HFH) Aft Fuselae Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-607 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-618, High Flight Hour (HFH) Vertical Stabilizer Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-618 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
AFB-688, High Flight Hour (HFH) Center Fuselage Nacelle Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
AFB-688 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A006 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A007, Two (2) IWPs within the 7,000 to 8,000 FH Compliance window
AYB-1166, High Flight Hour (HFH) Inner Wing Panel (IWP), Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0001-A007 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A008, Two (2) OWPs within the 7,000 to 8,000 FH Compliance window
AYB-1167, High Flight Hour (HFH) Outer Wing Panel (OWP) Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0001-A008 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A009, One (1) IWP within the 7,000 to 8,000 FH Compliance window
AYB-1166, High Flight Hour (HFH) Inner Wing Panel (IWP), Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0001-A009 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A00A, One (1) OWP within the 7,000 to 8,000 FH Compliance window
AYB-1167, High Flight Hour (HFH) Outer Wing Panel (OWP) Structure, Inspection of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0001-A00A Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A00B, HFH Recurring Inspections (200 FH)
200 FH Recurring Inspection
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0001-A00B Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A00C, HFH Recurring Inspections (1000 FH)
1000 FH Recurring Inspection
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0001-A00C Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0001-A00D, Launch & Recovery
Launch & Recovery
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0001-A00D Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
CLIN 0001 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
CLIN 0002 - Discrete Technical Directives
0002-A001, ACC-695 Single Seat, Navy Aircrew Common Ejection Seat (NACES) Joint Helmet Mounted Cueing System (JHMCS), Incorporation of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0002-A001 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0002-A002, ACC-695 FWD and AFT Seat, Navy Aircrew Common Ejection Seat (NACES) Joint Helmet Mounted Cueing System (JHMCS), Incorporation of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0002-A002 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0002-A003, AFC-400 (F/A-18C), Joint Helmet Mounted Cueing System (JHMCS) Retrofit for F/A-18C, Installation of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0002-A003 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0002-A004, AFC-400 "O/C" Kit, Joint Helmet Mounted Cueing System (JHMCS) Retrofit for F/A-18C, Installation of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0002-A004 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0002-A005, AFC-444, Joint Helmet Mounted Cueing System (JHMCS) F/A-18 FWD/AFT Cockpit, Installation of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0002-A005 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0002-A006, AFC-444 "O/C" Kit, Joint Helmet Mounted Cueing System (JHMCS) F/A-18 FWD/AFT Cockpit, Installation of
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0
0002-A006 Total- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0- 0
0002-A007, AFC-483 (F/A-18C/D)
Labor category for each individual position- 0- 0- 0- 0- 0
Labor category for each individual position- 0- 0- 0- 0- 0
Etc.- 0- 0- 0- 0- 0

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