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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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: EXAMPLE | Labor Rate | Direct Labor | Indirect Labor | Direct + Indirect Labor Cost | COM $ | Direct + Indirect + COM Cost | Other Direct Costs | Material | Non-Prime Entity Cost $ | Non-Prime Entity Handling Fee | Fixed Fee $ | Total Sell Price | |||||||||||
| Cost Elements | Shift | Source | Company | Category Title | FTEs | Hours | Rate | Direct Labor Cost | Overhead $ | 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 I | 1 | FPRA | Prime Contractor XX | Mechanic I | 5 | 2400 | $ 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 Manager | 1 | FPRA | Prime Contractor XX | Manager | 1 | 480 | $ 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 Mechanic | 1 | FPRA | Prime Contractor XX | Mechanic I | 2 | 960 | $ 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 Mechanic | 1 | FPRA | Prime Contractor XX | Mechanic II | 1 | 480 | $ 27.62 | $ 13,258 | $ 1.00 | $ 3.00 | $ 4.00 | $ 13,261.60 | $ 1.00 | $ 13,262.60 | $ 663.13 | $ 13,925.73 | |||||||
| Note A | Etc. | ||||||||||||||||||||||
| Note B | Etc. | ||||||||||||||||||||||
| Note C | Etc. | ||||||||||||||||||||||
| Note D | CLIN 0001 Total | 9 | 4320 | $ 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 I | 1 | FPRA | Prime Contractor XX | Mechanic I | 2 | 960 | $ 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 E | Maintenance Mechanic II | 2 | FPRA | Non-Prime Entity XX | Mechanic II | 1 | 480 | $ 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 A | Etc. | ||||||||||||||||||||||
| Note F | Etc. | ||||||||||||||||||||||
| Note D | CLIN 0002 Total | 3 | 1440 | $ 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: EXAMPLE | Labor Rate | Direct Labor | Indirect Labor | Direct + Indirect Labor Cost | COM $ | Direct + Indirect + COM Cost | Other Direct Costs | Material | Non-Prime Entity Cost $ | Non-Prime Entity Handling Fee | Fixed Fee $ | Total Sell Price | Total Sell Rate | |||||||||||
| Cost Elements | Shift | Source | Company | Category Title | FTEs | Hours | Rate | Direct Labor Cost | Overhead $ | 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 I | 1 | FPRA | Prime Contractor XX | Engineer I | 1 | 150 | $ 27.62 | $ 4,143 | $ 1.00 | $ 3.00 | $ 4.00 | $ 4,147.00 | $ 1.00 | $ 4,148.00 | $ 207.40 | $ 4,355.40 | ||||||||
| Note E | Engineer III | 1 | FPRA | Non-Prime Entity XX | Engineer III | 1 | 100 | $ 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 A | Etc. | |||||||||||||||||||||||
| CLIN 0003 Total | 2 | 250 | $ 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 D | CLIN 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 Entity | Non-Prime Entity Total Price | Offeror (Prime Contractor) Total Proposed Price | Non-Prime Entity Price % (Entity % of Offeror's Total Proposed Price) |
| Non-Prime Entity "A" (Name) | $50,000 | $2,000,000 | 2.50% |
| Non-Prime Entity "B" (Name) | $300,000 | $2,000,000 | 15.00% |
| Non-Prime Entity "C" (Name) | $75,000 | $2,000,000 | 3.75% |
| 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 Period | Totals & Unit Price | |
| for Option 1 Ordering Period | Totals & Unit Price |
for Option 2 Ordering Period
| Firm Fixed Price (FFP) Roll-up | Totals & Unit Price | ||
| for Base Ordering Period-FY16 | Totals & Unit Price | ||
| for Base Ordering Period-FY17 | Totals & Unit Price | ||
| for Base Ordering Period-FY18 | Totals & Unit Price | ||
| for Base Ordering Period | Totals & Unit Price | ||
| for Option 1 Ordering Period-FY17 | Totals & Unit Price | ||
| for Option 1 Ordering Period-FY18 | Totals & Unit Price | ||
| for Option 1 Ordering Period-FY19 | Totals & Unit Price | ||
| for Option 1 Ordering Period | Totals & Unit Price | ||
| for Option 2 Ordering Period-FY18 | Totals & Unit Price | ||
| for Option 2 Ordering Period-FY19 | Totals & Unit Price | ||
| for Option 2 Ordering Period-FY20 | Totals & Unit Price |
for Option 2 Ordering Period
| Cost Elements | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price | FTEs | Hours | Price |
| 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: Base | Labor Rate | Direct Labor | Indirect Labor | Direct + Indirect Labor Cost | COM $ | Direct + Indirect + COM Cost | Other Direct Costs | Material | Non-Prime Entity Cost $ | Non-Prime Entity Handling Fee | Fixed Fee $ | Total Sell Price | |||||||||||
| Cost Elements | Shift | Source | Company | Functional Area | Category Title | FTEs | Hours | Rate | Direct Labor Cost | Overhead $ | 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 |
This is the start of the file's text. The full file is on GovTribe.
File details come from the government source that posted it. Updated .