UNCLASSIFIED. UNCLASSIFIED Navy Page 1 of 126 P-1 Line #32

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1 Exhibit P-40, Budget Line Item Justification: PB 2016 Navy Date: February N: Aircraft Procurement, Navy / BA 05: Modification of Aircraft / BSA 1: Modification of Aircraft ID Code (A=Service Ready, B=Not Service Ready) : A Program Elements for Code B Items: Other Related Program Elements: Line Item MDAP/MAIS Code: 000 Resource Summary Item MDAP/MAIS Code(s): Prior Years FY 2014 FY 2015 Procurement Quantity (Units in Each) Gross/Weapon System Cost ($ in Millions) 5, , , , , , , Less PY Advance Procurement ($ in Millions) Net Procurement (P1) ($ in Millions) 5, , , , , , , Plus CY Advance Procurement ($ in Millions) tal Obligation Authority ($ in Millions) 5, , , , , , , (The following Resource Summary rows are for informational purposes only. The corresponding budget requests are documented elsewhere.) Initial Spares ($ in Millions) Flyaway Unit Cost ($ in Dollars) Gross/Weapon System Unit Cost ($ in Dollars) Description: This line item funds modifications to all models of the F/A-18 aircraft. The F/A-18 Naval Strike Fighter is a twin-engine, mid-wing, multi-mission tactical aircraft. The F/A-18 is employed in both Navy and Marine Corps squadrons. Commencing with the FY 1988 procurement, both the single seat and two-seat F/A-18s include a night attack capability. The F/A-18 can be missionized through selected use of external equipment to accomplish specific fighter or attack missions. This commonality provides the Operational Commander more flexibility in employing his tactical aircraft in a dynamic scenario. The primary design mission for the F/A-18 is a strike fighter which includes the traditional fighter applications, such as fighter escort and fleet air defense, combined with the attack applications, such as interdiction and close air support. Since fighter capabilities are available in either mission, a robust self-defense capability is retained. Current aircraft inventory (as of 24 July 14): F/A-18A - 95: Avg age 28.1 yrs (7445 hrs) - current service life 8,000 hrs F/A-18B - 21: Avg age 29.6 yrs (6531 hrs) - current service life 8,000 hrs F/A-18C - 371: Avg age 22.4 yrs (7113 hrs) - current service life 8,000 hrs F/A-18D - 131: Avg age 21.8 yrs (6896 hrs) - current service life 8,000 hrs F/A-18E - 252: Avg age 7.2 yrs (2170 hrs) - current service life 6,000 hrs F/A-18F - 258: Avg age 8.5 yrs (2795 hrs) - current service life 6,000 hrs EA-18G - 104: Avg age 3.1 yrs (864 hrs) - current service life 7,500 hrs tal Navy Page 1 of 126 P-1 Line #32 Volume 2-73

2 Exhibit P-40, Budget Line Item Justification: PB 2016 Navy Date: February N: Aircraft Procurement, Navy / BA 05: Modification of Aircraft / BSA 1: Modification of Aircraft ID Code (A=Service Ready, B=Not Service Ready) : A Program Elements for Code B Items: Other Related Program Elements: Line Item MDAP/MAIS Code: 000 Item MDAP/MAIS Code(s): Exhibits Schedule tal Title* 1 / Correction of Discrepancies (OSIP 11-84) (SAFETY /RELIABILITY/ IMPROVEMENT) 2 / Digital Communications System (DCS) (OSIP 10-99) (CAPABILITY IMPROVEMENT) 3 / F/A-18 Aircraft Structural Life Management Plan (SLMP) (OSIP 11-99) CBR+ (SAFETY / LIFE EXTENSION) 4 / Multi-Functional Information Distribution System (MIDS) (OSIP 12-99) (CAPABILITY IMPROVEMENT) P-3a P-3a P-3a P-3a Exhibits ID CD Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) - / 1, / / / / - - / / / / / / - - / / 1, / / / / - - / / / / / / - - / / USMC F/A-18 Upgrade ECP-583 (OSIP 21-00) (AVIONICS UPGRADE) P-3a - / / / / / - - / / Joint Helmet Mounted Cueing System (JHMCS) (OSIP 24-00) (CAPABILITY IMPROVEMENT) 7 / Advanced Targeting Forward Looking Infrared (ATFLIR) (OSIP 12-01) (CAPABILITY IMPROVEMENTS) 8 / F/A-18C/D/E/F and EA-18G Training System (OSIP ) (TRAINERS UPGRADE) 9 / E/F & EA-18G Correction of Operational Discrepancies (OSIP 14-03) (SAFETY /RELIABILITY/IMPROVEMENT) 10 / Core Avionics Improvements / Upgrades (OSIP ) (Capability and Reliability Improvements) P-3a P-3a P-3a P-3a P-3a - / / / / / - - / / / / / / / / / / / / - - / / / / / / - - / / / / / / - - / / Litening AT Targeting Pod (OSIP ) (CAPABILITY IMPROVEMENTS) P-3a - / / / / / - - / / AESA/AN-APG-65/AN-APG-73 (OSIP ) (AVIONICS UPGRADE) P-3a - / / / / / - - / / EW Unique (OSIP ) (Capability Improvements) P-3a - / / / / / - - / / Network Centric Operations: (OSIP ) (Avionics Upgrade) P-3a - / / / / / - - / / EA-18G Unique OSIP (011-10) (SAFETY /RELIABILITY/IMPROVEMENT) P-3a - / / / / / - - / / Power and Propulsion (11-13) (Safety, Readiness, Reliability) P-3a - / / / / / - - / / Infrared Search and Track (IRST) (04-14) (CAPABILITY IMPROVEMENTS) P-3a - / / - - / / / - - / / Automated Information Systems (AIS) (OSIP ) (Safety) P-3a - / / / / / - - / / F/A-18E/F and EA-18G SLEP (OSIP ) (SAFETY / LIFE EXTENSION) P-3a - / / / / / - - / / Priority Stores Integration (OSIP 10-16) (CAPABILITY IMPROVEMENT) P-3a - / / - - / - - / / - - / / Inactive OSIPs () P-3a - / / - - / - - / - - / - - / - tal Gross/Weapon System Cost - / 5, / / / / / Exhibits Schedule FY 2017 FY 2018 FY 2019 FY 2020 tal Title* 1 / Correction of Discrepancies (OSIP 11-84) (SAFETY /RELIABILITY/ IMPROVEMENT) P-3a Exhibits ID CD Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) - / / / / / / 1, Navy Page 2 of 126 P-1 Line #32 Volume 2-74

3 Exhibit P-40, Budget Line Item Justification: PB 2016 Navy Date: February N: Aircraft Procurement, Navy / BA 05: Modification of Aircraft / BSA 1: Modification of Aircraft ID Code (A=Service Ready, B=Not Service Ready) : A Program Elements for Code B Items: Other Related Program Elements: Line Item MDAP/MAIS Code: 000 Item MDAP/MAIS Code(s): Exhibits Schedule FY 2017 FY 2018 FY 2019 FY 2020 tal Title* 2 / Digital Communications System (DCS) (OSIP 10-99) (CAPABILITY IMPROVEMENT) 3 / F/A-18 Aircraft Structural Life Management Plan (SLMP) (OSIP 11-99) CBR+ (SAFETY / LIFE EXTENSION) 4 / Multi-Functional Information Distribution System (MIDS) (OSIP 12-99) (CAPABILITY IMPROVEMENT) P-3a P-3a P-3a Exhibits ID CD Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) Quantity / tal Cost (Each) / ($ M) - / / / / / / / / / / / 1, / 3, / / / / / / 1, / USMC F/A-18 Upgrade ECP-583 (OSIP 21-00) (AVIONICS UPGRADE) P-3a - / / / / - - / - - / / Joint Helmet Mounted Cueing System (JHMCS) (OSIP 24-00) (CAPABILITY IMPROVEMENT) 7 / Advanced Targeting Forward Looking Infrared (ATFLIR) (OSIP 12-01) (CAPABILITY IMPROVEMENTS) 8 / F/A-18C/D/E/F and EA-18G Training System (OSIP ) (TRAINERS UPGRADE) 9 / E/F & EA-18G Correction of Operational Discrepancies (OSIP 14-03) (SAFETY /RELIABILITY/IMPROVEMENT) 10 / Core Avionics Improvements / Upgrades (OSIP ) (Capability and Reliability Improvements) P-3a P-3a P-3a P-3a P-3a - / / - - / - - / - - / - - / / / / / - - / / / / / / / / / / / / / / 1, / / / / / 1, / 2, / Litening AT Targeting Pod (OSIP ) (CAPABILITY IMPROVEMENTS) P-3a - / - - / - - / - - / - - / / / AESA/AN-APG-65/AN-APG-73 (OSIP ) (AVIONICS UPGRADE) P-3a - / / / / / / 2, / EW Unique (OSIP ) (Capability Improvements) P-3a - / / - - / - - / - - / - - / / Network Centric Operations: (OSIP ) (Avionics Upgrade) P-3a - / / / / / / / EA-18G Unique OSIP (011-10) (SAFETY /RELIABILITY/IMPROVEMENT) P-3a - / / / / / / / Power and Propulsion (11-13) (Safety, Readiness, Reliability) P-3a - / / / / / / / Infrared Search and Track (IRST) (04-14) (CAPABILITY IMPROVEMENTS) P-3a - / / / / / / 1, / Automated Information Systems (AIS) (OSIP ) (Safety) P-3a - / / / / / / / F/A-18E/F and EA-18G SLEP (OSIP ) (SAFETY / LIFE EXTENSION) P-3a - / / / / / 1, / 1, / Priority Stores Integration (OSIP 10-16) (CAPABILITY IMPROVEMENT) P-3a - / / / / / / / Inactive OSIPs () P-3a - / - - / - - / - - / - - / - - / tal Gross/Weapon System Cost - / 1, / 1, / 1, / 1, / 6, / 19, *Title represents 1) the Number / Title for Items; 2) the Number / Title [DODIC] for Ammunition; and/or 3) the Number / Title (Modification Type) for Modifications. Note: tals in this Exhibit P-40 set may not be exact or add due to rounding. Justification: The overall goal of the modifications budgeted in is to implement commonality/capability and structural safety and reliability improvements. Navy Page 3 of 126 P-1 Line #32 Volume 2-75

4 Resource Summary Prior Years FY 2014 FY / Correction of Discrepancies (OSIP 11-84) Procurement Quantity (Units in Each) Gross/Weapon System Cost ($ in Millions) 1, , Less PY Advance Procurement ($ in Millions) Net Procurement (P1) ($ in Millions) 1, , Plus CY Advance Procurement ($ in Millions) tal Obligation Authority ($ in Millions) 1, , (The following Resource Summary rows are for informational purposes only. The corresponding budget requests are documented elsewhere.) Initial Spares ($ in Millions) Gross/Weapon System Unit Cost ($ in Dollars) tal Description: Corrections to discrepancies found during testing and evaluation can sometimes be incorporated into production aircraft, effective with the physical configuration audit which establishes the product baseline of the aircraft. However, when this cannot be done due to time constraints, retrofit of the changes into already delivered aircraft requires funding through the aircraft modification program. Additionally, aircraft discrepancies can be discovered during sustainment activities, engineering analysis, standard depot level evaluations, and/or during normal fleet operations. Not addressing these structural and system discrepancies will create maintenance and supply problems, and adversely impact safety of flight and operational readiness. This Operational, Safety and Improvement Program (OSIP) provides resources to correct such issues via Engineering Change Proposal (ECP) and other applicable procurement efforts by modifying, improving, and restoring aircraft structural safety and reliability to designed/required life limits. Modifications for the F/A-18 A/B/C/D aircraft include: flight controls, forward fuselage, aft fuselage, wing, critical structures, electrical, hydraulic, Environmental Control Systems (ECS), launch and recovery, fuel, mechanical, secondary power, Blue Angel modifications, and other sustainment activities. Corrections to the following items/conditions are required: Current Active Modifications: ECP 590 On Board Oxygen Generating System (OBOGS) Solid State Oxygen Monitor (SSOM), safety ECP ECP 609 F/A-18 A-D Inner Wing Conversion and Reliability Improvements ECP 1034-NI Trailing Edge Flap/Aileron Attach Log Bushing ECP 1102NI F/A-18 A-D Y508 Former Shear Tie Fastener Holes Retrofit - Modification to the fasteners near the Y508 Former Aft Shear Tie ECP 1121 F/A-18 A-D Main Landing Gear (MLG) Critical Components Retrofit ECP 1122 F/A-18 A-D NLG Critical Components Retrofit ECP 1098NI F/A-18 A-D Y615 Former and Bootstrap Retrofit ECP 1118NI F/A-18 A-D Y580.5/Y590.5 Former Replacement Modline ECP 1120NI F/A-18 A-D Upper Out Board Longeron Y453/Y508 Forward Section Splice Retrofit ECP 1137NI Redesign of Fire Extinguisher Temp. Compensating Pressure Switch (TCPS) ECP 1140NI Aileron Servocylinder Main Ram Linear Variable Displacement Transformer upgrade ECP 1142NI Y326.5 Leading Edge Extension (LEX) Support Fitting and Substructure Retrofit ECP 1142C1NI Y394.2 LEX Connecting Link Retrofit ECP 1148NI Speed Brake Arresting Hook Actuator Fitting Retrofit ECP XXX26 F/A-18 A-D Structural Stress Corrosion Cracking Issues ECP XXX27 F/A-18 A-D Subsystems Retrofit Upgrades Issues ECP XXX28 F/A-18 A-D ECS Subsystems Upgrade Issues ECP XXX29 F/A-18 A-D Fuel Related Upgrade Issues Navy Page 4 of 126 P-1 Line #32 Volume 2-76

5 ECP XXX30 F/A-18 A-D Flight Control Surfaces Issues ECP XXX32 F/A-18 A-D Y470 Inner Wing Panel Lug - Modification to the Y470 Inner Wing Panel Lug ECP-1159 Y557.5 Bulkhead Tub Retrofit ECP Mod of Aircraft Ground Servicing Engine Inlet Screen ECP JAX-F Navy Flight Demonstration Squadron (NFDS) mods, C&D Conversion Future Modifications: ECP 087S1 External Stores Electromagnetic Interference (EMI) Protection - Provide for the application of external stores EMI Protection. This ECP includes installation costs only. ECP 592 Fuselage Skin Crack - Safety improvement to the fatigue life of the forward skin section of the chem.-milled panels. ECP 608 Crease Longeron - Restores the load path lost when the crease longeron cracks at FS 453. ECP MB9425 Modified Navy Aircrew Common Ejection Seat (NACES) Backplate - Modification to the NACES backplate to prevent cracks ECP XXX5 Wing Spar Crack - Strengthens the existing front inner wing spar to improve fatigue life. ECP NI 931 Forward Lower Keel Modification - Improves fatigue life of the Nose Landing Gear (NLG) drag brace. ECP 609 (Bundled in) Interwing Conversion ECP XXX-21 (Bundled in ECP-609) - Converting Lot 10/11 wings to Lot 12 and above configuration. ECP 1086 NI F/A-18 A-D Modification of A/C (ECS) Test Set - Publication related updates ECP 1088 F/A-18 A-D Fuel Valve Interchangeability - Modification to upgrade fuel valves for configuration purposes ECP 1095 F/A-18 A-D MLG Side Brace Downlock Actuator Connection Link - Modification to upgrade the MLG actuator link ECP MB9445 Replacement of NACES Radio Beacon Actuator - Modification to incorporate a new and improved radio beacon signal in order to comply with new satellite requirements ECP 6376 F/A-18 A-D NACES Ejection Seat Improvements (ECP MB9431) - Publication related updates ECP 1149NI Fuel Dumping Pressure Relief Valve ECP XXX13 Bay 3 Shelf Redesign - Modify avionic shelves to withstand catapult fatigue loads. ECP XXX14 Bay 4 Shelf Redesign - Modify avionic shelves to withstand catapult fatigue loads. ECP XXX-16 Vertical Tail - Modify vertical tail former and spars to prevent fatigue cracking. ECP XXX-17 Canopy/Windscreen - Modify canopy/windscreen frames and address delamination. ECP XXX18 NLG/Main Landing Gear (MLG) Fatigue Improvements - Fatigue Improvements to include arresting gear planning link redesign ECP XXX23 Aft Fuselage Structure Failures - Modification to correct failed aft fuselage areas ECP XXX24 NACES Improved Upper Catapult Sleeve, Safety ECP - Modification to incorporate a redesigned NACES upper catapult sleeve ECP XXX25 F/A-18 B/D Canopy Sill Longeron Crack - Modification to beef up the canopy sill longeron to prevent severing condition ECP XXX31 F/A-18 A-D Kapton Wiring Modification Improvement - Modification to upgrade aircraft electrical wiring ECP XXX33 F/A-18 A-D NACES Retrofit Upgrades - AFC-XXX ECP 6431 F/A-18 A-D In-Flight Refueling Probe Timer Bellcrank Fitting ECP-1095 MLG Side Brace Downlock Actuator Connecting Link Upgrade ECP Fuel Tank Cavity Foam Material Change 1 / Correction of Discrepancies (OSIP 11-84) DEVELOPMENT STATUS/MAJOR DEVELOPMENT MILESTONES: Each change has been or will be tested prior to installation in the F/A-18. Navy Page 5 of 126 P-1 Line #32 Volume 2-77

6 Models of Systems Affected: F/A-18 A/B/C/D Procurement Financial Plan Modification Item 1 of 1: Correction of Discrepancies (OSIP 11-84) A Kits Recurring Modification Type: SAFETY /RELIABILITY/ IMPROVEMENT tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) Related RDT&E PEs: 1 / Correction of Discrepancies (OSIP 11-84) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal tal Cost ($ M) 1.1.1) ECP 590 OBOGS SSOM, Safety ECP - Organic 59 / / / / - - / - - / - - / - - / - - / - - / - - / / ) ECP 609 F/A-18 A-D Inner Wing Conversion and Reliability Improvements - Organic 1.1.3) ECP 1034 NI Trailing Edge Flap/Aileron Attach Log Bushing - Organic 1.1.4) ECP 1102 Y508 Former Shear Tie Fastener Holes Retrofit - Organic 1.1.5) ECP 1121 F/A-18 A-D MLG Critical Components - Part 1 kit - Organic 1.1.6) ECP 1121 F/A-18 A-D MLG Critical Components - Basic kit - Organic 1.1.7) ECP 1122 F/A-18 A-D NLG Critical Components - Part 1 kit - Organic 1.1.8) ECP 1122 F/A-18 A-D NLG Critical Components - Basic kit - Organic 1.1.9) ECP 1098NI F/A-18 A-D Y615 Former and Bootstrap Retrofit - Organic ) ECP 1118NI F/A-18 A-D Y580.5/Y590.5 Former Replacement Modline - Organic ) ECP 1120NI F/A-18 A-D Upper O/B Longeron Y453/Y508 Fw Section Splice - Organic ) ECP 1137NI Fire Extinguisher Temp Compensating Pressure Switch - Organic ) ECP 1140NI Aileron Servocylndr Main Ram Linear Var Displcmnt Trnsfrmr - Organic ) ECP-1142NI Y326.5 Lead Edge Ext (LEX) Spt Fitting & Substructure - Organic ) ECP-1142C1NI Y394.2 LEX Connecting Link Retrofit - Organic ) ECP 1148NI Speed Brake Arresting Hook Actuator Fitting Retrofit - Organic ) ECP XXX26 Structural Stress Corrosion Crack Issues - Organic 15 / / / - 12 / / - 12 / / - - / - - / - - / - - / - 39 / / / / - - / - - / - - / - - / - - / - - / - - / - - / / / / / / / - 95 / / - - / - - / - - / - - / / / / - - / - 5 / / - 5 / / - 8 / / / / / / / / - - / - - / - - / - - / - - / - - / - - / - - / / / / - - / - 5 / / - 5 / / - 5 / / / / / / / / - - / - - / - - / - - / - - / - - / - - / - - / / / / / / / - 50 / / / / / / / / / / / / - 60 / / / / / / / / / / / / - 50 / / - - / - - / - - / - - / / / / / / / / / / - - / - - / - - / / / - - / - - / / / / / / / / / / / / / / / / / / - - / - - / - - / / / / / / / / / / / - - / - - / / / / / / / - 4 / / - - / - - / - - / - - / / / - - / - - / - 60 / / - 60 / / / / / / / Navy Page 6 of 126 P-1 Line #32 Volume 2-78

7 Models of Systems Affected: F/A-18 A/B/C/D Financial Plan ) ECP XXX27 F/A-18 A-D Subsystems Retrofit Upgrades Issues - Organic ) ECP XXX28 F/A-18 A-D ECS Subsystems Upgrade Issues - Organic ) ECP XXX29 F/A-18 A-D Fuel Related Upgrade Issues - Organic ) ECP-XXX30 F/A-18 A-D Flight Control Surfaces Issues - Organic Modification Type: SAFETY /RELIABILITY/ IMPROVEMENT tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) Related RDT&E PEs: 1 / Correction of Discrepancies (OSIP 11-84) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal tal Cost ($ M) - / - - / - - / - 60 / / - 60 / / / / / / / / - - / - - / - 60 / / - 60 / / / / / / / / - - / - - / - 60 / / - 60 / / - 50 / / / / / / - - / - - / - 60 / / - 60 / / / / / / / ) ECP-XXX32 - F/A-18 A-D NACES Retrofit - / - - / - - / / / / / / / - - / / / Upgrades - Organic (1) ) ECP Y557.5 Bulkhead Tub Retrofit - Organic ) ECP Mod of Aircraft Ground Servicing Engine Inlet Screen - Organic ) ECP JAX F NFDS mods, C&D Conversion (Blue Angels) - Organic ) Archived ECPs - Organic 42,325 / / - - / - - / - 60 / / - 60 / / / / / / / / - - / - - / / / / / - - / - - / - - / - - / / / / / - - / - - / - - / - - / - - / - - / - - / - - / - 16 / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - 42,325 / Subtotal: Recurring - / / / / / - - / / / / / / / Non-Recurring 1.2.1) Installation Kits N/R - Organic - / / / / - - / - - / - - / - - / - - / - - / - - / - - / Subtotal: Non-Recurring - / / / / - - / - - / - - / - - / - - / - - / - - / - - / B Kits Recurring 2.1.1) Installation Equipment - Organic - / / / - - / - - / - - / - - / - - / - - / - - / - - / - - / Subtotal: Recurring - / / / - - / - - / - - / - - / - - / - - / - - / - - / - - / Non-Recurring 2.2.1) Installation Equipment N/R - Organic - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / Subtotal: Non-Recurring - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / Subtotal: Correction of Discrepancies (OSIP 11-84) 43,909 / / ,021 / ,686 / / - 1,686 / / / / / ,121 / ,003 / Subtotal: Procurement, All Modification Items - / / / / / - - / / / / / / / Support (All Modification Items) 3.1) Engineering Change Orders - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - 3.2) Data - / / / / - - / - - / - - / - - / - - / - - / - - / - - / Navy Page 7 of 126 P-1 Line #32 Volume 2-79

8 Models of Systems Affected: F/A-18 A/B/C/D Financial Plan Modification Type: SAFETY /RELIABILITY/ IMPROVEMENT tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) Related RDT&E PEs: 1 / Correction of Discrepancies (OSIP 11-84) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal tal Cost ($ M) 3.3) Training Equipment - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - 3.4) Support Equipment - / / / / / - - / / / / / - - / / ) ILS - / / / / / - - / / / / / / / (2) 3.6) Other Support - / / / / / - - / / / / / / / ) Interim Contractor Support - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - (3) 3.8) Installation Cost 30,251 / / ,204 / ,355 / / - 1,355 / ,508 / ,156 / / / ,798 / ,815 / Subtotal: Support - / / / / / - - / / / / / / / 1, Installation Subtotal: Installation - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - tal tal Cost (Procurement + Support + Installation) 1, , Navy Page 8 of 126 P-1 Line #32 Volume 2-80

9 Modification Item 1 of 1: Correction of Discrepancies (OSIP 11-84) Manufacturer Information Manufacturer Name: TBD Administrative Leadtime (in Months): Contract Dates Delivery Dates Manufacturer Location: TBD Production Leadtime (in Months): 1 / Correction of Discrepancies (OSIP 11-84) Dates FY 2014 FY 2015 FY 2017 FY 2018 FY 2019 FY 2020 Installation Information Method of Implementation (Organic): Not Installed - ECP 590 OBOGS SSOM, Safety ECP Installation Quantity: 335 Method of Implementation (Organic): Not Installed - ECP 609 F/A-18 A-D Inner Wing Conversion and Reliability Improvements Installation Quantity: 39 Method of Implementation (Organic): Not Installed - ECP 1034 NI Trailing Edge Flap/Aileron Attach Log Bushing Installation Quantity: 674 Method of Implementation (Organic): Not Installed - ECP 1102 Y508 Former Shear Tie Fastener Holes Retrofit Installation Quantity: 445 Method of Implementation (Organic): Organic - ECP 1121 F/A-18 A-D MLG Critical Components - Part 1 kit Installation Quantity: 121 Method of Implementation (Organic): Not Installed - ECP 1121 F/A-18 A-D MLG Critical Components - Basic kit Installation Quantity: 125 Method of Implementation (Organic): Organic - ECP 1122 F/A-18 A-D NLG Critical Components - Part 1 kit Installation Quantity: 100 Method of Implementation (Organic): Not Installed - ECP 1122 F/A-18 A-D NLG Critical Components - Basic kit Installation Quantity: 120 Method of Implementation (Organic): Not Installed - ECP 1098NI F/A-18 A-D Y615 Former and Bootstrap Retrofit Installation Quantity: 525 Method of Implementation (Organic): Not Installed - ECP 1118NI F/A-18 A-D Y580.5/Y590.5 Former Replacement Modline Installation Quantity: 566 Method of Implementation (Organic): Not Installed - ECP 1120NI F/A-18 A-D Upper O/B Longeron Y453/Y508 Fw Section Splice Installation Quantity: 220 Navy Page 9 of 126 P-1 Line #32 Volume 2-81

10 Modification Item 1 of 1: Correction of Discrepancies (OSIP 11-84) Installation Information Method of Implementation (Organic): Not Installed - ECP 1137NI Fire Extinguisher Temp Compensating Pressure Switch Installation Quantity: / Correction of Discrepancies (OSIP 11-84) Method of Implementation (Organic): Not Installed - ECP 1140NI Aileron Servocylndr Main Ram Linear Var Displcmnt Trnsfrmr Installation Quantity: 618 Method of Implementation (Organic): Not Installed - ECP-1142NI Y326.5 Lead Edge Ext (LEX) Spt Fitting & Substructure Installation Quantity: 526 Method of Implementation (Organic): Not Installed - ECP-1142C1NI Y394.2 LEX Connecting Link Retrofit Installation Quantity: 487 Method of Implementation (Organic): Not Installed - ECP 1148NI Speed Brake Arresting Hook Actuator Fitting Retrofit Installation Quantity: 432 Method of Implementation (Organic): Not Installed - ECP XXX26 Structural Stress Corrosion Crack Issues Installation Quantity: 475 Method of Implementation (Organic): Not Installed - ECP XXX27 F/A-18 A-D Subsystems Retrofit Upgrades Issues Installation Quantity: 475 Method of Implementation (Organic): Organic - ECP XXX28 F/A-18 A-D ECS Subsystems Upgrade Issues Installation Quantity: 475 Method of Implementation (Organic): Not Installed - ECP XXX29 F/A-18 A-D Fuel Related Upgrade Issues Installation Quantity: 475 Method of Implementation (Organic): Not Installed - ECP-XXX30 F/A-18 A-D Flight Control Surfaces Issues Installation Quantity: 475 Method of Implementation (Organic): Not Installed - ECP-XXX32 - F/A-18 A-D NACES Retrofit Upgrades Installation Quantity: 400 Method of Implementation (Organic): Not Installed - ECP Y557.5 Bulkhead Tub Retrofit Installation Quantity: 616 Method of Implementation (Organic): Not Installed - ECP Mod of Aircraft Ground Servicing Engine Inlet Screen Installation Quantity: 320 Method of Implementation (Organic): Not Installed - ECP JAX F NFDS mods, C&D Conversion (Blue Angels) Installation Quantity: 16 Method of Implementation (Organic): Not Installed - Archived ECPs Installation Quantity: Navy Page 10 of 126 P-1 Line #32 Volume 2-82

11 Footnotes: (1) Variants include single and dual seats, therefore some aircraft require 2 kits. (2) Other Support increases in FY16 due to significantly increased number of ECPs being managed (procured and installed). (3) Installation costs vary by FY due to different ECPs being installed. 1 / Correction of Discrepancies (OSIP 11-84) Navy Page 11 of 126 P-1 Line #32 Volume 2-83

12 Resource Summary Prior Years FY 2014 FY / Digital Communications System (DCS) (OSIP 10-99) Procurement Quantity (Units in Each) Gross/Weapon System Cost ($ in Millions) Less PY Advance Procurement ($ in Millions) Net Procurement (P1) ($ in Millions) Plus CY Advance Procurement ($ in Millions) tal Obligation Authority ($ in Millions) (The following Resource Summary rows are for informational purposes only. The corresponding budget requests are documented elsewhere.) Initial Spares ($ in Millions) Gross/Weapon System Unit Cost ($ in Dollars) tal Description: The Digital Communications System (DCS) consists of an upgraded AN/ARC-210 Receiver Transmitter (RT) (with embedded digital message transfer capability and embedded communications security) installed in the F/A-18 and integrated with the F/A-18 weapons system (mission computer, controls and displays, and communication subsystem). The DCS utilizes preformatted messages to communicate with standard United States Marine Corps, United States Navy, and United States Air Force digital communications devices to facilitate close air support, deep air strike, and tactical air control missions. Joint Staff has specified new standards for close air support platforms to address interoperability issues between air units and ground units who participate in Digitally-Aided Close Air Support missions. The requirement to meet these new interoperability standards are being satisfied with the upgrade of the DCS radio to the latest ARC-210 version, the RT-1990/RT-1990A radio. DCS reduces voice communications requirements which tend to be slow, inaccurate, and susceptible to meaconing, interference, jamming, and intrusion. DCS will enhance mission effectiveness by decreasing pilot workload which allows the pilot more time to counter increased threat capabilities (Operational Requirements Document# ). The RT-1990/RT-1990A radio also supports the North Atlantic Treaty Organization (NATO) standard anti-jam waveform, Second generation Anti-Jam Tactical UHF Radio for NATO (SATURN), and will greatly improve communication in a jamming environment as compared to current anti-jam waveforms. Finally, the next version of the ARC-210 radio, the RT-1990A will support the latest National Security Agency crypto-modernization initiative, allowing better encryption of voice and data traffic. This Operational Safety Improvement Program (OSIP) will also be used to address parts obsolescence issues and to perform non-recurring work associated with network centric operations and interoperability requirements. Current Active Modifications: Gen 5 Radio (RT-1990/A); 27C System Configuration Set (SCS); 29C SCS; H10 SCS; H12 SCS Future Modifications: KY-58M Vinson/ANDVT Cryptographic Modernization (VACM) DEVELOPMENT STATUS/MAJOR DEVELOPMENT MILESTONES: The AN/ARC-210 RT is being upgraded to a DCS RT-1990/RT-1990A. The F/A-18E/F and EA-18G DCS Close Air Support (CAS) interoperability requirements will be satisfied by retrofitting the RT-1990/ RT-1990A into Lot XXII through XXXV F/A-18E/F and Lot XXX through XXXV EA-18G aircraft under the H10 SCS. The F/A-18C/D DCS CAS interoperability requirements will be satisfied by retrofitting the RT-1990/RT-1990A into Lot VII through Lot XXI under the 27C SCS (formally known as 27X SCS). Navy Page 12 of 126 P-1 Line #32 Volume 2-84

13 Models of Systems Affected: F/A-18 and EA-18G Modification Type: CAPABILITY IMPROVEMENT Related RDT&E PEs: Procurement Financial Plan Modification Item 1 of 1: Digital Communications System (DCS) (OSIP 10-99) A Kits Recurring tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) 2 / Digital Communications System (DCS) (OSIP 10-99) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal tal Cost ($ M) 1.1.1) A-Kits Archive - Organic 483 / / - - / - - / - - / - - / - - / - - / - - / - - / - - / / Subtotal: Recurring - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / Non-Recurring 1.2.1) Installation Kits N/R - Organic - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / Subtotal: Non-Recurring - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / B Kits Recurring (4) 2.1.1) Gen 5 Radio (RT-1990/A) - Organic 104 / / / / / - 28 / / / / / / ,142 / ) 27C SCS - Organic - / / / / / - - / / - - / - - / - - / - - / - - / ) 29C SCS - Organic - / - - / - - / - - / / - - / / / - - / - - / - - / - - / ) H10 SCS - Organic - / / / / - - / - - / - - / - - / - - / - - / - - / - - / ) H12 SCS - Organic - / - - / / / / - - / / / - - / - - / - - / - - / ) B-Kits Archive - Organic 176 / / - - / - - / - - / - - / - - / - - / - - / - - / - - / / ) Prior Year Installation Costs - Organic 528 / / - - / - - / - - / - - / - - / - - / - - / - - / - - / / Subtotal: Recurring - / / / / / - - / / / / / / / Non-Recurring 2.2.1) Install Equipment N/R - Organic - / / / / / - - / / / - - / - - / - - / - - / Subtotal: Non-Recurring - / / / / / - - / / / - - / - - / - - / - - / Subtotal: Digital Communications System (DCS) (OSIP 10-99) 1,291 / / / / / - 28 / / / / / / ,329 / Subtotal: Procurement, All Modification Items - / / / / / - - / / / / / / / Support (All Modification Items) 3.1) Engineering Change Orders - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / ) Data - / / - - / - - / / - - / / - - / / / - - / - - / ) Training Equipment - / / - - / - - / - - / - - / - - / / - - / - - / - - / - - / ) Support Equipment - / / - - / - - / - - / - - / - - / - - / - - / - - / / - - / ) ILS - / / / / / - - / / / / / / / ) Other Support - / / / / / - - / / / / / / / Navy Page 13 of 126 P-1 Line #32 Volume 2-85

14 Models of Systems Affected: F/A-18 and EA-18G Modification Type: CAPABILITY IMPROVEMENT Related RDT&E PEs: Financial Plan tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) 2 / Digital Communications System (DCS) (OSIP 10-99) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal tal Cost ($ M) 3.7) Interim Contractor Support - / / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - Subtotal: Support - / / / / / - - / / / / / / / Installation Subtotal: Installation - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - - / - tal tal Cost (Procurement + Support + Installation) Navy Page 14 of 126 P-1 Line #32 Volume 2-86

15 Modification Item 1 of 1: Digital Communications System (DCS) (OSIP 10-99) Manufacturer Information Manufacturer Name: TBD Administrative Leadtime (in Months): Contract Dates Delivery Dates Manufacturer Location: TBD Production Leadtime (in Months): 2 / Digital Communications System (DCS) (OSIP 10-99) Dates FY 2014 FY 2015 FY 2017 FY 2018 FY 2019 FY 2020 Installation Information Method of Implementation (Organic): Not Installed - A-Kits Archive Installation Quantity: 483 Method of Implementation (Organic): Not Installed - Gen 5 Radio (RT-1990/A) Installation Quantity: 1142 Method of Implementation (Organic): Organic - B-Kits Archive Installation Quantity: 176 Method of Implementation (Organic): Not Installed - Prior Year Installation Costs Installation Quantity: 528 Footnotes: (4) The "Gen 5 Radio (RT-1990/A)" kits will replace the previously appropriated DCS (RT-1824) kits. Navy Page 15 of 126 P-1 Line #32 Volume 2-87

16 Resource Summary Prior Years FY 2014 FY / F/A-18 Aircraft Structural Life Management Plan (SLMP) (OSIP 11-99) CBR+ Procurement Quantity (Units in Each) Gross/Weapon System Cost ($ in Millions) 1, , , Less PY Advance Procurement ($ in Millions) Net Procurement (P1) ($ in Millions) 1, , , Plus CY Advance Procurement ($ in Millions) tal Obligation Authority ($ in Millions) 1, , , (The following Resource Summary rows are for informational purposes only. The corresponding budget requests are documented elsewhere.) Initial Spares ($ in Millions) Gross/Weapon System Unit Cost ($ in Dollars) tal Description: Incorporation of structural enhancements and changes is required to attain F/A-18 service life and maintain sufficient aircraft inventory to meet fleet operational requirements through FY Structural enhancements and changes include resolution of discrepancies identified as a result of structural test-16 and in-service experience. These Service Life Extension Program (SLEP) enhancements and changes to extend the life from 6,000 hours to 10,000 hours include: modifications to allow the entire airframe to extend flight hours; modifications to ensure structures currently limited to 78% of design life can achieve 100% life; modifications to ensure landing gear, catapult and attachment components can extend total landings. The unacceptable alternative to retrofitting would be the failure to reach full fatigue life for these aircraft and to not correct the structural defects discovered on fatigue test articles. In many cases, the mission capability of the aircraft would be adversely affected in addition to its reduced service life. As a result, aircraft may be prematurely removed from useful service. Center Barrel Replacement Plus (CBR+) is applicable to F/A-18A/B/C/Ds. Engineering Change Proposal (ECP) 904 Part 1 is the basic center barrel kit. ECP 904 Part 2 is required to extend Wing Root Fatigue Life Expended (WRFLE) and is not required for all aircraft. DEVELOPMENT STATUS/MAJOR DEVELOPMENT MILESTONES: Currently all Lot VI through XVII aircraft have 78% life limits without the structural life management plan modifications to bring them to 100% airframe life. McDonnell Douglas Corporation and Northrop Grumman Corporation developed ECP536 retrofit repair to modify these aircraft so they could restore the airframe to full life. ECP 536 was approved and validation was completed May The Fleet Readiness Center North Island developed ECP 904NI (CBR+) which was approved on 27 April 2000, ECP 904NI supersedes ECP 536. Validation started October 2000 and was completed in August Verification started August 2001 and was completed June ECP 536 moved from Operational, Safety and Improvement Program (OSIP) to OSIP in FY2002. Prior to FY14, the OSIP reflected four generic ECPs for SLEP efforts. Beginning in FY14, the budget reflects the more specific SLEP ECPs that were identified during non-recurring engineering efforts. Navy Page 16 of 126 P-1 Line #32 Volume 2-88

17 Models of Systems Affected: F/A-18 A/B/C/D Modification Type: SAFETY / LIFE EXTENSION Related RDT&E PEs: Procurement Financial Plan Modification Item 1 of 1: F/A-18 Aircraft Structural Life Management Plan (SLMP) (OSIP 11-99) CBR+ A Kits Recurring tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) 3 / F/A-18 Aircraft Structural Life Management Plan (SLMP) (OSIP 11-99) CBR+ tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal tal Cost ($ M) 1.1.1) CBR ECP 904 Part 1 (Basic) WRFLE SLEP / / / - - / - - / - - / - - / - - / - - / - - / - - / / Night Attack - NonOrganic (5) 1.1.2) CBR+ ECP 904 Part 1 (Basic) WRFLE SLEP / / - - / - - / - - / - - / - - / - - / - - / - - / - 2 / / Day Attack - NonOrganic (6) (7) 1.1.3) CBR ECP 904 Part 1 Loose parts - Organic - / - 2 / / - 21 / / - 21 / / - - / - - / - - / - - / - 23 / ) CBR+ ECP 904 Part 2 (Need Part 1) / / / - 8 / / - 8 / / - - / - - / - - / - - / / NonOrganic (8) 1.1.5) ECP 1099 NLG Retract Actuator Supports (AFC-579) - NonOrganic 1.1.6) ECP XXFCF09 Floor Segment -Fuel Bay, Ctr, Y374.8-Y453 - NonOrganic 1.1.7) ECP XXW02 Rib, Wing, Outer-Canted XW NonOrganic 1.1.8) ECP XXACF03 Plate,Structural, Aircraft- Duct,Y to Y NonOrganic 1.1.9) ECP XXACF04 Plate, Structural, Aircraft-Fus Ctr Sect, Y NonOrganic ) ECP XXW03 Spar, Wing, Outer-53.8% - NonOrganic ) ECP XXACF07 Support, Floor-Fuel Bay, Y to Y NonOrganic ) ECP XXACF08 Support,Floor-Fuel Bay,Y to Y NonOrganic ) ECP XXACF09 Longeron-Attach, Fuel Bay Floor to Keel, Y488 to Y526 - NonOrganic ) ECP XXW04 Spar Assy-Wing, Outer 68 % - NonOrganic ) ECP XXACF11 Support, Floor-Fuel Bay, Y NonOrganic ) ECP XXW01 Support, Structural Component, Aircraft-Outbd Pylon - NonOrganic 2 / / / / / - 2 / / / / / / / / - - / - 2 / / / - 47 / / / / / / / / - - / - - / - 2 / / - 2 / / / / / / / / - - / - - / - 2 / / - 2 / / / / / / / / - - / - - / - 2 / / - 2 / / / / / / / / - - / - - / - 2 / / - 2 / / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / Navy Page 17 of 126 P-1 Line #32 Volume 2-89

18 Models of Systems Affected: F/A-18 A/B/C/D Modification Type: SAFETY / LIFE EXTENSION Related RDT&E PEs: Financial Plan ) ECP XXW06 Fitting-Splice, Fwd, Spar No 1 - NonOrganic ) ECP XXW07 Splice Plate-Outbd, Lwr, Inner Wing, XW NonOrganic ) ECP XXW08 Splice Plate-Outbd, Upr, Inner Wing, XW NonOrganic ) ECP XXW09 Splice Plate-Inbd, Lower, Inner Wing, XW NonOrganic ) ECP XXW10 Splice Plate-Inbd, Upr, Inner Wing, XW NonOrganic ) ECP XXW11 Rib-Aft, Wing, Inner, XW NonOrganic ) ECP XXW12 Fitting-Splice, Aft, Spar No 1 - NonOrganic ) ECP XXW27 Spar-Fwd, Wing Panel, Inner - NonOrganic ) ECP XXW20 Spar, Wing, Outer-Intmd, No. 2 - NonOrganic ) ECP XXW21 Spar, Wing, Outer-Intermediate No. 1 - NonOrganic ) ECP XXACF13 Support, Floor-Fus Ctr Section, Y NonOrganic ) ECP XXACF14 Former,Fuselage Upr,Ctr Section Y NonOrganic ) ECP XXACF15 Former-Fus Ctr Sect, Side Hoisting, Y NonOrganic ) ECP XXACF17 Former-Fus Ctr Sect, Upper,Y NonOrganic ) ECP XXACF18 Former Segment-Fus Ctr Sect, Upper, Y NonOrganic ) ECP XXACF16 Former-Upper Segment Y NonOrganic ) ECP XXACF21 Longeron-Fus Ctr Sect, Side, Y Y NonOrganic ) ECP XXW15 Intercostal-Wing, Inner, Y NonOrganic ) ECP XXW16 Web-Intercostal, Wing, Inner, Y NonOrganic ) ECP XXW17 Intercostal-Wing, Inner, Y NonOrganic tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) 3 / F/A-18 Aircraft Structural Life Management Plan (SLMP) (OSIP 11-99) CBR+ tal Cost ($ M) tal Cost ($ M) tal Cost ($ M) tal tal Cost ($ M) - / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - 2 / / - 2 / / / / / / / / - - / - - / - 2 / / - 2 / / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - 2 / / / / / / / - - / - - / - - / - - / - - / - - / - 2 / / / / / / - - / - - / - - / - - / - - / - - / - 2 / / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / / - - / - - / - - / - - / - - / - - / - - / - 2 / / / / Navy Page 18 of 126 P-1 Line #32 Volume 2-90