Attachment_2_N0042117R0036_Section_C_ Draft_12192019.pdf

SECTION C

PERFORMANCE-BASED WORK STATEMENT (PBWS)

Distribution Statement A: Approved for Public Release Distribution Unlimited

1.0 Purpose

This PBWS defines the performance and tasking to provide Contractor Owned and Contractor Operated (COCO) aircraft and personnel to provide RS&C and Airborne TM to support a variety of testing.

2.0 SCOPE

The Naval Air Systems Command (NAVAIRSYSCOM) Program Manager Air-226 (PMA-226) CAS program provides COCO aircraft to the Department of the Navy (DoN) Fleet and Test customers. The primary mission of

Airborne Range Support Services (ARSS) is to provide RS&C and Airborne TM to support a variety of testing. This testing consists of subsurface, surface, and air testing with a number of multi-service projects for the Research, Development, Test and Evaluation (RDT&E) community at PMSR, CA.; PMRF, HI.; and Eglin Air Force Base

(AFB) Test & Training Complex, FL. During the testing and training, operations may cover a distance of several thousand square miles, whereby ships and private surface vessels need to be notified for the purpose of clearing the range.

For clarity, all references to the Federal Aviation Regulation in this PBWS will be by reference to Title 14, Code of

Federal Regulations (CFR) and abbreviated with the acronym “14 CFR”. References to the Federal Acquisition

Regulation will be abbreviated with the acronym “FAR”. When the requirements of this PBWS exceed the minimum requirements of 14 CFR, this PBWS takes precedence. Definitions contained in 14 CFR apply to all situations and conditions relating to flight operations, aircraft maintenance, and flight crew certifications.

3.0 APPLICABLE DOCUMENTS

(a) Title 14, CFR

(b) DoD 5500.7R Joint Ethics Regulation (JER)

(c) National Security Agency (NSA) Central Security Services (CSS) Policy Manual 3-16

(d) DoD 4140.25-M, Volume 2, "DoD Management of Bulk Petroleum Products, Natural Gas, and Coal, Chapter 16 Government Fuel Card Program Management Office DoD Fleet Card, Air Card and Sea Card

(e) Defense Contract Management Agency (DCMA) INSTRUCTION (INST) 8210.1C (Change 1), April 5, 2017, Contractor’s Flight and Ground Operations

(f) FAA Advisory Circular (AC) 91-91 Maintaining Public Aircraft

(g) Naval Air Instruction (NAVAIRINST) 13034.1F – NAVAIR Airworthiness and Cybersafe Process Manual

(h) United States Code (USC) Title 49 Part 830 Notification and Reporting of Aircraft Accidents or Incidents and Overdue Aircraft, and Preservation of Aircraft Wreckage, Mail, Cargo and Records

(i) 32 CFR 766 dtd 1970 Use of DoN Aviation Facilities by Civil Aircraft

(j) Air Force INST (AFI) 10-1001 Civil Aircraft Landing Permits

(k) AFI 10-1002 Agreement for Civil Aircraft Use of Air Force Airfields

(l) FAA AC 00-1.1B Public Aircraft Operations (PAO)

(m) DD Form 1149C Requisition and Invoice/Shipping Document Jan 2016

(n) DoD 5220.22-M National Industrial Security Program Operating Manual (NISPOM)

(o) 48 CFR 252.204–701(a) Safeguarding Covered Defense Information and Cyber Incident Reporting

(p) DoD Manual (DoDM) 5200.01 (DoD Information Security Program: Controlled Unclassified Information

(CUI)) Vol. 4 (enclosure 3 pages 11-18)

(q) DoD INST (DoDI) 5230.24 (Distribution Statements on Technical Documents)

(r) Homeland Security Presidential Directive-12 (HSPD-12) August 27, 2004

(s) Secretary of the Navy (SECNAV) M-5510.36 October 6, 2006

(t) National Security Decision Directive (NSDD) 298 Operations Security (OPSEC) Directive

(u) DoD INST 4715.4 Environmental Compliance at Installations Outside the United States

(v) FAA Order 8300.16 Major Repair and Alteration Data Approval/with Change 1 dated 12/7/15

(w) Military Standard (MIL-STD) 704F DoD Interface Standard: Aircraft Electric Power Characteristics

(12Mar2004)

(x) NAVAIRINST 3700.4A Safe-For-Flight Operations Certification

(y) FAR Part 31.2 Contracts with Commercial Organizations

(z) Commander, Naval Air Forces (CNAF) M-3710.7 Series – Naval Air Training and Operating Procedures

Standardization (NATOPS) General Flight and Operating INST

(aa) DoD Directive 5030.61 DoD Airworthiness Policy

(bb) Department of Defense Directive (DoDD) 5200.45 – INST for Developing Security Classification Guides

(cc) NAVAIRINST 3960.4C Project Test Plan Policy for Testing Air Vehicles, Air Vehicle Weapons, and Air

Vehicle installed Systems.

(dd) FAA AC91-70A (or as revised) Oceanic and International Operations

(ee) FAA AC91-70B (or as revised) Oceanic and Remote Continental Airspace Operations

4.0 REQUIREMENTS

The Contractor shall provide FAA certified aircraft and personnel capable of providing the services outlined below.

The Contractor shall utilize GFP and Government provided mission equipment IAW Tables 4-2 and 4-5 and CFE to meet the ARSS requirements. GFP and Government provided mission equipment will be identified at the TO level.

The Contractor shall ensure every ARSS flight has a pilot that holds, at minimum, Commercial pilot certificate with instrument rating, matching category/class rating, and a type rating (if applicable) for the aircraft IAW 14 CFR. For aircraft that require two pilots, the second-in-command pilot shall hold a commercial pilot certificate with an instrument rating and (if applicable) either a type rating or an ' Second in Command (SIC) Type Rating’ for the aircraft IAW 14CFR. All Contractor actions in execution of the contract shall be compliant with DoD 5500.7R JER.

4.1 RS&C Services

4.1.1 RS&C

i. RS&C

The Contractor shall operate its aircraft under the direction of Range Control Officer (RCO) or pre-mission instructions. The Contractor will receive an in-depth briefing and schedule upon arrival at the range from the RCO.

The contractor shall provide two aircraft for simultaneous presentations for RS&C Flights. The Contractor’s aircraft and personnel shall be capable of providing RS&C as detailed in the PBWS. The Contractor shall provide aircraft for RS&C for DoD ranges identified in individual TO’s. This tasking is an extremely high priority as it involves the safety of military, commercial, and private surface ships/vessels. The Contractor shall provide aircraft, equipment, personnel, materials, travel, per diem, and other ground and flight costs except as provided herein.

ii. Range Certification

For certification flights, NAVAIR project test plan policy applies. The offeror shall prepare a project test plan to compare platform performance characteristics against PBWS requirements. The Navy’s project test plan policy is

NAVAIRINST 3960.4C. The offeror shall assist Government personnel throughout the test plan approval process.

The offeror shall provide a final test report (IAW NAVAIRINST 3905.1A) at the conclusion of testing. The Offeror shall provide a test plan and test report to validate platform performance with required equipment to meet PBWS requirements. This plan shall provide a high-level description of the test strategy for integration, qualification, FAA

Certification Test, and performance testing to be conducted during the entire RS&C program effort. The Offeror shall describe the integration of test planning and verifiability of requirements with the systems engineering process

(CDRL A008). The Range Support Aircraft (RSA) Lead Test Engineer (LTE) will review and approve the test plan and make required coordination with the Sea Range and Targets to support the certification flights. The objective of the certification flights is to evaluate the surveillance radar using a target boat that would represent a typical small boat transiting the sea range. The aircraft will be tasked to locate contacts within the hazard pattern within the Range using standard surveillance techniques of parallel (or creeping) lines (5, 10, 15, or 20 NM separations (radar dependent)) as well as race track profiles against a surface target at beam, bow, and stern positions, at various altitudes. Aircraft and surface target positional data will be collected. The evaluation will consist of a single flight conducted in PMRF. The flight will be conducted against the High Speed Maneuverable Seaborne Target/High

Speed Maneuverable Surface Target (HSMST) and Targets of Opportunity (TOO) real world surface targets to evaluate the performance under operational conditions.

Range Certification consists of two (2) four-hour (hr.) flights for each aircraft configuration. The first flight can be completed at any time of the year, and will result in a temporary certification, which will allow the aircraft to be scheduled for PMRF operations. The second flight will be scheduled during the time of the year when sea states (the degree of turbulence at sea, generally measured on a scale of 0 to 9 according to average wave height) are typically at 4. If the offeror has more than one aircraft that are the same model with the same model radar installed, then only the first flight is required as long as one of the other aircraft has completed the second flight. The contractor shall confirm the second aircraft model and radar configuration prior to range certification. Persistence is the duration to continuously surveil an area with one or more assets.

iii. RS&C Target Identification and Communication Systems

The Contractor shall ensure aircraft with Target identification and communication systems will be used to clear the over water range at PMRF of approximately 640,000 Nautical Miles squared (NM2), and other areas as tasked. The

Contractor shall make voice communication contact with surface vessels during missions. If voice communication is unsuccessful, the RS&C aircraft will descend to make a visual identification and transmit the identification information back to the RCO.

iv. RS&C Aircraft Specifications and Requirements

The Contractor shall base aircraft at the contractor’s facility. The Contractor shall ferry the aircraft to and from mission locations. The Government will reimburse per flight minute. The flight operations required by RS&C tasking are planned to be Civil Aircraft operations and should be conducted within the 14 CFR however; the

Contractor may be required to operate in PAO status depending on the mission. The contractor shall abide by the

FAA “Public Use” notification procedures when PAO is a requirement.

RS&C Aircraft Specification and Requirements

Attribute Threshold Objective

Basing Contractors Facility N/A

Simultaneous Presentations Two (2) N/A

Mission endurance Six (6) hours N/A

Response time to Scheduling N/A N/A

Availability 95% N/A

Ceiling/Visibility Minimums for

Operation 1000 ft/3 mi

N/A

Range Certification flight Complete

(4.1.2.iii) No

N/A

Airspeed N/A N/A

Pounce Capability No Yes

Takeoff/Landing Crosswind Limits 15 knots (kts) 30kts

Persistence 6 hrs. N/A

Aircraft Range

Ability to transit between

Continental United States (CONUS) and Hawaii

N/A

Radar Coverage

Sweeps out to 80 Nautical Miles detection +/- 90 degrees from Flight

Path

N/A

Radar Coverage 80 NM wide sweep providing a 160

NM swath of coverage

N/A

Positional Accuracy of Track at

Probability of Detection Probability of

Detection (PD) Range

0.5 NM N/A

Probability of Detection (First pass) 90% 95%

Target detection 3 NM2 10 NM2 N/A N/A

Target Size 30 square meter target

150 square meter target

N/A N/A

PD Range 50 NM 80 NM N/A N/A

Sea State 3 3 N/A N/A

Surveillance Rate 8,000 NM2/hr. 12,000 NM2/hr. N/A N/A

Satellite Communications (SATCOM) No Yes N/A N/A

Vessel Classification No Yes

Maritime VHF Radio Yes N/A

Very High Frequency (VHF) radios Yes N/A

Ultra High Frequency (UHF) radios Yes N/A

UHF and VHF backup (can be single dual band radios) Yes

N/A

High Frequency (HF) radio Two (2) Per Aircraft N/A

Frequency Modulation (FM) Maritime radio Yes

N/A

Aircraft Global Positioning System

(GPS)

Yes

N/A

Automatic Identification System (AIS) Yes N/A

Table 4-1 Aircraft Specifications and Requirements

v. RS&C GFP Installation Requirements

The Contractor shall install and remove GFP listed in Table 4-2 below from aircraft as identified at the TO level.

The Contractor shall install and remove additional GFP identified at the TO level. The Contractor shall ensure that

GFP systems are installed and maintained IAW the aircraft’s airframe, engine, and avionics manufacturer’s specification. The Contractor shall provide FAA certified Airframe and Power Plant Maintenance Technicians to ensure GFP systems are installed and maintained IAW the aircraft’s airframe, engine, and avionics manufacturer’s specification.

RS&C GFP Installation Requirements

LVF10-612-(1) Dayton Granger Blade RF antenna (fixed wing CAS aircraft) operating at 433

Megahertz (MHz)

One (1) each

Large Area Tracking Range (LATR) Shipboard and Rotary Wing (RW) Technology Upgrade

(LSRTU) Specification Sheet (Reference Appendix E)

One (1) each

AT575-32_N AeroAntenna GPS https://www.aeroantenna.com/PDF/AT575-32_N.pdf One (1) each

Carry on PMRF Iridium GPS (PIGS)

One (1) each

Model 9601-DGS-LP, combined Antenna/Battery Pack Model SYN-LI-2AH

Two Kwik Tec STD-6C Suction Cup Tie Downs http://www.nalresearch.com/files/Tracking%20Modems/9601-DGS-LP/9601-DGS-

LP%20SW%20Version%201.2.0/Manuals/Product%20Information%20Model%209601-DGS-

LP.pdf

Table 4-2 PMRF/PMSR GFP Installation Requirements

4.1.2 RS&C PMSR Based Aircraft

i. RS&C

The Contractor shall operate its aircraft under the direction of RCO or pre-mission instructions. The Contractor will receive an in-depth briefing and schedule upon arrival at the range from the RCO. The contractor shall provide two aircraft for simultaneous presentations for RS&C Flights. The Contractor’s aircraft and personnel shall be capable of providing RS&C services as detailed in the PBWS. The Contractor shall provide aircraft for RS&C for DoD ranges identified in individual TO. This tasking is an extremely high priority as it involves the safety of military, commercial, and private surface ships/vessels. The Contractor shall provide aircraft, equipment, personnel, materials, travel, per diem, and other ground and flight costs except as provided herein.

ii. Range Certification

For certification flights, NAVAIR project test plan policy applies. The offeror shall prepare a project test plan to compare platform performance characteristics against PBWS requirements. The Navy’s project test plan policy is

NAVAIRINST 3960.4C. The offeror shall assist Government personnel throughout the test plan approval process.

The offeror shall provide a final test report (IAW NAVAIRINST 3905.1A) at the conclusion of testing. The Offeror shall provide a test plan and test report to validate platform performance with required equipment to meet PBWS requirements. This plan shall provide a high-level description of the test strategy to be conducted during the entire

RS&C program effort for integration, qualification, FAA Certification Test, and performance testing. The Offeror shall describe the integration of test planning and verifiability of requirements with the systems engineering process

(CDRL A008). The Range Support Aircraft (RSA) Lead Test Engineer (LTE) will coordinate the review and approve the test plan by the Navy Test and Evaluation Coordination Team (TECT) and make required coordination with the Sea Range and Targets to support the certification flights. The objective of the certification flights is to evaluate the surveillance radar using a target boat that would represent a typical small boat transiting the sea range.

The aircraft will be tasked to locate contacts within the hazard pattern within the inner sea range using standard surveillance techniques of parallel (or creeping) lines (5, 10, 15, or 20 NM separations (radar dependent)) as well as race track profiles against a surface target at beam, bow, and stern positions, at various altitudes. Aircraft and surface target positional data will be collected. The evaluation will consist of a single flight conducted in W-289 near Point Mugu. The flight will be conducted against the High Speed Maneuverable Seaborne Target/High Speed

Maneuverable Surface Target (HSMST) and Targets of Opportunity (TOO) real world surface targets to evaluate the performance under operational conditions.

Range Certification consists of two (2) four-hour (hr.) flights for each aircraft configuration. The first flight can be completed at any time of the year and will result in a temporary certification, which will allow the aircraft to be scheduled for PMSR operations. The second flight will be scheduled during the time of the year when sea states (the degree of turbulence at sea, generally measured on a scale of 0 to 9 according to average wave height) are typically at 4. If the offeror has more than one aircraft that are the same model with the same model radar installed, then only the first flight is required as long as one of the other aircraft has completed the second flight. The contractor shall confirm the second aircraft model and radar configuration prior to range certification. Persistence is the duration to continuously surveil an area with one or more assets.

iii. PMSR Aircraft Specifications and Requirements

The Contractor shall base aircraft within 50 NM from Point Mugu at a facility provided by the contractor on 1 OCT

2022 until the expiration date of the contract. The Contractor shall ferry the aircraft to and from mission locations.

The Government will reimburse flight minute. The flight operations required by RS&C tasking are planned to be

Civil Aircraft operations and should be conducted within the 14 CFR however; the Contractor may be required to operate in PAO status depending on the mission. The contractor shall abide by the FAA “Public Use” notification procedures when PAO is requirement.

RS&C PMSR Based Aircraft Specification and Requirements

Attribute Threshold Objective

Basing Contractor shall base one (1) aircraft within 50 NM from Point Mugu at a facility provided by the contractor on

1 OCT 2022 until the expiration date of the contract

N/A

Simultaneous Presentations Inner Sea Range Outer Sea Range Inner Sea Range Outer Sea Range

One (1) aircraft One (1) aircraft N/A N/A

Mission endurance N/A N/A

Response time to scheduling Within 24 Hours of Notification to the CR

N/A

Availability 95% 98%

Ceiling/Visibility Minimums for

Operation

200ft / 0.5mi N/A

Range Certification flight

Complete (4.1.2.iii)

Yes N/A

Airspeed N/A N/A

Pounce Capability No Yes

Takeoff/Landing Crosswind

Limits

15 knots (kts) 30kts

Persistence (Inner Sea Range) Inner Sea Range Outer Sea Range Inner Sea Range Outer Sea Range

4 hrs. 8 hrs. 6 hrs. 10 hrs.

Aircraft Range N/A N/A

RADAR Coverage N/A N/A

RADAR Coverage N/A N/A

Positional Accuracy of Track at

Probability of Detection (PD)

Range

0.5 NM N/A

Probability of Detection (First pass)

90% N/A

Inner Sea Range Outer Sea Range Inner Sea Range Outer Sea Range

Target detection 3 NM2 10 NM2 N/A N/A

Target Size N/A N/A N/A N/A

PD Range 20 NM 30 NM 25 NM 50 NM

Sea State 3 3 3 4

Surveillance Rate 2,000 NM2/hr. 8,000 NM2/hr. 4,000 NM2/hr. 12,000 NM2/hr.

Satellite Communications

(SATCOM)

No Yes

Vessel Classification No Yes

Maritime VHF Radio Yes N/A

Very High Frequency (VHF) radios

Yes N/A

Ultra High Frequency (UHF) radios

Yes N/A

UHF and VHF backup (can be single dual band radios)

N/A N/A

High Frequency (HF) radio Inner Sea Range Outer Sea Range Inner Sea Range Outer Sea Range

No Yes Yes N/A

Frequency Modulation (FM)

Maritime radio

N/A N/A

Aircraft Global Positioning

System (GPS)

N/A N/A

Automatic Identification System

(AIS)

Inner Sea Range Outer Sea Range Inner Sea Range Outer Sea Range

No Yes Yes N/A

Table 4-3 PMSR Aircraft Specification and Requirements

iv. PMSR GFP Installation Requirements

The Contractor shall install and remove GFP listed in Table 4-2 above from aircraft as identified at the TO level.

The Contractor shall install and remove additional GFP identified at the TO level. The Contractor shall ensure that

GFP systems are installed and maintained IAW the aircraft’s airframe, engine, and avionics manufacturer’s specification. The Contractor shall provide FAA certified Airframe and Power Plant Maintenance Technicians to ensure GFP systems are installed and maintained IAW the aircraft’s airframe, engine, and avionics manufacturer’s specification.

RS&C GFP Installation Requirements

LVF10-612-(1) Dayton Granger Blade RF antenna (fixed wing CAS aircraft) operating at 433 Megahertz

(MHz)

One

(1) each

Large Area Tracking Range (LATR) Shipboard and Rotary Wing (RW) Technology Upgrade (LSRTU)

Specification Sheet (Reference Appendix E)

One

(1) each

AT575-32_N AeroAntenna GPS https://www.aeroantenna.com/PDF/AT575-32_N.pdf

One

(1) each

Carry on PMRF Iridium GPS (PIGS)

One

(1) each

Model 9601-DGS-LP, combined Antenna/Battery Pack Model SYN-LI-2AH

Two Kwik Tec STD-6C Suction Cup Tie Downs http://www.nalresearch.com/files/Tracking%20Modems/9601-DGS-LP/9601-DGS-

LP%20SW%20Version%201.2.0/Manuals/Product%20Information%20Model%209601-DGS-LP.pdf

Table 4-2 PMRF/PMSR GFP Installation Requirements

4.1.3 Airborne TM Services

i. Missile TM

The Contractor shall provide an aircraft to support TM events utilizing a GFP TM system. The Contractor shall ensure the aircraft is capable of detecting, tracking, recording, and retransmitting the TM stream from a long-range, all-weather, subsonic cruise missile. The Contractor shall provide aircraft, equipment, personnel, materials, travel, per diem, and other ground and flight costs except as provided herein. The Contractor shall receive an in-depth briefing and schedule upon arrival at the tasked agencies site from the RCO. The Contractor shall coordinate with the RCO for guidance and any additional actions. The testing consists of subsurface, surface, and air testing with a number of multi-service projects for the RDT&E community at the PMRF, PMSR, and Eglin Air Force Base, Florida. During the testing/training, operations may cover a distance of several thousand square miles, whereby ships and private surface vessels need to be notified for the purpose of clearing the range.

ii. Raytheon Ktech Telemetry System (RTMS)

The Offeror shall provide a Test Plan and Test Plan Report to validate platform performance with required GFP to meet requirements. This plan shall provide a high-level description of the test strategy for integration, qualification, FAA Certification Test, and performance testing to be conducted during the RTMS capability establishment period.

The Offeror shall describe the integration of test planning and verifiability of requirements with the systems engineering process (CDRL A008).

a. The purpose of the tests is to certify capability of the TM system installed in contractor’s aircraft.

This system will be tested on the ground and in flight by contractor personnel. The ground tests will include a functionality test, telemetry data reception and tracking (single stream), and a ground

Electromagnetic Compatibility (EMC) Safety of Flight (SOF) test with engines turning. The flight portion will test the system for detection, acquisition, and tracking of Pulse Code

Modulation/Frequency Modulation (PCM/FM) and Shaped Offset Quadrature Phase-Shift Keying -

Telemetry Group (SOQPSK-TG) modulated telemetry sources. Testing will evaluate acquisition range at both low and high data rates in both modulations.

b. RTMS functional testing will commence by evaluating proper RTMS interface, specifically between the nose-mounted telemetry antenna and the telemetry equipment located in the racks.

c. The ground test will evaluate the functionality of the RTMS and if it performs as intended prior to flight test. The sequence of events is as follows: system functionality check, Hazards of

Electromagnetic Radiation to Personnel (HERP) measurement on the re-transmitting system, and ground EMC.

d. Flight test will evaluate max detection range and auto track performance of the RTMS and functionality of RTMS’s subsystems. Flight test will commence after ground tests of RTMS equipment on contractor aircraft have been successfully completed.

e. The exit criterion for these tests is to evaluate RTMS performance and its subsystems functionality.

Contractor shall conduct the test and provide NAVAIR with a data package of test results for review and evaluation of the RTMS ability to detect, track, record, and re-transmit RTMS data (CDRL

A008).

f. Raytheon Ktech Telemetry System (RTMS) Capabilities Interface Reference Document (IRD) is provided as Attachment (3). L and S band array dimension provided as Attachment (4).

iii. Aircraft Personnel

The contractor shall provide flight crews that are trained, qualified, and scheduled IAW Tittle 14- Aeronautics and

Space, CFR Part, 61, 141 and Part 135, Operating Requirements. (1) PIC, (1) SIC and (3) TM Mission Planning and Analysis operators shall be trained, qualified, and current in accordance with the contractors Government

Flight Representative (GFR) approved Training program, prior to conducting a government contracted flight.

iv. Communication

The Contractor shall ensure the aircrew will communicate with the Test Conductor on an assigned VHF or UHF frequency designated by the Range Officer.

v. TM aircraft Specifications and Requirements

The Contractor shall base aircraft at the contractor’s facility. The Contractor shall ferry the aircraft to and from mission locations. The Government will reimburse flight minutes. The flight operations required by TM tasking are planned to be FAA Civil Operation approved via STCs, or 8110-3s and 337s when flying in support of Government

Contracts and shall be conducted within the 14 CFR however; the Contractor may be required to operate in PAO status depending on the mission. The contractor shall abide by the FAA “Public Use” notification procedures when

PAO is requirement. The Contractor shall ensure the aircraft will be capable of maintaining proper situational awareness during a mission to ensure de-confliction with chase aircraft and proper positioning to support its TM relay function.

Table 4-4 TM Services Specification and Requirements

vi. TM GFP Installation

The Contractor shall install and remove GFP listed in Table 4-5 below from aircraft as identified at the TO level.

The Contractor shall install and remove additional GFP identified at the TO level. The Contractor shall provide FAA certified Airframe and Power Plant Maintenance Technicians to ensure GFP systems are installed and maintained

IAW the aircraft’s airframe, engine, and avionics manufacturer’s specification.

TM GFP Installation Requirements

Raytheon Ktech Telemetry System (RTMS) One (1) each

The rack assembly consists of three populated racks, a plate to which the racks are pinned, and a pallet to which the pallet plate is attached. The racks are designed and fabricated by Platform Systems, Inc. and are all structurally the same. They are approximately 53.0” tall, 22.1” wide, and 33.5” deep. The racks are stiffened using diagonal struts (2 on each side of each rack). Appendix D Figure 1 shows the populated equipment racks.

The racks will be referred to by numbers 1, 2, 3 reference Appendix D Figure 3, 4, 5). Rack #1 is the heaviest rack weighing approximately 388 lbs. and also has the highest vertical center of gravity (CG) location. Though the racks are tied together at the tops of the racks (reference Appendix D Figure 1), the final configuration shall depend on the contractors technical proposal. Raytheon Ktech Telemetry System (RTMS) Capabilities Interface

Reference Document (IRD) is provided as Attachment (3). L and S band array dimension provided as

Attachment (4)

Airborne pedestal One (1) each

Array antennas (L band and S band) One (1) each

Antenna Control Unit (ACU) One (1) each

TM equipment racks Three (3) each

TM operator seat Two (2) each

TM Recorder seat One (1) each

Carry on PIGS; Model 9601-DGS-LP, combined Antenna/Battery Pack

Model SN-LI-2AH ; Two Kwik Tec STD-6C Suction Cup Tie Downs One (1) each http://www.nalresearch.com/files/Tracking%20Modems/9601-DGS-LP/9601-DGS-

LP%20SW%20Version%201.2.0/Manuals/Product%20Information%20Model%209601-DGS-LP.pdf

Attribute Threshold

TM Flights One (1) Aircraft

TM Stream

S-band frequency, Pulse Code Modulation (PCM)/FM, with a data rate of at least

2.5 Megabits per second (Mbps) transmitted from a 5 watt transmitter on the missile

Bit Error Rate (BER) 1E-6 or better

Range 5 NM or greater

Geometry TM

TM from a missile transiting from the Florida Keys to Eglin AFB, FL at 0.75M and

15,000 feet MSL can be relayed to TM receivers at Homestead AFB or Cape San

Blas, FL for the entire transit

Reradiate Signal/Altitude

Reradiate a signal emanating from the surface for submarine-launched long-range, all-weather, and subsonic cruise missile. The Contractor shall ensure an threshold altitude of 25,000 ft. MSL and an objective altitude of 38,000 ft. MSL .

Time on Station 4 Hrs.

Power 115 VAC Mission Power to power the airborne telemetry system equipment.

VHF radios One (1) each

UHF radios One (1) each

UHF and VHF backup

(can be dual band radios) One (1) each

HF radio Two (2) each

Aircraft GPS One (1) each

Table 4-5 TM GFP Installation Requirements

4.1.4 Aircraft Mission Profiles

The aircraft mission profiles below are representative of typical operations conducted in a RS&C and Airborne TM environment. The Contractor shall provide aircraft capable of meeting the mission criteria provided below and IAW aircraft requirements in PBWS. Specific RS&C and Airborne TM mission scenarios are subject to change based on the mission profiles at the request of the customer.

Aircraft Mission Profiles (STANDARD DAY)

PMRF Profile

Day 1 Depart contractor’s facility and ferry aircraft to PMRF Barking Sands, Kauai.

Day 2 Attend test exercise briefing/scheduling meeting

Day 3 No-Fly/Standby

Day 4 Fly mission rehearsal flight

Day 5 No-Fly/Standby

Day 6 No-Fly/Standby

Day 7 Fly RS&C mission

Day 8 No-Fly/Standby

Day 9 Back up flight date

Day 10 Back up flight date

Day 11 Return ferry to contractor’s facility

PMSR Profile

Typical duration of mission profiles are visually represented in Appendix C (PMSR Outer and

Inner Sea Range)

Short duration mission profile (estimated 20% of the time); Duration: 4 hours RS&C the hazard area; Number of aircraft: One (1)

Medium duration mission profile (estimated 20% of all required sorties); Duration: 4-6 hours

RS&C the hazard area (referenced as red hatched area in figure 3)

Number of aircraft: One. The Government may request in advance a second aircraft due to the size of the hazard area.

Max duration mission profile (estimated 60% of all required sorties); Duration: 6-10 hours

RS&C the hazard area (referenced as yellow hatched area in figure 3)

Number of aircraft: Two (2).

Table 4-6 Aircraft Mission Profiles (Standard Day)

4.2 Contract Administration

4.2.1 Contractor’s Progress, Status and Management Report (CDRL A004)

Contractor’s Progress, Status and Management Report (CDRL A004) The Contractor shall track flight minutes, summary information, and detachment data associated with each corresponding CLIN and other data as outlined in (CDRL A004).

4.2.2 Post Award Conference (PAC)

The Contractor shall host a PAC with the Government no later than 30 days after contract award at the Contractor’s location. The PAC agenda must be established following contract award and is intended to orient both Government and Contractor personnel with contract requirements, schedule, and baseline expectations. The PAC must be conducted IAW FAR Subpart 42.5.

4.2.3 Program Management Reviews (PMR) and Report, Record of Meeting/Minutes (CDRL A007)

The Government will schedule and conduct PMRs on a semiannual basis at NAVAIRSYSCOM PMA-226, Cherry

Point, North Carolina, the Contractor’s facility, or other locations as directed by the COR. The Contractor shall attend all PMRs with appropriate personnel to make a presentation consisting of the following:

i. Overview of the work accomplished to date or since last review, the projected plan of action for completion of contract effort, and handout material documenting presentations.

ii. Identification and discussion of problems encountered, if any, and action taken to resolve the problems.

iii. Identification and discussion of issues, risks and the Contractor’s plan of action for mitigation.

The Contractor shall also:

i. Address its experience working as a team with the other CAS Contractors and the Government, identifying opportunities, successes and areas needing improvements.

ii. Record meeting minutes and actions.

4.2.4 Contractor Management Plan (MP) (CDRL A002)

The Contractor shall provide a Contractor Management Plan (MP) and Standard Operation Procedures (SOP) within

30 days of contract award that describes the Contractor’s organization, management procedures and modification schedules that are established for the initiation, monitoring, control and completion, test and verification, and reporting of contractual requirements to complete the tasks outlined in this PBWS and IAW (CDRL A002).

4.2.5 Fixed Rate Fuel Management

4.2.5.1 Fuel and Fuel Chits (CDRL A003)

This is a “dry” contract. The Government will provide access to fuel at United States Military Airfields and civil fields. The Government will provide appropriate fuel cards for each of the Contractor’s aircraft. All fuel purchased by the Contractor should be obtained from a military base whenever possible. Whenever non-contract fuel needs to be obtained from a civilian airport, the Contractor shall record the circumstances and justification IAW the DoD

4140.25-M. Commercial non-contract fuel must only be used by exception with SO or COR advance approval.

i. The Contractor shall not use any Government provided fuel for any flight other than those scheduled under this contract.

ii. The Contractor shall provide Fuel chit in legible form to identify date/time of purchase, s/n of the aircraft, contract number, and mission number from the flight schedule, which track all fuel consumption and provide fuel receipts, flight logs, and Fuel Reports to the Government IAW (CDRL

A003).

4.2.5.2 Fuel Card Training

The Contractor shall complete fuel card training IAW DoN Consolidated Card Program Management Division

(CCPMD) at least 30 days before first flight. All users of the AIR cards (pilot’s/flight commander’s/aircraft commander’s/crew chiefs) must perform DoN role-based refresher training every 2 years. Common Access Cards

(CAC) are required to register for training via the CCPMD website. For Contractors new to this site, the Contractor shall register its CAC the first time to access the site. The CCPMD training system uses the email associated with the Contractor’s CAC when registering completion of training to get a certificate. All Contractor fuel card users shall:

i. Register the CAC at: https://www.navsup.navy.mil/registration

ii. Register for and complete the Card User Certification Course via CCPMD home portal -https://my.navsup.navy.mil/webcenter/portal/ccpmd and select Air Card or go directly to Air Card training at https://my.navsup.navy.mil/webcenter/portal/ccpmd_ac/Training

iii. Complete the Online Certification

iv. Print the Certificate of completion and provide a copy to the COR within five working days, to be kept on file.

v. Contract users shall sign a Card User Statement of Understanding (SOU) after conducting training and provide a copy to the COR within five working days.

4.2.6 Mishap Response Plan (MRP) for Accidents and Incident Reporting

As required by DCMA INST 8210.1C , the Contractor shall report all aircraft accidents and incidents to include all air, ground mishaps and Occupational Safety and Health Administration (OSHA)/Safety violations, IAW its GFR approved MRP, Ground Operations Procedures (GOP) and Flight Operations Procedure (FOP). The Contractor shall immediately contact the local base Commanding Officer or Command Duty Officer or the officer conducting the exercise, as applicable and the COR. Leaving a voicemail alone is not sufficient. PMA-226 incident reporting phone numbers will be provided at award. Accident/Damage reports, at a minimum must be marked FOR OFFICIAL USE

ONLY (FOUO) or classified IAW the appropriate security classification guide.

https://www.navsup.navy.mil/registration https://my.navsup.navy.mil/webcenter/portal/ccpmd https://my.navsup.navy.mil/webcenter/portal/ccpmd_ac/Training

i. MRP Exercise: The Contractor shall exercise the MRP on an annual basis. As a minimum, this plan shall include the following procedures that conform to USC Title 830 National Transportation Safety

Board (NTSB).

ii. Immediate action checklist to ensure command, control, and coordination of the rescue or recovery effort.

iii. A notification plan which includes a current roster of Contractor and Government personnel

(including duty and non-duty phone numbers) to be notified in the event of an aircraft mishap

iv. Procedures for Contractor and subcontractor cooperation and participation in mishap investigations conducted by the Government. Procedures shall clearly define the differences between a Government legal investigation (used to satisfy claims) and a Government Safety investigation (used for mishap prevention).

v. The procedures shall clearly state the contractual obligation of Contractor personnel to provide information and participate in interviews by the Government safety investigation immediately upon request.

vi. The Contractor shall have procedures that require aircrew medical and toxicological testing immediately following a mishap.

vii. The toxicological samples shall be provided to the Government legal investigation board immediately upon request.

viii. The results of medical and toxicological testing shall be provided to the Government safety investigation board immediately upon request.

4.2.7 Waiver Requests

Each aircraft used in the performance of this contract must be operated and maintained IAW 14 CFR and its

NAVAIR IFC. If, in the performance of this contract, for any reason a contract requirement cannot be met, the

Contractor shall notify the PCO and the COR, and obtain approval from the GFR, prior to conducting operations.

The waiver request must cite the specific requirement that cannot be adhered to IAW DCMA INST 8210.1C.

4.3 Aircraft Certification (AC), Maintenance Practices and Operating Procedures

Aircraft must be certified, maintained and operated IAW 14 CFR and its NAVAIR IFC, with particular attention to the following areas:

AC 91-91 – Maintaining Public Aircraft

Part 21 – Certification Procedures for Products and Parts

Part 43 – Maintenance, Preventive Maintenance, Rebuilding and Alteration

Part 91 – General Operating and Flight Rules

Part 135 - Air Carrier and Operator Certification

4.3.1 FAA Airworthiness and Related Substantiation Data (CDRL A001)

Aircraft must possess a current FAA Airworthiness Certificate prior to the end of the standup capability period. The

Contractor shall provide a copy of FAA certificates and all other related airworthiness substantiation data for each aircraft within 30 calendar days of contract award and as generated or requested per (CDRL A001). The Contractor shall comply with all Airworthiness Directives (AD) and service bulletins must be evaluated for airworthiness and safety.

4.3.1.1 FAA Standard Airworthiness Certificates

For aircraft with FAA Standard Airworthiness Certificates, the Contractor shall maintain the aircraft IAW 14 CFR.

The Contractor shall secure FAA approval for each change to the configuration that is not defined in the aircraft’s

Airworthiness Certificate before the change is used in support of this contract. For each such modification, the

Contractor shall secure and provide the valid FAA-approved data within 15 days of contract award and as generated or requested (CDRL A001). For Type Certificated aircraft, if this data references FAA regulations as the standard, the Contractor shall provide Approved Data as defined in the FAA Order 8300.16 for any major alteration or major repair. Major alterations to aircraft with Standard Airworthiness Certificates shall have been certified as airworthy and properly documented using FAA Form 337 signed in blocks six (6) (Conformity) and seven (7) (Return to

Service) by persons authorized under 14 CFR § 43, and citing FAA Approval Data. The FAA may only certify modifications relating to powered systems for captive carriage if the operation of that system in not considered commercial purposes, per 49 USC § 40125.

4.3.1.2 FAA Special Airworthiness Certificates

For aircraft with FAA Special Certificates, the Contractor shall provide the Program Letter (PL) submitted to the

FAA for application of the airworthiness certificate used in support of this contract or latest PL associated with the current airworthiness certificate and the special certificate with the restrictions levied by the FAA. Under this certificate, the aircraft must be maintained IAW the operating limitations issued as part of that certificate. For each subsequent aircraft modification deviating from the FAA issued certificate, the Contractor shall secure and provide an updated FAA airworthiness certification, and associated operating limitations (CDRL A001), before the modification is used in support of this contract. Where the modification is a Major Change, as defined by 14 CFR, the Contractor shall provide the PL and secure the FAA's determination regarding the need for a new or amended certificate. (CDRL A001). All major alterations incorporated before contract award and during contract execution shall have sufficient data to determine that the equipment or provisions for the equipment meet the applicable civil, Original Equipment Manufacturer (OEM), Military Standard (MIL-STD), or some other recognized engineering substantiation data, for the type of aircraft concerned. Unless directed otherwise by the Government, the Contractor shall remove any major alteration incorporated before contract award that was not certified as airworthy by an appropriately rated FAA certified mechanic, aircraft manufacturer or repair station.

4.3.1.3 NAVAIR Airworthiness

i. Aircraft under this contract are planned to be Civil Aircraft operations and should be conducted within the 14 CFR regulations; however, the Contractor may be required to operate in PAO status depending on the mission.

ii. For aircraft under this contract requiring a NAVAIR issued IFC (See NAVAIRINST 13034.1F), the

Contractor shall provide airworthiness substantiation data IAW this PBWS, (CDRL A001).

iii. The Contractor shall notify the COR and the GFR of any proposed changes to the aircraft configuration, FAA certificate status, or operating limitations and procedures so an assessment of the changes can be made and modified IFC issued, if warranted. In addition, the Contractor shall provide airworthiness substantiation data IAW (CDRL A001).

Navy Airworthiness Support Data

4.3.1.3.1 The Contractor shall provide a single point-of-contact to manage the airworthiness certifications and to coordinate Contractor and Government certification efforts during the Stand-up phase of each Aircraft Type or during any significant aircraft modification requiring a new or updated NAVAIR IFC.

4.3.1.3.2 All aircraft under this contract require a NAVAIR issued IFC (NAVAIRINST 13034.1F). The Contractor shall provide airworthiness substantiation data IAW this PBWS, CDRL A001 and as required by NAVAIR. To ensure timely IFC release required to conduct PAO mission, aircraft must be fully operational and all substantiation data shall be provided at least thirty (30) days prior to required mission.

4.3.1.3.3 For all aircraft operating under a NAVAIR IFC, the Contractor shall notify the Contracting Officer’s

Representative (COR) of any proposed changes to the aircraft configuration, FAA certificate status, or operating limitations and procedures so an assessment of the changes can be made and a modified NAVAIR IFC issued, if warranted. In addition, the Contractor shall provide airworthiness substantiation data IAW CDRL A001 for the proposed change.

5.0 Operational Requirements

5.1 Mission Planning

Under the Commander, NAVAIRSYSCOM, PMA-226 is the overall CAS Program Manager. Depending on the mission and the customer, PMA-226 will designate SO to execute administrative tasks such as mission scheduling and coordination, and invoice certification. The CR shall coordinate with the Scheduling Officer (SO) on all formal requests for services to determine feasibility of support, associated cost of support, implications of support on other scheduled or potentially scheduled mission and any other necessary details requiring coordination. The Contractor shall provide a CR to contact, to cover scheduling 24 hours per day/seven days a week. Notwithstanding other directives of this PBWS, flight operations may be scheduled at any time, 24 hours a day/seven days a week, subject to a minimum mission flight time. Scheduled and planned maintenance requirements that may preclude aircraft availability should be coordinated as far in advance as possible with the SO so that supportable commitments can be adjusted. As soon as it is determined that missions cannot be met, the Contractor shall inform the Government if any aircraft are not able to meet assigned or future missions, via email to the COR. Pilot mission briefs are held prior to mission execution and will include detailed information for mission profile execution. The Contractor shall coordinate ground and flight crew daily schedules as necessary to meet the operational tasking of the SO.

5.1.1 SO Communications with Contractor

i. The Contractor shall designate a CR to coordinate with the SO.

ii. The designated SO is the PMA-226 Project/flight Schedule manager at Naval Air Station (NAS)

Patuxent River, Maryland.

iii. The SO and CR will communicate as often as required, but not less than once per month, to develop short and long range schedules and identify potential aircraft scheduled maintenance. This scheduling includes planned operations and required mission support personnel. Special scheduling arrangements or considerations may be made to ensure Contractor’s maintenance requirements.

iv. The Government reserves the right to cancel or not schedule flight services on any given day of detachment operations.

v. If an additional, unscheduled mission is tasked and there are no aircraft currently in an operational status with pilots, the Government will give the Contractor as much advance notice as possible for additional tasking before cancelling the event. Notwithstanding other directives of this PBWS, the

Contractor shall fulfill all missions ordered by the Government with at least 14 days prior notice.

5.1.2 Authorization of Flight Operations

All flight operations must be authorized through the SO, approved by the GFR and communicated to the CR by designated TO.

5.1.3 Released by the Government

When all flights for detachment operations have been completed, the SO will notify the CR, via email, that the deployment is complete. Following this notification, the CR shall complete and implement arrangements to return the aircraft, personnel, and equipment to the home base.

5.2 Basing

The Contractor shall ferry the aircraft to and from mission location with the exception of one aircraft based within

50 NM of Pt Mugu in support of PMSR.

i. For PMRF the Contractor shall base aircraft at the contractor’s facility.

ii. For PMSR the Contractor shall base one (1) aircraft within 50 NM from Point Mugu at a facility provided by the contractor.

iii. For TM the contractor shall base aircraft at the contractor’s facility

5.3 Mission Coordination

5.3.1 Mishap Prevention and Aviation Safety Program

The Contractor shall establish and maintain an Aviation Safety and Mishap Prevention Program and ensure it is reviewed by all crewmembers on an annual basis IAW DCMA INST 8210.1C.

5.3.2 Aviation Safety Official

i. The Contractor shall designate an Aviation Safety Official with specific duties and responsibilities defined IAW DCMA INST 8210.1C.

ii. The Contractor shall establish and maintain an Operational Risk Management (ORM) Program, IAW

DCMA INST 8210.1C (Change 1) and the MRP. Per DCMA INST 8210.1C, the Contractor shall establish and execute written procedures for responding to an aviation incident or accident as part of the MRP. The Contractor shall deliver all Accident and Incident reports to PMA-226 per its MRP. In addition to safety and reporting requirements outlined in PBWS paragraphs 4.2.6, 5.3.1, 5.4 and 6.5, the MRP must establish policies, responsibilities, and actions to be initiated if any aircraft becomes overdue from its active Flight Plan. The Contractor shall conduct an exercise of the MRP on an annual basis. In addition to the requirements of DCMA INST 8210.1C , the Contractor shall also establish procedures which conform to USC Title 49 Chapter 8 Part 830 NTSB.

5.3.3 Transient Military Aircraft

When in support of scheduled missions, aircraft provided under this contract are considered transient military aircraft and not subject to landing fees at DoD controlled airfields.

5.3.4 Civil Aircraft Landing Permits

The Contractor shall submit DD Form 2400 - Civil Aircraft Certificate of Insurance, DD Form 2401-Civil Aircraft

Landing Permit and DD Form 2402-Civil Aircraft Hold Harmless Agreement, IAW 32 CFR 766, to the COR. These agreements must be kept current during the entire ordering period under the contract. Landing permits shall be issued by the specific services office responsible for issuance of such permits for landing at CONUS/ Outside

Continental United States (OCONUS) USN, United States Marine Corps (USMC) and United States Air Force

(USAF) airfield facilities all, without restriction, to include the purchase of USG fuel, and support services on a not-to-interfere basis. USAF landing permits will comply with AFI 10-1001 Civil Aircraft Landing Permits and AFI 10-

1002 Agreement for Civil Aircraft Use of Air Force Airfields.

5.3.5 Maintenance Program

The Contractor shall maintain aircraft used in the performance of this contract IAW 14 CFR, its NAVAIR IFC, and this PBWS.

The Contractor shall manage remaining fatigue life to allow the aircraft to be safely operated throughout the ordering period of the contract and provide fatigue life status as part of configuration management in the MP (CDRL

A002).

The Contractor shall provide a list of all categories of parts with OEM defined life limits, and define in the MP, the path for replacing those parts on/before the required dates (CDRL A002).

5.3.6 Aeronautical…