Attach 1 - ODA STC Contract PWS_210318_Final.pdf

U.S. DOT Federal Aviation Administration

PERFORMACE WORK STATEMENT

Supplemental Type Certificate (STC) Development and Certification and

Associated Project Management

March 18, 2021

Version 8.0

Performance Work Statement i

Table of Contents 1 Introduction

1.1 Background 1

1.2 Scope of Work 1

2 Task Requirements

2.1 Task 1 – STC Certification of modifications on CL605/650 aircraft 2

2.1.1 Subtask 1.1 – Challenger Certification Support 2

2.1.2 Flight Inspection System/Modular Mission System 3

2.1.3 Modification of Challenger 605/650 Aircraft 4

2.2 Task 2 STC Certification of BE300/BE350ER/BE360ER 5

2.3 Milestones 6

2.4 Subtask 1.3 - Project Management 7

2.4.1 Monthly Status Reports (CDRL A001) 7

2.4.2 Subtask 1.6 - Monthly Financial Reports (CDRL A002) 8

3 End Results/Deliverables

5 Period of Performance

6 Place of Performance

7 Travel

8 Over and Above

9 Qualifications

9.1 Organizational Qualifications 10

9.2 Labor Category Qualifications 10

9.2.1 ODA Administrator 10

9.2.2 ODA Unit Members 11

9.2.3 Project Manager 11

10 Other Requirements

Appendix - Power Requirements Reference …...A-1

1 Introduction The Federal Aviation Administration (FAA) Flight Program Operations (AJF) performs multiple missions that require airborne operations, including: Aviation Safety Training (AST); Flight Inspection (FI); Research, Development, Test and Evaluation (RDT&E) support; and Critical Event Response/Transportation.

AJF requires services to accomplish the certification of aircraft modifications and associated project management. The contractor is required to have access to a valid Organization Designation Authorization (ODA) to provide Supplemental Type Certificate (STC) services for modifications to FAA aircraft throughout the performance period of the contract. The work will primarily be accomplished in Oklahoma City, OK or Atlantic City, NJ. Work may also be accomplished at a site selected by the contractor when direct access to the aircraft is not required.

1.1 Background

FAA Flight Program Operations (AJF) maintains and operates a fleet of aircraft in accordance with 14 CFR Part 135 operating. The FAA has an engineering staff that will work with the Contractor to develop the modifications. The Flight Program Operations Aircraft Maintenance Directorate will execute the modification and installation.

The flight inspection mission requires specific equipment to measure signals in space for the flight inspection of Navigational Aids (NAVAIDS), Instrument Flight Procedures (IFP), surveillance systems, lighting systems, and communication systems. The Flight Inspection System (FIS) being developed by the FAA will be called the Modular Mission System (MMS).

The MMS is removable and will allow the aircraft to be placed in different mission configurations. The FIS consists of the MMS equipment rack and operator console, along with various aircraft sensors and antennae.

1.2 Scope of Work

AJF requires contract ODA support for the execution of STC approval authority to develop and install the MMS on FAA aircraft, related engineering support, and project management of related projects. AJF requires certification for expected modifications on the Challenger 605/650 Series aircraft with an option for modifications to BE300 and BE350ER/BE360ER aircraft.

A technical interchange meeting to discuss the certification processes that will be implemented between the contractor and FAA engineering.

The authorization to issue STCs on CL605/650 and BE300/350ER/360ER is required before contract award.

The technical details in this PWS are a representative scope of the technical requirements although changes are expected during the Preliminary Design Review (PDR) process.

The contractor will develop the plan of action and a schedule that addresses identified milestones for STC development and aircraft modifications in cooperation with the FAA Engineering.

FAA aircraft are equipped with military grade avionics and equipment. Therefore, modifications involve the Military Certification Office (MCO). For this reason, the contractor will be required to make the STC application through the MCO. The ODA Organization Management team (OMT) will be advised and included in all correspondence related to the project. The contractor must supply their ODA Manual procedures for making application to the MCO for STC projects.

STC certifications for Challenger 605/650 aircraft will be required in the Base Year. STC certifications for the BE300/BE350ER/BE360ER aircraft will not be required in the base year, but will be required for the option years.

• Task 1: STC Certification for Challenger 605/650 aircraft

• Task 2: STC Certification BE300/BE350ER/BE360ER aircraft

• Task 3: Project Management

2 Task Requirements The FAA (COR) will provide the Contractor with direction on and approval of work on specific actions in coordination with AJF engineering. The Contractor must hold its employees responsible for confirming and abiding by their appropriate chain of command for performing work under this PWS.

The Contractor must hold a valid ODA and operate in compliance with FAA Order 8100.15 (current edition). AJF requires STC certification services on aircraft certified under 14 CFR Part 23 and 14 CFR Part 25. The contractor must have authority to issue STC’s on CL-605/650 and BE300/BE350ER/BE360ER. Contractor must demonstrate previous STC certification on part 25 75,000 lbs. MTW or less; and Part 23 12,500 lbs. MTW or less within the last 5 years from proposal date.

The initial STC for the CL605/650 aircraft must be completed within 6 months from award. FAA recognizes the timeline may be extended if issues arise that are beyond the offeror’s control.

2.1 Task 1 – STC Certification of modifications on CL605/650 aircraft

2.1.1 Subtask 1.1 – Challenger Certification Support

The contractor will perform identified tasks efficiently, accurately, on time, and in compliance with the requirements. The Contractor must participate as a member of a Government-led team as requested by the COR. The Contractor will participate in a Kick-Off meeting between the FAA Stakeholders, COR, and Contractor to review PWS requirements and understand work scope and deliverables. The Contractor must prepare and submit meeting minutes to the FAA that capture the discussions and understandings from the Kick-Off meeting. The Contractor must have the authority and ability to exercise the following functions:

• Outline the preliminary certification basis and methods of compliance

• Project manage the project to meet desired milestones

• Review and approve technical data and find compliance to the airworthiness standards

• Issue required STCs and amendments

• Issue airworthiness certificates and approvals

• Establish conformity of articles including test articles

• Determine conformity of test setup

• Determine conformity of installations of articles, including Type Inspection

Authorization (TIA) inspections on a product

• Perform compliance inspections

• Approve data for major alterations or major repairs

• Perform review and obtain acceptance of Instructions for Continued Airworthiness

2.1.2 Flight Inspection System/Modular Mission System (MMS)

The MMS is planned for installation in Challenger 605/650 aircraft, and in the B300/BE350ER/BE360ER aircraft. The MMS will be a removable system, so the aircraft can be readily adapted to other configurations that meet all FAA Flight Program mission requirements.

When MMS is deployed, the system will serve as a platform for the flight inspection and research, development, test and evaluation support missions.

The contractor will test, and/or confirm, as appropriate all parts and assemblies to show compliance to all applicable FAA requirements.

2.1.2.1 Modular Mission System Details:

• Mission Console, to include:

o General Micro System (GMS) Computer o Primary single monitor o Cortron keyboard/trackball o Comm control panel o Comm #4 Radio Tune Head (Gables) o Audio Control Panel (Becker) o Oxygen Mask connected to Comm o On Path & On Course Annunciators o Remaining Annunciators (1) Workstation Power, (2) Cabin WiFi (3) Mask

Mic, (4) Interphone Tie o Miscellaneous USB connectors, terminal rails/blocks, Ethernet jacks, PTT switch, dim control

• Mission Rack, to include:

o EDS-300 (TACAN/DME Pulse Analyzer) o Wifi o (not required to be listed - included in Flex module connector)Ethernet

Switch (Parvus 20-10) o AB3142 (Ballard Data Collector) o EVSF-1000 (Qty 2 - Nav/Marker/GBAS/Spectrum Analyzer Rcvrs) o Comm #4 transceiver (Genesys) o IRIG Timing o FIS GNSS (Trimble BX992) o Coaxial Switching o Coaxial Splitters o Circuit Breaker Panel/Box (All 28VDC) Laser Alt GMS Computer Monitor Ethernet Switch Panel Lighting Data Collector

EVSF-1000 #1 NAV

EVSF-1000 #2 NAV

EDS-300 DME/TAC

FIS GNSS (Trimble BX992) Data Link Cabin Wifi VersaSync IRIG Timing TVPS Camera DF Receiver DIGAR USB Charging Ports Relays & Misc Aux 28VDC MISC Laser Alt, Comm #4 CTRL Comm #4

2.1.2.2 Power Requirements

See Appendix A

2.1.3 Modification of Challenger 605/650 Aircraft

Modification of the aircraft must be compatible with the installation of the MMS. The contractor is expected to make certification recommendations applicable to the modifications being accomplished. This will include physical installation and required connections to aircraft systems. Amendments to Challenger STCs will be required for multiple aircraft configurations.

The installation will involve modifications that will affect the following areas:

2.1.3.1 Antennas

Additional antennas required by the FIS include VHF, UHF, and L-Band for VOR/Localizer, Glideslope, TACAN, DME, GNSS, Direction Finding (DF), and Spectrum Analyzer (S/A). Careful attention is devoted to ensure good placement of these antennas to reduce installation effects and separation from other RF sources.

Each antenna has a unique and complex 3-dimentional and frequency dependent reception/radiation pattern which must be known to calculate and report accurate signal strength. In the addition standard antenna installations provided by the original equipment manufacturer, additional antennas will be required for the STC. The table below lists the known antenna requirements. Additional requirements and adjustments may be needed in the critical design.

Antenna Type P/N

GLIDE SLOPE FA67.10A

VOR/LOC (2) DMN4-33/C

MARKER BEACON S35-1000-2

TACAN Top, Comm#4 S65-8282-123

DME DM N124-10

VHF/UHF/VDB/DataLink S65-111-309 TACAN Lower, Vertical VHF/UHF S65-8282-123

GPS (2) 105728

2.1.3.2 Sensors

FIS sensors consist of the navigation receivers, inertial reference unit (IRU), radar/laser altimeter, camera system, and pilot marks. A compatible IRU may need to be installed in support of this system.

2.1.3.3 Operator Console/ Modular Mission System

The flight inspection workstation includes seat/harness, console, keyboard/mouse, monitors, fight inspection selections, audio panel, and emergency equipment. Each installation is unique and may have additional characteristics such as radio tuner(s) for the inspector radio(s).

2.1.3.4 Cabin Configuration

The cabin configuration must be able to handle multiple configurations to accomplish all FAA missions. These configurations include with MMS installed, and with MMS removed and replaced with passenger seating.

2.2 Task 2 STC Certification of BE300/BE350ER/BE360ER

The FAA may require a new or amended STC for the MMS installation to be applied to the BE300/BE350ER/BE360ER aircraft. The Contractor must have the authority and ability to exercise the following functions:

• Outline the preliminary certification basis and methods of compliance

• Project manage the project to meet desired milestones

• Review and approve technical data and find compliance to the airworthiness standards

• Issue required STCs and amendments

• Issue airworthiness certificates and approvals

• Establish conformity of articles including test articles

• Determine conformity of test setup

• Determine conformity of installations of articles, including Type Inspection

Authorization (TIA) inspections on a product

• Perform compliance inspections

• Approve data for major alterations or major repairs

• Perform review and obtain acceptance of Instructions for Continued Airworthiness

Specifications for MMS installation in the BE300/BE350ER/BE360ER aircraft will be provided after contract award if FAA exercises this option.

2.3 Milestones

The Contractor will work with AJF to create certification schedules that includes the milestones listed below. Specific miles stones may be negotiated after contract award.

• Project Kickoff Meeting With ODA

• Preliminary Design Review (PDR)

• Project Notification Letter Submittal

• PSCP / System Description initial submittal

• Installation Design Review (CDR)

• Draft Certification Schedule Accepted

• Project Notification Letter Accepted

• PSCP / System Description accepted

• Final Certification Schedule Accepted

• Analysis and aircraft test plans submitted for review ICA submitted for review

• AFMS submitted for review

• Installation Meeting (Preliminary)

• Electrical drawings submitted for review

• Structural drawings submitted for review

• Analysis and aircraft test plans complete

• Approval of analysis and test plans

• Approval of ICA

• Approval of AFMS

• Approval of Electrical drawings

• Approval of Structural drawings

• Internal Installation Conformity & Testing Complete

• ODA STC Board Meeting (Interim)

• ODA Conformity Inspection Complete

• Begin Request for Issuance of Experimental Airworthiness Certificate

• ODA Ground Testing Complete

• Remove Aircraft Standard Airworthiness Certificate and Issue Experimental Airworthiness Certificate

• ODA Pre-Flight Test Meeting

• ODA Flight Test Complete

• Ground test report submitted

• Flight test report submitted

• MDL, CDL, IDL complete

• ODA STC Board Meeting (Final)

• Issue STC

• Return Aircraft Certificate to Standard Airworthiness

2.4 Subtask 1.3 - Project Management

The Contractor will provide Program and Project Management support for related modification projects. The Contractor must prepare and maintain a Project Management Plan (PMP). The Government will use the PMP to assess the adequacy of the resources. The Contractor must provide a PMP to include each task of this PWS as follows:

• Weekly Project review

• Brief tasks that are off schedule and a present a plan to put the project back on schedule

• Description of the planned schedule to include all milestones and deliverables;

• Identification of each process step required for completing the work;

• The period of time needed to accomplish each step;

• Description of the staffing resources allocated to each task, i.e., staffing plan; and

• Rationale for the project organization, staff utilization, and other resource allocations.

• The Contractor must keep the PMP current and resubmit the PMP for COR approval whenever any proposed changes that result in a schedule impact of more than ten (10) business days.

• Process for presenting over and above items

2.4.1 Monthly Status Reports (CDRL A001)

The Contractor must provide Monthly Status Reports (MSR). The Contractor must provide Monthly Financial Reports (MFR). The report must contain the information below in a contractor provided format:

• Overview of work completed, work in progress, and work planned for each task;

• Hours expended by task, labor category, and personnel;

• Status of individual deliverables;

• Identification of risk areas with recommended remedial actions;

• Status of all outstanding identified risks

• Summary of expenditures by resource and labor category for the monthly reporting period, as well as cumulative year-to-date totals for the performance;

• Any additional information pertinent to the Government in administering the performance of this effort when directed by the COR.

• Critical path report

• Documentation burndown list

2.4.2 Subtask 1.6 - Monthly Financial Reports (CDRL A002)

The Contractor must provide Monthly Financial Reports (MFRs). The report must contain the information below in a contractor provided format:

• CLINs used during month; EVMS report?

• Cost/hours funded or apportioned by CLIN;

• Cost/hours used by CLIN;

• Projected date when 75% of funds are spent;

• Projected date when funds are exhausted;

• Funds/hours remaining by CLIN;

• Other direct costs (ODCs) estimated, used, and remaining by month; and

• Summary of expenditures by resource and labor category for the monthly reporting period, as well as cumulative year-to-date totals for the performance period.

3 End Results/Deliverables The Contractor must verify that all submitted deliverables conform to applicable FAA policies, standards, and guidelines as listed in Section 2 and 3 of this PWS.

All days are calendar days unless otherwise specified. The Government’s initial review of each deliverable is performed in accordance with the terms listed in the Acceptance Criteria table on next page.

5 Period of Performance The contract Period of Performance is one (1) Base year with four (4) 1-year options to be exercised at the discretion of the FAA.

Acceptance Criteria Table

Task End Result/Deliverable

Due Date Acceptance Criteria

1 Technical Interchange/Kick Off Meeting

Technical Interchange/Kick off meeting will be scheduled as soon as practical after award.

Technical Interchange /Kick off meeting may be held at FAA facility in Oklahoma City, OK with access to video conference (if needed).

Travel will be authorized for an on-site visit (if required).

Kick off meeting will be scheduled for three business days. With two travel days.

1 Certification Recommendations

Ongoing; Final recommendations as per final schedule.

Certification recommendations will be evaluated by the Aircraft Maintenance Directorate for approval and acceptance.

Acceptance criteria includes certification recommendations based on identified modifications that meet regulatory requirements. Acceptance will be determined by the Aircraft Maintenance Directorate.

Options for BE-300 and/or BE350ER/BE360ER certification recommendations will be determined after contract award.

1 • Draft Project Management Plan

PMP

• Project Notification Letter (PNL)

• PSCP

10 calendar days after technical interchange Kick off meeting

Draft CL605/650 modification schedule created in coordination with the Aircraft Maintenance Directorate. Draft schedule must address milestones listed in section 3.2

Options for BE300/BE350ER certification requirements will be determined after contract award.

1 Aircraft Certification As per final schedule Approval of CL605/650 STC Certificate and Supporting Data

1 Airworthiness Certificate

As per final schedule Approval of CL605/650 Airworthiness Certificate for aircraft with completed modifications

3 Final Project Management Plan

(PMP)

20 calendar days after technical interchange Kick off meeting

Updates within 5 days whenever any proposed changes are expected to result in a schedule impact of ten (10) days or more

The PMP is accurate, complete, submitted on time in the COR approved format and is prepared in accordance with PWS.

Includes final CL605/650 Series modification schedule created in coordination with the Aircraft Maintenance Directorate. Final schedule must address milestones listed in section 3.2

3 Monthly Financial Reports

10th day of 1st full month following contract start;

Every 10th day of each month thereafter. If 10th is a weekend, report due the next business day.

The Monthly Financial Reports are accurate, complete, submitted on time in the COR approved format and is prepared in accordance with PWS

3 Close Out Meeting Documentation and Meeting Minutes

Documentation - 5 days prior to the Close Out Meeting

Meeting Minutes - Within 5 days after the Close Out Meeting

Close Out Meeting Minutes capture all relevant topics discussed and summarize contractor’s understanding of close out work scope and PWS requirements. Contractor format acceptable, meets COR approval of content, and is prepared in accordance with PWS

6 Place of Performance The Contractor will perform work enumerated throughout this PWS at FAA designated facilities when access to FAA aircraft is required. The contractor may accomplish the work at a contractor designated site when able, at the discretion of the FAA. When the ODA Administrator and unit members are working remotely, communication with the Aircraft Maintenance Directorate will be via online meetings, emails and voice calls.

7 Travel Travel will be required to Oklahoma City, OK, Atlantic City, NJ and other locations defined by the COR to complete the project. Workload may be organized to minimize travel requirements and maximize work being completed at a facility designated by the contractor, but must be within the United States.

Travel must be authorized by the CO in advance of the start of the travel. FAA travel policy details are provided in the contract, travel and per diem section.

Travel estimates are based on anticipated travel to have required in-person meetings and access to aircraft and data in Oklahoma City, OK, and possibly in Atlantic City, NJ.

Due to COVID, most interchanges will be virtual, but FAA recognizes some in person meetings may be required.

8 Over and Above Over and above contract line item will be included in case of unforeseen certifications requirements. This includes costs related to data gathering, materials or shipping costs.

Contractor must obtain written approval from the CO or COR before any over and above costs are accrued.

9 Qualifications

9.1 Organizational Qualifications

AJF requires an active ODA. The contractor must have authority to issue STC’s on CL- 605/650 and BE300/BE350ER/BE360ER. Contractor must demonstrate previous STC certification on part 25 75,000 lbs. MTW or less; and Part 23 12,500 lbs. MTW or less within the last 5 years from proposal date.

9.2 Labor Category Qualifications

The contractor shall provide personnel, services, and supervision for persons in the following labor categories.

9.2.1 ODA Administrator

The ODA administrator must be appointed in accordance with FAA Order 8100.15 (current edition). The ODA administrator must have technical experience with the functions performed under the ODA and a broad range of management experience. This experience must enable the ODA administrator to manage the entire ODA unit activities effectively.

9.2.2 ODA Unit Members

At least one engineering or flight test ODA unit member must meet the qualifications for a Designated Engineering Representative (DER). The FAA defines these qualifications in FAA Order 8100.8 (current edition), Designee Management Handbook. The ODA unit members need to meet only those requirements for the functions and areas they will perform. However, the requirement to have direct working experience with the FAA may be satisfied by having direct working experience within an ODA holder’s or other delegated organization. The following unit member expertise will be required:

• Engineering Unit Member - Electrical

• Engineering Unit Member - Mechanical

• Engineering Unit Member - Structural

• Test Pilot Unit Member

• Inspecting Unit Member - Electrical

• Inspecting Unit Member - Structural

• Inspecting Unit Member - Airworthiness

• Engineering Unit Member – Icing and Aero

• Engineering Unit Member – Software

• Engineering Unit Member – EWIS

• Engineering Unit Member – L-HIRF

• Engineering Unit Member – Fatigue

• Engineering Unit Member – System Safety

9.2.3 Project Manager

The assigned project manager must hold a bachelor's degree in management, business or a related field, and/or related experience.

10 Other Requirements The FAA will provide adequate office and meeting space, internet connection, utilities, telephone, and related services while working on the tasks at a FAA facility.

The FAA will provide access to credentials and FAA-issued hardware (Government Furnished Equipment (GFE) if un-escorted access to FAA facilities and access to the FAA network (VPN) is determined to be required. This determination will be made at the kick-off meeting.

Security screening/background checks will be required per U.S. Government policy as detailed on the contract.

The FAA will furnish pertinent information related to tasks a required to accomplish the tasks described in this PWS.

The Contractor must return all GFE to the FAA prior to contract close out or earlier when directed by the COR.

SIR Attachment A – Statement of Work Draft A-1

Appendix A– Power requirements

Total Load Normal Operation

Loading Chart Availability Chart

AC SUMMARY (KVA)

POWER SOURCE/ BUS POWERED DESIGN

GEN 1 30 16.55 14.93 21.74 15.92 21.61 13.45 15.07 8.26 14.08 8.39

AC BUS 1 1.07 0.82 6.67 1.75 6.67

AC UTILITY BUS 1 8 7.59 7.59 7.59 7.24 7.59 0.41 0.41 0.41 0.76 0.41

AC ESSENTIAL BUS 8 3.13 2.33 3.33 2.75 3.10 4.87 5.67 4.67 5.25 4.90

TRU 1 3.45 2.73 2.51 2.51 2.52 2.57 0.72 0.94 0.94 0.93 0.88

ESS TRU 1 3.45 2.02 1.68 1.64 1.65 1.68 1.43 1.77 1.81 1.80 1.77

GEN 2 30 19.39 17.25 21.22 18.19 21.37 10.61 12.75 8.78 11.81 8.63

AC BUS 2 12.71 11.12 15.09 12.04 15.17

AC UTILITY BUS 2 8 2.81 2.81 2.81 2.81 2.81 5.19 5.19 5.19 5.19 5.19

TRU 2 3.45 1.85 1.64 1.68 1.68 1.71 1.60 1.81 1.77 1.77 1.74

ESS TRU 2 3.45 2.02 1.68 1.64 1.65 1.68 1.43 1.77 1.81 1.80 1.77

Flight inspection system TRU 3.45 0.01 0.01 0.01 0.01 0.01 3.44 3.44 3.44 3.44 3.44

APU GEN 30 INOP INOP INOP INOP INOP INOP INOP INOP INOP INOP

ADG 15 INOP INOP INOP INOP INOP INOP INOP INOP INOP INOP

AC BUS 1 + AC BUS 2 + AC ESSENTIAL BUS 30 16.91 14.27 25.09 16.54 24.94 13.09 15.73 4.91 13.46 5.06

DC SUMMARY (Amps)

POWER SOURCE/BUS POWERED DESIGN

TRU 1 100 78.86 72.32 72.36 72.82 74.07 21.14 27.68 27.64 27.18 25.93

DC BUS 1 50 50.69 44.15 44.19 44.65 45.90 ‐0.69 5.85 5.81 5.35 4.10

DC UTILITY 1 50 28.17 28.17 28.17 28.17 28.17 21.83 21.83 21.83 21.83 21.83

TRU 2 100 53.35 47.19 48.45 48.52 49.42 46.65 52.81 51.55 51.48 50.58

DC BUS 2 50 38.03 31.87 33.13 33.20 34.10 11.97 18.13 16.87 16.80 15.90

DC UTILITY 2 50 15.32 15.32 15.32 15.32 15.32 34.68 34.68 34.68 34.68 34.68

ESS TRU 1 100 58.22 48.49 47.21 47.69 48.37 41.78 51.51 52.79 52.31 51.63

ESSENTIAL BUS (50%) 50 26.75 27.50 26.92 26.88 27.23 23.25 22.50 23.08 23.12 22.77

BATTERY BUS (50%) 50 31.47 20.99 20.29 20.81 21.14 18.53 29.01 29.71 29.19 28.86

EMERGENCY BUS (25%) 20 0.00 0.00 0.00 0.00 0.00 20.00 20.00 20.00 20.00 20.00

ESS TRU 2 100 58.22 48.49 47.21 47.69 48.37 41.78 51.51 52.79 52.31 51.63

ESSENTIAL BUS (50%) 50 26.75 27.50 26.92 26.88 27.23 23.25 22.50 23.08 23.12 22.77

BATTERY BUS (50%) 50 31.47 20.99 20.29 20.81 21.14 18.53 29.01 29.71 29.19 28.86

EMERGENCY BUS (25%) 20 0.00 0.00 0.00 0.00 0.00 20.00 20.00 20.00 20.00 20.00

APU BATTERY N/A 0.43 0.43 0.43 0.43 0.43 N/A N/A N/A N/A N/A

APU BATTERY DIRECT 0.43 0.43 0.43 0.43 0.43

EMERGENCY BUS (50%) 0.00 0.00 0.00 0.00 0.00

MAIN BATTERY N/A 8.63 1.50 1.50 1.50 1.50 N/A N/A N/A N/A N/A

MAIN BATTERY DIRECT 8.63 1.50 1.50 1.50 1.50

FIS TRU 100 20.25 20.25 20.25 20.25 20.25 79.75 79.75 79.75 79.75 79.75

Flight inspection system TRU

35 20.25 20.25 20.25 20.25 20.25 14.75 14.75 14.75 14.75 14.75

DC BUS 1 + DC BUS 2 100 88.72 76.02 77.32 77.85 80.00 11.28 23.98 22.68 22.15 20.00 ESSENTIAL BUS + BATTERY BUS 88 116.44 96.98 94.42 95.38 96.74 ‐28.44 ‐8.98 ‐6.42 ‐7.38 ‐8.74 UTIL BUS 1 GALLEY FEED 1 25 5.50 5.50 5.50 5.50 5.50 19.50 19.50 19.50 19.50 19.50 UTIL BUS 1 GALLEY FEED 2 25 13.34 13.34 13.34 13.34 13.34 11.66 11.66 11.66 11.66 11.66 UTIL BUS 2 GALLEY FEED 1 25 7.72 7.72 7.72 7.72 7.72 17.28 17.28 17.28 17.28 17.28 UTIL BUS 2 GALLEY FEED 2 25 1.90 1.90 1.90 1.90 1.90 23.10 23.10 23.10 23.10 23.10

10 Other Requirements