ESS Follow-On PWS FINAL R1.pdf

AIR FORCE AIR DOMINANCE SYSTEMS CENTER (AFADSC) 1

PRESIDENTIAL AND EXECUTIVE AIRPOWER DIRECTORATE 2

EXECUTIVE AIRCRAFT DIVISION (EAD) 3

TINKER AFB, OK 73145 4

PERFORMANCE WORK STATEMENT 6

(PWS) 7

For 8

ENGINEERING SUPPORT SERVICES 9

PREPARATION DATE: 29 OCTOBER 2025 12

PWS CONTROL NUMBER: PWS-27-ESS-01 15

CONTRACT NUMBER: FA8134-27-D-BXXX 18

PREPARING ORGANIZATION: AFLCMC/WVV TINKER AFB OK 73145-3020 21

1.0 SECTION I – OVERVIEW ................................................................................................................. 6 24

1.1 CONTRACTOR RESPONSIBILITY ........................................................................................................... 6 25

1.2 PROCURING CONTRACTING OFFICER’S (PCO) AUTHORITY ............................................................. 6 26

1.3 CALENDAR DAYS AND TIME MEASUREMENT ...................................................................................... 7 27

1.4 PLATFORM DESCRIPTIONS ........................................................................................................... 7 28

1.4.1 E-4B NATIONAL AIRBORNE OPERATIONS CENTER ..................................................................... 7 29

1.4.2 VC-25A AIR FORCE ONE ............................................................................................................. 7 30

1.4.3 NT-43A ........................................................................................................................................ 8 31

1.4.4 C-32A ........................................................................................................................................... 8 32

1.4.5 C-40B ........................................................................................................................................... 8 33

1.4.6 C-40C ........................................................................................................................................... 8 34

1.4.7 VC-25B THE NEXT AIR FORCE ONE ............................................................................................ 8 35

2.0 SECTION II – RECURRING ENGINEERING ................................................................................ 9 36

2.1 SYSTEMS ENGINEERING ................................................................................................................ 9 37

2.1.1 SYSTEMS ENGINEERING MANAGEMENT PLAN (SEMP) .............................................................. 9 38

2.1.2 SAFETY MANAGEMENT PLAN .................................................................................................... 10 39

2.1.3 SAFETY ANALYSIS AND REPORTING .......................................................................................... 10 40

2.1.4 ENGINEERING BASELINE CONTROL AND MAINTENANCE .......................................................... 10 41

2.1.5 RELIABILITY MAINTAINABILITY AND AVAILABILITY (RM&A) / SYSTEM FAILURE ANALYSIS 10 42

2.1.6 RELIABILITY AND MAINTAINABILITY (R&M) PLANNING AND EXECUTION ............................. 11 43

2.1.7 TECHNOLOGY ROADMAP (C-32A, C-40B/C, AND VC-25B) ..................................................... 12 44

2.1.8 FIELD AND DEPOT LEVEL MAINTENANCE HISTORICAL DATA .................................................. 12 45

2.2 SERVICE INFORMATION AND FAA AIRWORTHINESS DIRECTIVES ............................... 12 46

2.2.1 SERVICE INFORMATION AND FAA AIRWORTHINESS DIRECTIVES REVIEW ............................... 12 47

2.2.2 SERVICE LITERATURE EVALUATION .......................................................................................... 13 48

2.2.3 SERVICE ACTION REVIEW BOARD (SARB)/CONCURRENCE DISPOSITION MEETING ................ 17 49

2.2.4 GOVERNMENT INDUSTRY DATA EXCHANGE PROGRAM (GIDEP) REVIEW .............................. 17 50

2.2.5 CONFIGURATION DATA MANAGEMENT DATABASE .................................................................. 18 51

2.2.6 EMERGENCY, URGENT AND SHORT COMPLIANCE FAA AIRWORTHINESS DIRECTIVES (ADS) . 18 52

2.2.7 DISPATCH DEVIATION GUIDE AND FAA MINIMUM EQUIPMENT LIST ...................................... 18 53

2.2.8 AIRWORTHINESS MANAGEMENT PLANNING INFORMATION ...................................................... 18 54

2.2.9 FAA AIRWORTHINESS ACTIVITY REQUIREMENTS .................................................................... 19 55

2.2.10 ENGINE RECORDS ..................................................................................................................... 19 56

2.2.11 ENGINE MANAGEMENT PLAN .................................................................................................. 19 57

2.2.12 AUXILIARY POWER UNIT (APU) MANAGEMENT PLAN ........................................................... 20 58

2.2.13 AUXILIARY POWER UNIT (APU) MANAGEMENT PLAN ........................................................... 21 59

2.2.14 APU RECORDS ......................................................................................................................... 21 60

2.2.15 APU RECORDS REVIEW ........................................................................................................... 21 61

2.2.16 MAINTENANCE PROGRAM SUPPORT ........................................................................................ 21 62

2.2.17 FAA CERTIFICATION AND AIRWORTHINESS ............................................................................ 22 63

2.2.18 SERVICE INFORMATION CONFIGURATION DOCUMENT (SICD) ............................................... 22 64

2.2.19 MAINTENANCE PLANNING DOCUMENT REVISIONS ................................................................. 22 65

2.2.20 SCHEDULED MAINTENANCE CHECKS ...................................................................................... 22 66

2.2.21 MAINTENANCE INSPECTION REQUIREMENTS DOCUMENT....................................................... 23 67

2.2.22 TRAINING MANUALS AND MATERIALS .................................................................................... 23 68

2.3 MISSION ASSURANCE .................................................................................................................... 24 69

2.3.1 MISSION ANALYSIS .................................................................................................................... 24 70

2.3.2 FIELD ENGINEERING SUPPORT ................................................................................................... 24 71

2.3.3 IN-FLIGHT EMERGENCY SUPPORT ............................................................................................. 25 72

2.3.4 EMERGENCY SUPPORT ............................................................................................................... 25 73

2.3.5 AIRCRAFT MISSION SUPPORT .................................................................................................... 25 74

2.4 SYSTEM INTEGRATION ................................................................................................................. 26 75

2.4.1 SUPPORT ENGINEERING ............................................................................................................. 26 76

2.4.1.1 PLATFORM INTEGRATION (C-32A AND C-40B/C) .................................................................. 26 77

2.4.2 WEAPON SYSTEM ACTIVITY PLANNING .................................................................................... 26 78

2.4.3 MEETINGS .................................................................................................................................. 26 79

2.4.4 DATA REQUESTS ........................................................................................................................ 27 80

2.4.5 MASTER DATA FILE ................................................................................................................... 27 81

2.4.6 MASTER DATA FILES (MDF) INDEX .......................................................................................... 27 82

2.4.7 REFERENCE DESIGNATOR SUPPORT ........................................................................................... 27 83

2.4.8 TECHNICAL ORDER (TO) SUPPORT ............................................................................................ 27 84

2.4.9 SUBSTITUTE PARTS .................................................................................................................... 28 85

2.4.10 OBSOLESCENCE ........................................................................................................................ 28 86

2.4.11 HISTORICAL MAINTENANCE RECORDS .................................................................................... 28 87

2.4.12 HISTORICAL NUCLEAR HARDENING RECORDS ........................................................................ 28 88

2.4.13 HARDNESS MAINTENANCE/HARDNESS ASSURANCE SUPPORT ............................................... 28 89

2.4.14 HARDNESS DOCUMENT UPDATES ............................................................................................ 29 90

2.4.15 NUCLEAR HARDENING ASSESSMENT ....................................................................................... 29 91

2.4.16 HARDNESS ASSESSMENT .......................................................................................................... 29 92

2.4.17 ELECTROMAGNETIC EFFECTS AND ELECTRICAL LOADS ANALYSIS ........................................ 29 93

2.4.18 STANDARDS AND SPECIFICATIONS .......................................................................................... 30 94

2.4.19 ANTENNAS ............................................................................................................................... 30 95

2.5 TECHNICAL DATA .......................................................................................................................... 30 96

2.5.1 TECHNICAL ORDER (TO) SERVICES ........................................................................................... 30 97

2.5.2 AIR FORCE UNIQUE DATA ......................................................................................................... 31 98

2.5.3 WIRING DIAGRAM MANUALS (WDM) AND LISTS, AND COMMERCIAL DATABASES ................ 31 99

2.5.4 ILLUSTRATED PARTS CATALOG (IPC) ....................................................................................... 31 100

2.5.5 TO UPDATES - SCHEDULED INSPECTION AND MAINTENANCE REQUIREMENTS ........................ 31 101

2.5.6 SERVICE LITERATURE-DRIVEN CHANGES – TOS....................................................................... 32 102

2.5.7 FAST REACTION CHANGES – TOS .............................................................................................. 32 103

2.5.8 TO SUPPLEMENTS ...................................................................................................................... 32 104

2.5.9 CHECKLISTS AND WORKCARDS – TOS ...................................................................................... 32 105

2.5.10 MIL-SPEC REFORMATTING – TOS ............................................................................................ 32 106

2.5.11 TO DELIVERY REQUIREMENTS ................................................................................................ 33 107

2.5.12 TO DATABASES ........................................................................................................................ 33 108

2.5.13 TO STORAGE - MASTER FILES ................................................................................................. 33 109

2.5.14 TO LIBRARY ............................................................................................................................. 33 110

2.5.15 HISTORICAL DATABASE ........................................................................................................... 33 111

2.5.16 DISSEMINATION AND CONTROL OF DATA – TOS ..................................................................... 33 112

2.5.17 NOTIFICATION OF INADEQUATE MATERIAL ............................................................................ 33 113

2.5.18 FLIGHT MANUAL CHANGES ..................................................................................................... 34 114

2.5.19 TO INSPECTION AND ACCEPTANCE ......................................................................................... 34 115

2.5.20 TECHNICAL PUBLICATIONS ...................................................................................................... 34 116

2.5.21 CUSTOMER REQUESTED TO CHANGES (AFTO FORM 252) AND LOCAL GENERATED 117

PUBLICATION CHANGE REQUEST .................................................................................................. 35 118

2.5.22 GOVERNMENT FURNISHED SOURCE DATA .............................................................................. 35 119

2.5.23 TO STATUS AND SCHEDULE REPORT ....................................................................................... 35 120

2.5.24 PHASE-OUT .............................................................................................................................. 35 121

2.5.25 SERVICE BULLETIN (SB) AND AIRWORTHINESS DIRECTIVES (AD) STATUS REPORT ............. 36 122

3.0 SECTION III – NONRECURRING ENGINEERING (NRE) ........................................................ 36 123

3.1 ENGINEERING TASKS (ET) .................................................................................................................. 36 124

3.2 ENGINEERING PROJECTS (EP) ............................................................................................................ 36 125

3.2.1 EP PERIOD OF PERFORMANCE.................................................................................................... 37 126

3.3 ENGINEERING ASSIGNMENTS (EA)..................................................................................................... 37 127

3.3.1 EA PERIOD OF PERFORMANCE ................................................................................................... 37 128

3.4 ENGINEERING STUDIES ....................................................................................................................... 38 129

3.5 ENGINEERING SUPPORT ...................................................................................................................... 38 130

3.6 PROPOSAL PREPARATION ................................................................................................................... 38 131

3.7 ELECTROMAGNETIC EFFECTS TESTING ............................................................................................ 39 132

3.8 ENVIRONMENTAL SUPPORT ................................................................................................................ 39 133

3.9 ROUGH ORDER OF MAGNITUDE (ROM) ............................................................................................ 39 134

3.10 PROTOTYPE AND KIT-PROOF MODIFICATIONS ............................................................................... 39 135

3.10.1 CONTRACTOR PILOTS IN SUPPORT OF PROTOTYPE TESTING (C-32A, C-40B/C) .................... 40 136

3.11 AFTO 22 AND AF FORM 847 SUPPORT ............................................................................................ 40 137

3.12 UNIQUE TO REQUIREMENTS ............................................................................................................ 40 138

3.13 TIME COMPLIANCE TECHNICAL ORDER (TCTO) .......................................................................... 40 139

3.14 TECHNICAL ORDER CHANGES AND/OR TO FORMATTED SOURCE DATA...................................... 40 140

3.15 TECH ORDER CONTRACTOR QUALITY ASSURANCE ....................................................................... 41 141

3.16 TCTO VERIFICATION ........................................................................................................................ 41 142

3.17 TECH DATA REVIEW/UPDATE .......................................................................................................... 41 143

3.18 SOURCE DATA .................................................................................................................................... 41 144

3.19 DEFICIENCY REPORTING .................................................................................................................. 42 145

3.20 CONTRACT DELIVERABLES IN SUPPORT OF EP’S AND EA’S .......................................................... 42 146

4.0 SECTION IV – GENERAL ............................................................................................................... 42 147

4.1 CONTRACTOR LABOR HOUR REPORTING ......................................................................................... 42 148

4.2 NOTIFICATION OF EXPENDITURE ....................................................................................................... 42 149

4.3 NOTIFICATION OF COMPLETION/CLOSURE ....................................................................................... 43 150

4.4 PROGRAM SYNERGY ............................................................................................................................ 43 151

4.5 PROGRAM SECURITY ........................................................................................................................... 43 152

4.5.1 SECURITY REQUIREMENTS ......................................................................................................... 43 153

4.5.2 CRITICAL PROGRAM INFORMATION ........................................................................................... 44 154

4.5.3 CRITICAL COMPONENT IDENTIFICATION ................................................................................... 44 155

4.5.4 PROGRAM PROTECTION PLAN (PPP) .......................................................................................... 44 156

4.5.5 PROGRAM PROTECTION IMPLEMENTATION PLAN (PPIP) .......................................................... 44 157

4.5.6 OPERATIONS SECURITY (OPSEC) .............................................................................................. 44 158

4.5.7 SECURITY ................................................................................................................................... 45 159

4.5.8 FOREIGN GOVERNMENT/FOREIGN GOVERNMENT INFORMATION ............................................. 46 160

4.5.9 FMS RELEASE ............................................................................................................................ 46 161

4.5.10 TECHNICAL ASSISTANCE AGREEMENT .................................................................................... 46 162

4.6 COMPLIANCE WITH LAWS AND REGULATIONS ................................................................................. 47 163

4.7 DATA RIGHTS ....................................................................................................................................... 47 164

4.8 DRAWING QUALITY ............................................................................................................................. 47 165

4.9 MYBOEINGFLEET.COM (3RD PARTY LICENSE AGREEMENT) ............................................................ 47 166

4.10 MONTHLY STATUS REPORTS ............................................................................................................ 48 167

4.11 DATA ACCESSION LIST ...................................................................................................................... 48 168

4.12 CONTRACT FUNDS STATUS REPORT................................................................................................. 48 169

4.13 EARNED VALUE MANAGEMENT (EVM) REPORT ............................................................................ 48 170

4.14 PROGRAM MANAGEMENT PLAN ....................................................................................................... 48 171

4.15 CONFIGURATION MANAGEMENT PLAN ........................................................................................... 49 172

4.16 RISK MANAGEMENT PLAN ................................................................................................................ 49 173

4.17 QUALITY MANAGEMENT SYSTEM .................................................................................................... 49 174

4.18 QUALITY SYSTEMS PROVISIONS ....................................................................................................... 49 175

4.19 QUALITY ASSURANCE PROVISIONS .................................................................................................. 49 176

4.20 CONTRACTOR IDENTIFICATION ........................................................................................................ 49 177

4.21 MISSION ESSENTIAL CONTRACTOR SERVICES ................................................................................ 49 178

5.0 SECTION V – SERVICE SUMMARY ............................................................................................. 50 179

5.1 SERVICE SUMMARY (SS) REQUIREMENTS ......................................................................................... 50 180

5.2 PERFORMANCE OBJECTIVES AND THRESHOLDS ............................................................................... 50 181

5.3 SURVEILLANCE METHODS .................................................................................................................. 50 182

5.4 CONTRACTOR PERFORMANCE EVALUATION .................................................................................... 51 183

6.0 SECTION VI – GOVERNMENT FURNISHED PROPERTY (GFP) ........................................... 54 184

6.1 DATA ..................................................................................................................................................... 54 185

6.2 EQUIPMENT .......................................................................................................................................... 54 186

6.3 GFP FOR ENGINEERING ASSIGNMENTS ............................................................................................. 54 187

6.4 VC-25A AND VC-25B GFP DISPOSITION AND PLANT CLEARANCE ................................................. 54 188

7.0 SECTION VI – LIST OF APPENDICES ......................................................................................... 54 189

1.0 SECTION I – OVERVIEW 192

This Performance Work Statement (PWS) outlines the engineering support services, both recurring 193 and non-recurring, required to sustain and modernize specific aircraft as designated by the 194

Government. The scope of work encompasses the following weapon systems, with the 195 understanding that aircraft platforms, sites, and locations may be modified throughout the contract 196 period: 197

1) Air Force: E-4B/747; VC-25A/747; AFMC NT-43/737; C-32A/757; C-40B/C/737; VC-198

25B/747 199

NOTE: The Government reserves the right to add, modify, or remove supported aircraft platforms 200 and operational locations throughout the duration of this effort to accommodate evolving mission 201 requirements. 202

1.1 Contractor Responsibility 203

The Contractor shall: 204

1) Execute all work requirements as specified with this PWS 205

2) Manage and deliver Contract Data Requirements Lists (CDRL) items in accordance with 206 the following criteria 207

a. Submit all deliverables on or before specified due dates 208

b. Ensure accuracy and completeness of all submitted documentation 209

c. Comply with format and content requirements as defined in the CDRL 210

d. Maintain quality control standards throughout the submission process 211

e. Revise disapproved CDRLs within two (2) weeks of notification of unacceptance 212

1.2 Procuring Contracting Officer’s (PCO) Authority 213

The PCO is the sole authority authorized to modify or approve changes to: 214

1) Any requirements specified in this PWS 215

2) Any provisions contained within the contract 216

3) Any contractual terms and conditions 217

Any modifications implemented without explicit PCO approval are: 218

1) Considered unauthorized 219

2) Made at the Contractor’s own risk 220

3) Subject to rejection and/or removal 221

4) Not eligible for compensation 222

5) Potentially subject to contractual remedies 223

NOTE: Implementation of changes directed by any person other than the PCO, 224 regardless of their position or authority level, will be considered unauthorized and 225 outside the scope of this contract. 226

1.3 Calendar Days and Time Measurement 227

All references to “day(s)” within this PWS shall be interpreted as “calendar day(s)”—excluding 228 federal holidays, unless otherwise stated. All timeframes are based on the official time zone of the 229

Executive Aircraft Division, Tinker AFB. 230

NOTE: When the last day of a specified period falls on a weekend or Federal holiday, the period 231 shall extend to the next business day, unless otherwise specified in writing. 232

NOTE: Federal holidays are as follows: New Year’s Day, Martin Luther King's Birthday, 233

Washington’s Birthday, Memorial Day, Juneteenth National Independence Daty, Independence 234

Day, Labor Day, Columbus Day, Veterans Day, Thanksgiving Day, and Christmas Day. If the 235 holiday falls on Sunday, it is observed on Monday. If the holiday falls on Saturday, it is observed 236 on Friday. 237

1.4 PLATFORM DESCRIPTIONS 238

1.4.1 E-4B National Airborne Operations Center 239

The E-4B is the National Airborne Operations Center (NAOC) for the National Command 240

Authority (NCA) which includes the President of the United States, the Secretary of Defense and 241 the Chairman of the Joint Chiefs of Staff (CJCS). In case of national emergency or destruction of 242 ground command control centers, the E-4B provides a modern, highly survivable, command, 243 control and communications center to direct U.S. forces, execute emergency war orders and 244 coordinate actions by civil authorities. There are four E-4B aircraft in the Air Force inventory, 245 with one constantly on alert. 246

The E-4B aircraft, a militarized version of the Boeing 747-200, is a four-engine, swept-wing, long-247 range, high-altitude airplane capable of being refueled in flight. It is equipped with the electronics, 248 communications, and personnel and equipment required for the NAOC missions. The E-4B serves 249 as a worldwide, survivable enduring node of the National Military Command System (NMCS) for 250 the purpose of exercising national security responsibilities throughout the full spectrum of conflict. 251

The E-4B has electromagnetic pulse protection, nuclear and thermal effects shielding, an electrical 252 system designed to support advance electronics and a wide variety of communications equipment. 253

An advanced satellite communications system allows worldwide communications among strategic 254 and tactical satellite systems and the airborne operations center. 255

1.4.2 VC-25A Air Force One 256

The mission of the VC-25A, more commonly known as "Air Force One," is to provide senior 257 leader air transportation for the President of the United States. The fleet consists of two specially 258 configured Boeing 747-200 aircraft. These aircraft have been managed by Air Force Life Cycle 259

Management Center (AFLCMC) since they were deployed in the early 90s. These aircraft provide 260 safe, comfortable, reliable, worldwide air transport with a communications capability that provides 261 an “office in the sky” environment. The basic airframes, engines and avionics systems are 262 commercial-off-the-shelf (COTS) with unique mission support systems and equipment installed 263 to support mission requirements. The basic aircraft and unique systems are maintained to Federal 264

Aviation Administration (FAA) standards. 265

The contractor shall not use the VC-25A, in terminology or visually, in connection with 266 advertisement of any system/component installed on the aircraft. The Contractor shall ensure sub-267 contractors also do not use the VC-25A, in terminology or visually, in connection with 268 advertisement of any system/component installed on the aircraft. 269

1.4.3 NT-43A 270

The AFMC NT-43A aircraft is a Government owned, contractor operated Boeing 737-200 271 commercial derivative aircraft modified for special mission support. This aircraft was previously 272 an AF T-43A Navigation Trainer. 273

1.4.4 C-32A 274

The mission of the C-32A is to provide senior leader transportation for the Vice President, First 275

Lady and cabinet members. The fleet consists of four specially configured Boeing 757-200 aircraft 276 stationed at Joint Base Andrews, MD. The C-32A provides safe, comfortable and reliable 277 transportation for our nation’s leaders to locations around the world. Serves as an office in the sky 278 and provides critical senior leadership mission capabilities. The basic airframes, engines and 279 avionics systems are commercial-off-the-shelf (COTS) with unique mission support systems and 280 equipment installed to support mission requirements. 281

1.4.5 C-40B 282

The mission of the C-40B is to provide airlift and an office in the sky for combatant commanders. 283

The fleet is made up of four Boeing 737-700IGW commercial derivative aircraft stationed at Joint 284

Base Andrews, MD. The basic airframes, engines and avionics systems are COTS with unique 285 mission support systems and equipment installed to support mission requirements. 286

1.4.6 C-40C 287

The C-40C is a multi-mission aircraft providing rapid response to worldwide team travel and 288 special air mission tasking. The primary customers are Congress and Senate members and senior 289 military members. The fleet consists of seven Boeing 737-700IGW commercial derivative aircraft 290 modified for senior leaders. The basic airframes, engines and avionics systems are COTS with 291 unique mission support systems and equipment installed to support mission requirements. Three 292 aircraft are stationed at Joint Base Andrews, MD operated by Air National Guard (ANG) and four 293 are stationed at Scott AFB, IL and are operated by Air Force Reserve Corps (AFRC.) 294

1.4.7 VC-25B The Next Air Force One 295

The mission of the VC-25B, more commonly known as "The Next Air Force One," will provide 296 air transportation to the President of the United States (POTUS) ensuring he/she is able to execute 297 the duties of Head of State, Chief Executive, and Commander in Chief. The Boeing 747-8i 298 commercial aircraft was uniquely modified to provide POTUS, staff, and guests with safe 299 comfortable, and reliable air transport with a communications capability that provides a “flying 300

White House” environment. The modification of these aircraft is managed by Air Force Life Cycle 301

Management Center / WVB (AFLCMC/WVB). The modifications to the 747-8 aircraft include 302 the following major enhancements: 303

a. Avionics and flight deck – military communication, navigation, and surveillance 304 capabilities are added to the 747-8 flight deck. 305

b. Mission Communication Subsystem (MCS) – a new MCS is added to provide global 306 secure/non-secure voice, data, and video communications. 307

c. Interior – a customized Layout of Passenger Accommodation (LOPA) is required to 308 provide presidential accommodations, a Medical Compartment, Senior Staff 309

Compartment, Staff Area, Guest Area, Press Area, Forward and Aft Lower Lobe stowage, 310 and accommodations for aircrew. 311

d. Airframe and systems – airframe and system enhancements include electrical power 312 upgrades, autonomous enplaning/deplaning, autonomous baggage loading, and 313

Electromagnetic Environmental (E3) hardening. 314

The contractor shall not use the VC-25B, in terminology or visually, in connection with 315 advertisement of any system/component installed on the aircraft. The Contractor shall ensure sub-316 contractors also do not use the VC-25B, in terminology or visually, in connection with 317 advertisement of any system/component installed on the aircraft. 318

2.0 SECTION II – RECURRING ENGINEERING 319

The Recurring Engineering services (Section 2.1 through Section 2.4) and Technical Publications 320

(Section 2.9) will involve continuous Contractor action and will not require additional contractual 321 authorization or tasks for accomplishment. Government requests for services and tasks outside the 322 funded scope of Recurring Engineering and Technical Publications are as provided for in 323

Nonrecurring Engineering (Section 3.0). 324

2.1 SYSTEMS ENGINEERING 325

2.1.1 Systems Engineering Management Plan (SEMP) 326

The Contractor shall provide a Systems Engineering Management Plan (SEMP) that details the 327 engineering processes, systems, organization and resources required to support the platforms listed 328 in Section 1.0 of this PWS. The SEMP shall address the following: 329

a. Requirements analysis and management 330

b. Functional analysis and allocation 331

c. Integrated planning and scheduling 332

d. Technical Performance Measures (TPM) 333

e. Interface control 334

f. Baseline management 335

g. Technology insertion 336

h. Analysis, integration and test (to include system validation and verification) 337

i. System architecture development 338

(CDRL XX01) 339

2.1.2 Safety Management Plan 340

The Contractor’s safety program shall be maintained in accordance with the latest published 341 version of MIL-STD 882. The Contractor shall develop and deliver a contractor’s safety 342 management plan. 343

(CDRL XX18) 344

2.1.3 Safety Analysis and Reporting 345

The Contractor shall immediately report any situation that may affect ground or flight safety of 346 aircraft and/or personnel to the Government. The Contractor shall provide an initial response, 347 including a preliminary hazard analysis and an initial Risk Assessment Code (RAC) per MIL-STD 348

882 within 24 hours of a safety inquiry or discovery of a safety situation. The initial response shall 349 include a schedule and estimate of effort for completing analysis through the development of a 350 risk management recommendation. 351

(CDRL XX02) 352

2.1.4 Engineering Baseline Control and Maintenance 353

(Applies to: VC-25A, E-4B, C-32A, C-40B/C, and VC-25B) 354

The Contractor shall control and maintain the engineering data baseline for the disciplines 355 specified in Appendices D-F and M. The Contractor shall maintain the data by obtaining 356 supplemental analyses and incorporating the data into the baseline document. The Contractor 357 shall document the existing configuration and performance of the aircraft/system/function. 358

The Contractor shall update the baselines established through modifications and changes. The 359

Contractor shall incorporate data from third party changes and modifications using data provided 360 by the Program Office. The Contractor shall review the baselines annually or when directed. The 361

Contractor shall analyze and make recommendations to the Program Office using the baseline 362 data. 363

(CDRL XX03) 364

2.1.5 Reliability Maintainability and Availability (RM&A) / System Failure Analysis 365

(Applies to: E-4B) 366

The Contractor shall monitor RM&A, analyze and evaluate system performance, logistical health 367 and supportability issues affecting systems, as well as operations and maintenance performance. 368

The Contractor shall use all available data to analyze in-service systems on operational and depot 369 possessed aircraft to determine parts usage trends and generate recommended solutions to improve 370

RM&A and support and/or reduce costs by utilizing tools specifically developed to assist in 371 performing those requirements (for example: System Performance Dashboard Metric, CANN 372

Projections, Time Change Items (TCI) Reports, Windchill Risk and Reliability). The Contractor 373 shall utilize these tools to maintain current databases and update tools as necessary to perform 374 analysis on in-service systems. The Contractor shall respond to Program Office and field inquiries 375 on crew and ground-reported discrepancies. 376

The Contractor shall have access to Maintenance Information Systems (MIS) to provide a monthly 377

RM&A report that includes Basing & Logistics Analysis Data Environment (BLADE) and/or 378

Logistics, Installations and Mission Support – Enterprise View (LIMS-EV) mission capable and 379 non-mission capable rates, aircraft availability, non-mission capable drivers, system non-mission 380 capable drivers, completed monthly activities, and current open activities as part of the monthly 381 status report. 382

The Contractor shall have and maintain access to Government MIS to assist in analyzing in-service 383 systems on operational and depot possessed aircraft (for example: BLADE, Reliability and 384

Maintainability Information System (REMIS); Logistics, Installations and Mission Support – 385

Enterprise View (LIMS-EV); Integrated Maintenance Data Systems (IMDS); Comprehensive 386

Engine Management Systems (CEMS); Global Combat Support Systems – Air Force (GCSS-AF); 387

Enhanced Technical Information Management Systems (ETIMS)) and maintaining current 388 databases and update tools as necessary to perform analysis on in-service systems. 389

The Contractor shall provide R&M data and analysis support for evaluation of service literature 390 items that are applicable to the fleet, field and depot maintenance requirements/intervals. The 391

Contractor shall work with the Boeing DMS Process Action Team on Diminishing Manufacturing 392

Sources and Material Shortages (DMSMS) issues on request. The Contractor shall incorporate 393

DMSMS data from the DMS Process Action Teams if applicable into R&M analyses and 394 corrective action recommendations. The Contractor shall attend and support program meetings 395 intended to enhance system R&M and/or improve aircraft availability, maintenance, and mission 396 effectiveness. The Contractor shall attend industry, DoD, and Large Data Analytics 397 meetings/conferences to maintain awareness of R&M/DMSMS/Data Mining issues. 398

(CDRL XX06) 399

2.1.6 Reliability and Maintainability (R&M) Planning and Execution 400

(Applies to: C-32A and C-40B/C) 401

The Contractor shall develop and execute a platform R&M Plan that improves system reliability 402 performance and/or reduces costs. The plan shall employ and implement new tools as needed to 403 provide improved R&M capabilities to enhance platform support. The plan shall provide for: 404

• Data collection from the Government-provided and Boeing-provided sources. 405

• Continuing review and analysis of collected data to identify reliability, maintainability, and 406 availability issues. 407

• Generation of recommendations for resolution of selected reliability, maintainability, and 408 availability issues. 409

• Response to Program Office and field inquiries on crew and ground-reported discrepancies. 410

Examples of events that may also prompt inquiries are Deficiency Reports, ETOPS and 411

RVSM event reports, and Service Difficulty Reports. 412

• R&M data and analysis support for evaluation of service literature items that are applicable 413 to the fleet on request. 414

• R&M data and analysis support for evaluation of maintenance requirements and intervals. 415

• R&M data and analysis support for Diminishing Manufacturing Sources and Material 416

Shortages (DMSMS) issues in cooperation with the Program Office, the Contractor DMS 417 team, and the CLS contractor. 418

• Incorporation of DMSMS data into R&M analyses and corrective action recommendations. 419

• Attendance and support of program meetings intended to enhance system R&M and/or 420 improve maintenance effectiveness. 421

• Attendance of industry and DoD meetings in order to remain aware of R&M issues in the 422 commercial fleet including Boeing Fleet Team and Working Together Meetings. 423

(CDRL XX06, XX12) 424

2.1.7 Technology Roadmap (C-32A, C-40B/C, and VC-25B) 425

The Contractor shall develop a Technology Roadmap for each platform. The roadmap shall 426 include solutions to address worldwide aviation regulation changes, obsolescence, emergent 427 issues, and existing and/or new technologies that could impact mission performance. Items on the 428 roadmap shall be reviewed regularly and prioritized with Government Program Office input. Each 429 item on the roadmap shall identify the notional implementation schedule along with the pertinent 430 cost estimate data resulting from related nonrecurring engineering activities. 431

2.1.8 Field and Depot Level Maintenance Historical Data 432

(Applies to: VC-25A, E-4B, C-32A, C-40B/C, and VC-25B) 433

The Contractor shall maintain access to the Reliability and Maintainability Information System 434

(REMIS), Integrated Maintenance Data Systems (IMDS) or Global Combat Support Systems – 435

Air Force (GCSS-AF) Data Services. The Contractor shall use REMIS, IMDS, GCSS-AF, or 436

Contractor provided databases as necessary to obtain historical field and depot level discrepancy 437 data (e.g. AFTO 349 or equivalent data) in support of maintenance activities and general inquiries. 438

2.2 SERVICE INFORMATION AND FAA AIRWORTHINESS DIRECTIVES 439

2.2.1 Service Information and FAA Airworthiness Directives Review 440

The Contractor shall review publications pertaining to FAA compliance, Operational Safety, 441

Suitability and Effectiveness (OSS&E) and system/component Original Equipment Manufacturer 442

(OEM) information or suggested actions. The Contractor review shall include the following: 443

a. Service Bulletins (SB) 444

b. Service Letters (SL) 445

c. Structural Item Interim Advisories 446

d. Telegraphic Messages issued by the manufacturer of the aircraft 447

e. FAA Notices of Proposed Rule Making (NPRM) 448

f. Airworthiness Directives (AD) 449

g. Alternative Means of Compliance (AMOC) 450

h. Special Airworthiness Information Bulletins (SAIB) 451

i. FAA final rules 452

j. FAA Information for Operators (InFO) 453

k. FAA Safety Alert for Operators (SAFO) 454

l. Maintenance Tips 455

m. Operational Literature (Ops SB, Ops Ltr, etc) 456

n. Service Bulletins and Service Letters from vendors of components/black boxes specifically 457 identified by the Government 458

The Contractor shall attend industry and DoD meetings as needed to remain aware of in-service 459 issues in the commercial fleet including Boeing Fleet Team and Working Together Meetings. 460

Travel is separately authorized by the PCO. 461

NOTE: Service Information and FAA Directive reviews for NT-43A shall identify items 462 potentially applicable to those aircraft, based on the original factory configuration baseline T-43A 463 configuration (AFMC T-43). Such items shall be delivered as a group, monthly. 464

(CDRL XX04) 465

2.2.2 Service Literature Evaluation 466

(Applies to: VC-25A (except a.22, a.25, a.34, e), E-4B (except a.25, a.34, e), C-32A (except 467 a.21, a.22), and C-40B/C (except a.21, a.22), and VC-25B (except a.25)) 468

Except those determined to be informational only or non-applicable, the Contractor shall provide 469 an evaluation for all reviewed publications to the Government IAW following: 470

a. For service publications that include OEM recommended actions, the evaluation letter 471 shall include the following: 472

1. A summary of the activity discussed within the service publication and a brief 473 description of the changes made by any revision 474

2. A summary of benefits gained and/or consequences avoided by incorporation 475 considering the uniqueness of the aircraft mission, maintenance concepts and 476 unique configurations 477

3. A recommendation of Approve (to adopt, accomplish, or comply with all or 478 portion of publication which represents an aircraft inspection, modification, or 479 regulatory compliance action), Disapprove (to not adopt, accomplish, or comply 480 with all or portion of publication), Defer, and/or No Further Action (where the 481 publication corresponds to or is superseded by another publication which has been 482 or will be reviewed and any corresponding actions are addressed by or where the 483 publication has been previously complied with), including Contractor’s rationale. 484

4. Level of recommended incorporation: Field, Depot, Engine Shop Visit (ESV), 485 and/or Component Shop Visit (CSV) 486

5. Contractor Recommended Incorporation Time including threshold for 487 inspection/modifications and repetitive intervals for inspections (both commercial 488 and Air Force equivalent) 489

6. Publication Author (e.g. FAA, Rockwell, Honeywell, etc) 490

7. Publication Type: AD, SB, SL, SAIB, AMOC, Alert SB, and Special Attention 491

SB 492

8. Publication Number 493

9. Publication Title 494

10. Publication Release Date 495

11. Contractor Evaluation Submission Date 496

12. ATA (2 digit level minimum, 4 digit level if available in bulletin) 497

13. CAT Level (as stated by the publication and applicable for Engine SBs only) 498

14. Service publication effectivity by tail number/core engine, referencing group 499 number effectivity based on configuration. 500

15. ADs, SBs, and TCTOs/Airframe Change (AFC) associated with the subject 501 service publication 502

16. Identify (Y/N) if the service publication is software related, where publication 503 relates to new and revised software or software baseline for any level (aircraft, 504 system, component, carry-on, etc.) 505

17. Status of incorporation of previous revisions on each aircraft, engine, landing 506 gear, etc. (status will be determined and tracked from the best available data) 507

18. If an earlier version of the service publication has been completed, identify any 508 additional work requirements necessary 509

19. Identification of aircraft uniqueness or non-standard BCA modification issues 510 and concerns based upon available, published platform Tech Manuals (IPC, AMM, 511 etc.) 512

20. Identify affected Tech Orders and Tech Manuals, as identified in the publication 513

21. Identify (Y/N) if there is a potential for impact on nuclear hardness of the 514 aircraft 515

22. Identification of the applicable Aircraft Structural Integrity Program (ASIP) 516 control point in support of the Individual Aircraft Tracking Program (IATP). 517

23. Identify (Y/N) if there is a potential for impact to electromagnetic interference 518

(EMI), electromagnetic compatibility (EMC), radio frequency (RF) effects, 519 electrical load analysis (ELA), or Emission Security (EMSEC) 520

24. Provide affected discrepancy and replacement data (as needed). 521

NOTE: Government will provide supply data if unavailable to ESS Contractor 522

25. When Boeing warranty coverage is applicable, provide a synopsis of service 523 publication warranty coverage to include aircraft T/N(s) and expiration 524

26. Publication compliance time (as applicable) to include stated threshold for 525 inspection/modifications and repetitive intervals for inspections/modifications 526

27. Identification of existing or upcoming scheduled maintenance requirement(s), 527 such as work/task card number, TCTO number, shop visit work requirement, Time 528

Change Item (TCI), etc., when applicable to the service publication work 529 requirement and/or access 530

28. AD Effective Date (applicable for AD only) 531

29. Identify (Y/N) actions that affect spares if applicable 532

30. Labor hours required to accomplish inspection/modification as listed within the 533 service information publication 534

31. Specific material requirements including nomenclature, part number (P/N), 535 quantity, cost and re-order lead time as listed within the service information 536 publication 537

32. Special tooling requirements including nomenclature, tool part number(s), 538 quantity and tool cost as listed within the service information publication 539

33. Identify corresponding or superseding service publication(s) 540

34. Identify (Y/N) if the service publication affects the applicable programs 541

Extended Operations (ETOPS) configuration or compliance (including ETOPS In-542

Flight Start Program), Reduced Vertical Separation Minimum (RVSM) 543 configuration or compliance, a Principal Structural Element (PSE) (as identified in 544 publication), Maintenance Significant Item (MSI), Critical Safety Item (CSI), and 545 carry-on item 546

NOTE: MSIs and CSIs will be identified by the Government 547

b. For service publications that do not include OEM recommended actions and require 548 explanation beyond what information is included in the service publication, an evaluation 549 letter shall include the following: 550

1. A summary of the activity discussed within the service publication and a brief 551 description of the changes made by any revision 552

2. ADs, SBs, and TCTOs/Airframe Change (AFC) associated with the subject 553 service publication 554

3. Identification of aircraft uniqueness or non-standard BCA modification issues 555 and concerns based upon available, published Tech Manuals (IPC, AMM, etc.) 556

4. A recommendation (as needed), including Contractor’s rationale 557

5. Identify affected Tech Orders and Tech Manuals, as identified in the publication 558

6. Publication Author (e.g. FAA, Rockwell, Honeywell, etc) 559

7. Publication Type: AD, SB, SL, SAIB, AMOC, Alert SB, and Special Attention 560

SB 561

8. Publication Number 562

9. Publication Title 563

10. Publication Release Date 564

11. Contractor Evaluation Submission Date 565

c. For service publications which were reviewed by the Contractor per 2.2.2 and 566 determined to be Informational only, an evaluation letter for each is not required. Instead, 567 the Contractor shall summarize these items in a monthly letter that includes the following: 568

1. Publication Author (e.g. FAA, BCA, CFM, Honeywell, etc.) 569

2. Publication Type: AD, SB, SL, SAIB, AMOC, Alert SB, Special Attention SB, 570 etc. 571

3. Publication Number 572

4. Publication Title 573

d. For non-applicable service publications which were reviewed by the Contractor per 574

2.2.2, an evaluation shall not be provided to the Government. However, the Contractor 575 shall document/record the following in a database or as otherwise prescribed by each 576 program: 577

1. Publication Author (e.g. FAA, BCA, CFM, Honeywell, etc.) 578

2. Publication Type: AD, SB, SL, SAIB, AMOC, Alert SB, Special Attention SB, 579 etc. 580

3. Publication Number 581

4. Publication Title 582

5.…