amendment 0002 FA873022R0001 lebanon airfield ops.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

1. CONTRACT ID CODE

See Block #2

PAGE OF PAGES

2. AMENDMENT/MODIFICATION NO.

3. EFFECTIVE DATE

4. REQUISITION/PURCHASE REQ.NO.

5. PROJECT NO. (If applicable)

6. ISSUED BY AFLCMC/HBAK CODE FA8730 7. ADMINISTERED BY (If other than Item 6) CODE

AIR FORCE MATERIAL COMMAND, USAF

AFLCMC/HBAK

HANSCOM AFB, MA 01731

KATHRYN L. MACKESSY 7812254291

KATHRYN.MACKESSY@US.AF.MIL

8. NAME AND ADDRESS OF CONTRACTOR (No., street, county, State and ZIP Code) (X) 9A. AMENDMENT OF SOLICITATION NO.

FA8730-22-R-0001

X

9B. DATED (SEE ITEM 11)

10A. MODIFICATION OF CONTRACT/ORDER NO.

10B. DATED (SEE ITEM 13)

CODE FACILITY CODE

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

X The above numbered solicitation is amended as set forth in Item 14. The hour and date specified for receipt of Offers X is extended, is not extended.

Offers must acknowledge receipt of this amendment prior to the hour and date specified in the solicitation or as amended, by one of the following methods:

(a) By completing Items 8 and 15, and returning 0 copies of the amendment; (b) By acknowledging receipt of this amendment on each copy of the offer submitted; or (c) By separate letter or telegram which includes a reference to the solicitation and amendment numbers. FAILURE OF YOUR ACKNOWLEDGMENT TO BE RECEIVED AT THE PLACE DESIGNATED FOR THE RECEIPT OF OFFERS PRIOR TO THE HOUR AND DATE SPECIFIED MAY RESULT IN REJECTION OF YOUR OFFER.

If by virtue of this amendment you desire to change an offer already submitted, such change may be made by telegram or letter, provided each telegram or letter makes reference to the solicitation and this amendment, and is received prior to the opening hour and date specified.

12. ACCOUNTING AND APPROPRIATION DATA (If required)

13. THIS ITEM APPLIES ONLY TO MODIFICATION OF CONTRACTS/ORDERS,

IT MODIFIES THE CONTRACT/ORDER NO. AS DESCRIBED IN ITEM 14.

(X )

A. THIS CHANGE ORDER IS ISSUED PURSUANT TO: ( ) THE CHANGES SET FORTH IN ITEM 14 ARE MADE IN THE CONTRACT ORDER NO. ITEM

10A.

B. THE ABOVE NUMBERED CONTRACT/ORDER IS MODIFIED TO REFLECT THE ADMINISTRATIVE CHANGES (such as changes in paying office, appropriation data, etc.) SET FORTH IN ITEM 14, PURSUANT TO THE AUTHORITY OF FAR 43.103(b).

C. THIS SUPPLEMENTAL AGREEMENT IS ENTERED INTO PURSUANT TO AUTHORITY OF:

D. OTHER (Specify type of modification and authority)

E. IMPORTANT: Contractor X is not, is required to sign this document and return copies to the issuing office.

14. DESCRIPTION OF AMENDMENT/MODIFICATION (Organized by UCF section headings, including solicitation/contract subject matter where feasible.)

FMS DW-D-QAM Lebanon Airfield Ops RFP (FA8730-22-R-0001) Amendment 0002, SEE SCHEDULE

The proposal due date is extended to 21 January 2022.

Except as provided herein, all terms and conditions of the document referenced in Item 9A or 10A, as heretofore changed, remains unchanged and in full force and effect.

15A. NAME AND TITLE OF SIGNER (Type or print).

16A. NAME AND TITLE OF SIGNER (Type or print)

RICHARD L. AXTELL, JR.

15B. CONTRACTOR/OFFEROR

15C. DATE SIGNED 16B. UNITED STATES OF AMERICA

16C. DATE SIGNED

(Signature of person authorized to sign)

BY________________________________________

(Signature of Contracting Officer)

NSN 7540-01-152-8070 30-105 STANDARD FORM 30 (REV.10-83)

PREVIOUS EDITION UNUSABLE Prescribed by GSA ConWrite Version 7.5.0.1 FAR (48 CFR) 53.243 Created 23 Nov 2021 10:21 AM

FMS DW-D-QAM

LEBANON AIRFIELD

OPS

REQUEST FOR

PROPOSAL

AMENDMENT 0002

LIST OF ATTACHMENTS

FA8730-22-R-0001 0002 PAGE 2 OF 3

SCHEDULE:

This RFP (FA8730-22-R-0001) Amendment 0002 changes the original solicitation as follows:

A. Section A (Solicitation Cover Page - SF30) is changed as follows:

The proposal due date has been extended from 7 December 2021 to 21 January 2022

B. Section J (Exhibits & Attachments) is chnaged as follows:

1. Attachment 1 - SRD DW-D-QAM LEBANON AIRFIELD OPS has been amended and re-attached to this RFP

2. Attachment 5 - PRICING SPREADSHEET is attached to this RFP

SCHEDULE OF CHANGES

FA8730-22-R-0001 0002

DOCUMENT PGS DATE TITLE

ATTACHMENT 1 TBD 23 NOV 2021 SRD DW-D-QAM LEBANON AIRFIELD OPS

ATTACHMENT 5 1 22 NOV 2021 PRICING SPREADSHEET

System Requirements Document – Lebanon Airfield Ops Program – FMS Case DW-D-QAM

System Requirements Document (SRD)

Lebanon Airfield Operations Program for Hamat and Rayak Air Bases, Lebanon

FMS Case DW-D-QAM

Attachment 1

1. INTRODUCTION

The Lebanon Airfield Operations Program, FMS Case DW-D-QAM, will provide a Doppler VHF Omni

Directional Range/Distance Measuring Equipment (DVOR/DME) system to Hamat Air Base (AB). The program will also provide a DVOR/DME system, a Category I Instrument Landing Systems/Distance

Measuring Equipment (ILS/DME) system, and a Precision Approach Path Indicator (PAPI) to Rayak AB.

The DVOR/DMEs, ILS/DME, & PAPI systems shall be capable of supporting the Lebanese Air Force

(LAF) inventory aircraft and shall support Visual Flight Rules (VFR) and Instrument Flight Rules (IFR).

The systems shall be commercially available and meet or exceed applicable International Civil Aviation

Organization (ICAO) standards

2. REFERENCES

1. ICAO Annex 11 Air Traffic Services

2. ICAO Doc 4444 ATM/501, Procedures for Air Navigation Service Air Traffic Management

3. ICAO Document 8168, Volume 1, Procedures for Air Navigation Services – Aircraft Operations

(PANS-OPS) 5th Edition or Most Current Edition

4. ICAO Annex 10 Aeronautical Telecommunications

5. ISO 9001 or equivalent

6. ICAO Annex 14, Aerodromes, Volume I

7. North Atlantic Treaty Organization (NATO) Standard of Agreement (STANAG) 3316, Edition

10 for Type 1 Approaches

8. Attachment 1, Statement of Work (SOW) Lebanon Airfield Operations Program for Hamat and

Rayak Air Bases, Lebanon, FMS Case DW-D-QAM

9. National Electrical Code (NEC) 2010

10. Unified Facilities Criteria (UFC) 3-510-01, Foreign Voltages and Frequencies Guide with Change

2, 22 September 2009

11. UFC 3-520-01, Interior Electrical Systems with Change 1, 14 December 2010

12. MILSTD 129 Military Marking for Shipment and Storage

3. GENERAL REQUIREMENTS

3.1. FMS Case DW-D-QAM shall provide NAVAID systems to the LAF, as follows:

3.1.1. Hamat AB: one (1) DVOR/DME system.

3.1.2. Rayak AB: one (1) DVOR/DME system, one (1) Category I ILS/DME system, and one (1) PAPI system.

3.2. Equipment and Services

3.2.1. Spares shall be form, fit and functionally identical to and of the same quality as originally installed equipment. All LRU spares must be 100% tested prior to shipment. Spares shall be selected based on actual failure histories and reliability modeling results.

3.2.2. Test equipment shall include, as a minimum, one (1) digital multi-meter, one (1) digital scope, and one (1) digital power meter. All test equipment shall be provided IAW the supplier’s specifications.

3.2.3. Shelter utility telephone from the ILS/Localizer shelter, ILS/Glideslope shelter, DVOR shelter and air traffic control tower (ATCT) Cab, connected through each system’s remote equipment

(RCSU, RSI,…) infrastructure cables running to the ATCT.

3.2.4. Two (2) each VHF/UHF air traffic control (ATC) radios and antennas that may be moved to/from system shelter for the purpose of communicating with the flight commissioning (FC) aircraft and the ATCT. One (1) radio and antenna will be provided to each airbase, Hamat AB and Rayak AB, for use during the NAVAID systems FC process. Radio range shall be adequate for communications with FC aircraft.

3.2.5. The Contractor shall provide Factory Acceptance Test (FAT), site Installation and Check Out

(I&CO) to include a Site Acceptance Test (SAT), and flight commissioning services (including flight certification aircraft and crew, and technical ground support).

3.2.6. The NAVAID systems shall be produced in ISO 9001 qualified facilities or equivalent and be of solid state design.

3.3. Environmental and Mechanical

3.3.1. The Contractor shall provide equipment shelters with dual redundant environmental control units

(ECUs), a ventilation fan, interior lighting and an electrical power distribution system sufficient to maintain the ambient environmental conditions within the operating range of the equipment.

ECUs shall be sourced locally to the extent possible.

3.3.2. In the event of ECU failure to maintain ambient temperatures within the operating range of the equipment, the equipment shall provide an alert to the operator to take manual action to protect from overheating.

3.3.3. The Contractor shall provide an alarm in all shelters that is capable of being activated from the

ATCT Cab with a single switch to signal personnel within the shelters of an inbound aircraft emergency or attack.

3.3.4. The System shelters and antenna structures shall be capable of withstanding wind loads of 100 mph in its installed condition.

3.3.5. Measures shall be implemented to protect all equipment and minimize the effects of environmental conditions normally experienced in Lebanon, such as rust and corrosion, humidity, fog, wind-born sand, high temperatures, and ultra-violet (UV) exposure from extended sunlight.

3.4. Electrical and Communication

3.4.1. All systems shall be capable of using the base provided power of 50Hz, 220VAC.

3.4.2. Circuit breakers and fuses on all AC & DC power lines and internal circuits and surge suppression devices shall be provided for maximum protection for the equipment.

3.4.3. The Contractor shall connect infrastructure electrical power, provided by the LAF, to the systems shelter and terminate on an external electrical power panel.

3.4.4. The Contractor shall connect infrastructure communications, provided by the LAF, to the systems shelter and the ATCT Cab equipment.

3.4.5. The Contractor shall provide infrastructure electrical power and communication cable specifications and site termination locations to the LAF with sufficient time for the LAF to procure and install the cabling prior to system installation. The LAF will terminate the infrastructure cabling at Contractor specified locations.

3.4.6. The Contractor shall provide an Uninterruptable Power Supplies (UPSs) for each systems shelter and sized to power all shelter system equipment for a minimum of two (2) hours continuous operation, but is not required to support ancillary equipment, such as shelter lighting, air conditioning, heating, etc. The UPS shall be sourced locally to the extent possible.

3.4.7. All outside communication and power cables connected to the NAVAID systems shall be equipped with over voltage protection and shall meet best commercial practices for outside cable plant design and installation.

3.4.8. The Contractor shall provide an automatic voltage regulator (AVR) for each system shelter. The

AVR shall be sourced locally to the extent possible.

3.4.9. The Contractor shall provide a backup electrical power generator with an automatic transfer switch (ATS) for each system shelter. The backup generator shall be sourced locally to the extent possible.

3.4.10. Obstruction lights and lightning protection shall be provided for the shelter and antenna system structures.

4. SPECIFIC REQUIREMENTS

4.1. Performance Parameters for DVOR/DME

The two (2) DVOR/DME systems shall include comprehensive remote monitoring and control capabilities and the DME subsystem shall be high power. The DVOR and DME subsystem antennas shall be omni-directional. The DVOR and DME equipment shall be installed in a shelter appropriate for the environmental conditions at both Hamat and Rayak Air Bases, Lebanon.

4.1.1. The DVOR/DME shall consist of a complete dual redundant electronics system including automatic transfer and shutdown

4.1.2. The DVOR/DME shall be microprocessor controlled and designed for ease of installation, high reliability and maximum attention to fail safe characteristics in all monitoring systems.

4.1.3. Remote maintenance monitoring system shall meet the requirements of ICAO Annex 10, Volume

I, and include remote control and status equipment. A Remote Status Indicator (RSI) shall provide a clear DVOR/DME status indication in the air traffic control tower (ATCT) Cab. A

Remote Control and Status Unit (RCSU) shall provide DVOR/DME remote control and status indication in the ATCT Cab.

4.1.4. The DVOR/DME shall include Built-In Test Equipment (BITE) with fault diagnostics to the Line

Replaceable Unit (LRU) level accessible from a remote location (e.g., via modem). BITE shall provide continuous assessment of equipment/system status to identify out-of-tolerance parameters, and assist organizational-level maintenance personnel in identifying/isolating failed

LRUs for repair.

4.1.5. Performance Parameters for DVOR/DME

Parameter Requirement

Primary Power 220 VAC, 50 Hz

Environment (Operating) Equipment must operate within humidity parameters per FAA-G-2100H

Frequency Range 108.0 to 117.975 MHz ±

0.0005% selectable with 50KHz spacing

Transmitter Output Power Adjustable power sufficient to achieve ICAO performance specifications

Modulation Reference phase signal of 30

Hz FM ± 0.01%, center frequency of 9960 Hz ±

0.2%,variable phase signal of 30 Hz AM ± 0.01%, identification signal of 1020 Hz ± 0.01%, and voice of 300 – 3000 Hz ± 3.0 dB amplitude response

Pulse Repetition Rate ------

Receiver Sensitivity ------

Coverage 360° in azimuth, 0 to 40° in elevation

Minimum Range 120 NMi at 20,000 ft altitude

Accuracy (Bearing) ± 2.0 degrees, measured 4 wavelengths from the center of the antenna system

Accuracy (Range) ------

Capacity ------

DME Power Output Output power sufficient to achieve ICAO performance specifications

DME Frequency 960-1215 MHz (any of 252 X or Y channels)

DME Transponder Capacity 100 aircraft

DME Transponder Accuracy ± 0.04 nm

DME Identification Three letter Morse code at 1350 pps ± 25 pps

At the co-located ILS

DME Receiver Sensitivity 70% replies to interrogations at a level of -87 dBm as measured at the cabinet antenna connector

4.2. Instrument Landing System/Distance Measuring Equipment (ILS/DME)

The Category 1 ILS/DME System shall include comprehensive remote monitoring and control capabilities.

The system shall include a low power DME subsystem co-located with and integrated into the Glide Slope

(GS) subsystems, referenced to the approach threshold. The ILS/DME shall meet or exceed ICAO Annex

10 requirements.

4.2.1. ILS/DME shall meet the requirements for Category I precision approaches IAW ICAO Annex 10, Volume I.

4.2.2. ILS/DME shall consist of complete dual redundant electronics systems, including automatic transfer and shutdown.

4.2.3. The DME shall be a low power, small sector directional DME (i.e. ~ +/- 10 degrees of approach vector setting)

4.2.4. Localizer (LOC) antenna systems shall consist of a 14-element (minimum) wide aperture Log

Periodic Dipole (LPD) array of the capture-effect design.

4.2.5. ILS/DME shall be microprocessor controlled, and designed for ease of installation, high reliability and maximum attention to fail safe characteristics in all monitoring systems.

4.2.6. Remote monitoring system shall meet the requirements of ICAO Annex 10 Volume I, and include remote control and status equipment. A Remote Status Indicator (RSI) shall provide a clear

ILS/DME status indication in the air traffic control tower (ATCT) Cab. A Remote Control and

Status Unit (RCSU) shall provide ILS/DME remote control and status indication in the ATCT

Cab.

4.2.7. The ILS/DME shall be provided with Built-In Test Equipment (BITE) with fault diagnostics to the Line Replaceable Unit (LRU) level accessible from a remote location (e.g., via modem).

4.2.8. BITE shall provide continuous assessment of equipment/system status, to identify out-of-tolerance parameters, and assist organizational-level maintenance personnel in identifying/isolating failed LRUs for repair/replacement.

4.3. Performance Parameters for ILS/DME

Requirement Specification

Environment (Operating) Equipment must operate within humidity parameters per FAA-G-2100H

Primary Power 220 VAC, 50 Hz

Standby Power Battery backup system with two (2) hour minimum operation of critical equipment

Localizer Power Output Output power sufficient to achieve ICAO performance specifications

Localizer Frequency 108 – 111.975 MHz ± 0.0005%

Localizer Modulation Tones 90/150 Hz ± 0.01% navigation;

1020 Hz ± 50Hz identification

Localizer Coverage 25 nm within ±10º of the front course line;

17 nm between 10º and 35º of the front course line

Localizer Course Alignment Accuracy at runway threshold

± 0.015 DDM (± 35 ft)

GS Power Output Output power sufficient to achieve ICAO performance specifications

GS Frequency 328.6 – 335.4 MHz ± 0.0005%

GS Modulation Tones 90/150 Hz ± 0.01%

Glide Angle 2 to 4 degrees, adjustable at GS antenna

Glidepath Coverage 10 nm between 1.2 and 7.0 degrees above the horizon, with ± 8 degrees of the runway centerline

Glidepath Alignment Accuracy Within 0.075 θ from θ or ±0.002 DDM

DME Power Output Output power sufficient to achieve ICAO performance specifications

DME Frequency 960-1215 MHz (any of 252 X or Y channels)

DME Transponder Capacity 100 aircraft

DME Transponder Accuracy Transponder accuracy compliant with ICAO specifications

DME Identification Three letter Morse code at 1350 pps ± 10 pps

At the co-located ILS

DME Receiver Sensitivity 70% replies to interrogations at a level of -87 dBm as measured at the cabinet antenna connector

Built-In Test Equipment Automatically isolate faults to a single LRU ≥

80% of the time

Remote Status and Maintenance System MS Windows based; Dial-up capability; Capable of accepting inputs from other NAVAIDS equipment on site

4.4. Precision Approach Path Indicator (PAPI)

The Contractor shall provide one (1) PAPI system at Rayak AB, Lebanon and meet the following requirements.

4.4.1. The PAPI shall meet the requirements specified in ICAO Annex 14, Volume I, Vol.I para.

5.3.5.23 to 5.3.5.45

4.4.2. The average intensity in red light will be at least 15,000 cd for a horizontal beamspread -6°to +6° and a vertical angle of 3.5° below transition. The transition sector will not exceed 3 minutes of arc over the full beam width. The unit will use one pre-focus halogen lamp rated 200 W per light channel. The expected life of the lamps will be not less than 1500 hours at full intensity and typically 4000-6000 hours in actual service

4.4.3. The optical system for each light channel will consist of a high purity aluminum reflector, a red, through-coloured glass filter and two lenses made of optical glass

4.4.4. Lamps and filters will be easily replaceable without need of tools or requiring re-calibration or re-aiming of the PAPI unit

4.4.5. The PAPI unit will be mounted on three or four legs fitted with precision elevation adjustment hardware

4.4.6. The unit will be made from aluminum and fully protected against corrosion. It will be weatherproof

4.4.7. A special imprinted, hardened glass will be provided in front of the lenses to protect them against sandblast and to greatly reduce the time required for clearing any frost that has formed on the front glass. An extended hood will assist in the prevention of frost formation on the unit. A digital aiming device and custom case will be supplied with each system

CLIN CLIN description

0001AA Site Survey - Hamat AB $ 0001AB Site Survey - Rayak AB $

Total

0002AA DVOR/DME - Hamat AB $ 0002AB DVOR/DME - Rayak AB $

Total

0003 ILS/DME & PAPI - RAYAK $

0004AA Warranty 2 years - Hamat AB $ 0004AB Warranty 2 years - Rayak AB $

0005 CLS - Option Year 1 (option) $ 0006 CLS - Option Year 2 (option) $ 0007 CLS - Option Year 3 (option) $ 0008 Warranty 3rd Year (option) $ 0009 Over & Above Option 0010 Contractor Travel 0011 Data

TOTAL $0.00

NSP (not seperately priced)