12024B19R9503_Region_5_CWN_LFW_Air_Attack.pdf

OFFEROR’S COPY

(Ref. 48 CFR 1) Issuing Office:

NATIONAL INTERAGENCY FIRE CENTER

U.S. FOREST SERVICE, CONTRACTING

OWYHEE BUILDING - MS 1100

3833 S. DEVELOPMENT AVE

BOISE, ID 83705 This solicitation can be downloaded from the following Internet site: https://www.fbo.gov/ Offers Are Solicited For:

Call When Needed (CWN) for Air Attack Fixed Wing Aircraft (USFS Region 5)

Solicitation No:

12024B19R9503

Issued Date:

December 4, 2018

IMPORTANT – NOTICE TO OFFEROR

Offers will be due on January 10, 2019 @ 14:00 Mountain Standard Time.

- The offeror shall submit the following items in response to this solicitation:

1. SF-1449, block 17a: Provide address, telephone and DUNS number: blocks 30a-30c:

Complete, date, and sign.

2. Fill in the appropriate information requested in Sections B.1, B.3, B.4, and D.12.

3. Provide two (2) copies of your Business/Technical proposal in response to section E.2 of the solicitation. It is requested that all information on your technical proposal be provided via two (2) thumb drives which are readable by Microsoft Office or Adobe Acrobat.

Provide your responses to Sections E (Representations and Certifications) of the solicitation.

THE SOLICITATION PACKAGE SHALL BE RETURNED TO THE FOLLOWING ADDRESS:

National Interagency Fire Center U.S. Forest Service, Contracting Attn: Solicitation No. 12024B19R9503 3833 S. Development Ave Owyhee Building - MS 1100 Boise, ID 83705-5354

No facsimile (FAX) or e-mail offers will be accepted.

Offeror’s questions must be submitted and received by mail, e-mail or fax NLT December 20, 2018.

E-mail: rhoffman@fs.fed.us. Offerors may contact Robert Hoffman for information about this solicitation at 208-387-5681.

“The policy of the United States Department of Agriculture Forest Service prohibits discrimination on the basis of race, color, national origin, age, religion, sex, disability, family status, and/or political affiliation.” Persons believing they have been discriminated against in any Forest Service related activity should write to: Chief, Forest Service, USDA, P. O. Box 96090, Washington, DC 20090-6090

Previous editions of this form are obsolete. FS-6300-44 (11/79) https://www.fbo.gov/ mailto:rhoffman@fs.fed.us

U.S. Forest Service National Office i

Solicitation No. 12024B19R9503 Region 5 ATGS CWN Light Fixed Wing Aircraft

TABLE OF CONTENTS

SECTION A - SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

STANDARD FORM 1449

SECTION B - SUPPLIES OR SERVICES AND PRICE

B.1 SCHEDULE OF ITEMS

B.2 PROPOSED ADDITIONAL AIRCRAFT

B.3 PROPOSED DAILY AVAILABILITY / AVAILABILITY REDUCTION

B.4 AIRCRAFT

B.5 AGREEMENT PILOT QUALIFICATION

B.6 HOME BASE

B.7 DIRECTOR OF MAINTENANCE

B.8 EXCISE TAXES

B.9 PERFORMANCE PERIOD

B.10 STANDBY HOURS PER DAY

B.11 EXTENDED STANDBY HOURLY RATE

B.12 OVERNIGHT STANDARD PER DIEM RATE

SECTION C - DESCRIPTIONS/SPECIFICATIONS/ATTACHMENTS

C.1 SCOPE OF AGREEMENT

C.2 CERTIFICATIONS

C.3 GOVERNMENT FURNISHED PROPERTY

C.4 AIRCRAFT REQUIREMENTS

C.5 AIRCRAFT MAINTENANCE

C.6 AIRCRAFT AND EQUIPMENT SECURITY

C.7 AVIONICS REQUIREMENTS

C.8 CONTRACTOR-FURNISHED AVIONICS SYSTEMS

C.9 AVIONICS INSTALLATION AND MAINTENANCE STANDARDS

C.10 OPERATIONS

C.11 PERSONNEL

C.12 CONDUCT AND REPLACEMENT OF PERSONNEL

C.13 SUSPENSION AND REVOCATION OF PERSONNEL

C.14 SUBSTITUTION / REPLACEMENT OR ADDITION OF AIRCRAFT

C.15 FLIGHT HOUR AND DUTY LIMITATIONS

C.16 RELIEF PILOT

C.17 PERSONAL PROTECTIVE EQUIPMENT

C.18 ACCIDENT PREVENTION AND SAFETY

C.19 MISHAPS

C.20 INITIAL INSPECTION AND ACCEPTANCE

C.21 INITIAL PRE-USE INSPECTION EXPENSES

C.22 RE-INSPECTION EXPENSES

C.23 INSPECTIONS DURING USE

C.24 AUTHORIZED ORDERING ACTIVITIES

C.25 ORDERING PROCEDURES

C.26 POINT OF HIRE

C.27 ASSIGNED WORK LOCATION(S)

C.28 REIMBURSEMENT FOR MOBILIZATION AND DEMOBILIZATION COSTS

C.29 ORDERING AND PAYMENT FOR ADDITIONAL PILOT

C.30 MISCELLANEOUS COSTS TO THE CONTRACTOR

Solicitation No. 12024B19R9503 U.S. Forest Service Region 5 ATGS CWN Light Fixed Wing Aircraft National Office

TABLE OF CONTENTS

ii

C.31 DAILY AVAILABILITY REQUIREMENTS

C.32 UNAVAILABILITY

C.33 PAYMENT PROCEDURES

C.34 PAYMENT FOR AVAILABILITY

C.35 PAYMENT FOR FLIGHT - FLIGHT TIME MEASUREMENT

C.36 PAYMENT FOR EXTENDED STANDBY

C.37 PAYMENT FOR OVERNIGHT ALLOWANCE

C.38 FOOD AND DRINK

C.39 CONTRACTOR STAND-DOWN OR DEACTIVATION

C.40 COMMERCIAL FILMING AND VIDEOTAPING

C.41 CONDITION INSPECTION GUIDELINES RESTRAINT SYSTEMS

C.42 DEFINITIONS

C.43 ABBREVIATIONS

ATTACHMENT 1 - AUX-FM RADIO INTERFACE FS/OAS A-17

ATTACHMENT 2 - FS/AMD A-24 AVIONICS OPERATIONAL TEST STANDARDS (REV D)

(OCT 2010)

ATTACHMENT 3 - AIRPLANE PILOT QUALIFICATIONS AND APPROVAL RECORD

ATTACHMENT 4 - ADDITIONAL ASSISTANCE

ATTACHMENT 5 - CWN LFW PREUSE INSPECTION FORM

ATTACHMENT 6 - AIRPLANE APPROXIMATE FUEL CONSUMPTION RATES FOR SELECTED

AIRCRAFT

ATTACHMENT 7 - WAGE DETERMINATION

ATTACHMENT 8 - PUBLIC AIRCRAFT OPERATIONS DECLARATION

ATTACHMENT 9 - CPARS EVALUATION FORM

SECTION D - CONTRACT CLAUSES

D.1 52.252-2 CLAUSES INCORPORATED BY REFERENCE (FEB 1998)

D.2 CONTRACT TERMS AND CONDITIONS - COMMERCIAL ITEMS (52.212.4)

(DEVIATION 2017-1) (OCT 2018)

D.3 ADDENDUM TO 52.212-4 CONTRACT TERMS AND CONDITIONS - COMMERCIAL ITEMS

(OCT 2018) CLAUSES INCORPORATED BY REFERENCE

D.4 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT STATUTES OR

EXECUTIVE ORDERS -- COMMERCIAL ITEMS (52.212-5) (OCT 2018) APPLICABLE TO ALL

CLINS EXCEPT FOR CLIN 1.J

D.5 STATEMENT OF EQUIVALENT RATES FOR FEDERAL HIRES (FAR 52.222-42)

(MAY 2014)

D.6 AVAILABILITY OF FUNDS (FAR 52.232-18) (APR 1984)

D.7 PROPERTY AND PERSONAL DAMAGE

D.8 NOTICE OF CONTRACTOR PERFORMANCE ASSESSMENT REPORTING SYSTEM (JULY

2010)

D.9 INSPECTION AND ACCEPTANCE (AGAR 452.246-70) (FEB 1988)

D.10 POST AWARD CONFERENCE (AGAR 452.215-73) (NOV 1996)

D.11 AFFIRMATIVE PROCUREMENT OF BIO BASED PRODUCTS UNDER SERVICE AND

CONSTRUCTION CONTRACT (FAR 52.223-2) (SEPT 2013)

D.12 CONTRACTOR AUTHORIZED SIGNATURES

D.13 OPTION TO EXTEND SERVICES (FAR 52.217-8) (NOV 1999)

D.14 ECONOMIC PRICE ADJUSTMENT SPECIFIED FLIGHT RATE AGREEMENTS

D.15 ECONOMIC PRICE ADJUSTMENT FOR EXTENDED STANDBY

TABLE OF CONTENTS

iii

SECTION E – INSTRUCTIONS TO OFFERORS

E.1 INSTRUCTIONS TO OFFERORS - COMMERCIAL ITEMS (FAR 52.212-1) (OCT 2018)

(TAILORED)

E.2 EVALUATION-COMMERCIAL ITEMS (FAR 52.212-2) (OCT 2014) (TAILORED)

E.3 AWARD PROCESS

E.4 OFFEROR REPRESENTATIONS AND CERTIFICATIONS – COMMERCIAL ITEMS

(FAR 52.212-3) (OCT 2018)

E.5 CERTIFICATION REGARDING RESPONSIBILITY MATTERS (FAR 52.209-5)

(OCT 2015)

E.6 INFORMATION REGARDING RESPONSIBILITY MATTERS (FAR 52.209-7)

(JULY 2013)

E.7 PAST PERFORMANCE INFORMATION

E.8 SAFETY MANAGEMENT SYSTEM (SMS) COMPONENTS QUESTIONNAIRE

SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24, & 30

1. REQUISITION NUMBER

2. CONTRACT NO.

3. AWARD/EFFECTIVE

DATE

4. ORDER NUMBER

5. SOLICITATION NUMBER

12024B19R9503

6. SOLICITATION ISSUE

DATE

12/04/2018

7. FOR SOLICITATION

INFORMATION CALL:

a. NAME

ROBERT M. HOFFMAN

b. TELEPHONE NUMBER (No collect calls)

(208) 387-5681

8. OFFER DUE DATE/

LOCAL TIME

01/10/2019

1400 MT

9. ISSUED BY CODE 10. THIS ACQUISITION IS UNRESTRICTED OR SET ASIDE: 100% FOR:

NATIONAL INTERAGENCY FIRE CENTER

U.S. FOREST SERVICE – CONTRACTING

OWYHEE BUILDING - MS 1100

3833 S. DEVELOPMENT AVE

BOISE, ID 83705-5354

SMALL BUSINESS

WOMEN-OWNED SMALL BUSINESS

(WOSB) ELIGIBLE UNDER THE WOMEN-OWNED

SMALL BUSINESS PROGRAM

HUBZONE SMALL

BUSINESS

ECONOMICALLY DISADVANTAGED

WOMEN-OWNED SMALL BUSINESS

(EDWOSB)

NAICS: 481212

SERVICE-DISABLED

VETERAN-OWNED

SMALL BUSINESS

8 (A)

SIZE STANDARD:

1500 Employees

11. DELIVERY FOR FOB DESTINA-

TON UNLESS BLOCK IS

MARKED

SEE SCHEDULE

12. DISCOUNT TERMS

13a. THIS CONTRACT IS A

RATED ORDER UNDER

DPAS (15 CFR 700)

13b. RATING

14. METHOD OF SOLICITATION

RFQ IFB RFP

15. DELIVER TO CODE 16. ADMINISTERED BY CODE

NATIONAL INTERAGENCY FIRE CENTER

U.S. FOREST SERVICE – CONTRACTING

OWYHEE BUILDING - MS 1100

3833 S. DEVELOPMENT AVE

BOISE, ID 83705-5354

17a. CONTRACTOR/ CODE FACILITY 18a. PAYMENT WILL BE MADE BY CODE

OFFEROR CODE ALBUQUERQUE SERVICE CENTER

INCIDENT BUSINESS – CONTRACTS

101B SUN AVENUE, NE

ALBUQUERQUE, NM 87109 TELEPHONE NO. NINE-DIGIT DUNS NO. .

17b CHECK IF REMITTANCE IS DIFFERENT AND PUT SUCH ADDRESS IN

OFFER

18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK BELOW

IS CHECKED

SEE ADDENDUM

19.

ITEM NO.

20.

SCHEDULE OF SUPPLIES/SERVICES

21.

QUANTITY

22.

UNIT

23.

UNIT PRICE

24.

AMOUNT

SEE SECTION B (ATTACHED)

CALL WHEN NEEEDED FIXED WING AIRCRAFT FOR

ATGS MISSIONS (USFS REGION 5)

25. ACCOUNTING AND APPROPRIATION DATA

26. TOTAL AWARD AMOUNT (For Govt. Use Only)

27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA ARE ARE NOT ATTACHED

27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA ARE ARE NOT ATTACHED

28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN 1 .

COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND

DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY

ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED

HEREIN.

29. AWARD OF CONTRACT: REF. _________________ __ OFFER

DATED _______________ . YOUR OFFER ON SOLICITATION (BLOCK

5), INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE SET

FORTH HEREIN, IS ACCEPTED AS TO ITEMS:

30a. SIGNATURE OF OFFEROR/CONTRACTOR 31a. UNITED STATES OF AMERICA (SIGNATURE OF CONTRACTING OFFICER)

30b. NAME AND TITLE OF SIGNED (Type or print) 30c. DATE SIGNED 31b. NAME OF CONTRACTING OFFICER (Type or print) 31c. DATE SIGNED

AUTHORIZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION NOT USABLE STANDARD FORM 1449 (REV. 5/2011)

Prescribed by GSA - FAR (48 CFR) 53.212

SCHEDULE B

SUPPLIES OR SERVICES AND PRICE

B.1 SCHEDULE OF ITEMS

This is a Basic Ordering Agreement (BOA) for fully operated and maintained light fixed wing aircraft services, on a Call-When-Needed (CWN) basis, for the air tactical group supervision mission in behalf of the Pacific Southwest Region (California), Region 5. Aircraft shall meet the requirements of this schedule and the specifications included herein. Offerors shall list each aircraft to be considered for award. Awards will not be made for aircraft not considered suitable for the Government’s need, or at prices determined to be unreasonable.

B.2 PROPOSED ADDITIONAL AIRCRAFT

Offeror(s) have the option to propose additional aircraft which may be added to this agreement at a later date. These aircraft need not be available or mission ready at the time of award. The following minimum information is needed:

(1) The make/model/year/tail number of the aircraft.

(2) The proposed flight rate(s) of the aircraft.

(3) The proposed daily availability rate(s) of the aircraft.

(4) Estimated date when resource will be mission ready.

These additional aircraft may be added at the discretion of the Regional Aviation Officer (RAO) and the Contracting Officer (CO) and only by modification of the original agreement. When proposing additional aircraft place an *AA after “item” on the aircraft proposal sheet.

Note: If continuance of this BOA is considered to be in the Government’s best interest, the Government will notify Contractors 30 days prior to the annual renewal that they may revise pricing.

B.3 PROPOSED DAILY AVAILABILITY / AVAILABILITY REDUCTION

Offeror(s) shall propose a daily availability (AV) rate for each proposed aircraft using the table below. Offeror(s) may propose an availability reduction rate based on total assigned days per calendar year.

• Daily availability rate (day-by-day)

• Availability rate after 30 days*

• Availability rate after 60 days*

• Availability rate after 90 days*

*Note: Specified days are cumulative from the period beginning January 1 and Ending December 31 annually. Total days need not be consecutive.

Offerors are instructed to complete one schedule for each aircraft offered.

Aircraft Make: ______________________ Aircraft Model: __________________________

Manufactured Year: _________________ Aircraft Tail-Number: _____________________

Empty Weight: _____________________ Certified Max Gross Weight: _______________

Number of Seats: ___________________ Pressurized? (Yes or No): _________________

Horsepower per engine: ______________ Date aircraft would be mission ready: ________

PRICING INFORMATION

ITEM

1 DESCRIPTION UNIT(S) YEAR 1 YEAR 2 YEAR 3 YEAR 4 6 MONTH

EXTEND

1.a AVAILABILITY RATE

FOR DAYS 1-30* DAY $ $ $ $ $

1.b AVAILABILITY RATE

FOR DAYS 31-60* DAY $ $ $ $ $

1.c AVAILABILITY RATE

FOR DAYS 61-90* DAY $ $ $ $ $

1.d AVAILABILITY RATE

FOR DAYS 91+* DAY $ $ $ $ $

1.e HOURLY FLIGHT RATE** HOUR $ $ $ $ $

1.f RATE FOR AN

ADDITIONAL PILOT DAY $ $ $ $ $

1.g EXTENDED STANDBY

(PER HOUR)*** HOUR $51.00 $51.00 $51.00 $51.00 $51.00

1.h MISCELLANEOUS

CHARGES****

1.i TIME AND MATERIAL CLIN

1.j TRAVEL—As directed by the Govt. IAW the FTRs. NTE $30,000 $30,000 $30,000 $30,000 $30,000

*The Daily Availability Rate shall be evenly divisible by 56.

** The Hourly Flight Rate will be subject to adjustment in accordance with (IAW) the terms of D.13 (Economic Price Adjustment Specified Flight Rate Agreements). Refer to Attachment No. 6 for applicable gallons per hour.

***The Extended Standby Hourly Rate will be subject to adjustment in accordance with the terms of D.15 (Extended Standby Hourly Rate).

****Miscellaneous charges examples are airport landing fees, tie-down charges, hanger rental, etc.

B.4 AIRCRAFT

The aircraft furnished shall have certified power plant and airframe log books and other necessary papers substantiating the maintenance, overhaul, and airworthiness history.

Aircraft Performance Requirements

Capable of a minimum 240 KTAS at 18,000 feet pressure altitude, ISA+10C

With:

(A) 800 lb. payload.

(B) 4 hours fuel computed at 18,000 feet pressure altitude, ISA+10C

A minimum single engine service ceiling of 13,000 feet pressure altitude, ISA +10C

With:

(A) 800 lb. payload.

(B) 4 hours of fuel computed at maximum cruise power, 13,000 feet pressure altitude, ISA+10C

Aircraft. The aircraft shall be in airworthy condition throughout the performance period. All equipment required for original certification shall be installed and operable or be deferrable by a Federal Aviation Administration (FAA) approved Minimum Equipment List (MEL). However, all items required by this agreement may not be placed on an MEL as non-operational unless approved by a government Aviation Maintenance Inspector or the CO. As an example the following equipment, when inoperative, cannot be placed on an MEL with the aircraft continuing to be utilized under agreement.

• Emergency Locator Transmitter

• VHF-AM Transceivers

• P25 Digital VHF-FM Transceivers

• Transponder and altitude reporting systems

• Static pressure, altimeter, and automatic altitude reporting systems

All aircraft and installed equipment furnished under this contract shall be operable, free of damage, and in good repair. Aircraft systems and components shall be free of leaks, except within limitations specified by the manufacturer.

The aircraft interior shall be clean and neat. There shall be no un-repaired tears, rips, cracks, or other damage to the interior. All interior materials must meet FAA standards.

The aircraft exterior finish, including the paint, shall be clean, neat, and in good condition (i.e. no severe fading or large areas of flaking or missing paint etc.). High visibility paint schemes are desired. Any corrosion shall be within manufacturer or FAA acceptable limits.

All windows and windshields shall be clean and free of scratches, cracks, crazing, distortion, or repairs, which hinder visibility. Prior to acceptance temporarily repaired windows and windshields shall have permanent repairs completed or shall be replaced.

B.5 AGREEMENT PILOT QUALIFICATION

Pilots performing on this Agreement shall meet the requirements of Section C.11. All pilots offered may be evaluated in accordance with C.11.

B.6 HOME BASE (Base from which aircraft would normally be available)

Offeror shall enter the principle base of operation reflected in their 135 Operation Specifications.

The location reflected shall be a physical location located within the Regional boundary (State of California). The same aircraft number will not be awarded/administered under more than one Forest Service CWN agreement.

Location (Physical Address) State 24 hour phone number Back up phone number:

Fax Number:

Email(s) for ordering point or dispatch:

Note: The Government may inspect the offeror’s operation and maintenance facilities prior to award. The Forest Service provides oversight for its aviation operations as such the Regional Airworthiness and Pilot inspector shall have access to inspect pre-award/post award, and during the life of the agreement.

B.7 DIRECTOR OF MAINTENANCE

Offeror shall provide the name and address of the Director of Maintenance:

Name 24 hour phone number

B.8 EXCISE TAXES

Excise taxes and segment fees shall be included in your agreement price IAW FAR Clause 52.212-4(k) Taxes. The Agreement price includes all applicable Federal, State, and local taxes and duties.

B.9 PERFORMANCE PERIOD

It is anticipated that any Basic Ordering Agreement (BOA) resulting from this solicitation will be in effect for a period of up to four (4) years and six (6) months. The establishment of this BOA is anticipated by March 2019. The initial pricing will be in effect for 12 months after the date of award.

B.10 STANDBY HOURS PER DAY

9 Hours standby per day (Section C.31)

B.11 EXTENDED STANDBY HOURLY RATE

The extended standby pertains to hours on duty beyond the nine (9) hour duty day. Please refer to Section D.15 for information on how this rate is calculated.

B.12 OVERNIGHT STANDARD PER DIEM RATE

Rates as published in the Federal Travel Regulations (See Section C.37 for further explanation).

SCHEDULE C

DESCRRIPTIONS/SPECIFICATIONS/ATTACHMENTS

C.1 SCOPE OF AGREEMENT

(a) The intent of this solicitation and any resultant agreement is to obtain airplanes fully operated by qualified and proficient personnel and equipped to meet specifications contained herein for offered airplanes used in the administration and protection of public lands.

(b) The aircraft furnished may be used for fire support (primarily aerial supervision), project, law enforcement, and administrative flights. If the Contractor agrees to perform law enforcement flights, such agreement shall be in writing.

(c) The Government has Interagency and Cooperative Agreements with Federal and State Agencies and private landholders. Aircraft may be dispatched under this Agreement for such use.

(d) The Government does not guarantee the placement of any orders for service under this Agreement and the Contractor is not obligated to accept any orders. When the Government places an order for services, if the Contractor elects to accept the order, either through written acknowledgement or commencement of performance, an agreement will thereby be established. This agreement will include all of the terms and conditions called out under this

BOA.

C.2 CERTIFICATIONS

(a) Contractors or subcontractors shall hold a current Federal Aviation Administration (FAA) Air Carrier or Operating Certificate. Aircraft offered shall be listed by make, model, series and registration number on the Contracted Operator’s 14 CFR 135 Operating Certificate at time of inspection.

(b) Aircraft shall conform to its approved type design, be maintained and operated in accordance with the requirements of the 14 CFR 135 notwithstanding the aviation regulations of the States in which the aircraft may operate except those requirements specifically waived by the CO.

(c) All passenger-carrying flights shall be conducted in accordance with the Contractor’s/Operator’s 14 CFR part 135 operation specifications, and all FAA approved and accepted manuals.

C.3 GOVERNMENT FURNISHED PROPERTY

(a) If Government Furnished Property (GFP) is provided, the Contractor shall be required to sign a property receipt document. Upon Government request, GFP shall be returned to the Government in accordance with FAR Clause 52.245-1 (AUG 2010).

C.4 AIRCRAFT REQUIREMENTS

(a) Aircraft condition and equipment. The aircraft shall be in airworthy condition throughout the performance period. All equipment required for original certification shall be installed and operable or be deferrable by an FAA approved Minimum Equipment List (MEL).

(1) All aircraft furnished under this Agreement shall be operable, free of damage, and in good working order. Aircraft systems and components shall be free of leaks, except within limitations specified by the manufacturer.

(2) The aircraft interior shall be clean and neat. There shall be no un-repaired tears, rips, cracks, or other damage to the interior. All interior materials shall meet FAA standards.

(3) The aircraft exterior finish, including the paint, shall be clean, neat, and in good condition (e.g., no severe fading or large areas of flaking or missing paint, etc.) Military or other low visibility paint schemes are unacceptable. Any corrosion shall be within manufacturer or FAA acceptable limits.

(4) All windows and windshields shall be clean and free of scratches, cracks, crazing, distortion, or repairs, which hinder visibility. Repairs such as safety wire lacing and stop drilling of cracks are not acceptable as permanent repairs. Prior to acceptance, all temporarily repaired windows and windshields shall have permanent repairs completed or shall be replaced.

(5) Aircraft shall be equipped as required under 14 CFR Part 135 for VFR, IFR, night IFR operations below 24,000ft, flights above 10,000 feet, and flights in Class B Airspace.

In addition, each aircraft shall have:

(i) One strobe light mounted on top of the aircraft, plus a second mounted on the belly; or one white strobe light mounted on each wingtip and on the tail.

(ii) All radio/electronics items including: wiring, antennas, connectors/adapters and hardware, specified herein.

(iii) FAA approved high visibility, pulsating, forward facing conspicuity lighting.

(iv) Fire extinguishers, as required by 14 CFR 135.155, shall be hand-held bottle(s), with a minimum of 1.5 lbs. capacity and 2-B:C rating. Fire Extinguishers shall be maintained in accordance with current NFPA 10 standards and mounted with a quick release attachment accessible to the flight crew while seated.

(6) Each aircraft shall carry current copies of the following:

(i) Basic Ordering Agreement and all modifications. (Digital copies are authorized.)

(ii) The Interagency Airplane Data Record Card or Point-to-Point Aircraft Data Card shall be posted inside the aircraft.

(iii) Aeronautical charts covering area of operation.

Note: The use of electronic flight bags (EFB) is hereby authorized providing the following conditions are met:

- EFB’s used in the aircraft are FAA approved.

- All other Agreement items are readily available to the vendor and agency crew (tablet-style devices only, no laptops).

- Vendors must keep the device adequately charged to allow normal use and have a means of charging the device readily available without reliance on the government.

(7) Flight Hour Meter. Each aircraft shall be equipped with a flight hour meter, installed in a location observable by the pilot and front seat observer while seated. The meter shall measure actual flight time from takeoff to landing in hours and tenths.

(8) Cargo Restraint. The Contractor shall furnish tie downs, net(s), or cargo straps meeting requirements of 14 CFR to restrain cargo while in flight.

(9) Safety Belts. The aircraft furnished under this agreement shall have safety belts for all occupants and shoulder harnesses for front seat occupants meeting requirements of 14 CFR. The shoulder strap and lap belt shall fasten with a metal to metal single point quick release mechanism. Military style harnesses are acceptable. All occupants shall meet the above requirements during takeoffs and landings, when flying within 1,000 feet of the ground, and at other times as specified by the Pilot. Lap belt and shoulder harness condition; the following are NOT acceptable:

(i) Webbing. Webbing that is frayed 5 percent or more, torn webbing, crushed webbing, swelled webbing that results in twice the thickness of original web, or if difficult to operate through hardware, creased webbing (no structural damage allowed), and sun deterioration if it results in severe fading, brittleness, discoloration, and stiffness.

(ii) Hardware. Buckle or other hardware is inoperable, nylon bushing at shoulder harness-to-lap belt connection missing or damaged, fabricated bushings or tie wraps used as bushings, rust/corrosion if not minor in nature, wear beyond normal use.

(iii) Stitches. Broken or missing stitches, severe fading or discoloring, inconsistent stitch pattern.

(iv) Technical Standard Order (TSO) Tags (see 14 CFR 21.607). Missing or illegible tags are unacceptable unless inspection can confirm the suitability of installed equipment.

(v) Belts/fabric over 10 years from date of manufacture require close inspection because of the elements they are exposed to, but do not have to be replaced if it can be determined they are in serviceable condition and not life limited.

(10) First Aid Kit (Aeronautical). First aid kit shall be in a dust-proof and moisture-proof metal or heavy plastic container. The kit shall be readily accessible to the pilot and passengers. The contents will include the following minimum items:

Item Description Quantity Adhesive bandage compresses (3 inches long) 8 Antiseptic or alcohol wipes (packets) 10 Bandage compresses, (4 inches) 4 Triangular bandage compresses, 40 inch (sling) 2 Roller bandage, 4 inch x 5 yards (gauze) 2 Adhesive tape, 1 inch x 5 yards (standard roll) 1 Bandage scissors 1 Body Fluids Barrier Kit: 1

2-pair of latex gloves 1-face shield 1-mouth-to-mouth barrier 1-protective gown 2-antiseptic towelettes 1-biohazard disposal bag

Notes: Splints are recommended if space permits. Kits may be commercially available types which are FAA approved for the appropriate numbers of crew and passengers carried.

(11) Survival Kit. Aircraft will have sufficient equipment to sustain personnel for a 24-hour period. As a minimum, the survival kit will include the following:

Item Knife Aviation Type Signal Flares (6-each) Space Blanket (1-per occupant) Food (2-days emergency rations per occupant) Collapsible Water Bag Signal Mirror Matches (2-small boxes in waterproof containers) Water (1-quart per occupant {not required when operating over areas with adequate drinking water) Candles Whistle Nylon Rope or Parachute Cord (50 feet)

Note: A hand-held 760 channel VHF transceiver radio or satellite phone is recommended. It should be located on a crewmember rather than placed in the aircraft survival kit.

C.5 AIRCRAFT MAINTENANCE

(a) Aircraft Maintenance

(1) Offered aircraft shall be maintained in accordance with the OEM’s most recent revision of inspection program applicable to the serial number of the aircraft being inspected or an inspection program approved by the FAA under the Contractor’s 14 CFR 135 operations specification. All maintenance shall be accomplished in accordance with the standards established by 14 CFR Part 43, 91, and 135 standards and this Agreement.

(2) The Contractor shall identify the maintenance facilities and/or maintenance personnel used to fulfill the requirements of this Agreement.

(3) Aircraft operated with components and accessories on approved Time Between Overhaul (TBO) extension programs are acceptable, provided the Contractor who provides the aircraft is the holder of the approved extension authorization (not the owner, if the aircraft is leased), and shall operate in accordance with the extension.

(4) Offered aircraft shall be in compliance with all applicable FAA Airworthiness Directives (AD’s) as per 14 CFR 91.417 (a)(2)(v), and Service Bulletins (SB’s) with a time compliance requirement, referenced in an FAA Special Airworthiness Information Bulletin (SAIB) or are designated mandatory by the manufacturer.

(5) Each aircraft’s maintenance schedule shall include mandatory component retirement, replacement or overhaul time as specified in the OEM Airworthiness Limitations Section or equivalent OEM document and shall be in compliance with them.

(6) Each aircraft shall be in compliance with all OEM (recommended or mandatory) programs, documents and resultant inspections from programs such as Continued Airworthiness Programs (CAP), Structural Inspection Documents (SID), Supplemental Structural Inspection Documents (SSID) Corrosion Prevention and Control Programs (CPCP) and Electrical Wiring Interconnection Systems (EWIS) programs.

(7) Contract performance may subject the aircraft engine to frequent smoke, and ash ingestion. All aircraft shall comply with the erosion inspection procedures at the recommended intervals in accordance with the engine operation and maintenance manual for the Contracted aircraft.

(b) Maintenance Records

(1) All maintenance shall be accomplished in accordance with the standards established by 14 CFR Part 135; Advisory Circular (AC) 43.13, and the manufacturer's instructions and in accordance with those procedures established in the Contractor's maintenance program approved under 14 CFR Part 135 Operations Specifications.

(2) All maintenance performed shall be recorded in accordance with 14 CFR 43 and 91 including aircraft time-in-service and hour meter reading.

(3) A copy of the current maintenance record, required by 14 CFR 91.417(a)(2) shall be kept with the aircraft; Aircraft Permanent records shall be kept at the Home Base or maintenance facility. Additionally, All aircraft maintenance record entries and aircraft flight logs shall be transmitted to the operator’s home base (location the certificate is held) every 25 flight hours or seven (7) days - whichever occurs first.

(4) Aircraft Maintenance records shall be maintained in accordance with the FAA, AC;

No. 43-9C as revised.

(c) Maintenance Scheduling

(1) Contractor shall notify the Contracting Officer at least 16 flight hours prior to the initiation of any maintenance inspection. In addition the Contractor shall immediately notify the CO of any change of an engine, power train, control, or major airframe component and circumstances inducing the change.

(2) Routine maintenance shall be performed before or after the daily standby or as approved by the CO.

(3) Inspections shall be performed in a maintenance facility, host or alternate base, or in the best field conditions available.

(4) When any non-scheduled maintenance or repairs are performed due to mechanical or equipment deficiencies, a Government Aircraft Maintenance Inspector and the Contracting Officer shall be notified for "return to contract available” status, before the aircraft performs under the contract.

(d) Maintenance Flight

(1) A functional check flight shall be performed at the Contractor's expense following overhaul, repair, and replacement of any engine (installations of reciprocating engines that are new, rebuilt, or overhauled shall accumulate three (3) hours of operation, including two (2) hours in flight, prior to Government use), power train, or control equipment, and following any adjustment of the flight control systems before the aircraft resumes service under this Agreement. The result of any test flight shall be logged in the aircraft flight records by the Pilot. Results of test flights shall be reported to the U.S.

Forest Service Aircraft Maintenance Inspector (AMI) before the aircraft is returned to availability.

(e) Aircraft Weighing

(1) The aircraft’s required weight and balance data shall be determined by actual weighing of the aircraft every 36 calendar months for multi-engine aircraft. Mission Use Only single engine aircraft shall be weighed within the previous five (5) years. Data shall include an accurate and updated equipment list.

(2) All weighing of aircraft shall be performed on scales that have been certified as accurate within the previous one (1) year. The certifying entity may be any accredited weights and measures laboratory using standards traceable to the National Institute of

Standards and Technology (NIST). The scales should be listed by make model and calibration date in the aircrafts weight and balance documentation.

(3) Authorized Break - There will be no authorized break or period unless the aircraft has been assigned for 18 consecutive or more days and is coordinated with the CO and the regional AMI. The maximum allowed break or period shall not exceed 24 hours.

(f) Mechanics

(1) Mechanics or FAA part 145 Repair Stations assigned to work on aircraft shall have appropriate FAA certification and ratings.

(2) When the aircraft is not available due to required unscheduled maintenance, a pilot may function as a mechanic only if they possess a valid FAA mechanic certificate with the appropriate airframe and/or power plant ratings.

(3) Any time during which the pilot is engaged in mechanic duties performing unscheduled maintenance will apply against the pilot's duty day limitations. All time in excess of two (2) hours (not necessarily consecutive) must also apply against the pilot's flight limitations. After two (2) hours, every hour spent as a mechanic will be applied against pilot flight time limitation one-to-one.

(4) Only a certificated mechanic (holding an airframe and power-plant rating) or FAA part 145 Repair Station may perform scheduled maintenance and inspections. The primary or relief pilot on duty as a pilot must not perform scheduled maintenance and inspections.

(5) All mechanics and repair stations shall maintain the aircraft in accordance with requirements specified within this Agreement. The mechanic or repair station shall meet the requirements of 14 CFR Part 43.7

(6) Within any 24 hour period, personnel shall have a minimum of eight (8) consecutive hours off duty immediately prior to the beginning of any duty day. Local travel up to a maximum of 30 minutes each way between the work site and place of lodging shall not be considered duty time. When one way travel exceeds 30 minutes, the total travel time shall be considered as part of the duty day.

(7) Mechanics shall have two (2), 24 hour time periods off duty during any 14 day period.

(8) Duty includes standby, work, or alert status at any location.

(9) Mechanics may be removed from duty for fatigue or other causes created by unusually strenuous or severe duty before reaching duty limitations.

(10) The mechanic shall be responsible to keep the Government apprised of their ground duty limitation status.

C.6 AIRCRAFT AND EQUIPMENT SECURITY

(a) The Contractor is responsible for the security of their aircraft, vehicles and associated equipment used in the support of this contract.

(b) Aircraft shall be electrically and/or mechanically disabled by two (2) independent security systems whenever the aircraft is unattended.

(c) Deactivating security systems shall be incorporated into preflight checklists to prevent accidental damage to the aircraft or interfere with safety of flight.

(d) Examples of Unacceptable Locking Devices and Methods:

(1) Locking aircraft doors

(2) Fenced or gated parking area

C.7 AVIONICS REQUIREMENTS

(a) It is required that a complete set of schematic and wiring diagrams, covering all installed avionics systems be available at vendors Principal Base of Operations or maintenance facility.

(b) Required avionics systems and contractor offered avionics/communication equipment must meet the performance specifications as specified in FS/OAS A-24 at:

http://www.nifc.gov/NIICD/documents.html

(c) In order to facilitate field maintenance, a complete set of the wiring and schematic diagrams covering all installed avionics systems in the aircraft, shall be carried aboard each aircraft.

(d) Each aircraft shall be supplied a laptop computer and software with appropriate cable to support programming of VHF-FM radios and utilize programming ports.

C.8 CONTRACTOR-FURNISHED AVIONICS SYSTEMS

(a) The following required avionics systems shall be furnished, installed, and maintained by the Contractor in accordance with the manufacturer’s specifications and the installation and maintenance standards. All avionics systems, radios, components and other electronics shall be readily accessible for maintenance, and shall not interfere with passenger space or comfort.

(See Exhibit 7 for “preferred” configuration)

(1) Minimum Requirements:

(i) Three 760 VHF-AM Radios (COM 1, COM 2, COM 3)

(ii) Three VHF-FM Radios (FM 1, FM 2 & FM 3)

(iii) Separate Audio Control systems for the pilot, forward observer, and aft observer. (Total of three (3))

(iv) Dual VOR/LOC receiver systems http://www.nifc.gov/NIICD/documents.html

(v) Glide slope receiver system

(vi) Marker beacon receiver system

(vii) DME transceiver system

(viii) Autopilot system (three-axis preferred) that is STC’d for the make and model of aircraft offered.

(ix) Global Positioning System with moving map display.

(x) ELT Emergency Locator Beacon

(xi) An Automated Flight Following system (AFF)

(xii) One Mode S Transponder

(xiii) One Altimeter and Automatic Pressure Altitude Reporting system

(xiv) Automatic Dependent Surveillance-Broadcast (ADS-B) system “In” & “Out”

(xv) TCAS or TAS

(xvi) Class B Terrain Awareness and Warning System (TAWS)

(xvii) One Satellite Weather system with XM Aviator subscription or equivalent to be displayed upon a screen that is visible to both the PIC and SIC.

(xviii) VHF-FM Programming Ports

(xix) Three (3) dual USB Charging Ports

(2) Avionics Specifications: All required avionics systems shall be furnished, installed, and maintained by the Contractor in accordance with the manufacturer’s specifications and the installation and maintenance standards of this section.

(3) Communications Systems: Transmitters shall not open squelch on, or interfere with, other AM or FM transceivers on the aircraft which are monitoring different frequencies.

Transmit interlock functions shall not be used with communication transceivers.

VHF-AM Transceivers

(i) VHF-AM radios may be integrated into a NAV/COM instrument. All radios must be in a location accessible, visible and easily manipulated by the forward observer.

(ii) VHF-AM radios shall be TSO approved aeronautical transceivers, permanently installed, and operate in the frequency band of 118.000 to 136.975 MHz with a minimum of 760 channels in no greater than 25 KHz increments.

Transmitters shall have a minimum of 5 Watts carrier output power and shall not open squelch on, or interfere with, other AM or FM transceivers on the aircraft monitoring different frequencies.

VHF-FM Transceivers

(iii) Cockpit Radio Panel configuration: a minimum of two (2) FM radios, front panel mounted and grouped in contact with each other. The third FM radio must be in a location accessible, visible and easily manipulated by the forward observer.

(iv) All aircraft approved for fire operations shall use P25 Digital VHF-FM transceivers meeting the specifications of FS/OAS A-19. FM radios used in all aircraft shall be agency approved. FS/OAS A-19 and a list of currently approved FM radios can be found on the following website:

http://www.nifc.gov/NIICD/documents.html . The following requirements shall be met.

(v) VHF-FM radios shall be aeronautical transceivers, permanently installed in a location that is convenient to the PIC and SIC/observer, and operate in the frequency band of 138 to 174 MHz. All usable frequencies shall be programmable in flight. Narrowband and digital operation shall be selectable by channel for both MAIN and GUARD operation. Carrier output power shall be 6- 10 Watts nominal.

(vi) One transceiver shall have a GUARD capability constantly monitoring

168.625 MHz and have a tone of 110.9 on all GUARD transmissions.

Simultaneous monitoring of MAIN and GUARD is required. Scanning of GUARD is not acceptable. Aircraft not approved for Air Tactical operation only require one FM GUARD receiver.

(vii) Transceivers shall have the capability of encoding CTCSS sub audible tones on all channels. A minimum of 32 tones meeting the current TIA/EIA-603A standards shall be selectable.

(viii) Transceivers shall have the capability to display both receiver and transmitter frequencies. Activation indicators for transmit and receive shall be provided for both MAIN and GUARD operation.

(ix) The radio shall use an external broadband antenna covering the frequency band of 138 to 174 MHz (Comant CI-177-1 or equivalent).

(3) Audio Systems: PTT radio transmit will mix with and not mute all other radio receive audio.

(4) Intercom systems (ICS): ICS shall integrate with the aircraft audio control systems and mix with selected receiver audio. An ICS volume control and “hot mic” capability shall be provided for the pilot, forward observer, and aft observer. Passenger volume adjustments shall not affect the PIC. Hot mic may be voice activated (VOX) or controlled via an activation switch. The PIC shall have an isolation capability.

(5) Audio Control Systems:

(i) A separate audio control system shall be installed for the pilot, forward observer, and aft observer, which provide control, selection, and operation of multiple radio transceivers. Audio control panels shall not be combined in a single unit. Identical audio system controls shall be provided for the pilot, forward observer, and the aft observer, to select specific receiver audio outputs and transmitter microphone/PTT inputs of multiple radios. The aft observer audio control panel shall be located to provide adequate lighting for visibility during normal operating periods and all switches, dials and components are visible and located in an area where access to all controls are easily manipulated. An intercom system shall also be provided for the pilot, forward observer, and both aft observers.

(ii) Separate audio level controls shall be provided for the pilot, forward observer, and preferred for aft observer to independently adjust the intercom and receiver audio outputs to their respective headsets. Independent volume controls are required for each receiver.

(iii) Controls for the pilot, forward observer and preferred for aft observer shall independently adjust headphone volume for each communications receiver.

These controls shall be a built in, integral part of each audio controller.

(iv) Controls for transmitter selection and independent receiver selection of all required radios shall be provided for each required audio control system. Each system shall have the capability to simultaneously select and utilize a different transmitter. Side-tone shall be provided for the user as well as for cross monitoring by all installed systems. Receiver audio shall be automatically selected when the corresponding transmitter is selected. Receiver audio shall be provided to each position which requires ICS. Aft audio control systems are not required to provide NAV audio. All required passenger positions shall utilize the aft observer’s audio control system.

(v) Audio controls shall be labeled as COM 1, COM 2, COM 3, FM 1, FM 2, FM 3, etc. with the corresponding transceiver labeled to match and grouped in a sequence of all COM’s and FM’s (no mixing of COM’s and FM’s (unacceptable example being; COM1, FM1, COM2, FM2, COM3, FM3)). Audio shall be free of distortion, noise, or crosstalk. The system shall be designed for use with 600 ohm earphones and carbon equivalent, noise cancelling, boom type microphones. All required positions shall have JJ-033 and JJ-034 type microphone and headphone jacks separated by no more than 4 inches.

(vi) Crew positions shall have radio Push-To-Talk (PTT) switches on their respective flight controls. A PTT switch shall be provided to allow the forward observer to transmit without touching the flight controls.

(6) Aft Audio Control System: The audio controller shall be installed in a location that provides the operator in the aft observer position unobstructed access to the controls while seated. Aft passengers shall utilize this audio control system. If multiple aft audio controllers are installed, passengers shall utilize the most logical system.

(7) Navigation Systems

Global Positioning Systems (GPS), panel-mounted Aeronautical GPS units shall be permanently installed in the aircraft. The GPS shall: utilize WGS-84 datum; reference latitude and longitude coordinates in the DM (degrees/minutes/decimal minutes) mode;

utilize an approved, fixed, external aircraft antenna; and be powered by the aircraft electrical system. The GPS unit must have the ability for manual entry of waypoints in flight. The GPS installation shall be FAA-approved (or approval pending). Handheld and/or marine type equipment is not acceptable.

The GPS shall have a current navigation database (VFR and in route not over one (1) year old and IFR approach units not over 28 days old) covering the continental United States and Alaska, installed in the unit.

GPS with Moving Map. The GPS providing data to the moving map shall meet all of the above GPS requirements. The moving map’s display shall be at least 4.4 inches wide,

1.9 inches high, and show the aircraft’s present position relative to user selected waypoints and geographical features. The map may be integrated with the GPS.

(8) Surveillance Systems

(i) Emergency locator transmitters shall be automatic-fixed, installed in a conspicuous or marked location, and meet the requirements detailed in 14 CFR

91.207 (excluding section f). ELT antennas shall be mounted externally to the aircraft unless installed in a location approved by the aircraft manufacturer. TSO C91a or newer ELTs are required. Documentation of bi-annual registration from the National Oceanic and Atmospheric Administration (NOAA) is required for all TSO C126 and newer ELTs.

(ii) Automated flight following systems shall be compatible with the government’s tracking program (AFF.gov), utilize satellite communications, and use aircraft power via a dedicated circuit breaker. AFF shall be functional in all phases of flight and in all geographic areas where the aircraft will operate. The following additional requirements shall be met.

(A) A subscription service shall be maintained through the equipment provider allowing position reporting via the Government AFF Program.

The reporting interval shall be every two (2) minutes while in flight.

(B) AFF equipment shall be registered with AFF.gov providing all requested information. Changes to equipment and registration information shall be reported to AFF.gov ensuring the program is current prior to aircraft use. For assistance, the Fire Applications Help Desk (FAHD) may be reached at (866) 224-7677 or (360) 326-6002.

(C) An AFF operational test shall be performed prior to the annual compliance inspection. This test shall ensure that the system meets all requirements and is displayed in the AFF viewer with the correct information. A user name and password are required. Registration and additional information are available at https://www.aff.gov/.

https://www.aff.gov/

(D) If AFF becomes unreliable the aircraft may, at the discretion of the Government, remain available for service utilizing radio/voice systems for flight following. The system shall be returned to full operational capability within 5 calendar days after the system is discovered to be unreliable.

(E) This clause incorporates the Specific Section Supplement available at https://www.aff.gov/contractspecs.asp as if it was presented as full text herein.For questions about current compatibility requirements contact the AFF Program Manager listed under contacts at https://www.aff.gov

(9) Transponders: Systems shall meet the requirements of 14 CFR 91.215(a). Part 135 aircraft shall meet the “Mode S” requirements of 14 CFR 135.143(c). Transponder systems shall be tested and inspected every 24 calendar months as specified by 14

CFR 91.413.

(10) Altimeter and Automatic Pressure Altitude Reporting systems: Altimeter, static pressure, and automatic pressure altitude reporting systems shall be installed and maintained in accordance with the IFR requirements of 14 CFR Part 91. These systems shall be tested and inspected every 24 calendar months as specified by 14 CFR 91.411.

(11) Automatic Dependent Surveillance-Broadcast (ADS-B) system: ADS-B “IN” and “OUT” will be required for this contract by January 1st, 2020. All required equipment must meet contract specifications and the requirements detailed in 14 CFR 91.225, 91.227, & AC 20-172. ADS-B “IN” receivers must have the capability of receiving both 978 UAT and 1090 ES frequencies to allow capability of viewing all ADS-B “Out” equipped targets.

ADS-B Out equipment must be compliant with either Technical Standard Order (TSO)- C154c (Universal Access Transceiver) or TSO-C166b (1090 ES). Aircraft operating in Class A airspace are required to be equipped with avionics certified to TSO-C166b.

(12) Traffic Advisory System: One Active Traffic Advisory System (TAS) such as the BF Goodrich Skywatch (SKY 497), Ryan 9900 BX TAS or equivalent which meets the following specifications:

(i) The system must incorporate a separate horizontal situation display that indicates the presence and relative location of intruder aircraft, and an aural alert informing the crew of a Traffic Advisory (TA). The display must be easily readable under normal cockpit conditions and must be in a location convenient to the Pilot and the Observer. The system may be interfaced with a multi-function display such as a GNS-530 rather than installing a separate display.

(ii) The system must be capable of tracking up to 30 intruder aircraft and displaying the eight (8) most threatening. As a minimum, the system must be capable of displaying aircraft that are within two (2) NM of own aircraft.

(iii) The system must be capable of three (3) display modes: Normal (+or – 2700ft), Look-up (-2700 ft to +9000 ft), and Look-down (-9000 ft to +27000 ft).

(iv) The system must provide a pilot-initiated self-test function. The aural alerts shall be announced in a high-fidelity, distinguishable voice and must be heard in https://www.aff.gov/contractspecs.asp https://www.aff.gov/ the headsets of the Pilot and the Forward Observer. The forward observer position shall have the ability of turning off audio alerts.

(v) The installation of the (TAS) components shall be accomplished in accordance with the system manufacturer’s installation data and recommendations. The installation must be FAA approved.