Solicitation_-_AG-0116-S-15-0006_-_Fixed_Wing_BPA_.pdf

SEE ADDENDUMIS CHECKED

CODE 18a. PAYMENT WILL BE MADE BY

CODE

FACILITYCODE

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

OFFEROR

KETCHIKAN AK 99901

648 MISSION STREET

ALASKA REGION 10 - CONTRACTING

USDA FOREST SERVICE

CODE 16. ADMINISTERED BYCODE

X

X

X

481211

SIZE STANDARD:

100.00 % FOR:SET ASIDE:UNRESTRICTED OR0116

RFPIFB

10. THIS ACQUISITION ISCODE

RFQ

14. METHOD OF SOLICITATION

13b. RATING

NAICS:

SMALL BUSINESS

02/23/2015 1400 AS

01/21/2015

(907)228-6244RONALD SMITH

(No collect calls)

INFORMATION CALL:

FOR SOLICITATION 8. OFFER DUE DATE/LOCAL TIMEb. TELEPHONE NUMBER a. NAME

4. ORDER NUMBER3. AWARD/ 6. SOLICITATION

AG-0116-S-15-0006

5. SOLICITATION NUMBER

SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS 1. REQUISITION NUMBER PAGE OF

1 86 OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24, & 30

TELEPHONE NO.

17a. CONTRACTOR/

15. DELIVER TO

KETCHIKAN AK 99901

648 MISSION STREET

TONGASS NF KETCHIKAN AREA FED BLDG

9. ISSUED BY

7.

2. CONTRACT NO.

EFFECTIVE DATE

1,500

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

ISSUE DATE

DELIVERY FOR FOB DESTINA-

TION UNLESS BLOCK IS

MARKED

11.

SEE SCHEDULE

12. DISCOUNT TERMS

THIS CONTRACT IS A

RATED ORDER UNDER

DPAS (15 CFR 700)

13a.

SERVICE-DISABLED

VETERAN-OWNED

SMALL BUSINESS

HUBZONE SMALL

BUSINESS

8(A)

USDA FOREST SERVICE

WOMEN-OWNED SMALL BUSINESS

(WOSB) ELIGIBLE UNDER THE WOMEN-OWNED

SMALL BUSINESS PROGRAM

EDWOSB

24.

AMOUNT

23.

UNIT PRICE

22.

UNIT

21.

QUANTITY

20.

SCHEDULE OF SUPPLIES/SERVICES

19.

ITEM NO.

Alaska Region 10 - Tongass and Chugach Fixed-Wing Aviation Transportation Services

Blanket Purchase Agreement (BPA).

See attached.

REPONSES ARE DUE: February 23rd, 2015 @ 2:00 PM.

Quotes may be mailed or sent attached email to the Contracting Officer. Facsimile (faxed) bids will NOT be accepted.

(Use Reverse and/or Attach Additional Sheets as Necessary)

HEREIN, IS ACCEPTED AS TO ITEMS:

X

XX

DATED

RONALD P. SMITH

. YOUR OFFER ON SOLICITATION (BLOCK 5),

INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE SET FORTH

COPIES TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND DELIVER

ARE

ARE

31c. DATE SIGNED

27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA

31a. UNITED STATES OF AMERICA (SIGNATURE OF CONTRACTING OFFICER)

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

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

SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED.

27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA

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

OFFER

STANDARD FORM 1449 (REV. 2/2012)

Prescribed by GSA - FAR (48 CFR) 53.212

ARE NOT ATTACHED.

ARE NOT ATTACHED.

AUTHORIZED FOR LOCAL REPRODUCTION

PREVIOUS EDITION IS NOT USABLE

30b. NAME AND TITLE OF SIGNER (Type or print)

30a. SIGNATURE OF OFFEROR/CONTRACTOR

28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN

25. ACCOUNTING AND APPROPRIATION DATA

29. AWARD OF CONTRACT:

REF.

32e. MAILING ADDRESS OF AUTHORIZED GOVERNMENT REPRESENTATIVE

32c. DATE 32b. SIGNATURE OF AUTHORIZED GOVERNMENT REPRESENTATIVE

ACCEPTED, AND CONFORMS TO THE CONTRACT, EXCEPT AS NOTED:

32a. QUANTITY IN COLUMN 21 HAS BEEN

RECEIVED INSPECTED

40. PAID BY39. S/R VOUCHER NUMBER38. S/R ACCOUNT NUMBER

37. CHECK NUMBER

FINALPARTIAL

36. PAYMENT

FINALPARTIAL

35. AMOUNT VERIFIED

CORRECT FOR

34. VOUCHER NUMBER33. SHIP NUMBER

COMPLETE

32g. E-MAIL OF AUTHORIZED GOVERNMENT REPRESENTATIVE

42d. TOTAL CONTAINERS42c. DATE REC'D (YY/MM/DD)

42b. RECEIVED AT (Location)

42a. RECEIVED BY (Print)

41c. DATE41b. SIGNATURE AND TITLE OF CERTIFYING OFFICER

41a. I CERTIFY THIS ACCOUNT IS CORRECT AND PROPER FOR PAYMENT

STANDARD FORM 1449 (REV. 2/2012) BACK

24.

AMOUNT

23.

UNIT PRICE

22.

UNIT

21.

QUANTITY

20.

SCHEDULE OF SUPPLIES/SERVICES

19.

ITEM NO.

32f. TELEPHONE NUMBER OF AUTHORIZED GOVERNMENT REPRESENTATIVE

32d. PRINTED NAME AND TITLE OF AUTHORIZED GOVERNMENT REPRESENTATIVE

86 2 of

TABLE OF CONTENTS

SECTION A – SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS

Standard Form 1449

SECTION B – SUPPLIES OR SERVICES AND PRICES

B-1 Schedule of Items

B-2 Government Furnished Pilot

B-3 Home Base

B-4 Fuel Price Basis

B-5 Maintenance Capability

B-6 Vendor Offered Avionic Requirements

B-7 Additional Information to Be Submitted

SECTION C – DESCRIPTION/SPECIFICATIONS/WORK STATEMENT

C-1 Scope of Contract

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 or Replacement of Personnel, Aircraft, and Equipment

C-15 (RESERVED)

C-16 Flight Hour and Duty Limitations

C-17 Accident Prevention and Safety

C-18 Mishaps

3 Alaska Region 10 - Fixed Wing Transportation Services BPA

C-19 Personal Protective Equipment

C-20 Inspection and Acceptance

C-21 Pre-Use Inspection Expenses

C-22 Re-Inspection Expenses

C-23 Inspections During Use

C-24 Contract Period and Renewal Options

C-25 Authorized Ordering Activities

C-25a BPA Award Information…………………………………………………………………………….28

C-26 Ordering Procedures

C-27 Point of Hire

C-28 Assigned Work Location(s)

C-29 Payment Definitions

C-30 BPA Payment Procedures

C-31 Payment for Flights

C-32 Payment for Standby

C-33 Reserved

C-34 Minimum Charge

C-35 Cancellation Charge

C-36 Ordering and Payment for Additional Personnel

C-37 Additional Aircraft after Contract Award

C-38 Payment for Substitute/Replacement Aircraft

C-39 Lodging and Meals

C-40 Reserved

C-41 Payment for Overnight Allowances

C-42 Miscellaneous Costs to the Contractor

C-43 Definitions

C-44 Abbreviations

C-45 Exhibits, List of Attachments

EXHIBIT 01 Department of Labor, Wage Determinations EXHIBIT 02 Performance by Government-Furnished EXHIBIT 03 Restrain Systems Condition Inspection Guidelines EXHIBIT 04 Modification of Flight Service Blanket Purchase Agreement Form EXHIBIT 05 Additional Assistance

4 Alaska Region 10 - Fixed Wing Transportation Services BPA

EXHIBIT 06 Operations and Safety Information for Pilot EXHIBIT 07 Performance Report

SECTION D – CONTRACT CLAUSES

D-1 52.252-2 -- CLAUSES INCORPORATED BY REFERENCE (FEB 1998)………………… ……………………. 51

D-2 52.212-5 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT STATUTES OR

EXECUTIVE ORDERS--COMMERCIAL ITEMS…………………………………………………………………………………. 51

D-3 52.215-8 -- Order of Precedence -- Uniform Contract Format (Oct 1997)……………………….. 59

D-4 Contract Period………………………………………………………………………………………………………………. 59

D-5 Economic Price Adjustments……………………………………………………………………………………………. 60

D-6 Property and Personal Damage……………………………………………………………………………………….. 60

D-7 Option to Extend the Term of the Contract (FAR 52.217-9) (MAR 2000)…………………………. 60

D-8 Statement of Equivalent Rates for Federal Hires (FAR 52.222-42) (MAY 1989)……………….. 60

D-9 Federal Excise Tax…………………………………………………………………………………………………………… 61

D-10 Disputes………………………………………………………………………………………………………………………… 61

D-11 Permits and Responsibilities (FAR 52.236-7) (NOV 1991)……………………………………………… 61

D-12 Federal Excise Tax ………………………………………………………………………………………………………….. 61

D-13 52.233-1 Disputes…………………………………………………………………………………………………………. 62

D-14 Permits and Responsibilities (FAR 52.236-7) (NOV 1991)…………………………………………… 62

SECTION E – SOLICITATION PROVISIONS

E-1 FAR 52.252-1 Solicitation Provisions Incorporated by Reference (Feb 1998)…………………. .. 63

E-2 FAR 52.204-6 Data Universal Numbering System Number……………………………………… .. 63

E-3 FAR 52.204-7 -- System for Award Management…………………………………………………. .. 64

E-4 FAR 52.212-1 -- Instructions to Offerors -- Commercial Items (Feb 2012)……………………

E-5 EVALUATION-COMMERCIAL ITEMS (FAR 52.212.2) (JAN 1999) (TAILORED)……………

E-6 FAR 52.212-3 -- Offeror Representations and Certifications -- Commercial Items…………… ... 67

E - 2.1 – ORGANIZATIONAL EXPERIENCE……………………………………………………………

E - 2.2 SAFETY PLAN

E - 2.3 ACCIDENT HISTORY QUESTIONNAIRE………………………………………………………

E – 2.4 ORGANIZATIONAL PAST PERFORMANCE…………………………………………………

Note: Page numbers may have changed during drafts

5 Alaska Region 10 - Fixed Wing Transportation Services BPA

SECTION B – SUPPLIES OR SERVICES AND PRICES

B-1 Schedule of Items

This is a contract for fully operated and maintained light fixed wing aircraft services on a Call-When-Needed (CWN) basis. Aircraft shall meet the requirements of this schedule and the specifications included herein.

Awards will not be made for aircraft not considered suitable for the Government’s need, or at costs determined to be unreasonable. Materially unbalanced offers/quotes may be rejected.

Operators are reminded there is no obligation on the part of the government to use this agreement. The government will seek the best value to satisfy its transportation requirements.

Prices bid in the table below may be adjusted to reflect increases and decreases by submitting a request as stipulated in Section C-24. Per C-24, pricing for additional option years not required.

Note: Aircraft exceeding 6,000 pounds certified takeoff weight shall not include Federal Excise Fuel Tax

AIRCRAFT AND ASSOCIATED RATES BID SHEET

(Contractor to complete)

Make, Model, of Aircraft

Tail Number

Flight Rate Per Hour w/Fuel

Standby Rate

Minimum Charge

Cancellation

Charge

Note: List additional aircraft on separate sheet using same format

6 Alaska Region 10 - Fixed Wing Transportation Services BPA

Offered Aircraft (Contractor to Complete this Chart)

Aircraft

N# Make & Model

Empty Weight

HP Fuel (1) Fuel Type J = Jet A L= Low Lead

Maximum Certified Gross Weight

Equipment & Capacity Code (2)

(1) Fuel consumption expressed in gallons per hour at 65% power, at 5,000 feet MSL, at ISA, as stated in

Aircraft Flight Manual.

(2) Use Key Below

7 Alaska Region 10 - Fixed Wing Transportation Services BPA

Equipment Capacity Codes

A. Single Engine – (# of seats: ____) Indicate on chart # of seats following the code. (i.e., A 2 = single engine with 2 seats)

B. Multi Engine – (# of seats: ____) Indicate on chart # of seats following the code (i.e., B 4 = multi engine with 4 seats)

C. Large Cargo Doors D. High Wing E. Low Wing F. Turbocharged G. Turboprop H. Jet I. Pressurized J. Non-Pressurized K. Oxygen L. Air Tactical Avionics Type 1 M. Air Tactical Avionics Type 2 N. Air Tactical Avionics Type 3 O. Air Tactical Avionics Type 4 P. Relief Pilot(s) Available Q. Infrared R. Automated Flight Following (AFF) S. Aerial Photography

T. TCAS/TCAD

U. Floats: 1. Amphibious 2. Straight V. Other

*Note: In pressurized and non-pressurized aircraft, Pilots shall meet 14 CFR Part 135 Oxygen Requirements.

8 Alaska Region 10 - Fixed Wing Transportation Services BPA

DESCRIPTION OF AGREEMENT

(a) The Contractor shall furnish supplies or services, if and when requested by the Contracting Officer or his authorized representative during the period specified in the clause below entitled "Effective Period". Purchases (which may be referred to as calls) made hereunder may be written or oral. (b) Supplies or services will be identified on individual purchases issued in accordance with paragraph (a) above. Supplies and services purchased under this agreement shall be limited to

EXTENT OF OBLIGATION

The Government is obligated only to the extent of authorized Calls actually placed against this Blanket Purchase Agreement.

PURCHASE LIMITATION

No individual Call under this agreement shall exceed the simplified acquisition threshold. For the acquisition of commercial items no individual Call shall exceed $5,000,000.

EFFECTIVE PERIOD

This Blanket Purchase Agreement is effective for a base year beginning the date of award for 12 months and 4 optional year periods.

B-2 Government Furnished Pilot (see Exhibit 2)

Please Check

Contractor will will not authorize performance of work under the contract by a Government Pilot.

Notice Government requirements in Exhibit 2.

B-3 Home Base (Base from which aircraft would normally be available)

Offeror shall enter the location of their home base. The same aircraft number will not be awarded/administered under more than one Forest Service CWN contract.

Location (Physical Address) State

Note: Offers for furnishing services on a “Call-When-Needed” Basis are being solicited from operator’s located in Southeast or South Central Alaska

B-4 Fuel Price Basis

The following stated fuel prices are the basis for economic price adjustment of the fuel portion of the flight rate, as stated in the Economic Price Adjustment clause (D-4) of this contract:

(1) $ 0.00/gallon for 100 LL Avgas

(2) $ 0.00/gallon for Jet A.

Prices for fuel are obtained from the following web site: http://www.airnav.com/fuel/. The above average fuel prices were calculated on (date). See Economic Price Adjustment clause Section D.4

Note: Only aviation grade fuels are acceptable for aircraft under this contract.

B-5 Maintenance Capability

Offeror shall provide the name and address of the Director of Maintenance and the repair facility intended to be used during the performance of this contract:

9 Alaska Region 10 - Fixed Wing Transportation Services BPA http://www.airnav.com/fuel/

Director of Maintenance (Name) Business Address

Cell Phone No.

Phone No.

Fax No.

Repair Facility Business Address

Phone No.

Fax No.

The Government may inspect the offeror’s operation and maintenance facilities prior to award

10 Alaska Region 10 - Fixed Wing Transportation Services BPA

B-6 Vendor Offered Avionic Requirements in addition to those required in C.7 - Avionic Requirements

Vendors Additional Offered Avionics: The Vendor offers the following additional items by aircraft. If an item is checked and already is a required item, then the checked item is in additional offered avionics capability in addition to those requirements required in C.7.

If Additional Check the

Box

Requirements aircraft has in addition to those required in C.7 - Avionic Requirements.

List Aircraft By N Number With Added Avionics

An aeronautical VHF-AM radio transceiver

A panel mounted GPS in lieu of a handheld GPS

A moving map capable navigation system

A GPS Data Connector

A panel mounted VOR receiver system

Provisions for IFR operation

An aeronautical VHF-FM radio transceiver

A UHF Aeronautical Transceiver

A Low Band Aeronautical Transceiver

A Project 25 compliant digital aeronautical VHF-FM radio transceiver

Provisions for an Auxiliary VHF-FM Portable Radio

A VHF-FM Aeronautical Antenna

A UHF Aeronautical Antenna

A Low Band Aeronautical Antenna

An Accessory Power Source

A Transponder, Altitude Encoder and Static Systems (Reconnaissance)

A DME system

TCAS or TCAD

An Audio Control System

A separate audio control system for the ATGS instructor

An Intercommunications System for the pilot and co-pilot/observer

An Intercommunications System for the pilot, co-pilot/observer and all passengers

B-7 Additional Information to be submitted by the Offeror (See Section E)

11 Alaska Region 10 - Fixed Wing Transportation Services BPA

SECTION C – DESCRIPTION/SPECIFICATIONS/WORK STATEMENT

C-1 Scope of Contract

A. The intent of this solicitation and any resultant Contract is to obtain services on a Call When Needed (CWN) basis of light fixed wing aircraft fully operated by qualified personnel and equipped to meet specifications for use in administration and protection of Public Lands within Alaska Region 10, Chugach and Tongass National Forests of the Forest Service.

B. The aircraft furnished may be used for fire support, 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 contract for such use.

C-2 General Certifications

A. Contractors 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 Operators 135 Certificate.

B. Aircraft shall conform to its approved type design, be maintained and operated in accordance with the requirements of 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-3 Government Furnished Property

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 GFP (Short Form) FAR Clause 52.245-4 (APR 1984).

C-4 Aircraft Requirements

A. Aircraft Performance Requirements

1. Single engine aircraft shall have a power loading of not more than 13.5 pounds per horse power.

2. Multi engine aircraft shall be capable of at least 200 horse power; per engine; any engine developing less than 240 horse power shall be turbo/super charged. As dictated by Forest Service policy the Regional Aviation Officer, by letter, may waive the horsepower requirements for aircraft with demonstrated suitable single engine performance for assignments within Region 10. All multiengine aircraft shall comply with FAR 135.181 and/or 183, whichever is higher.

3. Each takeoff shall meet aircraft climb performance requirements of 14 CFR.

B. 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. Most single engine fixed wing aircraft used in Alaska shall be equipped with floats. Exceptions:

Cordova, Yakutat, Kenai Peninsula, Interior Alaska and special projects approved by the Regional Aviation Officer.

2. All aircraft furnished under this contract 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.

3. 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.

12 Alaska Region 10 - Fixed Wing Transportation Services BPA

4. 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.) Military or other low visibility paint schemes are unacceptable. Any corrosion shall be within manufacturer or FAA acceptable limits.

5. 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.

6. 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.

7. While operating under this agreement each aircraft shall carry current copies of the following:

a. Contract and all modifications.

b. DOT Exemption 9198 and the Interagency Aviation Transport of Hazardous Materials

Handbook/Guide (NFES 1068) (if required)

c. Aeronautical charts covering area of operation.

8. Flight Hour Meter. Each aircraft shall be equipped with a flight hour meter, which measures actual flight time from takeoff to landing in hours and tenths.

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

10. Safety Belts. The aircraft furnished under this contract 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 wear the seat belts 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:

a. 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.

b. 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.

c. Stitches. Broken or missing stitches, severe fading or discoloring, inconsistent stitch pattern.

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

e. Age. Belts/fabric over 10 years from date of manufacture requires close inspection because of the elements they are exposed to. Older belts do not have to be replaced if it can be determined they are in serviceable condition and not life limited.

SURVIVAL KIT AERONAUTICAL All aircraft will carry survival equipment. Survival kits will contain at least the following items and additional items required by local regulation as is appropriate for local climate and terrain conditions.

13 Alaska Region 10 - Fixed Wing Transportation Services BPA

The minimum equipment to be carried during the summer months:

Item Item Ax or hatchet (1), and Knife (1) Water Purification Tablets Magnesium Fire Starter Mosquito repellant containing DEET Whistle Mosquito headnet for each occupant (1) Signal Mirror Candles (5 each) Non-Marine Aerial Flares (6-each) Space Blanket (1 per occupant) Matches (2-small boxes in waterproof containers)

Nylon Rope or Parachute Cord (50-feet)

Food (Each occupant sufficient to sustain life for 1-week @ minimum of 1,000 calories per day)

An assortment of fishing tackle such as hooks, flies, lines, sinkers, etc.

Personal Locator Beacon (PLB) (Note: required only if Aircraft ELT requires tools to be removed)

In addition to the above, the following shall be carried as minimum equipment from October15 to April 1 of each year:

Pair of Snowshoes (1) Sleeping bag per two occupants (1) Wool blanket or equivalent for each occupant over 4-years of age (1)

A personal survival kit may be required of the pilot and occupants on certain flights. The following table lists the recommended survival items carried in a personal survival vest, clothing, or flight suit pockets:

Fire Starter - (matches in waterproof container, “metal matches”, etc.)

Laser rescue light or key chain LED light

Signal mirror Whistle Knife or tool containing a knife blade Water purification tablets Sealable clear plastic bag(s) Personal locator beacon (PLB) 360/720/760-channel VHF-AM radio transceiver or satellite telephone

Note: A hand-held 760 channel VHF transceiver radio is recommended. It should be attached, or immediately accessible, to a crewmember rather than placed in the aircraft survival kit.

C-5 Aircraft Maintenance

A. All aircraft shall be maintained to 14 CFR Part 43, 91, and 135 standards. The Contractor shall provide or arrange for sufficient maintenance capability to keep the aircraft in airworthy condition.

B. The Contractor shall identify the maintenance facilities and/or maintenance personnel used to fulfill the requirements of this contract.

C. 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.

D. Compliance with applicable mandatory manufacturer's bulletins, alert service bulletins, safety of flight bulletins, FAA Airworthiness Directives (AD), and the correction of maintenance deficiencies shall be accomplished prior to delivery and continue during contract performance.

14 Alaska Region 10 - Fixed Wing Transportation Services BPA

E. 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.

F. A copy of the current maintenance record required by 14 CFR 91.417 shall be kept at the Home Base or maintenance facility.

G. A test 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 3-hours of operation, including 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 contract. 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 contract availability.

H. When any non-scheduled maintenance or repairs are performed due to mechanical or equipment deficiencies, an AMI and the Contracting Officer (CO) shall be notified for "return to contract available” status, before the aircraft performs under the contract.

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

J. 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. Single engine aircraft shall be weighed within the previous 5 years, with an updated Equipment List of installed equipment.

K. All weighing of aircraft shall be performed on scales that have been certified. The certifying agency may be any accredited weights and measures laboratory.

C-6 Aircraft and Equipment Security

A. The security of Contractor provided aircraft and equipment is the responsibility of the Contractor.

B. Aircraft shall be electrically and/or mechanically disabled by two independent security systems whenever the aircraft is unattended. Deactivating security systems shall be incorporated into preflight checklists to prevent accidental damage to the aircraft or interfere with safety of flight.

C. Examples of Unacceptable disabling systems are:

1. Locked door/windows; and/or

2. Fenced parking areas.

C-7 AVIONICS REQUIREMENTS

Except for the ICOM, required avionics specifications as specified in FS/AMD A-24 at:

www.nifc.gov/NIICD/documents.html

C-8 CONTRACTOR FURNISHED AVIONICS SYSTEMS

1. MINIMUM REQUIREMENTS

All avionics used to meet this agreement shall comply with the requirements of paragraph 2 (AVIONICS SPECIFICATIONS) and paragraph 3 (AVIONICS INSTALLATION AND MAINTENANCE STANDARDS).

The following are the minimum avionics which shall be installed. Additional avionics may be required in section B of this agreement.

A. Point to Point Aircraft

Point to Point flights shall meet the requirements of 14 CFR 135. No additional avionics are required.

B. Back Country Aircraft

15 Alaska Region 10 - Fixed Wing Transportation Services BPA http://www.nifc.gov/NIICD/documents.html

Aircraft operating to or from airfields or airstrips designated as Category 4 and are not otherwise conducting special use missions shall meet the requirements of paragraph 1.C excluding 1.C.2).

C. Resource Reconnaissance Aircraft (All aircraft which are not used for fire operations or covered by paragraphs 1.A or 1.B)

1) One VHF-AM Radio (COM)

2) One Global Positioning System (GPS)

3) An Emergency Locator Transmitter (ELT)

4) An Automated Flight Following system (AFF) {Not required for aircraft only used for Law

Enforcement}

5) Equipment and lighting for night VFR operations in accordance with 14 CFR 135.159 and 14

CFR 135.161.

6) One of the following options for FM communications

(a) Option 1

1. RESERVED

(b) Option 2

1. An Intercom System (ICS)

2. An Audio Control system

3. One Amateur FM Radio (See paragraph 2.A.5)

(c) Option 3

1. RESERVED

(d) Option 4

1. An Intercom System (ICS)

2. An Audio Control system

3. One VHF-FM Radio (FM)

D. RESERVED

E. RESERVED

Note 1: RESERVED Note 2: RESERVED Note 3: RESERVED

2. AVIONICS SPECIFICATIONS

All avionics used to meet this agreement shall comply with the following requirements and paragraph 3

(AVIONICS INSTALLATION AND MAINTENANCE STANDARDS).

A. Communications systems

1) VHF-AM Radios

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.

2) VHF-FM Radios

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:

(a) 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

16 Alaska Region 10 - Fixed Wing Transportation Services BPA digital operation shall be selectable by channel for both MAIN and GUARD operation.

Carrier output power shall be 6-10 Watts nominal.

(b) Transceivers 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.

(c) 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.

(d) 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.

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

3) Auxiliary FM systems (AUX FM)

An interface to properly operate a portable FM radio through the aircraft audio control systems shall be provided using an MS3112E12-10S type bulkhead mounted connector with contact assignments as specified by FS/AMD A-17 available at the following website:

http://www.nifc.gov/NIICD/documents.html . Sidetone for the portable radio shall be provided (AEM AA34 or equivalent).

The following applies to all AUX FM installations:

(a) An external broadband antenna covering the frequency band of 138 to 174 MHz (Comant CI-177-1 or equivalent) shall be installed with the associated coax terminated in a bulkhead mounted BNC connector adjacent to the above 10 pin connector.

(b) A portable radio mount (Field Support Services AUX-EPH-RB or equivalent) shall be installed providing the crew unrestricted operation of the radio controls when connected with an 18 inch adapter cable.

(c) A VHF-FM radio meeting the requirements of paragraph 2.A.2) may be installed, in addition to the radios already required, in lieu of the AUX FM system.

4) Non-Standard Radios

Non-standard radios shall be aeronautical transceivers interfaced to the aircraft audio control systems and a compatible antenna via an approved installation. The radio shall be compatible with the requesting unit.

5) Amateur FM Radios

Amateur FM Radios are acceptable for use in the State of Alaska when approved on FAA Form 337 and meeting the following requirements:

(a) Permanently installed in a location that is convenient to the PIC and SIC/observer, and capable of transmitting and receiving in the 138-174 MHz frequency range. All usable frequencies shall be programmable in flight. Narrowband operation shall be selectable by channel. Carrier output power shall not exceed 10 Watts.

(b) 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.

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

(d) Interfaced through the aircraft audio control system for both transmit and receive operation.

The ICOM IC-2200H, IC-2300H and IC-V8000 radios with the MARS modification are known to meet these requirements:

17 Alaska Region 10 - Fixed Wing Transportation Services BPA

B. Audio Systems

1) Intercom systems (ICS)

ICS shall integrate with the aircraft audio control systems and mix with selected receiver audio.

An ICS volume control and a “hot mic” capability shall be provided for the PIC and SIC/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.

2) Audio Control systems

(a) General 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 (and PA if required).

Sidetone 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 SIC/observer’s audio control system unless an aft audio control system is installed. Drop cords may be used provided MS3112E10-6S type 6-pin connectors are installed adjacent to the required passenger headset jacks and wired for compatibility with an appropriate drop cord (Alpine Aerotech AAL280 series or equivalent).

Audio controls shall be labeled as COM-1, FM-1, AUX, PA etc… as appropriate or as COM-1, COM-2, COM-3, etc… with the corresponding transceiver labeled to match.

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.

The Vendor shall supply both the PIC and SIC/observer with aviation headsets (including microphones) which are compatible with the aircraft audio/ICS system.

The PIC shall have a radio Push-To-Talk (PTT) switch on their flight controls.

(b) Drop Cord Requirements

1. Coil cord with sufficient length to provide unrestricted movement according to mission requirements (Minimum 3 feet retracted)

2. 6-Pin MS3476L10-6P type connector on the coil cord

3. JJ-033 and JJ-034 type headset jacks at the housing

4. Large clip

5. Volume control

6. ICS switch with momentary and lock positions

7. Radio PTT switch (only for positions which require radio transmit)

(c) Aft Audio Control systems The audio controller shall be installed in a location that provides the operator directly behind the SIC/observer 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.

(d) Required Audio Control systems The following audio control systems are required based on mission type

1. RESERVED

2. RESERVED

3. Reconnaissance airplanes

A single audio control system for the PIC and SIC/observer

C. Navigation systems

1) Global Positioning Systems (GPS)

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(a) Aeronautical GPS Each required GPS shall be TSO approved, permanently installed where both the PIC and SIC/observer can clearly view the display, use an approved external aircraft antenna, and be powered by the aircraft electrical system. The GPS shall utilize the WGS-84 datum, reference coordinates in the DM (degrees/minutes/decimal minutes) format and have the ability to manually enter waypoints in flight. The GPS navigation database shall cover the State of Alaska and be updated within the preceding 36 months.

(b) Portable Aviation GPS Portable aviation GPS units (Garmin GPSMAP, aera, or equivalent) are acceptable when an Aeronautical GPS is not specified. They shall be securely mounted via an approved installation using the aircraft electrical system and a remote antenna. The GPS shall present information from an overhead perspective. The PIC shall have clear view of the display and unrestricted access to the controls. The SIC/observer shall also have a clear view of the display in Air Tactical aircraft. The GPS shall meet the above datum, coordinate, and database requirements for an aeronautical GPS. Portable GPS units are not acceptable for aircraft performing IFR or NVG operations.

(c) 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 3 inches wide, 1.5 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.

D. Surveillance systems

1) Emergency Locator Transmitters (ELT)

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. TSO C126 and newer ELTs require documentation of current registration from the national authority for which the aircraft is registered.

2) Automated Flight Following systems (AFF)

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 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/ .

(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.

(f) For questions about current compatibility requirements contact the AFF Program Manager listed under contacts at https://www.aff.gov

19 Alaska Region 10 - Fixed Wing Transportation Services BPA https://www.aff.gov/ https://www.aff.gov/contractspecs.asp https://www.aff.gov/

3) Transponders

Transponder 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.

4) 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.

5) Traffic Advisory Systems (TAS)

Traffic advisory systems shall be TSO approved, use active interrogation, graphically display traffic relative to the aircraft’s horizontal position, and provide alert audio to the PICs audio control system. The display shall be within view of the PIC and SIC/observer. The system shall provide coverage in all directions above and below the aircraft with a maximum range of at least 10 nautical miles. The display shall allow range selection of 2 miles or less.

E. General Systems

1) Autopilots

Autopilots shall be capable of operating the aircraft controls to maintain flight and maneuver it about the three axes.

2) RADAR Altimeters

RADAR altimeters shall be approved, operate from zero to a minimum of 2000 feet AGL and provide the operator an adjustable cursor which enables an altitude low (decision height) annunciation. The altitude low annunciation shall be clearly identified, and in the PIC’s primary field of view.

3) Multi-Function Displays (MFD)

MFDs shall be installed within view of the PIC and display GPS navigation information on a color moving map. TAS and weather data link information shall be displayed on the MFD when these systems are required.

4) Cockpit Voice Recorder (CVR)

Cockpit voice recorders shall meet all applicable regulations for standard and transport category aircraft.

5) Auxiliary Power Source (3 Pin)

An MS3112E12-3S type connector shall be installed and mounted in a location convenient to the SIC/observer and protected by a 10 Amp circuit breaker. Pin A shall be +28 VDC in 28 Volt aircraft. Pin B shall be airframe ground. Pin C shall be +14 VDC in 14 Volt aircraft. Pins A and C shall never be simultaneously wired to the connector. Refer to FS/OAS A-16.

6) Supplemental Antennas

Supplemental antennas shall be aeronautical broadband antennas and operate in the correct frequency band for the specified use. An approved coax, with sufficient length to connect to a unit installed between the PIC and SIC/observer plus 4 feet (minimum), shall be installed and terminated with a male BNC. The following antennas or equivalents shall be used.

(a) Low Band (32-50 MHz): Dayton-Granger 720061

(b) VHF-FM (138-174 MHz): Comant CI-177-1

(c) UHF 400-500 (406-512 MHz): Comant CI-275

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(d) UHF 700-800 (721-898 MHz): Comant CI-285

7) Supplemental Radio Kit Provisions

Space and mounting provisions between the PIC and SIC/observer shall be provided for the installation of a radio kit. The location shall allow for connection to the aircraft systems without interfering with flight controls or occupants. JJ-033 and JJ-034 audio jacks shall be installed next to the PIC and SIC/observer and interfaced to the PICs audio control system with PTT capability. The jack pair shall not be separated by more than 4 inches. An auxiliary power source shall be installed (paragraph 2.E.5)). A supplemental VHF-FM antenna shall be installed (paragraph 2.E.6).

8) Supplemental Air Attack Kit Provisions

Provisions for a supplemental radio kit (paragraph 2.E.7)) shall be provided, and a second supplemental VHF-FM antenna shall be installed.

9) Supplemental Radio Kits

Supplemental radio kits provided with the aircraft shall be securely installed between the PIC and SIC/observer, meet FAA flammability requirements, and be interfaced to the aircraft via the provisions of paragraph 2.E.7). The radio kit shall provide the capability for the aircraft to meet the equipment requirements of a Resource Reconnaissance Aircraft. See paragraph 1.C

10) Supplemental Air Attack Kits

Supplemental air attack kits provided with the aircraft shall be securely installed between the PIC and SIC/observer, meets FAA flammability requirements, and be interfaced to the aircraft via the provisions of paragraph 2.E.8). The air attack kit shall provide the capability for the aircraft to meet the equipment requirements of a Type II Air Tactical Aircraft. See paragraph 1.E.2).

11) VHF-FM Programming Ports

DB-9 type D-subminiature connectors shall be installed in a location convenient to the SIC/observer. These shall be wired for RS232 serial communication between all required VHF- FM radios and a laptop computer. Individual connectors or an FM select switch may be used.

Pin 2 shall be data transmitted from the FM. Pin 3 shall be data received by the FM. Pin 5 shall be signal ground. Compatible radio front panel connectors may be used to meet this requirement if serial adapter cables are provided with the aircraft. For example TDFM 136A radios s/n FDA1200 and higher.

12) GPS Data Connectors

DB-9 type D-subminiature connectors shall be installed in a location convenient to the SIC/observer. These shall be wired to receive RS232 serial data from the GPS to a laptop computer. Pin 2 shall be data transmitted from the GPS. Pin 5 shall be signal ground.

13) External Portable Aviation GPS Antennas

Antennas shall be TSO approved and compatible with the portable aviation GPS of the requesting unit.

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C-9 AVIONICS INSTALLATION AND MAINTENANCE STANDARDS

All avionics used to meet this agreement shall comply with the manufacturer’s specifications and installation instructions, federal regulations, and the following requirements.

A. Strict adherence to the guidelines in FAA AC 43.13-1B Chapter 11 “Aircraft Electrical Systems” and

Chapter 12 “Aircraft Avionics Systems” as well as FAA AC 43.13-2B Chapter 1 “Structural Data”, Chapter 2 “Communication, Navigation and Emergency Locator Transmitter System Installations” and Chapter 3 “Antenna Installation” is required.

B. All antennas shall be FAA approved, have a Voltage Standing Wave Ratio (VSWR) less than 3.0 to 1 and be properly matched and polarized to their associated avionics system.

C. Labeling and marking of all avionics controls and equipment shall be understandable, legible, and permanent. Electronic label marking is acceptable.

D. Avionics installations shall not interfere with passenger safety, space or comfort. Avionics equipment shall not be mounted under seats designed for energy attenuation. In all instances, the designated areas for collapse shall be protected.

E. All avionics equipment shall be included on the aircraft’s equipment list by model, nomenclature, and location.

F. Avionics systems shall meet the performance specifications of FS/OAS A-24 Avionics Operational Test Standards. For a copy of all FS/OAS documents visit http://www.nifc.gov/NIICD/documents.html .

C-10 Operations

A. General

1. Regardless of any status as a public aircraft operation, the Contractor shall operate in accordance with their approved FAA Operations Specifications and all portions of 14 CFR 39, 43, 61, 91, 135 (including those portions applicable to civil aircraft) and each certification required under this Contract unless otherwise authorized by the CO.

2. A Government Representative, Aviation Manager or Flight Manager may inspect the Pilot’s

Interagency Airplane Pilot Qualification Card for currency before any flight. The Flight Manager has mission control and can delay, terminate, or cancel a flight at any time.

B. Pilot Authority and Responsibilities

1. The Pilot-In-Command (PIC) is responsible for the safety of the aircraft, loading and unloading of occupants and cargo. The Pilot shall comply with the directions of the Government, except when in the Pilot's judgment compliance will be a violation of applicable federal or state regulations or contract provisions. The Pilot has final authority to determine whether the flight can be accomplished safely and shall refuse any flight or landing which is considered hazardous or unsafe.

2. The Pilot is responsible for computing the weight and balance for all flights and for assuring that the gross weight and center of gravity do not exceed the aircraft's limitations.

3. A takeoff performance calculation shall be accomplished. Under no circumstances will a takeoff be attempted if existing environment conditions at takeoff cannot be accurately addressed in the Aircraft Flight Manual (AFM) or Pilots Operating Handbook (POH).

4. No equipment such as radios, survival gear, fire tools, etc., shall be located in or on the aircraft in such a manner as to potentially cause damage, injury, or obstruct the operation of equipment or personnel (14 CFR 135.87).

5. Pilots will comply with company established 14 CFR 135 cockpit checklist for all flight operations.

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6. Single Engine Aircraft shall not operate in known instrument meteorological conditions (IMC).

7. Cell Phone Use. Cell phone use is prohibited within 50 feet of the aircraft during fueling operations.

8. Smoking is prohibited within 50-feet of fuel servicing vehicle, fueling equipment, or aircraft.

9. Aircraft Engine(s):

a. Prior to passenger or cargo loading/unloading, all engines shall be shut down, and all propellers shall have ceased rotation.

b. Aircrafts shall not be refueled while engines are running, propellers turning, or with passengers on board.

c. The Pilot shall not leave the cockpit of an aircraft unattended while the engine(s) are running.

10. Night Flying/Operations.