AG-024B-S-17-9112_Amend_0002.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

1. CONTRACT ID CODE PAGE OF PAGES

1 4

2. AMENDMENT/MODIFICATION NO. /3. EFFECTIVE DATE 4. REQUISITION/PURCHASE REQ. NO. 5. PROJECT NO. (If applicable)

Amendment 0002 March 27, 2017

6. ISSUED BY CODE 7. ADMINISTERED BY (If other than Item 6) CODE

USDA Forest Service – Contracting National Interagency Fire Center 3833 S. Development Ave., Suite 1100 Boise, ID 83705

Same as #6

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

AG-024B-S-17-9112

9B. DATED (SEE ITEM 11)

3/27/2017

10A. MODIFICATION OF CONTRACT/ORDER NO.

10B. DATED (SEE ITEM 13)

CODE FACILITY CODE

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

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

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

(a) By completing Items 8 and 15, and returning 1 copies of the amendment; (b) By acknowledging receipt of this amendment on each copy of the offer submitted;

or (c) By separate letter or telegram which includes a reference to the solicitation and amendment numbers. FAILURE OF YOUR ACKNOWLEDGMENT TO BE RECEIVED AT THE PLACE DESIGNATED FOR THE RECEIPT OF OFFERS PRIOR TO THE HOUR AND DATE SPECIFIED MAY RESULT IN REJECTION OF YOUR OFFER. If by virtue of this amendment you desire to change an offer already submitted, such change may be made by telegram or letter, provided each telegram or letter makes reference to the solicitation and this amendment, and is received prior to the opening hour and date specified.

12. ACCOUNTING AND APPROPRIATION DATA (If required)

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

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

(X) A. THIS CHANGE ORDER IS ISSUED PURSUANT TO: (Specify authority) THE CHANGES SET FORTH IN ITEM 14 ARE MADE IN

THE CONTRACT ORDER NO. IN ITEM 10A.

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

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

D. OTHER (Specify type of modification and authority)

E. IMPORTANT: Contractor is not, is required to sign this document and return 1 copies to the issuing office.

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

The purpose of this amendment is as follows:

1.Revise Section B-3, Capability from 2 hours fuel to 1.5 hours fuel as shown in pages below

2.Section C, Exhibit 22-Computed Gross Weight Table (B-3 (a), Exhibit 13)) has been replaced in it’s entirerty with the Exhibit 22 attached in page two of this amendment.

All other terms and conditions remain unchanged.

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

15A. NAME AND TITLE OF SIGNER (Type or print) 16A. NAME AND TITLE OF CONTRACTING OFFICER (Type or print)

DAVID P HERSHEY

15B. CONTRACTOR/OFFEROR 15C. DATE SIGNED 16B. UNITED STATES OF AMERICA 16C. DATE SIGNED

(Signature of person authorized to sign) (Signature of Contracting Officer)

NSN 7540-01-152-8070

Previous edition unusable

30-105 STANDARD FORM 30 (REV. 10-83)

Prescribed by GSA

FAR (48 CFR) 53.243

B-3 AIRCRAFT PERFORMANCE SPECIFICATIONS (MINIMUM) TO BE USED FOR PROPOSAL

EVALUATION PURPOSES AND AIRCRAFT WEIGHING AND WEIGHT VALIDATION

(a) Performance shall be based on minimum engine specification. Aircraft performance capabilities shall be determined by using the Standard Interagency Helicopter Load Calculation Method. (Exhibit 13, Interagency Helicopter Load Calculation)

Performance enhancing data (Power Assurance Checks, wind charts, etc) shall not be used. Only FAA approved charts based on minimum specification engine performance shall be used. As an example, Kaman K-1200 helicopters shall only use minimum specification engine performance data calculated from Rotorcraft FMS NO. 1, (USFS Fire Fighting).

Use (Exhibit 13, Interagency Helicopter Load Calculation and Exhibit 12, Hourly Flight Rates, Fuel consumption, and Weight Reduction Chart) per aircraft type and the appropriate Hover Ceiling Charts (HOGE and HIGE) from the approved Rotorcraft Flight Manual with current supplements and changes as applicable.

For field operations use current temperature and elevation for performance planning purposes.

(b) Aircraft Weighing and Weight Validation

(1) The aircraft’s equipped weight is determined using weight and balance data, which was determined by actual weighing of the aircraft in accordance with the manufacturer’s requirements and configured in accordance with the contract specifications, as proposed.

Additional weighing criteria:

(i) The weighing shall be accomplished by the Contractor or their agent.

(ii) 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 (See Form B, Exhibit 21).

(iii) Weighing shall be:

(A) Accomplished within 12 months prior to the due date of proposal submission, and

(1) Reserved

(B) At an interval of 24 months thereafter and / or

(C) Following any major repair or major alteration or change to the equipment list, which significantly affects the center of gravity of the aircraft.

(iv) Helicopter(s) under this solicitation shall:

(A) Remain at or below the contracted helicopter equipped weight as proposed in the base year of the contract. When there is a difference in the aircraft's weight between different sets of scales, scales shall be allowed a maintenance tolerance of .2 % (two tenths of a percent) of the scale reading for each set of scales. For example, a helicopter that weighed 6000 lbs on one scale set would be allowed a 12 lb tolerance on each scale set when compared. (Ref. NIST Handbook 44, Table 6).

(B) Be allowed a total of 1% above the contracted helicopter equipped weight as proposed during the combined contract option periods.

(v) Cowlings, doors and fairings shall not be removed to meet contract equipped weight for performance.

(vi) If the government requires additional equipment after contract award, no penalty will be assessed.

(2) After proposal evaluations and prior to or post award all Exclusive Use aircraft weighing shall be witnessed and validated by Agency Aircraft Inspector(s). If aircraft must be weighed post award it will be at the option of the Government. The objective of the second and separate weighing is to validate the contractor’s proposed weight as configured to comply with the solicitation requirements. Contractors are responsible for the costs associated with weighing the aircraft excluding Agency Aircraft Inspector costs.

All aircraft shall be weighed prior to start of the base year Mandatory Availability Period (MAP).

Applicable for Type III (Light) Helicopters Example:

CAPABILITY OF:

At 7,000 feet pressure altitude and 30°C with non-jettisonable jettisonable

Payload of 900 pounds, as determined by Exhibit 13, Standard Interagency Load Calculation form, using a standard pilot weight of 200 pounds and fuel for 1.5 hours as determined by Exhibit 12, Hourly Flight Rates, Fuel Consumption, and Weight Reduction Chart.

EXHIBIT 22 - COMPUTED GROSS WEIGHT TABLE (B-3 (a), Exhibit 13))

Aircraft Type

Bell 407 (Suppl 12) Bell 407 HP Airbus H125 (Astar B3e) (Suppl 28)

Max Gross Weight 4915 5000 4960 Pilot Weight 200 200 200

1.5 hours fuel 473 473 525 Weight Reduction 155 155 175 Payload 900 900 900 Aircraft max equipped weight 3187 3272 3160

Does not apply to aircraft that are not listed.