Amendment_0003.pdf

AMENDMENT OF SOLICITATION/MODIFICATION OF CONTRACT

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)

30-105-04EXCEPTION TO SF 30

APPROVED BY OIRM 11-84

STANDARD FORM 30 (Rev. 10-83) Prescribed by GSA

FAR (48 CFR) 53.243

The purpose of this amendment is to revise Attachment 5, HOGE Chart by changing the fuel reserve from 1 hour 30 minutes to 30 minutes.

1. CONTRACT ID CODE PAGE OF PAGES

J 1 7

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

16C. DATE SIGNED

BY 05-Dec-2014

16B. UNITED STATES OF AMERICA15C. DATE SIGNED15B. CONTRACTOR/OFFEROR

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

8. NAME AND ADDRESS OF CONTRACTOR (No., Street, County, State and Zip Code) X HTC711-15-R-R007

X 9B. DATED (SEE ITEM 11)

24-Nov-2014

10B. DATED (SEE ITEM 13)

9A. AMENDMENT OF SOLICITATION NO.

11. THIS ITEM ONLY APPLIES TO AMENDMENTS OF SOLICITATIONS

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

Offer 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.

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 copies to the issuing office.

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

10A. MOD. OF CONTRACT/ORDER NO.

2. AMENDMENT/MODIFICATION NO. 5. PROJECT NO.(If applicable)

6. ISSUED BY

3. EFFECTIVE DATE

05-Dec-2014

CODE

USTRANSCOM-AQ - HTC711

508 SCOTT DR

SCOTT AFB IL 62225-5357

HTC711 7. ADMINISTERED BY (If other than item 6)

4. REQUISITION/PURCHASE REQ. NO.

CODE

See Item 6

FACILITY CODECODE

EMAIL:TEL:

HTC711-15-R-R007

SECTION SF 30 BLOCK 14 CONTINUATION PAGE

SUMMARY OF CHANGES

SECTION SF 1449 - CONTINUATION SHEET

The following have been modified:

ATCH 5 - HOGE CHART

ATTACHMENT 5 – HOGE Chart

Applicable for Helicopters:

• Hovering out of ground effect (HOGE)

At 6,500 feet pressure altitude and 30 oC with a non-jettisonable Payload of 500 pounds, as determined by Standard Interagency Load Calculation form using a standard crew weight of 250 lbs per person and the total fuel weight required to travel 200nm at the aircraft’s cruise speed plus 30 minutes of fuel reserve and if established for aircraft type proposed, the Weight Reduction Chart.

Destinations are as follows:

Destination Origin 200 nm

HELICOPTER SERVICES FUEL CONSUMPTION, AND WEIGHT REDUCTION CHART

COMPANY AIRCRAFT TYPE

FUEL

CONSUMPTION

(gal/hr)

LOAD CALCULATION

Weight Reduction (lbs)

AGUSTA

WESTLAND AW 119 Koala 55 230 AW 139 129 Not Established EH 101 211 Not Established

AEROSPATIALE SA 315B 58 180

SA 316B 58 170

SA 318C 45 80

SA 319B 45 150

AS 330J 179 N/A

SA 332L1 160 N/A

SA 341G 45 170

AS 350B/350BA 45 130

AS 350B1 46 160

AS 350B2 48 160

AS 350B3 50 175

AS 350D 38 130

AS-355F-1/355F-2 58 140

AS 365N1 87 275

EC 120 31 Not Established EC 130B4 53 Not Established

EC 135 64 220

EC 145 80 Not Established EC 155B1 95 Not Established EC 225 183 Not Established

BELL: 47/SOLOY 23 120

204B (UH-1 Series) 86 200 204 Super B 90 200 205A-1 88 260 205A-1++ 90 260

206B-II 25 100

206B-III 27 130

206L-1 32 150 206L-3 38 180 206L-4 38 180 210 90 260 212 100 390 214B 160 380 214B1 145 380

214ST 133 420

222A 70 Not Established 222B 83 Not Established 222UT 83 Not Established 407 45 155 412 110 390

412HP 110 390

UH-1B 86 N/A

UH-1B Super 88 NA

UH-1F 88 N/A

UH-1H (13 engine) 88 N/A UH-1H (17 engine) 90 N/A

TH-1L 88 N/A

BOEING: BV-107 180 N/A

BV-234 405 N/A

HILLER: *SL-3/4 21 90

H-1100B 22 130 UH-12/Soly 23 100

KAMEN: H43-F 85 N/A

K-1200 85 N/A

MBB: BO105CBS 55 180

BK-117 77 160

McDONNELL- 500C 23 110

DOUGLAS: 500D/E 28 120

520N 32 100 530F 34 120 600N 41 155 900/902 69 210

SIKORSKY CH 53D 425 N/A

CH 54/S 64 525 N/A

: S-55T 47 170 S-58D/E 83 N/A

S-58T/PT6T-3 115 400

S-58T/PT6T-6 115 460

S-61N 170 N/A S-62A 70 300 S-70 160 N/A S-76C+ 90 Not Established S-92 178 Not Established

INTERAGENCY HELICOPTER LOAD CALCULATION

Instructions for completing the solicitation’s interagency Helicopter load chart:

1. HELICOPTER EQUIPPED WEIGHT – Equipped Weight equals the Empty Weight (as listed in the Weight and Balance Data) plus the weight of lubricants and onboard equipment required by contract (i.e. survival kit, rappel bracket, defensive armor).

2. FLIGHT CREW WEIGHT – Weight of the Pilot and any other assigned flight crewmembers on board (i.e.

Co-pilot, flight engineer, navigator). Number of crew multiplied by 250 pounds.

3. FUEL WEIGHT – Total number of gallons onboard multiplied by the weight per gallon (Jet Fuel = 7.0 lbs/gal; AvGas = 6.0 lbs/gal). The number of gallons required is calculated in the following manner:

Number of gallons of fuel is the amount the aircraft requires to travel 200nm at the aircraft’s cruise speed.

The number of gallons is then increased by the fuel weight of the 30 minute reserve to obtain the total gallons of fuel onboard.

For example, if the proposed aircraft’s cruise speed is 100 nautical miles per hour and the fuel consumption rate as determined from the HELICOPTER SERVICES FUEL CONSUMPTION, AND WEIGHT REDUCTION CHART provided above is 58 gallons per hour then the number of gallons would calculate to be 116 gallons ((200 nautical mph/100 nautical mph) * 58). The number of gallons of fuel for the fuel reserve would calculate to be 29 gallons (.5 *58). Therefore, the total number of gallons onboard is 145 gallons (116+29). The fuel weight would be 1,015 pounds (145 Gallons * 7 pounds).

4. OPERATING WEIGHT – Add items 1, 2 and 3.

5a. PERFORMANCE REFERENCES – List the specific Flight Manual supplement and hover performance charts used to derive Computed Gross Weight for Line 5b. In addition, provide a copy of the Flight Manual supplement and hover performance charts with the appropriate markings showing how it was derived.

5b. COMPUTED GROSS WEIGHT - Compute gross weights for HOGE for a Non-Jettisonable payload from the appropriate Flight Manual hover performance charts using the Pressure Altitude (PA) of 6,500 feet and temperature (OAT) 30 o Celsius.

6. WEIGHT REDUCTION – The Government Weight Reduction is required. The appropriate Weight Reduction value, for make & model, can be found in the Helicopter Services Fuel Consumption, and Weight Reduction Chart provided above.

7. ADJUSTED WEIGHT – Line 5b minus Line 6.

8. GROSS WEIGHT LIMITATION – Enter applicable gross weight limit from Limitations section of the basic

Flight Manual or the appropriate Flight Manual Supplement. This may be Maximum Gross Weight Limit for Take-Off and Landing, a Weight/Altitude/Temperature (WAT) limitation or a Maximum Gross Weight Limit.

9. SELECTED WEIGHT – The lowest weight, either line 7 or 8, will be entered. Applicable limitations in the Flight Manual must not be exceeded.

10. OPERATING WEIGHT – Use the value entered in Line 4.

11. ALLOWABLE PAYLOAD – Line 9 minus Line 10 is the maximum allowable weight (passengers and/or cargo) that can be carried for the scenario. Weight must be greater than 500 pounds.

SOLICITATION’S INTERAGENCY

HELICOPTER LOAD CHART

Hovering Out of Ground Effect – Non-Jettisonable Payload

Proposed Aircraft Make/Model:

N#:

Origin and Destination: PA: 6,500 feet OAT: 30 oC

1. HELICOPTER EQUIPPED WEIGHT:

2. FLIGHT CREW WEIGHT:

3. FUEL WEIGHT (_______gallons X 7 lbs per gal):

4. OPERATING WEIGHT (1 + 2 + 3):

5a. PERFORMANCE REFERENCES:

(List page/chart from FM) Attach a copy from the FM. The provided charts shall be marked by the

Offeror to show how the numbers were obtained.

5b. COMPUTED GROSS WEIGHT:

6. WEIGHT REDUCTION:

7. ADJUSTED WEIGHT

(line 5b – 6):

8. GROSS WEIGHT LIMITATION:

(FM Limitations Section)

9. SELECTED WEIGHT

(The lowest weight. Either line 7 or 8 will be entered):

10. OPERATING WEIGHT

(from line 4):

11. ALLOWABLE PAYLOAD (9 minus 10) (Weight must exceed 500 lbs):

(End of Summary of Changes)