Attachment G and G-1.pdf

OregonBuys Bid# S-62900-00015613– Type 2 Restricted Category Turbine Powered Helicopter

ATTACHMENT G

HELICOPTER SUMMARY

(PROPOSER MUST COMPLETE AND SUBMIT THIS PAGE WITH ITS PROPOSAL)

PROPOSER: ________________________________________________________

PRIMARY BASE LOCATION: _____________________________________

Proposers must submit a separate Helicopter Summary for each Primary Base location proposed, and for each helicopter designated at that Primary Base. Proposer must provide a copy of the current USFS/OAS Carding for each helicopter, mechanic, fuel truck and service/support vehicle designated under the Contract.

Company Address (Aircraft Hangar Location | “Home Base”):

COMPLETE EACH BOX AND CHECK YES OR NO FOR EACH YES/NO QUESTION BELOW.

HELICOPTER MAKE & MODEL:

FAA “N” NUMBER: YEAR BUILT:

GROSS WEIGHT: EMPTY WEIGHT:

FUEL CAPACITY (TOTAL GALLONS): FUEL (TOTAL HOURS):

NUMBER OF PASSENGERS (EXCLD PILOT): ENGINE H.P.:

ANNUAL INSPECTION (DATE ACCOMPLISHED):

GPS: YES NO

VHF RADIO (760 CHANNELS) : YES NO

P25 DIGITAL RADIO (NUMBER OF CHANNELS SELECTABLE):

CATEGORY (STANDARD OR RESTRICTED):

NUMBER OF HELMETS AVAILABLE (EXCLUDE PILOT):

JETTISONABLE PAYLOAD (HOGE-J) FROM “ATTACHMENT G-1”:

CARGO HOOK: YES NO

LONG LINE (HOW LONG):

CARGO NET, SWIVEL, AND LEADLINE (3000 lb. Minimum Rating): YES NO

MAIN ROTORS PAINTED IN CONTRASTING COLORS: YES NO

OregonBuys Bid# S-62900-00015613– Type 2 Restricted Category Turbine Powered Helicopter

ATTACHMENT G-1

AIRCRAFT PERFORMANCE DESIRABLE FEATURES

(PROPOSER MUST COMPLETE AND SUBMIT THIS PAGE WITH ITS PROPOSAL)

(30 POINTS MAX)

PROPOSER: __________________________________________________________________

PRIMARY BASE LOCATION: ________________________________________________

Proposers must submit a separate Aircraft Performance Desirable Features for each Primary Base location proposed, and for each helicopter designated at that Primary Base.

Type 2 Helicopter Minimum Performance:

Jettisonable payload (HOGE-J) of 1,850 pounds at 30 degrees C at 7,000 feet pressure altitude using a pilot weight of 200 pounds, and fuel for 1.5 hours.

Based on minimum performance requirements, 5 points will be awarded for each 100 lb. incremental increase for jettisonable payload (HOGE-J) above the minimum performance requirements.

Proposer shall provide an Interagency Helicopter Load Calculation form and FAA approved aircraft performance data (i.e., hover ceiling charts) and limitation used to compare gross weights and allowable payloads in the Interagency Load Calculations with this Attachment G-1. *Do not include the interagency weight reduction for make and model of helicopter.

HELICOPTER MAKE AND MODEL:

FAA “N” NUMBER:

EMPTY WEIGHT:

MAXIMUM PAYLOAD (HOGE)*:

Points Award Example:

Submitted aircraft jettisonable payload 1,950 pounds - minimum payload 1,850 pounds = 100 pounds (over the minimum) 100 pounds above minimum payload divided by 100 lbs. = 1 (rounded to nearest whole number) Multiply 1 x 5 points = 5 points (That is 5 points for every 100-pound increment above minimum payload)

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