Exhibit 13 - Aircraft Questionnaire_SEAT.pdf

EXHIBIT 13

AIRCRAFT QUESTIONNAIRE - SEAT

This questionnaire accurately completed will be used to determine the proposed aircraft payload capability.

REPRODUCE AND SUBMIT FOR EACH AIRCRAFT OFFERED - COMPLETE SHADED BLOCKS

Minimum Aircraft Requirements:

Must have a Standard and/or Restricted Airworthiness Certificate.

Aircraft certified under 14 CFR 23 or 25.

An aircraft make, and model for which engineering and logistical support, for continued airworthiness, is provided from the current type certificate holder or supplemental type certificate holder.

Minimum 1220 Shaft Horsepower VFR, Day Tank capacity of minimum 800 US gallons.

Aircraft capable of dispensing both water and fire retardant.

Minimum payload of 6,900 pounds with 2 hours and 30 minutes endurance, and 200 lb. pilot at 5,000’ PA Capable of operating from 5,000 ft. gravel runway at @ 7,000 ft PA and 30ºC, empty tank.

Cruise airspeed of at least 140 kts true airspeed at 7,000 ft PA and 30ºC, empty tank.

Aircraft must have the IAB approved, or Interim approved gate installed on the aircraft at the time of inspection.

All firefighting equipment must be available or installed at the time of inspection.

Payload amounts must be computed by using Exhibit 8: Airplane Approximate “Recommended Cruise” Fuel Consumption Rates, performance data from the Aircraft Flight Manual, weight and balance report, and equipment list that you provide.

Aircraft Make and Model FAA Registration # Serial # Cruise Airspeed

Tanker Number(s) If assigned Fire Gate Model Engine Installed

Aircraft Equipped Weight (Your aircraft weight & balance report & equipment list will be used to substantiate this weight – see note 1. below) Currently Installed Aircraft Equipment to be Removed to Achieve Offered Payload Below (If none, indicate NONE)

Equipment to be Added to Meet the Aircraft Specifications Requirements (If none, indicate

NONE)

EQUIPMENT ITEM WEIGHT EQUIPMENT ITEM WEIGHT

ENTER YOUR PROPOSED AIRCRAFT PAYLOAD (The aircraft make, model and payload that we confirm with you will be made a part of your offer and will be binding under any resulting contract.)

Note: By signing below, I acknowledge that I have included the following documentation to support the minimum aircraft requirements in Sections A and B:

(1) Current aircraft weight and balance report, as specified in Section B Weight and Balance

(2) Aircraft equipment list certified accurate at the time of weighing and any revisions to the list,

(3) Applicable Performance Charts

(4) Calculations showing performance characteristics of the aircraft. Calculations must include weight of the aircraft in contract configuration, crew, and fuel. (use 6.7 lbs. per gal. for fuel weight)

(5) 14 CFR Part 137 Certificate

By signing below, I certify to the best of my knowledge that the above information is accurate.

Name and Signature of Representative Completing this Form Date

OFFEROR’S NAME

DRAFT