B08_SOL_140D0424R0116_EU_MOCA.pdf

SECTION A – REQUIREMENTS AND PRICING

Solicitation 140D0424R0116 EU Helicopter Services, MORA, OLYM, NOCA

CONTRACT ACRONYMS

AC Advisory Circular AD Airworthiness Directive AIRS Aviation Invoice Reporting Support application AMS Aviation Management System A&P airframe and power-plant APCO Association of Public-Safety Communications Officials AQD Acquisition Services Directorate ASM Aviation Safety Manager ASO Aviation Safety Office ASTM American Society for Testing and Material ATC air traffic control AUR aircraft use report CASTPE Chief, Aviation Safety, Training and Program Evaluations CFR Code of Federal Regulations CO Contracting Officer COR Contracting Officer’s Representative CTCSS continuous tone coded squelch system DM degrees/minutes/decimal minutes DOI Department of Interior DOT Department of Transportation ELT emergency locator transmitter EPA Environmental Protection Agency ERG Emergency Response Guidebook EU exclusive use FAA Federal Aviation Administration FAR Federal Acquisition Regulations FS Forest Service FTR Federal Travel Regulations GVW gross vehicle weight GPM gallons per minute GPS global positioning system HIGE hover-in-ground effect HOGE hover-out-of-ground effect HOGEJ hover-out-of-ground effect, jettisonable

IAT interagency aviation training IBC Interior Business Center ICAO International Civil Aviation Organization ICS intercom system IFR instrument flight rules IIC Investigator in Charge IP Institute of Petroleum IPP Invoice Processing Platform ISA International Standard Atmosphere MMSB Manufacturer’s Mandatory Service Bulletins NFPA National Fire Protection Association NTSB National Transportation Safety Board NWCG National Wildfire Coordinating Group OAS Office of Aviation Services PA public address system PA pressure altitude PFD personal flotation device PIC pilot-in-command PPE personal protective equipment PSD plastic sphere dispenser PSI pounds per square inch PTT push to talk RPM revolutions per minute SFI Safety Foundation Incorporated STEP Single-skid, Toe-In and Hover Exit/Entry Procedures TBO time between overhaul TERO Tribal Employment Rights Ordinances TSO technical service order UL Underwriter’s Laboratory USDA United States Department of Agriculture VFR visual flight rules VNE velocity never exceed VOX voice activation VSWR voltage standing wave ratio

EU Helicopter Services, MORA, OLYM, NOCA

SCHEDULE OF SUPPLIES/SERVICES

A1. Item Requirement

The intent of this contract is to obtain a fully contractor operated and maintained exclusive use helicopter for 139 calendar days to support project/resource work, fire management, and search and rescue for the NPS and other agencies in the Pacific Northwest to include, but not limited to: Mount Rainier, Olympic and North Cascade National Parks (May 01-Sep 17). This contract has a Base Year with four 1-year Option Years.

ITEM DESCRIPTION

Designated Base: Enumclaw, WA (WA77)

Exclusive Use Period: 139 Days (May 01-Sept 17)

Aircraft Requirements: One light helicopter (As specified in Section B).

Crew Compliment Required: Pilot-in-Command (PIC) with relief pilot, fuel service vehicle driver with relief driver, and mechanic with relief mechanic. The Contractor may provide a mechanic that is also the fuel service vehicle driver.

Fuel Servicing Vehicle Requirement: One vehicle equipped as specified in Section B8.

Additional Fuel Trailers Requirement: Two fuel cache trailers are required for this contract. This is in addition to fuel truck required (See B8.6)

Minimum Helicopter Requirements:

Seating: Five (5) insured passenger seats not including pilot, but including copilot seat in an aircraft, normally single pilot operated.

Payload: Non-jettisonable payload (HOGE) of 450 pounds at 0 degrees Celsius at 14,000 feet pressure altitude using a pilot weight of 200 pounds, a 25-pound survival kit and for 1.0 hour of flight time.

Powerplant: Turbine engine

Airspeed: 155 knots VNE at sea level

Landing Gear: Skid Type

Fuel System: Crash Resistant Fuel System

Target Helicopter Requirements:

Payload: Non-jettisonable payload (HOGE) of 650 pounds at 0 degrees C at 14,000 feet pressure altitude using a pilot weight of 200 pounds, a 25-pound survival kit, and fuel for 1.0 hour of flight time.

Performance: BLR FastFin® or equivalent system Dual Hydraulics

Note 1: Payload amounts shall be computed by using the Government’s Standard Interagency Load Calculation Method and Form and the Helicopter Fuel Consumption and Weight Reduction Chart included under Exhibits along with the offered aircraft’s applicable Hover Ceiling Charts, weight and balance report and equipment list that you provide.

Note 2: Exhibits that will be applicable under the contract are included at the end of Section C.

EU Helicopter Services, MORA, OLYM, NOCA

A2. Schedule Of Services And Prices

IMPORTANT INFORMATION:

The contract price shall include all applicable Federal, State, and local taxes and duties as per FAR 52.212-4(k) Taxes.

A2.1 Instructions For Completion Of The Following Pricing Schedules:

1. Enter the offeror’s name on each pricing page being submitted. The name should correspond with the name entered on the SF1449 and the 14 CFR 135 holder’s name as established by the certificate holder. (Remittance address information different than that entered on the SF1449 form should be included on the “Offeror’s Miscellaneous Information” page included in Section E.)

2. Enter the applicable make and model of the aircraft being offered along with a daily availability, flight rate, dry flight rate, and extension rates for the base period and all option periods. Pricing must be included for all years for the offer to be acceptable.

3. Enter individual FAA registration number(s) of each aircraft where identified.

4. The Pricing Schedule pages included in this document will be made a part of subsequent individual conformed contract, if selected for award.

5. Complete and submit a separate Pricing Schedule for each aircraft offered. Offers will NOT be evaluated or considered for any item for which all pricing pages are not complete.

6. All pricing shall be in whole dollars only.

7. Complete all shaded areas only.

DESIGNATED

REPORTING BASE

Enumclaw Airport EXCLUSIVE USE PERIOD 139 Days

May 01, 2025 through September 17, 2025 (Estimated)

AIRCRAFT FOR

THIS

PRICING SCHEDULE

Make/Model FAA Registration

OFFEROR NAME

DESCRIPTION

PAY

ITEM

CODE

QUANTITY

UNIT

UNIT PRICE

EXTENDED AMOUNT

DAILY AVAILABILITY PRICE PER DAY – GUARANTEED SUBJECT TO BEING AVAILABLE

Daily Availability

AV

Guaranteed

DAYS

Estimated Flight Hours

FT

Estimated

FLIGHT HOURS

Flight Hours - Alaska

FD

EXTENSION (Optional)

EXTENSION (Optional) Estimated Flight Hour

Additional pay items (T&M line item)

See Additional Pay Items Schedule

$50,000.00 NTE

BASE PERIOD

ESTIMATED SUBTOTAL

EU Helicopter Services, MORA, OLYM, NOCA

DESIGNATED

REPORTING BASE

Enumclaw Airport EXCLUSIVE USE PERIOD 139 Days

May 01, 2026 through September 17, 2026 (Estimated)

AIRCRAFT FOR

THIS

PRICING SCHEDULE

*If Ordered

EXTENSION (Optional)

Additional pay items (T&M line item)

See Additional Pay Items Schedule

$50,000.00 NTE

OPTION PERIOD ONE

ESTIMATED SUBTOTAL

*The entire quantity is guaranteed if an order is placed. Not to be confused with Minimum Guarantee (see A2.2)

Enumclaw Airport EXCLUSIVE USE PERIOD 139 Days

May 01, 2027 through September 17, 2027 (Estimated)

AIRCRAFT FOR

THIS

PRICING SCHEDULE

EXTENSION (Optional)

Additional pay items (T&M line item)

See Additional Pay Items Schedule

$50,000.00 NTE

OPTION PERIOD TWO

ESTIMATED SUBTOTAL

*The entire quantity is guaranteed if an order is placed. Not to be confused with Minimum Guarantee (see A2.2)

EU Helicopter Services, MORA, OLYM, NOCA

DESIGNATED

REPORTING BASE

Enumclaw Airport EXCLUSIVE USE PERIOD 139 Days

May 01, 2028 through September 17, 2028 (Estimated)

AIRCRAFT FOR

THIS

PRICING SCHEDULE

EXTENSION (Optional)

Additional pay items (T&M line item)

See Additional Pay Items Schedule

$50,000.00 NTE

OPTION PERIOD THREE

ESTIMATED SUBTOTAL

*The entire quantity is guaranteed if an order is placed. Not to be confused with Minimum Guarantee (see A2.2)

Enumclaw Airport EXCLUSIVE USE PERIOD 139 Days

May 01, 2029 through September 17, 2029 (Estimated)

AIRCRAFT FOR

THIS

PRICING SCHEDULE

EXTENSION (Optional)

Additional pay items (T&M line item)

See Additional Pay Items Schedule

$50,000.00 NTE

OPTION PERIOD FOUR

ESTIMATED SUBTOTAL

*The entire quantity is guaranteed if an order is placed. Not to be confused with Minimum Guarantee (see A2.2)

EU Helicopter Services, MORA, OLYM, NOCA

A2.2 Minimum Guarantee. The Minimum Guarantee under the contract, as required by contract clause 52.216- 22, is 139 days of Daily Availability from the Rate Schedule for the first year of the contract. Immediately after contract award, the Contracting Officer will issue a task order obligating the guaranteed minimum amount.

However, the guaranteed quantity for daily availability is subject to reductions due to unavailability.

A2.3 Maximum Quantity. The maximum quantity of services the Government may order under the contract (ceiling amount) is $7,000,000. This amount is not historical or planned expenditure but set in accordance with FAR 16.504(a)(4).

A2.4 Obligation of Funding. Funding will not be obligated under the Indefinite-Delivery, Indefinite-Quantity (IDIQ) contract. The Contracting Officer will issue a separate task order prior to the exclusive use period for each option period covered under the contract. Each task order will obligate funding for the payment of aircraft services.

A2.5 In the Lower-48 states all fuel shall be provided by the contractor and should be included in the flight rate (wet rate).

A2.6 In Alaska, fuel will be furnished by the Government. All fuel not otherwise furnished by the Government must be purchased by or charged to the Contractor. The purchase must be approved by the Contracting Officer.

Fuel related costs shall be recorded as a line entry (i.e., date, fuel charge, dollar amount, and use-item code fuel charge [FC]), shall be used and shall be supported by paid legible, itemized invoices from the supplier. Certified true copies may be submitted in lieu of the original invoice.

A2.7 Rates for flight hours shall be in whole dollars. If the unit prices are adjusted during the life of the contract, they will be adjusted to a whole dollar as follows: amounts of 50 cents or less will be rounded down and amounts of 51 cents or more will be rounded up.

A3 Additional Pay Items (Time & Materials IAW FAR 52.212-4 Alt 1)

A3.1 Additional Pay Items Schedule

Note: The rates below are applicable for the entire five-year term of the contract.

ITEM

CODE

QUANTITY UNIT UNIT PRICE

Extended Standby – Pilot EP Indefinite Hour $62.00

Extended Standby – Driver ET Indefinite Hour $42.00

Extended Standby - Mechanic EM Indefinite Hour $50.00

Fuel Servicing Vehicle – Mileage SMM Indefinite Mile 350-749 gal - $1.89

Fuel Servicing Vehicle – Mileage SML Indefinite Mile 750-1,499 gal - $2.64

Fuel Servicing Vehicle – Mileage SMX Indefinite Mile 1,500 or more gal - $3.67

Fuel Charge (Alaska Only) FC Indefinite Gallons Actual Cost

Subsistence Allowance (Per Diem) PD Indefinite Overnight Standard or High GSA Rate

Special Charge for Miscellaneous Allowable Expenses (i.e., rental car expenses, tie downs, Dept. of Transportation fees, etc.)

SC Indefinite Each Actual Cost

See C21

EU Helicopter Services, MORA, OLYM, NOCA

A3.2 Aviation Fuel Information

The contract's hourly flight rates are subject to economic price adjustments (EPA) for changes in the price of the Jet Fuel (CONUS) fuel base price (see C13, Economic Price Adjustment-Fuel).

IMPORTANT NOTICE: The hourly flight rates proposed are subject to adjustment, up or down, due to the fluctuation in jet fuel price from the reference below. It is important for the contractor to understand the ramifications of the contract's Economic Price Adjustment clause (see C13). The referenced price below (in this section) should be considered when developing the hourly flight rates offered in your proposal. If the referenced price per gallon for jet fuel changes in accordance with section C13, the Government or contractor is entitled to an adjustment to the hourly flight rates based upon the change in fuel price per gallon and the economic cruise speed and fuel consumption of the contract aircraft. The Contractor agrees to accept price adjustments, up or down, based upon its aircraft fuel consumption information and the current reference price of jet fuel at the time of the adjustment. The adjustments will be made via issuance of a bilateral modification, which must be agreed to by both parties prior to being fully executed.

Make/model of Aircraft Jet Fuel Requested/Effective Date of Price Adjustment

Referenced Fuel Source Location: KTIW Tacoma Narrows Airport

Full service Fuel price obtained from http://www.airnav.com/fuel ph: 253-798-3779

Base Fuel Price $ 5.27 Fuel Price at adjustment (also becomes New Base)

Effective Date Date of Award Effective Date

Source Document Original Contract Source Document

Rate Adjustment $ X consumption rate of Increase or

Decrease Due

Current Flight Rates

1st Contract Year:

2nd Contract Year:

3rd Contract Year:

4th Contract Year:

5th Contract Year:

Adjusted Flight Rates

1st Contract Year:

2nd Contract Year:

3rd Contract Year:

4th Contract Year:

5th Contract Year:

*Base Fuel Prices will be updated at time of award.

http://www.airnav.com/fuel

SECTION B – TECHNICAL SPECIFICATIONS

EU Helicopter Services, MORA, OLYM, NOCA

GENERAL REQUIREMENTS

B1 Scope of Contract

B1.1 The intent of this contract is to obtain fully Contractor operated and maintained exclusive use helicopter flight services to transport personnel and/or cargo in support of Government natural resource missions. Contractor services include provisions of a helicopter, personnel, fuel servicing vehicle, fuel, and all other associated equipment as prescribed in this contract. Missions will include, but are not limited to, short-haul, search and rescue, STEP (single-skid, toe-in, hover entry/exit procedures) landings, fire suppression, fire monitoring, initial attack, prescribed fire and aerial ignition, law enforcement limited to nonthreatening surveillance and reconnaissance, and other administrative and related resource activities. Missions will require flight operations to be conducted above 10,000 feet PA but less than 18,000 feet PA for periods of time of up to two-hour duration.

Contractors must ensure compliance with applicable FAA regulatory requirements concerning the use of oxygen.

The Government will direct aircraft to support its missions and objectives.

B1.2 Law enforcement missions include but are not limited to, transporting Federal personnel to a law enforcement location, short-haul into grow sites, low-level reconnaissance, or surveillance flying, and prisoner transport. Law enforcement officers will fly with loaded firearms on-board the aircraft and may enter areas of potential contraband activity. Firearms will be transported in accordance with policy and guidance contained in the NWCG Standards for Helicopter Operations (NSHO) (formerly IHOG) and Interagency Aviation Transport of Hazardous Material. Each of these documents may be found at the following link:

https://www.doi.gov/aviation/library/guides. The pilot and air crew will jointly conduct risk assessments for all missions to determine the risk and hazards. No mission will be flown that presents a high level of risk.

B1.3 During the exclusive use period and any subsequent extension, aircraft furnished shall be subject to the exclusive use and control of the Government 24 hours per day, 7 days per week.

B1.4 The Government and Contractor must establish an effective working relationship to successfully complete this contract. The Contractor’s employees’ cooperation, professionalism, and positive attitude toward accomplishment of the mission and aviation safety are an integral element of this relationship.

B1.5 The Government has interagency and cooperative agreements with other Federal and State agencies and private landholders and may dispatch aircraft under this contract for such cooperative use.

B1.6 This aircraft may be dispatched to Alaska. Because deployment to Alaska usually requires transit through Canada, all required contractor personnel must possess current passports. For the Alaska-specific equipment and/or operational requirements, refer to the Alaska Supplement Exhibit (see Section C).

B2 Certifications

The Contractor must hold and keep current all the following required certificates and must ensure that contract aircraft are operated and maintained in compliance with those certificates at all times:

B2.1 A Federal Aviation Administration (FAA) Air Carrier or Operating Certificate which authorizes the Contractor to operate in the category and class of aircraft and under flight conditions required by this contract (e.g., rotorcraft, visual flight rules (VFR) day/night, passengers, and cargo) in the 48 contiguous United States and Alaska.

B2.2 A Title 14 of the Code of Federal Regulations, Part 135 (14 CFR 135) Air Carrier Certificate. These aircraft must be carried on the list required by 14 CFR 135.63 or Operations Specifications Part D, "Aircraft Listing," as appropriate.

https://www.aff.gov/

EU Helicopter Services, MORA, OLYM, NOCA

B2.3 A 14 CFR 133, Rotorcraft External Load Operations Certificate which authorizes Class B loads, as a minimum. The contract aircraft must be carried on the list required by 14 CFR 133.27(a) (Operations Specifications Part D, "D085 Aircraft Listing").

B2.4 A 14 CFR 137, Agricultural Aircraft Operations Certificate. These aircraft must be carried on the list required by 14 CFR 133.27(a) (Operations Specifications Part D, "Aircraft Listing").

B2.5 The contract aircraft must have a Standard Airworthiness Certificate. Installation of any equipment required by this contract must be FAA-approved.

B3 Order of Precedence (Specifications)

In the event of inconsistencies within the technical specification, the following order will be used in such resolution: (1) typed provisions of these specifications; (2) DOI Office of Aviation Services (OAS) supplements and/or exhibits incorporated by reference; (3) 14 CFR incorporated by reference; (4) aircraft manufacturer's specifications; (5) other documents incorporated by reference.

B4 Contracts

B4.1 The Contractor must maintain a complete, current copy of the contract, modifications, and task orders (if applicable) in each contract aircraft throughout the performance period.

B4.2 The pilot must have task order information (i.e., task number, performance period) in his/her possession prior to any flights under this contract and make this information available to government representatives on request.

B4.3 Electronic copies of contracts and task orders may be used. However, the contractor is responsible for ensuring that the documents are uploaded on an appropriate viewing device (e.g., laptop or tablet), which must be charged and made available at the aircraft for reference by government representatives upon request. Further, the contractor must agree to hold the government harmless for any inadvertent or accidental damage to the device.

EQUIPMENT REQUIREMENTS

B5 Condition of Equipment

The Contractor-furnished helicopter, and all other required equipment must be operable, free of damage, and in good repair. Aircraft systems and components must be free of leaks, except where specified by the manufacturer.

B6 Aircraft Equipment Requirements

The Contractor must provide one fully compliant helicopter that is equipped as shown below for each item:

B6.1 A complete set of current aeronautical charts covering the expected area of operations.

Note: Electronic flight bags are acceptable if authorized by the FAA in the company’s operation specifications.

B6.2 One digital hour meter installed in a location visible by the pilot and front seat observer while seated. The meter must be wired in series with a switch on the collective control, and a switch activated by engine or transmission oil pressure or by equivalent means, to record flight time only.

B6.3 Free air temperature gauge.

B6.4 One set of individual lap belts for each installed seat.

EU Helicopter Services, MORA, OLYM, NOCA

B6.5 Double strap shoulder harness with automatic or manual locking inertia reel for each front seat occupant.

Shoulder straps and lap belts must fasten with one single-point metal-to-metal, quick-release mechanism. Heavy-duty (military- style) harnesses with fabric loop connecting the shoulder harness to the male portion of the lap belt buckle are acceptable.

B6.5.1 Shoulder harnesses equipped with inertia reel (either single-strap or double-strap) for each aft cabin occupant. Shoulder harness straps and lap belts must fasten with a single-point, metal- to-metal, quick-release mechanism.

B6.6 Utility folding aft cabin seating for easy access to a flat cabin floor equipped with tie downs for carriage of bulky cargo.

B6.7 Fire extinguisher(s), as required by 14 CFR 135, must be a handheld bottle, minimum 2-B:C rating, mounted and accessible to the flight crew while seated. (See the fire extinguisher maintenance instructions in Section B29.)

B6.8 Dual controls for initial pilot performance evaluation. (May also be required for interim or recurrent pilot performance evaluations at the option of the Government.)

B6.9 Aircraft lighting for night operation in accordance with 14 CFR 91.205(c), including instrument lights.

B6.10 Flight instruments for low visibility flight conditions, including gyroscopic bank and pitch indicator (ADI), directional gyro, vertical speed indicator and rate of turn indicator or skid/slip indicator or inclinometer.

Note: In lieu of these listed instruments, a single, new generation electronic instrument providing combined data meeting at minimum the following TSO’s, C3e, C4c, and C113A.

B6.11 A strobe light (with either a white, or half- white/half-red lens) or a flashing LED (red or white), mounted on top of the aircraft or otherwise visible from above, with an independent activating switch. A red strobe or rotating beacon does not satisfy this requirement.

B6.12 High visibility, pulsating, forward-facing, conspicuity lighting.

B6.13 High visibility markings on main rotor blades as specified by the Acceptable Paint Schemes Exhibit.

B6.14 High-skid-type landing gear if manufactured for make and model.

B6.15 Personnel access steps for aircraft with a floor height greater than 18 inches to ensure safe entrance and exit from each door.

B6.16 Locking cap(s) on all fuel inlet ports.

Note: Closed-system, single-point refueling port dust caps need not have an FAA-approved locking device.

B6.17 Cabin heater and window defogger.

B6.18 Wire strike protection system (mechanical).

Note: If manufactured for the make and model of helicopter.

B6.19 Main rotor brake.

B6.20 Cabin doors which may be removed or opened in flight. (See B6.34.1)

B6.20.1 A sliding left rear door. (See B6.34.1)

EU Helicopter Services, MORA, OLYM, NOCA

B6.20.2 A protective covering for the floor to include the area adjacent to the installed floor guards and the area under the rear seats must be installed. Cargo tie down points to accommodate cargo in the area where the seat is removed must be installed.

B6.21 Cargo compartment, internal and external capable of accommodating 58-inch long shovels, rakes, and other tools as specified below:

For internal:

B6.21.1 15-cubic-foot baggage compartment within the aircraft fuselage specifically designed to carry cargo separate from the cabin.

Note: Requires rear bulkhead modification required on some models of aircraft.

For external:

B6.21.2 Cargo basket. An externally side-mounted basket constructed with tubular frame and expanded metal incorporating a locking lid to secure cargo.

Note: Aircraft must be equipped with a cargo basket such as the Dart Heli-Utility basket model D350-607-045 (96” length) or equivalent. Basket must be quick attach/detach.

All construction methods must be as prescribed by Advisory Circulars 43.13-1B and 43.13-2B or other FAA approval.

B6.22 Cargo restraint system for aircraft manufactured with a parcel/storage area behind the rear passenger seats.

B6.23 An accessory power source consisting of an MS 3112E-12-3S three-pin connector, accessible in the aft cabin. Pin B must be airframe ground; pin A must be +28VDC (for 28- volt aircraft); and pin C must be +14VDC (for 14- volt aircraft). The circuit must be protected by a 5-amp circuit protection.

B6.24 A first aid kit containing items specified in the First Aid and Survival Kits Exhibit (see Section C) must be carried aboard the aircraft on all flights.

B6.25 A survival kit containing items specified in First Aid and Survival Kits Exhibit (see Section C) must be carried aboard the aircraft on all flights and must be included in weight and balance/load calculations.

B6.26 A convex mirror for the pilot to observe the sling load.

B6.27 One keeperless cargo hook that may be loaded and locked in a single motion with one hand and is rated at the maximum lifting capacity of the aircraft. This hook must incorporate both an electrically activated release and a secondary mechanically activated release. The electric release must be activated by a switch on the cyclic. The switch must be guarded/protected to minimize the possibility of inadvertent activation. The secondary mechanical release must incorporate a hydraulically activated release if available for the make and model of helicopter. (See the cargo hook maintenance requirements in Section B29.)

B6.28 Cockpit-mounted external load indicator with readout of weight carried on the cargo hook.

B6.29 One collapsible, variable capacity water/retardant bucket. See the Water Bucket Use Procedures Exhibit (see Section C). The bucket must have a manufacturer's capacity adjustment commensurate with the maximum lifting capability (HOGE-J) of the contract aircraft at 5,000 feet pressure altitude (PA), 30˚ Celsius with a 200-pound pilot, 25-pound survival kit, and 1.5 total hours of fuel. The bucket must be capable of being operated with all increments of the longline; i.e., 50, 100, 150 feet.

EU Helicopter Services, MORA, OLYM, NOCA

B6.30 A second collapsible, variable capacity water/retardant bucket. See the Water Bucket Use Procedures Exhibit (see section C). The bucket must have a manufacturer's capacity adjustment commensurate with the maximum lifting capability (HOGE-J) of the contract aircraft at 7,000 feet PA, 30˚ Celsius with a 200- pound pilot, 25-pound survival kit, and 1.5 total hours of fuel. The bucket must also be capable of being operated with all increments of the longline; i.e., 50, 100, 150 feet.

Note: The bucket combinations provided in B6.29 and B6.30 must provide adjustments that allow the widest range of altitude/temperature combinations (subject to the limitations of the bucket manufacturer’s available sizes) for the maximum lifting capability of the helicopter beginning at 5,000 feet PA at 30˚ Celsius extending upward to 7,000 feet PA at 30˚ Celsius and above.

B6.31 A remote operating switch for the water/retardant bucket and/or remote hook clearly marked for "open" and "closed" and mounted on the collective control to avoid confusion with the airframe cargo hook release. The switch must be of a different design and must be mounted so as to not easily be confused with the RPM Control [Beep Range] switch.

B6.32 Part number MS 3101E-24-11S, nine-pin connector, for use as the power source for a helitorch or remote cargo hook. Pin D must be airframe ground. Pin E must be switched 28VDC, protected by a manually operable, 50- amp circuit breaker. The water bucket/tank open switch must also activate this circuit.

B6.32.1 A lanyard to support the connector and mounted within 12 inches of the cargo hook.

B6.32.2 This connector must have multiple circuit capacity sufficient to provide power and control for Contractor-furnished equipment. The longline remote hook, fixed tank, or water bucket must be wired through this connector. A list of water buckets with required pin wiring can be found in the USDA Forest Service/DOI OAS Drawing A-16 Exhibit (see Section C). Wiring diagrams for various equipment configurations are available from the U.S. Department of the Interior, Office of Aviation Services, 300 E. Mallard Drive, Suite 200, Boise, ID 83706, or USDA Forest Service, 3833 S. Development Avenue, Boise, ID 83705-5354.

B6.33 One remote cargo hook with related cabling and release system complying with the following specifications:

B6.33.1 Electrically activated remote cargo hook that may be loaded and locked in a single motion with one hand and that is rated at the maximum lifting capacity of the aircraft.

B6.33.2 The remote hook must be protected by a metal ring or cage that does not interfere with the use or function of the hook.

B6.33.3 Synthetic rope meeting the requirements of the Helicopter Synthetic Longline Requirements Exhibit (see Section C).

B6.33.4 Two ropes are required; one each in 50-foot and 100-foot lengths.

B6.33.5 Electrical cables must be protected from pinching by hooks or shackles and from damage caused by stretching of the line. The electrical wire must be long enough at the aircraft cargo hook end to prevent a swinging load from unplugging the electrical connector.

B6.33.6 All fabrication and installation methods must comply with 14 CFR 133 and Advisory Circular 43.13–1B.

B6.33.7 Operating switch for the remote hook. (See B6.31 for specifications. Only 1 switch required)

B6.34 Short-haul configuration. Helicopter to be equipped for short-haul and cargo letdown operations that must meet the following specifications:

EU Helicopter Services, MORA, OLYM, NOCA

B6.34.1 Sliding or hinged door on side which can be opened while in flight. Door locks must be provided to ensure that the door remains in closed and open positions. Doors may also be removed from the helicopter to meet these requirements provided the aircraft manual authorizes such removal.

B6.34.2 Dual external airframe mounted cargo hook system certified for Human External Cargo (HEC) operations.

B6.34.3 A Supplemental Type Certificate (STC’d) rappel fixture (used for short-haul spotter and aerial recon anchor) appropriate to the make and model offered. This anchor must be maintained in accordance with the manufacturer’s instructions for continued airworthiness.

B6.34.3.1 For AS350/H125 Series aircraft, a hoist operators anchor point installed per section 2.B.2.c and figure

(2) on page 23 in AS350 Service Bulletin No. 25.00.15. This anchor point will be used in lieu of the rappel fixture for the short-haul spotter’s safety harness tether.

B6.35 Snow/Tundra Pads.

Note: To be installed when requested by the government.

B6.36 Snow kit or necessary equipment to allow flight during falling snow.

B6.37 Engine intake filtering device or particle separator (if manufactured for model), capable of filtering sand and dust particles.

B6.38 The Contractor may be required to install National Park Service insignia on each side of the aircraft. The insignias are self-adhesive, approximately 9 inches high and 7 inches wide. Insignias will be furnished by the Government.

B6.39 Internal Litter Kit

Note: Fixed provisions must be installed. Litter to be installed when requested by the Government.

B7 Avionics Requirements

B7.1 General

B7.1.1 The Contractor must provide, install, and maintain the following systems in accordance with the manufacturer's specifications and the installation and maintenance standards of Section B7. Detailed avionics systems performance requirements are listed in Avionics Operational Test Standards (FS/OAS_A24F.pdf) (copies available upon request from OAS Avionics, or the most recent list may be found online at:

https://www.nifc.gov/resources/NIICD/niicd-documents .)

B7.2 Avionics Installation and Maintenance Standards

B7.2.1 Strict adherence to the recommendations in the following FAA Advisory Circulars is required: AC 43.13 1B Chapter 11, "Aircraft Electrical Systems," and Chapter 12, "Aircraft Avionics Systems”; AC 43.13 2B Chapter 1, "Structural Data," Chapter 2, "Communication, Navigation, and Emergency Locator Transmitter System Installations," and Chapter 3, "Antenna Installation."

B7.2.2 All avionics systems requiring an antenna must be installed with a properly matched, aircraft-certified antenna, unless otherwise specified. Antennas must be polarized as required by the avionics system and must have a voltage standing wave ratio (VSWR) of 3.0 to 1 or better.

https://www.faa.gov/regulations_policies/handbooks_manuals/aviation/ https://www.doi.gov/aviation/library/guides

EU Helicopter Services, MORA, OLYM, NOCA

B7.2.3 Although the contract aircraft may not be certified for flight under instrument flight rules (IFR), the aircraft's static pressure system, altimeter instrument system, and automatic pressure altitude reporting system must be maintained in accordance with the IFR requirements of 14 CFR Part 91.411 and inspected and tested every 24 calendar months, as specified by 14 CFR Part 43, appendices E and F.

B7.2.4 Transmitters shall not open squelch on, or interfere with, other AM or FM transceivers in the aircraft which are monitoring different frequencies. So-called “Transmit Interlock” functions shall not be used with communication transceivers.

B7.2.5 All installed transceivers must be placarded with designations matching the transmitter/receiver controls on the installed audio control system(s)

B7.3 Communications Systems

B7.3.1 One automatic-fixed Emergency Locator Transmitter (ELT), certified under TSO-C126 (or newer) which must be installed in a conspicuous or marked location, and meet the same requirements as those detailed for aircraft in 14 CFR 91.207 (excluding section f). If not powered by its own, integral battery, the ELT remote switch/light must be powered by unswitched aircraft power. ELT antennas must be mounted externally to the aircraft unless installed in a location approved by the aircraft manufacturer. TSO-C126 and newer ELTs require documentation of current registration with the National Oceanic and Atmospheric Administration (NOAA), or the national civil aviation authority with which the aircraft is registered.

B7.3.2 Two panel-mounted VHF-AM (VHF-1, VHF-2) aeronautical transceivers, each with a minimum of 760 channels covering 118.000 to 136.975 MHz. The transceivers must have channels selectable in no greater than 25 kHz increments and a minimum of 5 watts carrier output power. The transceivers’ operational controls must be mounted so they are readily visible and accessible to the pilot. Although not required by Federal Aviation Regulations, the aircraft’s radio call sign (normally the aircraft registration number) must be displayed on the instrument panel, in view of the flight crew.

B7.3.3 Two P25-compliant VHF-FM transceivers. Each transceiver (FM-1, FM-2) must provide selection of narrowband analog (12.5 kHz) or narrowband digital (12.5 kHz) operation on each of a minimum of 100 channels. Each transceivers’ operational controls must be located and arranged so that the pilot and observer/copilot when seated, have full and unrestricted movement of each control without interference from clothing, the cockpit structure, or the flight controls.

B7.3.3.1 Each VHF-FM transceiver’s operational frequency range must include the band of 136.0000 MHz to

173.9975 MHz. The operator(s) must be able to program any usable channels within that band, along with any required CTCSS tones, National Access Codes (NAC’s), or Talk Group ID’s (TGID’s), while in flight. Each VHF-FM transceiver must also incorporate a separate, programmable GUARD receiver, with accompanying GUARD transmit capability. Unless instructed by the Government for use on a specific project, all frequencies programmed for use under this Contract must be in the narrowband analog mode.

B7.3.3.2 Carrier output power for each VHF-FM transceiver must be 10 watts nominal value (original design specification). Each transceiver must be capable of displaying receiver and transmitter operating frequency, alpha-numeric channel labels, and must provide both receiver and transmitter activation indicators for MAIN and GUARD. Simultaneous monitoring of both MAIN and GUARD receivers is required. Scanning of the GUARD frequency is not acceptable.

B7.3.3.3 Prior to acceptance under this contract, at least one VHF-FM transceiver must be programmed with the narrowband analog GUARD receive and transmit frequencies of 168.625 MHz, with a 110.9 Hz CTCSS tone on transmit only.

B7.3.3.4 The following VHF-FM aeronautical transceivers are known to meet the above requirements:

EU Helicopter Services, MORA, OLYM, NOCA

Techni Sonics: TDFM-136, TDFM-136A, TDFM-136/NV, TDFM-136A/NV, TDFM-136B, TDFM-136B/NV.

Cobham: (formerly NAT) NPX-136D-070.

B7.3.3.5 Each required VHF-FM transceiver must be equipped with a conveniently located programming port, to facilitate programming via a government-owned laptop computer. The port(s) must be protected from accidental damage via contact, be hard-wired to the transceiver(s), not require switching of any cables for utilization, and must be conveniently located for ease of use. The Contractor must also furnish appropriate cables of adequate length, and/or any necessary adapters, to interconnect the aircraft programming ports to the serial and/or USB port(s) of the Government laptop computers as required.

NOTE: The “DIN” type connector receptacle on the front panel of some TDFM-136-series radios is part of an encryption feature and may not function as a programming port connector. This connector can be utilized for channel programming on model TDFM-136A, serial numbers FDA1200 and higher, and model TDFM-136B

ONLY.

B7.3.4 Provisions for auxiliary VHF-FM (AUX-FM) portable radio:

B7.3.4.1 Interface for installing and properly operating an auxiliary VHF-FM portable radio through the aircraft's audio control system(s). The interface must consist of the appropriate wiring from the audio control system, terminated in an ITT/Cannon type MS3112E12 10S 10-pin connector conveniently located for use by the observer/copilot, and utilizing the contact assignments as specified by drawing FS/OAS A-17 in Exhibit 8.

B7.3.4.2 One weatherproof, external, broadband antenna covering the 150-174 MHz band, with associated RG 58A/U (or equivalent) coaxial cable and connector, terminated in a bulkhead-mounted, female BNC connector (type UG-290A), conveniently located for use by the observer/copilot adjacent to the above 10-pin connector (Comant model CI 177 or equal).

B7.3.4.3 Mounting facilities for securely installing the auxiliary VHF-FM portable radio in the cockpit in accordance with the FAA AC 43.13-2B specifications. Locate and arrange the mounting facilities so that a seated observer/copilot has full and unrestricted movement of the radio's controls, without interference from the 18-inch adapter cable, clothing, cockpit structure, or flight controls.

B7.3.4.4 Positive-polarity microphone excitation voltage provided to the AUX-FM system from the aircraft DC power system through a suitable resistor network. A blocking capacitor must be provided to prevent the portable radio microphone excitation voltage from entering the system. Sidetone for the AUX-FM must also be provided (NAT model AA34-300, Premier model PA-34, or equivalent).

B7.3.4.5 In lieu of the above AUX-FM requirements, the Contractor may substitute an additional VHF-FM aeronautical transceiver (FM-3) which meets the requirements for the VHF-FM aeronautical transceiver(s) as detailed above.

B7.3.5 Automated Flight Following (AFF) Program

B7.3.5.1 One satellite-based aircraft tracking hardware for each aircraft offered, compatible with the government’s AFF Program (https://www.aff.gov). Not all available satellite-based tracking systems are compatible with the Government’s AFF Program, nor meets AFF’s requirements. The contractor must ensure that the aircraft hardware offered is compatible with AFF.gov. For questions about current compatibility requirements, select the “HELP” button at https://www.aff.gov.

B7.3.5.2 The AFF aircraft hardware must be powered by the aircraft’s electrical system, installed per the manufacturer’s installation manual, and operational in all phases of flight. AFF aircraft hardware must utilize as a minimum: Satellite communications, an externally or internally mounted antenna, provide data to the https://www.aff.gov/ https://www.doi.gov/aviation/safety/helmet

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Government’s AFF viewing software, use aircraft power via a dedicated circuit breaker for power protection, and be mounted to not endanger any occupant from AFF aircraft hardware during periods of turbulence. Antennas should be placed where they have the best view of the overhead sky as possible. Externally mounted antennas are recommended to improve system performance. Any visual indicators for remotely installed units must be mounted so that they can be easily viewed by the pilot.

B7.3.5.3 AFF communications must be always fully operational in all areas of operation. Contractors working in or accepting dispatches to the State of Alaska, Southern Canada, or Western Canada must have an AFF system capable of being always tracked in these locations. Not all manufacturers’ AFF equipment communication links will operate effectively in all geographic areas.

B7.3.5.4 The contractor must maintain a subscription service through the AFF aircraft hardware provider allowing AFF position reporting for satellite tracking via the Government AFF viewing software. The position-reporting interval must be every two minutes while the aircraft is in flight. The contractor must register their AFF aircraft hardware with the Government through https://www.aff.gov providing complete tail number; manufacturer and serial number of the AFF transceiver; aircraft make and model; and contractor contact information. If the contractor relocates previously registered AFF aircraft hardware into another aircraft, then the contractor must contact the government’s AFF Program making the appropriate changes prior to aircraft use. In all cases, the contractor must ensure that the correct aircraft information is indicated within AFF. The contractor must notify the Government of system changes, scheduled maintenance, and planned service outages.

B7.3.5.5 Registration contact information, a web accessible feedback form, and additional information is available at: https://www.aff.gov.

B7.3.5.6 Prior to the aircraft’s annual contract inspection, the contractor must ensure compliance with all AFF systems requirements. The contractor must additionally perform an operational check of the system. As a minimum, the operational check must consist of confirming the aircraft being tested is displayed in AFF.gov (indicating it is currently transmitting data to AFF.gov) and that all information displayed in AFF.gov is current.

A username and password are required to access AFF.gov. Log on to the AFF website at https://www.aff.gov to request a username and password.

B7.3.5.7 If AFF becomes inoperable/unreliable the aircraft may, at the discretion of the Government, remain available for service utilizing radio/voice system for flight following. The contractor will return the AFF system to full operational capability within 72 hours after the inoperative/unreliable unit is first discovered as defective.

B7.3.5.8 AFF Systems must comply with supplemental requirements contained in Specification Section Supplement document available at: https://www.aff.gov/support/Specification_Section_Supplement.pdf.

B7.3.6 Satellite Phone System.

B7.3.6.1 One Iridium-network based Satellite Telephone (Sat phone) system. The installation must be in accordance with 14 CFR 43.

B7.3.6.2 The sat phone handset, or remote dialer, must be mounted in a convenient location in the cockpit. The location must provide ready and unencumbered access to its controls by both front seat occupants.

B7.3.6.3 The sat phone system audio must be permanently interfaced to the aircraft audio system in the same manner as the aircraft radios, so that the pilot and observer/copilot can utilize the sat phone via their headsets. It is preferred that all occupants of the aircraft be able to converse over the sat phone through their headsets, though keypad access may be limited to the two front seat occupants.

B7.3.6.4 The sat phone system must provide the capability to pre-program at least six (6) telephone numbers that can be quickly selected by either front seat occupant while in flight.

https://www.aff.gov/ https://www.doi.gov/aviation/library/forms https://www.doi.gov/aviation/library/opm https://www.aff.gov/support/Specification_Section_Supplement.pdf

EU Helicopter Services, MORA, OLYM, NOCA

B7.3.6.5 A TSO C-129a L-band antenna, acceptable to the manufacturer of the Sat Phone system, must be installed on top of the fuselage, giving as much a view of the overhead hemisphere as possible.

B7.3.6.6 The Sat Phone system may be integrated into the Automated Flight Following system (see B7.3.5) using either the same Iridium communicator or a separate Iridium communicator. In the former case, it is acceptable for phone calls to interrupt the transmission of AFF position reports for brief periods of time, and flight crews must be instructed as to this conflictB7.4 Navigational Systems

B7.4.1 At least one of the following VFR navigations systems must be installed:

B7.4.1.1 One permanently installed, panel-mounted GPS system utilizing an approved, fixed external aircraft antenna. The navigational databases must be updated at least annually.

B7.4.1.2 One portable Aviation GPS unit (Garmin GPS 660 or 760 etc..) utilizing aviation-based software providing overhead orientation. Unit must be connected to remote antenna separate from GPS unit. Navigational databases must be updated at least annually.

B7.4.1.3 One tablet or mobile device, minimum size of 3.0 inches wide x 1.5 inches high, utilizing aviation application software (Foreflight, Gamin Pilot etc..) that incorporates overhead orientation and georeferencing of aircraft position on the map. The display must show aircraft position in relation to airspace boundaries, including military, controlled, and restricted areas. Application software must allow for disabling of internal GPS sourcing and allow for sourcing of external remote GPS antenna signal. Application software subscription must be current.

B7.4.2 All GPS systems must allow for continuous application of aircraft electrical power through circuit protected source.

B7.4.3 All GPS Systems must use WGS-84 datum and reference latitude and longitude coordinates in degrees, minutes, decimal minutes mode.

B7.4.4 All GPS Systems must ensure secure mounting and shall be able to provide the PIC a clear view of aircraft panel and the unit display and unrestricted access to aircraft and unit controls.

B7.4.5 Portable Aviation GPS units, GPS tablets, or mobile GPS device systems will not be used for aircraft primary navigation in aircraft conducting IFR operations.

B7.4.6 All GPS Systems must be able to display, in real time the GPS tracks of all flights. This data must be transferable to the Government upon request by the Government. All transferred data must include the date of each flight, along with a graphical overlay of the flight track on an aeronautical chart covering the area of operations.

B7.5 Audio Systems

B7.5.1 Two separate audio control systems (which may be combined in a single unit) for the pilot and observer/co-pilot to select receiver audio outputs and transmitter microphone/push to talk (PTT) audio inputs for all installed radios and public address (PA) systems. Each system must also allow the pilot and observer/copilot to independently adjust both the intercommunications system (ICS) and the receiver audio output levels.

B7.5.1.1 Transmitter selection and operation. Separate transmitter selection controls must be provided for both the pilot’s and observer/copilot’s microphone/PTT inputs. The system must be configured so the pilot and observer/copilot may each simultaneously select and utilize a different transmitter (or PA system when installed) via their respective microphone/PTT. Whenever a transmitter is selected, the companion receiver audio must automatically be selected for the corresponding earphone. Transmitter sidetone audio must be provided for the user as well as for cross-monitoring via the corresponding receiver selection switch on the other audio control

EU Helicopter Services, MORA, OLYM, NOCA system.

B7.5.1.1.1 The two aft cabin exit positions must be equipped to transmit on the radio(s). Whenever a radio (or PA, when so equipped) microphone input is selected at the observer/copilot's audio control panel, the aft cabin passengers' radio microphone inputs must automatically be connected to the same radio, and they must then be capable of transmitting on that radio via their respective radio transmit PTT switches.

B7.5.1.2 Receiver selection and operation. Separate controls must be provided for both pilot and observer/copilot to select audio from one or any combination of available receivers. The ICS-equipped aft passenger positions must monitor the receiver(s) as selected by the observer/copilot. The receiver audio output must be free of excessive distortion, hum, noise, and crosstalk, and must be amplified sufficiently to facilitate ease of use in a noisy cockpit/cabin environment.

B7.5.1.3 The audio system(s) controls must be located and arranged so that both the pilot and observer/copilot, when seated, have full movement of their respective controls without interference from their clothing, the cockpit structure, or the flight controls. Labeling and marking of controls must be clear, understandable, legible, and permanent. Electronic label maker marking is acceptable.

B7.5.2 An ICS for the pilot, observer/copilot, and all aft cabin positions. ICS audio must mix with, but not mute, selected receiver audio. An ICS audio level control must be provided for each position above. Adjustment of the ICS audio level at any position must not affect the level at any other position.