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COMMERCE BUSINESS DAILY ISSUE OF MAY 23,1996 PSA#1601Immigration & Naturalization Service, Procurement Division, 425 I
Street, N.W., Room 2208, Washington, DC 20536 15 -- BORDER PATROL HELICOPTERS POC John A.Russo Jr., Chief, General
Contracts INS, 202-305-4600. The Immigration and Naturalization
Service, Deparment of Justice (Border Patrol) plans to competitively
award a three year contract (base year plus two option years) for light
observation helicopters equipped with a gas turbine engine designed
specifically for the aircraft. The fixed price type contract will
include requirements for up to 15 helicopters per year deliverable
within 12 months of receipt of order/award, plus overhaul, overhaul
exchange or new procurement of main components, pilot transition
training and mechanics'factory maintenance training, warranties,
operating and maintenance manuals, illustrated parts catalogs and
provisions for updates of the same, weight and balance data, special
tools on as is needed basis, and technical field support. The
helicopter must: (1) be new and of current design and production, with
spare parts readily available; (2) contain all current and applicable
improvements with airworthiness directives, service bulletins and
service letters completed and incorporated as of the date of delivery;
(3) be FAA certified as a normal category helicopter, all accessories
installed to meet mission specifications to be FAA approved by a
Supplemental Type Certification (STC) or under a ''337'' Field
Approval; (4) meet the following minimum performance criteria: (a)
Normal patrol at 40-60 knots true airspeed/capable of accelerating to
130 knots true airspeed; (b) hover out of ground effect on a standard
day at maximum gross weight at a minimum of 6000 feet density altitude;
(c) have a reserve internal load capacity of a minimum additional 400
pounds with full fuel, oil, and accessories without exceeding the
certified gross weight of the aircraft; (d) have an endurance at normal
patrol speed and normal operational weight not less than 2.0 hours and
the ability to be equipped with an auxiliary fuel tank which will
increase minimum ocerall endurance to 4.0 hours at normal patrol speeds
or 3.5 hours minumum at pursuit speeds without exceeding standard
passenger, pilot and cargo enter of gravity limits both laterally and
fore and aft; and level fly over noise levels should not exceed 84
decibels, measured from 500 feet above the ground. Aircraft design
should permit min to max indiscriminate cabin loading without having to
move components or using any movable ballast to keep within certified
flight limitations. Consideration must be given to mission equipment
and crew profiles, i.e., 2 pilots with max fuel, 1 pilot with max fuel,
2 pilots with max fuel, FLIR and FLIR Operator, and 1 pilot with 3
passengers. The gas turbine engine shall permit instant starting
without the use of external power and, shall be capable of using JP-4.
JP-5, ASTM-1655, Type A, A1, and B fuels. A fuel filter kit to
eliminate the need for fuel additives when the ambient temperature is
below 40 degrees Fahrenheit, an engine wash kit, an automatic turbine
re-ignition system and an engine particle separator with mist
eliminator (if required) shall be installed. Normal seating for the
crew compartment shall consist of 2 pilot/co-pilot seats with no
configuration in the front for a third seating. The area betweenthe
pilot and the co-pilot shall be utilized for accessoriesand avionics
equipment. Dual controls will be provided. the rear passenger
compartment shall have a minimum of 2 seats. All seating positions
shall be provided with seat belts, with metal buckle design and
shoulder harnesses. A heat/defogger system and fresh air ventillation
shall be installed. An exterior keyed lock shall be provided for all
doors. Interested sources should reply to this announcement by mail by
COB 5 June 1996 to: Immigration and Naturalization Service, Department
of Justice, 425 I Street NW, Room 2208, Washington, D.C. 20536, Attn:
John A. Russo Jr. Replies may also be directed to Mr. Russo by
facsimile at (202) 514-3353. replies must be made by mail or facsimile
only. No telephone replies will be accepted. See numbered Note 22.
(0142) Loren Data Corp. http://www.ld.com (SYN# 0142 19960522\15-0001.SOL)
15 - Aircraft and Airframe Structural Components Index Page
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