schedule and SOW.docx
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- Attached to
- Fixed high wing monoplane Federal contract opportunity
- Solicitation number
- 12639522Q0203
About this file
This document includes a statement of work and schedule for a federal contract solicitation. The solicitation requires the delivery of two fixed wing aircraft by September 30, 2026 with options to purchase up to three additional aircraft through 2026. The aircraft must meet detailed technical specifications including a minimum 180 horsepower engine, constant speed propeller, maximum gross weight of 2,300 pounds, and specific avionics and instrument requirements. The period of performance is from award through five years. Quotes are due by July 13, 2022 and will be evaluated based on price, technical capability, past performance, and other factors. Award will be made to the responsible offeror providing the most advantageous solution to the Department of Agriculture Animal and Plant Health Inspection Service.
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Text version
CLINS CONTRACT PERIOD – Award through September 30, 2026
| No. Description | Quantity | Unit | Unit Price | Amount | ||
| 01. Aircraft | 2 | EA | $_______ | $_______ | ||
| 02. FY23 Optional aircraft | 1 | EA | $_______ | |||
| 03. FY24 Optional aircraft | 1 | EA | $_______ | |||
| 04. FY25 Optional aircraft | 1 | EA | $_______ |
Fixed Wing Aircraft, Factory New. Fixed wing airplane shall be of factory new manufacture to include specifications listed below:
· General Specifications, Aircraft Safety & Performance Needs
· Airplane is to be certified under FAA FAR Part 23.
· One-year entire airplane limited warranty.
· Airplane shall be ais to a high wing monoplane, two place tandem seating, tail wheel type.
· Engine: Lycoming, Minimum 180 hp (larger HP preferred).
· Propeller: Constant speed.
· Max Gross Weight: 2,300 lbs.
· Baggage area access door. Gravity feed fuel system. Landing lights.
· Navigation lights.
· Three-point strobe light system.
· 40-amp alternator minimum.
· Inertia reel shoulder harness, pilot and passenger. Extended skylight.
· Sight fuel gauges. Audible stall warning
· 406 MHz Emergency Locator.
· Left side swing out window with a maximum 22” opening that provides adequate angle for shooting.
· Adjustable front and rear seat. Dual flight controls with rear controls (stick throttle and prop) removable.
· Full floorboards. Rear seat cabin heat. Cabin fresh air vent. Map pocket.
· Vortex generators.
· Control stick covers both front and rear.
· 26-inch diameter tundra type tires.
· Short take-off and landing capability
· Stall speed with full flaps extended less than 50 mph at maximum gross weight
· Cruise speed minimum 125 mph (Faster mph preferred).
· Short take-off and landing capability.
· Avionics:
· Garmin G3X™ Touch with 10.6” display, Synthetic Vision, Front-loading SD™ card slot,
· Garmin GTR 20 VHF Comm, Garmin GTX 345R remote mode S transponder, Stereo Intercom, Video input capable of accepting input from a FLIR camera system and SiriusXM Weather/Audio ready
· Technisonic TDFM or equivalent FM radio to be installed in the instrument panel.
· Audio Panel with vox intercom, PTT option and remote volume for passenger.
· Push to talk for the passenger will be installed on the right floorboard for foot operation.
· Single plug and civilian two plug helmet jack installed in rear of right-side wing root panel for passenger and instrument panel for pilot.
· Stick grip installed on pilot control stick, three button switching minimum.
· Instruments:
· The following instruments are required if not incorporated in the Garmin G3X display.
· Altimeter
· Tachometer
· Compass
· Oil pressure
· Oil temperature
· Turn coordinator Airspeed indictor Volt/amp meter
· Cylinder head temp gauge
· Exhaust temp gauge.
· Hobbs meter
· Accessories:
· Automatic flagman installed on left gear.
· FLIR camera system with a minimum resolution of 640 installed on the left wing at the lift strut attach point of first aircraft delivered for test and evaluation purposes.
· Halon 1211,1301 fire extinguisher minimum 1.2 lbs. accessible to both pilot and passenger.
· Large pocket on the back of the pilot seat capable of holding shotgun shells.
· Brackets to secure a shotgun on the left side of passenger seat.
· Interior panel protection on left side and windowsill to protect against abrasion from shotgun.
· High visibility markings as follows:
· 1. Outer 4" of face rear side of one blade of propeller
· 2. Forward Leading edge of wing struts and jury strut on shooting side
· 3. High visibility markings should be of a color that shall be visible against the terrain over which the mission is flown. Change of background color during seasonal differences shall be considered. Tape may be used on leading edges of wing struts. Paint shall be used on the propeller.
52.217-5 Evaluation of Options.
As prescribed in 17.208(c), EVALUATION OF OPTIONS (JULY 1990) Except when it is determined in accordance with FAR 17.206(b) not to be in the Government’s best interests, the Government will evaluate offers for award purposes by adding the total price for all options to the total price for the basic requirement. Evaluation of options will not obligate the Government to exercise the option(s).
(End of provision)
52.217-6 Option for Increased Quantity. OPTION FOR INCREASED QUANTITY (MAR 1989) The Government may increase the quantity of supplies called for in the Schedule at the unit price specified. The Contracting Officer may exercise the option by written notice to the Contractor within [insert in the clause the period of time in which the Contracting Officer has to exercise the option]. Delivery of the added items shall continue at the same rate as the like items called for under the contract, unless the parties otherwise agree.
(End of clause)
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