Helicopters RFP Template



Instructions: This attachment contains the minimum specifications for the helicopter being purchased by NYSP. Bidders should enter their company name and proposed helicopter model in the spaces provided in the table below. Bidder’s Company Name: FORMTEXT ?????Bidder’s Proposed Helicopter Model: FORMTEXT ?????Bidders shall review each specification listed in the table below. For every item listed in the table, a Bidder shall enter a “Yes” in the column labeled Bidder Confirmation if they confirm that their proposed helicopter model meets or exceeds the listed specification. A Bidder shall enter a “No” in the column labeled Bidder Confirmation if their proposed helicopter model does not meet or exceed the listed specification. Bidders that enter a “No” in the Bidder Confirmation column for any item shall have their proposal deemed non-responsive by the State. In addition to its general right to seek clarification specified in the RFP, the State reserves the right to seek clarification from a Bidder after initial review of their Attachment 1 – Helicopter Specifications for any blank space in the Bidder Confirmation, Manufacturer Name and Manufacturer Model Number columns. If a Bidder responds to such a clarification request with a “No” a blank space in the Bidder Confirmation column or does not respond within three (3) business days from the State’s written request for clarification the Bid will be disqualified as non-responsive.For items where the Manufacturer Name column and the Manufacturer Model Number column are shaded grey in the table below, a Bidder shall enter the Manufacturer Name in the Manufacturer Name column and the Manufacturer Model Number in the Manufacturer Model Number column for the proposed item to be included in the proposed helicopter that meets or exceeds the listed specification. For items in the table below that specify an equivalent item is acceptable, the NYSP Aviation Unit shall be the sole determiner that the proposed item meets or exceeds the listed specification. The NYSP Aviation Unit may require a Bidder to provide additional documentation or information to assist in their determination of equivalency of proposed items.Bidders shall use the Inquiries process described in Section 1.9 – Inquiries and Designated Contacts of the RFP to address any questions or concerns around the specifications in this attachment. This includes any questions related to equivalency of items to the listed specification. Index#Helicopter SpecificationBidder Confirmation(Yes or No)Manufacturer NameManufacturer Model Number1Helicopter shall have a minimum useful load, which is defined as the weight of fuel, passengers, and cargo, of 4,000 pounds and have an interior capable of being changed to perform NYSP’s multiple mission profiles described in Section 1.3 New York State Police Overview of the RFP document. FORMDROPDOWN 2Helicopter shall be able to operate during the day, at night, and over all parts of the State, including its waterways and be equipped with dual flight controls. FORMDROPDOWN 3Helicopter shall be capable of flying a minimum of five hundred (500) hours per year. FORMDROPDOWN 4Systems and component quantities listed shall be installed in helicopter as specified herein and shall meet or exceed FAA certification requirements upon delivery to NYSP. In addition, all installed equipment on subsequent helicopters shall be the same as the equipment installed on the first helicopter, or achieve a standard of "commonality" as approved by the NYSP. FORMDROPDOWN 5Helicopter shall be zero time, no previous owner, factory new, twin turbine-engine powered, the latest improved model in current production, as offered to commercial trade. FORMDROPDOWN 6Helicopter shall be Category A certified according to 14 CFR Part 29, Airworthiness Standards: Transport Category Rotorcraft, with performance determined and scheduled so that if one engine fails at any time after the start of take-off, or in the approach to landing sequence (surface and elevated heliport), the helicopter can return to, and stop safely on the take-off area; or continue the take-off and climb-out, and attain a configuration and airspeed for single engine fly away performance in compliance with Sec. 29.67(a)(2), Climb: One Engine Inoperative; and, the landing performance determined and scheduled so that if one engine fails at any point in the approach path, the helicopter can either land safely or climb out and attain a configuration and speed allowing compliance with the climb requirement of Sec. 29.67(a)(2), Climb: One Engine Inoperative. FORMDROPDOWN 7Helicopter shall be Instrument Flight Rules (IFR) certified. FORMDROPDOWN 8Helicopter shall be Night Vision Imaging System (NVIS) certified. FORMDROPDOWN 9Helicopter shall accommodate at least two (2) pilot flight crew, a two (2) person medical crew, up to two (2) litter-borne patients, and all required Advanced Life Support equipment for patient treatment and resuscitation specified in Items 98 through 111 below. FORMDROPDOWN 10Helicopter shall be equipped with dual flight controls. FORMDROPDOWN 11Helicopter shall be equipped with wheeled landing gear and all required test panels, advisory and warning annunciators. FORMDROPDOWN 12Wheel gear shall be retractable including wheel doors. FORMDROPDOWN 13Landing gear shall be of the highest certificated type available by the manufacturer. FORMDROPDOWN 14Main rotor blades shall be painted with a high visibility paint scheme. FORMDROPDOWN 15Wire Strike Protection System or equivalent shall be installed on the helicopter. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????16Windshields shall be laminated glass-type, tinted, heated, high integrity, and bird-resistant. All cabin windows shall be tinted. FORMDROPDOWN 17Helicopter shall have a windshield bleed-air defogging system. FORMDROPDOWN 18Helicopter shall have a ram-air ventilation system. FORMDROPDOWN 19Helicopter shall have an Environmental Control System (ECS) including ducting to provide adequate cooling/heating distribution throughout cockpit and cabin. Heating system shall be a bleed-air type with a cockpit mounted temperature control panel and cabin Inside Air Temperature (IAT) display. FORMDROPDOWN 20Helicopter shall have nose and tail-cone easy access electronics compartments. FORMDROPDOWN 21Helicopter shall have easy access hydraulic system servicing quick disconnects. FORMDROPDOWN 22Helicopter shall have system inspection and service access panels. FORMDROPDOWN 23Helicopter shall have left and right cabin sliding door systems with left and right side rope guide. FORMDROPDOWN 24Helicopter shall have fast rope insertion/extraction system with arm extension/retraction capability and equal left and right side lateral extension. System shall be capable of being extended or retracted without the use of tools. In addition, system shall be rated for six hundred (600) pounds minimum weight. FORMDROPDOWN 25Latching mechanisms shall be installed to hold the sliding doors in the open position during loading/unloading, as well as on those occasions requiring doors to be open in flight. Latching mechanisms shall be clearly marked. Operating instructions and emergency egress directions shall be clearly displayed. Latch release and door closing shall be accessible from inside the cabin. FORMDROPDOWN 26Helicopter shall have door position advisory system for all doors. FORMDROPDOWN 27Helicopter shall have common keys for all helicopter door lock mechanisms including baggage door(s). Keys for all helicopter door lock mechanisms, including baggage door(s), for additional helicopters ordered under the contract shall have matching common keys to the first helicopter purchased by the New York State Police. FORMDROPDOWN 28Helicopter shall have hinged fuel filler cap(s). FORMDROPDOWN 29Helicopter shall have manually operated rotor brake with system pressure indicator and advisory light. FORMDROPDOWN 30Helicopter shall have Rotor Analysis Diagnostic System (RADS) provisions installed. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????31Helicopter shall have Health and Usage Monitoring System (HUMS) provisions and removable components installed. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????32Helicopter shall have cockpit stowage provisions for the flight manual, credit card holder, charts, and portable equipment (IPAD2 Size). FORMDROPDOWN 33Helicopter shall have cockpit mounted hour-meter, for tracking flight time, activated by a weight-on-wheels switch. Location of cockpit mounted hour-meter to be determined at time of design review. FORMDROPDOWN 34Helicopter shall have low-profile instrument panel with a glare shield. FORMDROPDOWN 35Helicopter shall have additional corrosion prevention coating of Zinc Chromate, Corrosion “X”, ACF 50 or equivalent. This requirement is necessitated by flight operations that will be conducted in and near salt-laden environments. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????36Engines shall be of new manufacture with performance capability to satisfy requirements of Item 5 above, and equipped with electronic controls, diagnostic systems, and engine wash kit. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????37Helicopter shall have fire detection and suppression systems. Protection from snow and foreign object damage shall be installed. Intake filters shall be “cleanable”. Inlet Barrier Filter preferred. FORMDROPDOWN 38Cockpit engine and gearbox indicating systems shall be an integrated display system. FORMDROPDOWN 39Avionics and electrical systems shall be installed and approved either as part of the helicopter’s original type certification, under supplemental type certificate, or installed meeting or exceeding FAA requirements and approved on FAA Form 337. All equipment shall have NVIS integrated lighting. FORMDROPDOWN 40Avionics and electrical bays shall be placarded to indicate equipment installed. FORMDROPDOWN 41Instrumentation and avionics shall be front-mounted in the instrument panel and center console with sufficient extra wiring to allow easy removal. FORMDROPDOWN 42Helicopter shall be equipped with a heavy duty battery, Ni-Cad, or preferred sealed Lead Acid, with voltage and amperage according to the certification requirements in this table, to power battery bus items, provide unassisted engine starting, and provide emergency power to essential systems in the event of primary DC power failure. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????43Dual starter/generators shall supply required DC electrical power, with each generator supplying power to its respective primary bus. FORMDROPDOWN 44Generators shall have the capacity to power the DC electrical system in the event of a single generator failure with the understanding that some non-essential systems shall require shedding for single generator operation. System shall include a DC generator control unit and fault detection circuitry. FORMDROPDOWN 45115 Volt/400Hz and 26 Volt/400 Hz AC power shall be provided by dual static inverters, or, one static inverter and one 10 KVA generator. System shall include monitoring and fault detection systems. FORMDROPDOWN 46Helicopter shall have DC external power receptacle with “APU door open” advisory on caution panel. FORMDROPDOWN 47Helicopter shall have fixed landing lights with switching interface to allow either normal or Pulselite use as per Item 50 below. FORMDROPDOWN 48Helicopter shall have Whelen LED position and anti-collision lighting, or equivalent. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????49Helicopter shall have Whelen LED recognition lighting, or equivalent, consisting of two forward facing, nose mounted lights integrated with Pulselite system as per Item 50 below. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????50Helicopter shall have Pulselite lighting system. System shall pulse both recognition and landing lights with the ability to select the Pulselite system either on or off by cockpit mounted switch so that the recognition and landing lights can function normally. FORMDROPDOWN 51Helicopter shall have Battery operated emergency egress lighting, with a minimum of twenty (20) minute battery life. FORMDROPDOWN 52Helicopter shall have low mounted external passenger/litter loading lights with cabin and cockpit activation capability. Lights shall be automatically deactivated by weight-on-wheel or collective mounted switch with a “Load Lt On” annunciator capsule mounted in the instrument panel. FORMDROPDOWN 53Helicopter shall have at least two (2) Wemac type cockpit ceiling mounted map lights with dimming capability, one for pilot use and one for co-pilot use. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????54Helicopter shall have non-skid, non-absorbent, cockpit and cabin floor covering sealed to protect helicopters substructure and prevent contamination from corrosive fluids. Where possible, a sealed, blood dam type flooring shall be installed. Cabin floor shall have flush mounted attachment fittings (no recessed mounts allowed) and tracking to accommodate the installation and removal of seats and medical litter systems as per mission requirements. Floor structure inspection panels shall be installed. FORMDROPDOWN 55The specified cockpit and cabin flooring shall be capable of being removed (not sealed to helicopter floor panels) to facilitate maintenance requirements. FORMDROPDOWN 56Helicopter shall have minimum four point restraint system for all cockpit and cabin seats. Access to all seat belts and shoulder harness mechanisms hidden by any structure will be by screw-mounted access panels. Five point restraint preferred; if available. FORMDROPDOWN 57Helicopter shall have Voice and Data Recorder (Black box) installed. FORMDROPDOWN 58Cockpit shall be of paperless design to eliminate the need to have paper charts and maps in the cockpit. An example would be Universal’s UCDs or Garmin’s GMX 200 that require subscriptions from Jeppesen. These displays usually take the place of the chart holders. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????59Helicopter shall have Engine and Airframe Log Books at time of delivery. FORMDROPDOWN 60Helicopter shall have Weight and Balance Data Sheet with equipment list for helicopter at delivery. FORMDROPDOWN 61All exterior parts of the airframe shall be covered with high quality polyurethane Imron or equivalent paint, including the inside of all component cowlings and panels. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????62Helicopter shall have am electric rescue hoist with a six hundred (600) pound capacity, including operator hand controls, grab bar switches, motor/cable, monitoring, emergency release mechanism, and operator restraint system. System power-up and master control shall be from cockpit. The hoist shall be removable with quick disconnect-type fittings and capable of at least 250 feet and 150 feet/min rate. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????63Helicopter shall have a remote camera installed on the hoist mechanism or fuselage so that hoist operations can be displayed on the MFDs (Multi-Function Displays) and/or down linked. FORMDROPDOWN 64Helicopter shall have at least three (3) portable fire extinguishers, one at each pilot station and one in the cabin. FORMDROPDOWN 65Helicopter shall have Removable External Cargo Hook system with cockpit weight on hook indicator, control panel, and emergency controls for both pilots. FORMDROPDOWN 66Helicopter shall have controllable aircraft spotlight with auto-stow (used to assist with aircraft landing ops). Activation switch shall be collective control mounted. System shall have a “light on” advisory. FORMDROPDOWN 67Helicopter shall have at least four (4) NVIS compliant flashlights, two mounted in cockpit and two mounted in cabin. Locations to be determined at time of design review. FORMDROPDOWN 68Helicopter shall have fully night vision integrated cockpit and cabin including all instrumentation, lighting, and displays. FORMDROPDOWN 69Helicopter shall have Digital Automatic Flight Control System with integrated digital autopilot/flight director computers, flight director mode selectors, autopilot controller, air data sensors, and servos. System shall be capable of full autopilot controlled cruise, approach, go-around, level-off, hover, and departure. FORMDROPDOWN 70Helicopter shall have at least four Flat Panel Liquid Crystal Display (LCD) Electronic Flight Instrumentation System incorporating two (2) separate and independent Directional Gyro (DG)/Vertical Gyro (VG) systems. System shall indicate airspeed, vertical speed, and altitude. FORMDROPDOWN 71Helicopter shall have two (2) Universal (latest Search and Rescue (SAR) version), or equivalent, Flight Management Systems (FMS). SAR automatic control and Wide Area Augmentation System (WAAS) capabilities preferred. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????72Helicopter shall have one (1) SAR Weather Radar System coupled to meet the requirements specified in Item 75 below. FORMDROPDOWN 73Helicopter shall have one (1) Integrated Traffic Alert and Collision Advisory System (TCAS) coupled to meet the requirements specified in Item 74 below. TCAS II preferred. FORMDROPDOWN 74Helicopter shall have one (1) Digital Moving Map System coupled to meet the requirements specified in Item 75 below. FORMDROPDOWN 75Helicopter shall have two (2) MFDs (One (1) MFD is acceptable, provided stand-by instruments are capable of providing full time display of heading, altitude and attitude to the Pilots In Command) integrated with weather radar, navigation data, TCAS, hoist camera, moving map system, satellite weather, thermal imaging systems, and include the capability to display Doppler hover and search pattern data. FORMDROPDOWN 76Helicopter shall have real time satellite flight following and satellite communication which shall interface through the helicopter. Two-way text messaging or email with pre-programmed and user-programmable capability. FORMDROPDOWN 77Helicopter shall have one (1) Davtron Density Altitude Indicator M-655-1 or equivalent. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????78Helicopter shall have two (2) Davtron M877 digital clocks, or equivalent, mounted in instrument panel. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????79Helicopter shall have one (1) battery temperature indicating system or equivalent, unless a sealed lead acid battery is used. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????80Helicopter shall have one (1) 406 MHz Emergency Locator Transmitter coupled to GPS for position information. Automatically Deployable Emergency Locator Transmitter (ADELT) preferred. FORMDROPDOWN 81Helicopter shall have one set of “stand alone” pressure instruments to include (1) standby horizon/navigation indicator with self power, (1) pressure altimeter, and (1) vertical speed indicator (VSI). FORMDROPDOWN 82Helicopter shall have Wulfsberg/Cobham Flexcomm radio system, or equivalent (may include one or two radios). System shall interface with State Police up to 900 megahertz radio system and be capable of communicating with all bandwidths used throughout the State. There shall be a control head in the cockpit and a control head in the cabin. Shall be P25 digitally-compliant and trunk capable. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????83Helicopter shall have an integrated radio system including, but not limited to: two (2) VHF Communications radios, two (2) Navigation radios, two (2) Mode S Transponders, one (1) Automatic Direction Finder (ADF) radio, and two (2) DME radios and indicators. FORMDROPDOWN 84Helicopter shall have six (6) audio panels with sufficient switching to control all installed radio and Internal Communications Systems (ICS) functions. Two (2) panels shall be located in the cockpit and the remaining four (4) in the cabin. Locations of audio panels to be determined at time of design review. FORMDROPDOWN 85Helicopter shall have eight (8) headset jacks flush mounted at locations to be determined at time of design review, based on make and model of helicopter offered with some being “ICS only” positions and one being an external jack. In addition, four (4) coil-cord type headset extensions with both ICS and transmit capability shall be furnished. Length of cords shall be determined by cabin movement ability. FORMDROPDOWN 86Helicopter shall have two (2) Radar Altimeters, one (1) at each pilot and co-pilot station or one (1) radar Altimeter which displays on both pilot and co-pilot stations. FORMDROPDOWN 87Helicopter shall have pilot and co-pilot ICS/transmit foot switches installed at appropriate angle to allow for toe operation. FORMDROPDOWN 88Helicopter shall have voice-activated cockpit and cabin ICS system with cockpit call and crew call indicators. A cockpit mounted on/off switch shall be installed that will isolate the cabin ICS system from the cockpit. Switch location to be determined at time of design review. FORMDROPDOWN 89Helicopter shall have all antennas, connectors, adapters, annunciators, and mounting systems specific to all radio components. Antenna layout shall require NYSP Aviation Unit consultation prior to mounting. FORMDROPDOWN 90Helicopter shall have one (1) Radio Master Switch to control all on/off radio functions. FORMDROPDOWN 91Helicopter shall have one (1) Removable and Controllable Searchlight of at least 30 million candle power which are IR and white light-capable (or equivalent searchlight of latest version). A “Searchlight On” advisory capsule shall be mounted on the instrument panel. Searchlight shall be slaved to system in Item 92 below. A single pendant control shall be available to the pilot, the co-pilot, or cabin crew with storage provisions. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????92Helicopter shall have one (1) triple sensor (CCD-TV, Night Vision, and Infrared detector) imaging system with integrated auto-tracking slaved to searchlight. System shall be coupled to MFDs. FORMDROPDOWN 93The video/IR hand controller shall be a quick-disconnect type with storage for controller located on co-pilot side of cockpit and shall have integrated NVIS lighting. Use from cockpit or cabin is required. Location of storage for controller to be determined at time of design review. FORMDROPDOWN 94An additional MFD shall be installed in the cabin so that it affords passengers the maximum viewing and be capable of displaying the information described in Item 75 above. FORMDROPDOWN 95Helicopter shall have HD color capable, IR compatible digital recording system and downlink transmission system with a portable downlink briefcase, antenna, and charger on a frequency compatible with current NYSP Aviation Unit broadcast equipment. (1.99-2.5Ghz, 4.4 -5.06Ghz and 6.425 -6.525Ghz.) FORMDROPDOWN 96Helicopter shall have one (1) XM Satellite Weather Information system, or equivalent, interfaced with MFDs as per Item 75 above. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????97The patient compartment/cabin area shall be isolated from the cockpit. FORMDROPDOWN 98All medical equipment storage, AC-DC power, medical suction systems, oxygen delivery systems and supplemental high intensity medical lighting shall be provided in a modular configuration, where possible, allowing efficient installation and removal in converting the helicopter to the airborne law enforcement / search and rescue configurations. FORMDROPDOWN 99Medical oxygen and power system busing, circuit breakers, and switching shall be controlled from the cockpit. FORMDROPDOWN 100Emergency shut off for the system shall be provided. The helicopter’s medical oxygen system shall interconnect with the modular system. FORMDROPDOWN 101Oxygen and power system “on” annunciators shall be displayed in the cockpit. FORMDROPDOWN 102Helicopter shall have separate static inverter for AC medical power system. FORMDROPDOWN 103An easily removable, palletized, medical electronics shelf, if required to accommodate electrical components, shall be fabricated in the event any standard electronics are located in the vicinity of the shelf where easy access to these components shall be impeded by the shelf’s location. FORMDROPDOWN 104System outlets and controls shall be color-coded: green for oxygen, white for suction, and black for electrical systems. FORMDROPDOWN 105Helicopter shall have at least two (2) 115 VAC dual outlets in cabin. Locations to be determined at time of design review. FORMDROPDOWN 106Helicopter shall have at least two (2) 28 V DC (7.5 amp max) multi-purpose outlets in cabin. Locations to be determined at time of design review. FORMDROPDOWN 107Helicopter shall have Medical Suction System: dual regulated pumps to provide continuous or intermittent suction in a range from 0 - 400 mm Hg, two suction regulation systems, two 1000 ml suction canisters with disposable inserts, and dual controls. FORMDROPDOWN 108Helicopter shall have dual adjustable oxygen flow meters (25 liters/min max flow each) with quick connect outlets (50 PSI). FORMDROPDOWN 109Oxygen shall be delivered from the primary system with a quantity indicating system installed in the cabin. FORMDROPDOWN 110At least one portable “Jumbo D” backup oxygen bottle shall be located and readily accessible in the cabin. Storage for two (2) additional "Jumbo D" oxygen bottles shall be located in the baggage compartment. All locations subject to approval at time of design review. FORMDROPDOWN 111Helicopter shall have a modular storage system for IV warmer, storage of Life-Pac, or equivalent equipment, portable suction kit, as well as other required electrical devices, resuscitation equipment, medical accessories and dressings. FORMDROPDOWN 112Helicopter shall have sufficient quantity or clusters of directionally controllable, high intensity, Wemac-style lights, to provide total patient and cabin illumination. Master light switch shall be cabin controlled with dimming capability. All cabin lighting shall be NVIS certified. Location of master light switch to be determined at the time of design review. FORMDROPDOWN FORMTEXT ????? FORMTEXT ?????113The cabin and cabin door area shall be equipped with momentary entry lighting that shall illuminate the cabin interior and exterior during patient loading or unloading. There shall be switches located by both cabin doors and an additional switch located on the cockpit capable of activating the lighting system. FORMDROPDOWN 114Modular patient litter loading systems shall be installed to permit the efficient, unobstructed, loading/unloading, and stable transport of up to two (2) litter-borne patients. Litter arrangement shall permit total body access by medical crew. Litter systems shall be removable to convert the helicopter to the airborne law enforcement/search and rescue/executive configuration. Litter locations shall not interfere with sliding door emergency egress controls. FORMDROPDOWN 115Helicopter shall have provision for second litter storage in baggage compartment. FORMDROPDOWN 116Helicopter shall have movable overhead IV hooks attached to rail systems that run parallel to litters, four (4) hooks per side. FORMDROPDOWN 117Helicopter shall have cabin medical seating arrangement with at least two attendant seats in single patient transport configuration. FORMDROPDOWN 118Helicopter shall have modular high density, utilitarian cabin seating for airborne law enforcement/tactical team transport/search and rescue with all belting, backrests and headrests, allowing for rapid re-configuration to achieve diverse mission sets. FORMDROPDOWN 119Helicopter shall have modular cabin seating for executive transports and executive interior which can be easily removed or installed to allow for transition to utility mission set. FORMDROPDOWN 120Helicopter shall have Gaseous Medical Oxygen system including all mounting, plumbing, removable canisters, activation controls, emergency shutoff, annunciators, quantity display, and monitoring system. System shall be installed with easy access to remove the canister for refilling outside the helicopters. An overboard bleed off vent shall be provided. Quantity indicator shall be wired so that the oxygen quantity can be checked with helicopter main battery on or off. FORMDROPDOWN 121Helicopter shall have color scheme that is consistent with current NYSP fleet design for planning purposes. Final exterior paint scheme shall be determined at the time of design review and shall consist of three different colors. NYSP seal to be painted on by Contractor. No decals. FORMDROPDOWN 122FAA registration numbers for helicopters shall be selected from NYSP Aviation Unit’s reserved lot. FORMDROPDOWN 123Helicopter shall have one (1) Flight Manual plus ten (10) year revision service, delivered with helicopter. Additional electronic copy is preferable. FORMDROPDOWN 124Helicopter shall have four (4) Engine operating and maintenance manuals plus ten (10) year revision service, delivered two months prior to helicopter delivery. Additional electronic copy is preferable. FORMDROPDOWN 125Helicopter shall have four (4) Engine and Airframe Illustrated Parts Breakdown Manuals plus ten (10) year revision service, delivered two months prior to helicopter delivery. Additional electronic copy is preferable. FORMDROPDOWN 126Helicopter shall have four (4) Airframe Maintenance Manuals plus ten (10) year revision service, delivered two months prior to helicopter delivery. Additional electronic copy is preferable. FORMDROPDOWN 127Helicopter shall have four (4) Wiring diagrams for all electrical systems delivered with helicopter. Diagrams shall be the latest revision. Additional electronic copy is preferable. FORMDROPDOWN 128Helicopter shall have four (4) Wiring Diagrams for all avionics installations delivered with helicopter. Diagrams shall be the latest revision. Additional electronic copy is preferable. FORMDROPDOWN 129Helicopter shall have operating and maintenance manuals for all installed avionics and special purpose equipment for helicopter plus 10 year revision service, delivered two months prior to helicopter delivery. Additional electronic copy is preferable. FORMDROPDOWN 130Helicopter shall have four (4) sets of detailed drawings for helicopter delivered with helicopter. FORMDROPDOWN 131Helicopter shall have exhaust covers. FORMDROPDOWN 132Helicopter shall have air inlet covers. FORMDROPDOWN 133Helicopter shall have pitot covers. FORMDROPDOWN 134Helicopter shall have cargo tie-downs appropriate to the proposed model of helicopter. FORMDROPDOWN 135Helicopter shall have main rotor tie-down appropriate to the proposed model of helicopter. FORMDROPDOWN 136Helicopter shall have specialized Tow-Bar for helicopter, if applicable. FORMDROPDOWN 137Helicopter shall have one (1) set of manual hoist cable cutters. FORMDROPDOWN 138Helicopter shall have two (2) sets of computer diagnostic system software with manuals. FORMDROPDOWN ................
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