STATEMENT OF COMPLIANCE TO TECHNICAL SPECIFICATIONS
The bidder must state in the last column opposite each parameter and required specifications either “Comply” or “Not Comply”. All pages shall be properly signed. Bidders must state here either “Comply” or “Not Comply” against each of the individual parameters of each Specification stating the corresponding performance parameter of the equipment offered. Statements of “Comply” or “Not Comply” must be supported by evidence in a Bidders Bid and cross- referenced to that evidence. Evidence shall be in the form of manufacturer’s un- amended sales literature, unconditional statements of specification and compliance issued by the manufacturer, samples, independent test data etc., as appropriate. A statement that is not supported by evidence or is subsequently found to be contradicted by the evidence presented will render the Bid under evaluation liable for rejection. A statement either in the Bidders statement of compliance or the supporting evidence that is found to be false either during Bid evaluation, post-qualification or the execution of the Contract may be regarded as fraudulent and render the Bidder or supplier liable for prosecution subject to the provisions of ITB Clause above goods manufactured by us
Technical Specifications
1. BASELINE REQUIREMENT
Item Specifications Comply/Not
Comply
1. CAS Aircraft Six (6) units
- Brand New
- “Brand New means condition of an
item wherein it is conspicuously new, unused and fresh from the manufacturer. (Air Force Dictionary, First Edition, 2003)”
- Factory New
“Factory New (FN) are material supplies which have been manufactured within the last two years, have been properly preserved and have traceability to the original manufacturer as accompanied by a certificate of “Original Equipment Manufacturer” (OEM), showing proof of the date of manufacture and assures that material submitted have been inspected by duly qualified inspection facility and test results may be requested for review. (Air Force Dictionary, First Edition, 2003)”
- Fully aerobatic
- Retractable Landing Gears
- Inadvertent Instrument
Meteorological Condition(IIMC)
Capable
- Instrument Flight Rules (IFR) Capable
a) Cruising Speed - Minimum two hundred twenty
(220) knots indicated airspeed (KIAS).
Item Specifications Comply/Not Comply
b) Endurance - Minimum of two hours and thirty
minutes (2+30) at armed
configuration and normal cruising speed; (w/o auxiliary tanks).
c) Seating Configuration - Dual Tandem seating
d) Payload - Min Payload: three thousand
(3,000) lbs;
- At least five (5) hard points,
- With at least six hundred (600) lbs capacity in each of the hard points
e) Service ceiling - At least twenty five thousand
(25,000) feet f) Short Take-off and
Landing (STOL)
- Maximum of three thousand
(3,000) meters/ nine thousand eight hundred forty two (9,842) feet take-off and landing roll at Maximum Gross Take-off Weight (MTOW)
2. Power Plant System - Brand New Turbine Engine(s)
- Time Between Overhauls (TBO) of at least three thousand (3,000) flight hours
- Operating limits suitable for
tropical country operation
(operates effectively in hot, humid & high altitude environments) - Re-start ability within fifteen (15)
minutes after shutdown 3.Weapons/Armament
System
- Capable for Day & Night Fighting
- Capable of airmunition mix
loading
- With two (2) .50 Cal guns (pods or built-in)
4. Avionics System - Compatible or better with current data bus MIL-STD 1553*
* A military standard published by the United States Department of Defense that defines the mechanical, electrical, and functional characteristics of a serial data bus. It was originally designed for use with military avionics, but has also become commonly used in spacecraft on-board data handling (OBDH) subsystems, both military and civil. It features a dual redundant balanced line physical layer, a (differential) network interface, time division multiplexing, half-duplex command/response protocol, and up to 31 remote terminals (devices).Military aircrafts utilize MIL-STD-1553 data buses, which allow complex electronic subsystems to interact with each other and the on-board flight computer. This is the military data bus of the aircraft. The data bus products function as the interface between the sub- system electronics and the 1553 data bus.
Item Specifications Comply/Not Comply a. Flight Instruments: - Equipped for Day Visual Flight
Rules (DVFR), Night Visual Flight Rules (NVFR) and Instrument Flight Rules (IFR)
(1) Flight Instruments - Electronic Flight Instruments (EFI) for altitude, attitude, airspeed and bearing (front and rear cockpit) - Must be brand new and calibrated
and can sustain high G forces (-3 to +7 Gs)
(2) Head Up Display (HUD)
- With integrated flight performance, navigation, and weapons targeting and delivery on the pilot’s Field of View (FOV) in day and night environments
(3) Multi-Function Display (MFD)
- Minimum of two (2) installed displays measuring at least 5x7 inches showing the aircraft flight performance, navigation, targeting
and tactical mission system
display (front and rear cockpit) (4) Hands-On Throttle
And Stick (HOTAS)
- Full Hands-On Throttle And Stick technology (both front and rear cockpit)
b. Navigation Equipment: - Basic for IFR flights
- Must be brand new and calibrated and can sustain high G forces (-3 to +7 Gs) (1) Global Positioning System/Inertial Navigation System (GPS/INS) - Linear/Angular Acceleration,
Velocity, Position, Attitude,
Magnetic and True Heading,
Altitude, Time Tag and Steering Data
(2) Digital Moving Map (DMM)
- Compatible with Night Vision Goggles (NVG) and has scaled maps of Asia Pacific Region
Item Specifications Comply/Not Comply (4) IFF Transponder - At least one (1) unit
- Identification information is provided in modes 1, 2, 3/A, C, 4 and S
(5) TACAN - Bearing and Range determination
c. Communication Equipment:
- Compatible/interoperable with the
existing AFP communications
equipment in plain and/or secure mode
(1) Multi Band - 2.000 to 300 MHz, capable of twenty (20) pre-set channels
(2) VHF-FM: - 30.00 to 75.95 MHz
(3) VHF-AM - 108.000 to 137.00 MHz
(4) UHF - 300 MHz to 3 GHz
5. Aircraft Lighting System
- NVG Compatible Interior & Exterior Lightings
- Dual mode (standard lightings and NVG flight mode)
6. Fire Control System - Compatible or better with current data bus MIL-STD 1553
- Capable of Air to Air & Air to Ground modes
- Equipped with EO/IR capable of Forward Looking Infra Red (FLIR), Imaging, and targeting System
(with Laser designator and
rangefinder), NVG compatible,
interfaced with the aircraft’s weapon system. EO/IR must have but not limited to the following:
Lightweight high stiffness composite body
With four axis active stabilization FOV of at least 26° to 0.35°
Thermal imager with wavelength of at least 3-5µm response
Daylight color camera with at least 26x zoom (FOV matched to IR)
Item Specifications Comply/Not Comply magnification ratio of at least 96x
With at least but not limited to the following options: Laser Spot Tracker, Navigation/Radar Interfaces, Displays & Recorders, Moving Map Systems, Digital Video Output
With laser options compatible with existing PAF munitions
7. Airframe - Certified crashworthy
- Corrosion resistant
- Should be rated for a minimum of twelve thousand (12,000) flight hours
- Must conform to military
specification (Low Tone Low
Visibility Gray Camouflage)
- With full organizational and technical signage
8. Survivability Features - Safety features of the aircraft for increased aircrew survival
a. EGRESS
- “Zero-Zero” ejection seat - Life Raft per seat
- Survival Kit per seat - First Aid Kit per seat
- Emergency Locator Transmitter Device per seat (covering 121.5 MHz and SARSAT range of 406 MHz)
b. Armor Plating
- Front and rear cockpit with armor plating in vulnerable sections of the cockpit and ballistic tolerance up to 7.62mm ammunition
c. Fuel Cell
- Self-sealing tank with certified ballistic tolerance of at least 7.62mm ammunition
d. External Stores - Jettisonable e. Radar Warning
Item Specifications Comply/Not Comply f. Missile Alert Warning
System (MAWS)
- Equipped
g. Chaff and Flare - Equipped
9. Environmental System
- Equipped with On-Board Oxygen Generation Systems (OBOGS)
- Cockpit Temperature
Control/Equipment Cooling - Anti-G system
2. INTEGRATED LOGISTICAL SUPPORT (ILS) REQUIREMENT
Item Specifications Not Comply Comply/
1. Training Program - It must cover the operational, maintenance, and mission support training requirements
- Supplier shall address all training and training support elements to
operators and maintenance
personnel involved in the operation of the aircraft
- Training shall be conducted in English
- Supplier shall pay the cost of training and its incidentals such as airfares,
board and lodging, local
transportation, subsistence
allowances, and insurances of
trainees for all training programs
connected with the aircraft
acquisition
- A separate and similar training aircraft shall be provided by the supplier. Hence, aircraft to be delivered shall not be used by the supplier for the training of pilots - Operational training (pilots and
maintenance) must be completed within thirty (30) days prior to the
Item Specifications Not Comply Comply/ delivery of the CAS aircraft at the
manufacturer’s training facility. It will at least include:
a. Pilot Training - Pilots shall undergo Functional Test Flight, Instructor and Operational Pilot Training in accordance at the manufacturer’s facility. All pilots shall also undergo simulator and actual training and performance planning on a day and night weapons delivery. In addition, all pilots shall also undergo actual NVG training. Position Nr of Pers 1. Functional Test Pilots 2 2. Instructor Pilots 4 3. Operational Pilots 2 b. Maintenance/ Specialist Personnel Training
- Maintenance officers shall undergo maintenance supervisor training and maintenance personnel shall undergo training on the two levels of
maintenance, namely;
Organizational Level Maintenance (OLM), and Field Level Maintenance (FLM) of following aircraft systems:
Position Nr of Pers Maintenance Officer 2 1. Engine System 2 2. Electrical System 2 3. Instruments System 2 4. Avionics system 2 5. Communications System 2
6. Air Plane General
(APG) 2 7. Pneudraulic / Hydraulic System 2 8. EGRESS 2 9. Environmental System 2 10. Airframe System 2
Item Specifications Not Comply Comply/ 11. Weapons System 2
And other aircraft related systems not mentioned above
2 each sys
2. Ground Support Equipment (GSE)
- The GSE must provide for servicing, handling, and maintenance of the aircraft in both Organizational and Field Levels.
- Two (2) sets, one (1) for main operating base and one (1) for forward deployment station, these equipment include but are not limited to the following:
a. Starting unit b. Towing Bar c. Aircraft Jacks d. Engine stands e. Hydraulic Cart f. Battery Charger g. Aux Tank Carrier h. Oxygen Servicing Unit i. Windshield/Canopy Rigger j. Flight Controls Template k. Tire Changer
l. Other AGE and accessories necessary for the maintenance and operation of the aircraft like aircraft cover, propeller blade cover, mooring, grounding wire, among others
- Tools, diagnostic and/or test
equipment, aerospace ground
equipment (one set each): a. Field Maintenance Tools b. Special Tools
c. Test Diagnostic Equipment d. Armament System maintenance
and repair tools
e. Armament Harmonization Kit
3. Technical Manuals Two (2) original copies and two (2) electronic copies of the following
Item Specifications Not Comply Comply/ checklist – twelve (12) copies, original
and electronic and Flight manual – six (6) copies, original and electronic must be provided:
Flight Manual Pilot checklist
Master Minimum Equipment List Aircraft Weight and Balance Manual Wiring Diagram Manual
Aircraft Maintenance Instruction Manual
Illustrated Parts Catalog Power Plant Build-up Manual Consumable Material List
Illustrated Tools and Equipment Manual
Ground Service Equipment (GSE) Technical Publications
Structural Repair Manual
Non- Destructive Inspection (NDI) Manual
Shop Test Equipment Manual General Information and Servicing Manual
Aircraft Towing Manual
Basic Weight Checklist and Loading Data
Aircraft Scheduled Inspection and Maintenance Requirements
Equipment Inventory List Corrosion Control Manual Non Nuclear Munitions Basic Information
Non Nuclear Munitions Loading Procedures
Non Nuclear Munitions Delivery Manual
Item Specifications Not Comply Comply/ Maintenance Instruction Armaments
System
Component Overhaul Manual Other Technical Orders and
Aircraft/System Equipment Manuals 4. Spare Parts
Program
- The supplier shall provide spares sufficient for two (2) years of operation with an annual utilization rate of six hundred (600) flight hours per aircraft. Fast-moving items and consumables shall be delivered together with the GOODS - The complete list of TCI, RCA, fast
moving items and consumables shall be provided by the supplier during the Opening of Bids (Price List to be included in the financial documents)
5. Product Support Information
- As part of the product support
information, publications and
technical bulletins shall also be provided as long as the aircraft are being operated by the PAF. It shall include among others;
Information Bulletins Service Bulletins Modification Bulletins 6. Multi-Media
Support
- An Electronic Copy of Operators Manual, Maintenance Manual and Illustrated Parts Catalogue
- Computer-Based Training (CBT) for the aircraft systems (power plant, electrical, airframe, etc.)
7. Interim Contract Support
- The Supplier shall be required to have an Interim Contract Support
(ICS) to ensure the proper
operation, maintenance, and
trouble-shooting of the aircraft upon acceptance of the delivery of aircraft. It shall include an ICS team
Item Specifications Not Comply Comply/ to conduct the transition training of
maintenance personnel for all
aircraft systems locally.
- In addition, at least one technical in- country representative shall provide services to the PAF for one year upon
acceptance of the GOODS. In
addition two technical in-country representative/ technicians will be supported by the proponent and shall continue providing On the Job Training to PAF maintenance crew for at least six (6) months starting from delivery
8. Warranty Program - The supplier shall cover Two (2) years warranty period per aircraft
which will commence upon
acceptance of each aircraft
- Any discrepancy due to material failure/factor shall be corrected expeditiously, which should not exceed sixty (60) days upon receipt of
notice by the technical
representative. If sixty (60) days turn around time is not possible, the supplier is under obligation to replace the affected component with a new one or provide a temporary replacement in order not to hamper the operational requirements of the AFP
Item Specifications Not Comply Comply/ 9. After Sales
Support
- After-sales services shall include supply of spares for the aircraft and
components, interim contract
support, technical support, and warranties, which will also cover the
armament and night fighting
systems. Technical support shall include query and answering (to include open/free access to online
information) and assistance on
defect investigation while the aircraft is being operated by the PAF
10. Life Cycle Management Information
- Information/ references/ software
regarding Mean Time Between
Failures (MTBF), lead time, shelf life, total life, repairable cycle assets, as well as information for repair and overhaul of components to include repair turn-around time and cost shall be provided. Likewise, the proponent shall also identify all the authorized repair facilities, local and abroad, where the items would be repaired or overhauled
11. Support
Equipment and Structures
- Supplier shall provide information regarding support equipment and
structures required for the
maintenance and operation of the CAS aircraft. Support equipment may include test equipment for aircraft systems, airframe, and field equipment. On the other hand, support structures shall include, among others, system test facilities 12. Spares and
Components Storage Procedures
- Supplier shall provide storage procedures of sensitive spares and components
DND Bids and Awards, Basement, Right Wing, Department of National Defense, DND Building, Camp General Emilio Aguinaldo, Quezon City; BAC Secretariat – (632) 421-3531/ 982-5626
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