aeroplane maximum takeoff weight (mtow)€¦ · 1.4 aeroplane maximum takeoff weight (mtow) 1.4.1...

In case of a doubts with reference to the interpretation of the provision, the Polish language version shall prevail. The translation into the English language is a supportive material.

No. The required value (limiting value) or the parameter required by the Awarding Entity Guideliness ValueCompliant? ‐ YES

Noncompliant? ‐ NO

1 2 3 4 5

1. Aircraft1.1 Aeroplane wingspan1.1.1 The wingspan of each delivered aeroplane shall not exceed 23 meters (the quotation shall include a drawing with

dimensions).State the wingspan.

1.2 Aeroplane length

1.2.1 The total length of each delivered aeroplane shall not exceed 20 meters (the quotation shall include a drawing with dimensions).

State the length.

1.3 Aeroplane height1.3.1 The total height of each delivered aeroplane shall not exceed 6.5 meters (the quotation shall include a drawing with

dimensions).State the height.

1.4 Aeroplane Maximum Takeoff Weight (MTOW)

1.4.1 The MTOW of each delivered aeroplane shall not exceed 16500 kg (please state the value for the offered aeroplane). State the value.

Translation of the Terms of Reference ZZP-86/18, Appendix No. 1 to the Offer, Limiting parameters / 77




1 2 3 4 51.5 Regulations

1.5.1 Each delivered aeroplane along with each item of equipment being an integral part of the aeroplane shall meet the requirements of the applicable regulations in force in Poland and in the European Union pursuant to the Regulation (EC) No. 216/2008 of the European Parliament and of the Council of 20 February 2008 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency, and repealing Council Directive 91/670/EEC, Regulation (EC) No. 1592/2002 and Directive 2004/36/EC , as amended or provisions replacing it and detailed regulations implementing the requirements of the Regulation (EC) No. 216/2008 or the provisions replacing the above‐mentioned normative acts with respect to initial and continuing airworthiness, requirements relating to the aeroplane equipment for performing specified air operations, including the detailed certification specifications concerning aeroplane construction CS23 Commuter or equivalent or CS25 or equivalent and CS‐AWO Subpart 2 or equivalent, relating to aeroplanes used for commercial air transport (Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council or the provisions replacing the above‐mentioned normative acts.

1.5.2 The systems and devices included in the delivered aeroplane and all equipment (version, model, equipment configuration etc.) shall meet the certification requirements concerning aeroplane construction: CS 23 Commuter or CS 25 and CS‐AWO Subpart 2 and/or, if applicable, other equivalent or additional regulations or requirements of EASA or FAA, ECAC, EUROCAE, RTCA and EUROCONTROL and, as a result, allow the Awarding Entity to meet the applicable requirements of Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council or the provisions replacing the above‐mentioned normative act with respect to commercial air transport and/or other applicable aviation regulations and/or equivalent regulations.

1.6 Electrical system1.6.1 The batteries supplying power to the 24/28V DC power system of the aeroplane shall be a technical solution based on the

NiCd (nickel‐cadmium) technology.





1 2 3 4 51.7 Avionics

1.7.1 Each delivered aeroplane shall meet the applicable regulations with respect to the installed avionics, particularly it shall prove compliance with Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council , with respect to commercial air transport in multi‐crew operations;

1.7.2 Each delivered aeroplane shall be in a configuration approved for ILS DME Category I, VOR, VOR DME approach and RNP Approach: LNAV, LNAV/VNAV, LPV in accordance with Commission Regulation (EU) No. 965/2012 dated October 5, 2008 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council, as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.

1.7.3 The aeroplane shall be in a configuration approved for performing arrivals, departures and en‐route flights in accordance with the following PBN specifications: RNAV5, RNAV1, RNP1, RNP4, RNAV10, in accordance with the applicable provisions, particularly Commission Regulation (EU) No. 965/2012 dated October 5, 2008 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council , as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.

1.7.4 Each delivered aeroplane shall be fitted with two GPS devices, integrated with avionics, as long‐range navigation systems (LRNS), suitable for meeting the requirements of the operational regulations within the scope compliant with Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council, as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.





1 2 3 4 51.7.5 Each delivered aeroplane shall be certified for IFR, VFR day and night flights, and for performing planned flights in known icing

conditions, in accordance with the applicable aircraft construction regulations; additionally, each delivered aeroplane shall be certified to meet the operational requirements, particularly in accordance with Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council, as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.

1.7.6 Each delivered aeroplane shall be fitted with a fully integrated avionics suite with a 'Glass Cockpit', providing independent navigational indications for the pilot in the left‐hand seat and the pilot in the right‐hand seat.

1.7.7 Weather radar (WX radar)

1.7.7.1 Each delivered aeroplane shall be fitted with a weather radar that shall be fully integrated with the reminder of the avionics suite and provide independent indications in the navigational mode for the pilot in the left‐hand seat and for the pilot in the right‐hand seat, in accordance with the applicable provisions, particularly with Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council, as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.

1.7.7.2 The weather radar shall have a turbulence detection function.





1 2 3 4 51.7.8 Flight Management System (FMS)

1.7.8.1 Each delivered aeroplane shall be fitted with two (2) Flight Management Systems; said systems shall be fully integrated with the avionics. The data shall be entered into these Flight Management Systems using individual alphanumeric keyboards (the solutions in which keyboards are displayed on the touch screens shall also be considered as meeting this requirement).

1.7.8.2 In the FMS there shall be installed a navigational database covering the whole world.

1.7.8.3 The databases in the Flight Management System shall be valid as of the day of the acceptance of the aeroplane and shall be provided with a subscription service for at least next 28‐day cycle after the day on which the aeroplane is handed over to the Awarding Entity.

1.7.9 Each delivered aeroplane shall be fitted with avionics displaying Electronically Visualized Approach Plates. The databases shall be valid as of the day of the acceptance of the aeroplane and shall be provided with a subscription service for next 28‐day cycle after the day on which the aeroplane is handed over to the Awarding Entity and shall include the navigational area of the place where the acceptance shall take place and the regions necessary to ferry the aeroplane to Poland.

1.7.10 Each delivered aeroplane shall be fitted with a system displaying the Electronically Visualized IFR Airways on the avionics displays. The databases of the Electronically Visualized IFR Airways shall be valid as of the day of the acceptance of the aeroplane and shall be covered with a subscription service for next 28‐day cycle after the day on which the aeroplane is handed over and shall include the navigational area of the place where the acceptance shall take place and the regions necessary to ferry the aeroplane to Poland.

1.7.11 Each delivered aeroplane shall be fitted with a three‐axis autopilot which shall interoperate fully with navigational devices and the FMS, in accordance with the applicable provisions, particularly Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.





1 2 3 4 51.7.12 Each delivered aeroplane shall be fitted with two (2) transponders, at least of the MODE S Enhanced Surveillance (EHS) type,

in accordance with the applicable provisions, particularly the requirements of EUROCONTROL, CS‐ACNS certification specifications, the EUROCAE ED‐73E standard or equivalent.

1.7.13 Each delivered aeroplane shall be fitted with the ADS‐B systems in accordance with the applicable provisions, particularly Commission Implementing Regulation (EU) No. 1207/2011 of 22 November 2011 laying down requirements for the performance and the interoperability of surveillance for the single European sky with subsequent amendments introduced by Commission Implementing Regulation (EU) No. 1028/2014 of 26 September 2014 amending Implementing Regulation (EU) No. 1207/2011 laying down requirements for the performance and the interoperability of surveillance for the single European sky and Commission Implementing Regulation (EU) No. 2017/386 of 6 March 2017 amending Implementing Regulation (EU) No. 1207/2011 laying down requirements for the performance and the interoperability of surveillance for the single European sky and any subsequent amendments introduced prior to the hand‐over of each aeroplane and with the EUROCONTROL requirements, the CS‐ACNS provisions or equivalent.

1.7.14 Each delivered aeroplane shall be fitted with at least one automatic ELT transmitter with at least 121.5 and 406 MHz broadcasting frequency ranges, in accordance with applicable provisions, particularly Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council with respect to commercial air transport operations, with EUROCAE ED‐62 requirements and having, without any reservations, a valid Type Approval published on the COSSPAS‐SARSAT web site.

1.7.15 Each delivered aeroplane shall be equipped with at least two independent speed indication systems, with a heated Pitot tube with a drain hole and a failure warning system for pressure port, in accordance with the applicable provisions, particularly the Commission Regulation (EU) No. 965/2012 dated October 5, 2012. laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.





1 2 3 4 51.7.16 Each delivered aeroplane shall be capable of performing flights in the RVSM space, in accordance with the applicable

provisions, particularly the Commission Regulation (EU) No. 965/2012 dated October 5, 2012. laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.

1.7.17 Each delivered aeroplane shall be fitted with an Airborne Collision Avoidance System at least of the ACAS II category, version 7.1., in accordance with the requirements of the Commission Regulation (EU) No. 1332/2011 of 16 December 2011 laying down common airspace usage requirements and operating procedures for airborne collision avoidance.

1.7.18 Terrain Awareness and Warning System (TAWS)

1.7.18.1 Each delivered aeroplane shall be fitted with Terrain Awareness and Warning System (TAWS) of the A class.

1.7.18.2 The TAWS databases shall be valid as of the day the aeroplane is accepted and shall be provided with a subscription service for at least next 56‐day cycle after the day on which the aeroplane is handed over to the Awarding Entity.

1.7.19 The avionics of each delivered aeroplane shall allow for obtaining performance data for take‐off and landing for specific aeroplane configurations compliant with the AFM.

1.7.20 Each delivered aeroplane shall be fitted with additional holders allowing for attaching, onto the control wheels or in front of the pilots, one iPad mini device for each pilot, as an Electronic Flight Bags (EFB) device used by the Awarding Entity (iPad mini 3) in a manner compliant with the requirements of the EASA AC‐20‐25 document of 9 February 2014 'Airworthiness and operational consideration for Electronic Flight Bags (EFBs)' or equivalent requirements and two USB power outlets or equivalent in the cockpit (with one outlet for each iPad mini by each pilot); said outlets shall meet the ETSO‐C71 and RTCA DO‐160 requirements or equivalent and be suitable for powering and recharging the batteries of the Electronic Flight Bags (EFB) devices of the Apple iPad mini type used by the Awarding Entity (iPad mini 3).

1.7.21 Each delivered aeroplane shall be fitted with connectors and/or slots for the electronic data carriers, used for updating the navigational databases, particularly: airspace charts, airway charts, obstacle charts, FMS, approach plates.





1 2 3 4 51.7.22 Each delivered aeroplane shall be fitted with:

1.7.22.1 The Cockpit Voice Recorder (CVR) and a separate Flight Data Recorder (FDR), in accordance with the applicable regulations, particularly Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.

1.7.22.2 Quick Access Recoder (QAR) or equivalent. The QAR shall be fitted with a data carrier allowing for transferring data from the QAR to a PC. The QAR shall record at least the parameters indicated as of the day of signing the Agreement in AMC1.1 CAT.IDE.A.190 to Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation.

1.7.22.3 The Contractor shall deliver, along with each aeroplane, a set of devices with corresponding software allowing for reading out and analyzing data registered in the installed QAR as specified in point 1.7.22.2.The Awarding Entity shall allow for using the PGS Vision/Analysis program in the 5.4.0 version owned by the Awarding Entity for the purpose of reading out and analyzing data, provided that a technical solution is delivered which shall allow for transferring data from the aeroplane to the PC computer with the PGS Vision/Analysis software installed and the read‐out and analysis of said data.

1.7.23 Satellite communication.

1.7.23.1 Each delivered aeroplane shall be fitted with telephone satellite communication allowing for initiating, answering and conducting conversations from the cockpit using pilot headsets used for aviation radio communication as well as relaying the call to the medical cabin;

1.7.23.2 Each delivered aeroplane shall be fitted with telephone satellite communication allowing for answering a call relayed by the pilot to the medical cabin using an additional receiver.

1.7.23.3 Not later than 3 months prior to the commencement of the acceptance of the first aeroplane the Contractor shall provide the Awarding Entity with the data necessary for the Awarding Entity to activate the satellite telephone service.





1 2 3 4 51.7.24 Each delivered aeroplane shall be fitted with an approved Controller‐Pilot Data Link Communication (CPDDLC) device with the

ATN VDL Mode 2 protocol; additionally, there shall be corresponding entries made in the approved AFM. Said device shall meet the applicable requirements, particularly Commission Regulation (EC) No. 29/2009 of 16 January 2009 laying down requirements on data link services for the single European sky and the Commission Implementing Regulation (EU) 2015/310 of 26 February 2015 amending Regulation (EC) No. 29/2009 laying down requirements on data link services for the single European sky and repealing Implementing Regulation (EU) No. 441/2014 as amended.

1.7.25 Radio communication

1.7.25.1 Each VHF radio installed in the aeroplanes shall have channel spacing of 8.33 kHz in accordance with the requirements of Commission Implementing Regulation (EU) No. 1079/2012 of 16 November 2012 laying down requirements for voice channels spacing for the single European sky.

1.7.25.2 Each delivered aeroplane shall be fitted with one HF radio with SELCAL function.

1.7.26 All databases shall be valid and provided by the Awarding Entity for the next cycle immediatelly following the day on which the aeroplane is handed over to the Awarding Entity.

1.8 Cockpit1.8.1 Each delivered aeroplane shall be fitted, as per current regulations, with anti‐smoke goggles for each pilot; said goggles shall

be adapted to accommodate oxygen masks in the cockpit,particularly the anti‐smoke goggles shall have a valid ETSO C‐99 authorization or equivalent.

1.8.2 Each delivered aeroplane shall be fitted with at least 3 pieces of Protective Breathing Equipment (PBE), including:‐ 2 devices available from the cockpit,‐ 1 portable device in the medical cabin,in the location dedicated for PBE.

1.8.3 Each delivered aeroplane shall be fitted with backlit holders, one for each pilot, for attaching Approach Plates, in accordance with the applicable provisions, particularly Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.





1 2 3 4 51.8.4 Each delivered aeroplane shall be equipped with pilot seats, with at least longitudinal and vertical adjustment, covered with a

sheep skin fabric or equivalent, with adjustable armrests, providing high level of work comfort during long flights.

1.8.5 Each delivered aeroplane shall be fitted with individual lighting with adjustable lamps for each pilot.

1.8.6 Each delivered aeroplane shall be fitted with anti‐glare shield in the cockpit.

1.8.7 Each delivered aeroplane shall be fitted with ball‐pen holders for each pilot;

1.8.7.1 Each delivered aeroplane shall be fitted with a headset for each pilot.

1.8.7.2 The headset shall be capable of passive noise attenuation (the headset shall cover the ears fully) and shall be fitted with an active noise attenuation system powered by an external power source.

1.8.7.3 Each headset shall be fitted with a microphone arm.

1.8.7.4 The headsets shall meet the ETSO‐C139a standard.

1.8.8 There shall be installed in the aeroplane 2 power outlets for powering the headsets from the on‐board power system; said outlets shall be suitable for the delivered headsets and shall be installed one per side.

1.8.9 Each delivered aeroplane shall be equipped with a first‐aid kit whose contents shall meet the requirements of AMC1 CAT.IDE.A.220 to Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation.

1.8.10 Each delivered aeroplane shall be equipped with at least one emergency axe or crowbar located in the flight personnel compartment (in the cockpit).

1.8.11 Each delivered aeroplane shall be fitted with life vests whose number shall correspond to the approved Maximum Operational Passenger Seating Configuration (MOPSC) and two life vests for the pilots and two life vests for infants.

1.8.12 Each delivered aeroplane shall be fitted with at least two flashlights, with one flashlight for each pilot.





1 2 3 4 51.9 Landing gear

1.9.1 Each delivered aeroplane shall be fitted with a landing gear, having the following characteristics:

1.9.1.1 fully retractable,

1.9.1.2 steerable,

1.9.1.3 fitted with an emergency extension system.

1.9.2 Each delivered aeroplane shall be fitted with a system preventing the wheels from blocking while breaking.

1.10 Powerplant

1.10.1 Each delivered aeroplane shall be fitted with two jet engines.

1.10.2 Each delivered aeroplane shall meet all requirements for a twin‐engined, Class A Performance aeroplane within the meaning of Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council as amended or the provisions replacing the above‐mentioned Regulation with respect to commercial air transport operations.

1.10.3 Each engine compartment shall be fitted with a fire extinguishing system.

1.11 Auxiliary Power Unit or an equivalent technical solution1.11.1 Each delivered aeroplane shall be fitted with an on‐board power source (APU or an equivalent technical solution) which shall

provide, while the aeroplane is stationary on the ground, in any weather conditions, and at ambient temperatures ranging from ‐20°C through +40°C, without any time limitations:

1.11.1.1 power for avionics and cabin lighting and

1.11.1.2 , simultaneously, power for the medical cabin and

1.11.1.3 , simultaneously,heating or cooling of the cabin.

1.11.2 During the operation of the APU or an equivalent technical solution on the ground it shall be allowed to pressure refuel the aeroplane.





1 2 3 4 51.12 Additional equipment (various)

1.12.1 Equipment for performing flights at night in the icing conditions.

1.12.1.1 The aeroplanes shall be fitted with additional devices for lighting or detecting ice formation during night operations in the icing conditions, in the expected or actual icing conditions, so as to meet the requirements of Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council, as regards point CAT.IDE.A.165 Additional equipment for operations in icing conditions at night.

1.12.1.2 If the requirement under point 1.12.1.1 is met by means of additional lighting, then said lighting shall not cause any glare or reflection which might impede the performance of the actions by the crew members.

1.12.2 The aeroplane shall be fitted with a device for detecting wind shear.

1.12.3 The aeroplane shall be fitted with a radio altimeter displaying measurement data on the displays.

1.12.4 The Awarding Entity shall carry out the electromagnetic cross‐interference tests between the medical equipment intended for use in the medical cabin and the on‐board equipment of the aeroplane;





1 2 3 4 51.13 Aeroplane performance‐ pursuant to the Aircraft Flight Manual ascertain whether the requirements for

Mission no. 1 and Mission no. 2 have been met and state the values obtained.

1.13.1 Mission no. 1 ‐ maximum range

1.13.1.1 The maximum range of the aeroplane shall not be lower than 2778 km (1500 NM), without taking into account any significant obstacles in the vicinity of the aerodromes, and taking into account the flight to an alternate aerodrome: ‐ climb after rejected approach to 1524 m (5000 ft), ‐ holding for 5 minutes at 1524 m (5000 ft) flight altitude, ‐ flight to the alternate aerodrome located 278 km (150 NM) away, ‐ landing approach and landing at the alternate aerodrome,‐ final fuel reserve for a flight of 30 minutes in holding with holding speed, over the alternate aerodrome, at an altitude of 457 m (1500 ft). ‐ for computing the maximum range it shall also be assumed that the take‐off aerodrome, landing aerodrome and alternate aerodrome are located at sea level, the runways are dry, windless conditions, ISA, IFR/IMC flight, no‐icing conditions.

The weight assumptions for calculating the maximum range:‐ weight of the patient on the stretcher shall be 136 kg (300 lbs), ‐ two pilots and two medical crew members with total weight of 363 kg (800 lbs), ‐ portable equipment and baggage of total weight of 227 kg (500 lbs) (including the weight of the medical oxygen bottle, i.e. 22.7 kg (50 lbs)),

The Basic Empty Weight configuration for calculating the maximum range shall meet the following assumptions:‐ a station for one patient on the stretcher,‐ 2 seats for the medical crew with backrest tilt adjustment,‐ 1 (one) seat with backrest tilt adjustment up to the angle of not less than 80 degrees from the vertical position,‐ nominal volume of liquid in the toilet tanks,‐ unusable fuel,‐ oils required for flight in the nominal volumes for each system,‐ equipment compliant with the requirements of this specification, particularly PBE, fire extinguisher, axe or crowbar.

The results of the calculations shall be submitted as an appendix to the quotation. They shall be done solely using the data from current (as of the calculation day) Airplane Flight Manual of a given aeroplane.





1 2 3 4 51.13.2 Mission no. 2 ‐ domestic flight with significant load

The performance of a missionwith a distance of 400 NM between the take‐off aerodrome and the destination aerodrome, from a aerodrome with an asphalt/concrete runway of 1300 meters. Without taking into account significant obstacles in the vicinity of the aerodromes. The flight shall be performed in accordance with the following assumptions:‐ the altitude shall not exceed FL250,‐ landing approach at the destination aerodrome,‐ climb after rejected approach to 5000 ft, ‐ holding for 5 minutes at 5000 ft, ‐ flight to the alternate aerodrome located 150 NM away, ‐ fligth to the alternate aerodrome at not more than FL250,‐ landing approach and landing at the alternate aerodrome, ‐ final fuel reserve for flight over the alternate aerodrome, 30 minutes of holding with holding speed, at an altitude of 1500 ft, ‐ the take‐off aerodrome, landing aerodrome and alternate aerodrome are located at sea level, the runways are dry, windless conditions, ISA, IFR/IMC flight, no‐icing conditions.

Weight assumptions for calculating a mission whose length is 400 NM:‐ weight of the patient on the stretcher shall be 136 kg (300 lbs),‐ two pilots and two medical crew members with total weight of 363 kg (800 lbs), ‐ two additional medical crew members with total weight of 181.5 kg (400 lbs), ‐ portable equipment and baggage of total weight of 227 kg (500 lbs) (including the weight of the medical oxygen bottle, i.e. 22.7 kg (50 lbs)),

1.13.2.1 The results of the

calculations shall be

submitted as an appendix

to the quotation.

They shall be done solely

using the data from current (as of the calculation

day) Airplane Flight Manual of a given aeroplane.





1 2 3 4 5The Basic Empty Weight configuration for calculating a mission of 400 NM length:‐ a station for one patient on the stretcher,‐ 2 seats for the medical crew with backrest tilt adjustment,‐ 1 (one) seat with backrest tilt adjustment up to the angle of not less than 80 degrees from the vertical position,‐ 1 low‐weight seat for the additional medical crew member,‐ nominal volume of liquid in the toilet tanks,‐ unusable fuel,‐ oils required for flight in the nominal volumes for each system,‐ equipment compliant with the requirements of this specification, particularly PBE, fire extinguisher, axe or crowbar.‐ hardcopy documentation necessary for a flight, particularly: Airplane Flight Manual, Pilot's Operating Handbook, Quick Reference Handbook, Weight & Balance Manual.‐ 2 pieces EFB ‐ iPad (assume iPad mini 3, with unit weight of 0.312 kg, owned by the Awarding Entity)‐other equipment necessary for performing this flight.





1 2 3 4 51.14 Flight endurance

1.14.1 The flight endurance shall be at least 3 hours in the aeroplane configuration as for Mission no. 1‐ maximum range, as specified in point 1.13.1.

1.15 Maximum service ceiling

1.15.1 The maximum service ceiling shall not be lower than FL 420.

1.16 The maximum ceiling at which it shall be possible to maintain the cabin altitude equal to 0 ft AMSL

1.16.1 Not lower than 24000 ft, AMSL, on the assumption that the take‐off aerodrome is located at sea level height.

1.17 Passenger/medical cabin

1.17.1 The requirements concerning passenger/medical cabin have been specified in point 2 hereto. Aircraft medical cabin.

1.18 Livery, placards, silks and decals

1.18.1 All placards, silks and decals in each aeroplane, aside from the cockpit, shall be in the Polish and English language versions.

1.18.2 All placards, silks and decals in each aeroplane, in the cockpit, shall be in the English language version.

1.18.3 The Contractor shall submit an aeroplane livery design within thirty (30) days of the day this Agreement is signed. The aeroplane livery design shall be similar to the livery design of the aeroplanes operated by the Buyer. The aeroplane livery design shall be assessed and approved by the Awarding Entity.

1.19 Ground Operations

1.19.1 Each delivered aeroplane shall be approved for the application of fluids at least of the following types: I, II and IV, for ground preflight de‐icing and anti‐icing procedures.





1 2 3 4 51.20 Pilot training

1.20.1 The Contractor shall provide, at his cost and expense, the training for eight (8) pilots of the Awarding Entity:

1.20.1.1 type rating for the offered aeroplane, including six (6) take‐offs and landings in the Awarding Entity's aeroplane, for each of the eight pilots;

1.20.1.2 the ATPL(A) exam if the offered type of the aeroplane requires such a licence to carry out the duties of a Pilot in Command;

1.20.1.3 the OPC exam for eight (8) pilots, including four (4) qualified to in eihter pilot's seat;

1.20.1.4 the UPRT from the left seat for eight (8) pilots;

1.20.1.5 the UPRT from the right seat for four (4) pilots;

1.20.1.6 the simulator training shall be performed in the FFS level D with a EASA‐issued certificate.

1.20.2 The training referred to in point1.20.1.1 shall cover: ACAS II, version 7.1, TAWS, RVSM, CDPLC, HF, and other systems with which the offered aeroplane is fitted.

1.20.3 The training and exams shall be carried out at an ATO in accordance with Commission Regulation (EU) No. 965/2012 dated October 5, 2012 laying down technical requirements and administrative procedures related to air operations pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council and Commission Regulation (EU) No. 1178/2011 dated November 3, 2011 laying down technical requirements and administrative procedures related to civil aviation aircrew pursuant to Regulation (EC) No. 216/2008 of the European Parliament and of the Council

1.20.4 The pilot training shall be carried out in groups of four (4) participants.





1 2 3 4 51.20.5 The pilot training in a simulator shall begin not earlier than three (3) months prior to the date on which the first aeroplane is

to be handed over and shall be finished before the commencement of the Technical Acceptance of the first aeroplane. The dates of the trainings shall be agreed upon at least two (2) months in advance. The 6 take‐offs and landings in the aeroplane shall take place on the following dates and in the following places:

1.20.5.1 For the first four (4) pilots immediately after the first aeroplane is handed over at the place where the handover is effected. The Contractor shall notify the Awarding Entity about the dates of the training at least twenty‐one (21) days in advance.

1.20.5.2 For four (4) other pilots ‐ in Poland up to thirty (30) days after the Aeroplane Ownership Transfer Title to the first aeroplane is transferred. The Contractor shall notify the Awarding Entity about the dates of the training at least fourteen (14) days in advance. The aeroplane shall be based at the F. Chopin International Aerodrome in Warsaw (EPWA).

1.20.6 The Contractor shall provide the Awarding Entity with access to the electronic version of the training materials used during the pilot training as well as access to AFM/POH, QRH, WBM, Avionics User Guide and other documents supporting the pilots as soon as it is feasible after the Agreement is signed, nonetheless, not later than after six (6) months; the number of these accesses shall be eight (8). The Contractor shall provide the above‐mentioned materials in the English language.

1.20.7 The costs incurred in connection with the use of the Awarding Entity's aeroplane (fuel, aerodrome fees and navigation fees) shall be covered by the Awarding Entity.

1.20.8 The travel and stay costs with respect to the Awarding Entity's personnel undergoing training, as specified in this paragraph, shall be borne by the Awarding Entity.





1 2 3 4 51.21 Training for mechanics/auditors/technical supervision inspectors

1.21.1 The Contractor shall, at his cost and expense, perform the training compliant with the requirements of the level 3 trainings in accordance with Part 66, at a certified Part 147 organization, for six (6) mechanics of the Awarding Entity. The theoretical and practical training shall cover all of the systems and installations constituting the equipment of the aeroplanes being the subject of the Agreement. The travel and stay costs with respect to the Awarding Entity's personnel undergoing training, as specified in this paragraph, shall be borne by the Awarding Entity.

1.21.2 The trainings shall cover the full scope, including the following specialties: ‐ airframe, avionics (B 1.1, B2), ‐ engine (B 1.1),‐ APU or equivalent technical solution (B 1.1),with respect to the theoretical scope, as proven by the exams necessary to obtain the type rating entry in the licence issued in accordance with Part 66, and with respect to the practical scope, concluding with the issuance of the documents proving the accomplishment of the practical training on a given type within the scope of line and base maintenance up to the level allowing to obtain the type certification entry in the licence issued in accordance with Part 66, in an aeroplane whose configuration shall be as similar as possible to the configuration of the aeroplanes delivered to the Awarding Party. The training for mechanics, covering the B1.1 and B2 level, shall be performed in two tours.

1.21.3 The Contractor shall, at his cost and expense, provide the theoretical and practical Engine Run training to three (3) mechanics of the Awarding Entity. This training shall be accomplished together with the training specified in 1.21.1.

1.21.4 The training for the mechanics within the scope specified in point 1.21.2 and 1.21.3 shall take place not earlier than three (3) months prior to the handover of the first aeroplane and shall be accomplished with respect to the training and the required practice prior to the first day of the technical acceptance of the first aeroplane. The dates of the trainings shall be agreed upon at least 2 months in advance.

1.21.5 The Contractor shall provide the Awarding Entity with eight (8) accesses to the training materials used during the training for the mechanics immediately after the Agreement is signed, nonetheless, not later than after six (6) months. The Contractor shall provide the above‐mentioned materials in the English language. The Contractor shall agree to use the training materials free of charge solely for the own purposes of the Awarding Entity.





1 2 3 4 51.21.6 The Contractor shall, at his cost and expense, immediately before or during the technical acceptance process of the first

aeroplane, through an authorized representative, provide training to one mechanic of the Awarding Entity within the scope of the scheduled maintenance, typical troubleshooting with respect to equipment and systems in the medical cabin installed in the aeroplane.

1.21.7 Notwithstanding other required trainings, the Contractor shall provide General Familarization training for six (6) persons indicated by the Awarding Entity; said training shall cover the aeroplane type whose configuration shall be similar to the highest possible extent to the configuration of the aeroplanes delivered to the Awarding Entity. This training shall be compliant with the requirements of Part 66 level 1 and be provided by a certified Part 147 organization at the registered office of the Awarding Entity not later than sixty (60) days prior to the first day of the technical acceptance of the first aeroplane.





1 2 3 4 51.22 Medical and technical personnel training

1.22.1 The Contractor shall, at his cost and expense, immediately before or during the acceptance process of the first aeroplane, through an authorized representative, provide training to the medical personnel of the Awarding Entity within the scope of the medical cabin operation, including the medical cabin equipment installed in it. The travel and stay costs with respect to the Awarding Entity's personnel undergoing training, as specified in this paragraph, shall be borne by the Awarding Entity. The scope of the training shall cover in particular:a) the stowage of the portable medical equipment,b) the loading and removing the stretcher with a patient,c) the loading and removing the incubator,d) the replacement of simple consumable items,e) using the electrical power system,f) using the medical gases systems,g) using the lighting system,h) using the optional equipment,i) other activities relating to the operation of the medical cabin systems,j) the authorized manner of washing and disinfecting the inside of the medical cabin and the equipment,k) the aeroplane emergency egress procedures for the crew and the patient.

1.22.2 The Contractor shall, at his cost and expense, provide the training for two medical personnel groups of the Awarding Entity, in the Polish language, at the Awarding Entity's registered office, within the scope of the operation of the portable medical equipment delivered by the Contractor under the contract. The groups of trainees shall comprise not more than ten (10) persons. The Contractor shall issue the documents as a proof of accomplishment of training by the trainees.





1 2 3 4 51.23 Maintenance requirements

1.23.1 The Contractor shall, at his cost and expense, provide support for the technical personnel of the Awarding Entity, whereby a mechanic or mechanics of the Part 145 organization with a valid Part 66 licence of the B1 and B2 category relating to the type of the delivered aeroplane or equivalent shall be present. The above‐mentioned support shall be provided by the Contractor for sixty (60) days.

1.23.2 The performance of the scheduled and unscheduled aeroplane maintenance within the scope of work of the Part 145 Maintenance Organization of the Awarding Entity with simultaneous adherence to the conditions specified in the regulations and approved manuals shall not have any influence on any warranties granted.

1.23.3 The Contractor shall provide, within the process of removing faults, the specialist engineering support for the Awarding Entity through the communication channels which will be indicated during the Agreement signing stage, during the whole period of operating the aeroplanes by the Awarding Entity.

1.24 Basic ground equipment

1.24.1 The following set of ground equipment shall be delivered with each aeroplane:

1.24.1.1 all devices and/or containers for performing necessary draining and taking of fuel samples; said devices and/or containers shall simultaneously protect against introducing any contamination to the fuel;

1.24.1.2 a complete, simple system for moving the aeroplane around the concrete apron ('beam', 'guide bar', etc.);

1.24.1.3 a set of covers, caps, dust covers and shields for: air inlets to the engine systems, APU, static and dynamic pressure systems, ventilation and cooling systems, gas and air exhausts ‐ protecting against contamination and accidental damage during parking and made of bright materials and marked in a visible way to attract one's attention to the need of removing them before take‐off.

1.24.1.4 the necessary protections to be used while the aeroplane is parked, particularly: protecting the flight control systems, doors, static dischargers and thrust reversers ‐ if applicable;

1.24.1.5 cargo bay items of equipment for stowing the objects in the cargo bays.

1.24.1.6 at least 10 sets of keys to the aeroplane doors and cargo bays,

1.24.1.7 at least 1 set of supports for the landing gear allowing for blocking the main landing gear wheel in both directions,





1 2 3 4 51.24.1.8 a set of adapters to lift the aeroplane,

1.24.1.9 a support protecting the aeroplane tail from coming in contact with the ground.

1.25 Tools and special equipment

1.25.1 The Contractor shall deliver 2 sets for lifting the aeroplane ‐ jacks along with any elements of jack sockets.

1.25.2 The Contractor shall deliver one (1) set of equipment (except for the standard tools) for performing scheduled and unscheduled line and base maintenance of the airframe, engines and avionics, of the lowest and immediately higher level, as results from the flight hours logged up to 1200 FH, and as prescribed by the scheduled technical maintenance program of the manufacturer and/or aeroplane maintenance manual (including the airframe, engines and avionics) and up to the maintenance level after two (2) years of use inclusive, in particular:

1.25.2.1 The Electric ground power systems (e.g. Ground Power Unit),

1.25.2.2 The hydraulic cart (if necessary for any aeroplane maintenance),

1.25.2.3 The battery charging device (e.g. Battery Charger),

1.25.2.4 Two (2) engine maintenance stands,

1.25.2.5 One set of a sling for removing an engine,

1.25.2.6 The Tire inflation cages ‐ for each type of wheels,

1.25.2.7 The avionic testers,

1.25.2.8 The pneumatic testers (Pitot Static Tester),

1.25.2.9 The adapters for pressure systems (e.g. inflating the wheels and shock absorbers with nitrogen, connecting gauges to the static and total pressure ports in the air systems, testing the fuselage pressurisation and pumping oxygen to the on‐board emergency oxygen system, etc.),

1.25.2.10 The adapters for hydraulic systems,

1.25.2.11 The test devices for airframe elements (e.g. Steering, WoW),

1.25.2.12 A set of computer programs for performing maintenance and tests of the systems along with adapters,





1 2 3 4 51.25.2.13 The adapters for testing the fuselage pressurisation system,

1.25.3 The set of equipment specified in 1.25.2 shall be delivered to the address indicated by the Awarding Entity not later than thirty (30) days prior to the deadline for handing over the first aeroplane.

1.25.4 The electronic maintenance support program.

1.25.4.1 The Contractor shall deliver to the Awarding Entity an electronic maintenance support program or an online access to such a program along with a registration performed on behalf of the Awarding Entity, if necessary.The term: 'electronic maintenance support program' shall be construed to mean software or an online application for planning and managing maintenance, including scheduled and unscheduled maintenance, the so‐called Maintenance Management Program or Maintenance Assistance System.

1.25.4.2 The Awarding Entity shall obtain the rights and capabilities to use the program/application specified in 1.25.4.1 not later than 30 days prior to the deadline for handing over the first aeroplane.

1.25.4.3 Immediately, but not later than within 7 days, after the rights and capabilities to use the program/application specified in 1.25.4.1 are obtained by the Awarding Entity, the Contractor shall commence the training of at least 10 users of the Awarding Entity; said training shall cover the operation of the 'electronic maintenance support program', and be conducted at the Awarding Entity's registered office.

1.25.4.4 The Contractor shall provide, as part of the total price indicated in the quotation and without any additional payment charged to the Awarding Entity, the usage of the 'electronic maintenance support program' along with the revision service and access to the maintenance system, if required, at least till the end of the year immediately following the year in which the handover of the second aeroplane took place.

1.25.4.5 The Contractor shall provide active usage of this program for at least fifteen (15) users with simultaneous usage of the system from at least five (5) stations.





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1.26 The list of parts considered as having a military use or dual use

1.26.1 The Contractor shall immediately, but not later than 6 months prior to the hand‐over day of the first aeroplane, notify the Awarding Entity in writing whether the performance of the Agreement entails the delivery of goods of strategic importance, as referred to in Article 3 point 3 of the Act dated November 29, 2000 on Trade with Foreign Countries in Goods, Technology and Services of Strategic Importance to the Security of the Country, and to Upholding International Peace and Security with Foreign Countries (Journal of Laws 2017.1050 consolidated text), hereinafter referred to as the Agreement; moreover, the Contractor shall submit a list of such goods.

1.26.2 Any data referred to in clause 1.26.1, aside from the list of the goods, shall have the goods control number assigned in accordance with:The Regulation of the Minister of Entrepreneurship and Technology dated February 28, 2018 on the list of armament which may be traded in only if a permit is issued (Journal of Laws 2018 item 482) – for armament;The Council Regulation (EC) no. 428/2009 dated May 5, 2009 setting up a Community regime for the control of exports, transfer, brokering and transit of dual‐use items (the Official Journal of the European Union 2009 L134/1 as amended) – for dual‐use items.





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1.27 Documentation of initial airworthiness

1.27.1 For every aeroplane the Contractor shall deliver, along with the aeroplanes, the documents meeting the following requirements:

1.27.1.1 With respect to aircraft manufactured in the European Union (EU) it shall be necessary to submit a Statement of Conformity, on the EASA Form 52, issued in accordance with Part 21A.163(b) or issued in accordance with Part 21A.130 (Part 21 constitutes an appendix to the Commission Regulation (EU) 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations) and confirmed by the relevant Aviation Authority or for the aircraft manufactured outside the European Union it shall be necessary to submit an Export Certificate of Airworthiness issued by the Aviation Authority of the country of the manufacturer (C of A/Export C of A/ Statement of Conformity).

1.27.1.2 The documents specified in point 1.27.1.1 shall be submitted in original.

1.27.1.3 The list of all design changes introduced in an aeroplane/engines/APU or equivalent ‐ a list of each Design Change (e.g. STC, EO, EB, FAA Form 337) embodied on the Aircraft/Engines/other equipment ‐ Applicant must establish EASA approval/acceptance of each design change except where automatically accepted via EASA Executive Director decisions.

1.27.1.4 Electrical Load Analysis

1.27.1.5 Aircraft/Engine/APU (or equivalent) log books and component log cards

1.27.1.6 Aircraft Weighing Report

1.27.1.7 Flight Test Report and a copy of manufacturers Flight Test completion declaration

1.27.1.8 List of Manufacturing Concessions/Deviations, if any

1.27.1.9 Cabin Configuration Control ‐ Copy of configuration drawing (LOPA)

1.27.1.10 Avionics Equipment List

1.27.1.11 Transponder Mode S ‐ Verification of Mode S code Mode S Code programmed and checked





1 2 3 4 51.27.1.12 ELT Code ‐ Verification and confirmation of ELT code. ELT Code programmed and checked

1.27.1.13 FDR / CVR Compliance Statement ‐ FDR required parameter verification and CVR recording performance

1.27.1.14 List of Derogations, Waivers and Exemptions from the TC ‐ if applicable, must be authorised in writing by EASA

1.27.1.15 Compass Check Certificate

1.27.1.16 List of Placards and Markings ‐ in accordance with TCDS, AMM chapter 11, AFM and national regulations

1.27.1.17 List of all serialized parts and devices installed in an aeroplane, stating, respectively: the catalogue numbers, serial numbers and Component Life Limit Status, if applicable, as an editable electronic file.

1.27.1.18 Airworthiness Directives Status Report

1.27.1.19 Modification Status Report

1.27.1.20 Repair and Damage Records (Major repairs previously embodied, including approval status (e.g. FAA 8110‐3 reports) Records containing unrepaired damages), if any

1.27.1.21 Air Data (Pitot / Static) System ‐ Leakage Test

1.27.1.22 RVSM Compliance Statement

1.27.1.23 A/c PBN Status Statement

1.27.1.24 Emergency Equipment List and Location

1.27.1.25 Equipment List ‐ (P/N, S/N, Soft‐ & Hardware Mods

1.27.1.26 Pattern of Passenger Briefing Cards





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1.28 Flight documentation1.28.1 The flight documentation shall be delivered along with each aeroplane; said documentation shall be in the English language,

in the electronic version and as a hardcopy, and the revision of said documentation shall be included in the aeroplane price and provided till the end of the operation of the aeroplanes by the Awarding Entity. Said documentation shall include particularly:

1.28.1.1 Airplane Flight Manual (AFM), Flight Manual Supplements (FMS) and Pilot’s Operation Handbook (POH) or equivalent documents;

1.28.1.2 Quick Reference Handbook (QRH) covering the operation of the aeroplane and the avionics or equivalent documents.

1.28.1.3 A Pilot's Check List or equivalent documents;

1.28.1.4 Weight and Balance Manual

1.28.2 The documentation specified in points from 1.28.1.1 through 1.28.1.4 shall be presented ready for handover as of the date of commencement of the technical acceptance of each aeroplane,

1.28.3 The flight documentation delivered in the electronic form adapted for PCs shall have the following characteristics:

1.28.3.1 allow for accessing it without Internet connection (offline),

1.28.3.2 have an active table of contents

1.28.3.3 have a search function capable of searching for words/phrases

1.28.3.4 allow for printing.

1.28.4 The electronic documentation shall also be capable of being viewed by means of an application installed on the iPad device.

1.28.5 Six (6) months prior to the handover date of the first aeroplane, the Awarding Entity shall be provided with the documentation containing data on operational suitability (Operational Suitability Data, OSD), in an electronic form, covering the following topics:

1.28.5.1 minimum training program qualifying to receive pilot qualifications on a given aeroplane type, including the specification of a given type;





1 2 3 4 51.28.5.2 specification, for the flight crew, of the type or version of the aeroplane and data specific to a given type;

1.28.5.3 minimum training program qualifying to receive certifying staff qualifications with respect to a given aeroplane type, including the specification of a given type;

1.29 Documentation of continuing airworthiness

1.29.1 Six (6) months prior to handing over the first aeroplane the Awarding Entity shall be provided with the technical documentation necessary for obtaining approval of the Awarding Entity's aeroplane maintenance program from the Polish aviation authority; said program shall cover the aeroplanes of the type scheduled for delivery to the Awarding Entity, ‐ in an electronic format, ‐ in the English language, including, particularly:

1.29.1.1 Manuals used to maintain continuing airworthiness of an aeroplane, particularly in the form of the following types of documents: Maintenance Review Board Report and Maintenance Planning Document and/or Maintenance Manual and/or Service Life & Time Limits Manual and/or Certification Maintenance Requirement Document;

1.29.1.2 Airplane Flight Manual – AFM and Pilots Operating Manual/Owners Manual (if applicable) along with Flight Manual Supplements (FMS))

1.29.1.3 other manuals necessary to perform flight operations, particularly in the form of the following types of documents: Quick Reference Handbook (QRH), Configuration Deviation List (CDL),

1.29.1.4 Master Minimum Equipment List

1.29.1.5 Aircraft Weight and Balance Manual (WBM)

1.29.1.6 Corrosion Prevention and Control Programme (CPCP)

1.29.1.7 Manuals for maintaining continuing airworthiness of the engines, including, particularly: Engine Maintenance Manual and Illustrated Parts Catalogue or equivalent manuals;

1.29.1.8 Manuals for maintaining continuing airworthiness of the Auxilliary Power Unit, including, particularly: Maintenance Manual and Illustrated Parts Cataloge or equivalent manuals;





1 2 3 4 51.29.1.9 The Contractor shall deliver the Component Maintenance Manuals for the maintenance of components and parts with

respect to which there are tasks envisioned in the continuing airworthiness documentation, but with respect to which the performance procedures have not been included in said documentation.

1.29.1.10 The Contractor shall deliver the documentation concerning:‐ the modifications embodied in accordance with Commission Regulation (EU) No. 748/2012 dated August 3, 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations or in accordance with equivalent regulations, particularly by means of Supplemental Type Certificates (STC) with respect to: Instruction for Continuing Airworthiness, Service Bulletins, Service Letters for each modification.

1.29.2 The continuing airworthiness documentation shall be delivered in an electronic form for the PC Windows operating system and shall allow access without Internet connection (offline ), have an active table of contents and shall have a search function capable of searching the text and printing as well as the possibility of using said documentation for the purpose of preparing own internal documents.

1.29.3 The documentation specified in point 1.29.1.1 shall be delivered in the electronic format allowing also for exporting to the 'electronic maintenance support program', the requirements for which have been specified in 1.25.4.

1.29.4 The Contractor shall deliver along with the first aeroplane the records necessary to maintain continuing airworthiness along with performing maintenance (Aircraft Continuing Airworthiness Records), up to the highest level of maintenance foreseen be the aeroplane, engine and other components manufacturers, except for overhauls, in an electronic format, in the English language, in a form allowing for recording said records on the mass storage carriers, and containing in particular:

1.29.4.1 Manuals used to maintain continuing airworthiness of an aeroplane, particularly in the form of the following types of documents: Maintenance Review Board Report and Maintenance Planning Document and/or Maintenance Manual and/or Service Life & Time Limits Manual and/or Certification Maintenance Requirement Document;

1.29.4.2 Set of Service Bulletins (SB), Mandatory and Alert Service Bulletins (ASB, EASB, etc.), service letters, service information and aeroplane tools information

1.29.4.3 Illustrated Parts Catalog (IPC) of the aeroplane

1.29.4.4 Fault Isolation Manual (FIM)





1 2 3 4 51.29.4.5 Airplane Flight Manual – AFM and Pilots Operating Manual/Owners Manual (if applicable) along with Flight Manual

Supplements (FMS))

1.29.4.6 other manuals necessary to perform flight operations, particularly in the form of the following types of documents: Quick Reference Handbook (QRH), Configuration Deviation List (CDL),

1.29.4.7 Master Minimum Equipment List

1.29.4.8 Aircraft Weight and Balance Manual (WBM)

1.29.4.9 Structure Repair Manual (SRM)

1.29.4.10 Non‐Destructive Testing Manual (NDT)

1.29.4.11 Corrosion Prevention and Control Programme (CPCP)

1.29.4.12 Manuals for maintaining continuing airworthiness of the engines, particularly the Engine Maintenance Manual, Engine Illustrated Parts Catalogue or equivalent manuals, Service Bulletins and Service Letters, service information, tools information;

1.29.4.13 Manuals for maintaining continuing airworthiness of the Auxilliary Power Unit or an equivalent system, including, in particular, the Maintenance Manual and the Illustrated Parts Catalogue or equivalent manuals, Service Bulletins and Service Letters, service information, tools information;

1.29.5 Along with the documentation specified in points from1.29.4.1 through 1.29.4.13 there shall be provided a revision service which shall be valid and active from the day the first aeroplane is handed over till, at least, the end of the next calendar year.

1.29.6 The access to the documentation specified in points from 1.29.4.1 through 1.29.4.13, in the English language and to the revision service of this documentation shall be provided to the Awarding Entity as of the first day of the technical acceptance of the first aeroplane, without any additional charge, in the form of concurrent access to the electronic version of the documentation on the Internet portals for at least thirty (30) users.





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1.30 Other documentation

1.30.1 The documentation allowing the Awarding Entity to obtain all Radio Licences for a given aeroplane; the list of said documentation shall be agreed upon by the Parties not later than three (3) months prior to the hand‐over of the first aeroplane. Said documentation shall be delivered to the Awarding Entity two (2) months prior to the day on which the technical acceptance of the first aeroplane shall commence

1.30.2 Not later than three (3) months prior to the deadline for handing over the first aeroplane the list of the recommended spare parts for two aeroplanes shall be delivered to the Awarding Entity,

1.31 Warranty

1.31.1 The Contractor shall grant the Awarding Entity the warranty for the delivered aeroplanes and all of their parts regardless of their manufacturer for the period of time which shall run from the day the Ownership Transfer Title to each aeroplane is transfered.

1.31.2 Each delivered aeroplane and equipment shall be factory‐new, have necessary attestation, opinions, certificates and permits applicable as of the day of the commencement of the technical acceptance of each aeroplane. A factory‐new aeroplane shall be considered to be an aeroplane whose manufacture commenced not earlier than after the day on which the Agreement is signed; said aeroplane shall also be unused.

1.31.3 The Contractor shall provide warranty to the Awarding Entity for the delivered aeroplanes for the period of time not shorter than the ones specified below:

1.31.3.1 The warranty period for the airframe structure shall not be shorter than 60 months or not less than 5000 flight hours, whichever is earlier. State the

values.

Number of months:Number of hours:

1.31.3.2 The warranty period for the avionic suite shall not be shorter than 60 months or not less than 5000 flight hours, whichever is earlier. State the

values.






1 2 3 4 51.31.3.3 The warranty period for the powerplants shall not be shorter than 60 months or not less than 2000 flight hours, whichever is

earlier, State the values.


1.31.3.4 The warranty period for the APU or an equivalent technical solution shall not be shorter than 60 months or not less than 2500 flight hours, whichever is earlier. State the

values.


1.31.3.5 The warranty period for the remaining airframe equipment other than the medical cabin installation shall not be shorter than 24 months or not less than 1000 flight hours, whichever is earlier. State the

values.


1.31.3.6 The warranty period for the installed medical cabin shall not be shorter than 36 months, without flight hour limitation.

State the values.


1.31.3.7 The warranty period for portable equipment of the medical cabin shall not be shorter than 24 months, aside from the incubator. State the

values.


1.31.3.8 The warranty period for the incubator shall not be shorter than 12 months.

State the values.


1.31.4 The warranty terms and conditions and the manner of performing warranty repairs, as specified in the points from1.31.3.1 through 1.31.3.6 shall be specified in detail in the Agreement.





1 2 3 4 51.31.5 The Contractor shall deliver the portable medical equipment along with the terms and conditions of the warranties granted by

the manufacturers and written statements of the authorized warranty service organizations confirming that the delivered devices are covered by the warranty.

1.31.6 The Contractor shall deliver the terms and conditions of the warranties granted by the manufacturers to the tools and special equipment, as specified in points from 1.25.1 through 1.25.2.13.





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2. Aircraft medical cabin

2.1 Medical cabin configuration2.1.1 General requirements:

2.1.1.1 The complete equipment of the cabin (including all options foreseen for the cabin as described hereinbelow), shall be approved by means of an STC, as per Commission Regulation (EU) No. 748/2012 dated August 3, 2012, as amended, laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations or regulations replacing the above‐mentioned normative acts.

2.1.1.2 The medical cabin together with its equipment shall meet the requirements specified in the following standards:‐ EN 13718‐2:2015 "Medical vehicles and their equipment ‐ Air ambulances . Part 2: Operational and technical requirements for air ambulances. "‐ EN 13718‐1:2014 "Medical vehicles and their equipment ‐ Air ambulances. Part 1: Requirements for medical devices used in air ambulances. ".

2.1.1.3 The Contractor shall allow the representatives of the Awarding Entity the consultations on the medical cabin design before the certification process begins.

2.1.1.4 The Contractor shall allow the representatives of the Awarding Entity at least two (2) consultations, at a mutually selected place, in order to discuss in detail the medical cabin design whilst said design is being prepared.

2.1.1.5 The final design of the medical cabin shall be accepted by an authorized representative of the Awarding Entity.

2.1.1.6 The Contractor shall use the devices rented by the Awarding Entity, which do not constitute the subject of the order, so as to perform the measurements and functional tests. The list of devices constitutes Appendix no. 16 to the Agreement. The ECMO Maquet Cardiohelp System along with the Maquet HU35 heater‐cooler unit for ECMO shall be an exemption and the technical parameters of these devices shall be supplied by the Awarding Entity.The ECMO Maquet Cardiohelp System along with the Maquet HU35 heater‐cooler unit for ECMO shall be provided by the Contractor for the design purposes and during the acceptance procedure of the first aeroplane.





1 2 3 4 52.1.2 The seats and the stretcher:

2.1.2.1 The station for transporting one (1) patient in a supine position on the stretcher or one (1) patient in the incubator provided that the dimensional requirements specified in PN‐EN 13718‐2:2015 "Medical vehicles and their equipment ‐ Air ambulances. Part 2: Operational and technical requirements for air ambulances. " are met, as referred to hereinbelow.

2.1.2.2 All of the seats shall be certified for take‐off and landing, particularly:

2.1.2.2.1 two (2) seats with backrest adjustment which are fitted with headrests and provide high level of work comfort during long flights;

2.1.2.2.2 one (1) reclining seat with backrest tilt adjustment to at least 80 degree from the vertical position, which is fitted with a headrest and provides high level of work comfort during long flights;

2.1.2.2.3 one (1) low‐weight seat, allowing for quick installation/removal, for the purpose of quick configuration conversions of the passenger/medical cabin.

2.1.2.3 The toilet seat shall meet the requirements for a seat certified for take‐off and landing and shall be fitted with seat belts.

2.1.2.4 The fabric (cover) of all of the seats in the medical cabin shall be easy washable.

2.1.2.5 The Contractor shall deliver the Recommendations and the medical cabin cleaning and disinfection guide specifying the actions (procedures) concerning, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices; said delivery shall take place on the day the medical cabin design is accepted.

2.1.2.6 The Contractor shall deliver a list of cleaning and disinfection liquids and submit a statement stating that the listed liquids have a marketing certification in Poland issued by the President of the Office of the Medicinal Products, Medical Devices and Biocidal Products; said delivery shall take place on the day the medical cabin design is accepted.

2.1.2.7 The disinfection liquids shall not have any adverse effects on the materials from which the components of the medical cabin, the structure, internal finishing and aeroplane equipment are made, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices.





1 2 3 4 52.1.3 The system for loading/unloading a patient on the stretcher or in the incubator:

2.1.3.1 The system shall have a foldable component for loading/unloading the stretcher with a patient on it/the incubator on the transport stand with full equipment.The system, after it is unfolded, shall allow for sliding the stretcher/incubator outside the contour of the aeroplane.The system shall allow free access to the stretcher/incubator outside the aeroplane by at least one person on the left side and one person on the right side of the system in order to load/unload the stretcher with a patient on it/the incubator on the transport stand.

2.1.3.2 The system shall provide for ergonomic and safe loading/unloading of: a) the patient on the stretcher in a supine position along with the medical equipment, b) the patient on the stretcher in a half‐sitting position along with the medical equipment, c) incubator on the transport stand with full equipment and a patient inside the incubator.

2.1.3.3 The system shall constitute an item of the fixed and/or portable aeroplane equipment and it shall be possible to stow the system in the aeroplane during a flight in a safe way.

2.1.3.4 The system shall allow for guiding the stretcher with a patient/the incubator with the transport stand with complete equipment during loading/unloading in a way which shall protect the aeroplane structure and equipment from damage.

2.1.3.5 The cabin shall have passenger doors or cargo doors whose dimensions shall allow for loading/unloading the patient on the stretcher (it shall be assumed that the width at shoulders of the patient along with the thermal protection and the vacuum mattress shall be 60 cm) and the incubator on the transport stand with complete equipment without colliding with the structural components and the equipment both inside and outside the aeroplane.





1 2 3 4 52.1.4 Patient station:

2.1.4.1 It shall be capable of installing either a stretcher (specified in point 2.1.5 hereinbelow) or an incubator (which is the subject of the order ‐ the relevant description of the requirements has been included in point 3.2).

2.1.4.2 It shall include a permanent mounting for the defibrillator; said mounting shall not be affixed to the stretcher (the defibrillator is the subject of the order ‐ the relevant description of the requirements has been included in point 3.1).The system for locking the defibrillator in the mounting shall be protected against accidental unlocking and shall allow for quick mounting/removal of the defibrillator without using any tools.

2.1.4.3 It shall include a permanent mounting for the Hamilton T1 ventilator; said mounting shall not be affixed to the stretcher (the ventilator is not the subject of the order, but shall be rented by the Awarding Entity).The system for locking the ventilator in the mounting shall be protected against accidental unlocking and shall allow for quick mounting/removal of the ventilator without using any tools.

2.1.4.4 It shall include a permanent mounting for four (4) B.Braun Perfusor Space infusion pumps; said mounting shall not be affixed to the stretcher; (the pumps are not the subject of the order, but shall be rented by the Awarding Entity).The system for locking the pumps in the mountings shall be protected against accidental unlocking and shall allow for quick mounting/removal of the pumps without using any tools.

2.1.4.5 It shall include a permanent mounting for the oxygen flowmeter with a regulator; said mounting shall not be affixed to the stretcher (the oxygen dispenser with a regulator is the subject of the order ‐ the relevant description of the requirements has been included in point 3.3). The oxygen dispenser shall be installed in the vicinity of the oxygen sockets.

2.1.4.6 It shall include a permanent mounting for the LSU Laerdal suction unit; said mounting shall not be affixed to the stretcher (the suction unit is not the subject of the order, but shall be delivered by the Awarding Entity).The system for locking the suction unit in the mounting shall be protected against accidental unlocking and shall allow for quick mounting/removal of the suction unit without using any tools.

2.1.4.7 Must include at least four (4) 12 VDC electrical outlets and four (4) 230 VAC electrical outlets and one (1) 28VDC electrical outlet, which have been specified in point 2.3.2.





1 2 3 4 52.1.4.8 Must include at least two (2) AGA oxygen sockets and one (1) AGA compressed air socket.

The socket shall be located in a place allowing for supplying the devices with oxygen and air, as specified in point 2.2.

2.1.4.9 The medical cabin shall be fitted with mountings (not fastened to the stretcher) used for suspending simultaneously 2 (two) containers with infusion solution above the patient station. Individual mounting load: 2 kg.

2.1.5 Stretcher:

2.1.5.1 The stretcher shall comply with PN‐EN 1865‐1:2010+A1:2015 "Patient handling equipment used in road ambulances. Part 1: General stretcher systems and patient handling equipment." (which superseded PN‐EN 1865‐1:2010 referred to in PN‐EN 13718‐2:2015).

2.1.5.2 Stretcher length: 195 cm (+2 cm/‐5 cm).

2.1.5.3 Stretcher width: 55 cm (±2 cm).

2.1.5.4 The stretcher shall be certified for take‐off/landing in a horizontal position.

2.1.5.5 The stretcher/incubator transport stand shall be fitted with a system for emergency disconnection from the mounting on the stretcher base.

2.1.5.6 Must be fitted with an attachable, flight‐certified bridge/rack used for attaching the following medical equipment, particularly: defibrillator (which is the subject of the order), Hamilton T1 ventilator (which is not the subject of the order, but shall be rented by the Awarding Entity) and 3 (three) B.Braun Perfusor Space infusion pumps (which are not the subject of the order, but shall be rented by the Awarding Entity), in case it is necessary to continue the transportation of the patient on the stretcher in an ambulance other than the aeroplane.

2.1.5.7 The stretcher shall be capable of variable adjustment or incremental adjustment with at least 5 (five) intermediate points for lifting the upper part of the patient torso, the adjustment angle shall range from 0 degrees through 75 degrees; the length of that part shall not be lower than 60 cm.

2.1.5.8 The stretcher shall have an adjustable footrest whose length shall not be lower than 90 cm. It shall be possible to lift the leg section by at least 15 degrees. It shall be possible to maintain the adjustment angle in all normal loading/unloading conditions.





1 2 3 4 52.1.5.9 The surface on which a patient may lie down shall meet the following requirements:

2.1.5.9.1 The surface for lying down shall be flat over its whole area and made from a durable and light structure (material). The area of the mattress underneath the chest of a patient shall be made from a durable and light material, which shall allow for cardiopulmonary resuscitation and which shall be resistant to constriction and which shall not spring back.

2.1.5.9.2 The surface for lying down shall be slip resistant and covered with a mattress which shall offer comfort to a patient. The mattress shall be strong enough to allow for carrying out cardiopulmonary resuscitation.

2.1.5.9.3 The mattress shall be capable of conforming to different stretcher settings. The mattress shall be securely fastened to the part of the stretcher underneath the mattress.

2.1.5.9.4 The mattress shall have tight seams so as to prevent patient fluids from penetrating the mattress and facilitate the disinfection. Additionally the disinfectants shall not have an adverse effect on the materials from which the mattress is made.

2.1.5.9.5 The mattress shall be washable and non‐absorbent. If the mattress comprises the cover and the filler, then the mattress design shall allow for their separate cleaning.

2.1.5.10 The seat belts for the patients on the stretcher:

2.1.5.10.1 The stretcher shall have at least the following seat belts: 4 point shoulder‐chest seat belt, 2 point hip seat belt and 2 point seat belt protecting lower extremities.

2.1.5.10.2 All stretcher seat belts shall be replaceable without using any tools.

2.1.5.10.3 The seat belts used shall have patches with data on their suitability; said patches shall be protected against the removal/fading of data provided on them.

2.1.5.10.4 The Contractor shall deliver the Recommendations and the medical cabin cleaning and disinfection guide specifying the actions (procedures) concerning, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices; said delivery shall take place on the day the medical cabin design is accepted.





1 2 3 4 52.1.5.10.5 The Contractor shall deliver a list of cleaning and disinfection liquids and submit a statement stating that the listed liquids

have a marketing certification in Poland issued by the President of the Office of the Medicinal Products, Medical Devices and Biocidal Products; said delivery shall take place on the day the medical cabin design is accepted.

2.1.5.10.6 The disinfection liquids shall not have any adverse effects on the materials from which the components of the medical cabin, the structure, internal finishing and aeroplane equipment are made, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices.

2.1.6 The dimmension and space:

2.1.6.1 The required dimensions of the free space shall meet the requirements of PN‐EN 13718‐2:2015:"Medical vehicles and their equipment ‐ Air ambulances. Part 2: Operational and technical requirements for air ambulances. ".

2.1.6.2 The space behind the headrest of the stretcher shall not be smaller than 40 cm from the patient's head (along the axis of the stretcher), and the width shall not be smaller than 40 cm and shall allow for the performance of the endotracheal intubation.It shall be allowed to change the position of the stretcher in order to meet the above‐mentioned requirement.

2.1.6.3 The space allowing for conducting chest compression on the patient, including using the Schiller Easy Pulse Chest Compression System (the Chest Compression System is not the subject of the order, but it shall be rented by the Awarding Entity), during the resuscitation, shall measure at least 85 cm between the upper surface of the mattress and the roof, and said space shall be measured at a section of the chest of the patient (along the axis of the stretcher), with the stretcher lying flat.

2.1.6.4 The distance between the medial edge of the stretcher and the opposite side of the aeroplane at a section of the chest of the patient, with doors closed, shall be at least 60 cm. In this area there may be located the medical personnel seats, as specified in point 2.1.2and the elements of the work area of the medical cabin.





1 2 3 4 52.1.7 Electrical system:

2.1.7.1 The electrical system of the medical cabin shall allow for the full and unlimited usage of all of the operating modes and functions of the medical equipment installed in the aeroplane (in accordance with the following 3 (three) variants) along with the lighting specified in point 2.4 and the drawer with the fluid warmer specified in point 2.1.8.2.7, in each of the cases: a) while on the ground with the GPU connected, b) with the APU turned off, c) in flight. There shall be checks performed to confirm that the described functionalities have been provided and the report on the positive outcome of the checks shall be submitted to the Awarding Entity not later than on the day the technical acceptance of the first aeroplane is accomplished. Each of the following device configuration variants needs a positive result of the check with respect to their simultaneous operation with the lighting and with the drawer with a fluid warmer switched on.

2.1.7.2 variant 1: a) Hamilton T1 ventilator (1 piece), b) defibrillator (1 piece), which is the subject of the order ‐ the description of the relevant requirements has been provided in point 3.1. c) B.Braun Perfusor Space infusion pumps (4 pieces), d) LSU Laerdal electric suction unit (1 piece), e) DISON BC‐1500A portable fridge for storing drugs;





1 2 3 4 52.1.7.3 variant 2:

a) Hamilton T1 ventilator (1 piece), b) defibrillator (1 piece), which is the subject of the order ‐ the description of the relevant requirements has been provided in 3.1. , c) B.Braun Perfusor Space infusion pumps (4 pieces), d) LSU Laerdal electric suction unit (1 piece), e) DISON BC‐1500A portable fridge for storing drugs; f) ECMO Maquet Cardiohelp System (1 piece) with a Maquet HU35 heater‐cooler unit for ECMO (1 piece) or devices which put a similar load on the electrical system of the aeroplane;

2.1.7.4 variant 3: a) transport incubator (1 piece), which is the subject of the order, and the description of its specification has been included in 3.2 with the chamber warming function activated, b) Hamilton T1 ventilator (1 piece), b) defibrillator (1 piece), which is the subject of the order ‐ the description of the relevant requirements has been provided in point 3.1; d) B.Braun Perfusor Space infusion pumps (4 pieces), e) LSU Laerdal electric suction unit (1 piece), f) DISON BC‐1500A portable fridge for storing drugs;

2.1.8 Usable and storage space:

2.1.8.1 The configuration and the location of the individual items in the usable and storage space of the medical cabin shall be approved by the Awarding Entity along with the whole design of the medical cabin as per the provisions of point 2.1.1.3‐2.1.1.5.





1 2 3 4 52.1.8.2 Cabinets with drawers:

2.1.8.2.1 The surface of the inside of the drawers shall be smooth and easily‐washable.

2.1.8.2.2 The drawers shall be fully removable from the cabinet so that they may be washed and disinfected.

2.1.8.2.3 The drawers shall have a security device against sliding out of the cabinet.

2.1.8.2.4 The drawers shall have a total volume not lower than 46 liters, in various sizes.

2.1.8.2.5 The drawers shall be equipped with a security device against spontaneous opening.

2.1.8.2.6 One (1) of the drawers shall be key‐lockable with at least five sets of keys.

2.1.8.2.7 One (1) of the drawers shall have the medical fluid (in bags) warming function: a) the volume of the drawer shall not be smaller than 6 liters, b) the drawer shall allow for warming medical fluids (in bags) and storing them in the temperature ranging from +40 degrees Celsius through +42 degrees Celsius, c) the drawer shall be fitted with an internal temperature gauge visible from outside of the drawer and a thermostat, d) the drawer warming shall be provided at every flight phase, with the APU operative, including also when the aeroplane is connected to the external power source on the ground.

2.1.8.2.8 There shall be one (1) drawer/container that shall be easily accessible for the medical personnel and intended for the PBE mask.

2.1.8.3 The space in which the shelves are installed:

2.1.8.3.1 Shall have a total volume of at least 190 liters, in various sizes.

2.1.8.3.2 Shall have closable free space of the shelves (the following shall be permitted: blinds, roller‐blinds, doors or the usage of individual load securing devices e.g. a net).

2.1.8.3.3 Shall be fitted with 1 (one) shelf/stowable top whose dimensions shall not be lower than (width x depth) 20 cm x 20 cm for preparing drugs, with raised edges protecting items from rolling off.





1 2 3 4 52.1.8.4 In the medical cabin there shall be necessary space and mounting for:

2.1.8.4.1 A single‐use container for medical waste whose volume shall be 1 liter (the container is not the subject of the order, but shall be rented by the Awarding Entity), allowing for easy replacement.

2.1.8.4.2 The holder for installing a single‐use bag for medical waste whose volume shall not be lower than 6 liters.

2.1.8.4.3 A portable fridge for storing drugs (which is not the subject of the order, but which shall be rented by the Awarding Entity); said drugs shall be protected against the movement of the fridge, with access, at a distance not higher than 1 meter, to a 12V DC or 230V AC electrical power outlet; The dimensions of the space shall not be lower than (height x width x depth): approx. 27 cm x 21 cm x 34 cm.

2.1.8.4.4 Paramedic backpack (which is not the subject of the order, but which shall be rented by the Awarding Entity) a) whose volume shall be approx. 119 liters, b) whose dimensions shall be (height x width x depth): 60 cm x 55 cm x 36 cm, c) whose weight shall be: approx. 20 kg.The Awarding Entity shall allow that the backpack be attached to the floor using belts.

2.1.8.4.5 The ECMO Maquet Cardiohelp System along with the Maquet HU35 heater‐cooler unit for ECMO or equivalent with respect to the dimensions and weights (which are not the subject of the order, and whose technical characteristics shall be provided by the Awarding Entity). The mounting shall allow for conducting a patient therapy, i.e. it shall be located in the immediate vicinity of the stretcher. The Awarding Entity shall allow that the medical cabin configuration be changed in order to temporarily use the ECMO device.





1 2 3 4 52.1.8.5 In the medical cabin there shall be a place to transport the following items and protect them against movement:

2.1.8.5.1 A bag with a Medumat Easy ventilator and an oxygen cylinder (which are not the subject of the order) a) whose volume shall be approx. 45 liters, b) whose dimension shall be (height x width x depth): 30 cm x 25 cm x 60 cm, c) whose weight shall be: approx. 10 kg.

2.1.8.5.2 A bag with a Pneupac BabyPAC 100 neonatal ventilator and an oxygen cylinder (which are not the subject of the order) a) whose volume shall be approx. 33 liters, b) whose dimension shall be (height x width x depth): 30 cm x 17 cm x 65 cm, c) whose weight shall be: approx. 12 kg.

2.1.8.5.3 A bag with the SonoSite iViz portable ultrasound scanner (USG; which is not the subject of the order, but which shall be rented by the Awarding Entity) a) whose volume shall be approx. 4.2 liter, b) whose dimension shall be (height x width x depth): 27 cm x 6 cm x 26 cm,

2.1.8.5.4 A bag with the Schiller Easy Pulse Chest Compression System (the Chest Compression System is not the subject of the order, but shall be rented by the Awarding Entity) a) whose volume shall be approx. 23 liters, b) whose dimension shall be (height x width x depth): 25 cm x 23 cm x 40 cm, c) whose weight shall be: approx. 7.1 kg.





1 2 3 4 52.1.8.6 In the medical cabin or in the cargo compartment there shall be suitable space for the safe transportation of:

2.1.8.6.1 Flexible litter a) whose dimensions in the folded state (height x width x depth) shall be 50 cm x 35 cm x 5 cm, c) whose weight shall be: approx. 2 kg.

2.1.8.6.2 Heating mat a) whose dimensions in the folded state (height x width x depth) shall be 42 cm x 32 cm x 12 cm, c) whose weight shall be: approx. 3 kg.

2.1.8.6.3 Vacuum mattress for adults a) whose dimensions in the folded state (height x width x depth) shall be 80 cm x 70cm x 30 cm, c) whose weight shall be: approx. 10 kg.

2.1.8.7 Other requirements:

2.1.8.7.1 The Contractor shall deliver the Recommendations and the medical cabin cleaning and disinfection guide specifying the actions (procedures) concerning, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices; said delivery shall take place on the day the medical cabin design is accepted.

2.1.8.7.2 The Contractor shall deliver a list of cleaning and disinfection liquids and submit a statement stating that the listed liquids have a marketing certification in Poland issued by the President of the Office of the Medicinal Products, Medical Devices and Biocidal Products; said delivery shall take place on the day the medical cabin design is accepted.

2.1.8.7.3 The disinfection liquids shall not have any adverse effects on the materials from which the components of the medical cabin, the structure, internal finishing and aeroplane equipment are made, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices.





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2.2 Oxygen and air system of the aircraft2.2.1 General requirements:

2.2.1.1 The oxygen and air system shall be fitted with visible pressure gauges (high pressure gauge in the pressurized gas systems and low pressure gauge in the oxygen and air system) and the following conditions shall be met:

2.2.1.1.1 There shall be a possibility of monitoring the current pressure in all pressurized gas systems in flight; said monitoring shall be easily available for the medical personnel.

2.2.1.1.2 There shall be a possibility of easy access for the purpose of opening and closing the valve in each pressurized gas system in flight by the medical personnel.

2.2.1.1.3 The medical oxygen and air supply sockets shall be located in the immediate vicinity of the equipment which they will be supplying, in a manner which shall make it impossible for the feeding line to be accidentally damaged or pulled out from the device whilst the medical or operational actions are undertaken in the cabin.

2.2.1.2 All sockets and connections of the oxygen and air system shall be of the 'AGA' type.

2.2.2 Requirements for the oxygen system inteded for the medical oxygen:

2.2.2.1 All lines of the medical oxygen and air system shall be designed and made in accordance with the requirements in force in aviation, paying special attention to the specific characteristics of the piping systems for medical gases.

2.2.2.2 The system shall be able to accommodate at least 4 (four) oxygen pressurized gas systems (i.e. four (4) composite cylinders whose volume shall be 4.7 litter and which shall have integrated pressure regulators), capable of being filled up to the pressure of 300 bar.Four (4) pressurized gas systems are not the subject of the order and shall be rented by the Awarding Entity for the period required to carry out the certification process with respect to the aeroplane oxygen installation.

2.2.2.3 The replacement of the pressurized gas systems shall be possible for the medical personnel both with respect to the formal and technical requirements.





1 2 3 4 52.2.2.4 The oxygen system shall provide the possibility of replacing at least two (2) pressurized gas systems without using any tools.

2.2.2.5 The Contractor shall, at his cost and expense, immediately before or during the acceptance process of the first aeroplane, through an authorized representative, provide training to the medical personnel of the Awarding Entity (2 persons) with respect to the operation of the medical gas systems.

2.2.2.6 The system shall be capable of switching manually to the next pressurized gas system so that it is possible to effect the changeover in flight. It shall be allowed to meet the above‐mentioned requirement by opening and closing the valves of the individual pressurized gas systems, provided that the requirement for providing an easy access to the valves in flight is met. All pressurized gas systems shall be connected in a way that will also allow for concurrent use of all pressurized gas systems, taking into account the limitations specified in EN 13718‐2:2015 "Medical vehicles and their equipment ‐ Air ambulances. Part 2: Operational and technical requirements for air ambulances.".

2.2.3 Requirements for the compressed air system:

2.2.3.1 The medical cabin shall be fitted with an air compressor whose characteristics shall allow for the operation of the Hamilton T1 ventilator (which is not the subject of the order, but which shall be rented by the Awarding Entity).

2.2.3.2 The air supplied by the compressor shall meet the following characteristics: a) oxygen concentration ‐ between 20.4% V/V and 21.4% V/V, b) maximum total oil content ‐ 0.1 mg/m3 measured in relation to ambient pressure (the liquid, aerosol or vapor phase of the substance shall be allowed), c) maximum concentration of carbon monoxide ‐ 5 ml/m3, d) maximum concentration of carbon dioxide ‐ 500 ml/m3, e) maximum concentration of water steam ‐ 67 ml/m3, f) maximum concentration of sulphur dioxide ‐ 1ml/m3, g) maximum concentration of NO+NO2 ‐ 2ml/m3.

2.2.3.3 The air supplied by the compressor shall be filtered so as to maintain the concentration of solid particulates below the P3 class level as specified in EN 143:2000; It shall be possible to ascertain the efficiency of the filter elements, e.g. by measuring pressure drop downstream of the filter.

2.2.3.4 The Contractor shall submit a document confirming the fulfilment of the above‐mentioned requirements.





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2.3 Electrical power supply of the medical cabin2.3.1 General requirements:

2.3.1.1 The electrical power supply of the medical cabin shall provide power to the medical devices connected in the variants specified in point 2.1.7.2‐2.1.7.4.

2.3.1.2 The electrical power system of the medical cabin shall provide power to all medical devices connected at any given time, with: a) an engine operational both on the ground and in flight, b) GPU connected, c) APU switched on.

2.3.1.3 By each outlet there shall be a placard stating the nominal voltage and current value which may be supplied by a given outlet.

2.3.1.4 Each outlet shall have visible signalling to show whether electric current is supplied to it.

2.3.1.5 Each outlet shall allow for connecting the medical equipment using the original connection systems delivered by the manufacturer of the medical devices.

2.3.1.6 None of the components of the medical cabin electrical system shall pass through the medical cabin space in a manner hampering medical or operational actions undertaken in said cabin; additionally said components shall be routed in a manner providing protection against accidental tearing out or damage.

2.3.1.7 The manner of connecting medical equipment shall make it impossible to disconnect said equipment from the electric power supply system.





1 2 3 4 52.3.2 Electrical outlets required for the station:

2.3.2.1 12/14 VDC electrical outlets:

2.3.2.1.1 In the place where the medical devices shall be used there shall be available at least four (4), independently protected, female, small cigarette lighter type 12/14 VDC outlets, which shall meet the requirements of ISO 4165:2005Road vehicles ‐ Electrical connections ‐ Double‐pole connection ;

2.3.2.1.2 The nominal voltage shall be 13.8 VDC;

2.3.2.1.3 The voltage shall remain between 12.4 and 15.1 VDC.

2.3.2.1.4 The outlets shall supply electrical current of, at least,: 14 A in one outlet, 7 A in each of the three (3) remaining outlets;

2.3.2.1.5 The total 12/14 VDC current value available at a given moment shall be at least 25 A.

2.3.2.2 24/28 VDC electrical outlets:

2.3.2.2.1 In the place where the medical devices shall be used there shall be available at least one (1) female cigarette lighter type 24/28 VDC outlet, which shall meet the requirements of MIL‐DTL‐26482 or equivalent;

2.3.2.2.2 The nominal voltage shall be 27.5 VDC;

2.3.2.2.3 The electrical outlet shall supply electrical current of at least 10 A.

2.3.2.3 230 VAC electrical outlets:

2.3.2.3.1 The total electrical power with respect to the 230 VAC electrical system shall be at least 1500 W continuous electrical power with sinusoidal current waveform.

2.3.2.3.2 In the place where the medical devices shall be used there shall be available at least four (4) female 230 VAC outlets of the CEE 7/7 type;

2.3.2.3.3 The outlets shall supply electrical current of at least: 6 A in one outlet, 3 A in each of the three (3) remaining outlets;





1 2 3 4 52.3.3 USB ports for the medical personnel and the passengers:

2.3.3.1 By each of the seats in the medical cabin there shall be at least one (1) USB type A port.

2.3.3.2 The electrical circuit of the USB ports shall power all devices connected to them at all times, with: a) an engine operational both on the ground and in flight, b) GPU connected, c) APU switched on.

2.3.3.3 Each of the USB ports shall provide electrical current of at least 5V and 2.4A if all medical devices are connected in the variants specified in point 2.1.7.2‐2.1.7.4.

2.3.4 The remaining requirements concerning the electrical system have been specified in the standards listed in point 2.1.1.2.

2.4 Medical cabin lighting2.4.1 The general medical cabin lighting shall provide not less than 50 lux illuminance.

2.4.2 The lighting of the whole stretcher area shall provide not less than 300 lux illuminance.

2.4.3 A spot lighting ‐ lighting provided for the task area for the medical personnel shall provide at least 400 lux illuminance; the task area shall be construed to mean the upper half of the stretcher.

2.4.4 The color temperature shall be within the following range: from 3800 K through 4300 K.

2.4.5 The lighting specified in point 2.4.2 or 2.4.3 shall allow for adjusting the illuminance from the maximum value down to near complete dimming.

2.4.6 The lighting specified in point 2.4.1‐2.4.3 shall be capable of being turned on/turned off independently from one another.

2.4.7 The spot lighting over the seats shall allow for reading and filling out the documents.

2.4.8 There shall be provided a possibility of using the lighting on the ground (while the aeroplane is stationary) and in flight.





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2.5 Other requirements concerning the medical cabin.2.5.1 The walls and the floor of the medical cabin along with the doorsteps shall be made of easily‐washable materials. The surface

of the floor shall have non‐slip characteristics including when wet. The floor shall be sealed and designed in a way allowing for collecting and removing liquid contamination.

2.5.2 The windows in the vicinity of the patient station shall be protected, from the side of the medical cabin, with a smooth, easily‐washable, transparent and disinfectable surface.

2.5.3 The medical cabin installation shall allow for an easy access to the control elements and electrical and gas system connections located in the medical cabin.

2.5.4 If the noise level in the medical cabin exceeds 85 dB, the medical cabin shall be fitted with a hearing protection system for the patient and personnel.

2.5.5 In the medical cabin there shall be an indicator displaying the cabin altitude in feet or meters; said indicator shall be located in a place visible for at least 1 (one) member of the medical personnel.

2.5.6 There shall be air conditioning (A/C) in the cabin.

2.5.7 The heating system shall provide cabin heating from 0⁰C through +18⁰C in less than 30 minutes with ambient temperature of 0⁰C.





1 2 3 4 52.5.8 The Contractor shall, at his cost and expense, immediately before or during the acceptance process of the first aeroplane,

through an authorized representative, provide training to the medical personnel of the Awarding Entity (2 persons) with respect to the medical cabin operation, including the medical cabin equipment installed in it, in particular: a) the stowage of the portable medical equipment, b) the loading and removing the stretcher with a patient, c) the loading and removing the incubator, d) the replacement of simple consumable items, e) using the electrical power system, f) using the medical gases systems, g) using the lighting system, h) using the optional equipment, i) other activities relating to the operation of the medical cabin systems, j) the authorized manner of washing and disinfecting the inside of the medical cabin and the equipment, k) the aeroplane emergency egress procedures for the crew and the patient.

2.5.9 The Contractor shall, at his cost and expense, provide the training for two medical personnel groups of the Awarding Entity, in the Polish language, at the Awarding Entity's registered office, with respect to the operation of the portable medical equipment delivered by the Contractor with respect to the performance of the additional subject of the Agreement. The trainee groups shall consist of not more than 10 persons. The Contractor shall ensure that every trainee shall be issued with a written proof of training. The trainings shall take place on the dates agreed upon by the Parties hereto, nonetheless, not later than 1 week after the day the first aeroplane is handed over.

2.5.10 For the medical cabin there shall be delivered an assembly/disassembly manual concerning the equipment of the components of the medical cabin; said manual shall be in the Polish language in an electronic format allowing for copying and printing out.

2.5.11 The required maintenance checks of the medical cabin shall be compatible with the aeroplane maintenance plan.





1 2 3 4 52.5.12 The Contractor shall deliver the Recommendations and the medical cabin cleaning and disinfection guide specifying the

actions (procedures) concerning, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices; said delivery shall take place on the day the medical cabin design is accepted.

2.5.13 The Contractor shall deliver a list of cleaning and disinfection liquids and submit a statement stating that the listed liquids have a marketing certification in Poland issued by the President of the Office of the Medicinal Products, Medical Devices and Biocidal Products; said delivery shall take place on the day the medical cabin design is accepted.

2.5.14 The disinfection liquids shall not have any adverse effects on the materials from which the components of the medical cabin, the structure, internal finishing and aeroplane equipment are made, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices.





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3 Medical devices

3.1 Transport defibrillator ‐ 2 sets3.1.1 The transport defibrillator configuration in the medical cabin:

3.1.1.1 The medical cabin shall be fitted with a rail system or fixing points or places for secure stowage of the transport defibrillator along with the ancillary accesories necessary for correct work.

3.1.1.2 The requirements concerning fitting the transport defibrillator in a location other than the one specified in point 2.1.5.6:

3.1.1.2.1 The transport defibrillator shall be installed in an immediate vicinity of the main stretcher, at a distance allowing for monitoring/defibrillating/ cardioversing/external cardiac pacing of the patient on the stretcher;

3.1.1.2.2 The installation location shall not hinder the loading/transportation/removal of the patient, including a patient requiring that the stretcher backrest be raised to the maximum position at all times;

3.1.1.2.3 The location in which the transport defibrillator shall be installed in the medical cabin shall allow for using all of the defibrillator functions at any phase of the flight;

3.1.1.2.4 The installation location shall allow for reading out the parameters from the transport defibrillator panel in flight by at least one member of the medical personnel at any phase of the flight;

3.1.1.2.5 The location where the transport defibrillator shall be installed shall allow for easy and fast dismounting/removal and mounting/fastening of the transport defibrillator without using any additional tools.





1 2 3 4 53.1.2 General requirements for the transport defibrillator:

3.1.2.1 The transport defibrillator shall have the following functions: vital sign monitoring, defibrillation, cardioversion and external cardiac pacing.

3.1.2.2 The transport defibrillator shall allow for performing defibrillation, cardioversion and external cardiac pacing of the patient in flight.

3.1.2.3 The transport defibrillator shall be intended for monitoring/electrotheraphy of: adults, children and neonates.

3.1.2.4 The defibrillator shall be factory‐new, manufactured not earlier than in the performance period of the scope of the Agreement.

3.1.2.5 The defibrillator shall offer a protection level against foreign matter (dust/water) of not less than IP 55.

3.1.2.6 The defibrillator shall be vibration and shock resistant as specified in the PN‐EN 1789+A2:2015‐01 "Medical vehicles and their equipment ‐ Road ambulances. " standard.

3.1.3 The detailed requirements for the transport defibrillator:

3.1.3.1 The transport defibrillator shall provide the defibrillation function, particularly:

3.1.3.1.1 both with respect to adults and children;

3.1.3.1.2 by means of single‐use adhesive electrodes;

3.1.3.1.3 manually and/or in a semi‐automatic manner;

3.1.3.1.4 using a biphasic waveform;

3.1.3.1.5 with a supplied energy at a range not lower than between: 2J and 200 J;

3.1.3.1.6 using an advisory mode (voice guidance) in the semi‐automatic mode of defibrillation.





1 2 3 4 53.1.3.2 The transport defibrillator shall provide the cardioversion function.

3.1.3.3 The transport defibrillator shall provide the pacing function, particularly:

3.1.3.3.1 external noninvasive;

3.1.3.3.2 using the permanent pacing mode and on‐demand stimulation mode;

3.1.3.3.3 using the stimulating impulses within a range of not lower than between: 40 imp/min and 170 imp/min;

3.1.3.3.4 using a stimulating current within a range of not lower than between: 0 mA and 140 mA.

3.1.3.4 The transport defibrillator shall provide the ECG monitoring function, particularly:

3.1.3.4.1 3‐lead and 12‐lead ECG;

3.1.3.4.2 arrythmia analysis (bradycardia and tachycardia) and the ST segment;

3.1.3.4.3 automatic interpretation and analysis of the ECG course of the curve;

3.1.3.4.4 displaying the ECG curve on the defibrillator screen;

3.1.3.4.5 print‐out of the displayed ECG curve;

3.1.3.4.6 automatic print‐out of the ECG course for critical events;

3.1.3.4.7 the augmentation of the ECG recording shall be adjustable.

3.1.3.5 The transport defibrillator shall provide the HR function:

3.1.3.5.1 the HR measurement within a range lower than between 30 and 240 beats per minute.

3.1.3.6 The transport defibrillator shall provide the blood oxygen saturation (SpO2) monitoring function:

3.1.3.6.1 the measurements shall be resistant to interference and motion artifacts;

3.1.3.6.2 measurement within a range not lower than between 50% and 99%.

3.1.3.7 The transport defibrillator shall provide the measurement function of: carboxyhaemoglobin (SpCO), methemoglobin (SpMet), total hemoglobin (SpHb).





1 2 3 4 53.1.3.8 The transport defibrillator shall provide the Non‐Invasive Blood Pressure (NIBP) function, particularly:

3.1.3.8.1 with respect to systolic blood pressure, diastolic blood pressure and mean blood pressure;

3.1.3.8.2 the measurement of the systolic blood pressure within a range not lower than between 40 mmHg and 240 mmHg;

3.1.3.8.3 the range of the diastolic blood pressure measurement shall not be lower than between 15mmHg and 200 mmHg;

3.1.3.8.4 the range of the mean blood pressure measurement shall not be lower than between 30mmHg and 220 mmHg;

3.1.3.8.5 with the following measurement modes: a) manual, b) automatic, in at least five (5) time intervals.

3.1.3.8.6 with oscillometric measurement.

3.1.3.9 The transport defibrillator shall provide the function of invasive blood pressure monitoring (IBP), particularly:

3.1.3.9.1 measurement using at least two (2) channels;

3.1.3.9.2 measurement within a range not lower than from ‐30mmHg through +300 mmHg;

3.1.3.9.3 pulse measurement within a range not lower than from 25 through 250 beats per minute.

3.1.3.10 The transport defibrillator shall provide the monitoring function with respect to body temperature measurement (core body temperature and percutaneous temperature):

3.1.3.10.1 the measurement shall be done within a range not lower than from +15 degrees Celsius through +45 degrees Celsius.

3.1.3.11 The transport defibrillator shall provide the monitoring function with respect to CO2 concentration in exhaled breath and respiratory rate (number of breaths per minute), particularly:

3.1.3.11.1 sidestream measurement with an intubated and non‐intubated patient monitoring function;

3.1.3.11.2 EtCO2 measurement within a range not lower than from 0 mmHg through 100 mmHg;

3.1.3.11.3 respiratory rate measurement within a range not lower than from 0 through 140;

3.1.3.11.4 capability of monitoring the EtCO2 curve on the screen with print‐out capability.





1 2 3 4 53.1.3.12 The transport defibrillator shall provide an alarm function, particularly:

3.1.3.12.1 signalisation for all monitored parameters;

3.1.3.12.2 memory function for limiting parameters for the main age groups.

3.1.3.13 The properties of the transport defibrillator screen:

3.1.3.13.1 displaying at least three (3) dynamic curves;

3.1.3.13.2 LCD display;

3.1.3.13.3 diagonal screen measurement of not less than 6.4";

3.1.3.13.4 operation mode: color.

3.1.3.14 The properties of the transport defibrillator printer:

3.1.3.14.1 the printer shall comprise an integral part of the device;

3.1.3.14.2 the width of the paper shall be at least 80 mm;

3.1.3.14.3 the number of channels that may be printed out at the same time shall be at least 3 (three);

3.1.3.14.4 the speed of the paper travel shall be 25mm/second and 50 mm/second.

3.1.3.15 The transport defibrillator shall provide the recording/storage function, particularly:

3.1.3.15.1 recording/storing the progress of the device operation, entering of patient data, patient condition, ECG curve sections, performed actions and events in the device memory with a print‐out function of such data;

3.1.3.15.2 the time trends with respect to all monitored parameters for at least 8 hours;

3.1.3.15.3 broadcasting all measured parameters from the defibrillator memory to the receiving device via a 3G modem or using Bluetooth technology;

3.1.3.15.4 it shall have a function allowing for blocking all wireless communication from the user level and/or as a factory default;





1 2 3 4 53.1.3.15.5 providing full compliance of the devices with the provisions of the Regulation (EU) 2016/679 of the European Parliament and

of the Council of 27 April 2016 on the protection of natural persons with regard to the processing of personal data and on the free movement of such data, and repealing Directive 95/46/EC (General Data Protection Regulation), particularly with respect to protection of the encrypted transmission of patient data, encryption of patient data in the device (using the higher‐level protocols e.g. the SHA256) and with respect to protection against unauthorized assess to patient data, located in the device.

3.1.3.16 The technical requirements/power source of the transport defibrillator:

3.1.3.16.1 mains and battery power supply as well as power supply from the aircraft power system ‐12V DC and/or 230V AC;

3.1.3.16.2 the electric capacity of the battery shall not be lower than 4 Ah;

3.1.3.16.3 the mean time of operation on battery (batteries) supply in the monitoring mode shall be at least 300 minutes;

3.1.3.16.4 at least 100 discharges on battery (batteries) supply with a discharge energy of not less than 200 J or highter;

3.1.3.16.5 displaying the battery charge level.

3.1.3.17 The weight of the device shall not exceed 10 kg.

3.1.3.18 Equipment:

3.1.3.18.1 batteries ‐ 4 pieces;

3.1.3.18.2 single‐use electrodes for ECG/defibrillation/cardioversion/cardiac stimultation for adults (20 pairs) and for children (10 pairs);

3.1.3.18.3 ECG patient 3‐lead cable ‐ 2 piecesThe Awarding Entity shall allow a 4‐lead cable if the manufacturer does not provide a 3‐lead cable with a given model;

3.1.3.18.4 ECG patient 12‐lead cable ‐ 1 piece;

3.1.3.18.5 SpO2 sensor (for different age groups, capable of measuring the parameters given in the specification) ‐ reusable;

3.1.3.18.6 temperature measurement sensor (core body temperature and percutaneous temperature);

3.1.3.18.7 a set of cuffs for NIBP for different age groups with a cable ‐ the full, available set;





1 2 3 4 53.1.3.18.8 EtCO2 measurement set:

a) for intubated patients ‐ 10 sets, b) for non‐intubated patients ‐ 3 sets.

3.1.3.18.9 set of single‐use IBP transducers ‐ 5 pieces;

3.1.3.18.10 printer paper ‐ 10 rolls;

3.1.3.18.11 a deployment bag for the device and accessories;

3.1.3.18.12 stationary device for loading and maintaining batteries;

3.1.3.18.13 software for transmitting data to a PC and for storing data;

3.1.3.18.14 all cables and other components which have not been listed hereinabove and which are necessary for the device to operate and to be powered;

3.1.4 Other requirements:

3.1.4.1 The transport defibrillator shall provide a communication function with the user in the Polish language (messages on the display and voice commands).







1 2 3 4 53.1.4.4 The disinfection liquids shall not have any adverse effects on the materials from which the components of the medical cabin,

the structure, internal finishing and aeroplane equipment are made, particularly: the stretcher, stretcher mounting base, walls, floor, glazed parts, seat belt and seat components, incubator along with a transport stand and stand‐mounted equipment, medical devices.

3.1.4.5 The Contractor shall, at his cost and expense, provide the training for two medical personnel groups of the Awarding Entity, in the Polish language, at the Awarding Entity's registered office, with respect to the operation of the portable medical equipment delivered by the Contractor with respect to the performance of the additional subject of the Agreement. The trainee groups shall consist of not more than 10 persons. The Contractor shall ensure that every trainee shall be issued with a written proof of training. The trainings shall take place on the dates agreed upon by the Parties hereto, nonetheless, not later than 1 week after the day the first aeroplane is handed over.

3.1.4.6 The time for commencing the repair by the service center shall not exceed 48 hours from the day the Awarding Entity notifies the service center.

3.1.4.7 The number of the repairs granting the right to have the device replaced with a new one shall be five (5).

3.1.5 Warranty:

3.1.5.1 At least for 24 months; the warranty period shall run from the day the device is delivered, as proven by the acceptance protocol.

State the offered warranty period in months.

3.1.6 Requirements concerning the documents required at the phase of the acceptance of the medical cabin design:

3.1.6.1 The Contractor shall submit a certificate of compliance for the subject of the order; i.e. the statement of the manufacturer or its authorized representative, stating under its own responsibility that the product is compliant with essential requirements.





1 2 3 4 53.1.6.2 The Contractor shall submit a certificate of compliance for the subject of the order issued by a notified body in order to be

obtain the CE mark.

3.1.6.3 The Contractor shall submit a folder/catalog/brochure/information/description of the manufacturer of the offered medical device, which shall contain technical data of such a device confirming that the characteristics described in this specification have been met and shall be in the Polish language in the electronic version allowing for copying and printing out.

3.1.6.4 The Contractor shall deliver a user's manual describing the device; said manual shall be in the Polish language in an electronic format allowing for copying and printing out.

3.1.6.5 The Contractor shall deliver a warranty card along with the warranty terms and conditions.

3.1.6.6 The Contractor shall deliver a written statement of an authorized warranty service center which provides warranty services in Poland; said statement shall prove that the delivered devices have been covered by warranty.





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3.2The transport incubator together with the mountings for the medical devices ‐ 2 sets (set no. 1 ‐ also with the NO therapy capability and the set no. 2 ‐ basic)

3.2.1. The set no. 1 shall comprise the following items in particular:

3.2.1.1 The incubator with the installed devices, including the incubator chamber along with the mattress and the patient mounting.

3.2.1.2 The incubator stand with the mountings for medical devices, listed in points 3.2.1.3‐3.2.1.8.

3.2.1.3 Two (2) composite gas systems (an oxygen one and an air one) with a volume of 4.7 liter each (which are not the subject of the order, but which will be rented by the Awarding Entity) or two (2) aluminum cylinders (an oxygen one, and an air one) with a volume of 2 liters each (which are not the subject of the order, but which will be rented by the Awarding Entity) along with the adapter allowing for connecting both types of gas tanks interchangeably.

3.2.1.4 The Hamilton T1 ventilator (which is not the subject of the order, but which will be rented by the Awarding Entity); in case of failure to meet the compatibility requirement of the Hamilton T1 ventilator with the NO therapy module (which is the subject of the order, and whose specification has been provided in point 3.4.), the Contractor shall deliver a different ventilator whose performance characteristics shall be similar to the Hamilton T1 ventilator and which shall be, at the same time, compatible with the NO module.

3.2.1.5 The Pneupac babyPAC 100 ventilator (which is not the subject of the order, but which will be rented by the Awarding Entity).The Awarding Entity does not foresee the simultaneous mounting of the Pneupac BabyPAC ventilator and Hamilton T1 ventilator.

3.2.1.6 The transport defibrillator (which is the subject of the order, and whose specification has been provided in point 3.1).

3.2.1.7 At least four (4) B.Braun Perfusor Space infusion pumps (which are not the subject of the order, but which will be rented by the Awarding Entity).





1 2 3 4 53.2.1.8 The nitric oxide therapy module (NO; which is the subject of the order, and whose specification has been provided in point

3.4) along with a cylinder with the volume of 2 liters of nitric oxide (which is not the subject of the order, but which will be rented by the Awarding Entity) and the dedicated cylinder mounting.

3.2.2 The set no. 2 shall comprise the following items in particular:

3.2.2.1 The incubator with the installed devices, including the incubator chamber along with the mattress and the patient mounting ‐ the same as in the Set no. 1.

3.2.2.2 The incubator stand with the mountings for medical devices, listed in points 3.2.1.3‐3.2.1.8.

3.2.2.3 The devices specified in point 3.2.1.3‐3.2.1.7.

3.2.3 The medical cabin of each delivered aeroplane shall be adapted to transport a transport incubator, particularly:

3.2.3.1 The system for incubator transportation (the transport stand with equipment) shall provide access to the incubator in a way that, after the system is installed in the aeroplane, the free space by the incubator, over the incubator and from the side of patient's head allows for opening and closing the incubator covers so as to remove the patient in an unrestricted manner.

3.2.3.2 The system for incubator transportation shall be adapted to the technical conditions specified by the incubator manufacturer and shall provide the possibility for supplying the incubator with the electrical current of 230V AC or 12V DC.

3.2.3.3 The system shall allow for easy switch over from the incubator's own power to the power fed by the electrical system of the aeroplane medical cabin.

3.2.3.4 The system shall allow for easy switch over from the incubator's own medical gas supply to the supply from the gas systems of the aeroplane medical cabin.





1 2 3 4 53.2.4 The system for transporting the incubator (the transport stand) shall have a mounting system, compliant with the aviation

regulations, for the devices listed in 3.2.1.3‐3.2.1.8, for both incubators, same as for the Set no. 1:

3.2.4.1 The location where the devices included in each Set shall be installed shall allow for the possibility of using all the functions of those devices, particularly for reading out the parameters from the panels of those devices by at least one member of the medical personnel at any phase of the flight.

3.2.4.2 The devices which are included in each Set shall be installed in the immediate vicinity of the incubator on the transport stand at a distance that shall allow for their use and in a location that shall not hinder the loading/transportation/unloading of the patient.

3.2.4.3 There shall be provided an easy and fast dismounting/removal and mounting/fastening of the devices included in each Set without using any additional tools.

3.2.4.4 The design of the system for incubator transportation (transport stand) shall provide the possibility of universal mounting of the system to the stretcher in the ground ambulances of Polish emergency medical systems in a manner that shall ensure safe transportation of the patient in the incubator for the purpose of performing the 'bed‐to‐bed' transportation using the stand compatible with the mounting system in the aeroplane.

3.2.4.5 The design of the system for incubator transportation (transport stand) shall have the attachable wheels allowing for easy movement of the incubator over the surface outside the aeroplane in two (2) axes.The casters and fitted with a break/locking system.

3.2.4.6 The layout of the medical devices attached to the transport stand shall not significantly increase the vertical dimension of the whole incubator, therefore, said layout shall also envision the installation of the devices in the horizontal dimension (i.e. by the main incubator chamber) in order to maximally lower the centroid.





1 2 3 4 53.2.5 The detailed requirements concerning the incubator:

3.2.5.1 The weight of the Set no. 1 shall not exceed 150 kg.

3.2.5.2 The dimensions of the set shall allow for uninhibited loading/unloading from the aeroplane without any risk of damage to the components of the set and the aircraft.

3.2.5.3 The hood (canopy) of the incubator shall be double‐wall.

3.2.5.4 The walls of the hood (canopy) shall be openable in order to provide access to the patient from at least the patient side and from the side of patient's head.

3.2.5.5 There shall be provided a possibility for sliding out the patient on the mattress quickly from the side of the patient's head in order to perform rescue actions (e.g. carry out the intubation).

3.2.5.6 The incubator shall be fitted with at least two (2) hand ports for attending to the patient.

3.2.5.7 The incubator shall be equipped with at least four (4) access ports for drains and the set of respirator tubes.

3.2.5.8 The battery operating time shall allow for at least 90 minutes of operation.

3.2.5.9 The incubator shall be fitted with a built‐in pulse oximeter.

3.2.5.10 The incubator shall have the adjustment function with respect to the temperature inside the hood (canopy), particularly:

3.2.5.10.1 temperature setting function with respect to the inside of the hood (canopy); the adjustment shall be from 22 degrees C through 38 degrees C;

3.2.5.10.2 the increments of the temperature adjustment shall be 0.1 degree C;





1 2 3 4 53.2.5.10.3 temperature measuring function with respect to the inside of the hood (canopy); the measurement shall be from 20 degrees

C through 42 degrees C;

3.2.5.10.4 the patient skin temperature sensor, allowing for the measurement within a range from 30 degrees C through 42 degrees C;

3.2.5.11 The incubator shall have a function for setting the concentration of oxygen under the hood (canopy) within a range from 21% through 50%.

3.2.5.12 The incubator shall be fitted with a humidifier under the hood (canopy).

3.2.5.13 The incubator shall be fitted with a display presenting the following data:

3.2.5.13.1 on/off status;

3.2.5.13.2 battery charge status;

3.2.5.13.3 AC/DC power supply;

3.2.5.13.4 patient temperature;

3.2.5.13.5 the air temperature under the hood (canopy);

3.2.5.13.6 SpO2 ‐ a read‐out from the pulse oximeter.

3.2.5.13.7 HR (heart rate) ‐ a read‐out from the pulse oximeter;

3.2.5.13.8 alarm indicators.

3.2.5.14 The incubator shall have alarms warning about the following issues:

3.2.5.14.1 system failure;

3.2.5.14.2 temperature sensor failure;

3.2.5.14.3 excessively low temperature;





1 2 3 4 53.2.5.14.4 excessively high temperature;

3.2.5.14.5 weak battery;

3.2.5.14.6 power supply failure;

3.2.5.14.7 internal air circulation interruption.

3.2.5.15 The incubator shall have a function for muting the alarms.

3.2.5.16 The incubator shall be fitted with a system for securing the patient; said system shall allow for safe transportation of the patient.


3.2.6.1 The incubator shall allow for communication with the user in the Polish and/or English language (messages on the display and voice commands) ‐ if so envisioned by the manufacturer.








1 2 3 4 53.2.6.5 The Contractor shall, at his cost and expense, provide the training for two medical personnel groups of the Awarding Entity, in

the Polish language, at the Awarding Entity's registered office, with respect to the operation of the portable medical equipment delivered by the Contractor with respect to the performance of the additional subject of the Agreement. The trainee groups shall consist of not more than 10 persons. The Contractor shall ensure that every trainee shall be issued with a written proof of training. The trainings shall take place on the dates agreed upon by the Parties hereto, nonetheless, not later than 1 week after the day the first aeroplane is handed over.

3.2.7 Warranty:

3.2.7.1 Shall not be shorter than 12 months, and shall run from the day the device is delivered, as proven by the acceptance protocol. State the offered warranty period in months.



3.2.8.2 The Contractor shall submit a certificate of compliance for the subject of the order issued by a notified body in order to be obtain the CE mark.







1 2 3 4 53.2.8.5 The Contractor shall deliver a warranty card along with the warranty terms and conditions.






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3.3 Oxygen flowmeter with a regulator ‐ 2 (two) sets3.3.1 General requirements concerning the oxygen flowmeter with a regulator:

3.3.1.1 It shall be capable of being connected to the AGA wall‐mounted socket.

3.3.1.2 There shall be mountings provided in the immediate vicinity of the patient in order to perform oxygen therapy.

3.3.1.3 Detailed requirements concerning the oxygen flowmeter with a regulator: a) the supply pressure of the oxygen flowmeter shall be between 4 and 5 bar, b) the oxygen flow adjustment range shall be from 0 through 15 l/min










1 2 3 4 53.3.3 Warranty:3.3.3.1 Shall not be shorter than 12 months, and shall run from the day the device is delivered, as proven by the acceptance protocol. State the

offered warranty period in months.












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3.4 Module for nitric oxide (NO) therapy ‐ 1 (one) set3.4.1 Detailed requirements for the module for nitric oxide (NO) therapy:

3.4.1.2 It shall be capable of being supplied with nitric oxide (NO) from the 800 ppm cylinder with 2‐liter capacity, compliant with the CGA626 standard.

3.4.1.3 It shall be capable of delivering NO by inhalation continuously.

3.4.1.4 It shall be capable of working with the Hamilton T1 ventilator (which is not the subject of the order, but which will be rented by the Awarding Entity); in case of failure to meet the compatibility requirement with the Hamilton T1 ventilator the Contractor shall deliver a different ventilator whose performance characteristics shall be similar to the Hamilton T1 ventilator, but which shall be, at the same time, compatible with the NO module.

3.4.1.5 It shall allow for continuous monitoring of NO, NO2, and O2 concentration in the breathing mixture using a sampling line.

3.4.1.6 It shall have a sampling line.

3.4.1.7 It shall operate in the ambient environment conditions in the following ranges:

3.4.1.7.1 temperature: from +5 degrees C through +39 degrees C;

3.4.1.7.2 pressure: from 65 kPa through 110 kPa.

3.4.1.8 It shall have a display presenting the current gas parameters and the battery charge level.

3.4.1.9 It shall have alarms with respect to the breathing mixture supply line; said alarms shall be triggered in the event of:

3.4.1.9.1 high concentration of NO;

3.4.1.9.2 low concentration of NO;

3.4.1.9.3 low concentration of O2;

3.4.1.9.4 high concentration of NO2.

3.4.1.10 It shall have battery power supply ensuring at least 4 hours of continuous operation.

3.4.1.11 It shall be capable of being connected to the external power source of 230 VAC.

3.4.1.12 The weight shall not exceed 5.5 kg.





1 2 3 4 53.4.2 Other requirements:





3.4.3 Warranty:

3.4.3.1 Shall not be shorter than 12 months, and shall run from the day the device is delivered, as proven by the acceptance protocol. State the offered warranty period in months.





1 2 3 4 53.4.4 Requirements concerning the documents required at the phase of the acceptance of the medical cabin design:








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