Νόμοι — ΦΕΚ A' 3/2025

MAINTENANCE TRACKING PROGRAM The Aircraft will deliver with an online computerized maintenance record service for one year from the date the Aircraft is delivered to the Purchaser. This service provides management and operations personnel with the reports necessary for the efficient control of maintenance activities. The service provides an accurate and simple method for staying abreast of aircraft components, inspections, service bulletins, and airworthiness directives while providing aircraft records of maintenance performed. On demand reports show the current status, upcoming scheduled maintenance activity, and historical aircraft maintenance. Semi-annual reports concerning projected annual maintenance requirements, component removal history, and fleetwide component reliability are provided as part of the service. Services are provided through a secure Internet site and require a computer with Internet connectivity. A local printer is required to print paper versions of the online reports and documentation.

LIMITED WARRANTIES The Seller’s King Air® 360C Limited Aircraft Warranty (Limited Aircraft Warranty) covers the Aircraft structure (defined below) other parts of the Aircraft not included in the definition of Aircraft Structure, Avionics hardware and software as noted below, Exterior Paint and Interior Finish items. The engines are warranted by Pratt and Whitney® Canada Corp. (P&WC). The propellers are warranted by Hartzell Propeller Inc. (Hartzell). The Limited Aircraft Warranty and summaries of P&WC new engine and Hartzell new propeller limited warranties are set out below. Available post-delivery: 21 K IN G AIR 3 6 0 C UTILITY IN TERIO R · O CTO BER 2 0 2 3 The Seller warrants each new King Air® 360C to be free from defects in material and workmanship for the following periods after delivery of the Aircraft to the Purchaser. (a) Five years on Aircraft Structure (fuselage, empennage, wing and control surfaces); and (b) Two years or 1,200 operating hours, whichever occurs first, for each part of the Aircraft not mentioned in (a) above, except avionics hardware and avionics software, engines and propellers; (c) Five years for standard Collins Aerospace® Avionics hardware and one year for Collins Aerospace® avionics software; and (d) Two years or 400 operating hours, whichever occurs first, for Exterior Paint and Interior Finish items. Any remaining term of this Limited Aircraft Warranty automatically transfers to subsequent purchasers of the Aircraft. Definitions Support Facility means Textron Aviation Parts Distribution, Textron Aviation-owned service facilities, and service facilities authorized by Textron Aviation to perform warranty service on the Aircraft. Service Facility means Textron Aviation-owned service facilities and service facilities authorized by Textron Aviation to perform warranty service on the Aircraft. Warranty Plolder means Aircraft owner. Seller’s Obligation Parts Seller’s obligation under this Limited Aircraft Warranty is limited to repairing the defective part or replacing the defective part with an exchange part, in Seller’s sole discretion, when: (a) the failure occurs within the applicable warranty period; (b) all of the following occur within 30 days of failure for a U.S. Warranty Holder and 45 days of failure for an international Warranty Holder: KING AIR 3 6 0 C UTILITY INTERIOR * OCTOBER 2 0 2 3 22 Facility from where the replacement part is procured; and (iii) the return part is accompanied by the Textron Aviation issued Return Authorization; and (c) the Support Facility identifies the part and determines the part is defective. The Seller may refuse a warranty claim not submitted within the above time frame. Replacement parts are only warranted for the remainder of the applicable, original Limited Aircraft Warranty period. In other words, a new warranty period is not established for replacement parts. No Aircraft part or equipment will be regarded as breaching this Limited Aircraft Warranty merely because, subsequent to its delivery, some modification or alternation becomes necessary for product improvements or in order to meet a change in the requirements of applicable Federal Aviation Regulations. Service Service under this Limited Aircraft Warranty must be performed at a Service Facility. The Warranty Holder will not be charged for parts or labor covered by this Limited Aircraft Warranty. The location of Service Facilities is available on the Seller’s website. Warranty Holder’s Responsibility All freight, transportation expenses, import duties, customs brokerage fees, sales taxes and use taxes, if any, on warranty repairs or replacement parts are the Warranty Holder’s sole responsibility. The Warranty Holder is responsible for the cost of getting the Aircraft to and from a Service Facility. Application This Limited Aircraft Warranty applies to Aircraft operated under normal, conventional, non-military use. It applies only to the repair or replacement of defective parts that have been used, maintained, and operated in accordance with the Federal Aviation regulations and the applicable manuals, bulletins, communications, or other written instructions of the Aircraft or component manufacturers. 23 KIN G AIR 3 6 0 C UTILITY INTERIO R · OCTOBER 2 0 2 3 (a) normal maintenance services (such as engine adjustments, cleaning, control rigging, brake and other mechanical adjustments, and maintenance inspections); (b) the replacement of service items (such as brakes, lights/bulbs, filters, de-ice boots, hoses, belts, tires, batteries, rubber-like items, fuel or lubricants); (c) normal deterioration of appurtenances (such as paint, cabinetry, and upholstery); (d) damage due to wear, exposure, environmental elements, and neglect; (e) parts, components or systems that have been modified or altered after delivery other than by the Aircraft manufacturer or in accordance with an alternation scheme approved in writing by Textron Aviation; (f) items that have been subjected to misuse, abuse, negligence, accident, foreign object damage (FOD); (g) items that have been installed, repaired, or altered by repair facilities not authorized by Textron Aviation; (h) items that, in Textron Aviation’s sole discretion, have been installed, repaired, or altered by other than Textron Aviation-owned service facilities contrary to applicable manuals, bulletins, and other written instructions provided by Textron Aviation so that the performance, stability, or reliability of such items are adversely affected; (i) any part or system that has been modified or altered by a third party at the Warranty Holder or its predecessor’s request and any part or system of the Aircraft affected by such modified or altered part or system; (j) vendor subscription services (including for items covered by the Limited Aircraft Warranty), software (except as specifically set out herein) and databases (collectively “Services”), and patches, replacements, revisions, updates or upgrades thereto (collectively “Updates”) and any impairment to the Aircraft or its components caused by Services or Updates; and (k) Warranty Holder or predecessor’s furnished equipment. The warranty provided for life-limited parts is pro-rated. For Aircraft components, parts, or systems with life limitations Seller’s liability under this Limited Aircraft Warranty is limited to the remaining pro-rated life of the defective part, calculated as of the date the defect is discovered and reported to Seller and per additional K IN G AIR 3 6 0 C U TILITY INTER IO R · O CTO BER 2 0 2 3 24 applicable Periods set out above. All warranty Periods expires as noted above, regardless of any remaining life limits on parts. WITH THE EXCEPTION OF THE WARRANTY OF TITLE AND TO THE EXTENT ALLOWED BY APPLICABLE LAW, THIS LIMITED AIRCRAFT WARRANTY IS EXPRESSLY IN LIEU OF ANY OTHER WARRANTIES, EXPRESSED OR IMPLIED, IN FACT OR BY LAW, APPLICABLE TO THE AIRCRAFT THERE ARE NO WARRANTIES WHICH EXTEND BEYOND THE DESCRIPTION ON THE FACE HEREOF. SELLER SPECIFICALLY DISCLAIMS AND EXCLUDES ALL OTHER WARRANTIES, INCLUDING, BUT NOT LIMITED TO, ANY IMPLIED WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE. THE REMEDIES OF REPAIR OR REPLACEMENT OF THE DEFECTIVE PART(S) AS SET OUT HEREIN ARE THE ONLY REMEDIES UNDER THIS LIMITED AIRCRAFT WARRANTY. SELLER EXPRESSLY AND SPECIFICALLY DISCLAIMS ALL OTHER REMEDIES, OBLIGATIONS, AND LIABILITIES, INCLUDING, BUT NOT LIMITED TO, LOSS OF AIRCRAFT USE, LOSS OF TIME, INCONVENIENCE, COMMERCIAL LOSS, LOSS OF PROFITS, LOSS OF GOODWILL, DIMUNITION OF MARKET VALUE, AND ANY AND ALL OTHER CONSEQUENTIAL, INDIRECT, INCIDENTAL, SPECIAL, MULTIPLE OR PUNITIVE DAMAGES, OR ANY DAMAGES TO THE AIRCRAFT CLAIMED BY PURCHASER OR ANY OTHER PERSON OR ENTITY UPON THE THEORIES OF NEGLIGENCE OR STRICT LIABILITY IN TORT. SELLER NEITHER ASSUMES NOR AUTHORIZES ANYONE ELSE TO ASSUME ON ITS BEHALF ANY FURTHER OBLIGATIONS OR LIABILITY PERTAINING TO THE AIRCRAFT NOT CONTAINED IN THIS LIMITED AIRCRAFT WARRANTY. THIS LIMITED AIRCRAFT WARRANTY WILL BE CONSTRUED UNDER THE LAWS OF THE STATE OF KANSAS AND ANY DISPUTES AND/OR CLAIMS ARISING THEREFROM WILL BE EXCLUSIVELY RESOLVED IN THE STATE AND/OR FEDERAL COURTS LOCATED IN WICHITA, KANSAS. THE PARTIES CONSENT TO PERSONAL JURISDICTION IN THE FORUM CHOSEN AND WAIVE THEIR RIGHT TO JURY TRIAL. ANY ACTION BY PURCHASER FOR BREACH OF THIS WARRANTY MUST BE COMMENCED WITHIN ONE (1) YEAR AFTER THE CAUSE OF ACTION ACCRUES. THE CAUSE OF ACTION ACCRUES WHEN THE PURCHASER FIRST LEARNS THAT THE WARRANTY HAS BEEN BREACHED. 16.2 Summary of P&WC’s New Engine Limited Warranty The Aircraft engines are warranted by P&WC. The following is a summary of the P&WC warranty for new PT6A engines. Please refer to the P&WC warranty documentation for complete terms and conditions. If there is an inconsistency between the summary provided herein and complete P&WC warranty documentation, the latter controls. 25 K IN G AIR 3 6 0 C UTILITY INTERIO R · O C TOBER 2 0 2 3 years [after delivery to the first operator], whichever occurs first, during which time P&WC will: at its option, repair or replace any Engine parts found to be defective including resultant damage to the Engine. Replacement parts may be new or serviceable. When P&WC supplies a replacement part, or issues credit towards the acquisition of a new part, the removed part becomes the property of P&WC. pay reasonable removal and reinstallation labour for the Engine or Engine parts, and reasonable transportation charges (excluding insurance, duties, brokerage fees, and taxes) to and from the facility designated by P&WC Warranty Administration. Following the expiration of the Basic Coverage Period, P&WC offers the Primary Parts Service Policy (“PPSP”) and the Extended Engine Service Policy (“EESP”),which it may cancel or change at any time. W hat is not covered Costs of normal scheduled maintenance services routine line maintenance and adjustment costs; or Hot Section Inspection (HSI) and refurbishment costs; or Engine overhaul or major refurbishment costs; and any other costs related to Engine maintenance not specifically covered under this Policy. Normal deterioration normal wear and tear and deterioration (note: a worn part capable of continued operation which, because it has been accessed, must be restored using repair schemes fully described in the applicable P&WC Engine Maintenance and/or Overhaul Manuals, is considered normal); and no warranty coverage is provided for the overhaul life of assemblies, service live limits of parts, and/or operating time limits. Unsupported parts P&WC reserves the right to exclude Policy coverage (i) for the following parts, and (ii) for subsequent Engine repairs or damages directly attributable to the use of the following parts which: K IN G AIR 3 6 0 C UTILITY IN TERIO R · O C TO BER 2 0 2 3 26 Department of Transport Certificate of Airworthiness, as applicable; or are not identified in the applicable P&WC Illustrated Parts Catalogue (“IPC”) and accompanied by the Supplier’s Release Certificate; or are not repaired in accordance with P&WC approved repair processes; or are not traceable, e.g. insufficient supporting documentation; and have been involved in an accident and for other part or Engine failure attributable to that part. Factors beyond P&WC’s control improper storage, usage, maintenance or operation of an Engine, part or accessory (e.g. non-compliance with P&WC’s written instructions, including without limitation, the applicable P&WC Engine Maintenance and Overhaul Manuals, P&WC Service Bulletins, or with the Aircraft Flight Manuals, and airworthiness regulations); any work performed on Engines without due cause, such as pre-purchase inspections, or scheduled maintenance performed at other than P&WC recommended intervals; accidents, collisions, propeller strikes, fire, flood, lightning strike, theft, explosion, riot, war, rebellion, seizure or any other belligerent acts, foreign object damage (FOD), erosion, corrosion, sulphidation or any other damage due to the operating environment; alteration to, modification of, or tampering with any Engine, part or accessory after delivery by P&WC, other than strictly in accordance with the applicable P&WC manuals and this Policy; use of stolen parts, or use of a part or Engine from which P&WC’s name, part number, identification mark or serial number has been removed or defaced; workmanship performed by a facility other than P&WC-owned manufacturing facilities; repair or overhaul of a defective part or Engine at a facility other than a facility designated by P&WC Warranty Administration; unused cycles (stub life) of an LCF part removed at the operator’s request prior to reaching the service limit; 2 7 K IN G A IR 3 6 0 C U TILITY IN TE R IO R · O C TO B ER 2 0 2 3 used in operations or on flight missions which compromise Engine or parts life or reliability when compared to typical commercial, corporate, or private transportation operations; insurance, duties, brokerage fees, and taxes; any other factor beyond P&WC’s control which is not specifically listed herein. In addition, as all of the above are considered to be factors beyond P&WC’s control, no pro-rata credit per the PPSP will be awarded on Primary Parts replaced, repaired, or exchanged following access to the Engine due to any of the above. Owner/operator responsibilities The coverage provided herein is subject to the following conditions: Maintenance The Engine must be operated and maintained in accordance with P&WC’s written instructions including, without limitation, the applicable P&WC Engine Maintenance and Overhaul Manuals, P&WC Service Bulletins, as well as the Aircraft Flight Manual and airworthiness regulations. Maintenance records Adequate records of Engine operation and maintenance must be kept. Upon request, P&WC is entitled to have access to such records. For Warranty service P&WC must be notified of any Defect within thirty (30) days of discovery, and any claim must be submitted within one hundred and eighty (180) days after such discovery. Any claim, which may include the return of defective parts, must be made through the P&WC source of supply (identified in the applicable P&WC IPC), or the P&WC designated facility or distributor which will furnish or has furnished the replacement parts. For any warranty work (including, without limitation, disassembly), the Engine must be sent to a facility designated by P&WC Warranty Administration, in accordance with P&WC’s written instructions. Any work performed at a facility other than a facility designated by P&WC Warranty Administration, without prior written authorization from P&WC Warranty Administration, will be at the claimant’s expense. K IN G AIR 3 6 0 C U TILITY IN TE RIO R · O CTO BER 2 0 2 3 2 8 ENGINES IDENTIFIED ON THE TITLE PAGE OF THIS DOCUMENT, INSTALLED IN TEXTRON AVIATION INC. AIRCRAFT AND OPERATED IN NON-MILITARY AIRCRAFT USED IN COMMERCIAL, CORPORATE, OR PRIVATE TRANSPORTATION SERVICE, AND IS GIVEN AND ACCEPTED IN PLACE OF ALL OTHER EXPRESS, IMPLIED OR STATUTORY TERMS, REPRESENTATIONS, WARRANTIES OR CONDITIONS, IN CONTRACT OR IN TORT, INCLUDING W ITHO UT LIMITATION, ANY WARRANTY OR CO NDITIO N OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE AND ALL SUCH OTHER TERMS, REPRESENTATIONS, WARRANTIES OR CONDITIONS ARE HEREBY EXPRESSLY DISCLAIMED. THE ONLY REMEDY FOR BREACH OF THIS WARRANTY IS AS SET OUT HEREIN. FOR GREATER CERTAINTY, IN NO EVENT SHALL P&WC BE RESPONSIBLE FOR ANY SPECIAL, INCIDENTAL OR CONSEQUENTIAL DAMAGES ARISING OUT OF OR IN CONNECTION WITH EITHER A BREACH OF THIS WARRANTY OR ANY TORTIOUS OR NEGLIGENT ACT OR OMISSION BY P&WC. SPECIAL, INCIDENTAL, OR CONSEQUENTIAL DAMAGES INCLUDE, W ITHOUT LIMITATION, ECONOMIC LOSS, LOSS OR DAMAGE TO ANY PROPERTY OR PERSON OR ANY OTHER EXEMPLARY, PUNITIVE OR SIMILAR DAMAGES, AS WELL AS EXPENSES INCURRED EXTERNAL TO THE ENGINE AS A RESULT OF AN ENGINE OR PART DEFECT. NO VARIATION OR EXTENSION OF THIS WARRANTY OR REMEDIES SHALL BE BINDING UNLESS IN W RITING AND SIGNED BY A DULY AUTHORIZED REPRESENTATIVE OF P&WC. YOUR ACCEPTANCE OF THIS ENHANCED WARRANTY FOR NEW ENGINES AND SERVICE POLICIES OR THE MAKING OF ANY CLAIM OR RECEIPT OF ANY BENEFIT HEREUNDER, CONSTITUTES YOUR ACCEPTANCE OF ALL THE FOREGOING TERMS, CONDITIONS AND LIMITATIONS. THIS WARRANTY IS GOVERNED BY THE LAWS OF THE PROVINCE OF ONTARIO, CANADA. This policy follows the Engine to subsequent owners, if applicable please notify P&WC. If you have any questions or require assistance regarding this Policy, please call or write to: Manager, Warranty Administration Pratt & Whitney® Canada Corp. 1000 Marie-Victorin Longueuil, Quebec, Canada, J4G 1A1 Telephone: 1 450 647-8180 Fax: 1 450 647-2831 Email: warranty@pwc.ca 29 K IN G AIR 3 6 0 C UTILITY IN TERIO R · O CTOBER 2 0 2 3 The following is a summary of the Hartzell warranty for new propellers. Please refer to applicable Hartzell warranty documentation for complete terms and conditions. If there is an inconsistency between the summary provided herein and complete Hartzell warranty documentation, the latter controls. HARTZELL PROPELLER INC. LIMITED WARRANTY FOR COMPONENTS OF A PRODUCT INSTALLED BY TEXTRON AVIATION INC. COVERAGE PROVIDED Products installed at Textron Aviation Inc. on King Air® 360C Aircraft. Hartzell Propeller Inc. (“Hartzell”) warrants that it will repair or replace defects in material or workmanship in the components of a product manufactured by Hartzell and installed by Textron Aviation Inc. on the King Air® 360C aircraft, including a de-ice boot, for a period of thirty-six (36) months from the date the product is first placed into service, or for the first 2,000 operating hours of use of the product, whichever occurs first, subject to the other terms and conditions of this limited warranty. All of the products identified above are hereinafter referred to as the “Products,” and their components hereinafter referred to as “Components.” DISCLAIMER OR LIMITATION OF WARRANTIES Unless prohibited by applicable law, and except for the limited warranties set forth above, Hartzell hereby disclaims any and all express and implied warranties, including but not limited to implied warranties of merchantability and fitness for a particular purpose. In the event disclaimer of implied warranties is not perm itted under applicable law, such implied warranties, including but not limited to implied warranties of merchantability and fitness for a particular purpose, are limited in duration and in scope of coverage to the duration and scope of coverage of the limited warranty. Some states do not allow limitations on how long an implied warranty lasts, so above limitation may not apply to you. TERMS AND CONDITIONS OF LIMITED WARRANTY COVERAGE In order to obtain coverage under Hartzell’s limited warranty, the Purchaser must notify Hartzell in writing of the warranty claim as soon as possible after obtaining knowledge of the potential claim, and in any event not later than ten (10) days following expiration of the limited warranty. Hartzell may withhold warranty repairs pending proof from Purchaser of the date the Product was placed into service, KIN G AIR 3 6 0 C UTILITY INTER IOR · O CTOBER 2 0 2 3 30 Purchaser describing the alleged defect. All initial transportation and handling charges must be prepaid by the Purchaser until warrantability is determined by Hartzell, at which time Hartzell may reimburse none, some, or all of these charges, at Hartzell’s discretion. In the event Hartzell determines, at its sole discretion, that the Product or Component thereof is covered under the limited warranty, Hartzell shall, at its election, either: (1) Have the Product or Component repaired and returned to Purchaser; (2) Deliver to Purchaser a replacement Product or Component; or (3) Issue a credit to the Purchaser in the amount of the actual purchase price for the Product. Hartzell reserves the right to replace Products or Components with remanufactured or re designed Products or Components of substantially equivalent quality. All warranty repair work will be accomplished at Hartzell’s principal place of business, a Hartzell Recommended Service Facility, or a third-party location pre-approved in writing by Hartzell. In the event Hartzell determines that the alleged defect is not covered by the limited warranty, the Product or Component will be returned to Purchaser, as is, transportation and handling charges collect. The only remedies under this limited warranty are as set forth above. Any Product repaired, or replacement Product provided, shall retain the balance of the limited warranty provided for herein. This limited warranty is not transferable to any person or entity. This limited warranty does not extend to future performance of a Product. WHAT IS NOT COVERED BY THIS LIMITED WARRANTY This limited warranty does not provide coverage for any of the following:

Normal maintenance and service.

Consumable Products and Components, and Products and Components that have reached the end of their normal usable life.

Product components not manufactured by Hartzell, which components may or may not be covered under warranties made by the manufacturers of those components.

Products and Components not purchased through Hartzell or one of its authorized distributors, or any Products or Components purchased by way of auction, salvage, or repossession.

Conditions, damage, or issues caused by, in whole or in part, or in any way related to: a. Accident, misuse, theft, or negligence. 31 K IN G AIR 3 6 0 C U TILITY IN T E R IO R · O C T O B ER 2 0 2 3 c. Alteration or modification of the Products or any Components. d. Acts of God or other environmental conditions. e. Use of the Products for purposes other than their normal use. f. Failure to seek and obtain warranty coverage in a timely matter. g. Deterioration or fading due to wear, exposure, or other cause, including but not limited to rust, cosmetic blemishes, and discoloration. h. Acts or omissions of any person or entity other than Hartzeil. DISCLAIMER OF INCIDENTAL AND CONSEQUENIAL DAMAGES HARTZELL HEREBY DISCLAIMS ANY AND ALL INCIDENTAL, CONSEQUENTIAL, SPECIAL, DIRECT, AND INDIRECT DAMAGES ARISING OUT OF OR RELATING TO THE PRODUCTS, INCLUDING BUT NOT LIMITED TO LOSS OF USE, INCONVENIENCE, LOST PROFITS, COVER, RENTAL REPLACEMENTS, COSTS AND EXPENSES OF “TROUBLESHOOTING,” AND TRANSPORTATION AND DELIVERY EXPENSES NOT PRE APPROVED IN WRITING BY HARTZELL. IN NO EVENT SHALL HARTZELL’S LIABILITY WITH RESPECT TO ANY PRODUCT, WHETHER UNDER THIS LIMITED WARRANTY, ANY IMPLIED WARRANTY, IN TORT, OR OTHERWISE, EXCEED THE PRICE PAID BY PURCHASER FOR THE PRODUCT. THESE DISCLAIMERS ARE INDEPENDENT OF ANY FAILURE OF THE ESSENTIAL PURPOSE OF ANY WARRANTIES OR REMEDIES PROVIDED TO PURCHASER, AND SHALL SURVIVE ANY DETERMINATION THAT A WARRANTY OR REMEDY FAILED OF ITS ESSENTIAL PURPOSE. SOME STATES DO NOT ALLOW THE EXCLUSION OR LIMITATION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATION OR EXCLUSION MAY NOT APPLY TO YOU. STATUTE OF LIMITATIONS No action may be brought against Hartzeil for breach of its limited warranty, any applicable implied warranty, or for any other claim relating to the Product, more than ten (10) days after expiration of the applicable limited warranty period. GOVERNING LAW This limited warranty shall be governed by, construed, and enforced in accordance with the laws of the State of Ohio, without reference to conflict of law principles. The United Nations Convention on Contracts for the International Sale of Goods shall not apply to this limited warranty. K IN G AIR 3 6 0 C U TILITY INTERIOR · OC TOBER 2 0 2 3 32 any warranties or representations on behalf of Hartzell. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, AND YOU MAY ALSO HAVE OTHER RIGHTS W HICH VARY FROM STATE TO STATE. Hartzell Propeller Inc. One Propeller Place Piqua, Ohio 45356 Phone: 937-778-4320

TRAINING AGREEMENT The first retail Aircraft Purchaser will be provided training for one (1) King Air® 360C crew, subject to the following:

A crew consists of up to two (2) current private or commercial licensed pilots with instrument and multi-engine ratings and one (1) mechanic with an A&P license or equivalent experience (each hereinafter referred to as a “Trainee” or collectively as “Trainees”).

Training will be conducted by Flight Safety International through Flight Safety Textron Aviation, Seller’s preferred training provider (or by Seller or another designated training organization, in Seller’s discretion), at the location designated by Seller. The organization providing training will be referred to as the “Trainer.”

Training will consist of the following: a. Ground school training for each pilot Trainee and theoretical classroom instruction for the mechanic Trainee in accordance with the Trainer’s standards. b. Except as set out below, pilot Trainees will be provided flight simulation training to simulator proficiency in accordance with the Trainer’s standards but not to exceed one (1) additional simulator session per pilot crew. i. A simulator that is certified will be used to provide training for the model BE-300 type rating and in lieu of a model specific simulator, training may be provided in the most appropriate type simulator available that is capable of accomplishing FAAtype rating with differencestraining provided. In Seller’s sole discretion and in accordance with Seller’s terms (including Purchaser’s cost), alternate pilot training may be provided if warranted by extraordinary circumstances. 33 K IN G A IR 3 6 0 C U T ILIT Y IN T E R IO R · O C T O B E R 2 0 2 3 and conditions established by the Trainer or Seller; b. Transportation of the Trainees to and from the training site and for all living expenses associated with the training; c. Providing an interpreter during the course of training for any of the Trainees not conversant in the English language; d. Extra charges, if any, for scheduling pilot Trainees in separate training classes; e. Reimbursing Seller at the retail rate for training provided if the Aircraft to be purchased by Purchaser does not deliver to Purchaser; and f. Ensuring compliance with TSA regulations including requirements that all current United States citizens present a current United States passport before training can start.

All training furnished under this Training Agreement will be scheduled to commence no earlier than three (3) months prior to Aircraft delivery and must be completed within twenty-four (24) months after the earlier of (a) Aircraft delivery or (b) commencement of the first training event for the Aircraft.

Seller or Trainer will schedule all training, furnish Purchaser training schedules and endeavor to schedule training at a time convenient for Purchaser. A rescheduling fee of five percent (5%) of the retail price of training a Trainee was scheduled to attend will be paid to Seller by Purchaser within thirty (30) days of the date of Seller’s invoice if a Trainee fails to appear for scheduled training, except for reasons beyond the Trainee’s control, unless Purchaser gives Seller written notice of cancellation received at least twenty-one (21) days prior to the scheduled training. For avoidance of doubt, this rescheduling fee applies to each Trainee who fails to attend training as scheduled and the exceptions to the rescheduling fee do not apply.

Neither Seller nor Trainer will be responsible for any delay in providing training.

Neither Seller nor Trainer will be responsible for the competency of any Trainee during and after training. Trainer will make the same efforts to qualify each Trainee as it makes in training other trainees; however, neither Seller nor Trainer can guarantee that any Trainee will qualify for any license, certificate or rating.

This Training Agreement is part of the Specification and Description and thus part of the Aircraft Purchase Agreement. Purchaser’s execution of the Aircraft Purchase Agreement constitutes Purchaser’s acceptance of the foregoing terms and conditions of the Training Agreement and Purchaser’s agreement that Seller can provide Purchaser’s name, address, the name and address of each Trainee and other relevant information to the Trainer for purposes of scheduling training. K IN G AIR 3 6 0 C UTILITY INTERIO R · O C TO BE R 2 0 2 3 34 U.S. + 1.844.44.TXTAV I INTERNATIONAL +1.316.517.8270 I TXTAV.COM © 2023 Textron Aviation Inc. All rights reserved. Product names, company names, trademarks, service marks, trade names, trademark designs and logos of Textron Aviation Inc. or its subsidiaries (collectively Marks ), whether or not appearing in large print, italics, or with trade marking symbols, are Marks of Textron Aviation Inc. or an affiliate and may be registered in the United States. Third party marks whether or not appearing in large print, italics, or with trade marking symbols are marks of others. October 2023 SD-TBP-360CSLK-1023 Textron A via tion CUSTOMER ACCEPTANCE CHECKLIST Aircraft Serial Number Aircraft Registration Date Customer Crew Aircraft Specialist BEW BOW HOURMETER END START TOTAL PRELIMINARY EXTERIOR INSPECTION □ Normal Procedures Checklist COCKPIT/CABIN INSPECTION □ Normal Procedures Checklist BY T E X T R O N A VIA TIO N +-EXTERIOR INSPECTION □ Keylocks - Check □ Doors - Check □ Windshields / Windows - Check Condition □ Pitot-Static Heat - Check □ Lights - Check □ Normal Procedures Checklist INTERIOR INSPECTION □ Normal Procedures Checklist - Cockpit Preparation □ Optional Equipment - Verify □ Electronic charts/FMS database - Check Current □ Weather - Brief □ Flight Profile - Brief TAKEOFF DATA ATIS WIND VISIBILITY CEILING TEMP BARO STARTING ENGINES □ Normal Procedures Checklist - Before Starting Engines □ Normal Procedures Checklist - Starting Engines □ Normal Procedures Checklist -- Before Taxi Clearance_____ TAXI □ Normal Procedures Checklist - Taxi □ Ice Protection Systems - Check □ Normal Procedures Checklist - Before Takeoff TAKEOFF/CLIMB □ Normal Procedures Checklist - Takeoff □ Normal Procedures Checklist - After Takeoff / Climb □ Ice Protection Systems - Check □ Com/Nav - Check □ Generators - Check □ Fuel crossfeed/transfer- Check □ APU - Operation (if equipped/required) NOTES CRUISE □ Normal Procedures Checklist - Cruise □ Avionics / Optional Equipment - Check □ All cabin drains - Check □ Temperature control-Check □ Wx Radar/XM weather - Check □ Flight phone - Check □ Cruise Performance Data - Record (next page) BY T E X T R O N A V I A TI ON LEFT RIGHT STANDBY N1 ITT N2 Oil Press Oil Temp Fuel Flow Fuel Qty KIAS Mach Altitude Temperature RAT OAT ISA Weight TAS □ AGHME Overflight (As Required) ALT UTC DESCENT / APPROACH / LANDING □ Normal Procedures Checklist - Descent □ Speedbrakes - Check □ APU - Start (if required) □ AOA - Check Vref □ Normal Procedures Checklist - Approach □ A/P Coupled ILS Approach - Check □ Normal Procedures Checklist - Before Landing and Landing ATIS WIND VISIBILITY CEILING TEMP BARO POSTFLIGHT □ Normal Procedures Checklist - After Landing and Shutdown □ Post-Flight Exterior Inspection - Complete EXTERIOR GROUND REVIEW Cabin Door □ Operation - Check □ Overall condition and appearance - Check □ Handle condition and operation - Check □ Seals condition and appearance - Check □ Frame condition and appearance - Check LH Fuselage □ Overall condition and appearance- Check □ Windows condition and appearance-Check □ Placards and Silkscreens Condition and appearance- Check LH Nose Section □ Overall condition and appearance- Check □ Door condition and operation- Check □ Windows condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check □ Landing gear and doors condition and appearance- Check LH Wing and Leading edge □ Overall condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check □ Landing gear and doors condition and appearance- Check LH Vertical Stabilizer □ Overall condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check NOTES LH Horizontal Stabilizer □ Overall condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check LH Cowl or Nacelle □ Overall condition and appearance- Check □ Doors condition and operation- Check RH Nose Section □ Overall condition and appearance- Check □ Door condition and operation- Check □ Windows condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check □ Landing gear and doors condition and appearance- Check RH Fuselage □ Overall condition and appearance- Check □ Windows condition and appearance-Check □ Placards and Silkscreens Condition and appearance- Check RH Wing and Leading edge □ Overall condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check □ Landing gear and doors condition and appearance- Check NOTES BY T E X T R O N A V IA T I O N RH Vertical Stabilizer □ Overall condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check RH Horizontal Stabilizer □ Overall condition and appearance- Check □ Placards and Silkscreens Condition and appearance- Check RH Cowl or Nacelle □ Overall condition and appearance- Check □ Door condition and operation- Check NOTES AIRCRAFT INTERIOR Cabin Chairs □ Seats clean and free of defects □ Seats have freedom of movement, secure in all stops □ Seats Recline and retract smoothly □ Check headrests and seat handles for operation and appearance □ Check seats for uniformity in color, texture, and finish □ Lavatory seat clean and free of defects Furnishings - Fwd Galley & Partition □ Drawers fit tight and secure L/H and R/H galley □ Check Finish for appearance, no scratches L/H and R/H galley □ Check partition doors for operation and smoothness L/H and R/H □ Check coffee drain for appearance Carpet, Side Panels, Tables & Overhead □ Carpet is clean throughout □ Carpet is not frayed □ Side Panels are tight and acceptable for appearance □ Side Panels are clean and free of scuffs □ Cup Holders are secure and acceptable for appearance □ Overhead panels are clean and have proper fit □ Oxygen drop down panels fit well in headliner □ Air outlets function and rotate all directions □ Light/table/dimming switches operational and rotate in all directions □ Cabin tables are clean and free of defects. Furnishings and Partitions □ Aft partition is free of defects and acceptable for appearance □ Aft partition doors open and close smoothly □ Lavatory side panels are clean □ Lavatory cabinetry is clean and free of scratches □ Cabin windows not burnt and free of hazing/crazing □ Partition doors operate freely no binding or noise □ Partition doors close tightly, no light leaks □ Partition door pop-ups do not hit bathtub fitting top Furnishings and Partitions Cont. □ Tables do not bind and extend / stow properly □ Cabin window shades operate smoothly and are not binding □ Cabin door does not leak □ Emergency exit(s) have no excessive noise around handles □ AFT relief tube has suction and extends and retract properly BY T E X T R O N A V IA TI O N □ Beverage drain has suction and is leak free □ Emergency exit panels do not gap and overlap side wall □ Check Cabin temp control hot/cold □ Cabin drawers open, close, and track freely Taxi / Takeoff and Cruise □ Partitions do not rattle □ Magazine Rack divider does not vibrate □ Pyramid cabinets do not rattle, and latches are free of vibration □ Tables remain stowed NOTES END USER CERTIFICATION Seller: Textron Aviation Inc. Aircraft: Make: Textron Aviation Inc. Model: B300C Serial Number TBD End-User of the Aircraft: Name: Address: /? t'ec K Country where Aircraft will be registered Countries! where Aircraft will be operated End-Use of the Aircraft (mark “X” on all that apply): Commercial/General Transport (e.g. sightseeing, VIP, personal, company, etc.) Government Transport Military Transport EMS Law Enforcement/Homeland Security ISR (intelligence, surveillance and reconnaissance) Utility (e.g. firefighting, news gathering, etc.) Military Training Other (please specify):_________ If the Aircraft will be exported, the exporter will include the Destination Control Statement as part of the export process: “These items are controlled by the U S. government and authorized for export only to the country of ultimate destination for use by the ultimate consignee or end-user(s) herein identified. They may not be resold, transferred, or otherwise disposed of, to any other country or to any person other than the authorized ultimate consignee or end-user(s), either in their original form or after being incorporated into other items, without first obtaining approval from the U.S. government or as otherwise authorized by U.S. law and regulations.” The undersigned certifies that the information provided is true and correct as of the date set out below. If this information changes prior to Aircraft delivery or the Purchase Agreement to which this Exhibit 1 is attached is assigned prior to Aircraft delivery, Purchaser or Assignee, respectively, will submit an updated End User Certification. Signature: Company: Name: Title: Date: G*rt.c PA (Rev. 4-2023) - Revision 00 Page 14 of 15 XXX (“Aircraft”) is hereby tendered by Seller to Purchaser for technical acceptance pursuant to Purchase Agreement dated: December , 2024, and its amendments. Exhibit 4 - Factory Technical Acceptance Certificate Purchaser or Purchaser’s authorized representative hereby confirms factory technical acceptance of the Aircraft equipped as reflected in the aforementioned Purchase Agreement. The specific information regarding the Aircraft and its engines at the time of Factory Acceptance is as follows: AIRFRAME: HOURS SERIAL NUMBER LEFT ENGINE: RIGHT ENGINE: PURCHASER Signature: Name: Title: Date: Location: SELLER Signature: Name: Title: Date: Location: 3 2 LOCATION: AIRCRAFT SERIAL NUMBER: AIRCRAFT REGISTRATION: DATE: CUSTOMER: FLIGHT CREW: AIRCRAFT SPECIALIST: BEW: BOW: HOURMETER END: HOURMETER START: TOTAL: EXTERIOR INSPECTION Normal Procedures Checklist MODIFICATIONS _Logbook Entries _ Interior configuration - Dual Air Ambulance - Installed per FAA STC Number: SA1213CH or updated alternative STC - as set out in Part 3 A, Modifications (form, function and fit checks) Interior configuration - Loose Equipment and Avionics - provided (form function and fit checks) Specific Items to Review: Patient Loader Operation, Manual Patient Loader Operation, Electric _ Database Loads updated and current for Atlantic Crossing 3 3 Document and Manuals Included and Return to Service Review of Authorization to Install STC on Serial Number:__ Review of Records Showing Installation of STC on Serial Number:_ Overview of Interior and Exterior Condition Loose Equipment Checklist Re-Confirmed 3 4 XXX (“Aircraft”) is hereby tendered by Seller to Purchaser for technical acceptance of the modifications pursuant to Purchase Agreement dated: December, 2024, and its amendments. Exhibit 6 - Modified Aircraft Technical Acceptance Certificate Purchaser or Purchaser’s authorized representative hereby confirms technical acceptance of the aircraft as modified and equipped as reflected in the aforementioned Purchase Agreement. The specific information regarding the Aircraft and its engines at the time of Factory Acceptance is as follows: AIRFRAME: HOURS SERIAL NUMBER LEFT ENGINE: RIGHT ENGINE: PURCHASER Signature: Name: Title: Date: Location: SELLER Signature: Name: Title: Date: Location: 3 5 TEXTRON AVIATION INC., MODEL: KING AIR 360C “DUAL AIR AMBULANCE INTERIOR” by STC NUMBER:SA1213CH. AIRCRAFT SERIAL NUMBER: FM-120 AT FARGO, NORTH DAKOTA, USA. Exhibit 7 - Aircraft Delivery Receipt THE AIRCRAFT IS HERBY IRREVOCABLY AND UNCONDITIONALLY ACCEPTED ON THE TERMS AND SUBJECT TO THE AGREEEMNT AS OF THE DATE FRIST SET FORTH ABOVE. Purchaser or Purchaser’s authorized representative herby confirms technical acceptance of the aircraft as modified and equipped as reflected in the aforementioned Purchase Agreement and verifies that the Aircraft has been inspected and generally conforms to the Specification and Description or Specification referenced above. Purchaser or Purchaser’s authorized representative also confirms receipt of the appropriate approved Flight Manual and Logbooks for the Aircraft. HOURS SERIAL NUMBER AIRFRAME: _ ___ LEFT ENGINE: _ __ RIGHT ENGINE: _ __ LEFT PROPELLER: _ __ RIGHT PROPELLER: _ ____ ACTUAL DELIVERY DATE: WARRANTY START DATE: ACTUAL DEPARTURE DATE: HELLENIC MINISTRY OF HEALTH FARGO JET CENTER, LLC Signature: Signature: Name: Name: Title: Title: 3 6 3 7 not to any other person, including but not limited to patients or users of the Products) that the Products at delivery and for 2 years after the delivery date ("Warranty Period") shall be free from faulty workmanship and defective materials. SECTION A. S e lle r’s warranty does not cover, and Seller shall under no circum stances or theory have any labil for, any defect caused by or related to (i) the failure of the P urchase r, its em ployees or agents, to follow strictly Seller's instructions concerning use, operation and maintenance of the Products, (ii) any abuse, neglect, or misusi of the Products, (Hi) alteration of the Products, (iv) norm al wear and tear, (v) interruptions in, or unsuitable, p ow er or communication sources or connectivity, (vi) environmental conditions, (vii) storage or handling by parties other tha Seller, (viii) design o f the Products, (ix) any o ther causes that are not S eller’s fault, or (x) any non-original Products or parts thereof not manufactured by Seller, provided, however, that Seller shall provide to Purchaser all pass through warranties received from the original su pplier or m anufacturer of such Products or parts thereof. In the event that the Products are not covered under the limited warranty due to a circumstance identified in this Section, Purchaser shall be liable to Seller for any expenses incurred in connection with assessing and re pairing such Products. S e lle r’s lim ited warranties hereunder shall not be enlarged, or in any other way affected by (and no obligation or liability shall rise from), Seller's rendering of advice or service relating to the Product or its installation, SECTION B. In the event that the defective Product or p a rt is covered under this Limited Warranty, P urchaser shall notify Seller within 30 days after discovery o f any defect and shall return the P ro duct or any defective part p ursu ant to S e lle r’s return instructions and within the time period instructed by Seller. Purchaser shall also be responsible for all costs of removal and Reinstallation of the Product or of any defective components and for all freight and shipment of any defective Product, parts, or R eplacem ent Product or p arts to and from S elle r’s warehouse, and for all travel costs for Seller's personnel. SECTION C. Should the Product or any part of the Product fail to function within normal use due to defect in materials or workmanship within the W arranty Period, Seller at its option will: (i) rep air or replace the applicable p art o f the Products; (ii) issue a 1 credit to Purchaser (the credit sh all be the lesser of the net invoiced price of the original part, or the current functio nally comparable part, or replacem ent part of the Products), or (iii) provide a functiona lly com parable replace m e nt p art of the Products at no charge. S eller’s choice of one o f the rem edies set forth in this Section shall be P u rc ha ser’s sole rem edy for breach of this lim ited warranty. SECTION D. To the extent that Seller has relied upon any specifications, information, representation of operating conditions or other data or inform ation supplie d by P urchaser to Seller in the selection or design of the Products and the preparation o f Seller's quotation, and in the event that actual operating conditions or other conditions differ from those represented by Purchaser and relied upon by Seller, any warranties or o ther provisions which are affected by such conditions shall be null and void, unless , otherwise m utually agreed upon in writing. SPECTRUM Aerom ed accordance with the Terms, the Seller shall provide a (one) qualified pilot (the “Pilot”) to assist as Pilot in Command (PIC) (Provided the Aircraft flies on US Registration) the ferry flight from Fargo, North Dakota to Purchaser’s base in Greece (Elefsis AFB). Purchaser’s representatives or Hellenic Air Force personnel shall have the right to be onboard during the ferry flight after acceptance, in accordance with Seller’s PIC requirements. 1.2 This Service is included in the price of this contract. 1.3 Operator acknowledges that all flights performed during the Entitlement Period will be within operator’s operational control. Operator further acknowledges that when performing the Services, the Pilots will be under operator’s exclusive directions provided that nothing herein shall cause the Pilots to be bound by operator’s instructions regarding the provision of Services if such instructions are, in professional judgement of the Pilots, illegal, unsafe or imprudent. 1.4 In performing the Services, operator shall respect the crew duty maximum flight times permitted under applicable laws and regulations including without limitation any local state, or national authority jurisdiction over the Pilots.

COST AND TAXES 2.1 Operational costs for the Aircraft’s ferry flight from Fargo, North Dakota to Athens are included as part of this contract. 2.2 Furthermore, Seller will cause the Aircraft to be insured in the Purchaser’s name and interest, solely for the ferry flight from Fargo, North Dakota to Athens, it being understood that the said insurance shall have a maximum duration of 15 days from the Aircraft delivery and shall immediately expire and lapse upon the Aircraft’s landing in Athens/Elefsis AFB. 2.3 Taxes or financial burdens imposed outside Greece in connection with the service provided pursuant to this Exhibit will be covered by Seller.

FAILURE TO PERFORM/RIGHT TO STOP WORK 3.1 If any of the following events occur, Seller may fail to perform or may stop performing the Services of Paragraph 1: a. An event beyond the reasonable control of the Seller; b. There are conditions existing or threatening that are dangerous to the safety, welfare or health of the Pilot; c. The government of any country or any governmental agency or authority refuses the Pilot’s permission to enter the country or Purchaser’s base of operation; or d. Performing the Services would subject to liability under applicable law, rule, regulation or order. Exhibit 10 - Ferry Flight from USA 3 9 Seller and its representative affiliates, officers, directors, agents, subcontractors, Pilots, employees and representatives (the “Indemnified Parties”) from and against any and all liabilities, claims, damages, losses and judgements, including reasonable attorney’s fees and related costs and expenses arising directly or indirectly our of the Services provided to this Exhibit including but not limited to claims arising by reason of a) injury or death of any person b) loss of use or damage to any property, including the Aircraft; or c) the performance of the Services under this Exhibit. 4.2 The foregoing release and agreement to defend, indemnify and hold harmless applies to claims by Purchaser and/or operator or third parties, no matter when such claims may be asserted and regardless of fault or theory of action, whether in contract or tort (including but not limited to the active, passive or imputed negligence of Seller), by statute or otherwise except that such agreement to defend, indemnify and hold harmless shall to apply to third party claims for death, bodily injury or third party property damage to the extent caused by Seller gross negligence or willful misconduct. 4.3 Article 4, including Purchaser’s and operator’s indemnity obligations, shall survive termination or expiry of the Aircraft Purchase Agreement.

INSURANCE Seller shall insure the Aircraft from Delivery to Purchaser Fargo, North Dakota, until the Aircraft lands in Athens against: a. All risks of loss of or damage to the Aircraft, including without limitation all risks of war or allied perils including hijacking, malicious damage, strikes, riots and civil commotion, in an amount of not less that the full replacement value of the Aircraft; b. Aviation liability, including third party liability, and liability to passengers including flight crew, in an overall limit not exceeding $200,000,000 US Dollars for any one occurrence; and c. Medical equipment carried on board. Purchaser shall be responsible for any applicable deductibles or co-insurance that apply to this insurance; Seller will provide an insurance certificate to the Purchaser 1 month prior to the Aircraft delivery in Fargo, North Dakota.

DISCLAIMER EXCEPT AS OTHERWISE PROVIDED IN THIS EXHIBIT, SELLER MAKES NO REPRESENTATION, WARRANTY OR GUARANTEE WHATSOEVER IN CONNECTION WITH THE FURNISHING OF THE SERVICES AND PURCHASER AND SELLER HERBY WAIVE, RELEASE AND RENOUNCE ALL WARRANTIES, CONDITIONS, OBLIGATION AND LIABILITIES OR SELLER AND ALL RIGHTS, CLAIMS AND REMEDIES OF PURCHASER AGAINST SELLER, EXPRESS OR IMPLIED, ARISING BY LAW OR OTHERWISE, WITH RESPECT TO THE SERVICES OR ANY OTHER THING 4 0 PARTICULAR PURPOSE, B) ANY IMPLIED WARRANTY OR CONDITION ARISING FROM COURSE OF PERFORMANCE , COURSE OF DEALING OR USAGE OF TRADE, C) ANY OBLIGATION, LIABILITY, RIGHT, CLAIM OR REMEDY IN TORT, WHETHER OR NOT ARISING FROM THE ACTIVE, PASSIVE OR IMPUTED NEGLIGENCE OF SELLER; AND D) ANY OBLIGATION, LIABILITY, RIGHT, CLAIM OR REMEDY FOR LOSS OF OR DAMAGE TO ANY PROPERTY INCLUDING THE AIRCRAFT, OR FRO LOSS OF USE, REVENUE OR PROFIT, OR FOR ANY LIABILITY OF SELLER TO PURCHASER OR TO ANY THIRD PARTY SELLER SHALL NOT BE LIABLE FOR ANY INDIRECT, INCIDENTAL, CONSEQUENTIAL, SPECIAL OR PUNITIVE DAMAGES OF ANY KIND OR NATURE UNDER ANY CIRCUMSTANCES.

PURCHASER REQUIREMENTS Purchaser shall obtain for Seller, at no cost to Seller, the necessary work permits, airport security clearances, authorizations, approvals and necessary endorsements of the Pilots licenses from the Hellenic civil aviation authority so that the Pilots may accomplish Services herein. 4 1 Syllabus, as per the course descriptions listed herein. All parties involved are committed, to their best efforts, to plan and complete the training prior to the technical receipt of the Aircraft. The delivery of training shall be subject to the provisions of Article 7 of this APA. All training as part of this contract for flight crew (Two (2) Pilots - Initial Course) and maintenance personnel (One (1) Maintenance Person - Beech 300 Series Maintenance Initial Course) will be per Section 17 of the attached KING AIR 360C (UTILITY INTERIOR) SPECIFICATION AND DESCRIPTION - OCTOBER 2023 REVISION B, SERIAL NUMBER FM-110 TO TBD. Syllabuses are provided for reference below. Any other syllabus required for this training will be provided to the trainees prior to commencing training at FlightSafety or other Textron Aviation Inc. designated training facility. 4 2 COURSE MODULE INITIAL RECURRENT PRIOR EXPERIENCE Course Length 17 Days 3 Days 4 - 5 Days Ground School 41.0 hours 10.0 hours 10.0 hours Systems Integration Training 4.0 hours N/A N/A Briefing/Debriefing 10.5 hours 4.5 hours 6.0 hours Simulator (Pilot Flying) 14.0 hours 6.0 hours 8.0 hours PRIOR EXPERIENCE COURSE This course is designed for pilots who want to obtain an ATP. Prerequisites may be required. Contact us for details. COURSE DATES For course dates, visit our website at www.fliqhtsafety.com ADDITIONAL INFORMATION Courses are approved by the FAA and other regulatory authorities; please contact us for details. Course modules and length may vary depending on regulatory authority. FOR MORE INFORMATION, CONTACT: +1 201.528.0170 or sales@fliqhtsafetv.com TRAINING LOCATIONS Tampa, Florida internal Use Only; I - 307337 R - 307336 PE - 307335 flightsafety.com · A Berkshire Hathaway company Rev 1.0.0.22 KING AIR 300 SERIES In-Center or Online Instructor-led LiveLearning' At the end of this course, participants will be able to demonstrate proper interpretation and utilization of technical data as well as recall major system and sub-system normal operations, safety precautions, ground handling, and system test procedures. The initial training programs are aligned with ATA104 Level III and regulatory requirements, as applicable. Client will obtain the ability to recall, interpret, identify, test, troubleshoot and correlate system information applicable to the specific aircraft or engine model. Initial training covers use of OEM documentation, component location, normal operation, inspection, service and repair of aircraft systems. GROUND SCHOOL COURSE MODULES HOURS ATA 100 Publications................................................................. 0.50 ATA 5-12 Aircraft General..........................................................2.00 ATA 20 Standard Practices....................................................... 0.50 ATA 21 Air Conditioning..............................................................7.75 ATA 22 Auto Flight...................................................................... 1.75 ATA 23 Communications...........................................................1.00 ATA 24 Electrical.........................................................................7.00 ATA 25 Equipment/Furnishings................................................. 1.25 ATA 26 Fire Protection............................................................... 1.00 ATA 27 Flight Controls...............................................................4.25 ATA 28 Fuel............................................................................... 5.00 ATA 30 Ice and Rain Protection................................................ 2.00 ATA 31 Indicating and Recording..............................................3.25 ATA 32 Landing Gear................................................................6.00 ATA 33 Lighting...........................................................................1.00 ATA 34 Navigation......................................................................1.25 ATA 35 Oxygen...........................................................................1.25 ATA 36 Pneumatics....................................................................0.50 ATA 37 Vacuum..........................................................................0.50 ATA 38 Water/Waste.................................................................. 0.50 ATA 44 Cabin Systems............................................................... 0.75 ATA 45 Central Maintenance System.......................................0.50 ATA 46 Information System.......................................................0.50 ATA 51-57 Structures................................................................. 4.00 ATA 61 Propellers/Propulsion....................................................2.50 ATA 71-80 Powerplant............................................................... 9.50 Ground School Training Hours............................................ 66.00 FOR MORE INFORMATION, CONTACT: +1 201.231 8663 or TRAINING LOCATIONS Wichita, Kansas ACADEMIC COURSE MODULES HOURS Welcome/lntroduction...............................................................1.00 Functional Application............................................................ 2.00 Systems Integration.................................................................1.00 Brief/Debrief*............................................................................ 0.50 Review/Exam............................................................................ 4.00 •Based upon availability and course schedule. Total Hours............................................................................ 74.50 APPROVALS AND LIMITATIONS FAA IA renewal Accepted Accredited for IA refresher training under Title 14 CFR part 65, § 65.93(a)(4) EASA Approved B1-T1 (Theory) CASA Approved B1.1 (Theory) DGCA Approved B1-T1 (Theory) GCAA - UAE Approved B1-T1 (Theory) UK CAA Approved B1-T1 (Theory) salesifofliahtsafetv.com Internal Use Only: 303169 LL - 307396 flightsafety.com · A Berkshire Hathaway company Rev 5.0.24 Η ισχύς του παρόντος νόμου αρχίζει από τη δημοσίευσή του στην Εφημερίδα της Κυβερνήσεως και της υπό κύρωση Σύμβασης από τη 16η Δεκεμβρίου 2024, ημερομηνία κατά την οποία υπογράφηκε η Σύμβαση. Παραγγέλλομε τη δημοσίευση του παρόντος στην Εφημερίδα της Κυβερνήσεως και την εκτέλεσή του ως νόμου του Κράτους. Αθήνα, 15 Ιανουαρίου 2025 Η Πρόεδρος της Δημοκρατίας ΚΑΤΕΡΙΝΑ ΣΑΚΕΛΛΑΡΟΠΟΥΛΟΥ Οι Υπουργοί Εθνικής Οικονομίας και Οικονομικών Εθνικής Άμυνας ΚΩΝΣΤΑΝΤΙΝΟΣ ΧΑΤΖΗΔΑΚΗΣ ΝΙΚΟΛΑΟΣ - ΓΕΩΡΓΙΟΣ ΔΕΝΔΙΑΣ Υγείας Υποδομών και Μεταφορών ΣΠΥΡΙΔΩΝ - ΑΔΩΝΙΣ ΓΕΩΡΓΙΑΔΗΣ ΧΡΗΣΤΟΣ ΣΤΑΪΚΟΥΡΑΣ Θεωρήθηκε και τέθηκε η Μεγάλη Σφραγίδα του Κράτους. Αθήνα, 16 Ιανουαρίου 2025 Ο επί της Δικαιοσύνης Υπουργός