OFFER#

ANTONOV AN-74K-100

TYPE:	Aircraft
DESCRIPTION:	Antonov AN-74K-100 Passenger
PRICE:	Upon Request
PACKING:	As is, Where is

ANTONOV AN-74K-100 PAX

AIRCRAFT: AN-74 TK-100

Section Description

A AIRCRAFT IDENTIFICATION

B CERTIFICATION OR AIRWORTHINESS

C CERTIFICATION OR REGISTRATION

D AIRCRAFT STATUS

E AIRFRAME MAINTENANCE PROGRAMME

F AIRWORTHINESS DIRECTIVES

G ENGINE MAINTENANCE PROGRAMME

H INSTALLED ENGINES

I INTERIOR CONFIGURATION

J GALLEY PROVISIONS

K LAVATORIES

L INTERIOR COLOURS

M PLACARDS AND LIGHTED SIGNS

N PRINCIPAL RADIO AND AVIONICS

A AIRCRAFT IDENTIFICATION
Manufacturer:	Antonov
Type and Model:	AN-74 TK-100
Serial Number:	14-07
Date of Manufacture:	May-1992

B CERTIFICATION OR AIRWORTHINESS
Category:	Large aircraft
End of Airworthiness Certificate:	May-2006

C CERTIFICATION OR REGISTRATION
Registered Operator:	EU

D AIRCRAFT STATUS
Aircraft FH:			2635
Aircraft Cyc:			1097
Current Major Overhaul Facility:			АРЗ-412, Kiev

Last Check
Check:	Date:	Interval		AC flight hours	AC cycles
F-8	01-Nov-2004	300 FH		2400 FH	1004 fl
Next Check
Check:	Date:	Interval		AC flight hours	AC cycles
F-9	-	300 FH		2700 FH	-
Remaining:				65 FH

E AIRFRAME MAINTENANCE PROGRAMME
Aircraft Maintenance Program Provided by:	Manufacturer, based on maintenance regulation
Repair Station Providing Service:	АРЗ-412, Kiev
Primary Line Maintenance Provided by:	Operator

F AIRWORTHINESS DIRECTIVES
As of February 2008	Full
Outstanding AD’s:	None
AD’s requiring repeat inspections:	None
AD’s to be terminated within 12 month:	None

G ENGINE MAINTENANCE PROGRAMME
Engine Aircraft Maintenance Program Provided by	Manufacturer, based on maintenance regulation
Engine Oil Type	ВНИИНП-50-1-4У

H INSTALLED ENGINES
Engine 1
Engine Manufacturer:	Мотор Сич
Engine Type and Model:	D-36 2A
Serial Number:	708036412A005
Date of Manufacture:	26-Oct-91
Total Flight Hours:	2691 FH
Total Cycles:	1097 cyc
Resource (FH):	3750 FH
Resource (Cyc):	2500 cyc
Resource (Date):	06-Aug-07
Remainder (FH)	1059 FH
Remainder (Cyc)	1403 cyc
Engine 2
Engine Manufacturer:	Мотор Сич
Engine Type and Model:	D-36 2A
Serial Number:	708036312A006
Date of Manufacture:	23-Oct-91
Total Flight Hours:	2691 FH
Total Cycles:	1097 cyc
Resource (FH):	3750 FH
Resource (Cyc):	2500 cyc
Resource (Date):	06-Aug-07
Remainder (FH)	1059 FH
Remainder (Cyc)	1403 cyc
APU
Engine Manufacturer:	“Гидравлика” Уфа
Engine Type and Model:	TA-12
Serial Number:	24012025
Date of Manufacture:	30-Nov-92
Total Flight Hours:	301 FH
Total Launches:	1111
Resource (FH):	1000 FH
Resource (launches):	2500
Resource (Date):	27-Jan-07
Remainder (FH)	699 FH
Remainder (launches)	1389

I INTERIOR CONFIGURATION
Passenger Seats	48
Provisions for Life Vests Under Seats	Yes

J GALLEY PROVISIONS
Galley Location	Manufacturer	Part Nr.	Equipped Water Power
FWD RH	-	-	Yes

K LAVATORIES
Number of Lavatories	One
Position	AFT

L INTERIOR COLOURS
Carpets	Blue
Leather Seats	Blue

M PLACARDS AND LIGHTED SIGNS
Language	English

Service life of 30 years; 40000 hours; 20000 landings.

At self-summer the equipment for the international flights and following systems is established: TCAS-67; RVSM; BRNAV; ELT AN-74TK-100 - passenger type.

Этот тип самолёта эксплуатируется по состоянию и на сегодня имеет только теоретически обоснованные ресурсы: - срок службы 30лет; 40000 лётных часов; 20000 посадок. Капитальные ремонты, программой ТО, не предусмотрены. Программа ТО имеет кроме оперативных и периодических форм, дополнительные работы КВР-1, КВР-2, КВР-3 (контрольно восстановительные работы), которые выполняются совместно с одной из очередных тяжёлых форм с установленной периодичностью. На предложенном ВС выполнены все формы и КВР-1. К настоящему времени подошел срок выполнения КВР-2. После выполнения этого обслуживания ВС может эксплуатироваться в течение двух лет и 3600часов. В пределах

Specification and photos are not contractual and are subject to verification upon inspection

NB: Aircraft offered for sale subject to contract, prior sale, withdrawal from the market and information regarding any aircraft or helicopter and provided verbally or in written documentation and/or contained within or associated paper-work should be taken as a guide only in determining the suitability, including that aircraft or helicopters specification and/or performance. We highly recommend that any buyer or lessee perform their own inspections and due diligence to verify any and all technical, performance and specification information contained therein including OEM claims.

PLEASE NOTE: AIRCRAFT SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION. WE DO NOT ACCEPT ANY LIABILITY FOR AIRCRAFT DEFECTS, HISTORY OR TECHNICAL RECORD ERRORS. IT IS THE BUYERS RESPONSIBILITY TO INDEPENDENTLY VERIFY THE AIRCRAFT AND COMPONENT HISTORY.

PLEASE BE ADVISED THAT INFORMATION INCLUDED IS CONFIDENTIAL IN NATURE AND IS BASED ON PRE-EXISTING BUSINESS RELATIONSHIP WITH THE LEGAL OWNER OF PROPERTY DESCRIBED HEREIN (IF APPLICABLE). AS SUCH, UPON RECEIPT OF SAID INFORMATION THE RECEIVER ACKNOWLEDGES THAT ANY UNAUTHORIZED CONTACT WITH SAID LEGAL SELLER WILL BE CHARACTERIZED AS A BREACH OF CONFIDENTIALITY AND SAID AGREEMENT MAY BE ENFORCED UNDER EXISTING LAW OR IN EQUITY.

This paper was prepared by General Equipment Inc.
The paper represents an offer of a partner of General Equipment Inc.
All rights are reserved by and for General Equipment Inc.
All content and ideas of this paper are the property of General Equipment Inc.

GENERAL EQUIPMENT INC.