OFFER#

IL-62M

TYPE:	Aircraft
DESCRIPTION:	1990 IL-62M
PRICE:	Upon Request
PACKING:	As is, Where is

1990 IL-62M

SPECIFICATION OF IL-62М aircraft СПЕЦИФИКАЦИЯ самолета Ил-62М

Serial number Серийный номер

5202

Airframe Планер

Manufacture date Дата выпуска	1990 y.
Total life (Hrs/Landings) Назначенный ресурс (часы, посадки)	35000 h., 7500 land., 20 y. Prolongation to 50000 h., 50 y
Total FLT hrs and Landings since new (Hrs/Landings) Налет СНЭ (*часы, посадки)*	31402 h. / 6328 land.
Total FLT hrs and Landings after last overhaul Налет после последнего *ремонта* *(Hrs/Landings) (часы, посадки)***	11182 h. / 2215 land
Date of last overhaul Дата *последнего ремонта*	30.04.1998. № 243 ГА
Number of overhaul accomplished Количество ремонтов	2
Time between two overhaul (Hrs/Landings) Межремонтный ресурс (*часы, посадки)*	15000 h., 3000 land,12y. Prolongation to 25000 h., 5500 land., 14 y (Further prolongation on a technical condition becomes every year till 20 y.)/

Engine Type *Тип*	№ 1 D-30KU-2	№ 2 Д-30КУ-2	№ 3 Д-30КУ-2	№ 4 Д-30КУ-2
Serial number *Серийный номер*	5138902225	3051228702224	3051248502229	51138702210
Manufacture date Дата выпуска	23.08.1989 г.	24.06.87 г.	28.11.85 г.	30.08.87 г.
Date of last major overhaul *Дата последнего ремонта*	25.03.2001 г.	07.12.00 г.	27.12.00 г.	24.03.01 г.
Total life (Hrs)	18000 h/3800 Cycle	18000 h/3800 Cycle	18000 h/3800 Cycle	18000 h/3800 Cycle
Total FLT hrs since new Hrs Налет СНЭ(*часы)*	10161 h., 1873 Cycle.	14361 h., 2797 Cycle.	11235 h., 2126 Cycle .	14051 h., 3019 Cycle.
Total FLT hrs after last *Налет после последнего* Overhaul (Hrs/) *ремонта (часы)*	2040 h., 457 Cycle.	3240 h., 656 Cycle.	3240 h., 658 Cycle.	1161 h., 322 Cycle.
Time between two overhaul *Межремонтный ресурс* *(Hrs/Years) (часы, годы)***	3000 h.., 8 y, 543 Cycle. till 6 000 H, prolongation is spent every calendar year.	3600 h.., 8 y, 905 Cycle. till 6 000 H, prolongation is spent every calendar year.	3600 h.., 8 y, 905 Cycle. till 6 000 H, prolongation is spent every calendar year.	3000 h.., 8 y, 543 Cycle. till 6 000 H, prolongation is spent every calendar year.

APU ВСУ

Type *Тип*	ТА - 6А
Serial number Серийный номер	0436А223
Manufacture date Дата выпуска	30.12.1990 y.
Total life (Hrs) Назначенный ресурс (часы)	3400 h., 5000 Cycle., 20 y
Total FLT hrs and since new (Hrs) Наработка СНЭ (часы)	2693 h., 2850 Cycle.
*Total FLT hrs and Landings after last overhaul Наработка после последнего ремонта* (Hrs)**	724 h., 898 Cycle.
Date of last overhaul Дата последнего ремонта	11.12.1998 y.
Number of overhaul accomplished Количество ремонтов	1
Time between two overhaul (Hrs/Years) Межремонтный ресурс (*часы, годы)*	1231 h., 2500 Cycle., 10 y Further prolongation on a technical condition becomes every year till 3400 h., or 5000 Cycle., or 20 y

The calendar resource established Ilyushin Design Bureau for this type ACs makes 50 years.

По посадкам КБ дает МРР еще на 2500, по часам 10 000, 2 года с последующим продлением по календарю. По движкам МРР продляться может до 6 000 часов, продление проводится ежегодно. С КБ и АРЗ по движкам у нас отличные отношения и мы всегда можем помочь в этом

LIST OF AVIONICS ONBOARD OF IL-62M

The basic equipment of the IL-62M includes all the instruments for altitude instrument flying under IFR as follows:

Pilot-static and gyro instruments (ICAO standards)		Country of Manufacture	Number of units
Gyro-magnetic compass system	TKSP-2P	Russian made	1 unit
Magnetic compass	KI-13	Russian made	1 unit
Navigation system	NV-PB-1	Russian made	1 unit
Navigation system	KURS-MP-70	Russian made	2 units
Navigation system	SD-67, SD-75	Russian made Russian made	1 unit 1 unit
Inertial systems	I-21	Russian made	2 units
Enhanced Ground Proximity Warning System	SSOS-«Vektor»	Russian made	2 units
Altitude indication and monitoring systems (RVSM)	VBE-2A	Russian made	2 units
Altitude indication and monitoring systems	Altimeter-921 (футомер)	USA	1 unit
Meteorological radar	GROZA-62A	Russian made	1 unit
Radio altimeter	RV-5MD	Russian made	2 units
ADF	ARK-15M	Russian made	2 units
Landing system (operates ILS mode)	KURS-MP-70	Russian made	2 units
VHF Comm transceiver	BAKLAN-20D (8,33 kHz)	Russian made	2 units
HF Comm transceiver	MICRON	Russian made	2 units
Transponder (operates ICAO standard modes)	SOM-64, SO-70	Russian made	1 unit
Additional navigation equipment installed
TCAS/ACAS-II	TCAS-II	Collins, USA	1 unit
Transponder S mode	TCAS-II	Collins, USA	1 unit
Transponder C mode	TCAS-II	Collins, USA	1 unit
GPS	TNL-2000 Approach Plus	USA	1 unit
Emergency radio beacon («KOSPAS-SARSAT» systems)	ARM-406P ARM-406AC1	Russian made Russian made	1 unit 1 unit

The average charge of fuel by our plane which has the admission for loading in 33 tons:

- at range of flight of 3000 km and more - 7 tons / hour, at the maximal loading 33 tons.

4. Technical Status of the Aircraft

4.1. Rough landing
What kind of work done
What kind of damage found no

Cases of aircraft damage by mercury not damaged
Indicate the damaged places and the taken measures.

4.2. There were cases of aircraft damage by
electric discharge and what damaged not damaged

4.3. Number of unpressurized places of cell tanks and location scheme no

4.4. Corrosion, cracks, crates see the Onboard book
and other external operational damages

4.5. Are there any comments concerning flight operation no

4.6. The state of cable and wiring of
Electrical equipment, Defects detected during exploitation no

4.7. Cases of wires damages in Switching devices and communication
boxes and methods of its removing no

4.8. Depth of the scratches on the damper support piston of the landing gear no

4.9. The state of the passenger cabin good

4.10. Where was made last articulation. R-2 Factory 243GA
Deviations points

5. GENERAL INFORMATION

5.1. Commercial loading - 33 tons, 24 passengers

- 168-180 passengers

5.2. Volume - 210м34.

5.3. Dimensions:

Entrance doors - 1.83 х 0.864м

Doors of cargo outlets

№1 - 1.31 х 1.26м

№2 - 1.00 х 1.26м

№3 - 0.7 х 0.76м

№4 - 1.07 х 1.15 х 1.26м

Crew	5
Cruise speed, km/h	820-900
Altitude, m	10000-12000
The maximal range of flight -	11 000 km.
Range with payload of 23000 kg (air navigational fuel reserve=5100 kg), km	7800
of ISA at the sea level), m	3300
Landing distance required (in conditions of ISA at the sea level), m	2500
Maximum takeoff weight, tons	165
Maximum landing weight, tons	105
Maximum fuel system capacity, l	105300
Permissible centrings, ADMC %:
- maximum-front	27
- maximum-back	34

1990 IL-62M Stage II. with TCAS. II categories ICAO.

Version; cargo-passengers (24 pass and 33 tons), passengers (168-180 max.).
Engines 2 Chapter ICАО on noise.
Ready immediately! The AIRWOTHINESS till April, 30th, 2009. In the further prolongation annually up to 2010 or 2013 without OH. We can provide to you prolongations under the Contract with you. The price includes the extension of airworthiness for 1 year up to April 2010.

Ilyushin Design Bureau gives TBO still IN ADDITION:

- on landings for + 2500 land,

- on hours + 10 000 hours,

- +2 years with the subsequent prolongation on Total life a calendar.

On engines TBO can last till 6 000 H, prolongation is spent every calendar year.

From Ilyushin Design Bureau and factory in the city of Kazan (Russia) and a factory on engines at us excellent relations and we can always help with it.

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 this email 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.
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All content and ideas of this paper are the property of General Equipment Inc.

GENERAL EQUIPMENT INC.

ТА - 6А