OFFER#

1990 BOEING MD-81

TYPE:	Aircraft
DESCRIPTION:	1990 Boeing MD-81 for Sale
PRICE:	Upon Request
PACKING:	As is, where is

1990 BOEING MD-81

General Specification

Boeing MD-81

Aircraft Data
Aircraft Model:				Boeing MD-81
Date of Delivery:				1990
Engine Model:				Pratt & Whitney JT8D-200 series
Noise Compliance (Current):				Stage III

Performance Data

Operational Weight
Maximum Taxi Weight:				141,000 lb
Maximum Take-Off Weight:				140,000 lb
Maximum Landing Weight:				128,000 lb
Maximum Zero Fuel Weight:				118,000 lb

Fuel Capacity
Left Tank:				1,383 gal
Right Tank:				1,383 gal
Center Tank:				3,074 gal
Fwd Aux Tank:				N/A
Aft Aux Tank:				N/A


Airframe Status				(Data as of March 4, 2008)

Total Flight Time:				34,429:56
Total Cycle:				34,037
Time since last "C" Check (Day)				228 Days
Time since last "C" Check (FH)				1417:21 FH
Time remaining to next “C” Check				2182:39 FH or 228 Days (whichever comes first)

Daily Utilization (FH vs. FC):				7.0 : 7.0

Maintenance History:				Item			Accomplish Data(Flight Hour)
				No.5 "C":			July 20,2007 (@33,012:35 FH)
				No.4 "C":			March 28,2006 (@36,343:32 FH)
				No.3 "C":			February 11,2005 (@27,712:51 FH)
				No.2 "C":			December 3, 2005 (@26,146:48 FH)

Maintenance Program:				MSG 3

Maintenance Interval:				Type			Interval
				A Check			450 Flight Hours
				C Check			3,600 Flight Hours or 15 Months

Product Enhancement:					(a) Insulation Blanket installed per AD2000-11-01.
					(b) Cockpit Security Door has been installed.
					(c) Modification to Class C Cargo compartment incorporated

Landing Gear Status			(Data as of March 3, 2008)

Maintenance Program:				20,000 Cycle or 10 Years

Position:		NLG				MLG-L/H			MLG-R/H
Serial Number:		R3956TU				MAL095			MAL040
Install Date:		July 16, 2007				June 30, 2000			June 30, 2000
Cycle since Last O/H:		1,276				15,236			15,236

Engine Status			(Data as of March 3, 2008)

Engine Model:				Pratt & Whitney JT8D-200 series
Takeoff Thrust sea-level rating (dry):				20,000 lb

APU Model:				Honeywell GTCP85-98DHF

Maintenance Program:				Condition Monitoring

Position:		No.1 Engine				No.2 Engine			APU
Model:		JT8D-217C				JT8D-217C			GTCP85-98DHF
Serial Number:		P725374				P725588D			P-1083
Total Time:		32,783				30,298			37,437
Total Cycle:		32,136				29,768			38,930
LSV description:		ESV2				ESV2			REPAIR
LSV date:		July 19, 2007				September 26, 2007			November 15, 2006
Time since LSV:		1,193				797			2,368
Cycle since LSV:		1,219				742			2,260
LLP Remain Cycle (First Limit):		7,597				7,634			-
HPC AD Due Date:		18 July 2019				25 September 2019

Cabin Equipment

Cabin Arrangement No.:				N01

Equipment:	Item			Manufacturer				Qty
	Seats:			Tenryu Industries				Total 163 (F:0/C:0/Y:163)
	Galleys:			Nordskog				3
	Lavatories:			JAMCO				2


Avionics

System	Qty	Description	Vendor	Model or Part Number

Digital Flight Guidance	2	Digital Flight Guidance Computer	Honeywell	4034241-971 or -973
	1	Flight Guidance Control Panel	Honeywell	4034242-934
HF System	1	(Provision only)
VHF System	2	VHF Communication Tranceiver	Collins	618M2D, 618M3 or 618M3A
Voice Recording System	1	Voice Recorder	Honeywell	965-6005-076 or -076ULD
Flight Recorder System	1	Digital Flight Data Recorder	SDC	980-4100-DXUS
Air Data Computing System	2	Digital Air Data Computer	Honeywell	HG280D80
Gyrosyn Compass System	2	Directional Gyro	Sperry	DG-206A or 2588302-4
Attitude System	2	Vertical Gyro	Honeywell	2587335-13 or -113
Marker Beacon System	1	Marker Beacon Receiver	Collins	51Z-4
VOR/ILS System	2	VOR/ILS Receiver	Collins	51RV-4
Weather Radar System	1	Weather Radar Receiver Transmitter	Bendix	RTA-4A
Radio Altimeter System	2	Radio Altimeter Tranceiver	T.R.T.	9599-607-14908
Enhanced GPWS	1	Enhanced GPW Computer	Honeywell	965-1076-020-214-214
TCAS	1	TCAS Computer	Collins	622-8971-022
Windshear Alert and Guidance System	1	Windshear Computer	Honeywell	4059845-911
DME System	2	DME Interrogator	Collins	860E-5
ADF System	2	ADF Receiver	Collins	ADF-700
ATC Transponder System	2	Mode S ATC Transponder	Collins	TPR-720
Performance Management System	1	PMS Computer Unit	Delco	7892551-011-010

Enhancement Status - AVIONICS	Compliance
EGPWS	Yes
TCAS Change 7.0	Yes
RVSM Capability	Yes
ATC mode S Transponder	Yes

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 Corp.
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GENERAL EQUIPMENT INC.