GENERAL   EQUIPMENT   INC.                    

 

8724 Sunset Drive #191Miami FL 33173 USA                                  

                                                  
Email:
info@generalequipment.infowww.generalequipment.info                                                       


 

 

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.

 

 

 

TAKE NOTICE!

 

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