GENERAL   EQUIPMENT   INC.                    

Aircraft Data

Aircraft Model:

Boeing MD-87

Date of Delivery:

1990

Engine Model:

Pratt & Whitney JT8D-217C

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:

112,000 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 February 25, 2008)

Total Flight Time:

32,083:28

Total Cycle:

31,979

Time since last "C" Check (Day)

365 Days

Time since last "C" Check (FH)

1,771 FH

Time remaining to next “C” Check

1,829 FH or 150 Days (whichever comes first)

Daily Utilization (FH vs. FC):

N/A

Maintenance History:

Item

Accomplish Data(Flight Hour)

No.5 "C":

March 21, 2007 (@ 30,312:51 FH)

No.4 "C":

December 19, 2005 (@ 27,878:42 FH)

No.3 "C":

September 30, 2004 (@ 25,474:58 FH)

No.2 "C":

June 29, 2003 (@ 21,124:34 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 17, 2008)

Maintenance Program:

20,000 Cycle or 10 Years

Position:

NLG

MLG-L/H

MLG-R/H

Serial Number:

CPI471

S0928

R7697

Install Date:

February 02,2008

April 17,2000

April 17,2000

Cycle since Last O/H:

2

14,429

14,429

Due Date for Next O/H:

March 01, 2017

December 07, 2009

April 10, 2010

Engine Status

(Engine: APU Data as of March 03, 2008)

Engine Model:

Pratt & Whitney JT8D-217C

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:

725907

728027

P-1045

Total Time:

28,110:35

23,844:00

25,774:18

Total Cycle:

28,837

23,906

27,943

LSV description:

ESV1

ESV1

Overhaul

LSV date:

February 22, 2008

May 30, 2007

October 27, 2006

Time since LSV:

0

1,594

1,881

Cycle since LSV:

0

1,518

2,143

LLP Remain Cycle:

9,295

6,910

-

　AD

February　07, 2017

December　19, 2013

Cabin Equipment

Cabin Arrangement No.:

N02

Equipment:

Item

Manufacturer

Qty

Seats:

Tenryu Industries

Total 134 (F:0/C:0/Y:134)

Galleys:

Nordskog

1

Lavatories:

JAMCO

2

Avionics

System

Qty

Description

Vendor

Model or Part Number

Digital Flight Guidance System

2

Digital Flight Guidance Computer

Honeywell

4034241-971 or -973

1

Flight Guidance Control Panel

Honeywell

4034242-934

HF System

2

HF Communication Tranceiver

Collins

618T-5 or 628T-2A with 999W-2

1

(Provision only)

VHF System

2

VHF Communication Tranceiver

Collins

618M2D, 618M3 or 618M3A

SELCAL System

1

SELCAL Decoder

Motorola

N1335B

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

GNSS, GFMS

1

Flight Management Unit

CMC

100-601900-202

Performance Management System

1

PMS Computer Unit

Delco

7892551-011-010

Enhancement Status - AVIONICS

Compliance

8.33 KHz channel spacing on VHF radio

Not

EGPWS

Yes

TCAS Change 7.0

Yes

RVSM Capability

Yes

BRNAV/PRNAV

Not

ATC mode S Transponder

Yes