OFFER#

SHORTS SD360-1

TYPE:	Aircraft
DESCRIPTION:	Shorts SD360-200
PRICE:	Upon Request
PACKING:	As Is, Where Is

SHORTS SD360-200

The aircraft features 36 passenger seats, a large forward cargo door, one recently overhauled engine, and freshly overhauled nose landing gear

type / model	Short SD3-60-200
mgtow	26,453 lbs.
total hours	33,271
total cycles	53,734
engines	Pratt & Whitney Canada PT6A-65AR
Propellers	Hartzell HC-B5MP3

Aircraft Airframe

Type and Model: SD3-60 200 Total Aircraft time: 33,271:25

Serial Number: SH3621 Total Aircraft cycles: 53,734

Configuration: 36 seats

Aircraft Status: Operational

Year of Manufacture: 1983

Weights

Maximum Takeoff: 26,453 lbs
Empty Weight: 17,131 lbs

Maximum Landing: 26,100 lbs
Payload 8,300 lbs

Maximum Ramp Weight:
26,553 lbs
Fuel Capacity: 576 gals

Landing Gear

Nose Gear Remaining

DRG/5133/84
OVH 10,500
10,500

DRG/5822/85 SLL 50,000 37,524

Sliding Tube OVH 10,500 10,500

SLL 55,000 45,524

Downlock Actuator OVH 10,500 10,500

SLL 50,000 21,047

Main Gear
Left

DRG/4/82 OVH 15,000 3,716

Wheel Lever SLL 70,000 26,610

DRG/6646/84 OVH 15,000 5,307

Drag Brace SLL 50,000 20,708

DRG/7751/83 OVH 15,000 5,305

Shock Absorber SLL 50,000 15,326

DRG/2537/84 OVH 15,000 928

Rear Pintle Pin SLL 50,000 20,490

DRG/14/83 OVH 15,000 2,573

Forward Pintle Pin SLL 75,000 48,401

DRG/6254/88 OVH 15,000 3,713

Retract Actuator SLL 50,000 18,846

Main Gear Left

DRG/5170/84 OVH 15,000 3,716

Wheel Lever SLL 70,000 25,802

DRG/745/88 OVH 15,000 2,790

Drag Brace SLL 50,000 23,208

DRG/7751/83 OVH 15,000 5,305

Shock Absorber SLL 50,000 25,504

DRG/8733/88 OVH 15,000 5,061

Rear Pintle Pin SLL 50,000 24,746

DRG/5907/85 OVH 15,000 5,064

Forward Pintle Pin SLL 50,000 30,565

DRG/4591/85 OVH 15,000 3,716

Retract Actuator SLL 50,000 22,259

Propellers

Type & Model: Hartzell HC-B5MP-3

Propeller TBO: 3,000 FH/ 60 months

Left Prop Right Prop

Serial Number: EVA 2526
EVA 2242

Hours remaining: 2,798.7
83.3

Time remaining: 58 months 23 months

Maintenance Program

Program Checks

IAW Shorts MRB

Calendar/Cyc/Hrs Rem.

3000CY/24MO
2699CY/22MO

3600FH/18MO 2413FH/7MO

4800FH/24MO 3619FH/15MO

4800FH/48MO 2626FH/20MO

9600FH/48MO 2699CY/22MO

14400FH/72MO 10173FH/21MO

1C-1200FH/12MO 97FH/3M0

2C-2400FH/24MO 1319FH/15MO

3C-3600FH/36MO 2519FH/27MO

1,5,9C-4800FH/48MO 2626FH/20MO

3,7,11C-4800FH/48MO
2626FH/20MO

D-4800FH/48MO
2626FH/20MO

2D-9600FH/96MO
3691FH/20MO

E14400FH/144MO
8491FH/68

Weight & Balance 36mo
15 mo

Engines

Type & Model: Pratt & Whitney PT6A-65AR
Engine TBO: Hard Time TBO 6,000 hrs

Hot Section 2,000

Left Engine Right Engine

Gas Gen Power Sec Gas Gen Power Sec

Serial Number: PCE 97123 PCE 97123 PCE 97057 PCE 97057

Hrs since new: 30,458.6 30,458.6 48,485
48,140

Cycles since new: 48,001 48,001 8,883.2 8,691.7

Hrs since overhaul: 83.6 83.6 18,689 18,344

Cycles since overhaul: 188 188 TBD

Time since hsi: n/a 1437.6

Cycle Limiter:
CT Disk – 2,359 remaining
1st & 2nd Stg PT - 38 remaining

Avionics Listing

VHF Comm: Dual Collins VHF-20,21
GPWS: Honeywell MK6 W/GPS

VHF Nav (VOR/ILS): Dual Collins VIR-30
FDR: Plessey

ADF: Dual Collins ADF-60
Compass System: Collins MC8-65

DME: Collins DME-40
Cabin Briefer/Pax PA: Collins 3460-2B

Transponder #1: Collins TDR-90
RMI: Dual Collins RMI-36

Transponder #2: Collins TDR-940
Flight Director Dual Collins FGC-65

TCAS: Collins TTR-920 Audio Panel: Dual Collins 346-B3

Marker Beacon: RMI: Dual Collins RMI-36

Radar Alt: Honeywell HG7502AC02 GPS KLN-90B

Weather Radar: Collins WXR-220 Attitude Dir. Ind.: Dual Collins ADI-84

CVR Fairchild A100A HSI Dual Collins HSI-70

Vertical Gyro: Dual Collins 332D-11T

Data as of July 2, 2008. Specifications are not guaranteed and any offer for the aircraft is subject to purchaser’s review and verification. Aircraft is subject to removal from market without notice.

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.