ENGINES

Make                              Pratt & Whitney

Model                             JT 8 D – 217 C

Description                   Two- shaft High- Bypass Turbofan

Engine thrust               20,000 pound- thrust

The engines offer Stage 3 noise compliance standards without the need for hush kits, enhanced short field performance, steeper and faster climb rates with roughly a 10 % reduction in fuel burn for extended range.

BAGGAGE COMPARTMENTS

Total - Forward, Mid & Rear                 937 cu / FT (26.5 CUm )

 

ENHANCED AVIONICS

RVSM Certified

TCAS Change 7. 0

Mode S Transponder EGPWS

STANDARD AVIONICS

2 x Digital Flight Guidance System:     Honey well 4034241- 971 or - 973 HF Radio: Collins 618 T- 5 or 628 T-2 A

2 x VHF Radios:                                 Collins 618 M 2 D, 618 M 3 or 618 M 3 A

Voice Recording System:                    Honey well 965 - 6005 - 076 or - 076 ULD Flight Recorder System: SDC 980 - 4100 - DXUS

2 x Air Data Computing System:          Honey well HG 280 D 80

2 x Gyrosyn Compass System:           Sperry DG-206 A or 2588302- 4 2 x Altitude System: Honey well 2587335 -13 or -113

Marker Beacon System:                      Collins 51Z- 4 2 x VOR / ILS System: Collins 51RV- 4

Weather Radar System:                      Bendix RTA- 4 A

2 x Radio Altimeter System:                T. R.T 9599 - 607-14908 EGPWS: Honey well 965 -1076 - 020 -214 -214

TCAS:                                                Collins 622- 8971- 022

Windshear Alert a System:                    Honey well 4059845 - 911 2 x DME System: Collins 8 . 6 E- 03

2 x ADF System:                                  Collins ADF-700

2 x ATC Transponder System:               Collins TPR-720

Performance Management System:D elco 7892551- 011- 010

 

INTERIOR CABIN

Forward Cabin

Two Forward Gal leys

Forward Closet

Forward Hallway Credenza /Side Ledge

Flight Attendant Stat ion

VIP Stateroom (located in front)

Stateroom Bed

Night Stand

20” Bulkhead Video Monitor

Stateroom Closet

Stateroom Toilet and Sink

Stateroom Vanity & Mirror

VIP Lounge

3 VIP Seats

3-place Divan

31” Video Monitor

High-Lo Conference/Coffee Table

Desk

2 Credenzas

Sidewall Table

Pocket Door

 

First Class Cabin

9 VIP Seats

Overhead Bins, LH Only

3 Centre Cabinets

Dr ink Rail, RH Only

Curtain between First & Coach

Premium Coach Seating/AFT Galleys / Lavatories

21 Premium Coach Seats with Extended Leg Room

2–24” Bulkhead Video Monitors

Overhead Bins

Food Service Area consisting of 3 Galleys

SAT Phone and IFE Instrument Closet

2 AFT Lavatories

AFT Flight Attendant Seat

Interior

36 Passenger Configurations completed in June 2012

EQUIPMENT SPECIFICATIONS

Delivery                         Date August 11, 1991

Manufacturer              McDonnell Douglas

Model                         DC-9-MD-87

Condition                    Used, New Interior & IFE Systems as of June 2012

Registration                 N Reg Aircraft

Total Time                   29,595.6 FLT HRS / 29,599 CYC

 

Delivered with newly completed C Check

Capacity                       36 plus crew

Engine Type                 JT8D-217C

DETAILED DESCRIP TION

Maxim Ramp Weight 141,000 lb

Maxim Take-off Weight 140,000 lb

Maxim Landing Weight 128,000 lb

Maxim Zero-Fuel Weight 112,000 lb

Ceiling 37,000 F T

PERFORMANCE

Max speed 925km/h (500kt), long range cruising speed 811km/ h (438kt).

Range with 130 passengers and reserves 4393km, (2372nm) , or optionally 5248km (2833nm). Range with max fuel 5522km (2980nm), or optionally 6764km (3650nm).

SATCOM SUMMARY REGARDING BROADBAND INTERNET, SPEED AND COST WHILE FLYING

1) Internet Broadband Speed = 332KB/SEC