Boeing 737 Advanced

ENGINES

ENGINE MODEL NUMBER JT8D-17
ENGINE MANUFACTURER PRATT & WHITNEY

RE ENGINE SERIAL NUMBER 702744B 7420.50 HOURS 4252 CYCLES 1632 TSOH
LE ENGINE SERIAL NUMBER 702757B 7420.50 HOURS 4252 CYCLES 1632 TSOH


APU ; GARRETT GAS TURBINE
Garrett GTCP 85-129
Serial Number P35444
Total Time ; 6638
Hobbs Time ; 754

Avionics

ELT 95N6088 96-39-0034 406 MHz
COMM COLLINS 822-1045-001 4743 8.33
COMM COLLINS 822-1045-001 10968 8.33
COMM COLLINS 822-1045-001 4743 8.33
SELCAL MOTOROLA NA134D2 145454
CVR SUNDSTRAND 980-6005-050 5442
TAWS UNIVERSAL 3010-00-00 1040
AIRSPEED 1 2083-09-1 145
AIRSPEED 2 2083-09-1 422
ALTIMETER 1 JG865C3 W-35
ALTIMETER 2 JG865C3 O-27
RADIO ALT 1 COLLINS 522-4825-001 3853
RADIO ALT 2 COLLINS 522-4825-001 3839
STDBY ALT WL102AM52 AG533
ADC 1 HONEYWELL HG480B13 M1218
ADC 2 HONEYWELL HG480B13 90112031
HS I 1 722-5025-001 7F668
HS I 2 722-5025-001 1H1557
ADI 1 722-5005-005 J7425
ADI 2 722-5005-005 6A240
RMI 1 1784460-655 82016489
RMI 2 1784460-655 9052508
FLT STEER COMP 1 COLLINS 622-2500-004 82016489
FLT STEER COMP 2 COLLINS 622-2500-004 9052508
IRU 1 LITTON 463001-8100-0413 2534 LTN-92
IRU 2 LITTON 463001-8180-0413 2538 LTN-92
RADAR RT SPERRY MI585161 2118
RADAR ANTENNA SPERRY MI585164-1 1950
TAWS UNIVERSAL 965-0476-088 2959
TCAS II ALLIED SIGNAL 066-50000-2220 9010 TPA-18A / ACAS II
LOW RANGE RAD ALT 1 COLLINS 622-3890-114 1279
LOW RANGE RAD ALT 2 COLLINS 622-3890-114 372
DME 1 COLLINS 622-2921-002 5910
DME 2 COLLINS 622-2921-002 5896
TRANDSPONDER 1 HONEYWELL 066-01127-1602 12127 MODE S ENHANCED ID
TRANDSPONDER 2 HONEYWELL 066-01127-1602 6044 MODE S ENHANCED ID
VOR/ILS COLLINS 622-3257-001 2795
VOR/ILS COLLINS 622-3257-001 2788
ADF 1 COLLINS 777-1492-005 15250
ADF2 COLLINS 777-1492-005 8087
FMS UNIVERSAL 1017-41-211 952 UNS-1
FDR SUNDSTRAND 980-4100-GOUS 4557 MEETS FAR 121.344 (b) (1)
HF 1 COLLINS 622-3371-001 4084
HF 2 COLLINS 622-3371-001 2395
MARKER RCV COLLINS 522-2996-011 14298
AIRSHOW 400 AIRSHOW 920050 1188
MAGNASTAR MAGNASTAR 724855 0686 C-2000
AIRCELL AIRCELL 401-11050-001 1105010074 ST3120
ROLL CONTROL CMP SPERRY 2588812-904 06811399
PITCH CONTROL CMP SPERRY 2588810-904 07801203

Features & Additional Equipment

In addition to the usual equipment of the 737-200 advanced, this aircraft has the following:

++ Twin, fully coupled (autopilot and flight director) Litton LTN72RL Inertial Navigation Systems with Navigation data base covering Europe, the Middle East and North Africa.
++S Single Universal UNS-1C Flight Management System.
++ Auxiliary Fuel System of 2,800 US gallons, manufactured by PATS Inc. giving a still-air range of approximately 3,800 nautical miles with NBA I.F.R. reserves.
++ Forward and rear cargo bay fire suppression system with automatic (infra-red or firewire) or manual discharge initiation giving cargo bay fire extinguishing with follow on “trickle” discharge for 2 hours 15 minutes (Halon level above 5%). Installation was completed in 1989.
++ Ramp-guard aircraft ground Security system installed.
++ Cold spare battery in stowage adjacent to main battery.
++ Floor proximity escape-path markings in forward and aft passenger cabins installed in Nov 88.
++ Allied Signal TCAS II Installation.
++ Forward crew toilet with wash basin.
++ Forward galley just aft of the cockpit equipped with coffee maker, ice box, drink stowages, etc.. Two flight attendant seats adjacent to the forward left hand main entry door.
++ Forward stateroom seating five passengers in a two seat/three-place berthable divan layout. Couch folds down to become a bed. Stateroom has its own Entertainment System with VIP lavatory/washroom adjoining.
S Large forward cabin seating twelve passengers at two four-place dining tables and on two two-place couches. The forward end of the cabin features a refreshment cabinet and full entertainment center. (There are two DVD players with five monitors situated around the cabin which show either the boarding video, movies or the Airshow 400.)
++ Large rear cabin seating ten passengers in two four-place groups around demountable folding tables and one two-place group with console table. This cabin features a large carry-on baggage stowage with folding internal shelves to allow the stowage of large items of baggage within the area. There are two large monitors in this cabin.
++ Rear galley with coffee maker, espresso machine, convection oven, bread warmer, boiling water spigot, hot and cold water faucet serving twin stainless steel sinks, ample cutlery and crockery stowage, large work surfaces and stowages for eight airline tray carriers. Two flight attendant seats in this location.
++ Rear full lavatory with full wash basin.

Interior & Exterior

INTERIOR NEW DECEMBER 2008 – Indianapolis Jet Center
19 PAX Seats certified for take-off and landing. No Expenses have been spared on this All New Custom Interior, including new wood, new plating, new entertainment system and completely new soft goods throughout. The interior has been tastefully appointed in neutral and elegant beige earthtones throughout.

EXTERIOR NEW JANUARY 2007 – Bizjet International

Overhaul Matterhorn White with Midnight Blue and Hunter Green accent stripes

History

This aircraft was purchased new from Boeing as a B737-200 Advanced, delivered from Boeing in October 1981 on the Swiss registry. The VIP Completion was facilitated by Air Research Aviation in Long Beach, California, for the installation of the 27 passenger (plus four flight attendants) corporate interior and auxiliary fuel tanks.

The final interior was completed in November 1982 and the aircraft entered service at that time. The original owner was owner operator by Petrolair System S.A. until 1997 when it was purchased and operated by the world renowned mogul Wayne Huizenga. The aircraft has been used solely for the transportation of private passengers and has never been used for public transport (hire and reward) or for charter. The aircraft has been maintained at major facilities in the United States and maintains the aircraft under the Daniels Low Utilization program. It has no damage history.


Weights

Max. taxi gross weight: 128,600 lbs.
Max. take_off weight: 128,100 lbs.
Max. flight weight (flaps 30 or 40): 108,000 lbs.
Max. landing weight: 107,000 lbs.
Max. zero fuel weight: 95,000 lbs.
Empty weight: 74,304 lbs.
(Empty weight A.P.S. weight less crew weight)
Max. wing fuel (2x10,132): 20,264 lbs.
Max. centre tank fuel: 16,344 lbs.
Max. aux. Fuel (2850 gal): 19,095 lbs.
Total fuel (7+8+9): 55,703 lbs.
Full fuel weight (l0)+(6): 127,418 lbs.
Full fuel payload (l)-(11): 1,182 lbs.
Maximum Payload (5)-(6): 23,285 lbs.
Full pax. Fuel: 49,885 lbs.

Additional Structural / Operational Data

++ The aircraft can fly approximately 3,800 nautical miles with NBAA reserves with full fuel, taking off at MTOW
++ Max. operating altitude 37,000 feet.
++ Operating Temperature limits 130 F to -100 F. (Above 8300 ft. - 100.6 F).
++ Acoustical limit max. landing wt. 78,200 (Flaps 40 dgrees).
++ Boeing forward airstair.
++ Internal locks on all exits (including r/h cockpit DV window) except forward left-hand passenger door which is externally lockable. Airstair operation is controlled by the same key.
++ Extensive additional corrosion protection.
++ Passive flame arrestors in the fuel tank vent system.
++ Fuel level measuring sticks calibrated in pounds.
++ First and second observers seats (cockpit).