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1981 BOEING 737-200
Serial: 22431/803
Registration: N787WH
Omni No.: P4028
Unit No.: PL471
Airframe Total Time: 7,370
Landings: 4229
| Engines: Pratt & Whitney JT8D-17 |
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#1 |
#2 |
| Serial Number: |
702744B |
702757B |
| Hours: |
7420.50 |
7420.50 |
| Cycles: |
4252 |
4252 |
| TSOH: |
1632 |
1632 |
| APU: GARRETT GAS TURBINE Garrett GTCP 85-129 |
| Serial Number: |
P35444 |
| Total Time: |
6638 |
| Hobbs Time: |
754 |
| 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 19 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 |
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| Paint and Interior: |
| Exterior: NEW JANUARY 2007 – Bizjet International |
| Overhaul Matterhorn White with Midnight Blue and Hunter Green accent stripes |
| 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. |
| Avionics: |
| ITEM |
MANUFACTURER |
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NOTE |
| ELT |
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406 MHz |
| COMM |
COLLINS |
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8.33 |
| COMM |
COLLINS |
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8.33 |
| COMM |
COLLINS |
|
8.33 |
| SELCAL |
MOTOROLA |
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| CVR |
SUNDSTRAND |
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| TAWS |
UNIVERSAL |
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| AIRSPEED 1 |
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| AIRSPEED 2 |
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| ALTIMETER 1 |
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| ALTIMETER 2 |
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| RADIO ALT 1 |
COLLINS |
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| RADIO ALT 2 |
COLLINS |
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| STDBY ALT |
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| ADC 1 |
HONEYWELL |
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| ADC 2 |
HONEYWELL |
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| HS I 1 |
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| HS I 2 |
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| ADI 1 |
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| ADI 2 |
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| RMI 1 |
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| RMI 2 |
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| FLT STEER COMP 1 |
COLLINS |
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| FLT STEER COMP 2 |
COLLINS |
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| IRU 1 |
LITTON |
|
LTN-92 |
| IRU 2 |
LITTON |
|
LTN-92 |
| RADAR RT |
SPERRY |
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| RADAR ANTENNA |
SPERRY |
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| TAWS |
UNIVERSAL |
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| TCAS II |
ALLIED SIGNAL |
|
TPA-18A / ACAS II |
| LOW RANGE RAD ALT 1 |
COLLINS |
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| LOW RANGE RAD ALT 2 |
COLLINS |
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| DME 1 |
COLLINS |
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| DME 2 |
COLLINS |
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| TRANDSPONDER 1 |
HONEYWELL |
MODE S |
ENHANCED ID |
| TRANDSPONDER 2 |
HONEYWELL |
MODE S |
ENHANCED ID |
| VOR/ILS |
COLLINS |
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| VOR/ILS |
COLLINS |
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| ADF 1 |
COLLINS |
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| ADF2 |
COLLINS |
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| FMS |
UNIVERSAL |
|
UNS-1 |
| FDR |
SUNDSTRAND |
|
MEETS FAR 121.344 (b) (1) |
| HF 1 |
COLLINS |
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| HF 2 |
COLLINS |
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| MARKER RCV |
COLLINS |
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| AIRSHOW 400 |
AIRSHOW |
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| MAGNASTAR |
MAGNASTAR |
|
C-2000 |
| AIRCELL |
AIRCELL |
|
ST3120 |
| ROLL CONTROL CMP |
SPERRY |
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| PITCH CONTROL CMP |
SPERRY |
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| Additional Features: In addition to the usual equipment of the 737-200 advanced, this aircraft has the following: |
S 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.
S 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.
S 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.
S Ramp-guard aircraft ground Security system installed.
S Cold spare battery in stowage adjacent to main battery.
S Floor proximity escape-path markings in forward and aft passenger cabins installed in Nov 88.
S Allied Signal TCAS II Installation.
S Forward crew toilet with wash basin.
S 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.
S 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.)
S 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.
S 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.
S Rear full lavatory with full wash basin. |
| ADDITIONAL Structural/Operational Data: |
S The aircraft can fly approximately 3,800 nautical miles with NBAA reserves with full fuel, taking off at MTOW.
S Max. operating altitude 37,000 feet.
S Operating Temperature limits 130°F to -100°F. (Above 8300 ft. - 100.6°F).
S Acoustical limit max. landing wt. 78,200 (Flaps 40°).
S Boeing forward airstair.
S 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.
S Extensive additional corrosion protection.
S Passive flame arrestors in the fuel tank vent system.
S Fuel level measuring sticks calibrated in pounds.
S First and second observers seats (cockpit). |
| 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. |
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Aircraft Specifications Subject to Verification Upon Inspection. Aircraft Subject to Prior Sale or Withdrawal from the Market. |
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Ask for more details about the for Sale of this aircraft:
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The following details, identifying this aircraft, are automatically included in your inquiry. Re: 1981 Boeing 737-200 For Sale Serial: 22431
Reg: 787WH |
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