1971 BOEING 727 100


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    Aircraft Summary


    General

    Year
    1971
    Manufacturer
    BOEING
    Model
    727-100
    Condition
    Used
    FlightRules
    IFR
    Description
    This very late production B727 100 has 200 landing gear, fuel tank system, pressurization and Autopak trip. Forward airstair door. LOWEST HOURS AND CYCLES OF ANY 727 100. NEVER IN AIRLINE SERVICE! HUGE SPARE PARTS PACKAGE!!!!!

    Airframe

    Total Time
    11794
    Total Landings
    5466
    Range
    4,000 NM
    Max Takeoff Weight
    175,000 lb
    Fuel Capacity Mass
    71,000 lb
    Winglets
    Yes
    Maintenance Tracking
    None
    Airframe Notes
    Lowest hours and cycles on any B727-100 in the world. One of last built with some 200 upgrades. Valsan 100 has about 500 or more miles extra range due to lower gross weight which gives lower fuel burns and higher climb altitudes quicker. 4000+ NM Many avionics upgrades with EFIS.

    Engine Program

    Engine Maintenance Program
    None
    Engine Program Notes
    All engines had Corrosion Inspections about two years ago.

    Engine 1

    Engine 1 Manufacturer
    PRATT & WHITNEY
    Engine 1 Model
    JT8D-217C
    Engine 1 Notes
    3412 TTSN 1102 TCYSN Fresh Corrosion Inspections 2017 (9 year Interval)

    Engine 2

    Engine 2 Manufacturer
    PRATT & WHITNEY
    Engine 2 Notes
    11,147 since new. 5917CYSN 8 year inspections done two years ago

    Engine 3

    Engine 3 Manufacturer
    PRATT & WHITNEY
    Engine 3 Model
    JT8D-217C
    Engine 3 Notes
    3412 TTSN 1102 TCYSN Fresh Corrosion Inspections 2017 (9 year Interval)

    Auxiliary Power Unit

    APU
    Yes

    Avionics

    Avionics/Radios
    EFIS: Digital Collins 86-C IRS: Honeywell Lasernav II COMM: Dual Collins 618M-2B with 8.33 kHz Spacing NAV: Dual Collins VIR-32 DME: Dual Collins DME-42 ADF: Dual Collins 51Y-2 Selcal: Jetcall 5 HF: Dual Collins 618-T2B with Selcal Rad Alt: Dual Collins 860-Fl Trans: Dual Collins TDR-94 with FM Immunity FMS: Dual Universal UNS-1L Radar: Collins WXT-250B FAS: Collins PRE 8OB Autopilot: Sperry SP-50-G TCAS: TCAS II Version 7 CVR: Yes FDR: Yes RVSM: Yes EGPWS: Honeywell SATCOM: Iridium EXTERIOR:Lower fuselage is Navy. Upper fuselage is White with Blue and Graystone coach lines. There is only one small patch on the entire fuselage. No doublers. INTERIOR:The 25 passenger cabin was designed by Donald Thompson and Associates. It is upholstered in Cream and Taupe leather and cloth. Manual accordion window shades. Forward Entryway: Entry to the aircraft is via built in airstairs which retract into the left side cabin, aft of the entry door. Right side crew galley and storage area. Forward right side toilet and vanity, hanging clothes closet.

    Additional Equipment

    Additional Equipment
    FULL VALSAN CONVERSION WITH NEW ENGINES FOR #1 & #3, Winglets,etc. at a cost of over $10,000,000. BOEING LONG RANGE FUEL TANKS 175K MGTOW INCREASE

    Exterior

    Year Painted
    2000
    Exterior Notes
    White top half with dark blue Belly.

    Interior

    Number of Seats
    25
    Galley
    Yes
    Galley Configuration
    Forward and Aft
    Crew Rest
    Yes
    Crew Rest Configuration
    Forward
    Lavatory
    Yes
    Lavatory Configuration
    Forward and Aft
    Interior Notes
    Forward Crew Galley, main living area Club seating next, Master bedroom and Bathroom with double club seating pax seating and lavs after that. Crème and Taupe leather with light wood laminates. Very Nice

    Modifications/Conversions

    Modifications/Conversions
    FULL VALSAN CONVERSION (Cost over $10,000,000 for new engines, Winglets, etc.) FLAP DROOP SYSTEM, (Increased range) SATCOM BOEING LONG RANGE TANKS (8 hours plus) IN FLIGHT ENTERTAINMENT WITH LARGE VIDEO SCREEN

    Inspection Status

    Inspection Status
    Plane has been stored for over one year and C Inspections are now due, We have Landing gear that was overhauled two years ago and only about 30 landings since then that is available for installation on this aircraft with low total hours from new.


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