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    1983 MESSERSCHMITT BO105P1983 MESSERSCHMITT BO105P
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    1983 MESSERSCHMITT BO105P

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    Aircraft Summary

    General
    Year
    1983
    Manufacturer
    MESSERSCHMITT
    Model
    BO105P
    Condition
    Used
    Description
    MBB BO-105 P1M Helicopter with FAA Approved Aircraft Inspection Program (AIP) COMPLETE! 
TTSN: 4632 HR
Airframe Landings: 7967

Maintenance is hour-based or condition-based, NOT calendar-driven, this aircraft is FULLY operational, with its Annual Inspection recently completed - Books are impeccable! 
Aircraft has been consistently stored in a temperature-controlled hangar, ensuring excellent preservation.
* Twin Engine Allison 250-C20B Turboshaft Engines:  840 hp, 130 knots cruise speed, 380 nm range -superior safety redundancy. 
* Rigid Titanium Rotor System: Cleared for +3.5G/-1G, composite rotor blades.
* Up to 5 Passenger Capacity: With rear clamshell doors for easy loading & ample storage.
* Excels at 11,000+ ft hover ceilings and high-temperature conditions, perfect for extreme environments.

FAA "EXPERIMENTAL EXHIBITION" Certified                 
*Blade Folding Kit AVAILABLE for tight spaces - Additional Fee*
    Airframe
    Total Time
    4632
    Range
    380 NM
    Max Takeoff Weight
    5,512 lb
    Max Cruise Speed
    130 knots
    Crash-Resistant Fuel System
    Yes
    Complete Logs
    Yes
    Rotor
    Rotor Notes
    ~~~~~~~~~~~~~~~~~~  TSO           Time Remaining
Main Rotor Blade #1      2144 FH         7855 FH
Main Rotor Blade #2     3043 FH        6957 FH 
Main Rotor Blade #3     3043 FH        6957 FH
Main Rotor Blade #4     2038 FH        7961 FH
Rotor Mast                     4591 FH        4409 FH
Tail Rotor Gear Box         767 FH        O/C
Intermediate Gear Box   1995 FH       O/C
Main Transmission 
Gear Box                          901 FH          O/C

Hydraulic Pumps: 
Pump #1                           2017 FH           383 FH
Pump #2                             495 FH         1905 FH
    Engine 1
    Engine 1 Manufacturer
    ROLLS ROYCE
    Engine 1 Model
    M250-C20B
    Engine 1 Notes
    ENGINE #1: 250-047        4708.8 FH (SNEW)
ROLLS-ROYCE Allison Engines
** Below FH Time Remaining to Overhaul **
Engine Turbine Module  2999.05 FH
Turbine Wheel #1             1274.05 FH
Turbine Wheel #2            1258.21  FH
Turbine Wheel #3            4353.76 FH
Turbine Wheel #4            4353.76 FH
Compressor Module        3064.99 FH
PT N2 Governor              1432.99 FH
FCU N1                            1114.07 FH
Fuel Pump                        2257.90 FH
Bleed Valve Assembly      1414.07 FH
    Engine 2
    Engine 2 Manufacturer
    ROLLS ROYCE
    Engine 2 Model
    M250-C20B
    Engine 2 Serial Number
    250-643
    Engine 2 Notes
    Rolls-Royce Allison 
ENGINE #2: 250-643        4708.8 FH (SNEW)
** Below FH Time Remaining to Overhaul **
Engine Turbine Module  2525.48 FH
Turbine Wheel #1               800.48 FH
Turbine Wheel #2              800.48 FH
Turbine Wheel #3              1601.64 FH
Turbine Wheel #4              1601.64 FH
Compressor Module          1441.21 FH
PT N2 Governor                 465.83 FH
FCU N1                              948.61 FH
Fuel Pump                        1680.51 FH
Bleed Valve Assembly       536.36 FH
    Modifications/Conversions
    Modifications/Conversions
    ** High Lift Blades
** Next Generation Tail Rotor Blades
** Dual Controls
    Avionics
    ADS-B Equipped
    Yes
    WAAS
    Yes
    Artificial Horizon
    Yes
    Avionics/Radios
    ~Garmin GTR200B COM Radio w/ Bluetooth 10 Watt25kHz
~GTX 327 Transponder/Timer GARMIN
~UAvionix Tailbeacon W/TSO NAV light, WASS ~GPS, ADS-B Out Transmitter
~VSI, MAG Compass, Altitude Gryo. VSI/OAT Gauge
~2 Becker Intercommand Audio Panel
~MIL Spec VHF Com's
~Full MIL Spec Avionics
    Exterior
    Year Painted
    1983
    Door Type
    Hinged and Sliding
    Exterior Notes
    Camo Matte Paint
    Interior
    Year Interior
    1983
    Number of Seats
    5
    Soundproofing
    Yes
    Interior Notes
    Original cloth seats: Pilot & Co-pilot and back bench seats (3 people)


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