N5125 - 1995 SAAB 2000


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    Aircraft Summary


    General

    Year
    1995
    Manufacturer
    SAAB
    Model
    2000
    Serial Number
    2030
    Condition
    Used
    Registration #
    N5125
    Description
    General Motors, the original owner since new, purchased the Saab 2000s to replace their Convair 580s. All three aircraft were utilized as corporate shuttles. The division that the aircraft were supporting was sold and subsequently the aircraft became excess to General Motors’ existing fleet. TCAS, Collins IFR, WXP-4220 Weather Radar, EFIS

    Airframe

    Total Time
    1991.0

    Avionics

    Avionics/Radios
    FMS (FLIGHT MANAGEMENT SYSTEM): CDU-4100 Control Display Unit FMC-4100 Flight Management Computer (in IAPS) DBU-4000 Data Base Unit (DSDD Disk Drive) GPS-4000 GPS RSS (RADIO SENSOR SYSTEM): RTU-4010 Radio Tune Unit VHF-422A VHF Comm Transceiver VIR-432 VHF Navigation Receiver DME-442 DME Transceiver ADF-462 ADF Receiver ANT-462 ADF Antenna (dual) ALT-55B Radio Altimeter ANT-52 Radio Altimeter Antenna RAC-870 Radio Altitude Converter TDR-94D Mode-S Transponder TTR-920 TCAS Transmitter Receiver TRE-920 TCAS Directional Antenna WXR WEATHER RADAR SYSTEM: RTA-854 Receiver/Transmitter/Antenna (turb) WXP-4220 Weather Radar Control Panel (turb) IAPS ASSEMBLY: ICC-4001 IAPS Card Cage CSU-4000 Configuration Strapping Unit IEC-4000 IAPS Environmental Controller IOC-4000 I/O Concentrator LHP-4000 Lightning/HIRF Protection (Left) LHP-4001 Lightning/HIRF Protection (Right) MDC-4000 Maintenance Diagnostic Computer PWR-4000 IAPS Power Supply EFIS (ELECTRONIC FLIGHT INSTRUMENT SYSTEM): DCP-4001 Display Control Panel EFD-4077 Electronic Flight Display (PFD, MFD) INC-4000 Inclinometer EICAS (ENGINE INDICATION/CREW ALERTING SYSTEM): DCU-4001 EICAS Data Concentrator ECP-4001 EICAS Control Panel EFD-4077 Electronic Flight Display (ED) LDU-4000 Lamp Driver Unit ADS (AIR DATA SYSTEM): ADC-850B Air Data Computer ARP-4001 Air Data Reference Panel AHS (ATTITUDE HEADING SYSTEM): AHC-85E Attitude Heading Computer FDU-70 Flux Detector Unit ICU-85 Internal Compensation Unit FCS (FLIGHT CONTROL SYSTEM): APP-85A Autopilot Panel ATC-4000 Automatic Trim Coupler FCC-4003 Flight Control Computer (IAPS) FCP-4001 Flight Control Panel SVO-85B Primary Servo (elevator) SVO-85B Primary Servo (aileron) SMT-85B Servo Mount

    Exterior

    Exterior Notes
    The exterior is painted white with a blue stripe.

    Interior

    Interior Notes
    The interior has 36 seats in “stretched” airline configuration. The first 5 rows have a seat pitch of 36 inches and the remaining 7 rows have 34 inches. The seats are covered in blue leather. Additional carry-on storage has been added in the forward cabin. An electronic noise suppression system, or Active Noise Control (ANC) enhances cabin comfort. There is a large lavatory in the forward cabin and well equipped galley in the aft section.

    Inspection Status

    Inspection Status
    The aircraft have been maintained in accordance with the Saab Maintenance Review Board (MRB) low utilization program since new. All will have a fresh “C” check and freshly overhauled propellers. Status sheets available upon request.


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