XA-CMG - BAC 1 11 400


    This listing is currently not for sale or available for charter


    Aircraft Summary


    General

    Manufacturer
    BAC
    Model
    1-11-400
    Serial Number
    079
    Condition
    Used
    Registration #
    XA-CMG
    Description
    Prior Detroit Pistons AC, Fresh C Insp 3/05, 75K GW Mod for Stage III STC, Exec Conf.

    Airframe

    Total Time
    20029.0
    Airframe Notes
    LANDINGS 21454

    Engine Program

    Engine Program Notes
    ENGINES Rolls Royce 511-14 Spey Left Right Serial Number 7069 7074 Time Since New 16,111 14,169 Cycles Since New 19,000 16,372 Time Since Overhaul 3,111 2,925 Cycles Since Overhaul2,528 2.425 Date of Overhaul 5/25/82 9/22/82 Overhauled By AIRWORK AVIALL SP72-666 Midlife 9/4/91 8/4/92 Total Time @ Midlife 15,145 12,949 TSML 2,238 2,168

    Engine 1

    Engine 1 Time
    3153
    Engine 1 Time Since
    SOH

    Engine 2

    Engine 2 Time
    2967
    Engine 2 Time Since
    SOH

    Avionics

    Avionics/Radios
    F/D Dual Collins FD108 A/P Sperry SPG-50 COMMS Dual Collins 618M2 NAVS Dual Collins 51-RV1 GLIDESLOPE (Collins Part of Nav) RADAR Bendix RDR-1E (Dual Scope) 1 color, 1 monochrome ALT Dual IDC ALERTER IDC (Single) RAD/ALT Collins AL101 (Dual Ind) ADF Dual Collins 51Y-4 DME Dual Collins TRANSPONDER Dual Collins TDR-90 EF COMM Collins 618T-3 A/S INDICATOR Dual IDC A/S COMPUTER Garrett (Single) VLF Global 500X (VFR Only) HF Collins 618T-3 FLITE FONE Wulfsberg VI FLIGHT REC. Fairchild 10020-1 SELCAL Motorola CVR Fairchild A-113

    Additional Equipment

    Additional Equipment
    The aircraft is now operating with the STC @ 75,000 GW.. AIM Emergency Horizon; Rosemont Temp. Probe; BKM Pitot Heat Monitor; FAR 121 internal and external emergency lighting; FAR 121 intercom, PA and flight attendant station; FAR 121 floor level emergency lighting; 40,000’ Max. altitude modifications; 8.2 PSI cabin pressure modifications; In flight positive latch on rear stairs to prevent opening in flight; Rear internal storage; Factory installed fuel dump system.

    Exterior

    Year Painted
    2007
    Exterior Notes
    March 2007

    Interior

    Year Interior
    2007
    Interior Notes
    March 2007

    Inspection Status

    Inspection Status
    Fresh C Inspection – March, 2000 AIRCRAFT MAINTENANCE HISTORY The airplane was maintained by American Airlines from 1966 to 1974; from 1974 to February 1983 by Dresser Industries, Inc; by Jet Fleet International, from 1983 to 1987 and by Round Ball One from 1987 to the 2000. The present owner is operating the aircraft in Mexico for charters. THERE HAS BEEN NO MAJOR DAMAGE RECORDED SINCE THE AIRPLANE WAS NEW TO DATE. All maintenance has been performed by FAA certified repair stations. When done off site and under Guardian Industries maintenance department, work was done at home base. Interior modifications, avionics and electrical updates have been done by Airesearch Co., Los Angeles, California and Georgetown Aircraft Preparation and modifications for re-entry into commercial service under FAR Part 121 was completed by Jet Fleet International Airlines, Dallas, Texas in April, 1983. The Aircraft is currently operated under a Part 125/letter of waive 91 by Round Ball One. MAXIMUM OPERATING ALTITUDE 40,000 Fleet MAXIMUM TAKEOFF WEIGHT 87,000 Pounds MAXIMUM ZERO FUEL WEIGHT 68,500 Pounds FUEL CAPACITY Wings 2700 U. S. Gallons Fuselage 1026 U. S. Gallons BASIC OPERATING WEIGHT (Present Config) 52,264.25 Pounds BOW C.G. 572.20 Date of Last Weigh September 10, 1991 Landing Gear Landings Since OH 9/29/91 @ 18355 and 20156 Operating Under the 75,000 # GW, Aircraft Can: Fly 4 hours with reserve No Passengers 3-1/2 hours with reserve Five Passengers 2 hours with reserve Full Passengers INSPECTION PROGRAM This aircraft was recently maintained under the FAA approved Round Ball One Maintenance Program. The aircraft was delivered to American Airlines in 1966 and maintained under the AAL inspection program. The present inspection program is in compliance with British Aerospace Low utilization maintenance planning guide and the manufacturers recommended corrosion control program. Inspection system is Computer Monitored with all LUMPG items in compliance, which are performed as required. Unscheduled inspections are provided for following hard landings, lighting strikes, flight through turbulent air, etc. Special inspections, compliance with AD notes, Federal Aviation Regulations and control of life limited components are controlled through the use of the computer system (Columbia). The Corrosion Control Program as required by AD 93-02-14 and SB 5-A-PM59987 was initiated March 7, 1994 with a FAA approved computer program. The first compliance of all requirements was completed June, 1994. The system is currently controlled by monthly due list. Airframe and Engine Life limited components conform to the BAE Inc. Maintenance Planning Guide for low utilization operators.


    Click Here to find your Operating Cost


    Aircraft.com does not own the rights to the images displayed on this site. We do not have information regarding the original seller or source of these images unless explicitly stated.