XA-CMG - BAC 1 11 400
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.
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