A9C-DAA - 1979 BOEING 737 200 EXECUTIVE

1979

BOEING

737-200 EXECUTIVE

22050

A9C-DAA

Used

The B737-268, MSN 22050 was manufactured during November 1979, delivered to Saudi Arabian Airlines (SAA) on 14 December 1979 and registered as HZ-AGT. The Aircraft registration was then changed to HZ-HM4 on 11 January 1980 for use as part of the Saudi Royal Fleet. When it was acquired by Mercury AVV (MAVV) in May 2004 the registration was changed to P4-OMC. Now the aircraft is under Bahrain registry and the registration number is A9C-DAA operated by Delmun Aviation Services. The transfer of ownership has been facilitated by International Aviation and Services Group (IASG), a UK based group, from Saudi Arabian Airlines to Mercury AVV. The Aircraft underwent heavy maintenance check at Alsalam Aircraft Company in Riyadh from 11 June 2003 to 22 May 2004, as part of the purchase agreement, and prior to transfer of ownership. The Aircraft was test flown on 20th of May 2004 and made its first flight for the new owner (MAVV) on the 24th of May 2004. The Aircraft has been exclusively utilized as an executive transport for the personal use of the current owner (MAVV) and VIP JETS acted as its Operator. At present operated by the same owner under Delmun Aviation Services. The Aircraft originally had 99 passenger seats when delivered to the previous owner, Saudi Arabian Airlines. The Aircraft interior was re-configured by SAA to VIP on 16 January 1980 and has been kept as is until todays date with the exception of a few changes including the reduction number of seats. MSN 22050 has accumulated 16694:50 flight hours and 11,236 flight cycles since new. Due to the nature of the Aircraft's operation since delivery, MSN 22050 is maintained to a low utilization maintenance program approved by Bahrain Civil Aviation.

16818.0

Alsalam Aircraft Company (AAC) which has a repair facility in Riyadh, KSA has been providing the scheduled maintenance of the Aircraft since it was acquired by Mercury AVV in 2004. Prior to that, the technical and airworthiness management has been handled by Saudi Royal Flight, Mid check being accomplished by Deutsche Lufthansa AG. The Maintenance program has been approved by Bahrain CAA. The period and frequencies of the maintenance tasks and inspections in the program are based on Boeing MPD (D6-17594) and CPCP Manual (D6-38528). The Aircraft has been maintained per the requirements of what is commonly referred to as a "low utilization" maintenance program. The minimum flight hours recommended by Boeing MPD to perform C check is FH 3,000. The Aircraft is currently under scheduled maintenance at Alsalam. It has accumulated less than 800 flight hours since the last D - Check which was performed by AAC in 2004.

Engines currently fitted on the aircraft has complied with all ADs up to date

SMOH

SMOH

ITEM VENDOR MODEL PART NUMBER QT Accessory Auto Pilot 65-52812-82 1 Computer, Pitch Sperry 2588810-901 1 Computer, Roll Sperry 2588812-901 1 Transceiver,Collins 622-3371-001 2 VHF Collins 822-1045-301 2 Recorder, Cockpit Voice Lockheed Martin 93A10030 1 Recorder, Digital Flight Data Honeywell Inc. 9804100-HQUS 1 Coupler, Yaw Damper Honeywell Inc. 4084042-911 1 Receiver, Marker Beacon Rockwell Collins 522-2996-011 1 Radar, Weather Bendix 2070410-0108 1 Altimeter, Radio Rockwell Collins 522-3698-002 1 Windshear, Detection Allied Signal 9650876030-B08 1 Receiver, VHF Navigation Rockwell Collins 51RV-5D 2 ADF Rockwell Collins 777-1492-004 2 DME Rockwell Collins 622-2921-001 2 Transponder, ATC Rockwell Collins 622-7878-01 2 System, TCAS Rockwell Collins TTR-920 1 Battery, INS Aero Quality Type 5001 2 Computer, Air Data Honeywell Inc. HG180U263 2 Adapter, VMO Harowe System 400801-1 2 Amplifier, Instrument Rockwell Collins 522-3120-004 2 Compass Rack Sperry 614937-101 2 Computer Steering Rockwell Collins 562A-5F5 1 Accessory Unit, Flight Instrument Boeing 65-52805-238 1 Coupler, Mach Trim Sperry 2590650-901 1 Adapter, HF Communication Transceiver Rockwell Collins 622-3699-001 2 Converter, Cabin Display Digital Intercontinental 33480-110 1 Comparator, Instrument Warning Rockwell Collins 522-3949-001 1 Gyro, Vertical Sperry 2587335-13 1 Gyro, Directional Sperry 2588302-1 2 Unit, Inertial Navigation Litton 4546620-01-02-28 2 Selcal Motorola NA 134D 1 Computer, MK VII Warning 965-0876-030 1 F/I Sw. VG Ledex 172938001 F/I Sw. Compass Ledex 172938001 F/I Sw. Computer Ledex 172938001 4.9 Avionics Modification Standard The Aircraft meets the following statutory avionics requirement: TCAS/ ACAS II software 7.0 compliant RVSM

2004

1980

40

The Aircraft has undergone several major modifications since it was first delivered. Significant modifications are listed here below: h Aircraft Interior Modification accomplished by The Dee Howard Company. h Installation of two Litton LTN-72-R INS accomplished by Deutsche Lufthansa AG. h Installation of dual Mode S (TCAS compatible) ATC Transponder System. h Installation of Collins Traffic Alert Collision and Avoidance System (TCAS II software 7.0) Transmitter/ Receiver done by Alsalam Aircraft Co. h Enhanced Ground Proximity warning System (EGPWS). h Installation of New Entertainment System for executive lounge area. h RVSM Upgrade h Installation Digital Air Data Computer installation h Installation of MFD V Colour Display V Universal Avionics

TBA later