B-2574 - 1999 BOEING 737 300

1999

BOEING

737-300

29407

B-2574

Used

IFR

CB Aviation is proud to bring to market this late model 737 300 located in Asia. The aircraft is currently in operation and owners would prefer to sell as part as package deal which would be a total of 3 x 737 300 including another a 1999 and 1996 737 300. All three aircraft are currently in operation. Please inquire regarding package pricing.

43971.0

TTAF: 43,971 Last C Check: 40,584 / 32,931

ENGINES: Model: CFM56-3C-1 Cycles Remaining Limiter: 586 / 4899 ENGINES Engine 1 Engine 2 APU Type/Model : CFM56-3C-1 CFM56-3C-1 APS2000/T-62T-47C1 S/N of delivered engine : 857865 856776 SP-E992539 Current location(MSN) : 29407 29407 29407 Thrust rating : 20000 lbs 20000 lbs Effective date : NOV 30.2014 NOV 30.2014 NOV 30.2014 Time Since New : 51335 51231 29556 Cycles Since New : 35863 34037 34354 Time Since Last Shopvisit : 10294 7863 10236 Cycles Since Last Shopvisit : 5958 5244 10496 Cycles remaining first limiter 586 4899 First limiter description : REAR SHAFT LPT SHAFT

AVIONICS: Major Avionic Equipment ATA Description Part Number QTY Manufacturer 22 Auto Throttle Computer 755SUE2-4 1 SMITHS IND 23 VDR-ACARS SYS 822-0323-002 1 ROCKWELL COLLINS 23 MK II CMU-ACARS 965-0758-001 1 HONEYWELL 23 SELCAL Decoder NA138-71413 1 AVTECH 31 DFDAU 2233000-816-1 1 TELEDYNE 34 Flight Control Computer 4051600-914 2 HONEYWELL 34 Air Data Computer 4061100-901HG480E1 1 HONEYWELL 34 TCAS II Computer 066-50000-2220 1 HONEYWELL 34 Marker BeaconReceiver 522-2996-011 1 ROCKWELL COLLINS 34 VHF Comm Tranciever 822-0323-002 2 ROCKWELL COLLINS 34 Interrogator- DME 622-4540-122 2 ROCKWELL COLLINS 34 VHF NAV VOR/ILS Reciever 822-0761-001 2 ROCKWELL COLLINS 34 Radio Altimeter 2067631-5154 2 HONEYWELL 34 Weather Radar -Transceiver 066-50008-0405 1 HONEYWELL 34 Transceiver- HF 622-5272-120 2 ROCKWELL COLLINS 34 ATC Transponder 066-01127-1301 2 HONEYWELL 34 EFIS – Symbol Generator 622-9436-101 2 ROCKWELL COLLINS 34 Digital Stall MGMT Computer 65-52822-7 2 BOEING 34 ADF Reciever 777-1492-005 2 ROCKWELL COLLINS 34 Enhanced GPWS 965-0976-060-216-216 1 ALLIEDSIGNAL AVIONICS INC 34 Inertial Reference Unit HG1050AE11 2 HONEYWELL 34 Elex Pressure Controller 763810-1 1 HAMILTON SUNDSTRAND CORP

OPERATIONAL WEIGHTS Date last weighing : 2014-05-04 Maximum Taxi Weight : 59193 Kgs 130500 Lbs Maximum Take-off Weight : 58967 Kgs 130000 Lbs Maximum Landing Weight : 51709 Kgs 114000 Lbs Maximum Zero Fuel Weight : 47627 Kgs 105000 Lbs Basic Empty Weight : 32555 Kgs 71771 Lbs Operating Empty Weight : 33538 Kgs 73937 Lbs FUEL Fuel Quantity Indication units : KgsX 1000 Fuel Flow Indication units : KGS/ HrX1000 Total Fuel Capacity : 16390 Kgs 36101 Lbs 5311 USg Capacity Center Wing Tank : 7138 Kgs 15723 Lbs 2313 USg Capacity Main Wing Tank : 4626 Kgs 10189 Lbs 1499 USg

White/Blue

126

Passenger compartment: 3-Class configuration 8 Business Class Seats at 42" pitch, 24 Premium EC seats at 35" pitch and 94 Economy Class Seats at 31” pitch. All seats are covered with fabric covers. All seats are equipped with life vests installed under seats. Cabin is fitted with floor mounted escape path lighting. 5 Attendant seats installed (2 fwd cabin, 3 aft section). 3 Lavatories installed (1 fwd cabin ,2 aft cabin). 3 Galley installed (G1&G2 in fwd cabin, G4B Aft cabin). ATA Description Qty(pax) Manfacturer Part number 25-25 First Class double seat 8 ALI KKY410 Series 25-25 Premium Economy Class seat 24 ALI KKY400 Series 25-25 Economy Class seat 94 ALI KKY400 Series 25-31 Galley 3 B/E 5520 Series

Last C Check: 40,584 / 32,931