B3651 - 1992 SAAB 340B

1992

SAAB

340B

289

Used

B3651

SAAB-340B REGISTRATION: B3651 SERIAL NUMBER: 289 Aircraft status information contained herein is ¡°as supplied¡± by the operator during the condition survey. Portions of supplied data were verified, in order to gain confidence in the operators maintenance system, by means of sampling, physical inspection and confirmation of hard copy records. It is not the intent of this report to provide data for Airworthiness Agency transfer or to provide an aircraft acceptance inspection EXECUTIVE SUMMARY AICRAFT DATA SUMMARY Type and Model SAAB340B Engine Type and model CT7-9B Manufacture Serial Number 289 Date of fist flight Delivery Date 24th March 1992 Current Registration CAAC Operator Shan Dong Airlines Configuration 36 seats Principal Avionics Equipment TCAS¢ò,GPS,GPWS Airframe Hours and cycles 18660 hours/ 17095 cycles Engine 1 Hours and cycles 14094 hours/ 12985 cycles Engine 2 Hours and cycles 12139 hours/ 10773 cycles AIRCRAFT HISTORY Review of the aircraft case database shows the history of the subject aircraft to be the following: Date Event Registration 24th March 1992 Delivered to China Southern CAAC 6th November 1996 Order placed and delivered to Shan Dong Airlines CAAC AIRCRAFT IDENTIFICATION Manufacture SAAB Aircraft AB Type & Model SAAB340B Serial Number 289 Delivery Date 24th March 1992 Current Registration CAAC Country of Registration CHINA Current Operator Shan Dong Airlines Aircraft Operating Limitation CAT ¢ñ CERTIFICATION OF AIRWORTHINESS Issuing Authority CAAC Number AC1390 Date of Issue 1st June 2001 Last Validated 11th December 2002 Expiry Date 31st December 2003 Category Passenger Transport CERTIFICATION OF REGISTRATION Issuing Authority CAAC Number NR0438 Date of Issue 24th Dec 1999 Registered Owner Shan Dong Airlines RADIO LICENCE Issuing Authority CAAC CERTIFICATE OF RADIO INSTALLATION APPROVAL Issuing Authority CAAC Number 2000-035 Date of Issue 28th Feb 2000 Last Validated 28th February 2000 NOISE CERTIFICATE Issuing Authority The Swedish Civil Aviation Administration Number 1/89 Date of Issue 20th June 1989 Compliance The Swedish Civil Aviation Administration and ICAO Annex 16 AIRFRAME STATUS Total Airframe Hours 18660 hours Total Cycles 17095 cycles Current Average Daily Utilization 5 hours/4cycles Current Major Overhaul Facility Shan Dong TAECO Engineering Co LTD AIRCRAFT MAINTENANCE PROGRAMME Airworthiness Authority Approval Hua Dong airworthiness administration of CAAC Check Type Never Exceed Period Time at last Check Next Scheduled Check due Flight Hours/ Cycles/Calendar Flight Hours/ Cycles/Calendar Flight Hours/ Cycles/Calendar 100 FH Check 100 hours 18407 FH 18800 FH 200 FH Check 200 hours 18510 FH 18900 FH 400 FH Check 400 hours 18296 FH 19100 FH 800 FH Check 800 hours 17890 FH 19500 FH 4000 FH Check 4000 hours 15503 FH 19503 FH 8000 FH Check 8000 hours 15503 FH 23503 FH 12000 FH Check 12000 hours 11490 FH 27503 FH 1Y Check 1 Year 30th March 2002 30th March 2003 2Y Check 2 Yeas 30th March 2002 30th March 2004 3Y Check 3 Years 24th March 2001 24th March 2004 4Y Check 4 Years 22nd March 2000 22nd March 2004 6Y Check 6 Years 22nd March 2000 22nd March 2004 12000 FL Check 12000 FL 11935 fl 23935 fl 15000 FL Check 15000/6000FL (first check /repeat interval) 14803 fl 20803 fl 24000 FL Check 24000 FL Not applicable now Not applicable now 30000 FL Check 30000 FL Not applicable now Not applicable now Note: FH - Flight Hours fl - flight cycles ADDITIONAL STRUCTURAL INSPECTION Program Type Ageing Aircraft Program Incorporated in to the operator maintenance schedule as per the manufactures MRB appendix C as AEP items, with task number suffix-80. Corrosion Prevention and Control Program Incorporated in to the operators maintenance schedule as per the manufactures MRB appendix D design concept and implementation guidelines Supplemental Structural Inspection Structural inspections are incorporated in to the operator maintenance schedule as per the manufactures MRB recommendations. Only 12000 flight landing and 15000 flight landing check items are applicable and accomplished since the aircraft delivered from new. NOTABLE MODIFICATIONS Notable Modification The following modifications were incorporated during operating ¡¤Installation of TCAS ¢ò ¡¤Installation of GPS Details for other modifications are signed on the aircraft log book PRINCIPAL OPERATING WEIGHTS Maximum Taxi Weight 13065 kg Maximum Take-off Weight 12930 kg Zero Fuel Weight 11795 kg Maximum Landing Weight 12700 kg Operating Empty Weight 8140 kg Last Weighting 22nd November 2000 FUEL DATA Fuel Capacity 3280 litres/ 866 US gallons Auxiliary Fuel MAIN ENGINES Engine Manufacturer Engine Type and Model GE CT7-9B Engine Position No.1 No.2 Engine Serial Number 785431 785493 Engine Total Time 14094 hours 12139 hours Engine Total Cycles 12985 cycles 10773 cycles Engine Maintenance The CT7-9Bengines are maintained on condition, with hot section borescope inspection scheduled every 800 flight hours and cold section borescope inspection every 200 flight hours. Time Between Overhauls Not applicable Not applicable Build Standard at Overhaul According to overhaul shop manual According to overhaul shop manual Last shop visit workscope For details see related document For details see related document Hours since last shop visit 2302 hours 760 hours Cycles since last shop visit 1970cycles 687cycles Hours since overhaul/performance restoration 2302 hours 760 hours Cycles since overhaul/performance restoration 1970cycles 687cycles Hours to engine limiter Not tracked Not tracked Cycles to engine limiter 1967 cycles 3756 cycles Engine cycles limiter Stage 2 disk Compressor rear shaft Location if not currently installed N/A N/A Current overhaul facility GE GE LANGDING GEARS Nose Landing Gear Part Number: AIR83566-1 Serial Number: LK9104476 Time Since New: 16,247 cycles Time Between Overhaul: 12,000 cycles Next Scheduled Overhaul: 6,327 cycles Life(scrap) Limit: Time remaining to life(scrap) Limit: Main Landing Gear Left Hand Right Hand Part Number: AIR83064-3 AIR83064-3 Serial Number: LK9104555 LK9200883 Time Since New: 15,747 cycles 7,130 cycles Time Between Overhaul: 12,000 cycles 12,000 cycles Next Scheduled Overhaul: 6,827 cycles 4,870 cycles Life(scrap) Limit: Time remaining to life(scrap) Limit: Current Overhaul Facilith: We send it back to manufacture for overhaul! AIRCRAFT INTERIOR SPECIFICATION INTERIOR CONFIGURATION/INFORMATION Passenger seating Total seat certificated 36 seats Current passenger seating 36 seats Seat manufacturer FEEL, today owned by BE Aerospace Seat model F7 Fire blocking standard See note below* Overhead luggage bins Hunting, today owned by AIM Flight deck Total seating capacity 2 flight crew +1 observer seat manufacturer IPECO Cabin attendants seating Quantity 1 Manufacturer Hunting, today owned by AIM Type 1 single fold-down Location At the forward galley bulkhead near the passenger door lavatory Quantity 1 Manufacturer Hunting, today owned by AIM Location forward Smoke detector fitted Yes Waste bin fire extinguishers yes Passenger entertainment Tape recorder TP3100-2A Entertainment system vendor TOPCAST CO,LTD Galley provision Galley identification Cabin location forward Equipment Trolley stowage 1 Catering box stowage 2 Water boiler 2 Water faucet 2 PRINCIPAL RADIO AND AVIONICS EQUIPMENT ATA Chapter 22-Auto Flight Equipment Quantity Manufacturer Model or Part No. FCC 1 COLLINS 622-7492-010/-210 PANEL AY-APP85 1 COLLINS 622-6208-005 PANEL AY-MSP85 1 COLLINS 622-6209-008 ATA Chapter 23-Communications Equipment Quantity Manufacturer Model or Part No. VHF Control Unit 2 COLLINS 622-6520-009 Transceiver-VHF 2 COLLINS 622-6152-011 HF Control Unit 1 COLLINS 622-6614-022 HF Transceiver 1 COLLINS 622-6557-011 PA Amplifier 1 COLLINS 622-4096-001 REU 1 TELEPHONICS 502-0066-005 CVR 1 HONEYWELL 980-6020-001 ATA Chapter 31-Indicating and Recording Equipment Quantity Manufacturer Model or Part No. FDAU 1 TELEDYNE 2231230-1A FDR 1 LOCKHEED 10077A500-803 Panel-Flight data entry 1 TELEDYNE 2229949 WEU 1 ULTRA 005WS00 ATA Chapter 34-Navigation Equipment Quantity Manufacturer Model or Part No. ADF Receiver 2 COLLINS 622-2362-001 ATC Transponder 2 COLLINS 622-1270-001 DME 2 ROCKWELL 622-6263-003 GPWS Computer 1 HONEYWELL 965-0476-088 Standby Altimeter 1 THALES 64141-360-1 UNS CDU 1 UNIVERSAL 1117-11 Standby Horizon 1 THALES H341ADM2 AHRC 2 COLLINS 622-6190-113 Radio Altimeter Transceiver 1 COLLINS 622-2855-011 TCAS Computer 1 COLLINS 822-1293-001 Weather Radar Transceiver 1 COLLINS 622-8440-003 VOR 2 COLLINS 622-6137-001 DDRMI 2 NORTHROP D3337LB2 ADC 1 COLLINS 622-4401-001 Processor Unit-Display 2 COLLINS 622-7713-004 Processor Unit-Multifunction 1 COLLINS 622-7718-004 UNS NCU-1K 1 UNIVERSAL 1116-40-1116 AIRCRAFT RECORDS AND DOCUMENTATION RECORDS AND DOCUMENTATION REVIEW Country of registration CHINA Aircraft records management The aircraft records are managed by engineering department of Shan Dong airlines. Records storage All the manuals and technical documents issued by manufacturer and vendor are stored in engineering division. The log book of parts stored in QC division. For More Detail Please Contact [email protected]

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