1990 BOEING MSN 24770

Transcription

1 BOEING MSN SPECIFICATION 1990 BOEING MSN S P E C I F I C A T I O N S A N D S U M M A R Y Spectre Air Captal, LLC Airpark Blvd. Horseshoe Bay, TX P: F:

2 2 BOEING MSN SPECIFICATION Aircraft Identification Manufacturer: The Boeing Company Type & Model: 737-3Y0 Serial Number: Manufacturer Date: October, 1990 Current Passenger Accommodation Variable Number: 148Y PM395 Line Number 1941 Current Registration: Country of Registration: Last Operator: N638CS United States of America Precision Air

3 3 BOEING MSN SPECIFICATION AIRFRAME STATUS Total Airframe Hours: Total Airframe Cycles: AIRCRAFT MAINTENANCE PROGRAMME Airworthiness Authority Approval: MSG-2 Maintenance Programme Check Type INTERVAL Time at Last Check Next Due 1A CHECK 250 FH 45203FH FH 1C CHECK 4000 FH 44717:53 FH 58717:53 FH D CHECK FH FH FH Certified Operating Design Weights Weights Pounds Kilograms Maximum Taxi Weight 135,,500 61,461 Maximum Take-Off Weight: 135,000 61,234 Maximum Landing Weight: 114,000 51,709 Max Zero Fuel Weight 106,500 48,307 FUEL TANKS Position Fuel Capacity (Pounds) Fuel Capacity (Kilograms) Tank Capacity Auxiliary Tanks No Fuel Quantity Indication Units Kilograms Fuel Quantity Drip Sticks Calibration Kilograms

4 4 BOEING MSN SPECIFICATION ENGINE DATA Engine Manufacturer Engine Type and Model: CFM INTERNATIONAL CFM56-3B1 CFM56-3B1 Engine Position: LEFT HAND RIGHT HAND Engine Serial Number: Engine Total Time (Hours): 37,760 39,829:20 Engine Total Cycles: 34,894 21,081 Date of LSV: March 10, 2010 TBA Time at LSV: 32,028 30,761 Cycles at LSV: 29,819 16,354 Time since LSV: 5,732 9,068:20 Cycles since LSV: 5,075 4,727 LLP Limiter: VARIOUS 2429 FC Various FC Take Off Thrust 20,000 lbs 20,000 lbs FADEC YES YES APU Model No: GTCP85-129H Part No: Serial No. P TSN 51642:18 CSN UNK

5 5 BOEING MSN SPECIFICATION NOSE LANDING GEAR Part Number: Serial Number: CPT2272ET Total Cycles Since New 46,446 Total Hours since New: 65,476 Date Of Last Overhaul: 13-Nov-07 Overhaul Interval: FC/ 10 YEARS Cycles Remaining To O/H: Date of Next Overhaul: 10-Nov-17 LEFT MAIN LANDING GEAR Part Number: Serial Number: 2664 Total Cycles Since New 46,647 Total Hours since New: 65,250 Date Of Overhaul: 13-Nov-07 Overhaul Interval: FC/ 10 YEARS Cycles to Next Overhaul: Date of Next Overhaul: 10-Nov-17 RIGHT MAIN LANDING GEAR Part Number: Serial Number: P01577 Total Cycles Since New 45,476 Total Hours Since New 63,706 Date Of Overhaul: 13-Nov-07 Overhaul Interval: FC/ 10 YEARS Cycles to Next Overhaul: Date of Next Overhaul: 10-Nov-17

6 6 BOEING MSN SPECIFICATION AVIONICS UNITS INSTALLED COMPONENT PART NUMBER MANUFACTURER AIR DATA COMPUTER # HONEYWELL AUTO THROTTLE COMPUTER 755SUE2-4 BOEING DIGITAL STALL WARNING COMPUTER # BOEING DIGITAL STALL WARNING COMPUTER # BOEING AUTO SLAT COMPUTER # BOEING AUTO SLAT COMPUTER # BOEING CABIN TEMP CONTROL HONEYWELL PRESSURE CONTROL HAMILTON SUNDSTRAND AIR DATA COMPUTER # HONEYWELL FLIGHT MANAGEMENT COMPUTER SMITH INDUSTRIES FLIGHT INSTALLATION ACCESS BOEING IRS TRANSFER RELAY LEDEX INC. IRS TRANSFER RELAY LEDEX INC. DIGITAL ANALOG ADAPTER #1 DG1035AB03 HONEYWELL ENGINE VIBRATION STAGE CONDITION 6670M2230 ENDEVCO DIGITAL ANALOG ADAPTER #2 DG1035AB03 HONEYWELL FLIGHT CONTROL COMPUTER B HONEYWELL YAW DAMPER A HONEYWELL DFCS ACCESSORY BOX BOEING FLIGHT CONTROLL COMPUTER A HONEYWELL PA AMPLIFIER ROCKWELL COLLINS REMOTE ELECTRONIC UNIT S AVTECH CORP. VHF COMM. TRANSCEIVER ROCKWELL COLLINS VHF COMM. TRANSCEIVER ROCKWELL COLLINS SELCAL DECODER N1401B MOTOROLA DME, INTERROGATOR ROCKWELL COLLINS DME, INTERROGATOR ROCKWELL COLLINS ATC TRANSPONDER ROCKWELL COLLINS FLIGHT DATA ACQUISITION UNIT TELEDYNE CONTROLS ELECTRONIC FLIGHT INSTALLATION PRO ROCKWELL COLLINS ELECTRONIC FLIGHT INSTALLATION PRO ROCKWELL COLLINS

7 7 BOEING MSN SPECIFICATION COMPONENT PART NUMBER MANUFACTURER RADIO ALTIMETER AME-SALES RADIO ALTIMETER AME-SALES ATC TRANSPONDER ROCKWELL COLLINS GROUND PROXIMITY COMPUTER HONEYWELL ADF, RECEIVER ROCKWELL COLLINS ADF, RECEIVER ROCKWELL COLLINS MARKER BEACON ROCKWELL COLLINS T/R UNIT, 50 AMPS QECO CORP T/R UNIT, 50 AMPS QECO CORP T/R UNIT, 50 AMPS QECO CORP BATTERY CHARGER ELDEC STATIC INVERTER 39B168-1C HONEYWELL AUTO SPEED BRAKE UNIT BOEING ANTI-SKID CONTROL UNIT HYDRO AIRE AIR CONDITIONING MODULE UNIT BOEING ENGINE ACCESSORY UNIT BOEING OVERHEAT DETECTOR FENWALL SAFETY ACCESSORY SWITCH BOEING ACCESSORY UNIT-FLAP SLAT BOEING APU CONTROL UNIT BOEING FIRE DETECTOR KIDDE AEROSPACE WINDOW HEAT CONTROL KOITO WINDOW HEAT CONTROL KOITO WINDOW HEAT CONTROL KOITO WINDOW HEAT CONTROL KOITO VHF NAV ROCKWELL COLLINS VHF NAV ROCKWELL COLLINS TCAS PROCESSOR COMPUTER HONEYWELL INERTIAL REFERENCE UNIT HG1050AD09 HONEYWELL INERTIAL REFERENCE UNIT HG1050AD09 HONEYWELL

8 8 BOEING MSN SPECIFICATION Statement of Aircraft Technical Operational Capability Technical Aircraft Capability: Cat IIIa 8.33 Spacing RVSM FM Immunity Airstairs Fitted