Registration: N328DP Serial Number: 3169 Delivery Date: 14 December 2000 Operated By: Ultimate JetCharters, Inc.

Transcription

1 Dornier 328Jet-310 Registration: N328DP Serial Number: 3169 Delivery Date: 14 December 2000 Operated By: Ultimate JetCharters, Inc.

2 Contents Chapter Title Page 1. Certification 3 2. Power Plant / APU 3 3. Operational Weights 3 4. Cockpit Layout 4 5. Cabin Layout 4 6. Cargo Layout I Volumes 4 7. Fuel System 4 8. Entertainment System 5 9. Avionics Wheels and Brakes Maintenance System Aircraft Data Drawings (LOPA) 9 2

3 1. CERTIFICATION Aircraft is FAR 121 compliant / JAA / EASA Aircraft is CAT I certified 2. POWER PLANT I APU PW306B with a thrust of 6,050 lbs. The engines are operated on-condition. Enrolled in Pratt & Whitney Canada FMP for 100% Coverage. Serial Number TSN CSN TSI CSI Cycles Remaining CD FC H.P.T. Disk No. 2 CD FC H.P.T. Disk No. 2 Last Shop visit for CD Mar-2004 at 5953 TTSN and 5993 TCSN Last Shop visit for CD May-2004 at 6529 TTSN and 6606 TCSN (minor repair) A heavy shop visit occurred on 31-Jan TTSN and 5990 TCSN APU Model: GTCP36-150(DD) P/N: S/N P-62 Time Since New 2487 Cycles Since New Time Since Installation Cycles Since Installation Not Recorded TBD TBD 3. CURRENT OPERATIONAL WEIGHTS Basic Operational Weights LBS KG are: Max Gross Taxi Weight (MGTW) 34, Max Take-Off Weight (MTOW) 34, Max Landing Weight (MLW) 31, Max Zero Fuel Weight (MZFW) 28, Operating Empty Weight 21,

4 4. COCKPIT LAYOUT a) Two Crew b) One Observer Seat The aircraft is equipped with Phase2 reinforced cockpit door 5. CABIN LAYOUT a) Passenger Seating 12 Seat Executive Two Club Seating Areas with model 4021 single seats One Double club area with model 4404 double seats 20 wide work table between each single seat 18 x 42 work table between double seats Credenza across from double seats with storage b) Passenger Service Units Reading lights Swivel Air Outlets Audio Speakers Oxygen c) Stowage Compartments Forward Closet Aft Closet d) Lavatories 1 Aft e) Galley Forward Galley Microwave Solid Surface Countertop Hot liquid Storage 6. CARGO LAYOUT I VOLUMES Max. Comp. Capacity (aft1/bulk) Max, Comp. Capacity (aft2/bulk) 882 lbs / 400 kg 771 lbs / 350 kg 7. FUEL SYSTEM The usable fuel tank capacity is 8,038lbs (4,542 liters), in wings and feeder tanks. Each wing tank has a capacity inner tank 2,373lbs (1,341 liters) and outer 1,462lbs (826 liters) and each feeder tank has a capacity of 184lbs (104 liters). The fuel quantity indication system is calibrated in lbs. 4

5 8. ENTERTAINMENT SYSTEM The aircraft is equipped with the following entertainment features: One 32 Boland Windowline Monitor Two 19 Boland Bulkhead Monitors Two 12 Boland Bulkhead Monitors 12 Wireless Headsets with 3 Audio Channels DVD Player CD Player MP3 Audio Input Rosenview Moving Map System with Remote Control 5

6 9. AVIONICS COMPONENT MODEL PARTNUMBER AHRS Fan Filter Filter Mounting Tray, AH~800 MT Fan Assembly, AH-800 MT Attitude Heading Ref. Unit AH-900 HG2011ACO4 AIR DATA Mounting Tray MT Co-Pilot Comm Wide Com Unit Mounting Tray MT Comm Connector Unit IK Connector Kit, Comm Unit Main IK Scrap Bus Kit lk Comm Unit, 25/8.33KHZ RCZ-833H Co-Pilot Nav Nav Unit (VOR/ILS) Digital RNZ-851C Nav Unit Mounting Tray MT VOR Connector Kit IK Connector Kit, Nav Unit Main lk Strap Bus Kit lk Data Acquisition Data Acquisition Unit DA DAU-Dornier Steep Approach DA Mount for DAU MT Display AMLCD FMS control Display CD Unit Display Unit DU MFD/EICAS Prim. Function BL Display Configuration Module lm Mount for IAC MT Flight Guidance Servo Bracket SM-201A Servo (ElevJAileron) SM-200A Servo (Rudder) SM-200A Pilot Comm Gasket Gasket Nav Unit (VOR/ILS/DME/ADF RNZ Nav Unit MT ADF Antenna AT ADF Antenna Connection Kit IK DME Connector Kit IK Strap Bus Kit lk Primus II Radios Mounting Clamp, RMU lk Flat Panel Radio Management AM Interposer MT-860A Audio Pane, Fixed Wing, AV-858A CD Head, 8.33Khz CD Radar Antenna Receiver WU Flat Plate lk Radio Altimeter Gasket Gasket Radio Altimeter RT

7 10. WHEELS AND BRAKES a) Nose Wheel Tires: Goodyear P/N: 2225 b) Main Wheel Tires: Goodyear P/N: c) Brakes: Bendix P/N: HA MAINTENANCE SYSTEM According to Low Utilization Maintenance Planning Document (LUMP) 11.1 Inspections Inspection Phase Repeat Interval Escalation Tolerance (1 time) Phase 1 2 Weeks 1 Week Phase 2 6 Months 1 Month Phase 3 12 Months 1 Month Phase 4 24 Months 2 Months Phase 5 48 Months 2 Months Phase 6 96 Months 2 Months Component Interval Life Limit L/H Gear Assy. 10 YRS / FL HRS (MRB) 65,000 FL (ALD) R/H Gear Assy. 10 YRS / FL HRS (MRB) 65,000 FL (ALD) Side Brace 10 YRS / FL HRS (MRB) 65,000 FL (ALD) Nose Gear Assy. 10 YRS / FL HRS (MRB) 65,000 FL (ALD) P/N GTCP (DD) 10,000 APU HRS (MRB) On Condition Compressor Rotor (MRB) 100,000 APU HRS Turbine Rotor (MRB) 10,000 APU HRS Combustion Chamber (Boro-Insp) 5000 APU HRS (MRB) Fuel Nozzles (Clean / Insp) 5000 APU HRS (MRB) Wiring Harness (Clean / Insp) 5000 APU HRS (MRB) 7

8 12. AIRCRAFT DATA A/C Reg. SeriaI Flight Flight Last * Next No. Hours Cycles C1+2-Check C4-Check N328DP * 07 Jan Gear Data (MLG and NLG) Assy Part Number Serial Number Next Gear Overhaul 22,000 FC or 10 Yrs (Remaining Time in FC) Barrel Assy LH Barrel Assy RH Barrel Assy NL CE024 CE024 IL063 13,399 FC remaining 13,399 FC remaining 13,399 FC remaining 8

9 13. Drawings 9

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13 For information contact: Dan Piraino Peter DeLisa Wilmington, DE Morristown, NJ T T F F dsp@tridentas.com pdd@tridentas.com Dale Horton Ted Glassman Orlando, FL Madison, CT T T F F jhorton@tridentas.com tedglassman@snet.net Contact Ultimate JetCharters to learn about how UJC can manage and operate your DornierJet: ULTIMATE JETCHARTERS, INC WEST AIRPORT DRIVE NORTH CANTON, OHIO T F