Aircraft General Specifications Nippon Cargo Airlines Co., Ltd. Boeing 747-400 Freighter This version of the Aircraft General Specifications replaces any previous version(s) issued, and are therefore hereby invalidated. All data shown is subject to prospective lessee/buyer inspection. 1/5
DATA PRODUCED: February 22, 2014 Aircraft General Data: Aircraft General Manufacturer: Boeing Model: B747-481F Manufacturer Serial Number: 34018 Current Registration: JA03KZ Date of Manufacturer: September 17th, 2006 Total Airframe Hours since New: 30408+26 Hours Total Airframe Cycles since New: 6172 Cycles Certification Base JCAB / Japan Civil Aviation Bureau Noise Compliant ICAO Stage 3 Overall Length Wingspan Overall Height Cruising Speed MAX. Speed 23ft 10in (70.66m) 211ft 5in (64.44m) 63ft 8in (19.4m) Mach 0.855 @ 35,000ft Mach 0.92 @ 35,000ft Engines Engine Model Cargo Compartments Cargo Configuration -Main deck volume -Lower deck volume Cargo Loading System Main Deck Cargo Compartment Lower Lobe Cargo Compartment Cargo Intercom System Lower Lobe Cargo Compartment Doors Main Deck Side Cargo Compartment Door Main Deck Nose Cargo Door Bulk Cargo Door the airplane is equipped with four General Electric CF6-80C2B1F - high bypass turbofan engines with FADEC. Main Deck: 30 Pallets / Lower Deck: 32 LD3s 21,462ft3 (607.7m3) 4,605ft3 (130,4m3) including 520ft3 (14.7m3) bulk cargo. A Telair electrically powered cargo transfer system is installed in the main deck cargo compartment, and in the forward and aft lower lobe cargo compartment. The main deck cargo compartment accommodates both container and pallet ULDs and is designed as a FAR Class E compartment Two cargo compartments are provided in the lower lobe are designed as FAR Class C compartments. The forward compartment and the constant section of the aft compartment accommodate container and/or pallet ULDs. The tapered section of the aft compartment accommodates bulk cargo. A cargo intercom system is installed The forward and aft, outward-opening cargo compartment doors have as structural clear opening, approximately 104 inches wide by 66 inches high. An outward-opening side cargo door has a clear opening, approximately 134 inches wide by 120 inches high (122 inches wide by 123 inches high between the door actuators). The nose cargo door is located forward and below the control cabin. The door swings upward to allow a rectangular minimum clear opening of 100 inches by 104 inches wide. A bulk cargo door is installed at approximately Body Station 2005 on the right side of the airplane. The door is an inward-opening, plug-type, and have a clear opening approximately 44 inches wide by 47 inches high. All data shown is subject to prospective lessee/buyer inspection. 2/5
Air Conditioning Air Conditioning Air Distribution Heating - ground Heating - in flight Cooling - ground Cooling -in flight The air conditioning system includes 3 identical air conditioning packs. Each pack has separate controls, cooling equipment and connects to a central air distribution system. The distribution system directs conditioned air from any combination of packs to the flight compartment, upper deck, main deck and lower lobe compartments. An air distribution system is installed for the main deck cargo compartment. A separate air distribution system is installed for each lower lobe cargo compartment. The forward and aft compartments are considered individual temperature control zones. When the airplane is on the ground, the system is capable of heating the flight compartment, upper deck, and main deck cargo areas to an average temperature of 24 degrees Celsius. The system is capable of heating either or both lower lobe cargo compartments to an average temperature of 27 degrees Celsius. While in flight, the system is capable of heating the flight compartment, upper deck, and main deck cargo areas to an average temperature of 26 degrees Celsius. The system is capable of heating either or both lower lobe cargo compartment to an average temperature of 27 degrees Celsius. When the airplane is on the ground, the system is capable of cooling the flight compartment, upper deck, and main deck cargo areas to an average temperature of 24 degrees. The system is capable of cooling either or both lower lobe cargo compartments to an average temperature of 16 degrees Celsius. While in flight, the system is capable of cooling the flight compartment and upper deck to an average temperature of 18 degrees Celsius. The system is capable of cooling either or both lower lobe cargo compartments to an average temp of 7 degrees Celsius. Compliance with Requirements Reduced Vertical Separation Minimum Long Range Navigation The airplane is equipped for reduced vertical separation minimum (RVSM) flight as defined by: Any airspace or route between FL 290 and FL 410 inclusive where aircraft are separated vertically by 1,000 feet (300 m). Prior to commencing RVSM operations, it is the responsibility of the Lessee / Buyer to obtain operational approval from the regulatory. The airplane is certified for long range navigation using the inertial reference system (IRS) as the sole source for navigation data in the flight management computer system. Weight & Structural Data: Max. Take Off Weight Max. Taxi Weight Max. Landing Weight Max. Zero Fuel Weight Delivery Empty Weight Fuel Capacity Range Capability at MAX Payload 875,000 lbs / 396,900 kgs 878,000 lbs / 398,254 kgs 652,000 lbs / 295,747 kgs 610,000 lbs / 276,696 kgs 351,380 lbs / 159,718 kgs 57,285 usg / 216,840 L 4400 nm / 8140 km All data shown is subject to prospective lessee/buyer inspection. 3/5
Engines: Manufacturer Model Engine Condition at Delivery General Electric CF6-80C2B1F "as is where is" S/N FH/FC since New FH/FC since Last SV Date of Last SV HPT FC Remaining Facility 706769* 25433 / 5054 7115 / 1423 20FEB12-01MAY12 9946 706770* 29600 / 5999 10366 / 2159 23MAY11-27JUL11 9001 706771* 30299 / 6134 11272 / 2338 28APR11-18MAY11 8866 706772* 29142 / 5922 10882 / 2265 07MAR11-10JUN11 9078 * note : These engines are installed on the other aircraft as of 22FEB2012 and will be transferred to RL473 by the date of redelivery Manufacturer Model Auxiliary Power Unit: Pratt & Whitney Canada PW901A Data as of 14JAN2014 S/N PCE900733 FH/FC since New FH/FC since Last SV Date of Last SV Facility 11823 / 12093 2126 / 2637 17JAN2012 REVIMA APU Landing Gear: Position Part Number Last Overhaul Cycles since OH (new) Days Remaining Nose Left Wing Right Wing Left Body Right Body 162U1500-54 N/A - (6172) 885 161U1500-209 N/A - (6172) 885 161U1500-210 N/A - (6172) 885 163U1500-121 N/A - (6172) 885 163U1500-122 N/A - (6172) 885 Maintenance Data: Check Date Last Accomplished FH / FC Interval Next Due C D Delivery Condition 16MAY2013 27727 / 5571 10000 Hours / 24 months 15MAY2015 N/A N/A 8 / 8 / 6 Years 16SEP2014 TBD Avionics / Communications: ACARS Management Unit Rockwell Collins 822-1239-151 1 ACMS Data Management Unit Teledyne Controls 2232000-02-B 1 ADF Receiver Rockwell Collins 822-0299-001 2 Air Data Computer Honeywell 4040800-911 3 Airborne Data Loader Alliedsignal 964-0401-006 1 ATC Control Panel Gables G6992-03 1 ATC Transponder Rockwell Collins 822-1338-005 2 Audio Communication Control Panel Rockwell Collins 1167015-141 4 CDU-FMS Honeywell 4077880-908 / 4058650-904 3 Cockpit Voice Recorder L-3 Communications 2100-1020-00 1 CVR Control Panel L-3 Communications S151-0040-00 1 DFDR Accelerometer Alliedsignal 971-4193-001 1 DFDR Solid State Alliedsignal 980-4700-042 1 Display, Integrated Standby Flight Display Thales C16221LA03 1 DME Interrogator Rockwell Collins 822-0329-001 2 EFIS Control Panel Rockwell Collins 622-8590-113 2 All data shown is subject to prospective lessee/buyer inspection. 4/5
EICAS / ND / PFD / Display Rockwell Collins 822-1714-100 6 EICAS Display Select Panel Rockwell Collins 622-8591-100 1 ELT (Fixed / Auto) Artex Aircraft 453-5004 1 ELT (Portable) Honeywell 1152794-1M431 2 Flight Control Computer Rockwell Collins 822-1261-101 3 Flight Management Computer Honeywell 4052508-952 2 GPWS Computer Honeywell 965-0976-003-222-222 1 HF Transceiver Rockwell Collins 822-0990-004 2 IRU Honeywell HG1050AE11 / HG1050AE1 3 Mode Select Panel Honeywell CG1234AC02 1 Multi-Mode Receiver - ILS/GPS Rockwell Collins 822-1821-001 3 QAR Penny & Giles D52000-64000 1 Radio ALT Transceiver Rockwell Collins 822-0334-002 3 Satcom Satellite Data Unit Rockwell Collins 822-0311-102 1 Selcal Decoder Avtech NA138-714C 1 TCAS Computer (Change 7.1) Rockwell Collins 822-1293-033 1 VHF Communication Transceiver Rockwell Collins 822-1250-002 3 VOR/MKR Receiver Rockwell Collins 822-0297-001 2 WXR Control Panel Honeywell 2041220-0430 1 WXR Transceiver Honeywell 066-50008-0408 2 Emergency Equipment: Fire Gloves DME Corporation 2993 1 First Aid Kit DME Corporation S6-01-0005-316 1 Life Vest (Adult / Child) Switlik Parachute S-51150-6300-117021 12 Oxygen Masks Scott Aviation 28301-02 3 Oxygen Masks, Full Face Scott Aviation MF10-02-01 / MF10-02-11 4 Smoke Hood (PBE) Essex PB&R MR-10036N 4 Galley: Oven Rack B/E Aerospace 236152 1 Oven Tray B/E Aerospace 236153 8 Coffee Maker B/E Aerospace 411-0001-139 1 Steam Oven B/E Aerospace 4323100-00-66-22 1 Standard Container Driessen BA017005 8 Upper Deck Configurations: Business Class Seat (L/H) Koito Industries 83222B17775-401 1 (2 seats) Business Class Seat (R/H) Koito Industries 83222B17775-402 2 (4 seats) Lavatory Monogram Sanitation NCA046-18001KZ 1 All data shown is subject to prospective lessee/buyer inspection. 5/5