AIRCRAFT GENERAL SPECIFICATIONS AIRBUS A310-304 FREIGHTER AIRCRAFT

航空发表于 2010-8-5 09:14:35

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ANNEXURE - V Page 1 of 5 AIRCRAFT GENERAL SPECIFICATIONS AIRBUS A310-304 FREIGHTER AIRCRAFT Aircraft Identification Cargo Configuration Manufacturer Airbus Industrie Main Deck - Single Row ULDs configuration Date of Manufacture May 1986 12 (88”x125”) or 11 (96”x125”)or 5 (125”x96”) Manufacturer Serial Numbers 407 - Side by Side ULDs configuration P to F conversion date Aug 2008 14 (125”x88”) or 12 (125”x96”) + 4 (88”x125”) Original & Current Registration VT-EJH Lower lobe Fwd- 3 Pallets 88”x125”or 96”x125” Engine 2 x GE80C2 A2 Lower lobe Aft - 7 LD3 containers+ Bulk APU 1x Honeywell GTCP 331-250H Note: Detailed description on page 5 Aircraft Weights Max Taxi Weight 153900 Kgs Major Avionics/ Navigation Equipment Max Take-Off Weight 153000 Kgs Description Part Number Vendor Qty Maximum Landing Weight 123000 Kgs FAC B471ABM5 Sextant 2 Maximum Zero Fuel Weight 113000 Kgs FCC B470ADM Sextant 2 Operating EmptyWeight 76500 Kgs HF 622-5272-001 Collins 2 Structural Limited Payload 36500 Kgs VHF 822-1044-003 Collins 3 Note: FMC 745SUE4B4 Smiths 2 Payload may be limited due aircraft performance WX 622-5132-105 Collins 2 criteria and/or sector fuel requirement. DME 622-4540-001 Collins 2 ADF 622-5222-002 Collins 2 Maintenance Programme ILS 822-0282-002 Collins 2 A Check Every 500 Hrs VOR 822-0726-002 Collins 2 C Check Every 18 months EGPWS 965-0576-002 Honeywell 1 HMV Check Every 5 Yrs LRRA 9599-607-14901 Thales 2 Engine Condition Monitoring Mode S 066-01127-1402 Honeywell 2 APU On Condition TCAS II 066-50000-2120 Honeywell 1 IRU 461800-300-2203 Litton 3 Maintenance Status Airframe ( as at 02 Nov 09) Salient Features complied Total Flight Hrs 62,573 FH 1. 120 minutes ETOPS approved Total Flight Cycles 24,916 FC 2. 8.33 KHz Channel spacing compliant Next Major Check 08 Oct 10 3. FM Immunity Compliant Next HMV Oct 12 4. TCAS II compliant NLG –Overhaul due at – 15 Apr 10 5. RVSM compliant MLG –LH - Overhual due at - Jul 17 6. BRNAV/RNP 10/ RNP5 compliant MLG –RH - Overhual due at - Jul 17 7. Impact activated ELT 406 installed Engine - Serviceable with no reduced boro inspection interval APU - Serviceable 8. ELS/EHS Mode S modification complied For information only ANNEXURE - V Page 2 of 5 AIRCRAFT GENERAL SPECIFICATIONS AIRBUS A310-304 FREIGHTER AIRCRAFT Aircraft Identification Cargo Configuration Manufacturer Airbus Industrie Main Deck - Single Row ULDs configuration Date of Manufacture May 1986 12 (88”x125”) or 11 (96”x125”)or 5 (125”x96”) Manufacturer Serial Numbers 413 - Side by Side ULDs configuration P to F conversion date Dec 2008 14 (125”x88”) or 12 (125”x96”) + 4 (88”x125”) Original & Current Registration VT-EJI Lower lobe Fwd- 3 Pallets 88”x125”or 96”x125” Engine 2 x GE80C2 A2 Lower lobe Aft - 7 LD3 containers+ Bulk APU 1x Honeywell GTCP 331-250H Note: Detailed description on page 5 Aircraft Weights Max Taxi Weight 153900 Kgs Major Avionics/ Navigation Equipment Max Take-Off Weight 153000 Kgs Description Part Number Vendor Qty Maximum Landing Weight 123000 Kgs FAC B471ABM5 Sextant 2 Maximum Zero Fuel Weight 113000 Kgs FCC B470ADM Sextant 2 Operating EmptyWeight 76500 Kgs HF 622-5272-001 Collins 2 Structural Limited Payload 36500 Kgs VHF 822-1044-003 Collins 3 Note: FMC 745SUE4B4 Smiths 2 Payload may be limited due aircraft performance WX 622-5132-105 Collins 2 criteria and/or sector fuel requirement. DME 622-4540-001 Collins 2 ADF 622-5222-002 Collins 2 Maintenance Programme ILS 822-0282-002 Collins 2 A Check Every 500 Hrs VOR 822-0726-002 Collins 2 C Check Every 18 months EGPWS 965-0576-002 Honeywell 1 HMV Check Every 5 Yrs LRRA 9599-607-14901 Thales 2 Engine Condition Monitoring Mode S 066-01127-1402 Honeywell 2 APU On Condition TCAS II 066-50000-2120 Honeywell 1 IRU 461800-300-2203 Litton 3 Maintenance Status Airframe ( as at 02 Nov 09) Salient Features complied Total Flight Hrs 60,781 FH 1. 120 minutes ETOPS approved Total Flight Cycles 24,301 FC 2. 8.33 KHz Channel spacing compliant Next Major Check 28 Oct 09 3. FM Immunity Compliant Next HMV Apr 13 4. TCAS II compliant NLG –Overhaul due at – Apr 17 5. RVSM compliant MLG –LH - Overhual due at - Oct 17 6. BRNAV/RNP 10/ RNP5 compliant MLG –RH - Overhual due at - Oct 17 7. Impact activated ELT 406 installed Engine - Serviceable with no reduced boro inspection interval APU - Serviceable 8. ELS/EHS Mode S modification complied For information only ANNEXURE - V Page 3 of 5 AIRCRAFT GENERAL SPECIFICATIONS AIRBUS A310-304 FREIGHTER AIRCRAFT Aircraft Identification Cargo Configuration Manufacturer Airbus Industrie Main Deck - Single Row ULDs configuration Date of Manufacture Aug 1990 12 (88”x125”) or 11 (96”x125”)or 5 (125”x96”) Manufacturer Serial Numbers 538 - Side by Side ULDs configuration P to F conversion date Apr 2007 14 (125”x88”) or 12 (125”x96”) + 4 (88”x125”) Original & Current Registration VT-EQS Lower lobe Fwd- 3 Pallets 88”x125”or 96”x125” Engine 2 x GE80C2 A2 Lower lobe Aft - 7 LD3 containers+ Bulk APU 1x Honeywell GTCP 331-250H Note: Detailed description on page 5 Aircraft Weights Max Taxi Weight 153,900 Kgs Major Avionics/ Navigation Equipment Max Take-Off Weight 153,000 Kgs Description Part Number Vendor Qty Maximum Landing Weight 123,000 Kgs FAC B471ABM5 Sextant 2 Maximum Zero Fuel Weight 113,000 Kgs FCC B470ADM Sextant 2 Operating EmptyWeight 76,500 Kgs HF 622-5272-001 Collins 2 Structural Limited Payload 36,500 Kgs VHF 822-1044-003 Collins 3 Note: FMC 745SUE4B4 Smiths 2 Payload may be limited due aircraft performance WX 622-5132-105 Collins 2 criteria and/or sector fuel requirement. DME 622-4540-001 Collins 2 ADF 622-5222-002 Collins 2 Maintenance Programme ILS 822-0282-002 Collins 2 A Check Every 500 Hrs VOR 822-0726-002 Collins 2 C Check Every 18 months EGPWS 965-0576-002 Honeywell 1 HMV Check Every 5 Yrs LRRA 9599-607-14901 Thales 2 Engine Condition Monitoring Mode S 066-01127-1402 Honeywell 2 APU On Condition TCAS II 066-50000-2120 Honeywell 1 IRU 461800-300-2203 Litton 3 Maintenance Status Airframe ( as at 02 Nov 09) Salient Features complied Total Flight Hrs 52973 FH 1. 120 minutes ETOPS approved Total Flight Cycles 20554 FC 2. 8.33 KHz Channel spacing compliant Next C Check 25 Aug 10 3. FM Immunity Compliant Last HMV Jul 12 4. TCAS II compliant NLG –Overhaul due at – 21 Aug 2010 5. RVSM compliant MLG –LH - Overhual due at - 31 Jul 2014 6. BRNAV/RNP 10/ RNP5 compliant MLG –RH - Overhual due at - 31 Jul 2014 7. Impact activated ELT 406 installed Engine - Serviceable with no reduced boro inspection interval APU - Serviceable 8. ELS/EHS Mode S modification complied For information only ANNEXURE - V Page 4 of 5 AIRCRAFT GENERAL SPECIFICATIONS AIRBUS A310-304 FREIGHTER AIRCRAFT Aircraft Identification Cargo Configuration Manufacturer Airbus Industrie Main Deck - Single Row ULDs configuration Date of Manufacture Aug 1990 12 (88”x125”) or 11 (96”x125”)or 5 (125”x96”) Manufacturer Serial Numbers 544 - Side by Side ULDs configuration P to F conversion date May 2007 14 (125”x88”) or 12 (125”x96”) + 4 (88”x125”) Original & Current Registration VT-EQT Lower lobe Fwd- 3 Pallets 88”x125”or 96”x125” Engine 2 x GE80C2 A2 Lower lobe Aft - 7 LD3 containers+ Bulk APU 1 x Honeywell GTCP 331-250H Note: Detailed description on page 5 Aircraft Weights Max Taxi Weight 153900 Kgs Major Avionics/ Navigation Equipment Max Take-Off Weight 153000 Kgs Description Part Number Vendor Qty Maximum Landing Weight 123000 Kgs FAC B471ABM5 Sextant 2 Maximum Zero Fuel Weight 113000 Kgs FCC B470ADM Sextant 2 Operating EmptyWeight 76500 Kgs HF 622-5272-001 Collins 2 Structural Limited Payload 36500 Kgs VHF 822-1044-003 Collins 3 Note: FMC 745SUE4B4 Smiths 2 Payload may be limited due aircraft performance WX 622-5132-105 Collins 2 criteria and/or sector fuel requirement. DME 622-4540-001 Collins 2 ADF 622-5222-002 Collins 2 Maintenance Programme ILS 822-0282-002 Collins 2 A Check Every 500 Hrs VOR 822-0726-002 Collins 2 C Check Every 18 months EGPWS 965-0576-002 Honeywell 1 HMV Check Every 5 Yrs LRRA 9599-607-14901 Thales 2 Engine Condition Monitoring Mode S 066-01127-1402 Honeywell 2 APU On Condition TCAS II 066-50000-2120 Honeywell 1 IRU 461800-300-2203 Litton 3 Maintenance Status Airframe ( as at 02 Nov 09) Salient Features complied Total Flight Hrs 55,580 FH 1. 120 minutes ETOPS approved Total Flight Cycles 21,646 FC 2. 8.33 KHz Channel spacing compliant Next Major Check 27 Nov 10 3. FM Immunity Compliant Next HMV Dec 11 4. TCAS II compliant NLG –Overhaul due at 27 Jan 2013 5. RVSM compliant MLG –LH - Overhual due at - 12 Dec 2014 6. BRNAV/RNP 10/ RNP5 compliant MLG –RH - Overhual due at - 12 Dec 2014 7. Impact activated ELT 406 installed Engine - Serviceable with no reduced boro inspection interval APU - Serviceable 8. ELS/EHS Mode S modification complied For information only ANNEXURE - V Page 5 of 5 Weights The max structural weight limits are as follows: Max Taxi Weight : 153900 kgs Max Take off Weight : 153000 kgs Max Landing weight : 123000 kgs Max Zero Fuel weight : 113000 kgs Typical Operating Empty Weight which includes 2 Cockpit crew + 1 Cabin crew and Catering items : 76500 kgs Structural limit payload : 36500 kgs NOTE; This payload may be further limited by aircraft performance and/or sector fuel requirements Main Deck Cargo Configuration The main deck cargo compartment is equipped with an access door which is located on the forward upper left hand side of the fuselage. The door is hydraulically powered. Manual operation using a hand pump is provided in the case of a hydraulic power failure. The main deck cargo door has two opening positions (i) a horizontal and (ii) a vertical which allows loading by crane. The horizontal opening position provides a clearance between the top of the cargo loading system and the door of 3.367 m (132.6 inches). In this condition the limiting factor for the loading height is given by the cargo compartment geometry. In the fully opened position (vertical position) the relevant dimension for direct loading into the aircraft is 1.873 m (73.8 inches). The main deck cargo compartment is provided with an integrated single row/side by side cargo loading system and is capable of housing the following ULD's  Single row configurations 12 ULDs in single row configuration or 11 ULDs in single row configuration or 5 ULDs in single row configuration OR  Side by side configurations 14 ULDs in side by side configuration or 12 ULDs in side by side configuration and 4 ULDs in single row configuration OR  Mixed configurations a mix of the above mentioned ULD's. Lower lobe forward cargo compartment 3 Pallets - 88 x 125 or 96 x 125 Lower lobe aft cargo comparment LD3 containers + Bulk

f214216709 发表于 2010-8-10 12:25:05

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songsimple 发表于 2012-2-20 19:10:35

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helloplan 发表于 2013-9-22 11:30:01

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tonyblairer 发表于 2014-5-27 19:15:15

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AIRCRAFT GENERAL SPECIFICATIONS AIRBUS A310-304 FREIGHTER AIRCRAFT