AIRCRAFT GENERAL SPECIFICATIONS AIRBUS A310-304 FREIGHTER AIRCRAFT

航空

游客，如果您要查看本帖隐藏内容请回复

航空

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 [88"x125"] ULDs in single row configuration or
11 [96"x125"] ULDs in single row configuration or
5 [125"x96"] ULDs in single row configuration
OR
 Side by side configurations
14 [125"x88"] ULDs in side by side configuration or
12 [125"x96"] ULDs in side by side configuration and 4 [88"x125"] 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

谢谢哦

guanshyy

kkkkkkkkkkkkkkkkkkkkkkkkkk

songsimple

谢谢分享 拿走学习 谢谢楼主

helloplan

谢谢分享

tonyblairer

很好的资料，谢谢分享