| MODEL A340-313 | AIRBUS A340-300 | A/C REG. |
Set.No. |
Delivery |
No. |
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| ENGINE TYPE/ THRUST : CFM A/C REG./No.of Eng: |
CFM56-5C4
34.000 SX-DFA,DFB 4 |
SX-DFA SX-DFB |
235 239 |
Nov-98 Nov-98 |
DELPHI OLYMPIA |
1 2 |
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| Thrust/Weight
Ratio: (T/W) Wing Loading: (W/S) lb/sqft |
0.2236 155.6 lb/sqft |
CABIN CONFIG:32C/267Y | ||||||
Cabin Comp. ROWS PAX C/A'S CLASS |
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| MAX.TAXI GROSS WGT Kg(lbs) (T/W)Ratio: |
275,900 (608,255) |
ZONE A 1
- 6 32 3
C ZONE B 7 - 24 140 4 Y ZONE C 25 - 33 72 0 Y ZONE D 34 - 41 55 5 Y |
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| MAX.TAKE-OFF WGT Kg(lbs) |
275,000 (606,271) |
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| MAX.LANDING WGT Kg(lbs) |
190,000 (418,878) |
TOTALS 299 12 | ||||||
| MAX.ZERO FUEL WGT Kg(lbs) |
178,000 (392,422) |
Certified for GPS
satellite navigation by JAA January 1994 |
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| DRY OPERATING WEIGHT/INDEX: 3CREW,12C/As Kg(lbs)Long Range |
134,127 102.93 (295,699) 34.0 % |
A/C
WEIGHT EMPTY : 127,605 Kg Date(16.09&04.11.98) INDEX= 89.23 CG in % MAC= 31.58% |
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| FUEL
CAPACITY (Fuel Density=2.97Kg/USG) |
Kg (lbs) (USG) (Litres) |
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| Outer Tanks L/R
------>
Inner Tanks L/R ------->
Center Tanks L/R ------>
Horz.Stab.Trim Tank ------>
|
5,726
(12,628) (1,929) (7,300) |
1 USG = 2.97 Kg 1 USG = 6.7 lb Fuel Density= 2.970 Kg/USgal or FUEL DENSITY = 0.785 Kg/lit @ 3.7841 lit/USgal |
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| 67,129
(147,994) (22,602) (85,550) |
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| 33,286
(73,363) (11,207) (42,420) |
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| 4,889
(10,778) (1,846) (6,230) |
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Kg lbs |
Cruise Performance at 20,000ft and above is based on CG position of 37%,unless otherwise stated. |
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TOTAL : Kg (lbs) USG (Litres) |
111,032 (244,783) (37,384) (141,500) |
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| AVERAGE
FUEL CONSUMPTION Cruise=35,000ft,M=0.82, VKTAS=470 ,4 engines |
Kg/hr (lbs/hr) 6 ,849 (15,099) (USG/hr) (2,305) |
SAR avg=0.0691 nm/kg FFlow=VKTS/SAR=(nm/hr)/(nm/kg)=kts/(nm/kg) Fuel Flow= 6,849 Kg/hr VKTAS=474.1 |
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| MAX. CARGO
CAPACITY: FWD 1 (Per hold) 2 Kg AFT 1 2 BULK 5 |
LD3 Based 9,522 19,044 |
Max.Cap-Kg
22,861 |
CARGO
Holds House: 6xLD3 or 2x(88"x125")pallets 1,587 Kg/LD3 pallete 12xLD3 or 2x(88"x125")pallets 4,626 Kg/pallete |
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9,522 9,522 3,468 |
18,507 3,468 |
6xLD3 or
2x(88"x125")pallets LD-MCR installed* 6xLD3 or 2x(88"x125")pallets *Installation of the LD-MCR induces a loss of one 88"/96" pallet or 2 LD3 containers |
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Combined Max.Capacity: Kg FWD+AFT+BULK |
44,836 cu.m cu.ft |
CARGO
Usable Volume data: Characteristics LD3 container PALLET Dimensions STD 88"x125" Volume/Item 4.47 10.52 No. of Items 30 10 Total volume* 153.8 124.9 LD3-->NAS 3610-2% , 60.4"&61.5" |
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| USABLE
CONTAINERIZED FWD CARGO VOLUME (p. cmp) AFT cu.m (cu.ft) BULK |
80.5 (2,841) 62.6 (2,211) 19.7 (696) |
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TOTAL (LD-MCR NOT INSTALLED) |
162.8 (5,748) |
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MAX.PAYLOAD STRUCTURAL (MZFW-DOW) Kg (Lbs) |
43,873 (96,723) |
AIRBUS Estimated:
48,194 Kg (106,250) lbs |
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STATIC TAKE-OFF THRUST-Kg (Per engine) kN(Lbs) |
15,422 151,2 (@SL24,4C) (34,000) |
1 sq.m= 10.7639sq.ft |
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OVERALL LENGTH m(ft) WING AREA sqm(sqft) WING SPAN m(ft) HEIGHT |
63.65 (208.8) 363.1 (3,908.4) 60.3 (197.8) 16.74 (54.9) |
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| CRUISING SPEED @ 35.000ft
ISA @M=0.82 Km/hr (kts) CRUISING ALTITUDE in (ft) |
875 (472.6) 8,230 to 15,550 (27 to 51,000ft) |
Max. Operating Speed: Mmo=0.86 1knot = 1.852 km/h |
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| RANGE with typical OWE with: 295 Passengers |
Km
n.m. 13,242 (7,150) 8,228 miles |
with allowance for 200nm diversion & International reserves |
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| OPERATIONAL NOISE LEVELS | Actual EPNdB | CHA-3 Limit | Total Margin EPNdB 23.6 |
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| -TKO
/Fly-Over -Sidelines /Lateral -Approach /Landing |
95.0 94.7 97.2 |
104.0 101.6 104.9 |
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| CFM56-5C2 | -5C3 | -5C4 | |
| Takeoff conditions (sea level) | |||
| - Max. takeoff (lb) | 31,200 | 32,500 | 34,000 |
| - Airflow (lb/sec) | 1,027 | 1,045 | 1,065 |
| - Bypass ratio | 6.6 | 6.5 | 6.4 |
| In-flight
performance (installed) (35,000 ft-Mach=0.80-ISA) |
Lufthansa and O.A. are using the -5C with their 340s at M0.82 |
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| - Max. climb thrust (lb) | 7,370 | 7,370 | 7,580 |
| - Overall pressure ratio at max. climb | 37.4 | 37.4 | 38.3 |
| - Max. cruise thrust (lb) | 6,910 | 6,910 | 7,100 |
| Engine characteristics | |||
| - Length (in) | 103 | 103 | 103 |
| - Fan diameter (in) | 72.3 | 72.3 | 72.3 |
| - Basic dry weight (lb) | 8,796 | 8,796 | 8,796 |
| Applications | A340-200 A340-300 |
A340-200 A340-300 |
A340-200 A340-300 |