A343TECH.GIF (25592 bytes) interior340.GIF (17104 bytes)
CFM56-5C
MODEL           A340-313 AIRBUS         A340-300

A/C REG.

Set.No.

Delivery

No.

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

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

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    

MAX.TAKE-OFF WGT

     Kg(lbs)

275,000

(606,271)

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

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%

  FUEL CAPACITY

(Fuel Density=2.97Kg/USG)

Kg             (lbs)  

(USG)          (Litres)

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

67,129      (147,994)

(22,602)      (85,550)

33,286        (73,363)

(11,207)      (42,420)

4,889        (10,778)

(1,846)         (6,230)

Kg               lbs     

Cruise Performance  at 20,000ft and above is based on CG position of 37%,unless otherwise stated.

TOTAL :     Kg     (lbs)   

USG (Litres)

111,032    (244,783)

(37,384)    (141,500)

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

MAX. CARGO CAPACITY:

FWD   1 

(Per hold)                                 2  

Kg                                 AFT   1 

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

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

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"

USABLE CONTAINERIZED     FWD

CARGO VOLUME (p. cmp)   AFT

cu.m (cu.ft)                         BULK

80.5            (2,841)

62.6            (2,211)

19.7               (696)

TOTAL

(LD-MCR NOT INSTALLED)

162.8            (5,748)

MAX.PAYLOAD STRUCTURAL

(MZFW-DOW)  Kg (Lbs)

43,873

(96,723)

AIRBUS Estimated:        48,194     Kg

                                   (106,250)     lbs

STATIC TAKE-OFF THRUST-Kg

(Per engine)    kN(Lbs)

15,422                   151,2

(@SL24,4C)      (34,000)

1 sq.m=    10.7639sq.ft

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)

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

RANGE with typical OWE

with: 295 Passengers

Km           n.m.

13,242      (7,150)

8,228 miles

with allowance for 200nm diversion & International reserves

OPERATIONAL NOISE LEVELS Actual EPNdB CHA-3 Limit

Total Margin EPNdB

23.6

-TKO              /Fly-Over

-Sidelines     /Lateral

-Approach    /Landing

95.0

94.7

97.2

104.0

101.6

104.9

x-5c.gif (11296 bytes)

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

- 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