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FCMC Fuel Control & Monitoring Computer 1.28.10 SDCU Smoke Detection Control Unit 1.26.10
FCU Flight Control Unit 1.22.10 VENT CONT Vent Controller 1.21.30
FM Flight Management 1.22.10 WHC Window Heat Computer 1.30.40
FMGEC Flight Management Guidance Envelope Computer 1.22.10 ZONE CONT Zone Controller 1.21.10
c:\…\22AUTOFLT.doc - create: 9 January 1995 - last saved: 18 April 2006
ATTACHMENT S
Excerpts from the Airbus A300400 FCOM
FACTUAL REPORT ATTACHMENTS DCA02MA001
.. ..., .:... .. .. . .... .., 2:: .;:v
.i . .
MAXIMUM TAXI WEIGHT
WEIGHT (BRAKES RELEASE)
MAXIMUM LANDING WEIGHT
MAXIMUM ZERO FUEL
WEIGHT"
MINIMUM WEIGHT
MAXIMUM TAKE-OFF .
..... ..-.' ..... . :..: : .. !
~ KG POUNDS
172600 380580
771 700 375 590
140 000 308 700
123000 27! 210
90000 198410
........ . .
: . \ ,
I
. .
! . C... ..... t
VMCG
. . .
-
114 in 15/0 and 15/15
113 in 15/20
109.5
1 - WEIGHTWCENTER OF GRAVITY
VMCA
A. Center of gravity limits
PERCENTAGE OF THE MEAN AERODYNAMIC CHORD,
LANDING GEAR EXTENDED. THE MAC IS 6.608 METERS
LONG (260.15 INCHES). STATION 0 IS LOCATED 6.3825
METERS (251.28 INCHES) FORWARDOF FUSELAGE NOSE.
THE LIMITS OFTHE CENTER OF GRAVITY ARE GIVEN IN
120.6 in 1510and 15/15
120 in 15/20
117.0
: Aircraft Center of gravity must always be within
presented limits regardless of fuel load.
Maneuver on ground :
- When the weight is higher than 152tons
(335 160 Ib), do not exceed f 65" on nose wheel
travel during towing. - When the weight is higher than 163.5tons
(360520Ib), do not exceed a maximum taxiing
speed of 15 kt during a turn.
Code : 0030 us
8. Weight limitations
- Maximum zerofuelweight is 130 DO0 kg (286 650 Ib)
when maximum take off weight is below 170 500 kg
- M(37a5x i9m5u0m Ib-)z.e rofuelweighti s 131 300 kg (288 810 Ib)
when maximum take-off we1 ht is below 167 800 kg
(369 920 1b)providedtheTRlhtankisemptyandthe
CENTER tankdepleted (in accordance with applicable
procedure, as described in FCOM 2.06.30 p B) prior
to eke-off.
Note : Residual CTR TK FQI reading is dependant
upon aircraft pitch attirude and is nor to be
considered as part of the ZNI! unless above
180 kg (400 Lbs).
Under exceptional conditions following a take off at any
weightwithin maxtakeoff weight and max landing weight
an immediate landing is permitted provided overweight
landing procedure is adhered to.
..E xaecmbeneportrgiomennaaclilit ceieossn diwtiohenrse ainre :c ontinuance 01 flight to
destination is not possible.
-
2 - SPEED
VMCA-VMCG
I ktCAS I M IAS I
A. Maximum operating speeds
The maximum operating limit speed VMO may lot be
deliberately exceeded in any regime of flight (climb, cruise
or descent). -
VMO
u 0 CAS (KT)
GE Eng. : 80C2A5-80C2A5F R
1 .:.................................... ............................ .......................................................................................................................... ............ .................................................................................................................................................................................................................. ...... :.~.'.~:.~.~:.~:.f:,~.f:.~.f:.~:.~:.~:.~:.~:.~:.~:.:.:.~:.~:.~:.~:.~:.':.':.~:.~:.~.':.~:.~:.:.~:,~.~:,~:.~:,f:,.:,.
I I
15 0
16 15
15 20
30 40
FUQHT CREW OPERATING MANUAL 1 7 1
250 kt
215 kt
205 k
175 M
0 P E RAT1 N G LI M lTATl0 N S
AfRCRAFT GENERAL
2.01.02
I REV 22 ISEQ 8001
B. Maximum flapdslats speeds (VE)
MAXIMUM SLATS/FLAPS EXTENDED SPEEDS OR
OPERATING SPEEDS
I Maximum operating altitude : 20000 ft I I SLATS 1 FLAPS I SPEED(IAS1 I
C. Gear operating speeds
VLO are the maximum speeds at which the landing
gear may be extended or retracted :
VLE is the maximum speed with landing gear
extended :
VLO extension : 270 kt/M 0.59
: 270 kt/M 0.65
VLO retraction : 240 kt/M 0.53
D. Kruger :
If Kruger cannot be retracted, do not
E. Manual pitch trim
When operating with manual pitch trim only,
do not exceed .................. 285 WO.78 M
exceed ....................... 300 ktr0.65 M
3 - MISCELLANEOUS
A. Minimum flight crew
I THE MiNlMUM FLIGHT CREW CONSISTS OF I 2 PILOTS. -. - I , .
: i
I R. Dispatchibiliiy
For dispatch in the event of equipment failure or missing
parts, refer to MEUCDL.
C. Fiight maneuvering load acceleration limits : .
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