Airbus A32X Family AOM

Transcription

A32X Family
Airman Operating Manual
Aircraft Model Provided by:
The X-Plane Freeware Project
Valid for X-Plane Versions 8.15+
FW/A32XAOM-V4
_Legal Notice
This document contains data © Airbus Industries and is only intended for
internal use. Under no circumstances may you copy this document, either in its
entirety or in parts, or make it available to anyone outside Freeworld Airways.
You may only print this document for private use.
© 2004-2005 FreeWorld Airways.
Fourth version, pulished June 20 2004
FW/A32XAOM-V4
FW/A32XAOM-V4
_Table of contents
1_ AIRCRAFT INFORMATION
1.1_ CONVERSION TABLE
2
1.2_ AIRCRAFT/ENGINE DESCRIPTIONS
2
1.3_ FUEL CAPACITY
2
1.4_ WEIGHTS
2
1.5_ ENGINE LIMITATIONS
3
1.6_ STRUCTURAL LIMITATIONS
3
1.7_ PERFORMANCE DATA & RUNWAY REQUIREMENTS
4
2_ FLIGHT CHARACTERISTICS
2.1_ DEPARTURE
2.1.1_ TAKE-OFF SPEEDS
5
2.1.2_ MAXIMUM TAKE-OFF N1
6
2.1.3_ NORMAL TAKE-OFF PATTERN
7
2.1.4_ MAXIMUM CLIMB N1
8
2.1.5_ CLIMB TABLES
9
2.2_ CRUISE
2.2.1_ RECOMMENDED /OPTIMUM/MAXIMUM CRUISE ALTITUDES
11
2.2.2_ CRUISE TABLES
13
2.3_ ARRIVAL
2.3.1_ DESCENT TABLES
15
2.3.2_ HOLDING PATTERNS
16
2.3.3_ APPROACH PROFILES (ILS/CIRCLING/VISUAL )
17
2.3.4_ LANDING SPEEDS/DISTANCES
20
2.4_ FLIGHT PLANNING
2.4.1_ FUEL MANAGEMENT DIRECTIVES
21
2.4.2_ FUEL PLANNING TABLES
23
2.4.3_ ALTERNATE PLANNING TABLES
27
3_ APPENDIXES
3.1_ APPENDIX I: NORMAL OPERATIONS CHECKLIST
© FreeWorld Airways. Reproduction and/or external use prohibited.
28
Page 1
FW/A32XAOM-V4
1_ Aircraft Infomation
1.1_ C ONVERSION
Most of the tables in this AOM are in metric units. Use the following formulas to convert
to imperial units, which are used in X-Plane.
Fuel:
6,676 lbs = 1 US gal. | 3028 kg = 1 US gal.
Weight:
1 kg = 2,2046 lbs
| 1 lb = 0,453 kg
1.2_ AIRCRAFT DESCRIPTION
-
Pilot Qualification Category:
(First officer L2)
Route Utilization Category:
(medium range)
Use CAT C for straight in approach (A321 CAT D),
CAT C for circling unless app. speed is greater than 140 KIAS, then use CAT D
ICAO Landing Capability: IIIa
A319LR ETOPS
Seating Capacity
A318-100 A319-100 A319-115LR A320-200
FreeWorld use
107
116
40/70
142
Maximum allowed
136
145
145
180
A321-200
175
220
1.3_ ENGINE DESCRIPTION
-
A318-100 .......... CFM
A319-115LR ...... CFM
A319-100 ......... CFM
A320-200 .......... CFM
A321-200 .......... CFM
56-5B8/P
56-5B7/P
56-5B6/P
56-5B4/P
56-5B3/P
rated
rated
rated
rated
rated
at
at
at
at
at
23500
23500
23500
27000
32000
lbs.
lbs.
lbs.
lbs.
lbs.
Thrust
Thrust
Thrust
Thrust
Thrust
1.4_ FUEL CAPACITY
(6,676 lbs. Per US gal.)
- Wing tanks: 4,127 US Gal. 27,500 lbs
- Center tank: 2,176 US Gal. 14,500 lbs
- Max. Fuel
6,303 US Gal 42,000 lbs (memory limitation) or 23860 L
- Maximum imbalance between left and right wing fuel tanks: 1000 lbs
NOTE: A319-115LR Extra fuel = 29680 lbs with 3ACT on cargo Total = 71680 lbs
1.5_ WEIGHTS (FWA COMPANY LIMITATIONS)
Empty weight
Max Ramp
Max Takeoff
Max Landing
Max zero fuel
A318-100
85,580 lbs 38,9 t
140,000 lbs 63,6 t
139,100 lbs 63,2 t
116,600 lbs 56,0 t
129,000 lbs 53,0 t
A319-100
86,500 lbs 39,3 t
156,100 lbs 70,9 t
155,200 lbs 70,5 t
137,800 lbs 61,0 t
129,000 lbs 57,0 t
Empty weight
Max Ramp
Max Takeoff
Max Landing
Max zero fuel
A320-200
88,900 lbs 40,4 t
162,940 lbs 74,0 t
162,040 lbs 73,60 t
142,200 lbs 64,5 t
134,000 lbs 61,5 t
A321-200
103,610 lbs 47,1 t
197,990 lbs 90,0 t
197,090 lbs 89,6 t
171,500 lbs 75,5 t
162,700 lbs 71,5 t
Page 2
A319-115LR
86,480 lbs 39,3 t
167,350 lbs 76,0 t
166,450 lbs 75,6 t
137,800 lbs 61,0 t
129,000 lbs 57,0 t
FW/A32XAOM-V4
1.6_ ENGINE LIMITATIONS
-
Max. starting EGT: 725°C
Max. continuous Temp: 915°C
TOGA Temp: 950°C (5mins)
Max. N1 Speed: 107%
1.7_ STRUCTURAL LIMITATIONS
- Flight maneuvering load acceleration limits
Clean configuration -1g to +2,5g
Slat and flaps extended 0g to +2g
- Operation limits
Maximum crosswind demonstrated for take off: 29 kts (39 kts A318)
Maximum crosswind demonstrated for landing: 33 kts (38 kts A318)
Maximum tailwind 10 kts
Maximum wind for autoland CAT II or CAT IIIB
Head wind: 30 kts
Tail wind:
10 kts
Cross wind: 20 kts
- Taxi speed
No more than 50% N1 for breakaway thrust without clearance
Max taxi speed on straightaway – 20 kts.
Max taxi speed on turns approx. 10 kts.
Minimum pavement width for 180° turn: 100’ (A321 105’)
- Maximum Operating Speed (VMO) 350 KIAS / (MMO) M.82M
- Minimum Control Speed Air - Vmca : 119 KIAS
- Minimum Control Speed Ground – Vmcg : 114 KIAS
- Maximum speed Windshield wipers in use/ 230 KIAS
- Maximum speed cockpit window open: 230 KIAS
- Max. Flaps / Slats Speeds (VFE):
LEVEL
POSITION SLATS FLAPS
Ind.
On
A318/319/320 A321
ECAM
1
230
230
FLIGHT PHASE
1
18
0
1
18
10
1+F
215
215
TAKE-OFF
2
22
15
2
200
215
3
22
20
3
185
195
FULL
27
40
FULL
177
190
TAKE-OFF/APPROACH
TAKEOFF/APPROACH/LANDING
LANDING
HOLDING
Page 3
FW/A32XAOM-V4
- Max. operating altitude with slats or slats and flaps extended is 20’000 ft (FL200)
-
Max.
Max.
Max.
Max.
Max.
Stall
Gear Extended Speed (VLE): 280 KIAS /( MLE) - M .67
Gear Operating Speed (VLO extension):
250 KIAS
Gear Operating Speed (VLO retraction):
220 KIAS
Altitude at which the landing gear may be extended: 25000ft (FL250)
Tire Speed on Ground (AFM): 195 KIAS
Speed with Full Flaps (VSO): 112 KIAS
- Turbulence penetration airspeed:
Turbulence penetration
A318/319/320
A321
At or above 20,000 ft
275 KIAS / M.76
300 KIAS / M.76
Below 20,000ft
250 KIAS
270 KIAS
-Ice & rain protection:
Engine anti-ice must be on during all ground and flight operation when icing conditions
exist, except during climb and cruise when the temperature is below –40°C SAT
1.8_ PERFORMANCE DATA
- Max. Certified Altitude: 37,000 ft
- Max. Operating Speed: 350 KIAS / M 0.82
1.9_ RUNWAY REQUIREMENTS
- Min. Take-Off Runway Length:7,220 ft
- Min. Landing Runway Length: 7,220 ft
Page 4
2,200 m
2,200 m
(at Sea Level, MTOW)
(at Sea Level, MLW)
FW/A32XAOM-V4
2_ Flight Characteristics
2.1_ DEPARTURE
2.1.1_ TAKE- OFF SPEEDS
Recommended takeoff speeds for A318/319/320/321.
WEIGHT LB
KG
197,000
190,000
180,000
170,000
160,000
155,000
89,500
86,400
81,800
77,300
72,700
70,306
CONF 1+F
V1/VR
V2
159/163
163
156/158
158
151/151
158
146/152
154
141/147
149
139/145
147
CONF 2
V1/VR
V2
166/166
168
162/162
164
156/156
160
151/151
156
147/147
151
145/145
149
CONF 3
V1/VR
V2
159/159
160
156/156
157
151/151
153
145/145
148
140/140
144
138/138
142









163
214
235
158
206
225
156
203
211
F
S
GREEN DOT
150,000
68,100
145,000
65,770
140,000
63,600
135,000
61,234
130,000
59,000
125,000
56,699
120,000
54,500
110,000
50,000
136/142
144
134/139
142
131/136
139
128/134
137
125/131
134
122/128
131
119/124
128
113/117
122
142/142
146
140/140
144
137/137
141
134/134
139
131/131
136
128/128
133
125/125
130
118/118
124
135/135
139
133/133
137
130/130
134
128/128
132
125/125
129
122/122
127
118/118
124
112/112
118
153
200
216
151
198
212
148
194
207
146
191
203
143
187
198
140
183
194
137
179
189
132
172
180
Page 5
FW/A32XAOM-V4
2.1.2_ MAXIMUM TAKE- OFF N1
NOTE: THESE ARE REAL PERFORMANCE NUMBERS, AND MAY NOT BE 100% ACCURATE IN X-PLANE
Page 6
2.1.3_ NORMAL TAKE- OFF PATTERN
FW/A32XAOM-V4
Page 7
FW/A32XAOM-V4
2.1.4_ MAXIMUM CLIMB N1
NOTE: THESE ARE REAL PERFORMANCE NUMBERS, AND MAY NOT BE 100% ACCURATE IN X-P LANE
Page 8
FW/A32XAOM-V4
2.1.5_ CLIMB TABLES
Page 9
FW/A32XAOM-V4
Page 10
FW/A32XAOM-V4
2.2_ CRUISE
2.2.1_ RECOMMENDED/OPTIMUM/MAXIMUM CRUISE ALTITUDES
MAXIMUM RECOMMENDED IN-CRUISE ALTITUDE
OPTIMUM ALTITUDES ON SHORT FLIGHTS
Page 11
FW/A32XAOM-V4
OPTIMUM AND MAXIMUM ALTITUDES
Page 12
FW/A32XAOM-V4
2.2.2_ C RUISE TABLES
Page 13
FW/A32XAOM-V4
Page 14
FW/A32XAOM-V4
2.3_ ARRIVAL
2.3.1_ DESCENT TABLES
Page 15
FW/A32XAOM-V4
2.3.2_ HOLDING PATTERNS
Max Holding Speeds and Leg Timing
Through 6000 ft.
200 KIAS, 1 min.
Above 6,000 through 14,000 ft.
230 KIAS (210 KIAS where published), 1 min.
Above 14,000 ft.
265 KIAS, 1 min. and 30 secs.
Page 16
2.3.3_ APPROACH PROFILES
FW/A32XAOM-V4
Page 17
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FW/A32XAOM-V4
FW/A32XAOM-V4
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FW/A32XAOM-V4
2.3.4_ LANDING SPEEDS / DISTANCES
VAPP DETERMINATION
-
Normal configuration:
The FMGS performs the following VAPP computation for landing in normal
configuration (CONF 3 or CONF FULL). These VAPP also apply for failure cases without
VRF
- VRF = VLS CONF FULL = 1,23 Vs CONF FULL -
WEIGHT LBS
96800
44000
105600
48000
110000
50000
114400
52000
132100
60000
140800
64000
149700
68000
158500
72000
167200
76000
318
319
CONF FULL 320
CONF FULL 321
108
108
111
-
113
113
116
-
117
117
121
117
117
122
125
121
126
126
130
125
130
134
129
138
133
137
141
3
3
CONF 3
CONF 3
113
113
115
-
118
118
120
-
123
123
125
122
128
128
130
127
126
132
135
131
137
139
135
143
139
143
147
KG
VRF
VRF
VRF
VRF
CONF FULL
VLS
VLS
VLS
VLS
CONF
CONF FULL
CONF
318
319
320
321
- VAPP = VRF or VLS + wind correction (1/3 Headwind or gust max. 15kt) -
REQUIRED LANDING DISTANCE (METERS)
WEIGHT KG
42000
46000
50000
54000
58000
62000
66000
70000
74000
78000
LBS
CONF 3
FULL
Page 20
1240
1220
1320
1220
1390 1470
1290 1360
1550
1430
1650
1510
1770
1590
1920
1670
2060
1810
2200
1930
FW/A32XAOM-V4
2.4_ Flight Planning
2.4.1_ FUEL MANAGEMENT DIRECTIVES
Page 21
FW/A32XAOM-V4
Page 22
FW/A32XAOM-V4
2.4.2_ FUEL PLANNING TABLES
Page 23
FW/A32XAOM-V4
Page 24
FW/A32XAOM-V4
Page 25
FW/A32XAOM-V4
Page 26
FW/A32XFOM-V4
2.4.3_ ALTERNATE PLANNING TABLES
Page 27
Normal operations checklist
Airbus A318/19/20/21
BEFORE START
GEAR ............................................................ DOWN/ALL GREEN
BRAKES / SUPER BRAKES ..................................................... SET
GROUND POWER UNIT (GPU) ............................... CONNECTED
BATTERY ................................................................................. ON
AVIONICS ................................................................................ ON
FUEL QUANTITY & DISTRIBUTION....................................... SET
WEIGHT & BALANCE ....................................................... CHECK
ALTIMETERS & CLOCKS ........................... SET & CROSS CHECK
EXTERIOR LIGHTS ................................................ AS REQUIRED
IFR CLEARANCE......................... OBTAINED (UNLESS ON TAXI)
FMS/GPS ..................................... PROGRAMMED / FP LOADED
TRANSPONDER....................................... STANDBY / SET CODE
DEPARTURE PROCEDURE ................................. REVIEWED/SET
VSPEEDS........................................................................... NOTED
ANTI-ICE............................................................................... OFF
_________________________________________________
PUSH-BACK
NAV LIGHTS.......................................................... AS REQUIRED
PUSH TUG ........................................................................ READY
AUXILIARY POWER UNIT (APU) ....................................... START
BLEED AIR .............................................................. SET TO ‘APU’
GROUND POWER UNIT (GPU) .............................. DISCONNECT
ATC CLEARANCE ....................................................... OBTAINED
BRAKES ......................................................................... RELEASE
_________________________________________________
ENGINE START
(When authorized engines may be started during pushback)
BRAKES (not required for start during push) ........................ SET
BEACON .................................................................................. ON
TIME ................................................................................. NOTED
ENGINE START PROCEDURE A318/19/20/21
FUEL PUMP..................................................................... ON
THROTTLE ............................................. FORWARDS/IDLE
FUEL HANDLE 1................................................... FULL/ON
ENGINE 1.................................................................. START
ENGINE GAUGES/WARNING LIGHTS ................ CORRECT
FUEL HANDLE 2................................................... FULL/ON
ENGINE 2................................................................. START
ENGINE GAUGES/WARNING LIGHTS ................ CORRECT
ENGINE N1 ............................................................. 19-22%
GENERATOR 1/2 ........................................................... ON
INVERTERS ..................................................................... ON
BLEED AIR ...................................................... SET TO ‘ALL’
AUXILIARY POWER UNIT (APU) ................................. OFF
START CHECKLIST .................................................... COMPLETE
_________________________________________________
PRE-TAXI
TAXI LIGHT ............................................................................. ON
ALTIMETERS ............................................. SET & CROSS CHECK
FLIGHT CONTROLS ........................................ FREE & CORRECT
BRAKES ......................................................................... RELEASE
_________________________________________________
BEFORE TAKEOFF
ANTI-ICE............................................................... AS REQUIRED
AUTO-BRAKES ...................................................... SET TO ‘RTO’
SPOILERS.......................................................................... ARMED
FLAPS ........................................... SET FOR TAKE-OFF (1+F/2)
AUTOPILOT ............................................. SET FOR DEPARTURE
HOLDING SHORT
LANDING LIGHTS ................................................................... ON
STROBES ................................................................................. ON
TRANSPONDER.............................................................. MODE C
CABIN .............................................................................. SECURE
TAKE-OFF TIME .............................................................. NOTED
_________________________________________________
AFTER TAKEOFF
TAXI LIGHT ........................................................................... OFF
LANDING GEAR .................................................... UP & LOCKED
AUTOPILOT ........................................................................... SET
AUTO-BRAKES ..................................................................... OFF
SPOILERS........................................................................... DOWN
FLAPS .................................................. RETRACT ON SCHEDULE
FW/CHK32X-2
CLIMB
EURO/WORLD: PASSING TRANSITION ALTITUDE
ALTIMETERS ............................... SET TO 1013 Hpa /29.92”Hg
PASSING FL100/10’000ft AMSL
LANDING LIGHTS .................................................................. OFF
STROBES ............................................................... AS REQUIRED
ENGINE PERFORMANCE.............................................. CHECKED
ALTIMETERS .................................... RESET AND CROSS CHECK
CABIN PRESSURE......................................................... CHECKED
CANADA/US: PASSING 18’000ft AMSL
ALTIMETERS ................................ SET TO 29.92”Hg /1013 HPa
_________________________________________________
CRUISE
NAVIGATION ............................................................... CHECKED
FUEL TANKS ......................................................... AS REQUIRED
ANTI-ICE .............................................................. AS REQUIRED
_________________________________________________
DESCENT
CABIN PRESSURE.............................................................. CHECK
FUEL SYSTEM ................................................................... CHECK
ANTI-ICE .............................................................. AS REQUIRED
ARRIVAL PROCEDURE ....................................... REVIEWED/SET
CANADA/US: PASSING FL180
ALTIMETERS ........................................ SET AND CROSS CHECK
PASSING FL100/10’000ft AMSL
LANDING LIGHTS ................................................................... ON
STROBES ..................................................... ON (OFF IN CLOUD)
EURO/WORLD: PASSING TRANSITION LEVEL
ALTIMETERS ....................................... SET AND CROSS CHECK”
_________________________________________________
APPROACH
CABIN.............................................................................. SECURE
FLIGHT INSTRUMENTS / HIS / OBS..................................... SET
FLAPS .................................................... EXTEND ON SCHEDULE
MDA ....................................................................................... SET
MISSED APPROACH PROCEDURE ............................. REVIEWED
_________________________________________________
LANDING
GEAR ............................................................... DOWN & LOCKED
TAXI LIGHT............................................................................. ON
FLAPS ............................................................ SET FOR LANDING
SPOILERS ......................................................................... ARMED
AUTO-BRAKES ........................................................ SET (1/2/3)
ATC CLEARANCE ...................................................... OBTAINED
_________________________________________________
AFTER LANDING
TIME................................................................................. NOTED
SPOILERS .......................................................................... DOWN
REVERSE THRUST ................................................................. OFF
FLAPS ....................................................................................... UP
TRANSPONDER ........................................................... STANDBY
STROBES ................................................................................ OFF
LANDING LIGHTS .................................................................. OFF
TAXI CLEARANCE...................................................... OBTAINED
_________________________________________________
SHUT-DOWN
BRAKES ................................................................ SET (V MODE)
TAXI LIGHT............................................................................ OFF
ENGINE 1/2 ........................................................ IDLE/CUT-OFF
SUPER BRAKES (CHOCKS) .......................................... INSERTED
ANTI-ICE ............................................................................... OFF
FUEL PUMPS .......................................................................... OFF
INVERTERS/GENERATORS.................................................... OFF
BEACON/NAV LIGHTS .......................................................... OFF
TIME................................................................................. NOTED
FUEL REMAINING ............................................................ NOTED
TRANSPONDER ............................................... code 2000 / OFF
BATTERY/AVIONICS ............................................................. OFF
FLIGHT PLAN / REPORT .................................. CLOSED / FILED

Airbus A32X Family AOM

Transcription

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