ci5233 factual report draft 20100722圖1.12-3 機身站位bs2080...
TRANSCRIPT
Microsoft Word - CI5233_Factual_report_draft_20100722.doc CI
5233
i
i
........................................................................................ iii
......................................................................................... v
1 ............................................................................. 1 1.1 ............................................................................. 1 1.2 ............................................................................. 4 1.3 .................................................................. 4 1.4 ...................................................................... 5 1.5 ............................................................................. 5
1.5.1 .......................................................................... 5 1.5.1.1 CM 1 ................................................................ 6 1.5.1.2 CM 2 ................................................................ 6 1.5.1.3 CM 3 ................................................................ 6
1.5.2 ............................................................ 7 1.5.2.1 CM 1 ................................................................ 7 1.5.2.2 CM 2 ................................................................ 7 1.5.2.3 CM 3 ................................................................ 7
1.5.3 72 ........................................... 7 1.5.3.1 CM 1 ................................................................ 7 1.5.3.2 CM 2 ................................................................ 8 1.5.3.3 CM 3 ................................................................ 9
1.6 ....................................................................... 11 1.6.1 ................................................................. 11 1.6.2 ..................................................................... 12 1.6.3 ................................................................. 13 1.6.4 ..................................................................... 13 1.6.5 ...................................................... 13
1.7 ........................................................................... 14 1.8 .................................................................... 14 1.9 .................................................................................. 15 1.10 ........................................................................... 15 1.11 ....................................................................... 15
1.11.1 .......................................................... 15 1.11.2 .......................................................... 15
ii
1.12 ..................................................... 20 1.12.1 46 .................................................... 22 1.12.2 48 .................................................... 26
1.13 ....................................................................... 27 1.14 .................................................................................. 27 1.15 ........................................................................... 27 1.16 ....................................................................... 28
1.16.1 ................................................... 28 1.16.2 ACARS RAS ........................................ 28
1.17 ....................................................................... 29 1.17.1 747-400 ACARS RAS .......... 29
1.17.1.1 ........................................................ 29 1.17.1.2 ...................................... 30 1.17.1.3 ACARS RAS ............. 30 1.17.1.4 RAM .................. 31
1.17.2 ........................................... 31 1.18 ........................................................................... 32
1.18.1 ............................................................. 32 1.18.2 AOC ......................................... 37 1.18.3 B747- 400 AOC-5 ............................... 40 1.18.4 ...................................................... 45
1.18.4.1 ................................................. 45 1.18.4.2 .................................................... 46 1.18.4.3 747-400 ................................... 47 1.18.4.4 747-400 ................... 52 1.18.4.5 747-400 ................... 53 1.18.4.6 747-400F ........................ 58
....................................................................................... 61
………………………………………………………………...63
iii
1.5-1 ............................................................ 5 1.6-1 ................................................... 11 1.6-2 .............................................................. 12 1.6-3 .............................................................. 13
iv
v
1.3-1 .. 4 1.6-1 ............................................... 14 1.11-1 CI 5233 SSFDR QAR ......................... 16 1.11-2 CI 5233 ............................................ 19 1.11-3 CI 5233 .................................................. 20 1.12-1 ................................................................ 21 1.12-2 23 1.12-3 BS2080 ... 24 1.12-4 .............................................. 24 1.12-5 ........................................... 25 1.12-6 ..................... 25 1.12-7 BS2598 APU ................ 27 1.16-1 ACARS RAS ............ 29 1.16-2 ACARS RAS . 29 1.18-1 .......................................................... 32 1.18-2 PERF INIT ................................. 34 1.18-3 THRUS LIM ................................... 35 1.18-4 TAKEOFF REF .............................. 36 1.18-5 ACARS ................................................... 41 1.18-6 AOC ...................................................................... 41 1.18-7 ................................................................... 42 1.18-8 ACARS .......................... 43 1.18-9 ACARS .......................... 43 1.18-10 ............................. 44 1.18-11 ..................................... 45 1.18-12 ............................................... 46
vi
1
2. CM 3360
for crosscheck”FMS4CDU
FMS-CDU
1.18.4.3ACARS5
2 Aircraft Communication Addressing and Reporting System
3Flight Management System
2
“- - -”FMS
FMS-CDUCM 3
6FCOMCM
FMS-CDU
RAMACARS RAS
flaps 20CM 3958°C
“6018*/37-42-5010”10/
“5932*/36-41-4911”CM 3
CM 1CM 1ACARS RAS
throttle
MAX
7Runway Analysis Manual 1.18.4.6
8 11 / 597,000 flaps 10 TO2assumed temperature57°C
9Outside Air Temperature, OAT 10 601,800 V1 137 /VR 142 /V2 150 /
11 60°C 593,200 V1 136 /VR 141 /V2 149 /
3
0650:48stick shaker
0650:51N190%104%0650:53stick
13Load Sheet 1.18.4.2
5
45 38 28
81 91 94
ATPL – AEROPLANE
302263
B747-400 97 02 20
99 12 28
B747-400 F/O 97 02 14
102 02 13
B737-800 F/O B747-400 F/O
99 08 31
99 10 31
99 10 31
12,773 35 5,720 13 3,208 15
12 922 08 795 19 763 04
90 248 36 233 22 232 46
30 88 43 88 16 72 13
7 22 24 27 25 22 24
B747-400 9,957 35 3,927 41 877 07
21 23 21
University of North Dakota, UND
83 6 85 8 B747-400 90
7 B747-400 92 3
B747-400 B747-400 9,957
12,773 3
1.5.1.2 CM 2
BAE System –
Flight Training Adelaide 91 4 29
92 6 A300-600R 94 8
B747-400 98 10 B747-400
B747-400 3,927 5,720
3
International Aviation Academy of
New ZealandIAANZ 94 3 31
95 2 B737-800 98 2
B747-400 B747-400 877
3,208 3
7
1.5.2.2 CM 2
1.5.3 72
1.5.3.1 CM 1
CM 1 99 2 28 0342
CI 5322 CM 1
2 28 1150 14 2 27
1850 CM 1 CM 1 1300 1400
1530 1530 3 1 0830
28 2300 5 6
3 1 1030
CM 1 3 1 1141 CI 5322
CM 1 3 1 1822
15 3 1 0522 CM 1
14 17 15 13
8
CM 1 1930 2330 3
2 0830 3
3 2 0830 0910 2100
3 2100
2150
CM 1 3 2 2334 CI 5321
CM 1 3 3 0709
3 2 1409 CM
1 CM 1 0810 0810 1330
2 1330 1600
3 4 0510 4
5 3 4 0510
CM 1 CM 1 2200 0500
CM 1
B747-400
2 28 24
1.5.3.2 CM 2
CM 2 99 3 1 0327 2
28 1027 CI 5233
1412 CM 2 CM 2
2300 3 2 0700 1345
9
CM 2 3 2 1635 CI 0012
3 3 0055
3 2 0755 CM 2 CM 2 0230
1 0415 1215
1630 7.5 3 4 0115
0400 0510
CM 2 CM 2 2230 0130
0700 0710 CM 2
CM 2
3 1
24
1.5.3.3 CM 3
CM 3 99 2 28 0342
CI 5322 2 28 1150
2 27 1850 CM 3 CM 3
1300 1400 1500 3 1 0700
5 2
3 1 1030
CM 3 3 1 1141 CI 5322
3 1 1822 3 1
0522 CM 3 CM 3 1930
2000 2300 3 2 0800
6 3 2 0800
1000 1930
10
CM 3 3 2 2334 CI 5321
3 3 0709
3 2 1409 CM 3 CM 3 0830
1130 1430 2330
5 2330 3 4
0130 0340 2
0340 3 4 0510
CM 3
11
1.6-1
561,110 lbs 610,000 lbs 266,201 lbs 827,311 lbs 874,999 lbs 231,501 lbs 595,811 lbs 666,001 lbs 22.8 % MAC
12
1.6-2
99 3 4 B-18723 B747-400F The Boeing Company 34266 1379 95 10 25 95 10 26 95-1036 98-10-146 98 10 16 99 10 15 15,052 39 2,508 3A Check 99 2 28 42 09 9 875,000 666,000
13
General Electric Company
CF6-80C2B1 CF6-80C2B1 CF6-80C2B1 CF6-80C2B1
706777 706149 706605 706780
95 10 24
89 6
30 92 12 12
95 10 24
38034 44
27809 07
15052 39
14
1.7
3 3 1353 3 4 0653
180 7 /
160 220 10 6,500 13,000
20,000 3 3 29.02
2100-1020-000017930CI 5233
Data Recorder, SSFDR Honeywell
980-4700-042 7333 27
16
SSFDR Thales
16 D243U316 Appendix G-285U0071-207 DFDACDFDR and AUX output Data
Frame Requirements
QAR Captain Clock
SSFDR GMT
1.11-117
SSFDR
829,760 lbs 560,960 lbs
2. 0841:17 RCTP18 0844:39
SSFDR
17 SSFDR QAR FDR QAR Stick Shaker
8Hz FDR GMT =QAR UTC +3
-0.758 =2.242 18 FDR GMT
17
10 N1
90% SSFDR QAR
2250:35 SSFDR Control Column Position
-0.1° 143 knots 2250:38
0° 149 knots
2250:43 Nose gear squat=Air
158 knots 12.15° 3 ft
2250:45 161 knots
164 knots 13 7 ft
1.11-2
2250:33 2250:36 2250:37 2250:40
4. SSFDR QAR Stick shaker
2250:48.24 2250:49.46 SSFDR
11 ft 12 ft 165 knots 163
knots-16 FPM -48 FPM
14.1° 12.7°
2250:50.24 2250:53.24 SSFDR
15 ft 38 ft 165 knots 170
knots 176 FPM 336 FPM
19 ACARS V1/VR/V2
141/147/155 knots 20 ACARS V1/VR/V2 151/166/177 knots
18
5. 2250:51 2251:07 N1 90%
104%1 4 EGT
813814828 811
6. SSFDR 1.11-3
19
20
1.12
1
BS2060BS2360300
1.12-4
1.12-5
1.12-6BS2180
U Channel Stringer Tie
1.12-5
abc1.12-7dBS2742~BS2760
27
1.13
1.16
1.16.1
99 3 12 1000 1200
V2155/
828,000
/
29
1.17.1.1
RAM
RAM
1.17.1.3 ACARS RAS
ACARS RAS
ACARS RAS
1
1. Compliance with SOP’s
Oral ExaminationPre-Flight Check
1.17.1.4 RAM
CBT 21 System Recurrent Training
Performance e-learning
RAM
RAM
Flight Management Computer,
1.18-1LNAV
VNAV
CDU
takeoff data
2. Position initialization, POS INIT, page
34
4. DEPARTURES page
5. Navigation radios, NAV RAD, page
6. Performance initialization, PERF INIT, page
7. Thrust limit, THRUST LIM, page
8. Takeoff reference, TAKEOFF REF, page
PERF INIT 1.18-2
gross weight, GR WTFUELzero fuel weight,
ZFWRESERVESCOST INDEX
cruise altitude, CRZ ALTcruise center of
gravity, CRZ CGSTEP SIZE
thrust limit page, THRUST LIM
1.18-2 PERF INIT
FMC
35
temperature, OATfull rated takeoff, TO
1percentage derate takeoff 1, TO1 2percentage
derate takeoff 2, TO2thrust reference mode
N1/EPR takeoff N1/EPR limitfull rated climb,
CLB 1percentage derate climb 1, CLB1
2percentage derate climb 2, CLB2
TAKEOFF REF, TAKEOFF
/FLAP/Acceleration height, ACC HT
engine out acceleration height, E/O ACCEL HT
36
thrust reduction, THR/wind/slope
V speeds, V1, VR, V2,trim, center of gravity, CG
/position, POS SHIFT
V FMC V1
V1MINheader line“V1MIN”data
37
FLNNN”
Rockwell Collins
/AOC
Boeing/Airbus
MTOW/V1/VR/V2
AOC B747- 400 AOC-5 USER
GUIDE
ACARSSAT
ACMSCMCMEMORY
ACARS ACARS ACARS
ACARS-APPLICATION MENU
TECHNICALATS AOCAOC CAL-5
1.18-5
AOC OPERATION
LOGPRFLIGHTENROUTE
REPORTSSENT MSGSWEATHER
REQRCVD MSGS 1.18-6
1.18-6 AOC
T/O DATAATISFLT
RELEASELOADSHEETDEPART
CLXDELAY JAPAN ATIS
AUSTRALIA ATIS 1.18-7
1.18-7
ACARS – T/O DATA REQ 1.18-8
ANTI-ICE
MELCDLAC PACKS
SEND 1.18-9
44
SITA
/QNH
V1/VR/V2
1.18-10
1.18-11 828,223 596,741
1.18-12
59
60
61
1 B-18723 2 B-18723 3 CM1 4 CM2 5 CM3 6 CM1 7 CM2 8 CM3 9 3
10 11 CM1 12 CM2 13 CM3 14 FLIGHT OPERATIONS MANUAL FOM 15 BOEING 747-400F Airplane Flight Manual AFM 16 BOEING 747-400F Airplane Flight Manual, Volume 2 17 BOEING 747-400 Flight Crew Training Manual 18 BOEING 747-400 Flight Crew Operations Manual FCOM
19 BOEING 747-400 Flight Crew Operations Manual, Volume 2 20 BOEING 747-400F Quick Reference Handbook QRH 21 B747-400 QUICK REFERENCE HANDBOOK 22 747-400 23 INSTRUCTOR MANUAL 24 FLIGHT CREW TRAINING PROGRAM 25 B747-400F 26 B747-400 AOC-5 USER GUIDE 27 B747-400 MEL/CDL 28 OP-37
29
62
30 Tail Strike 31 BOEING 747-400 FANS, Flight Management System, Pilot’s
Guide 32
i
i
........................................................................................ iii
......................................................................................... v
1 ............................................................................. 1 1.1 ............................................................................. 1 1.2 ............................................................................. 4 1.3 .................................................................. 4 1.4 ...................................................................... 5 1.5 ............................................................................. 5
1.5.1 .......................................................................... 5 1.5.1.1 CM 1 ................................................................ 6 1.5.1.2 CM 2 ................................................................ 6 1.5.1.3 CM 3 ................................................................ 6
1.5.2 ............................................................ 7 1.5.2.1 CM 1 ................................................................ 7 1.5.2.2 CM 2 ................................................................ 7 1.5.2.3 CM 3 ................................................................ 7
1.5.3 72 ........................................... 7 1.5.3.1 CM 1 ................................................................ 7 1.5.3.2 CM 2 ................................................................ 8 1.5.3.3 CM 3 ................................................................ 9
1.6 ....................................................................... 11 1.6.1 ................................................................. 11 1.6.2 ..................................................................... 12 1.6.3 ................................................................. 13 1.6.4 ..................................................................... 13 1.6.5 ...................................................... 13
1.7 ........................................................................... 14 1.8 .................................................................... 14 1.9 .................................................................................. 15 1.10 ........................................................................... 15 1.11 ....................................................................... 15
1.11.1 .......................................................... 15 1.11.2 .......................................................... 15
ii
1.12 ..................................................... 20 1.12.1 46 .................................................... 22 1.12.2 48 .................................................... 26
1.13 ....................................................................... 27 1.14 .................................................................................. 27 1.15 ........................................................................... 27 1.16 ....................................................................... 28
1.16.1 ................................................... 28 1.16.2 ACARS RAS ........................................ 28
1.17 ....................................................................... 29 1.17.1 747-400 ACARS RAS .......... 29
1.17.1.1 ........................................................ 29 1.17.1.2 ...................................... 30 1.17.1.3 ACARS RAS ............. 30 1.17.1.4 RAM .................. 31
1.17.2 ........................................... 31 1.18 ........................................................................... 32
1.18.1 ............................................................. 32 1.18.2 AOC ......................................... 37 1.18.3 B747- 400 AOC-5 ............................... 40 1.18.4 ...................................................... 45
1.18.4.1 ................................................. 45 1.18.4.2 .................................................... 46 1.18.4.3 747-400 ................................... 47 1.18.4.4 747-400 ................... 52 1.18.4.5 747-400 ................... 53 1.18.4.6 747-400F ........................ 58
....................................................................................... 61
………………………………………………………………...63
iii
1.5-1 ............................................................ 5 1.6-1 ................................................... 11 1.6-2 .............................................................. 12 1.6-3 .............................................................. 13
iv
v
1.3-1 .. 4 1.6-1 ............................................... 14 1.11-1 CI 5233 SSFDR QAR ......................... 16 1.11-2 CI 5233 ............................................ 19 1.11-3 CI 5233 .................................................. 20 1.12-1 ................................................................ 21 1.12-2 23 1.12-3 BS2080 ... 24 1.12-4 .............................................. 24 1.12-5 ........................................... 25 1.12-6 ..................... 25 1.12-7 BS2598 APU ................ 27 1.16-1 ACARS RAS ............ 29 1.16-2 ACARS RAS . 29 1.18-1 .......................................................... 32 1.18-2 PERF INIT ................................. 34 1.18-3 THRUS LIM ................................... 35 1.18-4 TAKEOFF REF .............................. 36 1.18-5 ACARS ................................................... 41 1.18-6 AOC ...................................................................... 41 1.18-7 ................................................................... 42 1.18-8 ACARS .......................... 43 1.18-9 ACARS .......................... 43 1.18-10 ............................. 44 1.18-11 ..................................... 45 1.18-12 ............................................... 46
vi
1
2. CM 3360
for crosscheck”FMS4CDU
FMS-CDU
1.18.4.3ACARS5
2 Aircraft Communication Addressing and Reporting System
3Flight Management System
2
“- - -”FMS
FMS-CDUCM 3
6FCOMCM
FMS-CDU
RAMACARS RAS
flaps 20CM 3958°C
“6018*/37-42-5010”10/
“5932*/36-41-4911”CM 3
CM 1CM 1ACARS RAS
throttle
MAX
7Runway Analysis Manual 1.18.4.6
8 11 / 597,000 flaps 10 TO2assumed temperature57°C
9Outside Air Temperature, OAT 10 601,800 V1 137 /VR 142 /V2 150 /
11 60°C 593,200 V1 136 /VR 141 /V2 149 /
3
0650:48stick shaker
0650:51N190%104%0650:53stick
13Load Sheet 1.18.4.2
5
45 38 28
81 91 94
ATPL – AEROPLANE
302263
B747-400 97 02 20
99 12 28
B747-400 F/O 97 02 14
102 02 13
B737-800 F/O B747-400 F/O
99 08 31
99 10 31
99 10 31
12,773 35 5,720 13 3,208 15
12 922 08 795 19 763 04
90 248 36 233 22 232 46
30 88 43 88 16 72 13
7 22 24 27 25 22 24
B747-400 9,957 35 3,927 41 877 07
21 23 21
University of North Dakota, UND
83 6 85 8 B747-400 90
7 B747-400 92 3
B747-400 B747-400 9,957
12,773 3
1.5.1.2 CM 2
BAE System –
Flight Training Adelaide 91 4 29
92 6 A300-600R 94 8
B747-400 98 10 B747-400
B747-400 3,927 5,720
3
International Aviation Academy of
New ZealandIAANZ 94 3 31
95 2 B737-800 98 2
B747-400 B747-400 877
3,208 3
7
1.5.2.2 CM 2
1.5.3 72
1.5.3.1 CM 1
CM 1 99 2 28 0342
CI 5322 CM 1
2 28 1150 14 2 27
1850 CM 1 CM 1 1300 1400
1530 1530 3 1 0830
28 2300 5 6
3 1 1030
CM 1 3 1 1141 CI 5322
CM 1 3 1 1822
15 3 1 0522 CM 1
14 17 15 13
8
CM 1 1930 2330 3
2 0830 3
3 2 0830 0910 2100
3 2100
2150
CM 1 3 2 2334 CI 5321
CM 1 3 3 0709
3 2 1409 CM
1 CM 1 0810 0810 1330
2 1330 1600
3 4 0510 4
5 3 4 0510
CM 1 CM 1 2200 0500
CM 1
B747-400
2 28 24
1.5.3.2 CM 2
CM 2 99 3 1 0327 2
28 1027 CI 5233
1412 CM 2 CM 2
2300 3 2 0700 1345
9
CM 2 3 2 1635 CI 0012
3 3 0055
3 2 0755 CM 2 CM 2 0230
1 0415 1215
1630 7.5 3 4 0115
0400 0510
CM 2 CM 2 2230 0130
0700 0710 CM 2
CM 2
3 1
24
1.5.3.3 CM 3
CM 3 99 2 28 0342
CI 5322 2 28 1150
2 27 1850 CM 3 CM 3
1300 1400 1500 3 1 0700
5 2
3 1 1030
CM 3 3 1 1141 CI 5322
3 1 1822 3 1
0522 CM 3 CM 3 1930
2000 2300 3 2 0800
6 3 2 0800
1000 1930
10
CM 3 3 2 2334 CI 5321
3 3 0709
3 2 1409 CM 3 CM 3 0830
1130 1430 2330
5 2330 3 4
0130 0340 2
0340 3 4 0510
CM 3
11
1.6-1
561,110 lbs 610,000 lbs 266,201 lbs 827,311 lbs 874,999 lbs 231,501 lbs 595,811 lbs 666,001 lbs 22.8 % MAC
12
1.6-2
99 3 4 B-18723 B747-400F The Boeing Company 34266 1379 95 10 25 95 10 26 95-1036 98-10-146 98 10 16 99 10 15 15,052 39 2,508 3A Check 99 2 28 42 09 9 875,000 666,000
13
General Electric Company
CF6-80C2B1 CF6-80C2B1 CF6-80C2B1 CF6-80C2B1
706777 706149 706605 706780
95 10 24
89 6
30 92 12 12
95 10 24
38034 44
27809 07
15052 39
14
1.7
3 3 1353 3 4 0653
180 7 /
160 220 10 6,500 13,000
20,000 3 3 29.02
2100-1020-000017930CI 5233
Data Recorder, SSFDR Honeywell
980-4700-042 7333 27
16
SSFDR Thales
16 D243U316 Appendix G-285U0071-207 DFDACDFDR and AUX output Data
Frame Requirements
QAR Captain Clock
SSFDR GMT
1.11-117
SSFDR
829,760 lbs 560,960 lbs
2. 0841:17 RCTP18 0844:39
SSFDR
17 SSFDR QAR FDR QAR Stick Shaker
8Hz FDR GMT =QAR UTC +3
-0.758 =2.242 18 FDR GMT
17
10 N1
90% SSFDR QAR
2250:35 SSFDR Control Column Position
-0.1° 143 knots 2250:38
0° 149 knots
2250:43 Nose gear squat=Air
158 knots 12.15° 3 ft
2250:45 161 knots
164 knots 13 7 ft
1.11-2
2250:33 2250:36 2250:37 2250:40
4. SSFDR QAR Stick shaker
2250:48.24 2250:49.46 SSFDR
11 ft 12 ft 165 knots 163
knots-16 FPM -48 FPM
14.1° 12.7°
2250:50.24 2250:53.24 SSFDR
15 ft 38 ft 165 knots 170
knots 176 FPM 336 FPM
19 ACARS V1/VR/V2
141/147/155 knots 20 ACARS V1/VR/V2 151/166/177 knots
18
5. 2250:51 2251:07 N1 90%
104%1 4 EGT
813814828 811
6. SSFDR 1.11-3
19
20
1.12
1
BS2060BS2360300
1.12-4
1.12-5
1.12-6BS2180
U Channel Stringer Tie
1.12-5
abc1.12-7dBS2742~BS2760
27
1.13
1.16
1.16.1
99 3 12 1000 1200
V2155/
828,000
/
29
1.17.1.1
RAM
RAM
1.17.1.3 ACARS RAS
ACARS RAS
ACARS RAS
1
1. Compliance with SOP’s
Oral ExaminationPre-Flight Check
1.17.1.4 RAM
CBT 21 System Recurrent Training
Performance e-learning
RAM
RAM
Flight Management Computer,
1.18-1LNAV
VNAV
CDU
takeoff data
2. Position initialization, POS INIT, page
34
4. DEPARTURES page
5. Navigation radios, NAV RAD, page
6. Performance initialization, PERF INIT, page
7. Thrust limit, THRUST LIM, page
8. Takeoff reference, TAKEOFF REF, page
PERF INIT 1.18-2
gross weight, GR WTFUELzero fuel weight,
ZFWRESERVESCOST INDEX
cruise altitude, CRZ ALTcruise center of
gravity, CRZ CGSTEP SIZE
thrust limit page, THRUST LIM
1.18-2 PERF INIT
FMC
35
temperature, OATfull rated takeoff, TO
1percentage derate takeoff 1, TO1 2percentage
derate takeoff 2, TO2thrust reference mode
N1/EPR takeoff N1/EPR limitfull rated climb,
CLB 1percentage derate climb 1, CLB1
2percentage derate climb 2, CLB2
TAKEOFF REF, TAKEOFF
/FLAP/Acceleration height, ACC HT
engine out acceleration height, E/O ACCEL HT
36
thrust reduction, THR/wind/slope
V speeds, V1, VR, V2,trim, center of gravity, CG
/position, POS SHIFT
V FMC V1
V1MINheader line“V1MIN”data
37
FLNNN”
Rockwell Collins
/AOC
Boeing/Airbus
MTOW/V1/VR/V2
AOC B747- 400 AOC-5 USER
GUIDE
ACARSSAT
ACMSCMCMEMORY
ACARS ACARS ACARS
ACARS-APPLICATION MENU
TECHNICALATS AOCAOC CAL-5
1.18-5
AOC OPERATION
LOGPRFLIGHTENROUTE
REPORTSSENT MSGSWEATHER
REQRCVD MSGS 1.18-6
1.18-6 AOC
T/O DATAATISFLT
RELEASELOADSHEETDEPART
CLXDELAY JAPAN ATIS
AUSTRALIA ATIS 1.18-7
1.18-7
ACARS – T/O DATA REQ 1.18-8
ANTI-ICE
MELCDLAC PACKS
SEND 1.18-9
44
SITA
/QNH
V1/VR/V2
1.18-10
1.18-11 828,223 596,741
1.18-12
59
60
61
1 B-18723 2 B-18723 3 CM1 4 CM2 5 CM3 6 CM1 7 CM2 8 CM3 9 3
10 11 CM1 12 CM2 13 CM3 14 FLIGHT OPERATIONS MANUAL FOM 15 BOEING 747-400F Airplane Flight Manual AFM 16 BOEING 747-400F Airplane Flight Manual, Volume 2 17 BOEING 747-400 Flight Crew Training Manual 18 BOEING 747-400 Flight Crew Operations Manual FCOM
19 BOEING 747-400 Flight Crew Operations Manual, Volume 2 20 BOEING 747-400F Quick Reference Handbook QRH 21 B747-400 QUICK REFERENCE HANDBOOK 22 747-400 23 INSTRUCTOR MANUAL 24 FLIGHT CREW TRAINING PROGRAM 25 B747-400F 26 B747-400 AOC-5 USER GUIDE 27 B747-400 MEL/CDL 28 OP-37
29
62
30 Tail Strike 31 BOEING 747-400 FANS, Flight Management System, Pilot’s
Guide 32